Eagle PDF
Eagle PDF
Model: 5000i
Start Date: 05/01/1999
Model: 9100i
Start Date: 05/01/1999
Model: 9200i
Start Date: 05/01/1999
Model: 9400i
Start Date: 05/01/1999
Model: 9900i
Start Date: 05/01/1999
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06/26/2002
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Copyright © 06/26/2002 International Truck and Engine Corporation
TRUCK SERVICE MANUAL i
Table of Contents
INTRODUCTION. .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .1
SAFETY INFORMATION.. . .. .. .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. .. .. . .. .. .. .. . .2
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ii TRUCK SERVICE MANUAL
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TRUCK SERVICE MANUAL 1
INTRODUCTION
Use with Circuit Diagram Book CTS-5298 or S08225.
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SAFETY INFORMATION
IMPORTANT – Read the following before starting the service procedure.
The information contained in this International Service Manual Section was current at the time of printing
and is subject to change without notice or liability.
You must follow your company safety procedures when you service or repair equipment. Be sure to understand
all of the procedures and instructions before you begin work on the unit.
International uses the following types of notations to give warning of possible safety problems and to give
information that will prevent damage to the equipment being serviced or repaired.
WARNING – A warning indicates procedures that must be followed exactly. Personal injury
or possible death can occur if the procedure is not followed.
CAUTION – A caution indicates procedures that must be followed exactly. If the procedure is not
followed, damage to equipment or components can occur.
NOTE – A note indicates an operation, procedure or instruction that is important for correct service.
Some procedures require the use of special tools for safe and correct service. Failure to use these special
tools when required can cause injury to service personnel or damage to vehicle components.
This service manual section is intended for use by professional technicians, NOT a “do-it-yourselfer.” It is
written to inform these technicians of conditions that may occur on some vehicles, or to provide information
that could assist in the proper service of a vehicle. Properly trained technicians have the equipment, tools,
safety instructions, and know-how to do a job properly and safely. If a condition is described, DO NOT assume
that the service section applies to your vehicle. See your International Truck Dealer for information on whether
this service section applies to your vehicle.
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Group ELECTRICAL
Table of Contents
1. DESCRIPTION. .. . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . ..5
1.1. POWER DISTRIBUTION SYSTEM. .. . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . ..5
1.2. GROUND SYSTEM. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . ..5
2. OPERATION.. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .5
2.1. COMMON SYSTEM COMPONENTS. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . .. . .. .. . .5
Fuses And Circuit Breakers. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .5
Junction Adapters And Studs. .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . ..5
Relays And Solenoids. . .. . . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . . . . . .. . . . . . . .. .6
2.2. BATTERY POWER DISTRIBUTION (WITHOUT 3+1 BATTERY SYSTEM). . . . . . . . . . . . . . . . . . . . . . . . .6
2.3. IGNITION POWER.. .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. . .6
2.4. ACCESSORY POWER. .. . .. . .. . . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . ..6
2.5. START POWER.. . . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . ..6
2.6. VEHICLE GROUND SYSTEM.. .. . .. . .. . .. .. . .. . .. .. . .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. . .. .. . .. . .. .. . .. . .. . .6
2.7. 3+1 BATTERY SYSTEM. . .. . . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . . ..6
Engine Running Mode. . . .. . . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . ..7
Engine OFF Mode.. . .. .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. .. . .. .. . .7
3. TROUBLESHOOTING. .. . . .. . . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . ..7
3.1. GENERAL TROUBLESHOOTING. .. . .. .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. . .7
3.2. TESTING 3 +1 BATTERY SYSTEM. .. . . . . . . . . . .. . . . . . . . . .. . . . . . . . . . .. . . . . . . . . . .. . . . . . . . . . .. . . . . . . . . . .. . .8
3.3. TESTING IGNITION POWER DISTRIBUTION SYSTEM. .. .. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. . .. .. .9
4. COMPONENT LOCATIONS. .. .. . .. . .. .. . .. .. . .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. . .. .. . .. .. . .. . .9
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1. DESCRIPTION
1.1. POWER DISTRIBUTION SYSTEM
The power distribution system provides power to the key switch, the starter solenoid, and the (B1) and (B2)
battery studs. The 150 amp. megafuse, which must be replaced when blown, supplies power to the (B1) and
(B2) battery studs. Power from the (B1) and (B2) battery studs is then distributed to the fuse block and
individual fused circuits. Fuse F7-A is located in the feed circuit for the key switch and provides protection
for the key switch and any unfused circuits attached to the key switch.
2. OPERATION
Refer to the 12V POWER DISTRIBUTION circuit diagrams in CTS-5298 or S08225.
CAUTION – Never replace a fuse or circuit breaker with a higher load rated fuse or circuit breaker.
Fuses are standard (Type III circuit breakers are optional), except for headlights and windshield wipers, which
have Type I circuit breakers.
Most of the fuses and/or circuit breakers are located in the Power Distribution panel in the cab. The Power
Distribution panel cover contains a listing of installed circuit protection devices, size and location.
Type III circuit breakers open if current flow exceeds the rated capacity and can be reset by depressing the
reset button on the breaker after the overload condition has been removed.
Type I circuit breakers (headlights and windshield wipers) reset automatically. However, if the excessive
current flow condition causing the breaker to open is not corrected, the circuit breaker will reopen and
remain open until the winding cools, then automatically reset. With an overload condition present, the
circuit breaker will cycle (open and close) until the condition is corrected. The circuit breaker will become
hot to the touch.
NOTE – Type I circuit beakers must only be replaced with approved Navistar Type I circuit breakers.
In the circuit diagrams, bussed adapters and studs are most often, but not always, given a name such as (B2)
Battery Adapter (498), etc. These junction connections can be either feeds or grounds and are identified as
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6 1 POWER DISTRIBUTION AND GROUND SYSTEM
such. The bus adapters have a common feed or ground and the other terminals are connected internally by
a bus bar.
Relays and solenoids are switching devices. International uses only suppressed relays and solenoids to
prevent voltage spikes from damaging electronic components in the vehicle electrical system. Once a
transistor has been "spiked," it may not fail immediately, but its life will be shortened.
Note that relays used inside the cab are not sealed, but relays in less protected areas, such as the engine
compartment, are sealed for longer life.
NOTE – Only replace relays and solenoids with correct International parts.
A. Energizes the accessory adapter relay (145), applying power to A3 accessory adapter (501).
B. Flows to A1 Accessory Adapter (499) and to the Electric Wiper Intermittent Relay.
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With the engine running, power (7 volts) from the alternator “R” terminal energizes the isolated battery magnetic
switch, closing the contacts. This links the positive terminal of the deep cycle and cranking motor batteries,
recharging all four batteries and supplying power from all four batteries to both the (B1) and (B2) battery studs.
The deep cycle battery supplies power to components receiving power from the (B2) battery stud.
The three cranking batteries supply power to the components receiving power from the (B1) stud.
3. TROUBLESHOOTING
Refer to the 12V POWER DISTRIBUTION circuit diagrams in CTS-5298 or S08225.
A. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of
charge (SOC) or higher. This represents an open circuit voltage (OCV) of 12.4 volts. Batteries
with an OCV of 12 volts or less are either completely discharged or have a dead cell.
B. Before beginning these test procedures, check any light or indicator lamp filaments that are
suspected of being open (burned out). This is done to avoid unnecessary extensive circuit checks.
C. Before beginning these test procedures, inspect all connectors for loose or damaged pins,
wires, etc. Refer to TEST EQUIPMENT AND CONNECTOR REPAIR section in GROUP 08 -
ELECTRICAL in the CTS-5000 Master Service Manual.
D. When the technician determines that a fuse is blown, while checking its condition, he is directed
to locate the cause of the overload condition and to repair it. While no further instruction on this
procedure is listed in the diagnostic tables, the common procedure is as follows: isolate sections
of the circuit by disconnecting connectors, and measure the resistance to ground to find the circuit
that is shorted to ground. Then locate the damaged spot in the wire or connector and repair.
E. Diagnostics for circuits that are malfunctioning by sticking in the on position are generally not
covered in detail. It is assumed that the technician knows to check for a malfunctioning switch,
relay, or solenoid.
If this does not assist in correcting the problem, proceed to the section(s) that provide detailed troubleshooting
guide for the specific circuits.
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4. COMPONENT LOCATIONS
(B1) Battery Stud. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . . Power Distribution Panel
(B2) Battery Stud. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . . Power Distribution Panel
(1) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Left Side of Engine Cowl
(2) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Right Side of Engine Cowl, Above Conn. 3
(3) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Right Side of Engine Cowl, Below Conn. 2
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1. 150A MEGAFUSE
2. TO (B1) BATTERY STUD
3. START MAG SWITCH
4. NO BUS BAR WITH 3+1 BATTERY SYSTEM
5. TO HEATER
6. (3) ENGINE HARNESS CONNECTOR
7. (2) CHASSIS HARNESS CONNECTOR
8. RIGHT HAND DASH GROUND STUD
9. FUSE BLOCK GROUND STUD
10. (B2) BATTERY STUD
11. (B1) BATTERY STUD
12. KEY SWITCH
13. LEFT HAND DASH GROUND STUD
14. (1) FRONT END HARNESS CONNECTOR
15. GROUND CIRCUITS
16. DASH PANEL
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Figure 2 Cab Wiring (Power Distribution Center/Fuse Panel) (B1) and (B2) Battery Stud
1. CIRCUIT 14A FROM START MAG SWITCH
2. 3+1 CAB HARNESS CONNECTS TO 3+1 ENGINE HARNESS
3. CIRCUIT 14A FROM 3+1 MAG SWITCH
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Table of Contents
1. DESCRIPTION.. . .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. ..21
1.1. CIGAR LIGHTER (CAB).. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . ..21
1.2. CLOCK (CAB).. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. .21
1.3. ELECTRIC WINDOW - RIGHT. .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. . .. .. . ..21
1.4. ELECTRIC WINDOW - RIGHT AND LEFT. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. .21
1.5. DEFROSTER FANS. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. . .. .. . ..21
1.6. ELECTRIC WINDSHIELD WIPERS — INTERMITTENT WIPE AND WASH. . . . . . . . . . . . . . . . . . . . . . .21
1.7. ELECTRIC HORN. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. .21
1.8. MIRRORS - HEATED AND LIGHTED.. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. . .. .. .. ..21
1.9. MIRRORS - MOTORIZED. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . .. . .21
1.10. C.B. RADIO CAB POWER SOURCE. .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. ..21
1.11. C.B. RADIO ACCOMMODATION PACKAGE. . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . .22
1.12. CAB RADIO AND SPEAKERS.. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . ..22
1.13. OWNER/OPERATOR SPARE SWITCH. .. . . .. . . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. .22
1.14. ELECTRIC LOCK - RIGHT AND LEFT.. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. ..22
1.15. INTERVISION DISPLAY. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. ..22
1.16. EATON VORAD COLLISION AVOIDANCE EVT-300. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. ..22
1.17. TEMPERATURE/COMPASS DISPLAY.. .. . .. .. .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. ..22
1.18. ROAD RELAY IV.. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .. .22
1.19. HEATED SEAT-DRIVER.. . . . . . . .. . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . . . . . .. . . . .22
1.20. HEATED SEAT-PASSENGER.. . . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . . .. . .. . . .. . .. .22
2. OPERATION. .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. .22
2.1. CIGAR LIGHTER (CAB).. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . ..23
2.2. CLOCK (CAB).. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. .23
2.3. ELECTRIC WINDOW - RIGHT (ONLY). .. . . . .. . . . . .. . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . .23
Window Down Operation. . . . . . .. . . . . . . . . .. . . . . . . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . . . .. . . . . .23
Window Up Operation. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. .23
2.4. ELECTRIC WINDOW - RIGHT AND LEFT. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. .23
Right Window Down Operation. .. . . .. . .. . . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . . .. . .. .23
Right Window Up Operation. .. .. . .. .. .. .. . .. .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. ..24
Left Window Down Operation.. . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .24
Left Window Up Operation.. . .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. ..24
2.5. DEFROSTER FANS. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. . .. .. . ..24
2.6. ELECTRIC WINDSHIELD WIPERS - INTERMITTENT WIPE AND WASH. .. . .. . .. . .. . .. . .. . .. . .. .24
Two Speed Wiper With Intermittent Wiper And Washer Operation. . . . .. . . . . . . .. . . . . . . .. . . . .24
2.7. ELECTRIC HORN. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. .26
2.8. MIRRORS - HEATED AND LIGHTED.. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. . .. .. .. ..26
2.9. MIRRORS - MOTORIZED. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . .. . .26
2.10. C.B. RADIO CAB POWER SOURCE. .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. ..26
2.11. C.B. RADIO ACCOMMODATION PACKAGE. . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . .26
2.12. CAB RADIO AND SPEAKERS.. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . ..26
2.13. OWNER/OPERATOR SPARE SWITCH. .. . . .. . . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. .27
With Fuse. .. . . .. . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. .27
Without Fuse.. . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. .27
2.14. ELECTRIC LOCK - RIGHT AND LEFT.. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. ..27
2.15. INTERVISION DISPLAY. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. ..27
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3. TROUBLESHOOTING. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .28
3.1. TESTING CIGAR LIGHTER (CAB). .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .28
3.2. TESTING CLOCK (CAB). . . .. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .29
3.3. TESTING ELECTRIC WINDOW - RIGHT.. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .30
3.4. TESTING ELECTRIC WINDOW - RIGHT AND LEFT. .. . .. .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .32
3.5. TESTING DEFROSTER FAN(S).. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .37
3.6. TESTING WINDSHIELD WIPER AND WASHER SYSTEM. . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . .38
3.7. TESTING ELECTRIC HORN. .. . . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .42
3.8. HEATED AND LIGHTED MIRRORS. . . . . .. . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . ..43
Testing Heated Mirrors. . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . ..43
Testing Mirror Lights. . . . . . . .. . . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . . .. . . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . . .. .44
3.9. MOTORIZED MIRRORS.. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .45
Testing Right Motorized Mirror. . . . . . . .. . . . . . . . . . . . . .. . . . . . . . . . . . . .. . . . . . . . . . . . . .. . . . . . . . . . . . . . .. . .45
Testing Dual Axis Motorized Mirrors.. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .47
3.10. TESTING CB POWER SOURCE. .. .. . .. .. .. .. . .. .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. .49
3.11. TESTING RADIO-CB ACCOMMODATION PACKAGE. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .50
3.12. TESTING RADIO-CAB SPEAKERS.. .. . .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .51
3.13. TESTING OWNER/OPERATOR SPARE SWITCH (FUSED). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .54
3.14. TESTING OWNER/OPERATOR SPARE SWITCH (NON-FUSED). . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .55
3.15. TESTING ELECTRIC LOCK – RIGHT AND LEFT. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . . .56
3.16. TESTING INTERVISION CIRCUITS. . . .. . . . .. . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . ..59
3.17. TESTING EATON VORAD COLLISION AVOIDANCE EVT-300 CIRCUITS. . . . . . . . . . . . . . . . . . . . . .61
3.18. TESTING TEMPERATURE/COMPASS DISPLAY CIRCUITS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .63
3.19. TESTING ROAD RELAY IV CIRCUITS. .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .64
3.20. TESTING HEATED SEAT-DRIVER. . . . .. . . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . ..65
3.21. TESTING HEATED SEAT-PASSENGER. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. . .. . .. . .66
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1. DESCRIPTION
1.1. CIGAR LIGHTER (CAB)
The Cigar Lighter circuit provides power to the Cigar Lighter or other item plugged into the lighter socket. The
socket is located to the right of the driver at the base of the wing panel.
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2. OPERATION
Refer to CAB ACCESSORIES circuit diagrams in CTS-5298 or S08225.
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With the window switch in the down position, power from switch terminal 5 is applied to the motor on circuit
83L. Circuit 83M from the motor to the switch terminal 2 becomes the ground circuit. With the switch in the
down position, switch terminals 2 and 1 are connected, completing the path to ground.
Window Up Operation
With the window switch in the up position, power from switch terminal 2 is applied to the motor on circuit 83M.
Circuit 83L from the motor to the switch terminal 5 becomes the ground circuit. With the switch in the up
position, switch terminals 5 and 6 are connected, completing the path to ground.
With the passenger’s side switch (1041) in the neutral position and the driver’s side right window switch (1040)
in the down position, power from switch terminal 5B is applied to the motor on circuit 83J through terminals 6
and 5B of switch (1041) to circuit 83M. Circuit 83L from the motor, through switch (1041) terminals 2B and 1,
circuit 83K to switch (1040) terminal 2B becomes the ground circuit.
With the passenger’s side switch in the down position, power from terminal 5B is applied to circuit 83M. Ground
is supplied on circuit 83L through switch (1033), circuit 83K, and switch (1040) from circuit 83-GB.
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With the passenger’s side switch (1041) in the neutral position and the driver’s side right window switch (1040)
in the up position, power from switch terminal 2B is applied to the motor on circuit 83K through terminals 1
and 2B of switch (1041) to circuit 83L. Circuit 83M from the motor, through switch (1041) terminals 5B and 6,
circuit 83J to switch (1040) terminal 5B becomes the ground circuit.
With the passenger’s side switch in the up position power from terminal 2B is applied to circuit 83L. Ground is
supplied on circuit 83M through switch (1033), circuit 83J, and switch (1040) from circuit 83-GB.
With the window switch in the down position, power from switch terminal 4 is applied to the motor on circuit
83N. Circuit 83F from the motor to the switch terminal 1 becomes the ground circuit. With the switch in the
down position, switch terminals 2B and 1 are connected, completing the path to ground.
With the window switch in the up position, power from switch terminal 1 is applied to the motor on circuit 83F.
Circuit 83N from the motor to the switch terminal 4 becomes the ground circuit. With the switch in the up
position, switch terminals 2B and 4 are connected, completing the path to ground.
If held more than one second wiper speed increases directly to high.
Down If wiper is off, turns wiper on to low speed.
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If held more than one second wiper enters it’s longest delay mode.
Bottom Button In If pressed less than 1/2 second, wiper performs a single lowspeed dry
(WASH) wipe (mist function).
If pressed and held more than 1/2 second, wiper continues in low speed
and washes for 2 seconds or until released (whichever occurs later).
After release wiper continues to cycle in low speed for 3 seconds, then
wiper returns to previous state.
The electric windshield wiper with intermittent wipe and wash switch (1171) is an electronic device which
controls the wiper relays and the washer pump depending on how the switch and washer button are pressed.
Ignition switched power — With the ignition switch on power from 10 amp fuse F10-B is applied to wiper-low
speed delay relay (143) terminal 86, wiper-high speed delay relay (143) terminal 86, and windshield washer
w/wiper delay switch (1171) terminal 1.
Battery power — Battery power from 15 amp fuse F4-D is applied to wiper-high speed delay relay (143)
terminal 30, windshield washer pump (9) on circuit 87B, and windshield wiper motor connector (430) terminal A.
Low Speed Wiper Operation — When the wiper switch selects low wiper speed, a ground from the wiper
switch (1171) terminal 3 is applied to wiper- low speed relay (143) terminal 85. This energizes the relay
applying 12 volts from the closed contacts of high – speed relay (142) terminal 87 to the low speed winding of
the wiper motor through connector (430) terminal D.
High Speed Wiper Operation — When the wiper switch selects high wiper speed, a ground from the wiper
switch (1171) terminal 4 is applied to wiper- high speed relay (142) terminal 85. This energizes the relay
applying 12 volts from terminal 87 to the high speed winding of the wiper motor through connector (430)
terminal E.
The wiper switch also energizes the low speed relay (143), with a ground on circuit 82B, to open the park
circuits and prevent 12 volts from being applied to the low speed winding of the wiper motor.
Park Operation — Note that power is always present at the P terminal of the crank motor. When the wipers
are turned off and the wiper blades are not parked, the circuit between wiper motor P and S is closed. In this
position, power at P goes through the contacts and out S, through the normally closed contacts of the wiper
relay (143) and back to the low speed winding of the wiper motor. The motor continues to operate until the
park switch rotates, opening the circuit between terminal S and P, and closing the circuit between S and X,
parking the wipers and turning off operation.
Windshield Washer Operation — When the wiper switch selects the windshield washer, ground from switch
(1171) is applied from terminal 5 to circuit 87A of the washer pump motor.
Intermittent Wiper/Wash Operation — The electronic wiper switch (1171) controls the washer and the low
and high speed wiper circuits to perform intermittent wiping and washing as requested.
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Mirror Lights — Power to the mirror lights is controlled by the cab and trailer lights relay (464–R9). Refer to
LIGHT SYSTEMS for that system. Power from cab and trailer lights relay (464–R9) is applied to 15A fuse
F8-C, which supplies power to operate the mirror lights.
Dual Axis Motorized Mirrors — The dual axis motorized mirror switch 1137 receives power from ignition
relay (462–R1), through 10A fuse F5–A, on circuit 78C, through connector (1137), when the key is in the
on or accessory position. Twisting the mirror control switch knob selects which mirror will be controlled.
Positioning the L/R switch to the Left or Right position will cause the controlled mirror to move to the Left or
Right. Positioning the U/D switch to the Up or Down position will cause the controlled mirror to move Up or
Down. Ground for the circuits is supplied from GND Adapter (456) on circuit 78–GA through connector (1137).
Use the DUAL AXIS MOTORIZED MIRROR circuit diagrams in CTS-5298 or S08225 to determine which
circuits are energized to move the mirrors.
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This option provides switched battery power on circuit 14AQ for owner/operator connections. Power from the
(B2) battery stud is applied, through 30A fuse F10–A, to the spare accessory relay (167) common terminal.
With the key switch in the on or accessory position the relay is energized applying the power to the spare
accessory switch (517). When switch 517 is turned on, power is applied to circuit 14AQ.
Without Fuse
This option provides switched battery power on circuit 14AQ for owner/operator connections directly through
the spare accessory switch (517).
When driver switch (1042) or passenger switch (1043) are pushed to the unlock position, a ground from ground
adapter (456) will be applied through terminal 2B and terminal 3 of the actuated switch to terminal 86 of the
power lock relay – unlock (1140). This will energize the relay, applying 12 volts to terminal 30 of the relay,
circuits 81H, 81K and 81J to the left and right power locks. A ground from de-energized power lock relay (1139)
will be on terminal 30, circuit 81D, 81E and 81F to the left and right power locks. This will unlock the doors.
When driver switch (1042) or passenger switch (1043) are pushed to the lock position a ground from ground
adapter (456) will be applied through terminal 2B and terminal 1 of the actuated switch to terminal 86 of the
power lock relay (1139). This will energize the relay, applying 12 volts to terminal 30 of the relay, circuits 81D,
81E and 81F to the left and right power locks. A ground from de-energized power lock relay – unlock (1140)
will be on terminal 30, circuit 81H, 81J and 81K to the left and right power locks. This will lock the doors.
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3. TROUBLESHOOTING
Refer to the CAB ACCESSORIES circuit diagrams in CTS-5298 or S08225 for the following discussion.
A. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of
charge (SOC) or higher. This represents an open circuit voltage (OCV) of 12.4 volts. Batteries
with an OCV of 12 volts or less are either completely discharged or have a dead cell.
B. Before beginning these test procedures, check any light or indicator lamp filaments that are
suspected of being open (burned out). This is done to avoid unnecessary extensive circuit checks.
C. Before beginning these test procedures, inspect all connectors for loose or damaged pins, wires,
etc. Refer to section in GROUP 08 - ELECTRICAL in the CTS-5000 Master Service Manual.
D. When the technician determines that a fuse is blown, while checking its condition, he is directed
to locate the cause of the overload condition and to repair it. While no further instruction on this
procedure is listed in the diagnostic tables, the common procedure is as follows: isolate sections
of the circuit by disconnecting connectors, and measure the resistance to ground to find the circuit
that is shorted to ground. Then locate the damaged spot in the wire or connector and repair.
E. Diagnostics for circuits that are malfunctioning by sticking in the on position are generally not
covered in detail. It is assumed that the technician knows to check for a malfunctioning switch,
relay, or solenoid.
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4. COMPONENT LOCATIONS
B1 Battery Stud.. . .. .. . .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . . . . . Power Distribution Panel
B2 Battery Stud.. . .. .. . .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . . . . . Power Distribution Panel
(9) Washer Pump.. . .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . . . . . Washer Bottle
(20) Horn Connector. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Frt Engine Crossmember
(76) Horn (Inline). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Front End Harness at Lower Left, Radiator
(142) Wiper High Speed Delay Relay. . . . . . . . . . . . . . .. . . . . . Power Distribution Panel
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Figure 5 Instrument Panel Installation Showing Cigar Lighter and Aux. Power Source
1. WING PANEL
2. L.H. INSTRUMENT PANEL
3. AUX. POWER SOURCE LOCATION
4. CIGAR LIGHTER LOCATION
5. INSTRUMENT PANEL SUPPORT RAIL
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Figure 8 Right Side Only, Power Window Switch and Power Feed
1. FUSE F4–B, 25 AMP
2. ELECTRIC WINDOW RELAY (1159)
3. ELECTRIC WINDOW SWITCH (1158)
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Figure 28 EATON VORAD Collision Avoidance EVT-300 Circuits — Side Sensor W/51”, 72” Pro Sleeper
1. EATON VORAD — SIDE SENSOR
2. SIDE SENSOR WIRING HARNESS
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Figure 29 EATON VORAD Collision Avoidance EVT-300 Circuits — Side Sensor W/Daycab
1. EATON VORAD — SIDE SENSOR W/PAINTED STEPS
2. SIDE SENSOR WIRING HARNESS
3. EATON VORAD — SIDE SENSOR W/ALUMINUM STEPS
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Figure 30 EATON VORAD Collision Avoidance EVT-300 Circuits — Side Sensor Chassis Skirt
1. CHASSIS SKIRT
2. EATON VORAD — SIDE SENSOR
3. SIDE SENSOR WIRING HARNESS
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Figure 31 EATON VORAD Collision Avoidance EVT-300 Circuits — Driver Display Unit
1. EATON VORAD COLLISION AVOIDANCE DRIVER DISPLAY/CONTROL ELECTRONIC
CONTROL
2. INSTRUMENT PANEL
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Figure 32 EATON VORAD Collision Avoidance EVT-300 Circuits — Side Display Unit
1. A-PILLAR TRIM COVER
2. EATON VORAD SIDE DISPLAY MODULE INSTRUMENT
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Figure 36 EATON VORAD Collision Avoidance EVT-300 Circuits — Side Sensor Wiring Harness
W/51” Pro Sleeper
1. EATON VORAD SLEEPER BOX SIDE SENSOR WIRING HARNESS CONNECTOR
2. EATON VORAD SLEEPER BOX WIRING HARNESS
3. EATON VORAD CAB SIDE SENSOR WIRING HARNESS CONNECTOR
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Figure 37 EATON VORAD Collision Avoidance EVT-300 Circuits — Side Sensor Wiring Harness
W/Daycab
1. EATON VORAD CAB SIDE SENSOR WIRING HARNESS CONNECTOR
2. EATON VORAD CAB WIRING HARNESS
3. TRAILER SOCKET
4. EATON VORAD CAB SIDE SENSOR WIRING HARNESS CONNECTOR
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Figure 38 EATON VORAD Collision Avoidance EVT-300 Circuits — Side Sensor Wiring Harness
W/72” Pro Sleeper
1. EATON VORAD SLEEPER BOX SIDE SENSOR WIRING HARNESS CONNECTOR
2. EATON VORAD SLEEPER BOX WIRING HARNESS
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Table of Contents
1. DESCRIPTION. . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . ..113
1.1. BATTERY POWER. . .. .. .. .. . .. .. .. .. . .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. . .. .. .. .. . .. .. .. ..113
Remote Start Terminal.. . . . . . .. . . . . . . .. . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . .113
1.2. CHARGING CIRCUITS. . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . ..113
With 3+1 Isolated Battery System.. . .. .. . .. . .. .. . .. . .. .. . .. . .. . .. .. . .. . .. .. . .. . .. . .. .. . .. . .. .. . ..113
1.3. CRANKING MOTOR CIRCUITS.. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. ..113
Cranking Motor. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. .. . ..113
Cranking Motor Circuits. .. . . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. .113
Cranking Motor Thermal Overcrank Protection. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . .113
2. OPERATION.. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. . .. ..114
2.1. BATTERY POWER. . .. .. .. .. . .. .. .. .. . .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. . .. .. .. .. . .. .. .. ..114
Remote Start Terminal.. . . . . . .. . . . . . . .. . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . .114
2.2. CHARGING CIRCUITS. . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . ..114
With 3+1 Isolated Battery System.. . .. .. . .. . .. .. . .. . .. .. . .. . .. . .. .. . .. . .. .. . .. . .. . .. .. . .. . .. .. . ..114
2.3. CRANKING MOTOR CIRCUITS.. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. ..114
Cranking Motor. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. .. . ..114
Cranking Motor Circuits. .. . . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. .114
Cranking Motor Thermal Overcrank Protection. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . .115
3. TROUBLESHOOTING. . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. .115
3.1. BATTERIES AND CABLES.. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .. ..115
Battery Test Procedure. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. ..116
Battery Cable Voltage Loss Test. . . . . . .. . . . . . . . . . . . .. . . . . . . . . . . . .. . . . . . . . . . . . .. . . . . . . . . . . . .. . . . . .117
3.2. STARTING MOTOR SYSTEM CIRCUITS AND COMPONENTS. . . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . . ..119
Starter Solenoid Circuit Test - Part 1. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . . . . . .. . . . . . .. . .119
Starter Solenoid Circuit Test - Part 2. . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . .120
Starter Magnetic Switch Circuit Test - Part 1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .122
Starter Magnetic Switch Circuit Test - Part 2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .123
Starter Motor Replacement Test. . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .124
Testing Thermal Overcrank Protection System. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . .125
3.3. VEHICLE CHARGING SYSTEM. . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . .126
Batteries Undercharged. . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . .126
Alternator Tests. . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .127
Alternator Wiring Test.. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. .127
Alternator Replacement Test — Voltage Output Test. .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .128
Alternator Replacement Test — Amperage Output Test. . . . . . .. . . . . . . . . . . . . . .. . . . . . . . . . . . . . .129
Alternator Replacement Test — Replacement. . .. . . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . . .. . .130
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1. DESCRIPTION
1.1. BATTERY POWER
The vehicle batteries, connected in parallel, provide power via the positive battery cable which is connected
to the cranking motor solenoid "B" terminal. Depending upon battery box location, some vehicles have two
positive cables to the cranking motor.
The negative battery terminals are connected to the cranking motor ground terminal, which is connected to the
frame rail. The engine and cab are also connected by ground cables to the cranking motor ground.
An optional 3+1 isolated battery system is available. Refer to POWER DISTRIBUTION AND GROUND
SYSTEM section for discussion about this system.
An optional remote start terminal allows an external battery power source to either charge the vehicle batteries
or assist in cranking the engine.
The alternator output "B" terminal is connected to the start magnetic switch “B” terminal and to the crank
motor solenoid “B” terminal.
On vehicles with this system, 7 volt output from the alternator “R” terminal is used to energize the isolated
battery magnetic switch whenever the alternator is operating. (Refer to the POWER DISTRIBUTION AND
GROUND SYSTEM section for information on the 3+1 system.)
The Delco MT–41 Series cranking motor is used with the standard engine in the 5000i series truck, and the
Delco MT–42 series cranking motor is standard for the 9000i series vehicles. It provides the rotation of the
engine crank via the flywheel needed to start the engine.
Cranking Motor Circuits
The cranking motor circuits provide power to the cranking motor to turn over the crankshaft of the engine. If all
other systems are operational, the engine will start.
On vehicles with thermal overcrank protection (optional system), excessive cranking will cause cranking motor
temperature to reach a pre-set thermal overcrank limit, and the thermal switch will open causing the motor
to dis-engage. This protects the starting motor from heat damage. When the crank motor cools, the switch
closes permitting the crank motor to operate again.
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114 3 BATTERY, CHARGING AND CRANKING SYSTEMS
2. OPERATION
Refer to CHARGING AND CRANKING circuit diagrams in CTS-5298 or S08225.
The negative battery terminals are connected to the cranking motor ground terminal, which is connected to the
frame rail. The engine and cab are also connected by ground cables to the cranking motor ground.
An optional 3 +1 isolated battery system is available. Refer to POWER DISTRIBUTION AND GROUND
SYSTEM for this system.
The remote starter terminal allows an external battery power source to either charge the vehicle batteries or
assist in cranking the engine. Connect the external source positive cable to the remote start terminal and the
external source negative cable to vehicle frame rail.
To use an external power source to charge the deep cycle battery (with 3+1 system) at the same time as the
cranking batteries, a jumper must be used to connect the positive deep cycle battery terminal to the positive
terminal of the cranking batteries.
The alternator output “B” terminal is connected to the start magnetic switch “B” terminal and to the crank
motor solenoid “B” terminal.
For a complete discussion on operating principles for alternators, refer to GROUP 08 - ELECTRICAL in the
CTS-5000 Master Service Manual for the specific alternator being serviced.
On vehicles with this system, 7 volt output from the alternator “R” terminal is used to energize the isolated
battery magnetic switch whenever the alternator is operating. (Refer to POWER DISTRIBUTION AND
GROUND SYSTEM section for the 3+1 system.)
For complete information on operation and servicing this cranking motor and optional cranking motors used on
these vehicles, refer to GROUP 08 - ELECTRICAL in the CTS-5000 Master Service Manual.
Cranking Motor Circuits
With the key in the start position, ignition voltage from start feed adapter (509) is applied through circuit 17B
to energize the starter magnetic switch.
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3 BATTERY, CHARGING AND CRANKING SYSTEMS 115
Battery power from the (B1) battery stud (circuit 14A) is always present at the “B” terminal of the magnetic
switch. With the start magnetic switch energized, battery power is applied through circuit 17C to energize the
crank motor solenoid.
With the crank motor solenoid energized, the solenoid engages the cranking motor and battery power causes
the motor to rotate. When the starter switch is released, a spring returns the solenoid to the released position.
On vehicles with thermal overcrank protection (optional system), the start magnetic switch control coil ground
circuit 17D is connected to the normally closed thermal switch (275). The thermal switch is located in the end
of the cranking motor. The thermal switch is grounded at the engine ground stud.
If excessive cranking causes cranking motor temperature to reach pre-set thermal overcrank limits, the
thermal switch opens causing the start magnetic switch to de-energize, turning off power to the cranking motor
solenoid S terminal, dis-engaging the cranking motor.
When the crank motor cools, the switch closes permitting the crank motor to operate again.
3. TROUBLESHOOTING
Refer to CHARGING AND CRANKING circuit diagrams in CTS-5298 or S08225.
A. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of
charge (SOC) or higher. This represents an open circuit voltage (OCV) of 12.4 volts. Batteries
with an OCV of 12 volts or less are either completely discharged or have a dead cell.
B. Before beginning these test procedures, check any light or indicator lamp filaments that are
suspected of being open (burned out). This is done to avoid unnecessary extensive circuit checks.
C. Before beginning these test procedures, inspect all connectors for loose or damaged pins,
wires, etc. Refer to TEST EQUIPMENT AND CONNECTOR REPAIR section in GROUP 08 -
ELECTRICAL in the CTS-5000 Master Service Manual.
D. When the technician determines that a fuse is blown, while checking its condition, he is directed
to locate the cause of the overload condition and to repair it. While no further instruction on this
procedure is listed in the diagnostic tables, the common procedure is as follows: isolate sections
of the circuit, by disconnecting connectors, and measure the resistance to ground to find the circuit
that is shorted to ground. Then locate the damaged spot in the wire or connector and repair.
E. Diagnostics for circuits that are malfunctioning by sticking in the on position are generally not
covered in detail. It is assumed that the technician knows to check for a malfunctioning switch,
relay, or solenoid.
WARNING – When handling batteries, always wear face or eye protection, have water supply
available, assure good ventilation, and be sure no open flames are present.
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116 3 BATTERY, CHARGING AND CRANKING SYSTEMS
1. Disconnect both battery terminals at each battery. Check each battery visually.
3. Apply a 300A load for 15 seconds. Turn off load and wait one minute.
a. If 12.4V or more - go to step 4.
b. If less than 12.4V - recharge then repeat step 3.
4. Apply a test load equal to 50% of the battery CCA rating at 0°F (-18°C). After 15 seconds,with the load
still applied, measure and record terminal voltage ________. Turn the load off.
5. Estimate the battery temperature. If measured voltage does not meet or exceed the value shown in
the following table, replace the battery.
6. Clean all cable ends and terminals of the battery with a wire brush.
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3 BATTERY, CHARGING AND CRANKING SYSTEMS 117
Slow cranking is often caused by high resistance in the battery cables or connections, especially in cold
weather. After all batteries check good (Battery Test Procedure) and terminals are clean and tight, check the
battery cables. To do this place a specific load on the batteries at the starter. This load will be supplied
by the adjustable carbon pile.
The voltage drop in the positive cable plus the voltage drop in the negative cable equals the difference
between the battery voltage and the starter voltage due to the cables. The maximum acceptable loss has been
calculated only for the specific load specified in the test.
1. Tighten nuts holding battery cables to the solenoid and starter terminals.
NOTE – The solenoid BAT terminal is at battery voltage when batteries are connected.
2. Connect carbon pile positive lead to start solenoid “B” terminal and negative lead to starter ground terminal
(Battery Cable Voltage Loss Test Figure).
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118 3 BATTERY, CHARGING AND CRANKING SYSTEMS
3. Connect voltmeter from the starter solenoid “B” terminal to battery positive post.
4. Adjust load to 500A, quickly read and record positive cable voltage. Turn off the load and allow carbon
pile to cool.
5. Connect voltmeter from negative battery post to starter ground terminal. Attach ground lead directly to
stud and not the cable end.
6. Adjust load to 500A, read and record negative cable voltage. Turn off the load.
If system loss is 0.6V or less, go to STARTING MOTOR SYSTEM CIRCUITS AND COMPONENTS.
If system loss is greater than 0.6V, repair or replace cable(s) with excessive voltage loss and retest.
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To check the interconnecting cables between the batteries, while cranking, measure the terminal voltage of
each battery by touching voltmeter leads to the post of each battery (refer to the Figure below).
If the difference between any two battery readings in the same battery box is more than 0.5 volt or any cable is
warm to the touch, replace the interconnecting cables.
Starter shifting in and out, or not pulling in, is often caused by high resistance in the starter solenoid circuit.
When the solenoid circuit has excessive voltage loss, the starter pinion sometimes may not engage the
flywheel. If it does engage, it may drop out too soon when battery voltage drops. The solenoid circuit includes
the starter magnetic switch and leads connected to the starter solenoid.
On vehicles with overcrank protection, refer to Testing Thermal Overcrank Protection System before
performing this test.
1. Disconnect circuit 17C from the starter solenoid “S” terminal. Connect the carbon pile positive lead to
circuit 17C and negative lead to the starter ground. Connect the voltmeter positive lead to the solenoid
battery stud and the negative lead to the starter motor ground stud (not to carbon pile clamp).
2. Have an assistant push the start button or turn key switch. The magnetic switch should energize with a
clicking sound. If the switch doesn’t "click," either the switch is defective (refer to Starter Magnetic Switch
Circuit Test) or there is no voltage from the key switch circuit.
3. Adjust the carbon pile to 100 amp load. Measure and record cable voltage. Release the start button or
key switch. If the reading is more than .5 volt lower than the value shown in the table in Battery Test
Procedure, perform that test and Battery Cable Voltage Loss Test.
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120 3 BATTERY, CHARGING AND CRANKING SYSTEMS
4. Move the voltmeter negative lead from the starter motor ground stud to the end of circuit 17C that is
connected to the carbon pile. Do not connect to carbon pile clamp.
5. Push and hold the start button again and re-adjust the carbon pile load to 100 amps. Read and record
voltage to the solenoid. Release the start button or key switch.
If circuit loss is 1.0 volt or less, go toStarter Magnetic Switch Circuit Test - Part 1.
If circuit loss is more than 1.0 volt, go toStarter Solenoid Circuit Test - Part 2.
If the voltage loss in Test 1 was more than 1 volt, the loss is excessive. The loss may be from loose terminals,
corrosion, or a worn out start magnetic switch. To locate the problem:
2. Connect DMM positive lead to solenoid BAT stud and negative lead to large terminal of magnetic switch. If
voltage shows on meter, move meter lead to the other large magnetic switch terminal.
3. Push start button with key on or turn key switch to start position. Turn on and adjust carbon pile to 100
amp load. Read and record first wire voltage loss. Release start switch.
4. Connect DMM positive lead to other (opposite) large terminal on magnetic switch and negative lead to
circuit 17C (not to carbon pile clamp).
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5. Push start button or turn key switch to start position. Turn on and adjust carbon pile to 100 amp load.
Read and record second wire voltage loss. Release start switch.
If circuit loss is more than 0.8 volt, repair or replace wire, then go to step 6.
6. Connect DMM across the two large magnetic switch terminals (battery voltage will show immediately).
7. Push start button or turn key switch to start position. Turn on and adjust carbon pile to 100 amp load.
Read and record ________ voltage loss across the magnetic switch.
8. If the voltage drop is greater than 0.2 volt, replace the magnetic switch.
9. Remove carbon pile. Leave circuit 17C disconnected (use tape to insulate) to perform Starter Magnetic
Switch Circuit Test - Part 1 (below).
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122 3 BATTERY, CHARGING AND CRANKING SYSTEMS
A magnetic switch that does not close or drops out too soon can be caused by high resistance or an open in
the control circuit.
1. Disconnect circuit 17C from start solenoid “S” terminal and insulate with tape. Connect voltmeter positive
lead to the starter solenoid BAT stud and negative lead to the starter motor ground stud.
2. Have an assistant push the start button (with key on) or turn key to start position.You should hear the
magnetic switch relay “click." If not, proceed anyway. Read and record battery cable voltage. Release
start switch.
3. Connect the voltmeter positive lead to the small magnetic switch terminal and the negative lead to the
switch ground screw. (Magnetic switch is internally grounded through the mounting.)
4. Have an assistant push the start button (with key on) or turn key to start position. Read and record
magnetic switch voltage. Release the start switch.
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3 BATTERY, CHARGING AND CRANKING SYSTEMS 123
If circuit loss is 1.0 volt or less and the magnetic switch closes, circuit is OK.
If circuit loss is 1.0 volt or less and the magnetic switch doesn’t close, replace the switch and repeat the test.
If circuit loss is more than 1.0 volt, go to Starter Magnetic Switch Circuit Test - Part 2 (below).
If Starter Magnetic Switch Circuit Test - Part 1 has shown a voltage loss greater than 1.0V, perform this test
using a digital multimeter (DMM). Leave circuit 17C disconnected from the starter solenoid.
1. With the key on and start button depressed or key switch in start position, and the voltmeter leads in the
positions shown for each step:
a. Measure magnetic switch to starter motor ground. If reading is within 1.0 volt of battery voltage, repair
magnetic switch ground. If reading is not within 1.0 volt of battery voltage, go to Step B.
b. Measure and record ______ solenoid to key voltage.
c. Measure and record ______ key switch voltage.
d. Measure and record ______ key to start button voltage.
e. Measure and record ______ start button voltage.
f. Measure and record ______ start button to magnetic switch voltage.
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124 3 BATTERY, CHARGING AND CRANKING SYSTEMS
If greater than 1.0 volt, repair or replace any circuit or component with excess voltage loss.
If any of the circuits or component checks (B through F) show full battery voltage with the start button
depressed or key switch in start position, then an open circuit exists in the portion of the circuit between the
DMM leads. Repair that portion and connect circuit 17B to the starter solenoid.
If all previous battery tests have been performed, the vehicle batteries and starter wiring have
been checked.
The starter magnetic switch can fail to "hold in" during cold weather cranking due to low voltage,
even though the switches and circuits check OK. With this failure you will hear the starter failing to
stay engaged with the flywheel. It is caused by low system voltage releasing the magnetic switch.
If this condition exists, have an assistant clamp a heavy battery jumper cable between the two
big (5/16") studs on the magnetic switch while cranking. Caution - The studs are battery
voltage and the engine should crank when the jumper is connected. Remove jumper to
stop cranking. If the engine cranks properly with jumper in place, replace the magnetic switch
and make sure starter mounting bolts are tight.
B. Checking Available Voltage At Starter
If all previous battery tests have been performed, the vehicle batteries and starter wiring have
been checked, but the engine still cranks slowly, check available voltage at the starter.
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3 BATTERY, CHARGING AND CRANKING SYSTEMS 125
1. While cranking engine, measure voltage between the starter BATT terminal and starter ground.
a. If voltage is 9.0 volts or more, the problem must be in the starter (or engine). Replace the starter.
b. If the voltage is less than 9.0 volts, go to Battery Cable Voltage Loss Test.
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126 3 BATTERY, CHARGING AND CRANKING SYSTEMS
Before beginning test procedures: check battery cables and alternator wiring (especially grounds) for clean,
tight connections. Wires and connectors should not be damaged or corroded.
Perform the following checks before removing the alternator from the vehicle.
2. Check alternator drive belt tension (refer to GROUP 12 - ENGINE, Cooling in the CTS-5000 Master
Service Manual for belt tension specifications). As a general rule, if the alternator fan can be rotated by
pulling on the fan with one finger, the belt is too loose.
3. Inspect for defective batteries as described in GROUP 08 - ELECTRICAL, Battery Section in the
CTS-5000 Master Service Manual.
4. Wiring defects. Visually check wiring, clamps, and connections for clean, tight connections, free of
damage and corrosion.
5. With the engine OFF, check voltage to ground at the BAT terminal of the alternator. A zero reading
indicates an open in circuit 2, between the alternator and batteries.
6. A defective component or wiring defect may be causing a small current drain that is less than the fuse
rating for the circuit so the fuse does not open. To locate the unwanted current drain:
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3 BATTERY, CHARGING AND CRANKING SYSTEMS 127
Alternator Tests
The alternator output must reach the batteries and accessory loads with a minimum amount of voltage loss.
Any loss slows the rate of charge to the batteries and can cause the batteries to be undercharged. Discharged
batteries can damage the starter and cause vehicle electrical components to operate improperly.
Most alternators control the maximum system voltage using a voltage regulator. Maximum voltage output
is available at the alternator BAT terminal, but if any voltage is lost in the wiring, something less than the
maximum will reach the batteries and load devices. The greatest losses occur when the charging system
is outputting at the maximum rated level (amps).
Instead of using alternator current output this test uses the same amount of current but draws it from the
batteries (must be fully charged). Using the carbon pile load, the current flows in reverse through the circuit
without the engine running.
1. Without the engine running, connect the carbon pile to the alternator output terminal and ground.
2. Connect voltmeter between alternator output terminal and positive battery terminal.
3. Adjust the carbon pile to alternator rated output (amps). Rated output is stamped on the case or on a tag.
4. Read voltmeter and record positive circuit voltage loss. Immediately turn the carbon pile off.
5. Move the voltmeter connections to between the alternator, ground and negative battery terminal. Adjust
carbon pile to rated output (amps) of the alternator.
6. Read voltmeter and record negative circuit voltage loss. Immediately turn carbon pile off.
If system loss is greater than 0.7V, repair circuit(s) with excessive voltage loss and retest. Then go to
Alternator Replacement Test.
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128 3 BATTERY, CHARGING AND CRANKING SYSTEMS
If the wiring tests have been performed (circuits OK), adjust alternator belt and tighten mounting bolts and
ground connections. Batteries must be near full charge with more than 12.4 volts no load voltage.
2. With NO electrical loads turned on, start the engine. Fast idle engine until voltage stabilizes (does not
increase) for 2 minutes.
3. Check and record alternator output voltage _______V (should not exceed 15.5 volts).
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1. With vehicle at shop temperature, connect carbon pile and clamp-on ammeter as shown (see Figure
above). Clamp around all wires connected to alternator “B” terminal. (To use an ammeter without an
induction clamp, disconnect circuits to alternator “B” terminal and connect meter shunt between alternator
B+ terminal and all circuits previously removed.)
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130 3 BATTERY, CHARGING AND CRANKING SYSTEMS
2. With NO electrical loads turned on, start the engine, and speed up and maintain a high RPM.
3. Turn on and adjust carbon pile until ammeter reads its highest value and record ______A.
5. If reading is zero (no output), the rotor should be magnetized with the alternator hooked up normally. To do
this, momentarily connect a jumper lead from the alternator “B” terminal to the indicator “R” terminal. This
will restore normal residual magnetism.
4. COMPONENT LOCATIONS
B1 Battery Stud. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . ... . . . . . Power Distribution Panel
B2 Battery Stud. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . ... . . . . . Power Distribution Panel
B Alternator Stud. . . . . . . . . . . . . . .. . . . . . . . . . . . . . .. . . . . . . .. . . . . . Back of Alternator
G Alternator Stud. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . . ... . . . . . Back of Alternator
B Cranking Motor Solenoid Stud. . . . . . . . . . . . . . . . . . . .. . . . . . Back of Cranking Motor Solenoid
M Cranking Motor Solenoid Stud. . . . . . . . . . . . . . . . . . . .. . . . . . Back of Cranking Motor Solenoid
R Alternator Stud. . .. . . . .. . . . . .. . . . .. . . . .. . . . . .. . . . .. . .. . . . . . Back of Alternator
S Cranking Motor Solenoid Stud. . . . . . . . . . . . . . . . . . . .. . . . . . Back of Cranking Motor Solenoid
(1) Dash Panel Connector.. . .. . .. .. . .. .. . .. .. . .. .. . ... . . . . . Left Side of Engine Cowl
(2) Dash Panel Connector.. . .. . .. .. . .. .. . .. .. . .. .. . ... . . . . . Right Side of Engine Cowl, Above Conn. 3
(3) Dash Panel Connector.. . .. . .. .. . .. .. . .. .. . .. .. . ... . . . . . Right Side of Engine Cowl, Below Conn. 2
(40) Key Switch. .. . .. .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . ... . . . . . Behind Left Side of Instrument Panel
(275) Thermo Overload Switch. . . . . . . . . . . . . . . . . . . . . .. . . . . . At the Cranking Motor
(509) Start Feed Adapter. .. . . . . . . . . . . . . . . . .. . . . . . . . . .. . . . . . 6" Left of Fuse Panel, Near Heater Control
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1. 150A MEGAFUSE
2. TO (B1) BATTERY STUD
3. START MAG SWITCH
4. NO BUS BAR WITH 3+1 BATTERY SYSTEM
5. TO HEATER
6. (3) ENGINE HARNESS CONNECTOR
7. (2) CHASSIS HARNESS CONNECTOR
8. RIGHT HAND DASH GROUND STUD
9. FUSE BLOCK GROUND STUD
10. (B2) BATTERY STUD
11. (B1) BATTERY STUD
12. KEY SWITCH
13. LEFT HAND DASH GROUND STUD
14. (1) FRONT END HARNESS CONNECTOR
15. GROUND CIRCUITS
16. DASH PANEL
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Table of Contents
1. DESCRIPTION. .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .141
2. OPERATION.. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .141
3. TROUBLESHOOTING. .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .141
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1. DESCRIPTION
Use with Circuit Diagram Book CTS-5298 or S08225.
When activated, the ether start system injects a measured amount of ether into the engine intake system to
assist starting. The system will only function if the engine temperature is less than approximately 40°F (5°C).
2. OPERATION
The ether start switch on the instrument panel receives ignition voltage from 10A fuse F10-A (location may
vary) when the key is on. The switch is a momentary-on (normally open) type switch. When the switch is
closed, power is applied to the ether control valve coil. If the thermo switch is closed, a measured amount
of ether is injected into the engine intake system.
The ether control valve coil is grounded through the ether thermo switch mounted on the side of the engine
block, which closes at less than 40°F (5°C) and opens when engine block temperature exceeds 50°F (10°C).
3. TROUBLESHOOTING
1. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of charge (SOC)
or higher. This represents an open circuit voltage (OCV) of 12.4 volts. Batteries with an OCV of 12 volts or
less are either completely discharged or have a dead cell.
2. Before beginning these test procedures, check any light or indicator lamp filaments that are suspected of
being open (burned out). This is done to avoid unnecessary extensive circuit checks.
3. Before beginning these test procedures, inspect all connectors for loose or damaged pins, wires, etc.
Refer to TEST EQUIPMENT AND CONNECTOR REPAIR section in GROUP 08 — ELECTRICAL in
the CTS-5000 Master Service Manual.
4. When the technician determines that a fuse is blown, while checking its condition, he is directed to locate
the cause of the overload condition and to repair it. While no further instruction on this procedure is listed in
the diagnostic tables, the common procedure is as follows: isolate sections of the circuit, by disconnecting
connectors, and measure the resistance to ground to find the circuit that is shorted to ground. Then locate
the damaged spot in the wire or connector and repair.
5. Diagnostics for circuits that are malfunctioning by sticking in the on position are generally not covered in
detail. It is assumed that the technician knows to check for a malfunctioning switch, relay, or solenoid.
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142 4 ELECTRICAL TROUBLESHOOTING ETHER START
4. COMPONENT LOCATIONS
(1) Dash Panel Connector.. . .. . .. .. . .. .. . .. .. . .. .. . ... . . . . . Left Side of Engine Cowl
(2) Dash Panel Connector.. . .. . .. .. . .. .. . .. .. . .. .. . ... . . . . . Right Side of Engine Cowl, Above Connector 3
(3) Dash Panel Connector.. . .. . .. .. . .. .. . .. .. . .. .. . ... . . . . . Right Side of Engine Cowl, Below Connector 2
(72) Ether Start At Dash Panel. . . . . . . . . . . . . . . . . . . . . .. . . . . . Front End Harness
(494) I1 Ignition Adapter. .. . . . .. . . . .. . . . .. . . . .. . . . .. . .. . . . . . Behind Fuse Panel
(504) L2 Panel Light Feed Adapter. .. . .. . .. . .. . .. . ... . . . . . Behind Instrument Panel/Switch Breakout
(506) L4 Panel Lights Gnd Adapter. . . . . . . . . . . . . . . . .. . . . . . Behind Instrument Panel/Switch Breakout
(600) Ether Start On/Off Switch. . .. . .. . .. . .. . .. . .. . ... . . . . . At Switch Cluster
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Table of Contents
1. DESCRIPTION. .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .153
1.1. HORTON ENGINE FAN CONTROLS. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .153
1.2. KYSOR ENGINE FAN CONTROLS.. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .153
2. OPERATION.. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .153
2.1. CATERPILLAR C-10, C-12 AND 3406E. . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .153
ADEM III ECM Fan Control. .. . . . . . . .. . . . . . . .. . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . .153
Horton Engine Fan.. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .154
Kysor Engine Fan.. . .. . .. .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. .155
Kysor Engine Fan.. . .. . .. .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. .155
2.2. DETROIT DIESEL SERIES 60. . . . .. . . . . . . . . .. . . . . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . .156
Horton Engine Fan Controls.. . . .. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . .. . . .. . . .. . .156
Kysor Engine Fan Controls. .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . .157
2.3. CUMMINS N14E. . .. . . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .158
Horton Engine Fan Controls With ECM Control System. .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .158
Kysor Engine Fan Controls With ECM Control System. . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .158
2.4. CUMMINS ISM AND AHD. . . . .. . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .158
Horton Engine Fan Controls With ECM Control System. .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .158
Kysor Engine Fan Controls With ECM Control System. . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .159
2.5. INTERNATIONAL I6 HEUI.. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .159
Horton Engine Fan Controls With ECM Control System. .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .159
Kysor Engine Fan Controls With ECM Control System. . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .160
3. TROUBLESHOOTING. .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .160
3.1. ENGINE COOLING FAN CONTROLS, HORTON AND KYSOR WITH CATERPILLAR C–10,
C-12 AND 3406E. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .160
Testing Fan Solenoid and Circuits.. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .160
Testing A/C Compressor High Pressure Switch (228) and Circuits.. .. . .. . .. .. . .. . .. .. . .. .162
Testing (Optional) Engine Fan Override Switch (659). . . . . . . . . . .. . . . . . . . . . . . . . .. . . . . . . . . . . . . .163
3.2. ENGINE COOLING FAN CONTROLS, HORTON AND KYSOR WITH DETROIT DIESEL
SERIES 60 DDEC III. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .164
Testing Fan Solenoid and Circuits.. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .164
Testing A/C Compressor High Pressure Switch (228) and Circuits.. .. . .. . .. .. . .. . .. .. . .. .165
3.3. ENGINE COOLING FAN CONTROLS, HORTON AND KYSOR WITH CUMMINS M11 AND N14
CELECT. . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . .166
Testing Fan Solenoid and Circuits.. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .166
Testing A/C Compressor High Pressure Switch (228) and Circuits.. .. . .. . .. .. . .. . .. .. . .. .167
3.4. ENGINE COOLING FAN CONTROLS, HORTON AND KYSOR WITH CUMMINS ISM AND
AHD. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .168
Testing Fan Solenoid and Circuits.. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .168
Testing A/C Compressor High Pressure Switch (228) and Circuits.. .. . .. . .. .. . .. . .. .. . .. .169
Testing (Optional) Engine Fan Override Switch (659). . . . . . . . . . .. . . . . . . . . . . . . . .. . . . . . . . . . . . . .169
3.5. ENGINE COOLING FAN CONTROLS, HORTON AND KYSOR WITH INTERNATIONAL I6 HEUI
ENGINE. . .. .. . .. . .. . .. .. . .. . .. .. . .. . .. . .. .. . .. . .. .. . .. . .. . .. .. . .. . .. .. . .. . .. . .. .. . .. . .. .. . .. . .. . .. .. . .. . .. .170
Testing Fan Solenoid and Circuits.. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .171
Testing A/C Compressor High Pressure Switch (228) and Circuits.. .. . .. . .. .. . .. . .. .. . .. .171
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152 5 ELECTRICAL TROUBLESHOOTING FANS
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5 ELECTRICAL TROUBLESHOOTING FANS 153
1. DESCRIPTION
1.1. HORTON ENGINE FAN CONTROLS
The ECM is used to control the Horton engine cooling fan. Other fan control components include:
The fan solenoid relay is controlled by the ECM using information from the coolant temperature sensor,
retarder solenoid status and A/C high pressure switch.
The optional engine fan override switch allows the driver to disable the control voltage from the ECM and keep
the fan turned on. An indicator will light during the time the fan would normally be off.
The solenoid relay is controlled by the ECM using information from the coolant temperature sensor, retarder
solenoid status and A/C high pressure switch.
The optional engine fan override switch allows the driver to disable the control voltage from the ECM and
keep the fan turned on.
2. OPERATION
2.1. CATERPILLAR C-10, C-12 AND 3406E
ADEM III ECM Fan Control
Refer to circuit diagram HORTON AND KYSOR ENGINE FAN WITH C10, C12, and 3406E ENGINES circuits
in CTS-5298 or S08225.
The ECM uses inputs from the engine coolant temperature sensor, retarder solenoid status and the A/C high
pressure switch (228) to determine when the fan should be on. To turn the fan on, the ECM applies OV to the
fan solenoid relay. To turn the fan off, the ECM applies 12V to the fan solenoid relay.
• If the engine speed is less than 2250 RPM and any of the following conditions exists:
• Engine not running or
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154 5 ELECTRICAL TROUBLESHOOTING FANS
The ECM turns the fan off under the following conditions:
• Engine speed is greater than 2250 RPM or all of the following conditions exists:
• Coolant temperature sensor is less than 198°F (92°C) for C-10 and C-12 or Coolant temperature sensor is
less than 207°F (97°C) for 3406E and
• The fan has been on for 30 seconds and
• Engine retarder ON strategy is not active and
• A/C high pressure switch is not active.
NOTE – Once the ECM has turned the fan on, the fan will remain on for a minimum of 30 seconds to
avoid unnecessary fan clutch cycling (except at engine start-up: it will run for only two seconds after
the engine has reached the programmed low idle (700–750 rpm).
When the ECM energizes the fan solenoid, it causes the fan solenoid to energize. This disengages the
fan clutch.
Horton Fan Clutch Assembly - The fan clutch is engaged by air pressure supplied by the fan solenoid. The
fan clutch is spring loaded off and air pressure is required to overcome the spring and engage the clutch.
Horton Normally Open Fan Solenoid (227) -The N.O. fan solenoid (227) supplies air pressure to engage the
fan clutch when the solenoid is not energized. Energizing the solenoid turns off the air pressure to the fan
clutch, causing the fan clutch to disengage.
When the optional engine fan override switch is not installed, the solenoid is energized by a 12V signal
on circuit 23A from ECM connector (400) terminal 28. The solenoid ground circuit, 23–GA, is grounded
through circuit 11–GC.
When the optional engine fan override switch is installed, the solenoid is energized by a 12V signal on circuit
23A from ECM connector (400) terminal 28 through switch (659). The solenoid ground circuit, 23–GA, is
grounded through circuit 11–GC.
The engine fan override switch has an indicator LED which will light during the time the fan would normally be
off, when the override switch is on. The 12V signal on circuit 23A from ECM connector (400) terminal 28 will
flow through the LED in switch (659). The LED is grounded through circuit 23–GY.
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5 ELECTRICAL TROUBLESHOOTING FANS 155
The engine fan override switch is illuminated with an LED. 12 volts from the panel feed adapter (503) is
supplied on circuit 62M. Ground for the LED is supplied on circuit 11–GR.
When the optional engine fan override switch is installed, the solenoid is energized by a 12V signal on circuit
23A from ECM connector (400) terminal 28 through switch (659). The solenoid ground circuit, 23–GA, is
grounded through circuit 11–GC.
Kysor Fan/Clutch Assembly —The fan clutch is disengaged by air pressure supplied by the fan solenoid. The
fan clutch is spring loaded on and air pressure is required to overcome the spring and disengage the fan clutch.
Kysor Normally closed (N.C.) Fan Solenoid (227) — The N.C. fan solenoid (227) does not supply air
pressure to disengage the fan clutch when the solenoid is not energized. Energizing the solenoid turns on
the air pressure to the fan clutch, causing the fan clutch to disengage.
When the optional engine fan override switch is not installed, the solenoid is energized by a 12V signal
on circuit 23A from ECM connector (400) terminal 28. The solenoid ground circuit, 23–GA, is grounded
through circuit 11–GC.
The engine fan override switch has an indicator lamp which will light during the time the fan would normally be
off, when the override switch is on. The 12V signal on circuit 23A from ECM connector (400) terminal 28 will
flow through the LED in switch (659). The LED is grounded through circuit 23–GY.
The engine fan override switch is illuminated with an LED. 12 volts from the panel feed adapter (503) is
supplied on circuit 62M. Ground for the LED is supplied on circuit 11–GR.
When the optional engine fan override switch is installed, the solenoid is energized by a 12V signal on circuit
23A from ECM connector (400) terminal 28 through switch (659). The solenoid ground circuit, 23–GA, is
grounded through circuit 11–GC.
Kysor Fan/Clutch Assembly — The fan clutch is disengaged by air pressure supplied by the fan solenoid. The
fan clutch is spring loaded on and air pressure is required to overcome the spring and disengage the fan clutch.
Kysor Normally Closed (N.C.) Fan Solenoid (227) —The N.C. fan solenoid (227) does not supply air
pressure to disengage the fan clutch when the solenoid is not energized. Energizing the solenoid turns on
the air pressure to the fan clutch, causing the fan clutch to disengage.
When the optional engine fan override switch is not installed, the solenoid is energized by a 12V signal
on circuit 23A from ECM connector (400) terminal 28. The solenoid ground circuit, 23–GA, is grounded
through circuit 11–GC.
The engine fan override switch has an indicator lamp which will light during the time the fan would normally be
off, when the override switch is on. The 23V signal on circuit 23A from ECM connector (400) terminal 28 will
flow through the LED in switch (659). The LED is grounded through circuit 23–GY.
The engine fan override switch is illuminated with an LED. 12 volts from the panel feed adapter (503) is
supplied on circuit 62M. Ground for the LED is supplied on circuit 11–GR.
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156 5 ELECTRICAL TROUBLESHOOTING FANS
Refer to circuit diagram HORTON AND KYSOR ENGINE FAN WITH SERIES 60 ENGINE circuits in CTS-5298
or S08225.
The ECM controls the Horton fan system. The Horton fan clutch is spring-loaded so the fan is off. Air pressure
from a normally open (N.O.) fan solenoid is used to engage the fan clutch.
The ECM controls the fan solenoid (227) by opening or closing the solenoid ground. The ECM turns the fan on
when at least one of the following conditions occur:
Horton Fan Solenoid (227) — The normally open (N.O.) fan solenoid supplies air pressure to engage the fan
clutch. When the solenoid is not energized, the fan clutch is engaged. The solenoid receives ignition
power from 10A fuse F9–A, whenever the key is on. The solenoid coil ground is connected by circuit 23D to
ECM connector (273) terminal A2. A2 is an ECM digital output terminal. ECM connector (273) terminal A2
is either low (ground) or high (12 volts).
When the ECM wants the fan off, terminal A2 and circuit 23D are low (ground). This grounds the fan solenoid
causing it to energize and air pressure necessary to engage the fan is turned off.
When the ECM wants the fan on, ECM connector (273) terminal A2 and circuit 23D are high (12 volts),
causing the fan solenoid (227) to be de-energized (no ground). with the solenoid de-energized, air pressure
from the normally open solenoid engages the fan clutch.
AC High Pressure Switch (228) — This switch is normally closed and opens when A/C compressor head
pressure exceeds 300 psi. The switch closes when the head pressure drops below 210 psi.
Digital input circuit 23C from ECM connector (273) terminal F1 is connected to one side of the A/C pressure
switch. The other switch terminal is connected by circuit 23–GB to ground. With the switch in its normally
closed position, circuit 23C is low (ground). When the switch is open, circuit 23C is high (5V).
When the ECM sees circuit 23C high, it causes fan solenoid circuit 23D to be at a HIGH state (12V), which
de-energizes the fan solenoid, engaging the fan clutch. When this occurs, the fan clutch will remain engaged
for a minimum of three minutes after the A/C pressure switch returns to a closed position, to reduce fan cycling.
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5 ELECTRICAL TROUBLESHOOTING FANS 157
The ECM controls the Kysor fan system. The Kysor fan clutch is spring-loaded so the fan is on. Air pressure
from a normally closed (N.C.) fan solenoid is used to disengage the fan clutch.
The ECM controls the fan solenoid (227) by opening or closing the solenoid ground. The ECM turns the fan on
when at least one of the following conditions occur:
The International– installed components include the fan clutch, fan solenoid (227), and the A/C high pressure
switch (228).
Kysor Fan Solenoid (227) —The normally closed (N.C.) fan solenoid supplies air pressure to disengage
the fan clutch. When the solenoid is not energized, the fan clutch is engaged. The solenoid receives
power from 10A fuse F9–A, whenever the key is on. The solenoid coil ground is connected by circuit 23D to
ECM connector (273 terminal A2. A2 is an ECM digital output terminal. ECM connector (273) terminal A2
is either low (ground) or high (12 volts).
When the ECM wants the fan off, terminal A2 and circuit 23D are low (ground). This grounds the fan solenoid
causing it to energize and to provide the air pressure necessary to disengage the fan.
When the ECM wants the fan on, ECM connector (273) terminal A2 and circuit 23D are high (12 volts),
causing the fan solenoid (227) to be de-energized (no ground). With the solenoid de-energized, there is no air
pressure from the normally closed solenoid applied to the fan clutch, which is spring loaded on.
AC High Pressure Switch (228) — This switch is normally closed and opens when A/C compressor head
pressure exceeds 300 psi. The switch closes when the head pressure drops below 210 psi.
Digital input circuit 23C from ECM connector (273) terminal F1 is connected to one side of the A/C pressure
switch. The other switch terminal is connected by circuit 23–GB to ground. With the switch in its normally
closed position, circuit 23C is low (ground). When the switch is open, circuit 23C is high (5V).
When the ECM sees circuit 23C high, it causes fan solenoid circuit 23D to be at a HIGH state (12V), which
de-energizes the fan solenoid, engaging the fan clutch. When this occurs, the fan clutch will remain engaged
for a minimum of three minutes after the A/C pressure switch returns to a closed position, to reduce fan cycling.
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158 5 ELECTRICAL TROUBLESHOOTING FANS
Refer to circuit diagram HORTON AND KYSOR ENGINE FAN WITH N14E ENGINES circuits in CTS-5298
or S08225.
To turn the fan off: The ECM applies 12 volts through the 21–way ECM Interface connector (251) to circuit
23D to the fan solenoid (227), causing the solenoid to energize, turning off the air pressure which keeps the
fan engaged. The fan is spring loaded in the disengaged position.
A. When the ECM senses the engine coolant has reached the preset temperature limit, the ECM
turns off the voltage to circuit 23D. This causes the fan solenoid to de-energize, which applies air
pressure to the fan clutch engaging the fan.
B. The second way the fan is turned on is when the A/C compressor head pressure exceeds 300
psi, the A/C high pressure switch (228) opens and removes the ground on circuit 23C to ECM
connector terminal T. The ECM will turn off 12 volts on circuit 23D. This causes the fan solenoid to
de-energize, which applies air pressure to the fan clutch engaging the fan. When the A/C head
pressure drops below 210 psi, the switch closes, the ECM applies 12 volts to circuit 23D which
energizes the fan solenoid and the fan turns off.
Kysor Engine Fan Controls With ECM Control System
To turn the fan off: The ECM applies 12 volts through the 21–way ECM interface connector (251) to circuit
23D to the fan solenoid (227), causing the solenoid to energize, turning on the air pressure which overrides
the fan clutch spring, turning the fan off.
A. When the ECM senses the engine coolant has reached the preset temperature limit, the ECM
turns off the voltage to circuit 23D. This causes the fan solenoid to de-energize, which applies air
pressure to the fan clutch engaging the fan.
B. The second way the fan is turned on is when the A/C compressor head pressure exceeds 300
psi, the A/C high pressure switch (228) opens and removes the ground on circuit 23C to ECM
connector terminal T. The ECM will turn off 12 volts on circuit 23D. This causes the fan solenoid to
de-energize, which applies air pressure to the fan clutch engaging the fan. When the A/C head
pressure drops below 210 psi, the switch closes, the ECM applies 12 volts to circuit 23D which
energizes the fan solenoid and the fan turns off.
Refer to circuit diagram HORTON AND KYSOR ENGINE FAN WITH AHD and ISM ENGINES circuits in
CTS-5298 or S08225.
To turn the fan off: When the optional engine fan override switch is not installed, the ECM applies 12 volts on
circuit 23A from ECM connector (1093) terminal 28 circuit 23D to the fan solenoid (227), causing the solenoid
to energize, turning off the air pressure that keeps the fan engaged. The fan is spring loaded in the disengaged
position. The solenoid is grounded through circuit 23–GA and 11–GC.
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5 ELECTRICAL TROUBLESHOOTING FANS 159
When the optional engine fan override switch is installed, the solenoid is energized by 12 volts on circuit
23A from ECM connector (1093) terminal 28 through switch (659), which then applies the voltage on circuit
23D to the fan solenoid (227), causing the solenoid to energize, turning off the air pressure that keeps the
fan engaged. The fan is spring loaded in the disengaged position. The solenoid is grounded through circuit
23–GA and 11–GC.
The engine fan override switch has an indicator lamp which will light, during the time the fan would normally be
off, when the override switch is on. The 12V signal on circuit 23A from ECM connector (400) terminal 28 will
flow through the LED in switch (659). The LED is grounded through circuit 23–GY.
The engine fan override switch is illuminated with an LED. 12 volts from the panel feed adapter (503) is
supplied on circuit 62M. Ground for the LED is supplied on circuit 11–GR.
A. When the ECM senses the engine coolant has reached the preset temperature limit, the ECM
turns off the voltage to circuit 23D. This causes the fan solenoid to de-energize, which applies air
pressure to the fan clutch engaging the fan.
B. The second way the fan is turned on is when the A/C compressor head pressure exceeds 300 psi,
the A/C high pressure switch (228) opens the fan solenoid circuit. This causes the fan solenoid to
de-energize, which applies air pressure to the fan clutch engaging the fan. When the A/C head
pressure drops below 210 psi, the switch closes, energizing the fan solenoid and the fan turns off.
To turn the fan off: The ECM applies 12 volts through the 21–way ECM interface connector (251) to circuit
23A, which is connected to the normally closed A/C high pressure switch (228), which then applies the voltage
on circuit 23D to the fan solenoid (227), causing the solenoid to energize, turning on the air pressure which
overrides the fan clutch spring, turning the fan off.
When the optional engine fan override switch is not installed, the solenoid is energized by a 12V signal
on circuit 23A from ECM connector (400) terminal 28. The solenoid ground circuit, 23–GA, is grounded
through circuit 11–GC.
When the optional engine fan override switch is installed, the solenoid is energized by a 12V signal on circuit
23A from ECM connector (400) terminal 28 through switch (659). The solenoid ground circuit 23–GA, is
grounded through circuit 11–GC.
The engine fan override switch has an indicator lamp which will light when the override switch is on. The 12V
signal on circuit 23A from ECM connector (400) terminal 28 will flow through the LED in switch (659). The
LED is grounded through circuit 23–GY.
The engine fan override switch is illuminated with an LED. 12 volts from the panel feed adapter (503) is
supplied on circuit 62M. Ground for the LED is supplied on circuit 11–GR.
Refer to circuit diagram HORTON AND KYSOR ENGINE FAN WITH I6 HUEI ENGINES circuits in CTS-5298
or S08225.
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160 5 ELECTRICAL TROUBLESHOOTING FANS
To turn the fan off: The ECM applies a ground through the gray engine connector, pin 8, to fan control
connector (1075) terminal A. Circuit 97EFS, from engine fan control connector (1075) terminal A, connects
to the fan solenoid (227), causing the solenoid to energize, turning off the air pressure that keeps the fan
engaged. The fan is spring loaded in the disengaged position. 12 volts is supplied to fan solenoid connector
(227), terminal A from key switch (40) through circuit 13, circuit 13U, fuse F9–A, circuit 23 and circuit 23D.
A. When the ECM senses the engine coolant has reached the preset temperature limit, the ECM
removes the ground from circuit 97EFS. This causes the fan solenoid to de-energize, which
applies air pressure to the fan clutch engaging the fan.
B. The second way the fan is turned on is when the A/C compressor head pressure exceeds a preset
limit the A/C high pressure switch (228) opens and signals the EC to engage the fan. When the A/C
head pressure drops below a preset limit the switch closes, signaling the ECM to turn the fan off.
To turn the fan off: The ECM applies a ground on circuit 97EFS from engine fan control connector (1075)
terminal A to the fan solenoid (227), causing the solenoid to energize, turning on the air pressure which
overrides the fan clutch spring, turning the fan off. 12 volts is supplied to fan solenoid connector (227), terminal
A from key switch (40) through circuit 13, circuit 13U, fuse F9–A, circuit 23 and circuit 23D.
Turning the fan on: The fan is turned on similarly to the Horton fan except air pressure is removed when the
solenoid is de-energized. This permits the fan clutch spring to engage the fan.
3. TROUBLESHOOTING
A. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of
charge (SOC) or higher. This represents an open circuit voltage (OCV) of 12.4 volts. Batteries
with an OCV of 12 volts or less are either completely discharged or have a dead cell.
B. Before beginning these test procedures, check any light or indicator lamp filaments that are
suspected of being open (burned out). This is done to avoid unnecessary extensive circuit checks.
C. Before beginning these test procedures, inspect all connectors for loose or damaged pins,
wires, etc. Refer to TEST EQUIPMENT AND CONNECTOR REPAIR section in GROUP 08 —
ELECTRICAL in the CTS-5000 Master Service Manual.
D. When the technician determines that a fuse is blown, while checking its condition, he is directed
to locate the cause of the overload condition and to repair it. While no further instruction on this
procedure is listed in the diagnostic tables, the common procedure is as follows: isolate sections
of the circuit, by disconnecting connectors, and measure the resistance to ground to find the circuit
that is shorted to ground. Then locate the damaged spot in the wire or connector and repair.
E. Diagnostics for circuits that are malfunctioning by sticking in the on position are generally not
covered in detail. It is assumed that the technician knows to check for a malfunctioning switch,
relay, or solenoid.
3.1. ENGINE COOLING FAN CONTROLS, HORTON AND KYSOR WITH CATERPILLAR
C–10, C-12 AND 3406E
Testing Fan Solenoid and Circuits
Refer to HORTON and KYSOR ENGINE FAN WITH C10, C12 AND 3406E ENGINES circuit diagram in
CTS-5298 or S08225.
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5 ELECTRICAL TROUBLESHOOTING FANS 161
Before beginning this test procedure, inspect all connectors for loose or damaged pins, wires, etc.
International OEM connector (400) mates with Caterpillar ECM OEM connector. This is an AMP 40–pin
connector, with the International side having female terminals (sockets) and the Caterpillar side having pins.
NOTE – No tests in this manual require testing “into” the Caterpillar OEM connector.
When testing the International side of connector (400), never insert meter probes into the sockets, as
the probes will damage the sockets. Always use test leads of the type described in Inspecting Electrical
Connectors, Test Leads of this manual. The test leads must fit snugly into the sockets without expanding
the sockets.
NOTE – Disconnecting (400) from the ECM will cause incremental amounts of Trip Data to be lost.
An “Event Recorder Data Lost” code may also be logged. The loss of this data will not affect engine
operation, but will affect the accuracy of the data. Ask the owner/operator if they want data recorded
before disconnecting.
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162 5 ELECTRICAL TROUBLESHOOTING FANS
Refer to HORTON & KYSOR ENGINE FAN WITH C–10, C–12 and 3406E ENGINES circuit diagram in
CTS-5298 or S08225.
Before beginning this test procedure, inspect all connectors for loose or damaged pins, wires, etc.
NOTE – Perform the preceding test, Testing Fan Solenoid and Circuits, before performing this test.
Table 31 Testing A/C Compressor High Pressure Switch (228) and Circuits
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF
POINTS SPEC. SPEC.
1. Off Disconnect connectors A/C pressure <5 ohms. Go to next Replace switch.
(228) and (400). At switch. step.
A/C pressure switch,
measure resistance
across the switch
terminals. (If you
suspect the switch is
not opening at 300 PSI,
replace switch.)
2. Off Measure resistance (400) <5 ohms. Go to next Locate open in
from (400) terminal 5, terminal 5 step. circuit 23-G or
circuit 97-G, to (228) to (228) 97-G between
terminal B, circuit 23-G. terminal B. (400) and (228),
then repair.
3. Off Measure resistance (400) >5 ohms. Go to next Locate open
from (400) terminal 41 terminal 41 step. in circuit 23C
to (228) terminal A, to (228) between (400)
circuit 23C. terminal A. and (228), then
repair.
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5 ELECTRICAL TROUBLESHOOTING FANS 163
Table 31 Testing A/C Compressor High Pressure Switch (228) and Circuits (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF
POINTS SPEC. SPEC.
4. Off Measure resistance (400), >100K Go to next Locate short to
from (400) terminal 41 terminal 41 ohms. step. ground in circuit
to ground. to ground. 23C, then repair.
5. Off The A/C high pressure
switch circuits check
good. Reconnect
(400) and (228). If you
suspect the A/C switch
is not working properly,
replace the switch and
test system operation.
Refer to HORTON & KYSOR ENGINE FAN WITH C-10, C-12 and 3406E ENGINES circuit diagram in
CTS-5298 or S08225.
This switch is intended to last the life of the truck. If it is determined to be defective it should be replaced. It
is not a repairable item.
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164 5 ELECTRICAL TROUBLESHOOTING FANS
3.2. ENGINE COOLING FAN CONTROLS, HORTON AND KYSOR WITH DETROIT
DIESEL SERIES 60 DDEC III
Testing Fan Solenoid and Circuits
Refer to HORTON & KYSOR ENGINE FAN WITH SERIES 60 ENGINES circuit diagram in CTS-5298
or S08225.
Before beginning this test procedure, inspect all connectors for loose or damaged pins, wires, etc.
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Refer to HORTON and KYSOR ENGINE FAN WITH SERIES 60 ENGINES circuit diagram in CTS-5298
or S08225.
Before beginning this test procedure, inspect all connectors for loose or damaged pins, wires, etc.
NOTE – Perform preceding test, Testing Solenoid and Circuits, before performing this test.
Table 34 Testing A/C Compressor High Pressure Switch (228) and Circuits
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off Remove connector (273) (273), F1 >100K Go to next Locate short to ground
from ECM. Disconnect to gnd. ohms. step. in circuit 23C between
connector (228) from connectors (273) and
A/C pressure switch. At (228), then repair.
connector (273) terminal
F1, measure resistance
to gnd.
2. Off With A/C pressure switch A/C <5 ohms. Go to next Replace switch.
disconnected, measure pressure step.
resistance between switch.
switch terminals.
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Table 34 Testing A/C Compressor High Pressure Switch (228) and Circuits (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
3. Off At connector (228) (228), <5 ohms. Go to next Locate open or poor
measure resistance to 23-GB to step. connection in circuit
ground at circuit 23-GB. gnd. 23-GB or path to
ground at neg. battery
terminal, then repair.
4. Off Connect (228) to switch. (273), F1 <5 ohms. Go to next Locate open or
At connector (273) to gnd. step. poor connection in
terminal F1, measure circuit 23C between
resistance to ground. connectors (273) and
(228), then repair.
5. Off A/C high pressure switch
and circuits check good.
If you suspect that the
A/C high pressure switch
is not opening at the
correct pressure, replace
the switch and retest.
3.3. ENGINE COOLING FAN CONTROLS, HORTON AND KYSOR WITH CUMMINS
M11 AND N14 CELECT
Testing Fan Solenoid and Circuits
Refer to HORTON and KYSOR ENGINE FAN WITH N14 ENGINE circuit diagram in CTS-5298 or S08225.
Before beginning this test procedure, inspect all connectors for loose or damaged pins, wires etc.
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5 ELECTRICAL TROUBLESHOOTING FANS 167
Refer to HORTON and KYSOR ENGINE FAN WITH N14 ENGINE circuit diagram in CTS-5298 or S08225.
Before beginning this test procedure, inspect all connectors for loose or damaged pins, wires etc.
NOTE – Perform preceding test, Testing Fan Solenoid and Circuits, before performing this test.
Table 36 Testing A/C Compressor High Pressure Switch (228) and Circuits
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off Disconnect connectors A/C pressure <5 ohms. Go to Replace switch.
(251), (252) and (190). switch. next
At A/C pressure switch, step.
measure resistance
across the switch
terminals. (If you
suspect the switch is
not opening at 300 PSI,
replace switch.)
2. Off Measure resistance (251), <5 ohms. Go to Locate open in
from (251) terminal T to terminal T to next circuit 23C between
(228) terminal A. (228) terminal step. (251) and (228),
A. then repair.
3. Off Measure resistance (251), >100K Go to Locate short to
from (251) terminal T to terminal T to ohms. next ground in circuits
ground. gnd. step. 23C, then repair.
4. Off Measure resistance (252) terminal <5 ohms. Go to Locate open in
from (252) terminal 10 10 to (228) next circuit 23-GB or
to (228) terminal B. terminal B. step. 97-G between (252)
and (228), then
repair.
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Table 36 Testing A/C Compressor High Pressure Switch (228) and Circuits (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
5. Off Measure resistance (190) terminal <5 ohms. Go to Locate open in
from (190) terminal V to V to (228) next circuit 23-GB or
(228) terminal B. terminal B. step. 97-GA between
(252) and (190).
Repair condition.
6. Off Reconnect connectors.
The A/C pressure switch
circuits and components
check good.
3.4. ENGINE COOLING FAN CONTROLS, HORTON AND KYSOR WITH CUMMINS
ISM AND AHD
Testing Fan Solenoid and Circuits
Refer to HORTON and KYSOR ENGINE WITH AHD and ISM ENGINE circuit diagram in CTS-5298 or S08225.
Before beginning this test procedure, inspect all connectors for loose or damaged pins, wires, etc.
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Refer to HORTON and KYSOR ENGINE WITH AHD and ISM ENGINE circuit diagram in CTS-5298 or S08225.
Before beginning this test procedure, inspect all connectors for loose or damaged pins, wires, etc.
NOTE – Perform preceding test, Testing Fan Solenoid and Circuits, before performing this test.
Table 38 Testing A/C Compressor High Pressure Switch (228) and Circuits
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off Disconnect connectors A/C <5 ohms. Go to Replace switch.
(251), (252) and (190). pressure next
At A/C pressure switch, switch. step.
measure resistance
across the switch
terminals. (If you suspect
the switch is not opening
at 300 PSI, replace
switch.)
2. Off Measure resistance from (251) <5 ohms. Go to Locate open in circuit
(251) terminal T to (228) terminal T next 23C between (251) and
terminal A. to (228) step. (228), then repair.
terminal A.
3. Off Measure resistance (251), >100K Go to Locate short to ground
from (251) terminal T to terminal T ohms. next in circuits 23C, then
ground. to gnd. step. repair.
4. Off Measure resistance from (252) <5 ohms. Go to Locate open in circuit
(252) terminal 10 to (228) terminal next 23-GB or 97-G between
terminal B. 10 to (228) step. (252) and (228), then
terminal B. repair.
5. Off Measure resistance from (190) <5 ohms. Go to Locate open in circuit
(190) terminal V to (228) terminal V next 23-GB or 97-GA
terminal B. to (228) step. between (252) and
terminal B. (190). Repair condition.
6. Off Reconnct connectors.
The A/C pressure switch
circuits and components
check good.
Refer to HORTON and KYSOR ENGINE FAN WITH AHD and ISM ENGINE circuit diagram in CTS-5298
or S08225.
This switch is intended to last the life of the truck. If it is determined to be defective it should be replaced. It
is not a repairable item.
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Before beginning these test procedures, inspect all connectors for loose or damaged pins, wires, etc.
CEC module connector (379) mates with the ECM connector. This is a 60–pin connector, with the chassis
side having female terminals (sockets) and the engine side having pins.
NOTE – No tests in this manual require testing “into” the black ECM connector.
When testing the chassis side of connector (379), never insert meter probes into the sockets, as the
probes will damage the sockets. Always use breakout box (ZTSE-4445) as described in International
Engine/Vehicle Manual EGES-175.
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Refer to HORTON and KYSOR ENGINE FAN WITH I6 HEUI ENGINE circuit diagrams in CTS-5298 or S08225.
Before beginning this test procedure, inspect all connectors for loose or damaged pins, wires, etc.
NOTE – Perform preceding test, Testing Fan Solenoid and Circuits, before performing this test.
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Table 41 Testing A/C compressor High Pressure Switch (228) and Circuits
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off Disconnect connectors A/C <5 ohms. Go to Replace switch.
(228) and (379). At A/C pressure next
pressure switch, measure switch. step.
resistance across the
switch terminals. (If you
suspect the switch is
not opening at 300 PSI,
replace switch.)
2. Off Measure resistance from (379) <5 ohms. Go to Locate open in circuit
(379) terminal 33, circuit terminal 33 next 23A between (400)
23A to (228) terminal A. to (228) step. and (228), then repair.
terminal A.
3. Off Measure resistance from (379) >100K Go to Locate short to ground
(379) terminal 33 to terminal 33 ohms. next in circuit 23A, then
ground. to ground. step. repair.
4. On Turn on key switch. (228) 12 ± 1.5 Go to Locate open or poor
Measure voltage from terminal B volts. next connection in circuits
(228) terminal B to to ground. step. between connector
ground. (228) and key switch
(40), then repair.
5. Off The A/C high pressure
switch circuits check
good. Reconnect (379)
and (228). If you suspect
the A/C switch is not
working properly, replace
the switch and test system
operation.
4. COMPONENT LOCATIONS
(2) Dash Panel Connector.. . .. . .. .. . .. .. . .. .. . .. .. . ... . . . . . Right Side of Engine Cowl, Above Connector 3
(3) Dash Panel Connector.. . .. . .. .. . .. .. . .. .. . .. .. . ... . . . . . Right Side of Engine Cowl, Below Connector 2
(227) Fan Solenoid. . .. . .. .. . .. . .. . .. . .. . .. . .. . .. . .. . ... . . . . . At Front of Engine (Outside Dash Panel, Left Side, with
Cummins ISM and AHD)
(228) A/C Pressure Switch. . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . On A/C Compressor
(251) CELECT 21–Way ECM Connector. . . . . . . . . . .. . . . . . At Engine Harness Near ECM (With M11E and N14E)
(273) Detroit Diesel ECM Connector . . . . . . . . . . . . . . .. . . . . . To ECM Mounted on Dash Engine Side (With Detroit
Diesel)
(379) CEC Module Connector. . . . . . . . . . . . . . . . . . . . . . .. . . . . . On Engine (With I6 HEUI)
(400) OEM Interface Connector. . . . . . . . . . . . . . . . . . . . .. . . . . . On Engine (With C-10, C-12 and 3406E)
(659) Engine Fan Override Switch. . . . . . . . . . . . . . . . . .. . . . . . At Switch Cluster
(1074) Engine Fan Control Connector. . . . . . . . . . . . . .. . . . . . On Engine (With I6 HEUI)
(1093) ECM Interface Connector. . . . . . . . . . . . . . . . . . . .. . . . . . On Engine (With ISM and AHD)
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Figure 75 Engine Fan Wiring, Caterpillar 3406E (Viewed From Top of Engine)
1. CIRCUIT 77C
2. ENGINE HARNESS
3. FAN CIRCUITS TO ENGINE WIRING AT DASH PANEL
4. A/C HIGH PRESSURE CUT–OUT (228)
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Table of Contents
1. DESCRIPTION. .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .187
2. OPERATION.. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .188
2.1. ECM POWER CIRCUITS.. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .188
2.2. VEHICLE SPEED SENSOR. . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .188
2.3. COOLANT LEVEL SENSOR. . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . .188
2.4. ATA DATALINK CONNECTOR.. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .189
2.5. J1939 DATA LINK. . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . .189
2.6. CRUISE CONTROL. .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .189
2.7. SERVICE BRAKE SWITCH.. .. .. .. .. .. . .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .190
2.8. CLUTCH SWITCH.. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .190
2.9. VEHICLE SPEED SENSOR. . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .190
2.10. SPEEDOMETER/TACHOMETER CONNECTOR. . .. .. . .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. . .. .190
2.11. THROTTLE POSITION SENSOR.. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .191
2.12. ENGINE BRAKE. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. .191
2.13. ANTILOCK BRAKE SYSTEM. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .192
2.14. IDLE SHUTDOWN TIMER. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .192
3. TROUBLESHOOTING. .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .193
3.1. DETERMINING FAULT CODES.. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .193
Reading Flash Codes .. . .. .. .. .. . .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .193
3.2. IMPORTANT STEPS BEFORE TESTING. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .195
3.3. INSPECTING ELECTRICAL CONNECTORS. . . . . . . .. . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . .195
Visual Inspection. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .195
Performing Electrical Tests At International Connection (400) To ECM.. .. .. .. .. .. .. .. .. 196
Test Leads.. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .196
Replacing International Components. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . .196
3.4. TESTING HELLA RELAY. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .196
3.5. TESTING ELECTRICAL POWER SUPPLY TO ECM. .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. .197
Testing Switched Power Supply To ECM. . . . . .. . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . .. . . . . .197
Testing Unswitched Battery Feed To ECM. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..197
3.6. DIAGNOSTIC CONNECTOR (137) AND DATA LINK CIRCUITS. . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .198
Testing Diagnostic Connector Power and Ground Circuits. . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .198
Testing Diagnostic Connector and Speedometer/Tachometer Positive and Negative
Data Link Circuits.. . .. . .. . . .. . .. . . .. . .. . .. . . .. . .. . .. . . .. . .. . . .. . .. . .. . . .. . .. . . .. . .. . .. . . .. . .. . .199
3.7. THROTTLE POSITION SENSOR (TPS). . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . .201
Testing Throttle Position Sensor (TPS) and Circuits. . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .201
3.8. VEHICLE SPEED SENSOR (VSS). .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .202
Inspecting And Adjusting the Adjustable Vehicle Speed Sensor (VSS). . . . . . . . . . . . . . . . . .202
Testing Vehicle Speed Sensor (VSS).. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .202
Testing Vehicle Speed Sensor (409). .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .203
Testing Vehicle Speed Sensor To ECM Circuits. .. . .. . . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .203
3.9. CRUISE AND PTO CONTROLS. . . . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .204
Testing Cruise On/Off Switch and Circuits. . .. . .. . .. . . .. . .. . . .. . .. . .. . . .. . .. . .. . . .. . .. . . .. . .. . .205
Testing Cruise Set/Resume Switch and Circuits. . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . .205
3.10. CLUTCH SWITCH (55).. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. 206
Testing Clutch Switch and Circuits.. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .206
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 187
1. DESCRIPTION
The C-10, C-12 and 3406E engines use the ADEM III electronic controller. This controller provides engine
and vehicle functions including:
ENGINE FUNCTIONS
A. Electronic Governing*
B. Fuel/Air Ratio Control*
C. Injection Timing Control*
D. Service Diagnostics**
E. Torque Rise Shaping*
F. Trip Data Recording*
*Caterpillar System
**Caterpillar/International System
VEHICLE FUNCTIONS
A. Cruise Control*
B. Data Links*
C. Engine Brake Controls*
D. Engine Protection System*
E. Idle Shutdown Timer*
F. Progressive Shifting*
G. PTO Controls*
H. Vehicle Speed Limiting*
*Caterpillar/International System
Certain programmable parameters that affect the engine electronic control systems may be changed with
electronic service tools.
The parameters are stored in the system Electronic Control Module (ECM) and are protected from
unauthorized change by passwords. The programmable parameters are either “System Parameters” or
“Customer Parameters.”
System Configuration Parameters are set at the factory and affect emissions and horsepower ratings within a
family of engines. Factory passwords must be obtained and used to change System Configuration Parameters.
Customer Selectable Parameters are variable, and are used to specify operating parameters for: cruise
control, PTO operation, vehicle speed limits, progressive shifting, type of engine protection system, RPM
and horsepower ratings within the engine family . Customer passwords are needed to change Customer
Parameters.
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188 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
Since each C-10, C-12 or 3406E control system is electronically programmable to individual owner
specifications, the operating parameters will vary from vehicle to vehicle.
Some of these parameters may cause the engine to operate in a way that the driver (or service technician)
does not expect, if proper training has not taken place. This may lead to power or performance complaints
and/or service time, when the engine is operating correctly.
International provides an ATA Diagnostic connector (137) for connecting an Electronic Service Tool (EST) to
the electronic engine control system. The Diagnostic connector is located on the instrument panel left side.
2. OPERATION
Refer to CATERPILLAR C-10 and C-12 and 3406E ENGINE circuit diagrams CTS-5298 or S08225.
This section describes specific electrical operation of International installed circuits and components,
referencing specific circuits, connectors and components by number.
Battery power from the (+) battery terminal of the cranking motor solenoid is always applied on circuits 97B
and 97C through connector (400) terminals 52 and 53 to the ECM. These circuits are protected by fuses
(217) and (218).
Refer to 12V CHARGING and CRANKING WITH CATERPILLAR C-10, C-12 and 3406E ENGINES circuit
diagrams CTS-5298 or S08225.
The ECM uses this power to maintain a portion of memory used for customer trip data accumulators.
Disconnecting this circuit does not affect engine operation or factory/customer parameters or logged diagnostic
codes. Refer to the Caterpillar Troubleshooting Manual for additional information on this feature.
Two types of sensors are available. The threaded (adjustable) sensor is used on most transmissions.
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 189
coolant level switch connects to the engine harness at connector (249). Four circuits from connector (402)
connect the low coolant switch to the ECM through the 21–way ECM connector (400).
The coolant level switch (402) receives a 5 volt signal on circuit 34B(5V) from the ECM (400). When the
coolant level is above the probe, the switch sends a high signal (3.5 volts minimum) on circuit 34A and a low
signal (0.5 volt maximum) on circuit 34 to the ECM (400).
When the coolant level is below the probe, the switch sends a low signal (0.5 volt maximum) on circuit 34A and
a high signal (3.5 volts minimum) on circuit 34 to ECM (251).
The low coolant level switch is grounded through circuit 34–G to ECM (251).
NOTE – The low coolant level switch cannot be tested with a multimeter in the ohmmeter mode. This is
due to the fact that the switch is an electronic switch and not a mechanical switch.
A. Circuit 98A(+) is the positive data link connection, and it is fed by the positive data link connector
(514), connector (190), circuit 98B(+) and circuit 98(+) coming from the ECM connector (400).
B. Circuit 98C(-) is the negative data link connection, and it is fed by the negative data link connector
(515), circuit 98B(-), connector (190), and circuit 98B(-) coming from the ECM connector (400).
C. Circuit 97DL is a 12 volt feed and is fed from bat stud (B1) circuit 14W, circuit 14AA, 20A fuse
F5–D, and circuit 97DL. Thus it provides power for the electronic service tool.
D. Circuits 11–GR and 11–GT connect to the panel light ground adapter (506) and provide a ground
for the electronic service tool.
A. Circuit 98YL(+) is the positive data link connection. It originates from ECM connector (400),
terminal 50. The circuit is connected to J1939 terminating resistor connector (1098), terminal A
and J1939 backbone connector (1097), terminal A.
B. Circuit 98GN(-) is the negative data link connection. It originates from ECM connector (400),
terminal 34. The circuit is connected to J1939 terminating resistor connector (1098), terminal C
and J1939 backbone connector (1097), terminal B.
C. Circuit 98SHD is the data link shield connection. It originates from ECM connector (400), terminal
42. The circuit is connected to J1939 terminating resistor connector (1098), terminal B and J1939
backbone connector (1097), terminal C.
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190 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
The cruise on/off switch is lighted to allow for easy location in the dark. Cruise on/off switch circuit 97AE is an
input to the ECM at connector (400) terminal 20. The ground side of the on/off switch is connected through
circuits 97–GC, 97–GB, 97–GA and 97–G to connector (400) terminal 5. With the switch on, the ECM sees 0
volts at connector (400) terminal 20. With the switch off, the ECM sees 5 volts at connector (400) terminal 20.
The cruise set/resume switch is lighted to allow for easy location in the dark. Set/resume switch terminal 2 is
connected to the ECM through circuits 97–GB, 97–GA and 97–G to the connector (400) terminal 5. Set/resume
switch Set terminal 3 is an input (circuit 97AB) to the ECM through connector (400) terminal 35. Set/resume
switch Resume terminal 1 is an input (circuit 97AA) to the ECM through connector (400) terminal 44.
With the set/resume switch in the set position, the ECM sees 0 volts at connector (400) terminal 35 and
5 volts at terminal 44.
In resume position, the ECM sees 5 volts at connector (400) terminal 35 and 0 volts at terminal 44.
In the set/resume neutral position, the ECM sees 5 volts at both connector (400) terminals 35 and 44.
The clutch switch connects to the cab harness at connector (294). Clutch switch circuit 97AH is an input to the
ECM through connector (400) terminal 22. The ground side of the clutch pedal switch is grounded through
circuits 97–GH, 97–GA, and 97–G to connector (400) terminal 5. With the driver’s foot off the clutch pedal
(switch closed), the ECM sees 0 volts at terminal 22. When the driver depresses the clutch pedal (switch
opens), the ECM sees 5 volts at terminal 22.
Data link negative connector (515) terminal C is connected by circuit 47/48(-) to speedometer/tachometer
connector (421). Data link negative connector (515) terminal A is connected by circuit 98C(-) to the ATA data
link connector (137) terminal B. ATA data link connector (137) can be used to access information on the
data link using an electronic service tool.
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 191
The pedal mounted throttle position sensor is attached directly to the throttle pedal assembly and requires
no adjustment. This sensor can be replaced separately from the throttle pedal assembly, however, an
incorrectly calibrated pedal mounted throttle position sensor assembly cannot be calibrated — the pedal
assembly must be replaced.
Refer to circuit diagram CATERPILLAR C-10, C-12, or 3406E — CRUISE CONTROL in CTS-5298 or S08225.
The TPS connects to the cab harness at three-pin connector (404). When the ECM is powered (key switch
on), the TPS receives operating voltage (8 volts) at terminal A on circuit 99A which is connected to ECM
connector (400) terminal 4. TPS terminal B is grounded by circuit 99–GA, 97–GA, 97–G through ECM
connector (400) terminal 5.
TPS terminal C outputs the variable throttle position signal on circuit 99 to ECM connector (400) terminal 66.
The pedal mounted TPS should produce a Duty Cycle of 10 to 22 percent at low idle and 75 to 90 percent at
full throttle. An electronic service tool can be used to monitor the signal. The percent duty cycle is translated in
the ECM into a throttle position percentage of 3 to 100%.
For a complete description of engine brake operation, refer to the appropriate Caterpillar Service Manual.
There are two owner selected engine brake operation modes, which are COAST and LATCH.
If the COAST mode (standard mode) is selected, the engine brake operates when:
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192 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
• The engine brake operates when the driver applies the service brake, but the engine brake continues
to operate (latches on, so to speak) after the driver takes his foot off the brake. The engine brake stays
engaged (latched on) until one of the other ECM inputs changes: clutch pedal depressed, throttle pedal
depressed, engine speed drops below 800 rpm or the brake pedal is depressed a second time.
Control of the engine brake is shared by the driver and the ECM. The driver turns the engine brake on or off
and selects how much engine brake is desired (number of cylinders). The ECM monitors certain engine
parameters, then enables the engine brake system when all conditions are acceptable.
An on/off switch (434) is used to enable (turn on) the engine brake control system. With the on/off switch
closed, the circuit between ECM connector (400) terminal 5 and the engine brake selector switch terminal 2
is complete.
The engine brake selector switch (433) has three circuits: Low, Medium and a common or ground circuit
connected to the engine brake on/off switch.
Selector switch terminal 2 is connected by circuit 24A to the engine brake on/off switch (434) at terminal 5.
When the on/off switch is on, the circuit between the engine brake selector switch (433) terminal 2 and ECM
connector (400) terminal 5 is complete.
With the selector switch (433) in the Low position, the ECM sees a 0 volt signal at connector (400) terminal 23
and a 5 volt signal at terminal 40.
With the selector switch (433) in the Medium position, the ECM sees a 0 volt signal at connector (400) terminal
40 and a 5 volt signal at terminal 23.
With the selector switch (433) in the High position, the ECM sees a 0 volt signal at connector (400) terminals
40 and 23.
The timer is activated and the countdown (from the customer selected time) begins when:
Ninety seconds before the programmed time is reached, the Yellow Serv/Check Engine light will begin to flash
rapidly. If the driver moves the clutch (294) or service brake (141) pedal during this 90–second time period, the
clutch switch (294) or the brake switch (141) contacts will open up and the timer will be overridden until it is
reset. The timer is reset and begins counting over by moving the vehicle a short distance.
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 193
A code (Override of Idle Shutdown Timer) will be logged when the driver overrides the timer within the
90–second time period. If the timer is activated and allowed to shut down the engine, then a code (Idle
Shutdown Timed Out) will be set. These codes record an event — they do not indicate a fault in the system.
IMPORTANT – Note that the system shuts the engine down, but does not turn off power to the vehicle.
3. TROUBLESHOOTING
A. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of
charge (SOC) or higher. This represents an open circuit voltage (OCV) of 12.4 volts. Batteries
with an OCV of 12 volts or less are either completely discharged or have a dead cell.
B. Before beginning these test procedures, check any light or indicator lamp filaments that are
suspected of being open (burned out). This is done to avoid unnecessary extensive circuit checks.
C. Before beginning these test procedures, inspect all connectors for loose or damaged pins,
wires, etc. Refer to TEST EQUIPMENT AND CONNECTOR REPAIR section in GROUP 08 -
ELECTRICAL in the CTS-5000 Master Service Manual.
D. When the technician determines that a fuse is blown, while checking its condition, he is directed
to locate the cause of the overload condition and to repair it. While no further instruction on this
procedure is listed in the diagnostic tables, the common procedure is as follows: isolate sections
of the circuit by disconnecting connectors, and measure the resistance to ground to find the circuit
that is shorted to ground. Then locate the damaged spot in the wire or connector and repair.
E. Diagnostics for circuits that are malfunctioning by sticking in the on position are generally not
covered in detail. It is assumed that the technician knows to check for a malfunctioning switch,
relay, or solenoid.
During normal vehicle start-up, turning the key to the on position causes the Serv/Check Engine light to come
on as a system test. The light remains on for about six seconds, then goes off. If the Serv/Check Engine light
stays on after the initial start-up, the ECM has detected a problem with the system.
All C-10, C-12 and 3406E equipped vehicles have a yellow Serv/Check Engine light located in the left gauge
cluster. This light communicates engine status.
If during vehicle operation, the Serv/Check Engine light comes on, that indicates an active fault is present. The
light will remain on, but blink approximately every five seconds for a brief 1/2 second.
The yellow Serv/Check Engine light can be used to read fault codes by following the procedure in the following
paragraph.
1. Turn the key to the on position. The yellow Serv/Check Engine light will turn on for approximately five
seconds, then turn off for several more seconds, then begins to FLASH any logged codes.
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194 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
2. The yellow Serv/Check Engine light will FLASH the first digit. At the end of first digit there is a one
or two second pause.
3. The yellow Serv/Check Engine light will FLASH the second digit. At the end of the second digit there will
be a two or three second pause before the next fault code number is FLASHED.
4. The second and all successive fault codes will FLASH until all codes have been FLASHED. It will stop
FLASHING after the last code has been flashed. To see the fault codes again, repeat the process.
5. Flash code 55 indicates that there are no logged diagnostic codes. For a listing of Caterpillar Flash
codes, refer to the Caterpillar Electronic Troubleshooting manual. Codes are also listed in the EZ- Tech
or PRO-LINK 9000 manual.
7. Start engine and allow to run at low idle for about 30 seconds.
9. Hold cruise set/resume switch in either position until codes begin to FLASH, then release.
10. The yellow Serv/Check Engine light will FLASH the first digit. At the end of the first digit there is a one
or two second pause.
11. The yellow Serv/Check Engine light will FLASH the second digit. At the end of the second digit there will
be a two or three second pause before the next fault code number is FLASHED.
12. The second and all successive fault codes will FLASH until all codes have been FLASHED. It will stop
FLASHING after the last code has been flashed. To see the fault codes again, repeat steps 4 through 6.
13. Flash code 55 indicates that there are no logged diagnostic codes. For a listing of Caterpillar flash
codes, refer to the Caterpillar Electronic Troubleshooting manual. Codes are also listed in the EZ-Tech
or PRO-LINK 9000 manual.
This section includes diagnostic tables for International– installed circuits and components that are part
of the Caterpillar electronic engine control system.
To begin the process, refer to the appropriate Caterpillar Electronic Troubleshooting Manual and
follow their directions.
If the Caterpillar diagnostics indicate that an International circuit is suspect, use the diagnostic tables included
in this section for a step-by-step procedure. Refer to the appropriate circuit diagram for CATERPILLAR C-10,
C-12 or 3406E ENGINES IN CTS-5298 or S08225.
The EZ-Tech or PRO-LINK 9000 EST’s with the Caterpillar programs can be used to read fault codes,
customer and engine parameters and monitor various switches and sensors.
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 195
2. Verify the problem. Is the complaint due to misunderstood customer selected parameters? Use an EST
to review customer selected parameters.
4. Avoid Preconceived Ideas! Eliminate any non-electrical causes for the problem first (contaminated
fuel, clogged air filters, etc.).
The troubleshooting guide requires checking specific connectors. Use the following steps to determine if
the connector is causing the problem. If a defective condition is found, make the necessary corrections
and continue the process.
1. Check the connector lock mechanism or retaining screw. Make sure the connector is capable of
properly locking the connector together.
2. Perform a 10 pound pull-test on each terminal/wire in the connector. Each terminal/wire assembly
should easily withstand 10 pounds of pull and remain in the connector. This test determines (A) if the
wire is properly in the terminal and (B) if the terminal is properly inserted into the connector. Correct
any defects noted.
3. Visually inspect wiring. Inspect for worn or damaged wires. Check for pinched or damaged harness.
4. Visually inspect connectors. Verify that pins and sockets are free of corrosion, dirt or other contaminants
and damage. Verify correct alignment and location of terminals in the connector.
5. Check individual pins and sockets. This is especially important with an intermittent symptom. Using a
new pin, insert the pin into each socket, one at a time, checking for a good grip on the pin by the socket.
Repeat for each pin on the mating side of the connector, using a new female terminal for the test.
6. Inspect Engine Ground Stud. Inspect this ground and other related grounds for clean, tight connections
that are free of corrosion and/or other defective conditions.
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196 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
International OEM connector (400) mates with Caterpillar ECM connector J1. This is a Deutsch 40–pin
connector, with the International side having female terminals (sockets) and the Caterpillar side having pins.
NOTE – No tests in this manual require testing “into” the Caterpillar J1 connector.
When testing the International side of connector (400), never insert meter probes into the sockets, as the
probes will damage the sockets. Always use test leads of the type described in Test Leads, in the following
paragraph. The test leads must fit snugly into the sockets without expanding the sockets.
Test Leads
To construct test leads, attach an insulated alligator clip to a suitable length of 16 gauge wire. On the other
end, use Deutsch HDT-48–00 Crimp Tool to install male terminal 1651958C1.
Signal Reading Probes, Caterpillar part number 7X1710, can also be used.
When replacing electrical switches, connectors (including pins and sockets), relays or other components, use
only approved International replacement parts. Many of the switches have gold or silver plated contacts and
some of the connectors have gold plated terminals. By using correct replacement parts, you maintain the
design integrity of the system.
All of the relays and other solenoids installed by International are suppressed to prevent voltage spikes from
damaging electrical components. Again, use only International replacements for these components.
The part number and relay circuit diagram are embossed on the relay body. The terminals are numbered on
the relay in the same manner as in the circuit diagrams.
1. With relay removed, measure resistance between terminals 30 and 87A. If resistance is less than 5
ohms, go to step 2; otherwise replace the relay.
2. Measure resistance between terminals 30 and 87. If resistance is 100K ohms or more, go to step 3;
otherwise replace the relay.
3. Using 12V battery source and test leads, connect (+) lead to terminal 85 and (-) lead to terminal 86. If relay
energizes with an audible click sound, go to step 4; otherwise replace the relay.
4. While relay is energized, measure resistance between terminals 30 and 87. If resistance is less than 5
ohms, go to step 5; otherwise replace the relay.
5. While relay is energized, measure resistance between terminals 30 and 87A. If resistance is 100K ohms or
more, the relay is good; otherwise replace relay.
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 197
Procedure for Testing Unswitched Battery Feed To ECM tests the unswitched battery power circuits to the ECM.
NOTE – Disconnecting (400) from the ECM will cause incremental amounts of Trip Data to be lost.
An “Event Recorder Data Lost” code may also be logged. The loss of this data will not affect engine
operation, but will affect the accuracy of the data. Ask the owner/operator if they want data recorded
before disconnecting.
NOTE – Disconnecting (400) from the ECM will cause incremental amounts of Trip Data to be lost.
An “Event Recorder Data Lost” code may also be logged. The loss of this data will not affect engine
operation, but will affect the accuracy of the data. Ask the owner/operator if they want data recorded
before disconnecting.
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198 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 199
Testing Diagnostic Connector and Speedometer/Tachometer Positive and Negative Data Link Circuits
NOTE – Disconnecting (400) from the ECM will cause incremental amounts of Trip Data to be lost.
An “Event Recorder Data Lost” code may also be logged. The loss of this data will not affect engine
operation, but will affect the accuracy of the data. Ask the owner/operator if they want data recorded
before disconnecting.
NOTE – A multimeter cannot be used to measure the voltage of the signal on these circuits.
Table 45 Testing Diagnostic Connector and Speedometer/Tachometer Positive and Negative Data
Link Circuits
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF
POINTS SPEC. SPEC.
1. Off Disconnect conn. (400) (137), 98A >100K Go to next Locate short to
from ECM, and (421) from (+) to gnd. ohms. step. ground, then
speedometer unit. If other repair.
devices are connected at
data link connectors (514)
and (515), disconnect them.
At conn. (137) measure
resistance from terminal A,
circuit 98A(+) to ground.
2. Off At conn. (137) measure (137), >100K Go to next Locate short to
resistance from terminal B, 98C(-) to ohms. step. ground, then
circuit 98C(-) to ground. gnd. repair.
3. Off At conn. (137) measure (137) >100K Go to next Locate short
resistance between terminal between ohms. step. circuit between
A, circuit 98A(+) and terminal 98A(+) and circuits
B, circuit 98C(-). 98C(-). connected to
terminal A
98A(+), 98(+),
47/48(+) and
terminal B98C(-),
98B(-), 47/48(-),
then repair.
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200 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
Table 45 Testing Diagnostic Connector and Speedometer/Tachometer Positive and Negative Data
Link Circuits (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF
POINTS SPEC. SPEC.
4. Off At connector (400), use (137), <5 ohms. Go to next Locate open or
test lead to jumper terminal 98A(+) to step. poor connection
8, circuit 98(+) to gnd. At gnd. in circuit
connector (137) terminal 98A(+) between
A, circuit 98A(+) measure connectors (514)
resistance to ground. and (137) or
open or poor
connection
in circuit
98(+) between
connectors (514)
and (400), then
repair.
5. Off With jumper still in place (421), <5 ohms. Go to next Locate open or
at terminal 7, circuit 98(+), 47/48(+) to step. poor connection
measure resistance to gnd. in circuit 47/48(+)
ground at circuit 47/48(+) between
and connector (421). connectors (421)
and (514), then
repair.
6. Off At connector (400) use test (137) <5 ohms. Go to next Locate open or
lead to jumper terminal 8, between step. poor connection
circuit 98(+) to terminal 98A(+) and in circuit
9, circuit 98B(-). At conn. 98C(-). 98C(-) between
(137) measure resistance connectors (515)
between terminal A, circuit and (137), or
98A(+) and terminal B, open or poor
circuit 98C(-). connection
in circuit
98B(-) between
connectors (515)
and (400), then
repair.
7. Off With jumper still in place, at (421), <5 ohms. Locate open All data link
connector (421) measure 47/48 (-) in circuit circuits check
resistance between 47/48(-) to gnd. 47/48 (-) good.
and ground. between
conn. (421)
and (515),
then repair.
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 201
NOTE – Disconnecting (400) from the ECM will cause incremental amounts of Trip Data to be lost.
An “Event Recorder Data Lost” code may also be logged. The loss of this data will not affect engine
operation, but will affect the accuracy of the data. Ask the owner/operator if they want data recorded
before disconnecting.
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202 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
1. Disconnect engine harness connector (250) from the sensor. Loosen the locknut and remove the sensor.
The harness connector and sensor should be free of damage or corrosion. Remove any metal shavings or
debris from the sensor.
2. To install the adjustable sensor, turn in until the sensor contacts the transmission speedometer gear, then
back out one full turn. Tighten locknut to 15 ft-lbs. (20.3 N•m). This assures that the sensor is adjusted
properly for the next test.
To perform this test construct two test leads using terminals (1680205C1) and suitable length of 16GA wire.
WARNING – A jack must never be used alone to support vehicle. The jack may lower and
serious injury could result. Always support vehicle with floor jacks. Always block wheels to prevent
vehicle from moving.
WARNING – EXTREME CAUTION should be used to prevent personal injury resulting from
contact with rotating vehicle wheels when connecting test leads.
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 203
This procedure tests the International speed sensor circuits between connectors (409) and (400).
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204 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
NOTE – Disconnecting (400) from the ECM will cause incremental amounts of Trip Data to be lost.
An “Event Recorder Data Lost” code may also be logged. The loss of this data will not affect engine
operation, but will affect the accuracy of the data. Ask the owner/operator if they want data recorded
before disconnecting.
The EZ-Tech or Pro-Link Electronic Service Tools (EST) can be used to monitor system parameters relating
to Cruise Control operation. Use the EST to monitor operation of system switches, including the Cruise
On/Off, Set/Resume, service brake and clutch switch.
NOTE – Disconnecting (400) from the ECM will cause incremental amounts of Trip Data to be lost.
An “Event Recorder Data Lost” code may also be logged. The loss of this data will not affect engine
operation, but will affect the accuracy of the data. Ask the owner/operator if they want data recorded
before disconnecting.
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 205
NOTE – Disconnecting (400) from the ECM will cause incremental amounts of Trip Data to be lost.
An “Event Recorder Data Lost” code may also be logged. The loss of this data will not affect engine
operation, but will affect the accuracy of the data. Ask the owner/operator if they want data recorded
before disconnecting.
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206 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
NOTE – If the vehicle is equipped with an Allison transmission, this switch is replaced with a jumper
connection.
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 207
The clutch switch should be mounted so that the switch actuator makes contact with the clutch pedal arm when
the arm is depressed 0.5 inch at the point of actuator contact. The bracket can be bent forward or backward for
adjustment. An audible click (switch closing) should be heard when the pedal is released.
NOTE – Disconnecting (400) from the ECM will cause incremental amounts of Trip Data to be lost.
An “Event Recorder Data Lost” code may also be logged. The loss of this data will not affect engine
operation, but will affect the accuracy of the data. Ask the owner/operator if they want data recorded
before disconnecting.
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208 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 209
NOTE – Do not use meter to test low coolant sensor. It may cause damage to the circuit board located
in the sensor.
NOTE – Disconnecting (400) from the ECM will cause incremental amounts of Trip Data to be lost.
An “Event Recorder Data Lost” code may also be logged. The loss of this data will not affect engine
operation, but will affect the accuracy of the data. Ask the owner/operator if they want data recorded
before disconnecting.
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210 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
NOTE – Disconnecting (400) from the ECM will cause incremental amounts of Trip Data to be lost.
An “Event Recorder Data Lost” code may also be logged. The loss of this data will not affect engine
operation, but will affect the accuracy of the data. Ask the owner/operator if they want data recorded
before disconnecting.
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 211
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212 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
4. COMPONENT LOCATIONS
(1) Dash Panel Connector.. . .. . .. .. . .. .. . .. .. . .. .. . ... . . . . . Left Side of Engine Cowl
(2) Dash Panel Connector.. . .. . .. .. . .. .. . .. .. . .. .. . ... . . . . . Right Side of Engine Cowl, Above Conn. 3
(3) Dash Panel Connector.. . .. . .. .. . .. .. . .. .. . .. .. . ... . . . . . Right Side of Engine Cowl, Below Conn. 2
(94) Back-Up Light Switch.. . .. .. . .. . .. .. . .. .. . .. .. . ... . . . . . On Transmission
(137) 6–Way Data Link Connector. . . . . . . . . . . . . . . . . .. . . . . . Power Distribution Panel
(141) Ser. Brake Switch/Cruise Switch. . . . . . . . . . . . .. . . . . . Dash Panel, Left Side, Engine Side.
(190) Cab Overlay to Engine Harness. . . . . . . . . . . . . .. . . . . . Right Instrument Panel
(217) Inline Fuse. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Near ECM
(218) Inline Fuse. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Near ECM
(227) Fan Solenoid. . .. . .. .. . .. . .. . .. . .. . .. . .. . .. . .. . ... . . . . . At Front of Engine
(228) Refrigerant Pressure Switch. . . . . . . . . . . . . . . . . .. . . . . . On A/C Compressor
(229) Engine Oil Temp Sender. . .. . .. .. . .. . .. . .. .. . ... . . . . . Left Side of Engine
(275) Thermal Overcrank Protection. . . . . . . . . . . . . . . .. . . . . . At the Cranking Motor
(294) Clutch Switch Connector. . . . . . . . . . . . . . . . . . . . . .. . . . . . Near Clutch Switch
(400) OEM Interface Connector. . . . . . . . . . . . . . . . . . . . .. . . . . . On Engine
(402) Low Coolant Level.. .. .. .. .. .. .. .. .. .. .. .. .. .. ... . . . . . In Instrument Panel to Left of Tachometer
(403) J1922 Data Link. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Dash Panel Right Side
(404) Throttle Position Sensor. . . . . . . . . . . . . . . . . . . . . . .. . . . . . Behind Left Instrument Panel
(409) Vehicle Speed Sensor. . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . On Transmission to Engine Harness
(420) Right Gauge Cluster. . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Gauge Cluster
(421) Speedo./Tach. Module. . . .. . . .. . .. . . .. . . .. . . .. .. . . . . . Behind Speedo./Tach. Gauge
(422) Speedo./Tach. Module. . . .. . . .. . .. . . .. . . .. . . .. .. . . . . . Behind Speedo./Tach. Gauge
(423) Left Gauge Cluster. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Left Gauge Cluster
(424) Left Gauge Cluster. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Left Gauge Cluster
(514) Data Link — Positive.. . . .. . . .. . . .. . . .. . . .. . . .. .. . . . . . Behind Instrument Panel/Behind Cluster
(515) Data Link — Negative.. .. .. .. . .. .. .. .. . .. .. .. ... . . . . . Behind Instrument Panel/Behind Cluster
(640) Stop Light Switch. . . . .. . . . . .. . . . .. . . . . .. . . . . .. . .. . . . . . Dash Panel, Left Side Engine Compartment
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 213
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214 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 215
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216 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 217
1. GROUND STUD
2. CIRCUIT 11–GR, RADIATOR GROUND
3. (228) A/C PRESSURE SWITCH CONNECTOR
4. TO ENGINE WIRING AT DASH PANEL
5. (1097) BACKBONE FOR J1939
6. ETHER THERMOCOUPLE CIRCUIT 21A
7. J1922 DATALINK CONNECTOR
8. (1098) TERMINATION RESISTOR FOR J1939
9. TRANSMISSION TEMPERATURE GAUGE CONNECTOR
10. (229) ENGINE OIL TEMPERATURE GAUGE CONNECTOR
11. (275) THERMAL OVERCRANK CONNECTOR
12. (400) INTERNATIONAL ECM CONNECTOR
13. CIRCUIT 17C
14. CIRCUIT 97/97A
15. FUSIBLE LINK
16. CIRCUIT 11–GS
17. CIRCUIT 2–G
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218 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 219
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220 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
1. CIRCUIT 2
2. CIRCUIT 14
3. CIRCUIT A2
4. CIRCUIT 2-G
5. CIRCUIT 2-G
6. CIRCUIT 2
7. CIRCUIT 14
8. CIRCUIT 2-G
9. CIRCUIT 2
10. CIRCUIT 14
11. CIRCUIT 14
12. CIRCUIT 2
13. CIRCUIT 2-G
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 221
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222 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 223
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224 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
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6 CATERPILLAR C-10, C-12 AND 3406E ENGINES 225
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226 6 CATERPILLAR C-10, C-12 AND 3406E ENGINES
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7 DETROIT DIESEL SERIES 60 ENGINES 227
Table of Contents
1. DESCRIPTION. .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .229
2. OPERATION.. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .229
2.1. ECM POWER CIRCUITS.. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .230
2.2. SHUTDOWN OVERRIDE/DIAGNOSTIC SWITCH. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .230
2.3. ATA DATA LINK CONNECTOR. . .. . . .. . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . .230
2.4. IDLE SHUTDOWN FEATURE. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . .231
2.5. COOLANT LEVEL PROBE. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . .231
2.6. ELECTRONIC ACCELERATOR PEDAL ASSEMBLY. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .231
2.7. CRUISE CONTROL. .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .232
2.8. VEHICLE SPEED SENSOR (VSS). .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .232
2.9. CLUTCH SWITCH.. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .232
2.10. SERVICE BRAKE SWITCH. . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .232
2.11. IDLE TIMER/PARK BRAKE SWITCH.. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .233
2.12. ENGINE BRAKE. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. .233
2.13. ANTILOCK BRAKE INTERFACE. . . . . . . . . .. . . . . . . . . . . . . . .. . . . . . . . . . . . . .. . . . . . . . . . . . . . .. . . . . . . . . . . . . .233
3. TROUBLESHOOTING. .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .233
3.1. DETERMINING FAULT CODES.. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .234
Diagnostic OnOff/Shutdown Override Switch. . . . . . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . .234
EZ-Tech and PRO-LINK 9000 Electronic Service Tools (EST).. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .235
3.2. INSPECTION.. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .235
Before Troubleshooting. .. . . . . . . . .. . . . . . . . .. . . . . . . . .. . . . . . . . . .. . . . . . . . .. . . . . . . . .. . . . . . . . .. . . . . . . . .235
Testing Relays. . .. .. . .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. .235
3.3. ACCELERATOR PEDAL (TPS/IVS). . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .236
Testing Throttle Position Sensor (TPS). . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .236
Testing Idle Validation Switch (IVS).. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .237
Testing Accelerator Pedal (TPS/IVS) Circuits. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .238
3.4. DIAGNOSTIC CONNECTOR (137) AND DATA LINK CIRCUITS INCLUDING
SPEEDOMETER/TACHOMETER INPUT CIRCUITS.. .. . .. .. . .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. .240
Testing Diagnostic Connector Power and Ground Circuits. . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .240
Testing ATA Data Link Circuits.. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .240
3.5. CRUISE/PTO CONTROL SYSTEM AND RELATED COMPONENTS.. . . .. . .. . . .. . .. . . .. . .. . . .. . .242
Testing Clutch Switch.. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .242
Testing Service Brake Switch And Circuits.. . . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . . . . . .243
Testing Cruise On/Off Switch. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .244
Testing Cruise Set/Resume Switch And Circuits. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .245
3.6. VEHICLE SPEED SENSOR (VSS). .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .247
Inspecting And Adjusting the Adjustable Vehicle Speed Sensor (VSS). . . . . . . . . . . . . . . . . .247
Testing Vehicle Speed Sensor (VSS).. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .247
Testing Vehicle Speed Sensor (VSS) Circuits To ECM. . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . .248
3.7. ENGINE BRAKE SYSTEM.. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .249
Testing Engine Brake Switches and Circuits. . . . .. . . . . . . . . . . . . . .. . . . . . . . . . . . . . .. . . . . . . . . . . . . . .249
3.8. DIAGNOSTIC ON/OFF/SHUTDOWN OVERRIDE SWITCH (260). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .251
Testing Diagnostic On/Off/Shutdown Override Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .251
3.9. PARK BRAKE (IDLE TIMER) SWITCH (268). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .252
Testing Park Brake Switch (268) and Circuits. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .252
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1. DESCRIPTION
The Detroit Diesel Electronic Control system (DDEC III) provides an electronic fuel control system, electronic
engine protection and other operational controls.
DDEC III is standard on Series 60 engines and provides many engine/vehicle functions including:
• Cruise/PTO Controls
• Automatic Idle Shutdown Timer (3–100 Minutes)
• Engine Diagnostics
• Engine Protection System
• Engine Cooling System
• Engine Brake Control
• Speedometer/Tachometer Input Signals
• ABS/Traction Control Interface
Refer to Detroit Diesel manual furnished with the vehicle for additional feature information.
Since each Series 60 DDEC III system is electronically programmable to individual owner specifications, the
operating parameters will vary from vehicle to vehicle. These parameters include: maximum cruise speed,
maximum road speed settings and many others.
The “brain” of the DDEC III system is the Electronic Control Module (ECM), located on the left side of the
engine. The ECM receives inputs from the following International components:
The ECM receives inputs from sensors and switches, then outputs signals to the injectors, engine brake relay
and other system components.
2. OPERATION
The ECM is connected to the International electrical system at two points (or three points with antilock
brakes installed).
A. International engine harness 30–way ECM connector (273) connects to ECM. This connector links
the International switches, sensors and data links and supplies ignition power to the ECM.
B. ECM power cable connector (676) supplies unswitched battery power and a ground path to
the ECM.
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C. Additionally, with ABS/traction control system, the International 2–way J1922 data link connector
(403) connects the circuits to ECM communications connector (1160) and is used to provide
communications between the ECM and the ABS/traction control system controller.
Refer to the DETROIT SERIES 60 – ENGINE SYSTEMS circuit diagrams in CTS-5298 or S08225.
The ECM is grounded through circuits 11–GA, 11–GB, and 11–GC to a splice. From the splice the circuits are
grounded through circuit 11–G, connector (N/L) and circuit 11–G to the negative battery cable.
When the key switch is in the ignition or start position, power is applied to circuit 13Z, 5A fuse F6–D, circuit
13D, connector (2), and circuit 13D to the ECM (273).
The switch is connected to the negative battery terminal by way of circuits 97–GD and 97–GA, connector
(190), circuits 97–GA and 97–G, connector (N/L), circuits 97–G and 11–G, connector (N/L) and circuit 11–G to
the negative battery terminal. The switch is connected to the ECM by way of circuit 97AU, connector (190), and
circuit 97AU to ECM (273). Closing the switch causes the voltage state of circuit 97AU to change to ground,
indicating to the ECM that the switch has been toggled to the on position. Thus the ECM will switch modes to
display fault codes or the absence of codes by flashing the engine warning light and the stop engine light. The
red stop engine light will flash the active codes and the yellow engine warning light will flash the inactive codes.
The ATA data link connector (137), which is located on the left instrument panel, has circuits in four of the
six cavities. The data link circuits are a twisted wire pair because twisting the wires helps shield them from
interference. The circuits are as follows:
A. Circuit 98A(+) is the positive data link connection and it is fed by the positive data link connector
(514), the jumper bus bar, circuit 98(+), connector (190), and circuit 98(+) coming from the ECM
connector (273).
B. Circuit 98C(-) is the negative data link connection and it is fed by the negative data link connector
(515), the jumper bus bar, circuit 98B(-), connector (190), and circuit 98B(-) coming from the
ECM connector (273).
C. Circuit 97D is a 12 volt circuit and is fed from B1 Battery Stud to circuit 14W and 14AA, through
20A fuse F5–D. Thus it provides power for the electrical service tool.
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D. Circuits 97–GR and 11–GT are connected to the panel lights ground adapter (506), and provide a
ground for the electronic service tool.
If these conditions are present, the ECM counts down the customer selected length of time until 90 seconds
before the scheduled engine shutdown is to occur. At this time the yellow engine warning light begins to flash
rapidly. The idle timer can be disabled by depressing the accelerator pedal. This will allow the idle timer to be
overridden if longer idle time is wanted. The shutdown timing sequence can be re-started by releasing and
re-applying the parking brake.
If the idle timer shuts the engine down, fueling is stopped, but ignition voltage is still present to the ECM on
circuit 13D at connector (273).
NOTE – The key switch must be cycled to off and back to on before the engine will start.
NOTE – The engine is shut down, but power to the cab is not turned off.
The TPS acts like a potentiometer. Movement of the pedal results in a variable signal being sent to the ECM.
This signal is proportional to the pedal position. A five volt signal from the ECM (273) is sent through circuit
99A, connector (190), and circuit 99A to the potentiometer of TPS/IVS (267). The variable potentiometer wiper
signal (varies with pedal position) is returned from the TPS/IVS (267) over circuit 99, connector (190), and
circuit 99 to the ECM (273). The TPS/IVS (267) potentiometer is grounded through circuit 99–R, connector
(190) and circuit 99–R to the ECM (273).
The IVS is used to verify when the accelerator pedal is in the idle position. One side of the idle validation
switch (273) is connected to circuit 99B, connector (190), and circuit 99B to the ECM (273). The ECM sets
this input at 5 volts and when the throttle is at idle a ground is applied to this input by the idle validation
switch (267). This ground pulls the input voltage down to nearly zero, telling the ECM that the accelerator
pedal is in the idle position. The ground path that is applied by the IVS (267) is through circuits 99–GA and
97–GA, connector (190), circuits 97–GA and 97–G, connector (N/L), circuit 97G and 11–G, connector (N/L),
and circuit 11–G to the negative battery terminal.
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The ECM analyzes the signals received from the TPS/IVS, making certain that the signals fall within certain
parameters. For example, if the IVS signal indicates that the pedal is in the idle position, the ECM expects to
see a TPS signal that indicates no throttle (or very little) is being applied. If the ECM does not see a logical
response from both, a fault code will be logged. The TPS/IVS timing cannot be checked using a multimeter.
The cruise control and PTO systems share the same components, which include a cruise on/off switch (435),
cruise set/resume switch (436), service brake switch (141), park brake switch (268), clutch pedal switch
(294) and vehicle speed sensor (250).
The lighted cruise on/off switch (435) is connected by circuit 97AE, connector (190), and circuit 97AE to the
ECM (273). The other side of switch (435) is connected through circuits 97–GC, 97–GB, 97–GA, connector
(190), circuits 97–GA and 97–G, connector (N/L), circuits 97–G and 11–G, connector (N/L), and circuit 11–G to
negative battery stud. With the switch in the on position, the voltage state at the ECM input changes to ground,
telling the ECM that the switch is in the on position.
The lighted set/resume switch (436) is connected by circuit 97AB, connector (190), and circuit 97AB to the
ECM (273). The switch is also connected by circuit 97AA, connector (190) and circuit 97AA to the ECM (273).
The switch (436) is connected to the panel lights ground adapter (506) by way of circuits 62–GK and 11–GP.
With the switch held in the set position, circuit 97AB is switched to ground signaling the ECM (273). With the
switch held in the resume position, circuit 97AA is switched to ground, signaling the ECM (273).
Two types of sensors may be used. The threaded (adjustable sensor is used on most transmissions. A new
push-in sensor (non-adjustable) is used on some transmissions.
The clutch switch is connected by circuit 97AH, connector (190), and circuit 97AH to the ECM (273). The other
side of the switch is connected through circuits 97–GH, 97–GA, connector (190), circuit 97–GA and 97–G,
connector (N/L), circuits 97–G and 11–G, connector (N/L), and circuit 11–G to negative battery stud.
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The engine brake can provide braking when the vehicle is in the cruise control mode. For example, if the
vehicle is in the cruise control mode, going down hill, and the engine brake is selected, the ECM will control the
engine brake with respect to the cruise control set speed. The amount of braking will not exceed the number
of cylinders selected at the brake selector switch.
The lighted two position engine brake on/off switch (434) receives a ground signal on circuits 24–GA and
97–GA, connector (262), circuits 97–GA and 97–G, connector (N/L), circuits 97–G and 11–G, connector (N/L),
and circuit 11–G to the negative terminal of the batteries. In the on position a ground signal is sent from the
switch on circuit 24AJ to the engine brake selector switch (433).
When switch (433) is placed in the first position, a ground is applied to circuit 24AE, connector (190) and circuit
24AE to the ECM (273). This tells the ECM to enable the brake solenoid for two of the cylinders.
When switch (433) is placed in the second position, a ground is applied to circuit 24AF, connector (190) and
circuit 24AF to the ECM (273). This tells the ECM to enable the brake solenoids for four of the cylinders.
When switch (433) is placed in the third position, a ground is applied to circuit 24AE, connector (190) and
circuit 24AE to the ECM (273) and circuit 24AF, connector (190), and circuit 24AF to the ECM (273). This
tells the ECM to enable the brake solenoids for all six of the cylinders.
3. TROUBLESHOOTING
Refer to the DETROIT SERIES 60 – ENGINE SYSTEMS circuit diagrams in CTS-5298 or S08225.
A. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of
charge (SOC) or higher. This represents an open circuit voltage (OCV) of 12.4 volts. Batteries
with an OCV of 12 volts or less are either completely discharged or have a dead cell.
B. Before beginning these test procedures, check any light or indicator lamp filaments that are
suspected of being open (burned out). This is done to avoid unnecessary extensive circuit checks.
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C. Before beginning these test procedures, inspect all connectors for loose or damaged pins, wires,
etc. Refer to TEST EQUIPMENT AND CONNECTOR REPAIR section in the GROUP 08 —
ELECTRICAL in the CTS-5000 Master Service Manual.
D. When the technician determines that a fuse is blown, while checking its condition, he is directed
to locate the cause of the overload condition and to repair it. While no further instruction on this
procedure is listed in the diagnostic tables, the common procedure is as follows: isolate sections
of the circuit, by disconnecting connectors, and measure the resistance to ground to find the circuit
that is shorted to ground. Then locate the damaged spot in the wire or connector and repair.
E. Diagnostics for circuits that are malfunctioning by sticking in the position are generally not covered
in detail. It is assumed that the technician knows to check for a malfunctioning switch, relay, or
solenoid.
The yellow Engine Warning Light is turned on if a minor fault occurs. A fault code is also logged. This
indicates the problem should be diagnosed as soon as possible.
The ECM turns on the yellow Engine Warning Light and the red Stop Engine Light and stores a fault code
if a major fault is detected. If this occurs, the vehicle should be brought to a safe stop and the engine shut down.
A diagnostic check may be performed using the diagnostic on/off switch, the EZ-Tech or Pro-Link 9000 EST.
The diagnostic on/off switch is used to signal the ECM to flash the yellow Engine Warning light and the red
Stop Engine light to flash codes. The red Stop Engine light will flash the ACTIVE codes and the yellow
Engine Warning light will flash the INACTIVE codes.
If no fault codes are logged, the code "25" will be flashed out on the yellow Engine Warning Light. For example,
the yellow Engine Warning light blinks out: FLASH, FLASH. The first digit is a 2, then a half-second pause:
FLASH, FLASH, FLASH, FLASH, FLASH. The second digit is a 5. Code 25 is System OK.
The diagnostic on/off switch is used to flash codes in the following circumstances:
A. When the engine is not running and the ignition switch is on, toggling and releasing the diagnostic
on/off switch will flash out the engine codes. Toggling then releasing the diagnostic on/off switch a
second time will stop the ECM from flashing the codes.
B. When the engine is idling and not in an "engine protection condition," toggling and releasing the
diagnostic on/off switch will flash out the engine codes. Toggling then releasing the diagnostic
on/off switch a second time will stop the ECM from flashing the codes.
The Detroit Diesel Troubleshooting Manual contains flash code descriptions and diagnostic procedures.
If the fault code(s) or symptoms indicate a need to troubleshoot an International installed circuit or component,
procedures are included in this chapter or other CTS-5000 Master Service Manual sections.
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7 DETROIT DIESEL SERIES 60 ENGINES 235
The EZ-Tech or the PRO-LINK 9000 electronic service tools (EST) with a Series 60 program can be used to
read logged fault codes and monitor many of the system switches and operating parameters. Refer to the
EZ-Tech and PRO-LINK 9000 manuals for information on using the EST.
International vehicles include an 6-way diagnostic connector used to access the system with an EST.
The diagnostic tables in this section are not designed for specific symptoms, but designed to test those circuits
and components installed by International. Use DDEC III diagnostics procedures to identify the suspect circuit
or system, then use the procedures included in this section to troubleshoot the specific International circuit.
3.2. INSPECTION
NO TESTS in this section require testing "into" the DDEC ECM.
Before Troubleshooting
A. Before troubleshooting, make sure that the vehicle batteries are fully charged!Check battery
cables and grounds for clean, tight connections free of damage and corrosion. Many of the voltage
tests included in the procedures will give misleading readings if the batteries are not fully charged.
B. Before troubleshooting a particular circuit, inspect connectors for pushed back, loose or damaged
(spread or bent), or corroded terminals, or wires with cut strands, etc. The wires and connections
must be free of damage or corrosion. When some connectors corrode, a light white residue will
be present that must be removed.
C. Before troubleshooting, inspect the suspect circuit grounds for clean, tight connections free of
damage or corrosion.
Testing Relays
International circuits use suppressed relays for controlling power to load devices (Figure 69). The suppression
feature (a resistor circuit parallel to the relay coil) prevents voltage spikes from damaging electronic
components in the vehicle. These relays must be replaced with approved International parts.
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236 7 DETROIT DIESEL SERIES 60 ENGINES
The part number and relay circuit diagram are embossed on the relay body. The terminals are numbered on
the relay in the same manner as in the circuit diagrams.
2. Measure resistance between terminals 30 and 87. If resistance is 100K ohms or more, go to step 3;
otherwise replace the relay.
3. Using 12V battery source and test leads, connect (+) lead to terminal 85 and (-) lead to terminal 86. If relay
energizes with an audible click sound, go to step 4; otherwise replace the relay.
4. While relay is energized, measure resistance between terminals 30 and 87. If resistance is less than 5
ohms, go to step 5; otherwise replace the relay.
5. While relay is energized, measure resistance between terminals 30 and 87A. If resistance is 100K ohms or
more, the relay is good; otherwise replace relay.
These tests should be performed if a DDEC III fault code indicates a problem in the circuits or if the EZ-Tech or
PRO-LINK 9000 indicates that the TPS/IVS is not working properly while monitoring switches.
This test checks the TPS circuits in the accelerator pedal assembly. This test will identify if the resistance of
the pedal circuits is within specifications.
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7 DETROIT DIESEL SERIES 60 ENGINES 237
Perform preceding test before performing this test. This test checks the IVS circuits in the accelerator
pedal assembly.
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238 7 DETROIT DIESEL SERIES 60 ENGINES
Inspect TPS/IVS circuits and connectors as outlined in Before Troubleshooting. This test checks the cab and
engine harness TPS/IVS circuits for opens, shorts to ground, shorts to "hot" circuits and shorts to other circuits
in the harness and checks the circuits for continuity.
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7 DETROIT DIESEL SERIES 60 ENGINES 239
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240 7 DETROIT DIESEL SERIES 60 ENGINES
This table checks the power and ground circuits to the diagnostic connector (137).
This test checks the data link circuits between ECM connector (273) and the diagnostic connector (137)
and the speedometer/tachometer connector (421).
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7 DETROIT DIESEL SERIES 60 ENGINES 241
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242 7 DETROIT DIESEL SERIES 60 ENGINES
IMPORTANT – The following cruise control test procedures must be performed in the sequence that they
appear in this manual. Each test relies on information from the previous test procedure.
NOTE – The clutch switch is a normally open switch, adjusted to be closed when the pedal is in the
released (foot off) position.
NOTE – Use the EZ-Tech or PRO-LINK 9000 EST to check clutch switch operation. If the EST indicates
the clutch switch is not operating properly, perform this procedure.
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7 DETROIT DIESEL SERIES 60 ENGINES 243
NOTE – Use the EZ-Tech or PRO-LINK 9000 EST to check service brake switch operation. If the EST
indicates the service brake switch is not operating properly, perform this procedure.
NOTE – Vehicle air brake system must be fully charged for this test.
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244 7 DETROIT DIESEL SERIES 60 ENGINES
NOTE – Use the EZ-Tech or PRO-LINK 9000 EST to check cruise on/off switch operation. If the EST
indicates the cruise on/off switch is not operating properly, perform this procedure.
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7 DETROIT DIESEL SERIES 60 ENGINES 245
NOTE – Use the EZ-Tech or PRO-LINK 9000 EST to check set/resume switch operation. If the EST
indicates the set/resume switch is not operating properly, perform this procedure.
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246 7 DETROIT DIESEL SERIES 60 ENGINES
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7 DETROIT DIESEL SERIES 60 ENGINES 247
1. Disconnect engine harness connector (250) from the sensor. Loosen the locknut and remove the sensor.
The harness connector and sensor should be free of damage or corrosion. Remove any metal shavings or
debris from the sensor.
2. To install the sensor, turn in until the sensor contacts the transmission speedometer gear, then back out
one full turn. Tighten locknut to 15 ft-lbs. (20.3 N•m). This assures that the sensor is adjusted properly
for the next test.
To perform this test construct two test leads using terminals (1680205C1) and suitable length of 16GA wire.
WARNING – A jack must never be used alone to support vehicle. The jack may lower and
serious injury could result. Always support vehicle with floor jacks. Always block wheels to prevent
vehicle from moving.
WARNING – EXTREME CAUTION should be used to prevent personal injury resulting from
contact with rotating vehicle wheels when connecting test leads.
1500 to
3500 with
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248 7 DETROIT DIESEL SERIES 60 ENGINES
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7 DETROIT DIESEL SERIES 60 ENGINES 249
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250 7 DETROIT DIESEL SERIES 60 ENGINES
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7 DETROIT DIESEL SERIES 60 ENGINES 251
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252 7 DETROIT DIESEL SERIES 60 ENGINES
NOTE – Vehicle air system must be fully charged for this test.
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7 DETROIT DIESEL SERIES 60 ENGINES 253
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7 DETROIT DIESEL SERIES 60 ENGINES 255
4. COMPONENT LOCATIONS
(B1) Battery Stud. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . . Power Distribution Panel
(B2) Battery Stud. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . . Power Distribution Panel
(2) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Right Side of Engine Cowl, Above Connector 3
(3) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Right Side of Engine Cowl, Below Connector 2
(94) Back-Up Light Switch. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . . . . . On Transmission
(137) 6-Way Data Link Connector. . . . . . . . . . . . . . . . . . .. . . . . . Power Distribution Panel
(141) Ser. Brake Switch/Cruise Switch. . . . . . . . . . . . .. . . . . . Dash Panel, Lt. Side, Engine Side
(190) Cab Overlay to Elect. Eng. Harness. . . . . . . . .. . . . . . Right Instrument Panel
(227) Fan Solenoid.. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .. . . . . . At Front of Engine
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Table of Contents
1. DESCRIPTION. .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .267
2. OPERATION.. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .267
2.1. ECM POWER CIRCUITS.. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .268
2.2. ATA DATA LINK CONNECTOR. . .. . . .. . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . .268
2.3. DIAGNOSTIC ON/OFF SWITCH. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .269
2.4. IDLE/DIAGNOSTIC SWITCH. .. . .. . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .269
2.5. ELECTRONIC ACCELERATOR PEDAL ASSEMBLY. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .269
2.6. COOLANT LEVEL SWITCH.. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . .270
2.7. CRUISE CONTROL. .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .270
2.8. CLUTCH SWITCH.. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .271
2.9. VEHICLE SPEED SENSOR. . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .271
2.10. ENGINE BRAKE. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. .271
2.11. ANTILOCK BRAKE INTERFACE. .. .. .. . .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .272
2.12. GAUGES AND WARNING LIGHTS. . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .272
3. TROUBLESHOOTING. .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .272
3.1. ONBOARD DIAGNOSTICS WITH ENGINE RUNNING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. .272
3.2. PERFORMING A DIAGNOSTIC CHECK WITH THE ENGINE OFF. . . . . . .. . . . . . . . . . . . . . . . . . . . . . . .273
3.3. COMPULINKTM.. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .274
3.4. EZ-TECH OR PRO-LINK ELECTRONIC SERVICE TOOL (EST). .. . . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .274
3.5. INSPECTING INTERNATIONAL ENGINE HARNESS ECM CONNECTOR (252). . . . . . . . . . . . . . .275
3.6. RELAYS.. .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. .277
3.7. TESTING RELAY. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .277
3.8. ACCELERATOR PEDAL TPS/IVS.. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. .278
Testing Throttle Position Sensor (TPS). . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .278
Testing Idle Validation Switch (IVS).. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .279
Testing Accelerator Pedal (TPS/IVS) System for "Short or Open" Circuits. . . . . . . . . . . . . .280
Testing TPS/IVS Circuits for Continuity. .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .281
Accelerator/ECM Calibration.. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .283
3.9. LOW COOLANT SWITCH. .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . .. . . . .283
Testing Low Coolant Level Switch and Circuits.. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .283
3.10. POWER SUPPLY CIRCUITS TO ECM.. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .284
Testing Unswitched Battery Power Circuits and ECM Ground Circuit. . . . . . . . . . . . . . . . . . . .284
Testing Switched Ignition Power To ECM . .. . .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. . .. .. .. . .. .. .. . .. .. .285
3.11. SERVICE BRAKE AND CLUTCH SWITCHES. .. .. . .. .. .. . .. .. . .. .. .. . .. .. . .. .. .. . .. .. . .. .. .. . .. .. .286
Testing Clutch Switch.. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .286
Testing Clutch Switch Circuits for “Open and Short” Condition. . .. . .. . . .. . .. . . .. . .. . . .. . .287
Testing Clutch Switch Circuits For Continuity. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .288
Testing Service Brake Switch (141). . .. .. .. . .. .. . .. .. .. . .. .. . .. .. .. . .. .. . .. .. .. . .. .. . .. .. .. . .. .. .289
Testing Service Brake Switch Circuits for "Open and Short" Condition.. .. . .. .. . .. .. . .. .290
Testing Service Brake Switch Circuits for Continuity. .. . . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . .. . . . .291
3.12. ENGINE BRAKE. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. .292
Testing Engine Brake Components and Circuits. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .292
Testing Engine Brake Switches. . . .. . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . .292
3.13. ATA DATA LINK CONNECTOR (137) AND SPEEDOMETER/TACHOMETER INPUT
CIRCUITS. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .293
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1. DESCRIPTION
The N14 controller provides many engine/vehicle functions including:
• Cruise/PTO Controls
• Tachometer/Speedometer Input To Gauges
• Idle Shutdown
• Adjustable Low Idle Speed (In-Cab)
• Engine Cooling Fan Control
• Self Diagnostics
• Engine Protection System
• Engine Brake Control
Refer to the Cummins Engine Manual furnished with the vehicle for additional feature information.
Since each engine control system is electronically programmable to individual owner specifications, the
operating parameters will vary from vehicle to vehicle. These parameters include: maximum cruise speed,
shift schedules, governor type (automotive type or variable speed), idle RPM, full engine shutdown as part
of the engine protection system and many others.
The electronic control module (ECM) is the control center of the CELECT system. The ECM receives input
from Cummins and International sensors and switches, processes the information, then used electrical signals
to control engine and vehicle functions.
The ECM receives information from the sensors and switches and sends signals to the injectors, fuel shutoff
valve and engine brake relay.
2. OPERATION
Refer to Cummins N14 CELECT — ENGINE CONTROLS circuit diagrams in CTS-5298 or S08225.
The ECM is connected to the International electrical system at three points (or four points with antilock
brakes installed).
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A. International engine harness 28–way ECM connector (252) connects to ECM port B. This
connector links International sensors, switches and the diagnostic connector to the ECM.
B. International 21–way connector (251) connects to the Cummins sensor harness. This connector
links the International installed engine brake components, low coolant switch, fan controls and
switched voltage to the ECM.
C. The International ECM power connector (216) connects to the Cummins actuator harness. This
connector supplies the unswitched power to the ECM and provides an ECM ground circuit to the
engine ground stud.
D. Additionally, with ABS/traction control system, the International ECM connector (252), connects
to the Cummins sensor harness located near the front of the ECM. J1922 Data Link connector
(403) connects to the ABS system.
The ECM is grounded through the Cummins harness, ECM power harness connector (225) and circuit 97–G to
the engine ground stud. The engine ground stud is connected to the cranking motor ground stud, frame rail
and negative battery terminal.
Turning the key switch to the ignition or start position applies power to circuit 13, 13Z, 5A fuse F6–D and
circuit 13D to the 21–way ECM connector (251).
The ATA data link connector (137), which is located on the left instrument panel, has circuits in four of the
six cavities. The data link circuits are a twisted wire pair because twisting the wires helps shield them from
interference. The circuits are as follows:
Circuit 98A(+) is the positive data link connection, and it is fed by the positive data link connector (514), the
jumper bus bar, circuit 98(+), connector (190), and circuit 98(+) coming from the ECM connector (252).
Circuit 98C(-) is the negative data link connection, and it is fed by the negative data link connector (515), the
jumper bus bar, circuit 98B(-), connector (190) and circuit 98B(-) coming from the ECM connector (252).
Circuit 97DL is a 12 volt feed and is fed from the battery adapter (498), circuit 14BK and 20A fuse F5–D.
Thus it provides power for the electronic service tool.
Circuit 11–GR, 11–GT is connected to the panel lights ground adapter (506), and provides a ground for the
electronic service tool.
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The engine idle speed can be adjusted by the switch in increments of 25 rpm by toggling the switch. Maximum
idle speed is 800 rpm and minimum idle speed is 550 rpm. When the idle has been changed and the key
turned off, the new setting is saved in memory. This feature is owner selected and can be turned off with an
electronic service tool.
The switch is connected to the ECM common/ground connection by way of ECM connector (252), circuits
97–G and 97–GA, connector (190) and circuits 97–GA and 97–GD. Momentarily placing the switch in the
increment position applies ground to circuit 97AV, connector (190) and circuit 97AV to the ECM (252). This
causes the engine idle rpm to increase 25 rpm.
Momentarily placing the switch in the decrement position applies ground to circuit 97AU, connector (190) and
circuit 97AU to the ECM (252). This causes the engine idle rpm to decrease 25 rpm.
The TPS is attached to the accelerator pedal and acts like a potentiometer. Movement of the pedal results in
a variable signal being sent to the ECM that is proportional to pedal position. A 5 volt signal from the ECM
connector (252) is applied to circuit 99A, connector (190), circuit 99A and the TPS/IVS (267). The variable
wiper signal (varies with pedal position) from TPS/IVS (267) is returned to the ECM over circuit 99, connector
(190), circuit 99 and ECM connector (252). This variable signal tells the ECM the position of the accelerator
pedal. The TPS (267) is grounded through circuit 99–GA, connector (190) and circuit 99–GA to the ECM (252).
NOTE – Any time the accelerator pedal sensor (TPS) is disconnected from the ECM with the key switch
on, the TPS and ECM must be recalibrated.
The IVS is used to indicate when accelerator pedal is in the low idle position and when the pedal is not in the
low idle position. A ground path from the ECM connector (252), circuits 97–G and 97–GA, connector (190),
circuits 97–GA and 99–GA is applied to the TPS/IVS (267).
When the accelerator is in the low idle position, the IVS (267) applies a ground signal to circuit 99B, connector
(190) and circuit 99B to the ECM (252). When the accelerator is not in the idle position, the IVS (267) applies a
ground signal to circuit 99C, connector (190) and circuit 99C to the ECM (252).
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The ECM analyzes the signals received from the TPS and IVS to make certain that the signals fall within
certain parameters. For example: if the IVS signal indicates that the accelerator pedal is in the idle position,
the ECM expects to see a TPS signal that indicates that no throttle is applied. If it does not see a logical
response from both, a fault code may be logged.
The ECM and accelerator pedal must be calibrated to one another for proper engine response. Therefore,
the ECM and accelerator pedal must be calibrated when the accelerator pedal is initially installed, when an
accelerator pedal is replaced, when a new calibration is downloaded to the ECM, or when the accelerator
pedal wiring is disconnected at the pedal, the cab floor, or the ECM connector. To recalibrate the ECM and the
accelerator pedal, move the key switch to ignition position, slowly move the accelerator pedal from idle position
to fully depressed position and then release. Repeat this cycle two more times to assure proper calibration.
The coolant level switch (249) receives a 5 volt signal on circuit 34B(5V) from the ECM (251). When the
coolant level is above the probe, the switch sends a high signal (3.5 volts minimum) on circuit 34A and a low
signal (0.5 volt maximum) on circuit 34 to the ECM (251).
When the coolant level is below the probe, the switch sends a low signal (0.5 volt maximum) on circuit 34A and
a high signal (3.5 volts minimum) on circuit 34 to ECM (251).
The low coolant level switch is grounded through circuit 34–G to ECM (251).
NOTE – The low coolant level switch cannot be tested with a multimeter in the ohmmeter mode. This is
due to the fact that the switch is an electronic switch and not a mechanical switch.
Once the system is active, the driver can accelerate beyond the set speed by depressing the accelerator
pedal. When the pedal is released, cruise control is reactivated when the vehicle speed reaches the previously
set speed.
Cruise is deactivated and returns to the standby mode in several ways: the brake or clutch pedal is depressed,
the engine speed (rpm) drops below 1000 rpm, or the vehicle speed (mph) drops below 30 mph.
The resume switch can be used to reactivate cruise at the previous set speed or the set switch can be used
to establish a new set speed.
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While in the active mode, the coast feature is used to decrease vehicle speed and establish a new lower set
speed. By holding select switch in the coast position, vehicle speed decreases until the switch is released;
the speed at release becomes the new set speed.
While in the active mode, the accelerate feature is used to increase the vehicle speed and establish a new
higher speed. By holding the select switch in the accel position, vehicle speed increases until the switch is
released; the speed at release becomes the new set speed.
The lighted cruise control on/off switch (435) receives a ground signal on circuits 97–GC, 97–GA, connector
(259), circuits 97–GA, 97–G and 11–G from the negative battery terminal. In the on position, a ground signal is
sent from the switch on circuit 97AE, connector (190) and circuit 97AE to ECM connector (252) terminal 2.
This indicates to the ECM that the cruise control switch is in the on position. In the off position, circuit 97AE
returns to its 12 volt value, indicating to the ECM that the switch is off.
The lighted cruise set/resume switch is a momentary switch. This switch receives a ground signal on circuits
97–GB, 97–GA, connector (259), circuits 97–GA, 97–G and 11–G from the negative battery terminal. The
cruise selector switch sends a ground signal from the switch on circuit 97AB, connector (190) and circuit
97AB to the ECM connector (252) terminal 12 while in the set/accel position. In the resume/coast position,
the switch sends a ground signal by way of circuit 97AA, connector (190) and circuit 97AA to the ECM
connector (252) terminal 22.
The switch is provided a ground path over circuits 97–GH, 97–GA, connector (259), circuits 97–GA, 97–G and
11–G from the negative battery terminal. The clutch switch (294) sends a ground signal by way of circuit 97AH,
connector (190) and circuit 97AH to the ECM connector (252) terminal 4 while the clutch pedal is released.
Two types of sensors are available. The threaded (adjustable) sensor is used on most transmissions. A
push-in (non-adjustable) sensor is used on some transmissions.
When lighted switch (433) is placed in the first position, a ground is applied to circuit 24AE, connector (190),
and circuit 24AE to the ECM (252). This tells the ECM to enable the brake solenoid for the front two and rear
two cylinders on the N14E engine when braking is called for.
When switch (433) is placed in the second position, a ground is applied to circuit 24AF, connector (190) and
circuit 24AF to the ECM (252). This tells the ECM to enable the brake solenoid for the center two cylinders on
the N14E engine when braking is called for.
When switch (433) is placed in the third position, a ground is applied to circuit 24AF and 24AE to the ECM
(252). This tells the ECM to enable all solenoids and use all cylinders for braking.
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3. TROUBLESHOOTING
Refer to Cummins N14 CELECT — ENGINE CONTROLS circuit diagrams in CTS-5298 or S08225.
This section includes troubleshooting charts for International installed circuits and components that are part
of the CELECT Electronic Control system. To begin the troubleshooting process, refer to the appropriate
Cummins manual and follow their directions. If the Cummins diagnostics (fault codes) indicate that the suspect
circuits are International circuits or components, then use the charts in this section.
The EZ-Tech or Pro-Link 9000 EST can also be used to determine if the International switches and components
are working properly. If they are not, use a Fluke digital multimeter (DMM) to troubleshoot the circuits.
If the Cummins diagnostic codes or the EZ-Tech or the Pro-Link indicates a problem with International installed
circuits, the diagnostic tables in this chapter provide step-by-step test procedures.
A. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of
charge (SOC) or higher. This represents an open circuit voltage (OCV) of 12.4 volts. Batteries
with an OCV of 12 volts or less are either completely discharged or have a dead cell.
B. Before beginning these test procedures, check any light or indicator lamp filaments that are
suspected of being open (burned out). This is done to avoid unnecessary extensive circuit checks.
C. Before beginning these test procedures, inspect all connectors for loose or damaged pins,
wires, etc. Refer to TEST EQUIPMENT AND CONNECTOR REPAIR section in GROUP 08 —
ELECTRICAL in the CTS-5000 Master Service Manual.
D. When the technician determines that a fuse is blown, while checking its condition, he is directed
to locate the cause of the overload condition and to repair it. While no further instruction on this
procedure is listed in the diagnostic tables, the common procedure is as follows: isolate sections
of the circuit, by disconnecting connectors, and measure the resistance to ground to find the circuit
that is shorted to ground. Then locate the damaged spot in the wire or connector and repair.
E. Diagnostics for circuits that are malfunctioning by sticking in the position are generally not covered
in detail. It is assumed that the technician knows to check for a malfunctioning switch, relay, or
solenoid.
If the warning lights remain on, it is an indication that the ECM has detected a problem. The CELECT system
can show and record certain problems. The problems are shown as fault codes. The fault codes are recorded
in the ECM.
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8 CUMMINS N14 ELECTRONIC ENGINE SYSTEM 273
If a fault is detected (becomes active) during vehicle operation, the driver is alerted by the illumination of
either the yellow Engine Warning light or the red Stop Engine light. The yellow Service/Check Engine light
may also be illuminated.
The yellow Engine Warning light turns on to warn the driver of an active component or system fault that should
be serviced as soon as possible to solve the problem, but the situation is not considered an emergency.
The red Stop Engine light turns on to warn the driver that there is a major CELECT system problem and the
vehicle should be stopped and engine shut down as soon as is safely possible.
The yellow Service/Check Engine light (engine protection system) turns on to warn the driver that:
7. Red Engine Stop light will flash code with one or two seconds between digits.
8. Yellow Engine Warning light will flash indicating the end of that fault code, and then start over and
repeat the same fault code.
9. To go to the second fault code, move the Idle/Diagnostic Inc/Dec switch to the Inc position and then
release it. The process will then repeat itself as indicated in steps 5 through 8.
10. To move back to the last or previous fault code, move the Idle/Diagnostic Inc/Dec switch to the Dec
position and then release it. The process will then repeat itself as indicated in steps 5 through 8.
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274 8 CUMMINS N14 ELECTRONIC ENGINE SYSTEM
11. To stop the diagnostics procedure, correct the faults or move the diagnostic on/off switch to off, and turn
the vehicle key switch to the off position.
NOTE – Cummins CELECT engine diagnostics must be run with the engine NOT RUNNING.
If BOTH the yellow Engine Warning and red Engine Stop lights come on momentarily and then go out, it is an
indication that engine faults are present.
If BOTH the yellow Engine Warning and red Engine Stop lights come on and stay on, it is an indication that
no engine faults are present.
For example, the yellow Engine Warning light flashes once. The red Engine Stop light flashes:
FLASH
FLASH — FLASH
Digit number three is 3. Yellow Engine Warning lamp flashes once. The fault code is 123
3.3. COMPULINKTM
CELECT vehicles have a data link connected to the ATA data link connector (137) The Cummins CompulinkTM
electronic service tool can be connected to the connector to program owner-specified information into
the engine, monitor the system, and aid in troubleshooting the engine. Consult the Cummins CELECT
Troubleshooting and Repair Manual. The CompulinkTM may be available at the nearest Cummins Authorized
Service Center.
CompulinkTM must be used with a CELECT service cartridge to communicate with a CELECT engine. A
PACE or PT PACER cartridge will not work properly.
NOTE – On the Cummins CompulinkTM, since no alpha characters are available, use the up arrow and
down arrow to move through the alphabet.
The EZ-Tech or Pro-Link 9000 can also be used to monitor operation of various switches and controls and
perform other diagnostic tasks. The specific capabilities and operating instructions are included in the EZ-Tech
or Pro-Link 9000 documentation.
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8 CUMMINS N14 ELECTRONIC ENGINE SYSTEM 275
2. Inspect the connector for pushed back or expanded terminals in the following manner:
a. Insert the tool (Cummins part number 3823383) into each Amp connector (Tool In Connector Figure)
Do not force the tool into the connector.
b. A terminal that is not pushed back or expanded will have a surface to tool gap (Tool In Connector
Figure) of approximately 0.050 inch (1.3 mm). If the tool touches the connector, replace the terminal.
c. Push the tool into the terminal until the tool touches the connector (Surface Tool Gap Figure). Slowly
remove the tool from the terminal. A small resistance (6 to 10 ounces) must be felt (Tool Touching
Connector Figure). If the resistance is not felt, the terminal is expanded and must be replaced.
d. Repeat steps A through C to check for pushed back or expanded terminals for all terminals in the
ECM connector.
e. Inspect the connector pins in the ECM. If the pins are bent (Inspect Connector Pins Figure), have a
Cummins dealer replace the ECM.
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8 CUMMINS N14 ELECTRONIC ENGINE SYSTEM 277
3.6. RELAYS
International circuits use suppressed relays for controlling power to load devices. The suppression feature (a
resistor circuit parallel to the relay coil) prevents voltage spikes from damaging electronic components in the
vehicle. These relays must be replaced with the correct International part.
Relays used in exposed areas such as the engine compartment are sealed relays and have a different part
number than those in the cab. The part number is embossed on the relay. There is also a circuit diagram of the
relay located on the relay body. The terminals are numbered on the relay in the same manner as in the circuit
diagrams. To test the relay, refer toTesting Relay.
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278 8 CUMMINS N14 ELECTRONIC ENGINE SYSTEM
NOTE – The following four tests, Testing Throttle Position Sensor (TPS), Testing Idle Validation Switch
(IVS), Testing Accelerator Pedal (TPS/IVS) System for “Short or Open” Circuits and Testing TPS/IVS
Circuits for Continuity must be performed in sequence.
The tests should be performed if a Cummins fault code indicates a problem in the circuits or if the CompulinkTM
EZ-Tech or Pro-Link 9000 EST indicates that the TPS/IVS is not working properly while monitoring switches. If
CompulinkTM detects a fault with the IVS circuits while monitoring switches, the display would show Idle
Validation Switch = Fault. If a fault is present while monitoring Percent Of Throttle, the percent displayed
does not indicate actual throttle position.
NOTE – Testing Throttle Position Sensor (TPS) and Testing Idle Validation Switch (IVS) check operation
of the APS and IVS, but do not check the timing between the two functions.
This test checks the TPS circuits in the accelerator pedal assembly. This test will help identify if the resistances
are within specifications and if there are any opens or shorts in the TPS, but will not verify the correct
switching of the IVS and TPS.
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This test checks the IVS circuits in the accelerator pedal assembly.
Perform Testing Throttle Position Sensor (TPS) above, before performing this test.
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This test checks the cab and engine harness TPS/IVS circuits for opens, shorts to ground, shorts to "hot"
circuits and shorts to other circuits in the harness.
NOTE – Perform Testing Throttle Position Sensor (TPS) and Testing Idle Validation Switch (IVS) before
performing this test.
Table 76 Testing Accelerator Pedal (TPS/IVS) System for “Short or Open” Circuits
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off With (267) disconnected, Go to Replace connector
disconnect connector next step. terminals if damaged.
(252) from ECM and If ECM pins are
inspect ECM connector. damaged, have
Refer to Inspecting Cummins dealer
International Engine replace ECM. Refer
Harness ECM Connector to Accelerator/
(252). ECM Calibration to
recalibrate the ECM to
TPS/IVS.
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Table 76 Testing Accelerator Pedal (TPS/IVS) System for “Short or Open” Circuits (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
2. Off At connector (252) use (252), >100K Go to Locate short to ground,
test leads and measure 99B, 99C, ohms. next step. in circuit where terminal
resistance to gnd. at 97-G, 99, resistance is less than
terminals 6, 9, 10, 11, 18 99A and 100K ohms, then
and 19 (circuits 99B, 99C, 99-G to repair.
97-G, 99, 99A and 99-G). gnd.
Do not use probes or leads
other than Cummins P/N
3822758 or the connector
could be damaged.
3. Off At connector (252) use (252), >100K Go to Locate short between
test leads and measure between ohms. next step. any circuits where
resistance between 99B, 99C, resistance between
terminals 6, 9, 11, 18 and 99, 99A, terminals is less than
19 (circuits 99B, 99C, 99, 99-G and 100K ohms, then
99A and 99-G) and all all other repair.
other terminals in (252). cir. in
conn.
4. On At connector (252) use (252), <1.5 Go to Test Locate short to
test leads and measure 99B, 99C, volts. Chart unwanted voltage
voltage to gnd. at 97-G, 99, below. source in any circuit
terminals 6, 9, 10, 11, 99A and where more than
18 and 19 (circuits 99B, 99-G to 1.5 volts is present,
99C, 97-G, 99, 99A and gnd. then repair. Refer
99-G). to Accelerator/
ECM Calibration
to recalibrate ECM/
accelerator pedal.
This test checks the individual TPS and IVS circuits (cab and engine harness) for correct resistance while
disconnected from the accelerator pedal assembly and ECM.
NOTE – Perform the preceding three tests before performing this test.
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Accelerator/ECM Calibration
The electronic accelerator pedal assembly and the ECM must be calibrated when:
This test procedure requires a VOM to check the International harness for opens, shorts to ground, or shorts
to other circuits in the International harness. The low coolant sensor has complex circuits and a VOM
should not be used to test the sensor as it may damage the circuits.
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Table 79 Testing Unswitched Battery Power Circuits and ECM Ground Circuit
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off Check ECM power Go to Correct poor
harness connector next connections.
at starter (circuit 97, step.
97A and 97-G) and
at connector (225) for
clean, tight connections.
Connections good?
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Table 79 Testing Unswitched Battery Power Circuits and ECM Ground Circuit (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
2. Off Check the two 15 amp ECM fuses. <5 ohms. Go to Locate cause of
fuses located in the next overload condition,
engine harness for open step. then correct. Replace
condition. with correct rated fuse.
3. Off Disconnect ECM power (225), 97 12 ± 1.5 Go to Locate cause of low or
connector (225) from and 97A to volts. next no voltage in circuit 97
Cummins engine harness. gnd. step. or 97A from B+ terminal
Measure voltage to gnd. or starter, then repair.
at circuits 97 and 97A.
Battery voltage present?
4. Off At connector (225) (225), 97 to 12 ± 1.5 Go to Locate open or high
measure voltage between 97-G. volts. next resistance in circuit
circuits 97 and 97-G. step. 97-G between (225)
Battery voltage present? and engine gnd. stud,
then repair.
5. On At connector (225) (225), 97 to >7 volts. Go to Locate cause of excess
measure voltage between 97-G while next voltage drop in cranking
circuits 97 and 97-G while cranking. step. circuit, then repair.
cranking engine.
6. Off Unswitched battery power
circuits and ECM ground
circuit at connector (225)
checks good.
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CAUTION – When testing at ECM connector (252), do not use probes or leads other than Cummins
test lead, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
Table 82 Testing Clutch Switch Circuits for "Open and Short" Condition
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off With clutch switch Go to Replace harness
disconnected, remove next connector terminals
ECM connector (252) step. if damaged. If ECM
from the ECM. Refer pins are damaged,
to Inspecting Navistar have Cummins dealer
Engine Harness ECM replace ECM. Refer
Connector (252) and to Accelerator/ ECM
inspect connector. ECM Calibration to recalibrate
harness connector or ECM/ accelerator pedal.
ECM pins OK?
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Table 82 Testing Clutch Switch Circuits for "Open and Short" Condition (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
2. Off Turn all CELECT cab (252), >100K Go to Locate short to gnd. in
switches to off or neutral 97AH and ohms. next circuit where resistance
position and set service 97-G to step. at terminal was less than
brake using trailer hand gnd. 100K ohms, then repair.
valve. Use test leads and
measure resistance to
gnd. at connector (252)
terminal 4 and 10 (circuit
97AH and 97-G).
3. Off With CELECT cab (252), >100K Go to Locate short between
switches still in off or 97AH and ohms. next circuits, then repair.
neutral position and 97-G and step.
service brake set, use all other
test leads and measure circuits.
resistance between
terminals 4 and 10
(circuit 97AH and 97-G)
and all other terminals in
connector (252).
4. On At connector (252), (252), <1.5 volts. The Locate short to
use test leads and 97AH and clutch unwanted voltage
measure voltage to gnd. 97-G to switch source in circuit with
at terminals 4 and 10 gnd. circuits more than 1.5 volts,
(circuit 97AH and 97-G). are free then repair. Refer
of short to Accelerator/ ECM
circuits. Calibration to recalibrate
Perform ECM/ accelerator pedal.
Testing
Clutch
Switch
Circuits
for
Continuity
CAUTION – When testing at ECM connector (252), do not use probes or leads other than Cummins
test leads, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
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Testing Service Brake Switch Circuits for "Open and Short" Condition
Perform Testing Service Brake Switch (141) before performing this test.
CAUTION – When testing at ECM connector (252), do not use probes or leads other than Cummins
test leads, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
Table 85 Testing Service Brake Switch Circuits for "Open and Short" Condition
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off With connector (141) Go to Replace harness
disconnected from brake next step. connector terminals
switch, remove connector if damaged. If ECM
(252) from the ECM. Refer pins damaged, have
to Inspecting International Cummins dealer replace
Engine Harness ECM ECM.
Connector (252) to
inspect connector. ECM
connector and ECM pins
OK?
2. Off Turn all CELECT cab (252), >100K Go to Locate short to ground. in
switches to off or neutral 97AL and ohms. next step. circuit where resistance
position and disconnect 97-G to at terminal was less than
clutch switch. Use test gnd. 100K ohms, then repair.
leads and measure
resistance to gnd. at
connector (252) terminals
13 and 10 (circuits 97AL
and 97-G).
3. Off Use test leads and (252), >100K Go to Locate short between
measure resistance 97AL to ohms. next step. any circuit where
between terminal 13 97-G and resistance between
and 10 (circuits 97AL all other terminals is less than
and 97-G) and all other circuits. 100K ohms, then repair.
terminals in connector
(252).
4. On At connector (252), use (252), <1.5 The Locate short to unwanted
test leads and measure 97AL and volts. brake voltage source in circuit
voltage to ground at switch
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Table 85 Testing Service Brake Switch Circuits for "Open and Short" Condition (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
terminals 13 and 10 97-G to circuits with more than 1.5 volts,
(circuits 97AL and 97-G). gnd. are free then repair.
of short
circuits.
Perform
Testing
Service
Brake
Switch
Circuits
for
Continuity.
CAUTION – When testing at ECM connector (252), do not use probes or leads other than Cummins
test leads, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
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a. With switch in on position, resistance between terminals 5 and 6 and between 2 and 3 should be
less than 5 ohms.
b. With switch in off position, resistance should be 100K ohms or more.
c. To test the LED in the switch, connect B+ test lead to terminal 7 and ground terminal 8. LEDs should
illuminate.
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Testing Data Link Circuits Between Diagnostic Connector, ECM and Speedometer/Tachometer Unit
CAUTION – When testing at ECM connector (252), do not use probes or leads other than Cummins
test leads, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
Table 89 Testing Data Link Circuits Between Diagnostic Connector, ECM and Speedometer/Tachometer
Unit
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off Disconnect ECM Go to Replace harness
connector (252) from next connector terminals
the ECM. Refer to step. if damaged. If ECM
Inspecting International pins are damaged,
Engine Harness ECM have Cummins
Connector (252) and dealer replace ECM.
inspect connector. ECM Refer to Accelerator/
harness connector OK? ECM Calibration to
recalibrate ECM/
accelerator pedal.
2. Off Disconnect connector (252), >100K Go to Locate short circuit
(421) from speedometer/ 98B(-) and ohms. next to ground in circuit
tachometer unit and 98(+) to step. where resistance is
if additional devices gnd. less than 100K ohms,
have been connected to then repair.
(514) and (515) data link
connectors, they must
be disconnected. At
connector (252), using
test leads, measure
resistance to gnd. at
terminals 8 and 27 (circuit
98B[-] and 98[+]).
3. On At connector (252) use (252), >100K Go to Locate short between
test leads and measure 98B(-) and ohms. next circuits where
resistance between 98(+) and step. resistance between
terminals 8 and 27 (circuit all other terminals is less than
98B[-] and 98[+]) and circuits in 100K ohms, then
all other terminals in conn. repair.
connector.
4. On At connector (252) use (252), <1.5 volts Go to Locate short to
test leads and measure 98B(-) and next unwanted voltage
voltage to gnd. at 98(+) to step. source in circuit where
terminals 8 and 27 gnd. more than 1.5 volts
(circuits 97B[-] and 98[+]). is present at terminal,
then repair.
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Table 89 Testing Data Link Circuits Between Diagnostic Connector, ECM and Speedometer/Tachometer
Unit (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
5. Off At connector (252) use (137) , <5 ohms. Go to Locate open or poor
test lead to jumper 98C(-) to next connection in circuit
terminal 8 (cir. 98B[-]) gnd. step. 98B(-) or 98C(-)
to gnd. At connector (137) between connectors
measure resistance to (252) and (137), then
gnd. at terminal B (cir. repair.
98C[-]).
6. Off With connector (252) (421), 47/ <5 ohms. Go to Locate open or poor
terminal 8 (cir. 98B[-]) 48(-) to gnd. next connection in circuit
still jumpered to gnd., at step. 47/48(-) between
connector (421) measure connectors (515) and
resistance to gnd. at (421), then repair.
circuit 47/48(-).
7. Off At connector (252) use (137), <5 ohms. Go to Locate open or poor
test lead to jumper 98A(+) to next connection in circuit
terminal 27 (cir. 98[+]) gnd. step. 98(+)/(98A+) between
to gnd. At connector connectors (252) and
(137) measure resistance (137), then repair.
terminal A (cir. 98A[+]) to
ground.
8. Off With connector (252) (421), 47/ <5 ohms. Go to Locate open or poor
terminal 27 (cir. 98[+]) 48(+) to next connection in circuit
still jumpered to gnd., at gnd. step. 47/48(+) between
connector (421) measure connectors (514) and
resistance to gnd. at (421), then repair.
circuit 47/48(+).
9. Off The data link circuits
between ECM connector
(252), diagnostic
connector (137) and
speedometer/ tachometer
connector (421) test good.
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CAUTION – When testing at ECM connector (252), do not use probes or leads other than Cummins
test leads, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
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CAUTION – When testing at ECM connector (252), do not use probes or leads other than Cummins
test leads, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
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1. Disconnect engine harness connector (250) from the sensor. Loosen the locknut and remove the sensor.
The harness connector and sensor should be free of damage or corrosion. Remove any metal shavings or
debris from the sensor.
2. To install the adjustable sensor, turn in until the sensor contacts the transmission speedometer gear, then
back out one full turn. Tighten locknut to 15 ft-lbs. (20.3 N•m). This assures that the sensor is adjusted
properly for the next test.
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Construct test leads using terminals (International Part No. 1680205C1), short length of 16 gauge wire
and alligator clips.
WARNING – A jack must never be used alone to support vehicle. The jack may lower and
serious injury could result. Always support vehicle with floor jacks. Always block wheels to prevent
vehicle from moving.
WARNING – EXTREME CAUTION should be used to prevent personal injury resulting from
contact with rotating vehicle wheels when connecting test leads.
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To check circuits between the ECM and the speedometer/tachometer unit, refer to ATA Data Link Connector
(137) and Speedometer/Tachometer Input Circuits.
CAUTION – When testing at ECM connector (252), do not use probes or leads other than Cummins
test leads, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
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4. COMPONENT LOCATIONS
B1 Battery Stud.. . .. .. . .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . . . . . Power Distribution Panel
(1) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Left Side of Engine Cowl
(2) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Right Side of Engine Cowl, Above Connector 3
(3) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Right Side of Engine Cowl, Below Connector 2
(72) Ether Start Connector. . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Front End Harness, At Lower Left of Radiator
(94) Back-up Light Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . On Transmission
(137) 6-Way Data Link Connector. . . . . . . . . . . . . . . . . . .. . . . . . Power Distribution Panel
(141) Service Brake Switch/Cruise Switch. . . . . . . . .. . . . . . Dash Panel, Left Side, Engine Side
(216) ECM Power Connector. . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Start Motor
(227) Fan Solenoid.. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .. . . . . . At Front of Engine
(228) Refrigerant Pressure Switch. . . . . . . . . . . . . . . . . .. . . . . . On A/C Compressor
(229) Engine Oil Temp Sender. .. . .. .. . .. . .. .. . .. . .. .. . . . . . Left Side of Engine
(230) Cab Overlay to Elect. Eng. Harn.. . . . . . . . . . . .. . . . . . Right Instrument Panel
(235) Transmission Oil Temp (Inline). . .. . . . .. . . .. . . .. . . . . . On Front of Transmission
(249) Low Coolant Level Switch. . . . . . . . . . . . . . . . . . . . .. . . . . . To Engine Harness
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Table of Contents
1. DESCRIPTION. .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .321
2. OPERATION.. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .322
2.1. ECM POWER. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .322
2.2. ATA DATA LINK CONNECTOR. . .. . . .. . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . .322
2.3. DIAGNOSTIC ON/OFF SWITCH. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .323
2.4. IDLE/DIAGNOSTIC SWITCH. .. . .. . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .323
2.5. ELECTRONIC ACCELERATOR PEDAL ASSEMBLY. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .323
2.6. COOLANT LEVEL SWITCH.. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . .324
2.7. CRUISE CONTROL. .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .324
2.8. BRAKE SWITCH . . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . .325
2.9. CLUTCH SWITCH.. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .325
2.10. VEHICLE SPEED SENSOR. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .326
2.11. ENGINE BRAKE SWITCHES. . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . .326
2.12. GAUGES AND WARNING LIGHTS. . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .326
2.13. J1939 DATA LINK. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . .326
3. TROUBLESHOOTING. .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .326
3.1. ONBOARD DIAGNOSTICS WITH ENGINE RUNNING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. .327
3.2. PERFORMING A DIAGNOSTIC CHECK WITH THE ENGINE OFF. . . . . . .. . . . . . . . . . . . . . . . . . . . . . . .328
3.3. CUMMINS ELECTRONIC SERVICE TOOL.. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .329
3.4. EZ-TECH OR PRO-LINK ELECTRONIC SERVICE TOOL (EST). .. . . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .329
3.5. RELAYS.. .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. .329
3.6. TESTING RELAY. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .329
3.7. ACCELERATOR PEDAL TPS/IVS.. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. .330
Testing Throttle Position Sensor (TPS). . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .330
Testing Idle Validation Switch (IVS).. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .331
Testing Accelerator Pedal (TPS/IVS) System for “Short or Open” Circuits. . . . . . . . . . . . . .332
Testing TPS/IVS Circuits for Continuity. .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .333
Accelerator/ECM Calibration.. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .335
3.8. LOW COOLANT SWITCH. .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . .. . . . .335
Testing Low Coolant Level Switch And Circuits. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. .335
3.9. POWER SUPPLY CIRCUITS TO ECM.. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .336
Testing Unswitched Battery Power Circuits And ECM Ground Circuit. . . . . . . . . . . . . . . . . . .336
Testing Switched Ignition Power To ECM . .. . .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. . .. .. .. . .. .. .. . .. .. .337
3.10. SERVICE BRAKE AND CLUTCH SWITCHES. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .338
Testing Clutch Switch.. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .338
Testing Clutch Switch Circuits for "Open and Short" Condition. . . .. . . . . . . .. . . . . . . .. . . . . . .338
Testing Clutch Switch Circuits For Continuity. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .340
Testing Service Brake Switch (141). . .. .. .. . .. .. . .. .. .. . .. .. . .. .. .. . .. .. . .. .. .. . .. .. . .. .. .. . .. .. .340
Testing Service Brake Switch Circuits for "Open and Short" Condition.. .. . .. .. . .. .. . .. .341
Testing Service Brake Switch Circuits for Continuity. .. . . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . .. . . . .342
3.11. ENGINE BRAKE.. . .. . .. .. . .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. .343
Testing Engine Brake Components And Circuits. .. . . . . . . .. . . . . . . . .. . . . . . . . .. . . . . . . . .. . . . . . . .343
Testing Engine Brake Switches. . . .. . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . .344
3.12. ATA DATA LINK CONNECTOR (137) AND SPEEDOMETER/TACHOMETER INPUT
CIRCUITS. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .344
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9 CUMMINS ISM AND AHD ENGINE SYSTEM 321
1. DESCRIPTION
This chapter covers International installed components and circuits that directly interact with the Cummins ISM
and AHD (AHD is synonymous with Signature Series) engines. This chapter provides:
• Operation descriptions of International installed components and circuits which work with the Cummins
engine controls.
• Troubleshooting charts for those circuits and components installed by International.
• Locations for International installed circuits.
Refer to the Cummins Engine Manual furnished with the vehicle for other information.
The Cummins ISM and AHD engines use the CM570 engine controller. The controller provides many
engine/vehicle functions including:
• Cruise/PTO Controls
• Tachometer/Speedometer Input To Gauges
• Idle Shutdown
• Adjustable Low Idle Speed (In-Cab)
• Engine Cooling Fan Control
• Self Diagnostics
• Engine Protection System
• Engine Brake Control
• J1939 Datalink (Used for Diagnostics and to Interface With Transmission and ABS).
Refer to the Cummins Engine Manual furnished with the vehicle for additional feature information.
Since each engine control system is electronically programmable to individual owner specifications, the
operating parameters will vary from vehicle to vehicle. These parameters include: maximum cruise speed,
shift schedules, governor type (automotive type or variable speed), idle RPM, full engine shutdown as part
of the engine protection system and many others.
The electronic control module (ECM) is the control center of the system. The ECM receives input from
Cummins and International sensors and switches, processes the information, then uses electrical signals
to control engine and vehicle functions.
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322 9 CUMMINS ISM AND AHD ENGINE SYSTEM
The ECM receives information from the sensors and switches and sends signals to the injectors, fuel shut off
valve and engine brake relay.
2. OPERATION
Refer to the Cummins AHD and ISM — ENGINE CONTROLS circuit diagrams in CTS-5298 or S08225.
A. International engine harness 50–way ECM connector (1091) connects to ECM port C-1. This
connector links several International sensors, switched power, unswitched power ground,
switches, diagnostic connector to the ECM and the J1939 data link. The J1939 data link will
interface with the transmission and ABS as required.
B. International 31–way connector (1093) connects to the Cummins sensor harness. This connector
links the vehicle speed sensor, low coolant switch, air conditioner power switch and engine fan
controls to the ECM.
The ECM is grounded from the battery on circuit 11G which is split into circuits 11GCF, 11GCB, 11GCK,
11GCJ, and 11GCH for input to 50–way ECM connector (1091).
Turning the key switch to the ignition or start position applies power to circuit 13Z, 5A fuse F6–D and circuit
13D to the 50–way ECM connector (1091).
The ATA data link connector (137), which is located on the left instrument panel, has circuits in four of the
six cavities. The data link circuits are a twisted wire pair because twisting the wires helps shield them from
interference. The circuits are as follows:
Circuit 98A(+) is the positive data link connection and it is fed by the positive data link connector (514), the
jumper bus bar, circuit 98(+), connector (190), and circuit 98(+) coming from the ECM connector (1091).
Circuit 98C(-) is the negative data link connection and it is fed by the negative data link connector (515), the
jumper bus bar, circuit 98B(-), connector (190) and circuit 98B(-) coming from the ECM connector (1091).
Circuit 97DL is a 12 volt feed and is fed from the battery adapter (498), circuit 14BK and 20A fuse F5–D.
Thus it provides power for the electronic service tool.
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9 CUMMINS ISM AND AHD ENGINE SYSTEM 323
Circuit 11–GR, 11–GT is connected to the panel lights ground adapter (506) and provides a ground for the
electronic service tool.
The engine idle speed can be adjusted by the switch in increments of 25 RPM by toggling the switch.
Maximum idle speed is 800 RPM and minimum idle speed is 550 RPM. When the idle has been changed and
the key turned off, the new setting is saved in memory. This feature is owner selected and can be turned off
with an electronic service tool.
The switch is connected to the ECM common/ground connection by way of ECM connector (252), circuit
97–G and 97–GA, connector (190) and circuits 97–GA and 97–GD. Momentarily placing the switch in the
increment position applies ground to circuit 97AV, connector (190) and circuit 97AV to the ECM (252). This
causes the engine idle RPM to increase 25 RPM.
Momentarily placing the switch in the decrement position applies ground to circuit 97AU, connector (190) and
circuit 97AU to the ECM (252). This causes the engine idle RPM to decrease 25 RPM.
The TPS is attached to the accelerator pedal and acts like a potentiometer. Movement of the pedal results in
a variable signal being sent to the ECM that is proportional to pedal position. A 5 volt signal from the ECM
connector (1091) is applied to circuit 99A, connector (190), circuit 99A and the TPS/IVS (267). The variable
wiper signal (varies with pedal position) from TPS/IVS (267) is returned to the ECM over circuit 99, connector
(190), circuit 99 and ECM connector (1091). This variable signal tells the ECM the position of the accelerator
pedal. The TPS (267) is grounded through circuit 99–G, connector (190) and circuit 99–G to the ECM (1091).
NOTE – Any time the accelerator pedal sensor (TPS) is disconnected from the ECM with the key switch
on, the TPS and ECM must be recalibrated.
The IVS is used to indicate when accelerator pedal is in the low idle position and when the pedal is not in
the low idle position. A ground path from the ECM connector (1091), circuit 97–GA, connector (190), circuit
99–GA is applied to the TPS/IVS (267).
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324 9 CUMMINS ISM AND AHD ENGINE SYSTEM
When the accelerator is in the low idle position, the IVS (267) applies a ground signal to circuit 99B, connector
(190) and circuit 99B to the ECM (1091). When the accelerator is not in the idle position, the IVS (267) applies
a ground signal to circuit 99C, connector (190) and circuit 99C to the ECM (1091).
The ECM analyzes the signals received from the TPS and IVS to make certain that the signals fall within
certain parameters. For example: if the IVS signal indicates that the accelerator pedal is in the idle position,
the ECM expects to see a TPS signal that indicates that no throttle is applied. If it does not see a logical
response from both, a fault code may be logged.
The ECM and accelerator pedal must be calibrated to one another for proper engine response. Therefore,
the ECM and accelerator pedal must be calibrated when the accelerator pedal is initially installed, when an
accelerator pedal is replaced, when a new calibration is downloaded to the ECM, or when the accelerator
pedal wiring is disconnected at the pedal, the cab floor, or the ECM connector. To recalibrate the ECM and the
accelerator pedal, move the key switch to ignition position, slowly move the accelerator pedal from idle position
to fully depressed position and then release. Repeat this cycle two more times to assure proper calibration.
The coolant level switch (249) receives a 5 volt signal on circuit 34B(5V) from the ECM (1093). When the
coolant level is above the probe, the switch sends a high signal (3.5 volts minimum) on circuit 34A and a low
signal (0.5 volt maximum) on circuit 34 to the ECM (1093).
When the coolant level is below the probe, the switch sends a low signal (0.5 volt maximum) on circuit 34A and
a high signal (3.5 volts minimum) on circuit 34 to ECM (251).
The low coolant level switch is grounded through circuit 34–G to ECM (1093).
NOTE – The low coolant level switch cannot be tested with a multimeter in the ohmmeter mode. This is
because the switch is an electronic switch and not a mechanical switch.
Once the system is active, the driver can accelerate beyond the set speed by depressing the accelerator
pedal. When the pedal is released, cruise control is reactivated when the vehicle speed reaches the previously
set speed.
Cruise is deactivated, and returns to the standby mode in several ways: the brake or clutch pedal is depressed,
or the vehicle speed (mph) drops below 30 mph.
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9 CUMMINS ISM AND AHD ENGINE SYSTEM 325
The resume switch can be used to reactivate cruise at the previous set speed, or the set switch can be used
to establish a new set speed.
While in the active mode, the coast feature is used to decrease vehicle speed and establish a new lower set
speed. By holding select switch in the coast position vehicle speed decreases until the switch is released;
the speed at release becomes the new set speed.
While in the active mode, the accelerate feature is used to increase the vehicle speed and establish a new
higher speed. By holding the select switch in the accel. position, vehicle speed increases until the switch is
released; the speed at release becomes the new set speed.
The cruise control switches are used as PTO or idle adjustment controls when the vehicle road speed is not
present (this is a customer selected parameter). The cruise set/resume switch is also used during on-board
diagnostics (when the diagnostic switch is in the on position) to move through the diagnostic fault code list.
Refer to the operators manual furnished with the vehicle for specific cruise control operating instructions.
When the vehicle is not moving and the cruise on/off switch is off, the engine idle speed can be adjusted by
the set/resume switch in increments of 25 RPM by toggling the switch. Maximum idle speed is 800 RPM
and minimum idle speed is 550 RPM.
When the vehicle is not moving and the cruise on/off switch is on, the PTO speed can be adjusted with
the set/resume switch.
The lighted cruise control on/off switch (435) receives a ground signal on circuits 97–GC, 97–GA, connector
(190), on circuit 97–GA from (1091). In the on position, a ground signal is sent from the switch on circuit
97AE, connector (190) and circuit 97AE to ECM connector (1091) terminal 23. This indicates to the ECM
that the cruise control switch is in the on position. In the off position, circuit 97AE returns to its 12 volt value,
indicating to the ECM that the switch is off.
The lighted cruise set/resume switch is a momentary switch. This switch receives a ground signal on circuits
97–GB, connector (190) on circuit 97–GA, from (1091). The cruise selector switch sends a ground signal from
the switch on circuit 97AB, connector (190) and circuit 97AB to the ECM connector (1091) terminal 14 while in
the set/accel. position. In the resume/coast position, the switch sends a ground signal by way of circuit 97AA,
connector (190) and circuit 97AA to the ECM connector (1091) terminal 24.
When the brake is applied the ground will be removed signaling the ECM that the brake has been applied.
The switch is provided a ground path over circuits 97–GH, 97–GH, through connector (190) on circuit 97–GA
from (1091). The clutch switch (294) sends a ground signal by way of circuit 97AH, connector (190) and circuit
97AH to the ECM connector (1091) terminal 4 while the clutch pedal is released.
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Two types of sensors are available. The threaded (adjustable) sensor ids used in most transmissions. A new
push-in (non-adjustable) sensor is used on some transmissions.
When lighted switch (433) is placed in the first position, a ground is applied to circuit 24AE, connector (190),
and circuit 24AE to the ECM (1091). This tells the ECM to enable the brake solenoid for the front three cylinders
on the ISM engine and enables the solenoids for two cylinders on the AHD engine when braking is called for.
When switch (433) is placed in the second position, a ground is applied to circuit 24AF (and 14AP with the
AHD), through connector (190) to ECM (1091). This tells the ECM to enable the brake solenoid for the
rear three cylinders on the ISM engine and enables the solenoids for four cylinders on the AHD engine
when braking is called for.
When switch (433) is placed in the third position, a ground is placed on circuit 24E. Ground is also placed on
circuit 24AF (and 24AP with the AHD), through connector (190) to the ECM (1091). This tells the ECM to
enable the brake solenoids for all cylinders on the ISM engine and the AHD engine when braking is called for.
A. Circuit 98YL(+) is the positive data link connection. It originates from ECM connector (1091),
terminal 46. The circuit is connected to J1939 terminating resistor connector (1098), terminal
A, J1939 backbone connector (1097), terminal A, and J1939 cap diagnostic connector (1095),
terminal A.
B. Circuit 98GN(-) is the negative data link connection. It originates from ECM connector (1091),
terminal 37. The circuit is connected to J1939 terminating resistor connector (1098), terminal C,
J1939 backbone connector (1097), terminal C, and J1939 cap diagnostic connector (1095),
terminal B.
C. Circuit 98SHD is the data link shield connection. It originates from ECM connector (1091), terminal
36. The circuit is connected to J1939 terminating resistor connector (1098), terminal B, J1939
backbone connector (1097), terminal B, and J1939 cap diagnostic connector (1095), terminal C.
3. TROUBLESHOOTING
Refer to the Cummins AHD and ISM — ENGINE CONTROLS circuit diagrams in CTS-5298 or S08225.
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9 CUMMINS ISM AND AHD ENGINE SYSTEM 327
This section includes troubleshooting charts for International installed circuits and components that are part of
the CM570 Electronic Control system. To begin the troubleshooting process, refer to the appropriate Cummins
manual and follow their directions. If the Cummins diagnostics (fault codes) indicate that the suspect circuits
are International circuits or components, then use the charts in this section.
The EZ-Tech or PRO-LINK 9000 EST can also be used to determine if the International switches and
components are working properly. If they are not, use a Fluke digital multimeter (DMM) to troubleshoot
the circuits.
If the Cummins diagnostic (fault codes) or the EZ-Tech or the PRO-LINK indicate a problem with International
installed circuits, the diagnostic tables in this chapter provide step-by-step test procedures.
A. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of
charge (SOC) or higher. This represents an open circuit voltage (OCV) of 12.4 volts. Batteries
with an OCV of 12 volts or less are either completely discharged or have a dead cell.
B. Before beginning these test procedures, check any light or indicator lamp filaments that are
suspected of being open (burned out). This is done to avoid unnecessary extensive circuit checks.
C. Before beginning these test procedures, inspect all connectors for loose or damaged pins,
wires, etc. Refer to TEST EQUIPMENT AND CONNECTOR REPAIR section in GROUP 08 —
ELECTRICAL in the CTS-5000 Master Service Manual.
D. When the technician determines that a fuse is blown, while checking its condition, he is directed
to locate the cause of the overload condition and to repair it. While no further instruction on this
procedure is listed in the diagnostic tables, the common procedure is as follows: isolate sections
of the circuit, by disconnecting connectors, and measure the resistance to ground to find the circuit
that is shorted to ground. Then locate the damaged spot in the wire or connector and repair.
E. Diagnostics for circuits that are malfunctioning by sticking in the position are generally not covered
in detail. It is assumed that the technician knows to check for a malfunctioning switch, relay, or
solenoid.
If the warning lights remain on, it is an indication that the ECM has detected a problem. The CM570 system
can show and record certain problems. The problems are shown as fault codes. The fault codes are recorded
in the ECM.
If a fault is detected (becomes active) during vehicle operation, the driver is alerted by the illumination of
either the yellow Engine Warning Light or the red Stop Engine Light. The yellow Service/Check Engine
Light may also be illuminated.
The yellow Engine Warning light turns on to warn the driver of an active component or system fault that should
be serviced as soon as possible to solve the problem, but the situation is not considered an emergency.
The red Stop Engine light turns on to warn the driver that there is a major system problem and the vehicle
should be stopped and engine shut down as soon as is safely possible.
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328 9 CUMMINS ISM AND AHD ENGINE SYSTEM
The yellow Service/Check Engine Light (engine protection system) turns on to warn the driver that:
NOTE – Cummins CM570 engine diagnostics must be run with the engine NOT RUNNING.
If BOTH Yellow Engine Warning andRed Engine Stop lights come ON and stay ON, it is an indication that
no engine faults are present.
If BOTH the yellow Engine Warning and red Engine Stop lights come on momentarily and then go out, it is an
indication that engine faults are present.
If BOTH the yellow Engine Warning and red Engine Stop lights come on and stay on, it is an indication that
no engine faults are present.
7. Red Engine Stop will flash code with one or two seconds between digits.
8. Yellow Engine Warning light will flash indicating the end of that fault code, and then start over and
repeat the same fault code.
9. To go to the second fault code, move the Set/Resume switch to the Inc. position and then release it. The
process will then repeat itself as indicated in steps 5 through 8.
10. To move back to the last or previous fault code, move the Set/Resume switch to the Dec position and then
release it. The process will then repeat itself as indicated in steps 5 through 8.
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9 CUMMINS ISM AND AHD ENGINE SYSTEM 329
11. To stop the diagnostics procedure, correct the faults or move the diagnostic On/Off switch to the off,
and turn the vehicle key switch to the off position.
The EZ-Tech or Pro-Link 9000 can also be used to monitor operation of various switches and controls and
perform other diagnostic tasks. The specific capabilities and operating instructions are included in the EZ-Tech
or Pro-Link 9000 documentation.
3.5. RELAYS
International circuits use suppressed relays for controlling power to load devices. The suppression feature (a
resistor circuit parallel to the relay coil) prevents voltage spikes from damaging electronic components in the
vehicle. These relays must be replaced with the correct International part.
Relays used in exposed areas such as the engine compartment are sealed relays and are a different part
number than those in the cab. The part number is embossed on the relay. There is also a circuit diagram of the
relay located on the relay body. The terminals are numbered on the relay in the same manner as in the circuit
diagrams. To test the relay, refer toTesting Relay below.
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330 9 CUMMINS ISM AND AHD ENGINE SYSTEM
The tests should be performed if a Cummins fault code indicates a problem in the circuits or if the Compulink,
EZ-Tech or Pro-Link 9000 EST indicates that the TPS/IVS is not working properly while monitoring switches. If
CompulinkTM detects a fault with the IVS circuits while monitoring switches, the display would show Idle
Validation Switch = Fault. If a fault is present while monitoring Percent Of Throttle, the percent displayed
does not indicate actual throttle position.
NOTE – The following two tests, Testing Throttle Position Sensor (TPS) and Testing Idle Validation Switch
(IVS), check operation of the TPS and IVS, but do not check the timing between the two functions.
This test checks the TPS circuits in the accelerator pedal assembly. This test will help identify if the resistances
are within specifications and if there are any opens or shorts in the TPS, but will not verify the correct
switching of the IVS and TPS.
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9 CUMMINS ISM AND AHD ENGINE SYSTEM 331
Perform Testing Throttle Position Sensor (TPS) before performing this test.
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332 9 CUMMINS ISM AND AHD ENGINE SYSTEM
This test checks the cab and engine harness TPS/IVS circuits for opens, shorts to ground, shorts to “hot”
circuits and shorts to other circuits in the harness.
Table 99 Testing Accelerator Pedal (TPS/IVS) System for “Short or Open” Circuits
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off With (267) disconnected, Go to next Replace connector
disconnect connector step. terminals if damaged.
(1091) from ECM and If ECM pins are
inspect ECM connector. damaged, have
Connector and ECM pins Cummins dealer
OK? replace ECM. Refer
to Accelerator/
ECM Calibration to
recalibrate the ECM to
TPS/IVS.
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9 CUMMINS ISM AND AHD ENGINE SYSTEM 333
Table 99 Testing Accelerator Pedal (TPS/IVS) System for “Short or Open” Circuits (cont.)
2. Off At connector (1091) use (1091), >100K Go to next Locate short to ground
test leads and measure 99B, 99C, ohms. step. in circuit where terminal
resistance to gnd. at 97-GA, resistance is less than
terminals 3, 13, 49, 47, 99, 99A 100K ohms, then repair.
48 and 10 (circuits 99B, and 99G
99C, 97-GA, 99, 99A and to gnd.
99-G). Do not use probes
or leads other than
Cummins P/N 3822758
or the connector could be
damaged.
3. Off At connector (1091) use (1091), >100K Go to next Locate short between
test leads and measure between ohms. step. any circuits where
resistance between 99B, 99C, resistance between
terminals 3, 13, 49, 47, 97-GA, terminals is less than
48 and 10 (circuits 99B, 99, 99A, 100K ohms, then repair.
99C, 97-GA, 99, 99A and 99-G
and 99-G) and all other and all
terminals in (1091). other
circuits.
4. On At connector (1091) (252), <1.5 Go to Locate short to
use test leads and 99B, 99C, volts. Testing unwanted voltage
measure voltage to gnd. 97-GA, TPS/IVS source in any circuit
at terminals 3, 13, 49, 47, 99, 99A Circuits for where more than
48 and 10 (circuits 98B, and 99-G Continuity. 1.5 volts is present,
99C, 97-GA, 99, 99A and to gnd. then repair. Go
99-G). to Accelerator/
ECM Calibration
to recalibrate ECM/
accelerator pedal.
This test checks the individual TPS and IVS circuits (cab and engine harness) for correct resistance while
disconnected from the accelerator pedal assembly and ECM. Perform the preceding three tests before
performing this test.
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9 CUMMINS ISM AND AHD ENGINE SYSTEM 335
Accelerator/ECM Calibration
The electronic accelerator pedal assembly and the ECM must be calibrated when:
This test procedure requires a VOM to check the International harness for opens, shorts to ground, or shorts
to other circuits in the International harness. The low coolant sensor has complex circuits and a VOM
should not be used to test the sensor as it may damage the circuits.
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336 9 CUMMINS ISM AND AHD ENGINE SYSTEM
Table 101 Testing Low Coolant Level Switch And Circuits (cont.)
4. Off Measure resistance of 34, 34A, <5 ohms. Go to Locate open or poor
circuits 34, 34A, 34-G 34-G, and next connection in circuit(s),
and 34B(5V) between 34B(5V) step. if resistance is more
connectors (249) and between than 5 ohms, then
(1093). (249) and repair.
(1093).
5. Off The low coolant switch
circuits check good. If
problem is still present,
replace low coolant
switch. If problem
persists, have Cummins
dealer diagnose ECM
operation.
Table 102 Testing Unswitched Battery Power Circuits And ECM Ground Circuit
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off Check ECM power Good Go to Correct poor
harness connector at con- nec- next connections.
starter circuits 14A, tion. step.
1B and 11-G and at
connector (675) and
(1094) for clean, tight
connections.
2. Off Check the two 15 amp ECM fuses. <5 ohms. Go to Locate cause of
fuses located in the next overload condition,
engine harness for open step. then correct. Replace
condition. with correct rated fuse.
3. Off Disconnect ECM power (1094), 4C 12 ± 1.5 Go to Locate cause of low
connector (1094) and 14D to volts. next or no voltage in circuit
from Cummins engine gnd. step. 14C or 14D from
harness. Measure batteries, then repair.
voltage to gnd. at circuits
14C and 14D. Battery
voltage present?
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9 CUMMINS ISM AND AHD ENGINE SYSTEM 337
Table 102 Testing Unswitched Battery Power Circuits And ECM Ground Circuit (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
4. Off At connector (1094) (1094), 14C 12 ± 1.5 Go to Locate open or high
measure voltage between to 11-G. volts. next resistance in circuit
circuits 14C and 11-G. step. 11-G between (1094)
Battery voltage present? and batteries, then
repair.
5. On At connector (1094) (1094), >7 volts. Go to Locate cause of
measure voltage between 14C to next excess voltage drop in
circuits 14C and 11-G 11-G while step. cranking circuit, then
while cranking engine. cranking. repair.
6. Off Unswitched battery power
circuits and ECM gnd.
circuit at connector (1094)
checks good.
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9 CUMMINS ISM AND AHD ENGINE SYSTEM 339
CAUTION – When testing at ECM connector (1091), do not use probes or leads other than Cummins
test leads, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
Table 105 Testing Clutch Switch Circuits for "Open And Short" Condition
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off With clutch switch Go to next Replace damaged
disconnected, remove step. harness connector
ECM connector (1091) terminals if
from the ECM. ECM damaged. If ECM
harness connector or pins are damaged,
ECM pins OK? have Cummins
dealer replace
ECM. Refer to
Accelerator/ECM
Calibration to
recalibrate ECM/
accelerator pedal.
2. Off Set service brake using (1091), >100K Go to next Locate short to
trailer hand valve. 97AH and ohms. step. gnd. in circuit
Disconnect clutch switch 97-GA to where resistance
(294). Use test leads gnd. at terminal was less
and measure resistance than 100K ohms,
to ground at connector then repair.
(1091) terminal 2 and 10
cir. 97AH and 97-GA).
3. Off Use test leads and (1091), >100K Go to next Locate short
measure resistance 97AH and ohms. step. between circuits,
between terminals 2 and 97-GA and then repair.
10 (cir. 97AH and 97-GA) all other
and all other terminals in circuits.
connector (1091).
4. On At connector (1091), (1091), <1.5 The clutch Locate short to
use test leads and 97AH and volts. switch unwanted voltage
measure voltage to gnd. 97-GA to circuits source in circuit with
at terminals 2 and 10 (cir. gnd. are free more than 1.5 volts,
97AH and 97-GA). of short then repair.
circuits.
Perform
Testing
Clutch
Switch
Circuits for
Continuity.
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340 9 CUMMINS ISM AND AHD ENGINE SYSTEM
CAUTION – When testing at ECM connector (1091), do not use probes or leads other than Cummins
test leads, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
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9 CUMMINS ISM AND AHD ENGINE SYSTEM 341
Testing Service Brake Switch Circuits for "Open and Short" Condition
Perform Testing Service Brake Switch (141) before performing this test.
CAUTION – When testing at ECM connector (1091), do not use probes or leads other than Cummins
test leads, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
Table 108 Testing Service Brake Switch Circuits for "Open and Short" Condition
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off With connector (141) Go to next Replace harness
disconnected from step. connector terminals
brake switch. Remove if damaged. If ECM
connector (1091) pins damaged, have
from the ECM. ECM Cummins dealer
connector and ECM pins replace ECM.
OK?
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342 9 CUMMINS ISM AND AHD ENGINE SYSTEM
Table 108 Testing Service Brake Switch Circuits for "Open and Short" Condition (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
2. Off Disconnect clutch (1091), >100K Go to next Locate short to gnd.
switch. Use test leads 97AL and ohms. step. in circuit where
and measure resistance 97-GA to resistance at terminal
to ground at connector gnd. was less than 100K
(1091) terminals 1 and ohms, then repair.
10 (circuits 97AL and
97-GA).
3. Off Use test leads and (1091), >100K Go to next Locate short between
measure resistance 97AL to ohms. step. any circuit where
between terminal 1 and 97-G A and resistance between
10 (cir. 97AL and 97-G) all other terminals is less than
and all other terminals in circuits. 100K ohms, then
connector (1091). repair.
4. On At connector (1091), (1091), <1.5 The brake Locate short to
use test leads and 97AL and volts. switch unwanted voltage
measure voltage to 97-GA to circuits are source in circuit with
gnd. at terminals 1 and gnd. free of short more than 1.5 volts,
10 (circuits 97AL and circuits. then repair.
97-GA). Perform
Testing
Service
Brake
Switch
Circuits for
Continuity.
CAUTION – When testing at ECM connector (1091), do not use probes or leads other than Cummins
test leads, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
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Table 109 Testing Service Brake Switch Circuits for Continuity (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
2. Off At ECM connector (1091) (141), 97AL <5 ohms. Go to Locate open or poor
use test lead to jumper to 97-GF. next connection in circuit
terminal 1 to terminal 10 step. 97-GF or 97-GA
(cir. 97AL to 97-GA). At between connectors
brake switch connector (1091) and (141), then
(141) measure resistance repair.
between circuits 97AL
and 97-GF.
3. Off The service brake switch
circuits and switch
check good.
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Testing Data Link Circuits Between Diagnostic Connector, ECM and Speedometer/Tachometer Unit
CAUTION – When testing at ECM connector (1091), do not use probes or leads other than Cummins
test lead , Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
Table 112 Testing Data Link Circuits Between Diagnostic Connector, ECM and
Speedometer/Tachometer Unit
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
1. Off Disconnect ECM conn. Harness Go to Replace harness
(1091) from the ECM. conn. OK. next conn. terminals if
Inspect conn. ECM step. damaged. If ECM
harness connector OK? pins are damaged,
have Cummins
dealer replace ECM.
Refer to Accelerator/
ECM Calibration to
recalibrate ECM/
accelerator pedal.
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Table 112 Testing Data Link Circuits Between Diagnostic Connector, ECM and
Speedometer/Tachometer Unit (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
2. Off Disconnect connector (1091), >100K Go to Locate short circuit to
(421) from speedometer/ 98B(-) and ohms. next gnd in circuit where
tachometer unit and 98(+) to step. resistance is less
if additional devices gnd. than 100K ohms, then
have been connected repair.
to (514) and (515) data
link connectors, they
must be disconnected.
At connector (1091),
using test leads, measure
resistance to gnd. at
terminals 26 and 27
(circuit 98B[+] and 98[-]).
3. On At connector (1091) (1091), >100K Go to Locate short between
use test leads and 98B(-) and ohms. next circuits where
measure resistance 98(+) and step. resistance between
between terminal 26 and all other terminals is less than
terminal 27 (circuits 98B[+] circuits in 100K ohms, then
and 98[-]) and all other conn. repair.
terminals in connector.
4. On At connector (1091) use (1091), <1.5 volts. Go to Locate short to
test leads and measure 98b(-) and next unwanted voltage
voltage to gnd. at 98(+) to step. source in circuit where
terminals 26 and 27 gnd. more than 1.5 volts
(circuits 98B[+] and 98[-]). is present at terminal,
then repair.
5. Off At connector (1091) use (137), <5 ohms. Go to Locate open or poor
test lead to jumper terminal 98C(-) to next connection in circuit
27 (cir. 98B[-]) to gnd. At gnd. step. 98B(-)/98C(-) between
connector (137) measure connectors (1091) and
resistance to gnd. at (137), then repair.
terminal B (cir. 98C[-]).
6. Off With connector (1091) (421) 47/ <5 ohms. Go to Locate open or poor
terminal 27 (circuit 98B[-]) 48(-) to next connection in circuit
still jumpered to ground, at gnd. step. 47/48(-) between
speedometer/ tachometer connectors (515) and
connector (421) measure (421), then repair.
resistance to gnd. at
circuit 47/48(-).
7. Off At connector (1091) use (137), <5 ohms. Go to Locate open or poor
test lead to jumper terminal 98A(+) to next connection in circuit
27 (cir. 98[+]) to gnd. At gnd. step. 98(+)/98(+) between
connector (137) measure connectors (1091) and
resistance terminal A (137), then repair.
(circuit 98A[+]) to gnd.
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Table 112 Testing Data Link Circuits Between Diagnostic Connector, ECM and
Speedometer/Tachometer Unit (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
8. Off With connector (1091) (421), 47/ <5 ohms. Go to Locate open or poor
terminal 27 (cir. 98[+]) still 48(+) to next connection in circuit
jumpered to ground, at gnd. step. 47/48(+) between
connector (421) measure connectors (514) and
resistance to gnd. at (421), then repair.
circuit 47/48(+).
9. Off The data link circuits
between ECM connector
(1091), diagnostic
connector (137) and
speedometer/ tachometer
connector (421) test good.
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CAUTION – When testing at ECM connector (1091), do not use probes or leads other than Cummins
test leads, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
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Table 114 Testing Cruise Control On/Off Switch and Circuits (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
6. Off At connector (1091) (1091), >100K Go to Locate short between
measure resistance 23 to ohms. next circuit 97AE and
between terminal 23 and all other step. any circuit where
all other terminals in terminals. resistance between
connector. terminals is less than
100K ohms, then
repair.
7. On At connector (1091) (1091), <1.5 volts. Go to Locate short between
measure voltage from 97AE to next circuit 97AE and
terminal 23 (circuit 97AE) gnd. step. unwanted voltage
to ground. source, then repair.
8. Off At connector (1091) use (435), <5 ohms. Go to Locate open or
test lead to jumper terminal 97AE to next poor connection in
23 (cir. 97AE) to gnd. At gnd. step. circuit 97AE between
connector (435) measure connectors (1091) and
resistance to gnd. at circuit (435), then repair.
97AE.
9. Off Measure the resistance Between <5 ohms. Go to Locate open or poor
between connector (1091), (1091), next connection in circuit
terminal 10 (cir. 97-G) and terminal step. 97-GC, 97-GA or
connector (435), cir. 10 and 97-G, then repair.
97-GC. (435),
97-GC.
10. Off The cruise On/Off switch
and circuits check good.
CAUTION – When testing at ECM connector (1091), do not use probes or leads other than Cummins
test leads, Part No. 3822758. The connector will be damaged. The leads must fit snug without
expanding the connector terminal.
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1. Disconnect engine harness connector (1099) from the sensor. Loosen the locknut and remove the sensor.
The harness connector and sensor should be free of damage or corrosion. Remove any metal shavings or
debris from the sensor.
2. To install the adjustable sensor, turn in until the sensor contacts the transmission speedometer gear,
then back out one full turn. Tighten lock nut to 15 ft-lbs. (20.3 N•m). This assures that the sensor
is adjusted properly for the next test.
Testing Vehicle Speed Sensor
Construct test leads using terminals (International Part No. 1680205C1), short length of 16 gauge wire
and alligator clips.
WARNING – A jack must never be used alone to support vehicle. The jack may lower and
serious injury could result. Always support vehicle with floor jacks. Always block wheels to prevent
vehicle from moving.
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WARNING – EXTREME CAUTION should be used to prevent personal injury resulting from
contact with rotating vehicle wheels when connecting test leads.
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To check circuits between the ECM and the speedometer/tachometer unit, refer toATA Data Link Connector
(137) and Speedometer/Tachometer Input Circuits.
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4. COMPONENT LOCATIONS
B1 Battery Stud.. . .. .. . .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . . . . . Power Distribution Panel
(1) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Left Side of Engine Cowl
(2) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Right Side of Engine Cowl, Above Connector 3
(3) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Right Side of Engine Cowl, Below Connector 2
(72) Ether Start Connector. . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Front End Harness, At Lower Left of Radiator
(94) Back-up Light Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . On Transmission
(137) 6-Way Data Link Connector. . . . . . . . . . . . . . . . . . .. . . . . . Power Distribution Panel
(141) Service Brake Switch/Cruise Switch. . . . . . . . .. . . . . . Dash Panel, Left Side, Engine Side
(190) Cab Overlay to Elect. Eng. Harn.. . . . . . . . . . . .. . . . . . Right Instrument Panel
(227) Fan Solenoid . . . . . . .. . . . . . . . . .. . . . . . . . .. . . . . . . . .. . . . . . At Front of Engine
(228) Refrigerant Pressure Switch . . .. . .. . .. . .. . .. . .. . . . . . On A/C Compressor
(229) Engine Oil Temp. Sender. .. . .. . .. . .. . .. . .. . .. .. . . . . . Left Side of Engine
(235) Transmission Oil Temp. (Inline). . . .. . . . . .. . . . .. . . . . . On Front of Transmission
(249) Low Coolant Level Switch. . . . . . . . . . . . . . . . . . . . .. . . . . . To Engine Harness
(267) Accelerator Pedal. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . To Cab Overlay
(294) Clutch Switch Connector. . . . . . . . . . . . . . . . . . . . . .. . . . . . Near Clutch Switch
(420) Right Gauge Cluster. . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Gauge Cluster
(421) Speedo./Tach. Module. .. . . .. . . .. . . .. . . .. . . .. . .. . . . . . Behind Speedo./Tach. Gauge
(422) Speedo./Tach. Module. .. . . .. . . .. . . .. . . .. . . .. . .. . . . . . Behind Speedo./Tach. Gauge
(423) Left Gauge Cluster. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Left Gauge Cluster
(424) Left Gauge Cluster. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Left Gauge Cluster
(514) Data Link — Positive. . . .. . . .. . . .. . . .. . . .. . . .. . .. . . . . . Behind Instrument Panel/Behind Cluster
(515) Data Link — Negative. .. .. . .. .. .. .. .. . .. .. .. .. .. . . . . . Behind Instrument Panel/Behind Cluster
(1091) Electronic Control Module ECM. . . . . . . . . . . . .. . . . . . At ECM
(1093) ECM Interface Connector. . . . . . . . . . . . . . . . . . . .. . . . . . At Engine Harness near ECM
(1094) ECM Power Connector. . . . . .. . . . . .. . . . . .. . . . .. . . . . . At Engine Harness near ECM
(1099) Vehicle Speed Sensor. . . . . .. . . . . .. . . . . .. . . . . .. . . . . . On Transmission
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Table of Contents
1. DESCRIPTION. .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .373
2. OPERATION.. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .373
2.1. CEC POWER AND GROUND. . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . .374
2.2. ACCELERATOR POSITION SENSOR (APS) AND IDLE VALIDATION SWITCH (IVS).. .. .. .. .374
2.3. BAROMETRIC AIR PRESSURE (BAP) SENSOR. . . . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . .375
2.4. AIR TEMPERATURE SENSOR (ATS). .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .375
2.5. ATA DATA LINK CONNECTOR. . .. . . .. . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . .375
2.6. DIAGNOSTIC ON/OFF SWITCH. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .376
2.7. CRUISE CONTROL/PTO SYSTEM. .. . .. . . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .376
2.8. CLUTCH SWITCH.. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . . .. . . . .376
2.9. COOLANT LEVEL PROBE. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . .377
2.10. VEHICLE SPEED SENSOR (VSS). .. . . . .. . . . .. . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . .. . . . .. . . .377
2.11. SERVICE BRAKE SWITCH. .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . .377
2.12. ANTILOCK BRAKE INTERFACE. . . . . . . . . .. . . . . . . . . . . . . . .. . . . . . . . . . . . . .. . . . . . . . . . . . . . .. . . . . . . . . . . . . .377
2.13. ENGINE BRAKE. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. .377
3. TROUBLESHOOTING. .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .378
3.1. DETERMINING FAULT CODES.. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .378
Reading Flash Codes. . . .. . . . . . .. . . . . . .. . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . .379
3.2. IMPORTANT STEPS BEFORE TESTING. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .379
3.3. INSPECTING ELECTRICAL CONNECTORS. . . . . . . .. . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . .380
Visual Inspection. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .380
Performing Electrical Tests at CEC Module Connector (379). . . . . . . . . . . . . .. . . . . . . . . . . . . . . . .380
Replacing International Components. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . .380
3.4. TESTING HELLA RELAY. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .381
3.5. CEC POWER AND GROUND SYSTEM CIRCUITRY.. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .381
3.6. ACCELERATOR (APS/IVS), BAROMETRIC AIR PRESSURE (BAP) AND AMBIENT AIR
TEMPERATURE SENSOR SYSTEMS (ATS). . . . .. . . . . . . . . . .. . . . . . . . . .. . . . . . . . . . .. . . . . . . . . .. . . . . . . . . .384
3.7. DIAGNOSTIC CONNECTOR (137) AND DATA LINK CIRCUITS. . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .386
Testing Diagnostic Connector Power and Ground Circuits. . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .386
3.8. TESTING DIAGNOSTIC CONNECTOR AND SPEEDOMETER/TACHOMETER POSITIVE AND
NEGATIVE DATA LINK CIRCUITS. . .. . . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .387
3.9. VEHICLE SPEED SIGNAL.. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .388
Testing Vehicle Speed Sensor (303). .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .. . . .. . .389
Testing Vehicle Speed Sensor To ECM Circuits. .. . .. . . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .390
3.10. CRUISE AND PTO CONTROLS.. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .391
Testing Cruise On/Off Switch and Circuits. . .. . .. . .. . . .. . .. . . .. . .. . .. . . .. . .. . .. . . .. . .. . . .. . .. . .391
Testing Cruise Set/Resume Switch and Circuits. . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . .391
3.11. CLUTCH SWITCH (294). . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .392
Testing Clutch Switch and Circuits.. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .392
Adjusting Clutch Switch.. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. .393
3.12. SERVICE BRAKE SWITCH (141). . . . . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . .393
Testing Service Brake Switch and Circuits. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .393
3.13. TESTING LOW COOLANT SENSOR AND CIRCUITS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .394
3.14. ENGINE BRAKE CONTROLS. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .. . . .395
Testing Engine Brake Switches and Circuits. . . . .. . . . . . . . . . . . . . .. . . . . . . . . . . . . . .. . . . . . . . . . . . . . .395
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1. DESCRIPTION
Refer to Diagnostic Manual EGES-175 for detailed information.
The Diamond Logic CEC is standard on International engines and provides many engine/vehicle functions
including:
A. Cruise/PTO Controls
B. Engine Diagnostics
C. Engine Protection System
D. Engine Cooling System
E. Exhaust Brake Control
F. Speedometer/Tachometer Input Signals
G. ABS/Traction Control Interface.
Refer to the International manual furnished with the vehicle for additional feature information.
Since each CEC is electronically programmable to individual owner specifications, the operating parameters
will vary from vehicle to vehicle.
The CEC receives inputs from sensors and switches, then outputs signals to the injectors, exhaust brake
solenoid, and other system components.
For information on remote PTO control for body builder applications, refer to Miscellaneous Information
in CT-471 Body Builder Book.
2. OPERATION
Refer to the circuit diagram I6 HEUI-ENGINE CONTROLS in CTS-5298 or S08225.
The CEC is connected to the International electrical system at CEC module connector (379).
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Power is supplied from the batteries to circuit 14A, a 40A power relay fuse, circuit 14B, positive battery
connector, circuit 14B, power connector (490), and circuit 14B to the Electronic Control Module (CEC) power
relay (396) contacts.
Power is also supplied from the (B1) battery feed stud to circuit 14BB, fuse F10B, circuit 97DCT, circuit
97CT, bulkhead connector (190), and circuit 97CT to the Module power relay coil. From the relay, power is
applied to circuit 97AH and pin 25 of the CEC (379).
When key switch (24) is moved to the ignition position, power is supplied to circuit 13AA, fuse F10C, circuit
97DS, circuit 97CR, bulkhead connector (190), and circuit 97CR to pin 24 of the CEC (379). This signals the
CEC that the ignition switch is on and causes the CEC to internally switch pin 25 to ground. This completes the
circuit for the Module power relay (396) and energizes the relay. With the relay energized, power is applied
through the relay contacts to circuit 97CM and a splice. From the splice power is applied to the CEC pins 21,
22, and 41 on circuits 97CL, 97CK, and 97AL respectively.
Grounds for the CEC pins 1, 2, 23, and 42 are through circuits 11–GW, 11–GX, 11–GY, and 11–GZ respectively,
to a splice. From the splice, ground is through circuit 11–G, the battery harness connector (490), circuit 11–G,
negative battery connector (665) and circuit 11–G to the negative battery terminal.
2.2. ACCELERATOR POSITION SENSOR (APS) AND IDLE VALIDATION SWITCH (IVS)
The Accelerator Pedal Position Sensor (APS) is a potentiometer type sensor which, when supplied with a
5 volt reference signal from the Electronic Control Module (CEC), provides a linear analog voltage signal
that indicates the driver’s demand for power. The APS signal is used in calculating desired fuel quantity
and injector timing.
The Idle Validation Switch (IVS) is a 1/12 volt switch that provides the CEC with a redundant signal to verify
when the pedal is in the idle position.
These two functions are integrated into one component mounted on the accelerator pedal. The pedal
assembly is serviceable to the extent that the APS/IVS can be replaced without replacing the complete pedal.
The engine Electronic Control Module (CEC) determines the position of the accelerator pedal by processing
the input signals from the Accelerator Position Sensor (APS) and Idle Validation Switch (IVS).
The CEC sends a regulated 5 volt signal through the black CEC module connector (379), circuit 97U, engine
connector (190), circuit 97U to a splice, and circuit 99C to the APS/IVS (267). The APS then returns a variable
voltage signal (depending on pedal position) from connector (267), circuit 99A, connector (190) and circuit
99B to CEC module connector (379). The APS is grounded through circuit 99B/97W, connector (190), and
circuit 97W/97BW to CEC (379).
The CEC learns the lowest and highest pedal positions by reading and storing the minimum and the maximum
voltage levels from the APS. In this manner the CEC “auto-calibrates” the system to allow maximum pedal
sensitivity. The CEC auto-calibrates as the key is on, but when the key is turned off, these values are lost.
When the key is turned on again, this process starts over. When the pedal is disconnected (or a new one is
installed), the pedal does not need to be calibrated, as the calibration happens when the key is turned on.
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The Idle Validation Switch (IVS) (267) receives 12 volt ignition voltage from ignition adapter (494) circuits
13BBB, fuse F10A, circuit 47A and circuit 99E. When the pedal is not in the idle position (throttle applied),
the IVS sends this 12 volt signal to the CEC over circuit 99D, clutch switch (294), connector (190), and
circuit 99D to the CEC (379).
The CEC (379) compares the inputs it receives on circuit 99B and circuit 97A from the APS/IVS to verify
when the pedal is in the idle position. If the APS signal from circuit 99B indicates throttle is being applied,
then the CEC expects to see 12 volts at IVS circuit 97A. If the APS signal, circuit 99B, indicates throttle is not
applied, then the CEC expects to see 0 volts at the IVS circuit 97A. The timing process is critical between
the APS and the IVS sensors. For this reason, it is very difficult to determine if the APS/IVS assembly is
working properly using a volt-ohmmeter.
The CEC (379) sends a regulated 5 volt signal from CEC (379) on circuit 97U, through the black CEC module
connector (379), circuit 97U, engine connector (190), circuit 97U to a splice, and circuit 97BL to BAP sensor
(1160). The BAP sensor (1160) returns a variable voltage signal (represents atmospheric pressure) on circuit
97CD, connector (190) and circuit 97CD to the CEC (379). The BAP sensor (1160) is grounded by circuit
97Z/97W, connector (190), circuit 97BW to the CEC (379) signal ground.
The CEC module connector (379) sends a regulated 5 volt reference signal through circuit 97AX to the
Air Temperature Sensor (463). As the temperature changes, the sensor changes resistance and provides
the CEC with an air temperature signal voltage. The sensor is grounded through circuit 97BU/97BW to
the CEC signal ground.
The ATA data link connector (137), which is located on the left instrument panel, has circuits in four of the
six cavities. The data link circuits are a twisted wire pair because twisting the wires helps shield them from
interference. The circuits are as follows:
A. Circuit 98X(+) is the positive data link connection, and it is fed by the positive data link connector
(514), circuit 98(+), connector (190), and circuit 98(+) coming from the CEC module connector
(379).
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B. Circuit 98B(-) is the negative data link connection, and it is fed by the negative data link connector
(515), circuit 98C(-), connector (190), and circuit 98C(-) coming from the ECM CEC module
connector (379).
C. Circuit 97DL is a 12 volt feed and is fed from the battery adapter (497), circuit 14DLF, and 5A fuse
F10–D. Thus, it provides power for the electronic service tool.
D. Circuit 11–GR is connected to ground adapter (453), and provides a ground for the electronic
service tool.
The cruise control switches and circuitry are also used for in-cab control of preset, variable, and mobile PTO
operation applications and required programming of the engine CEC.
Power is supplied to the lighted cruise control on/off switch (391) through I1 ignition adapter, circuit 13AA, fuse
F-10C, circuit 97DS and circuit 97AD. When the on/off switch is in the on position, power is supplied through
circuit 97CF, circuit 97CF, dash connector (190) and circuit 97CF to CEC (379). This enables the cruise control.
The lighted cruise set/resume (436) is a momentary switch. This switch receives 12 volts on circuits 97CA and
97CF from the cruise on/off switch (435) when it is in the on position. The cruise selector switch sends 12 volts
from the switch on circuit 97DJ, connector (190), and circuit 97DJ to CEC module connector (379) terminal 32
while in the set position. In the resume position, the switch sends 12 volts by way of circuit 97DK, connector
(190), and circuit 97DK to the ECM CEC module connector (379) terminal 22. If the cruise control speed has
not been engaged, momentarily depressing the switch causes the CEC to resume the last engine RPM setting.
If the cruise control is already engaged, momentarily depressing the resume/accel portion of the switch will
cause the engine RPM and speed to increase in small incremental amounts until the desired speed is reached.
For information on remote PTO control for body builder applications, refer to Miscellaneous Information
in CT-471 Body Builder Book.
The clutch switch (294) is a normally open (N.O.) switch that is adjusted so that its contacts are closed when
the clutch pedal is in the released position. Depressing the clutch pedal causes the switch contacts to open.
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Twelve (12) volts is supplied to connector (294) terminal B from I1 ign. adapter (494) through circuit 13BBB,
fuse F-10A, circuit 47A and circuit 97. When the switch is closed 12 volts is applied on circuit 97A through
connector (190) to CEC (379).
Two types of sensors are available. The threaded (adjustable) sensor is used on most transmissions. A new
push-in style sensor (nonadjustable) is used on some transmissions.
With the cruise control on/off switch in the on position, power is also applied from the switch to the cruise
set/resume switch (392) through circuit 97CA. Momentarily depressing the set portion of this switch supplies a
12 volt signal to the CEC through circuit 97DA, dash connector (190), and circuit 97DH/7DJ. This engages the
cruise control and causes the CEC to maintain the current engine RPM. If the cruise control speed is already
set, depressing the switch in the set position causes the engine RPM to decrease until the switch is released.
With the cruise control on/off switch (391) in the on position, depressing the resume/accel portion of the
set/resume switch (392) supplies a 12 volt signal to the CEC through circuit 97DE, dash connector (190) and
circuit 97DE/97DK. If the cruise control speed has not been engaged, momentarily depressing the switch
causes the CEC to resume the last engine RPM setting. If the cruise control is already engaged, momentarily
depressing the resume/accel portion of the switch will cause the engine RPM and speed to increase in small
incremental amounts until the desired speed is reached.
The cruise control switches and circuitry are also used for in-cab control of preset, variable, and mobile PTO
operation applications and required programming of the engine CEC.
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board (390) in parallel. The CEC senses the voltage drop, across the parallel resistance, through (390)
and will control the engine accordingly.
The engine brake relay (286) disables engine braking when the ABS is active.
When engine brake on/off switch (434) is on and the engine brake relay is not energized, a ground is sent from
G1 ground adapter (453) on circuit 24–GA, 24AN and 24AT to terminals 2 and 5 of engine brake on/off switch
(434). When engine brake select switch (434) is on, ground will be available at terminals 3 and 6 of the switch.
5 volts from CEC connector (379) will be applied to resistor printed circuit board (390), terminal F. This voltage
will drop across a 2.2K ohm resistor (which may be selected in parallel with other resistors).
When engine brake select switch (433) is in the 1 position, only the 2.2k ohm resistor connected to terminal D
in the printed circuit board (390) will affect the voltage drop in the circuit. This will signal the CEC to select
compression braking on two cylinders of the engine.
When engine brake select switch (433) is in the 2 position, ground from (434) is supplied from terminal 3,
on circuit 24AD, to resistor printed circuit board (390) terminal C. 5 volts from CEC connector (379) will be
applied to resistor printed circuit board (390). The voltage drop across the parallel resistance between the
2.2K ohm and the 680 ohm resistor of printed circuit board (390) will signal the CEC to engage compression
braking on four cylinders of the engine.
When engine brake select switch (433) is in the 3 position, ground from (434) is supplied from terminal 3, on
circuit 24AD, through switch (433), contacts 6, 2 & 3 to resistor printed circuit board (390) terminals B and C. 5
volts from CEC connector (379) will be applied to resistor printed circuit board (390). The voltage drop across
the parallel resistance between the 2.2K ohm, the 680 ohm and the 121 ohm resistor of printed circuit board
(390) will signal the CEC to engage compression braking on all six cylinders of the engine.
3. TROUBLESHOOTING
A. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of
charge (SOC) or higher. This represents an open circuit voltage (OCV) of 12.4 volts. Batteries
with an OCV of 12 volts or less are either completely discharged or have a dead cell.
B. Check any light or indicator lamp filaments that are suspected of being open (burned out). This is
done to avoid unnecessary extensive circuit checks.
C. Inspect all connectors for loose or damaged pins, wires, etc. Refer to TEST EQUIPMENT AND
CONNECTOR REPAIR section in GROUP 08 — ELECTRICAL in the CTS-5000 Master Service
Manual.
D. When the technician determines that a fuse is blown, while checking its condition, he is directed
to locate the cause of the overload condition and to repair it. While no further instruction on this
procedure is listed in the diagnostic tables, the common procedure is as follows: isolate sections
of the circuit, by disconnecting connectors, and measure the resistance to ground to find the circuit
that is shorted to ground. Then locate the damaged spot in the wire or connector and repair.
E. Diagnostics for circuits that are malfunctioning by sticking in the on position are generally not
covered in detail. It is assumed that the technician knows to check for a malfunctioning switch,
relay, or solenoid.
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The EZ-Tech™ or PRO-LINK 9000® electronic service tools (EST) can be used to identify logged fault codes.
Refer to the EST manual for operating instructions.
The Serv/Check Engine and Warn Engine lights can be used to read fault codes by following the procedure
following.
1. Hold in the diagnostic on/off button and turn the key to the on position. Release the diagnostic button.
Do not start the vehicle.
2. The Serv/Check Engine light will FLASH one time. This indicates the beginning of active fault codes.
3. The Warn Engine light will FLASH repeatedly signalling the active fault codes. The number of flashes
should be counted in sequence.
4. At the end of each digit of the code there will be a short pause.
5. After each active code is displayed the Serv/Check Engine light will FLASH once to indicate the next code.
6. Once all active codes have been displayed, the Serv/Check Engine light will FLASH twice to indicate the
beginning of the inactive codes.
8. Once the inactive codes have been displayed, the Serv/Check Engine light will FLASH three times to
indicate that all stored codes have been displayed.
If the diagnostics indicate that a circuit external to the engine is suspect, use the diagnostic tables included in
this section for a step-by-step procedure. Refer to the appropriate circuit diagram for International I6 HEUI
— ENGINES in CTS-5298 or S08225.
2. Verify the problem. Is the complaint due to misunderstood customer selected parameters? Use an EST
to review customer selected parameters.
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4. Were the codes logged about the same time as the symptoms appeared? Were the codes logged
repeatedly?
5. Are the logged codes related to other symptoms? Do they have a common cause?
6. Avoid preconceived ideas! Eliminate any non-electrical causes for the problem first (contaminated
fuel, clogged air filters, etc.).
The troubleshooting guide requires checking specific connectors. Use the following steps to determine if
the connector is causing the problem. If a defective condition is found, make the necessary corrections
and continue the process.
1. Check the connector lock mechanism or retaining screw. Make sure the connector is capable of
properly locking the connector together.
2. Perform a 10 pound pull-test on each terminal/wire in the connector. Each terminal/wire assembly
should easily withstand 10 pounds of pull and remain in the connector. This test determines (A) if the
wire is properly in the terminal and (B) if the terminal is properly inserted into the connector. Correct
any defects noted.
3. Visually inspect wiring. Inspect for worn or damaged wires. Check for pinched or damaged harness.
4. Visually inspect connectors. Verify that pins and sockets are free of corrosion, dirt or any other
contaminants, and damage. Verify correct alignment and location of terminals in the connector.
5. Check individual pins and sockets. This is especially important with an intermittent symptom. Using a
new pin, insert the pin into each socket, one at a time, checking for a good grip on the pin by the socket.
Repeat for each pin on the mating side of the connector, using a new female terminal for the test.
6. Inspect Engine Ground Stud. Inspect this ground and other related grounds for clean, tight connections
that are free of corrosion and/or other defective conditions.
CEC module connector (379) mates with the black ECM connector. This is a 60–pin connector, with the
International side having female terminals (sockets) and the ECM side having pins.
NOTE – No tests in this manual require testing “into” the black ECM connector.
When testing the chassis side of CEC module connector (379), never insert meter probes into the sockets,
as the probes will damage the sockets.Always use breakout box (ZTSE-4445) as described in International
Engine/Vehicle Manual EGES-175.
When replacing electrical switches, connectors (including pins and sockets), relays or other components, use
only approved International replacement parts. Many of the switches have gold or silver plated contacts and
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some of the connectors have gold plated terminals. By using correct replacement parts, you maintain the
design integrity of the system.
All of the relays and other solenoids installed by International are suppressed to prevent voltage spikes from
damaging electrical components. Again, use only International replacements for these components.
The part number and relay circuit diagram are embossed on the relay body. The terminals are numbered on
the relay in the same manner as in the circuit diagrams.
2. Measure resistance between terminals 30 and 87. If resistance is 100K ohms or more, go to step 3;
otherwise replace the relay.
3. Using 12V battery source and test leads, connect (+) lead to terminal 85 and (-) lead to terminal 86. If relay
energizes with an audible click sound, go to step 4; otherwise replace the relay.
4. While relay is energized, measure resistance between terminals 30 and 87. If resistance is less than 5
ohms, go to step 5; otherwise replace the relay.
5. While relay is energized, measure resistance between terminals 30 and 87A. If resistance is 100K or
more, the relay is good; otherwise replace relay.
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Table 119 Accelerator (APS/IVS), Barometric Air Pressure (BAP) and Ambient Air Temperature Sensor
Systems (ATS) (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
6. Off At (267), move jumper to (379), cavity <1 ohm. Go to Locate open or poor
cavity B, circuit 99B and 11, 97BW to next connection in circuit
ground. At (379) cavity 11, ground. step. 97BW/97W, bulkhead
measure resistance of cir. connector (190), or
97BW to ground. cir. 97W/99B, then
repair.
7. Off At (267), move jumper (379), cavity <1 ohm. Go to Locate open or
to cavity C, cir. 99C and 3, 97U to next poor connection in
ground. At (379) cavity ground. step. circuit 97U, bulkhead
3, measure resistance of connector (90), or cir.
circuit 97U to ground. 97U/99C, then repair.
8. Off At (267), move jumper to (379), cavity <1 ohm. Go to Locate open or poor
cavity D, circuit 99D and 27, 99D to next connection in circuit
ground. At (379) cavity ground. step. 99D, or bulkhead
27, measure resistance of connector (190), then
circuit 99D to ground. repair.
9. Off Remove jumper and End test. Replace APS/IVS. If
reconnect connectors. problem persists,
APS/IVS circuits check refer to Engine
good? Is problem Diagnostic Manuals.
corrected?
10. Off Is a fault code present for Go to Go to Step 15.
BAP sensor? next
step.
11. Off Disconnect BAP sensor (379), cavity <1 ohm. Go to Locate open or poor
connector (1160). Install 11, 97BW to next connection in circuit
jumper wire from cavity ground. step. 97Z/97W, bulkhead
1, cir. 97Z to ground. connector (190), or
Disconnect CEC module circuit 97W/97BW,
connector (379). At cavity then repair.
11, measure resistance of
cir. 97BW to ground.
12. Off At (1160), move jumper (379), cavity <1 ohm Go to Locate open or
wire to cavity 2, circuit 3, 97U to next poor connection in
97BL and ground. At ground. step. circuit 97U, bulkhead
(379) cavity 3, measure connector (190), or
resistance of circuit 97U to circuit 97U/97Bl, then
ground. repair.
13. Off At (1160), move jumper (379), cavity <1 ohm. Go to Locate open or poor
wire to cavity 3, circuit 97D 29, 97CD to next connection in circuit
and ground. At (379) cavity ground. step. 97CD or bulkhead
29, measure resistance of connector (190), then
circuit 97CD to ground. repair.
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Table 119 Accelerator (APS/IVS), Barometric Air Pressure (BAP) and Ambient Air Temperature Sensor
Systems (ATS) (cont.)
STEP KEY ACTION TEST SPEC. YES-IN NO-OUT OF SPEC.
POINTS SPEC.
14. Off Remove jumper and End test. Replace BAP sensor.
reconnect connectors. If problem persists,
BAP system circuits refer to Engine
check good? Is problem Diagnostic Manuals.
corrected?
15. Off Is a fault code present for Go to End test.
the ATS system? next
step.
16. Off Disconnect ATS connector (379), cavity <1 ohm. Go to Locate open or poor
(463). Install jumper wire 12, 97AX to next connection in circuit
from cavity B, circuit 97AX ground. step. 97AX, then repair.
to ground. Disconnect
CEC module connector
(379). At cavity 12,
measure resistance from
circuit 97AX to ground.
17. Off At (463), move jumper to (379), cavity <1 ohm. Go to Locate open or poor
cavity A, circuit 97BU and 11, 97BW to next connection in circuit
ground. At (379), cavity ground. step. 97BW/7BU, then
11, measure resistance of repair.
circuit 97BW to ground.
18. Off Remove jumper and End test. Replace ATS. If
reconnect connectors. problem persists,
ATS system circuits refer to Engine
check good? Is problem Diagnostic Manuals.
corrected?
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Table 120 Testing Diagnostic Connector Power and Ground Circuits (cont.)
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF
POINTS SPEC. SPEC.
2. On Re-install fuse F10D. (137), 97DL 12 ± 1.5 Go to next Locate cause of no
At connector (137), to ground. volts. step. or low voltage in
measure voltage from circuit 97DL, then
circuit 97DL to ground. repair.
3. On At connector (137), (137) 12 ± 1.5 Power Locate open or
measure voltage between between volts. and gnd. poor connection
circuit 97DL and circuit 97DL and circuits in circuit 11-GR
11-GR. 11-GR. to diag- or ground adapter
nostic (43), then repair.
conn.
(137)
check
good.
Table 121 Testing Diagnostic Connector and Speedometer/Tachometer Positive and Negative Data
Link Circuits
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF
POINTS SPEC. SPEC.
1, Off Disconnect CEC (137), 98(+) >100K Go to next Locate short to
module connector (379) to ground. ohms. step. ground, then repair.
from ECM and (421)
from speedometer unit.
If other devices are
connected at data link
connectors (514) and
(515), disconnect them.
At connector (137)
measure resistance
from terminal A, circuit
98(+) to ground.
2. Off At connector (137) (137), >100K Go to next Locate short to
measure resistance 98B(-) to ohms step. ground, then repair.
from terminal B, circuit ground.
98B(-) to ground.
3. Off At connector (137), (137) >100K Go to next Locate short circuit
measure resistance between ohms. step. between circuits
between terminal 98(+) and connected to
A, circuit 98(+) and 98B(-). terminal A 98(+),
terminal B, circuit 47/48(+) and
98B(-). terminal B 98B(-),
47/48(-), then repair.
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Table 121 Testing Diagnostic Connector and Speedometer/Tachometer Positive and Negative Data
Link Circuits (cont.)
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF
POINTS SPEC. SPEC.
4. Off At CEC module (137), 98(+) <5 Go to next Locate open or poor
connector (379), use to ground. ohms. step. connection in circuit
test lead to jumper 98(+) between
terminal 16, circuit connectors (514)
98A(+) to ground. and (137) or open
At connector (137) or poor connection
terminal A, circuit 98(+) in circuit 98A(+)
measure resistance to between connectors
ground. (514) and (379),
then repair.
5. Off With jumper still in (421), <5 Go to next Locate open or poor
place at terminal 16, 47/48(+) to ohms. step. connection in circuit
circuit 98A(+), measure ground. 47/48(+) between
resistance to ground connectors (421)
at circuit 47/48(+) and and (514), then
connector (421). repair.
6. Off At CEC module (137) <5 Go to next Locate open or poor
connector (379) use between ohms. step. connection in circuit
test lead to jumper 98(+) and 98B(-) between
terminal 16, circuit 98B(-). connectors (515)
98A(+) to terminal and (137), or open
17, circuit 98C(-). or poor connection
At connector (137) in circuit 98C(-)
measure resistance between connectors
between terminal (515) and (379),
A, circuit 98(+) and then repair.
terminal B, circuit
98B(-).
7. Off With jumper still in (421), <5 Locate open All data link circuits
place, at connector 47/48(-) to ohms. in circuit check good.
(421) measure ground. 47/48(-)
resistance between between
47/48(-) and ground. conn. (421)
and (515),
then repair.
Construct test leads using terminals 1680205C1, short length of 16 gauge wire and alligator clips.
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WARNING – A jack must never be used alone to support vehicle. The jack may lower and
serious injury could result. Always support vehicle with floor jacks. Always block wheels to prevent
vehicle from moving.
WARNING – EXTREME CAUTION should be used to prevent personal injury resulting from
contact with rotating vehicle wheels when connecting.
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NOTE – If the vehicle is equipped with an Allison transmission, this switch is replaced with a jumper
connection.
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The clutch switch should be mounted so that the switch actuator makes contact with the clutch pedal arm when
the arm is depressed 0.5 inch at the point of actuator contact. The bracket can be bent forward or backward for
adjustment. An audible click (switch closing) should be heard when the pedal is released.
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4. COMPONENT LOCATIONS
(B1) Battery Stud. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . . Power Distribution Panel
(94) Back-Up Light Switch. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . . . . . On Transmission
(137) 6–Way Data Link Connector. . . . . . . . . . . . . . . . . .. . . . . . Power Distribution Panel
(141) Service Brake Switch/Cruise Switch. . . . . . . . .. . . . . . Dash Panel, Left Side, Engine Side
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Table of Contents
1. DESCRIPTION. .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .409
1.1. AIR DRYER. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .409
1.2. TRUCK BODY CONNECTION. . . . .. . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . .409
1.3. TRAILER CONNECTION. . .. . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . . .. . . . . . . .409
1.4. FOUR WHEEL TRAILER CONNECTION. .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. . .. . . .. . . .. . .409
1.5. TWO SPEED AXLE WIRING. . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . .409
2. OPERATION.. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .410
2.1. AIR DRYER. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .410
2.2. TRUCK BODY CONNECTION. . . . .. . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . .410
2.3. TRAILER CONNECTION. . .. . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . . .. . . . . . . .410
Red Terminal - Stop Light. . . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .. . . . . .410
Yellow and Green Terminals - Turn And Hazard Lights. . . . .. . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . .410
Brown Terminal - Tail Light. .. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .410
Black Terminal - Marker Light . . .. . .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . ..411
Blue Terminal - Trailer ABS.. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. ..411
White Terminal - Trailer Socket Ground. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. .. . .. ..411
2.4. TRAILER CONNECTION FOUR WHEEL TRAILER — FRAME MOUNTED. . . . . . . . . . . . . . . . . . . . .411
Red Terminal — Stop Light.. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. ..411
Yellow and Green Terminals — Turn and Hazard Lights. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. .411
Brown Terminal — Tail Light. .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. .412
Black Terminal — Marker Light.. . .. .. .. . .. .. .. . .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. . .. .. .. . .. .. .. . .. .. .412
Blue Terminal — Trailer Auxiliary Power. . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .412
White Terminal —Trailer Socket Ground. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .412
Two Speed Axle Wiring. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .412
3. TROUBLESHOOTING. .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .412
3.1. AIR DRYER. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .413
3.2. TRUCK BODY CONNECTION. . . . .. . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . .414
Testing Marker Lights Power Feed. . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . .414
Testing Ground Circuit.. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. .415
3.3. TRAILER CONNECTION. . .. . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . . .. . . . . . . .416
Testing Stop Light Circuit. . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .416
Testing Turn and Hazard Circuits. .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .417
Testing Tail Light Circuit. .. .. . .. .. .. .. . .. .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. .. .. .418
Testing Marker Light Circuit. . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .. . . . . . . .418
Testing ABS Trailer Circuit. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .419
Testing Trailer Socket Ground Circuit.. .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. .420
3.4. TWO SPEED AXLE WIRING. . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . .421
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1. DESCRIPTION
1.1. AIR DRYER
The air dryer collects and removes moisture and contaminants from the vehicle’s compressed air system
before the moisture reaches the first air reservoir. The heater and thermoswitch assembly, located in the air
dryer, prevents freeze-up in the purge drain valve during cold weather operation.
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2. OPERATION
2.1. AIR DRYER
Turning the key switch on applies ignition power on circuit 13AH to energize the air dryer control relay (146).
With the relay energized, battery voltage on circuit 14AD, fuse F10–A and circuit 39A from battery adapter (B1)
passes through the relay normally open (N.O.) contacts (30 to 87). It then flows out the relay on circuit 39B,
through connector (1), and is applied to the air dryer assembly’s electrical pigtail.
The air dryer thermocouple closes at less than 50°F/10°C, applying battery power to the heater element
located in the air dryer assembly. The air dryer control relay ground circuit 13-GAD is grounded through ground
adapter (455), then through 11-GE to ground stud at left dash panel.
Terminal 1 of the truck body junction block is grounded through circuit 11-GM to trailer socket ground inside the
cab, 11-GN and 11-GI to ground stud at left dash panel.
Turning the headlights to park or on energizes the trailer marker lights relay. This delivers battery power from
(B2) stud through circuit 14H, 14E, fuse F3-A, circuit 58D, relay (463-R8), circuit 58R, and 58S to terminal 2 of
the truck body junction block.
When the tractor brakes are applied, the vehicle stop light switch supplies power through circuit 70A/70D to
energize the stop light relay (464)/R10. With the stop light relay energized, power from the (B1) battery stud,
circuit 14K/14F, fuse F7-D, and circuit 70E is sent through the normally open contacts of stop light relay on
circuit 70C, conn. (922), conn. (925), and circuit 70C to trailer socket conn. (112) at the red terminal.
In the LEFT TURN mode (or hazard switch on), power flows from (B1) battery stud through circuit 14K, 14R,
fuse F2-D, circuit 55, flasher, circuits 14BK, 55A and 16BK to turn signal switch. From the switch it flows
through circuit 56E to energize relay (464)/R11. With the left turn relay energized, power flows from (B1)
battery stud through circuits 14K, 14L, fuse F7-B, circuit 56H, through normally open contacts of left turn relay,
and circuit 56C conn. (923), conn. (926) and circuit 56D to the trailer socket (112) yellow terminal.
In the RIGHT TURN mode (or hazard switch on), power flows from (B1) battery stud through circuits 14K,
14R, fuse F2-D, circuit 55, flasher, circuits 14BK, 55A and 16BK to turn signal switch. From the switch it flows
through circuit 57E to energize relay (464)/R12. With the right turn relay energized, power flows from (B1)
battery stud through circuits 14K, 14L, fuse F7-C, circuit 57H, through normally open contacts of right turn
relay, and circuit 57C conn. (923), conn. (926) and circuit 57D to the trailer socket (112), green terminal.
Brown Terminal - Tail Light
When the headlight and trailer light switches are closed, power flows from (B2) battery stud through circuit
14W, 14B, fuse F8-A, and circuit 50 to headlight switch (465). It then flows out of the switch through circuit
58E, cab and trailer lights switch (466), and circuit 58P to energize tail light relay (464)/R9. When relay
energizes, power flows from (B2) battery stud through circuits 14W, 14B, fuse F3-C, and circuit 68 to tail light
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relay. Power then flows through relay normally open contacts, circuit 68E, circuit 68B, conn. (922), conn.
(925), and circuit 68A to the brown terminal of trailer socket (112).
NOTE – The cab trailer lights switch is a momentarily open interrupt switch.
Depressing the switch will interrupt the power to the trailer socket brown terminal.
When the headlight and trailer light switches are closed, power flows from (B2) battery stud through circuits
14W, 14B, fuse F3–D, and circuit 50 to headlight switch (465). It then flows out of the switch through circuit
58E, cab and trailer lights switch (466), and circuit 58C to energize trailer marker lights relay (463-R8). When
the relay energizes, power flows from (B2) battery stud through circuits 14W, 14E, fuse F3-A, circuit 58D, relay
(463-R8), circuits 58R, 58S , conn. (923), conn. (926) and circuit 58A to the trailer socket black terminal.
With ignition key on power flows from (B1) through circuit 14CP, fuse F10–A, circuit 94AH, ABS trailer relay
(470), circuit 94AF to the trailer socket (112) blue terminal.
The white terminal of (112) is grounded through circuit 11–GAL to sleeper ground, and circuits 11–GN and
11–GI to ground stud at left dash panel.
With Pro Sleeper, the white terminal of (112) is grounded through circuit 11–GAL to trailer socket ground inside
sleeper, circuit 11–GN to the sleeper ground, through circuit 11–GAN to the trailer socket ground inside the
cab, and circuits 11–GN and 11–GI to ground stud at left dash panel.
When the tractor brakes are applied, the vehicle stop light switch supplies power through circuit 70A/70D to
energize the stop light relay (464)/R10. With the stop light relay energized, power from the (B1) battery stud,
circuit 14K/14F, fuse F7–D, and circuit 70E is sent through the normally open contacts of stop light relay on
circuit 70C, connector (922), conn. (925), conn. (318), conn. (113) and circuit 70C to trailer socket connector
(112) at the red terminal.
In the LEFT TURN mode (or hazard switch on), power flows from (B1) battery stud through circuits 14K,
14R, fuse F2–D, circuit 55, flasher, circuits 14BK, 55A and 16BK to turn signal switch. From the switch it
flows through circuit 56E to energize relay (464)/R11. With the left turn relay energized, power flows from
(B1) battery stud through circuits 14K, 14L, fuse F7–B, circuit 56H, through normally open contacts of left
turn relay, circuit 56C, conn. (923), conn. (926), conn. (316), conn. (113) and circuit 56C to the trailer socket
(112), yellow terminal.
In the RIGHT TURN mode (or hazard switch on), power flows from (B1) battery stud through circuits 14K,
14R, fuse F2–D, circuit 55, flasher, circuits 14BK, 55A and 16BK to turn signal switch. From the switch it
flows through circuit 57E to energize relay (464)/R12. With the right turn relay energized, power flows from
(B1) battery stud through circuits 14K, 14L, fuse F7–C, circuit 57H, through normally open contacts of right
turn relay, circuit 57C, connector (923), conn. (926), conn. (316), conn. (113) and circuit 57C to the trailer
socket (112), green terminal.
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When the headlight and trailer light switches are closed, power flows from (B2) battery stud through circuits
14H, 14D, fuse F8–A and circuit 50 to headlight switch (465). It then flows out of the switch through circuit
58E, cab and trailer lights switch (466) and circuit 58P to energize tail light relay (464)/R9. When the relay
energizes, power flows from (B2) battery stud through circuit 14W, 14B, fuse F3–C and circuit 68 to tail light
relay. Power then flows through relay normally open contacts, circuit 68E, circuit 68B, connector (922), conn.
(925), conn. (316), conn. (113) and circuit 68B to the brown terminal of trailer socket (112).
NOTE – The cab trailer lights switch is a momentarily open interrupter switch.
Depressing the switch will interrupt the power to the trailer socket brown terminal.
When the headlight and trailer light switches are closed, power flows from (B2) battery stud through circuits
14W, 14B, fuse F3–D and circuit 50 to headlight switch (465). It then flows out of the switch through circuit
58E, cab and trailer marker lights switch (466), and circuit 58C to energize trailer maker lights relay (463–R8).
When the relay energizes, power flows from (B2) battery stud through circuits 14W, 14E, fuse F3–A, circuit
58D, relay (463–R8), circuits 58S, connector (923), conn. (926), conn. (316), conn. (113) and circuit 58R to
the trailer socket black terminal.
With ignition key on, power flows from (B1) through circuit 14CP, fuse F10–A, circuit 94AH, ABS trailer relay
(470), circuit 94AF, connector (922), conn. (925), conn. (318), conn. (113) and circuit 94AF to the trailer
socket (112) blue terminal.
With frame mounted connector for four wheel trailer, the white terminal of (112) is grounded through circuit
11–GN to junction block ground.
With ignition key on, power flows from (B1) battery stud through circuits 14K, 14R, fuse F2–C, circuit 14S,
ignition relay (462)/R1, and circuit 13P to ignition adapter 12 (495). Then power flows through circuit 93, two
speed axle switch (417), circuits 93A and 93B to the speedometer/tachometer module connector (421). When
the axle is shifted into high range, air is supplied to the axle shift circuit opening the two speed axle switch
and changing the voltage signal to 0 at the speedometer/tachometer module. Thus speed and mileage
are calculated for the different axle ratio.
3. TROUBLESHOOTING
A. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of
charge (SOC) or higher. This represents an open circuit voltage (OCV) of 12.4 volts. Batteries
with an OCV of 12 volts or less are either completely discharged or have a dead cell.
B. Before beginning these test procedures, check any light or indicator lamp filaments that are
suspected of being open (burned out). This is done to avoid unnecessary extensive circuit checks.
C. Before beginning these test procedures, inspect all connectors for loose or damaged pins,
wires, etc. Refer to TEST EQUIPMENT AND CONNECTOR REPAIR section in GROUP 08 —
ELECTRICAL in the CTS-5000 Master Service Manual.
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D. When the technician determines that a fuse is blown, while checking its condition, he is directed
to locate the cause of the overload condition and to repair it. While no further instruction on this
procedure is listed in the diagnostic tables, the common procedure is as follows: isolate sections
of the circuit, by disconnecting connectors, and measure the resistance to ground to find the circuit
that is shorted to ground. Then locate the damaged spot in the wire or connector and repair.
E. Diagnostics for circuits that are malfunctioning by sticking in the position are generally not covered
in detail. It is assumed that the mechanic knows to check for a malfunctioning switch, relay, or
solenoid.
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4. COMPONENT LOCATIONS
J7 Junction Point. . . . . . . . . . . . . . .. . . . . . . . . . . . . . .. . . . . . . .. . . . . . In Dash Panel Left Side
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Figure 133 Trailer Connection With Trailer Cable Wired Directly to Cab Harness
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Figure 134 Trailer Connection With Four Wheel Trailer N/Sleeper Box
1. TRAILER SOCKET WIRING
2. TRAILER IN-LINE CONNECTOR (316)
3. TRAILER IN-LINE CONNECTOR (318)
4. HARNESS ASSEMBLY
5. CONNECTORS (922) & (923)
6. MAIN CAB HARNESS
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Table of Contents
1. DESCRIPTION. .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .435
1.1. BACK-UP LIGHTS. .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. .435
1.2. CAB AND TRAILER LIGHTS SWITCH. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .435
1.3. CAB CLEARANCE AND IDENTIFICATION LIGHTS. .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .435
1.4. CAB DOME, READING, AND COURTESY LIGHTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .435
1.5. DAYTIME RUNNING LIGHTS (DRL) MODULE WIRING-STANDARD USA AND CANADA. . .435
1.6. FOG LIGHTS.. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .435
1.7. HEADLIGHT SWITCH AND DIMMER SWITCH WIRING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .435
1.8. HEADLIGHTS .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .435
1.9. PANEL LIGHTS. . . .. . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .436
1.10. PARK/TURN/MARKER LIGHTS.. . .. .. . .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. .436
1.11. SPOTLIGHT. .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .436
1.12. STOP, TAIL, TURN AND HAZARD SIGNAL LIGHTS WITH FLASHER. . . . . . . . . . . . . . . . . . . . . . . . .436
1.13. WORK LIGHT WITHOUT SLEEPER.. .. . .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .436
1.14. WORK LIGHT WITH PRO SLEEPER. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .436
2. OPERATION.. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .436
2.1. BACK-UP LIGHTS. .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. .436
2.2. CAB AND TRAILER LIGHTS SWITCH AND RELAYS WIRING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .436
2.3. CAB CLEARANCE AND IDENTIFICATION LIGHTS. .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .437
2.4. CAB DOME, READING, AND COURTESY LIGHTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .437
2.5. DAYTIME RUNNING LIGHTS (DRL) MODULE WIRING-STANDARD USA AND CANADA. . .437
2.6. FOG LIGHTS.. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .438
2.7. HEADLIGHT SWITCH AND DIMMER SWITCH WIRING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .438
2.8. HEADLIGHTS .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .438
2.9. PANEL LIGHTS. . . .. . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .439
2.10. PARK/TURN/MARKER LIGHTS . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .439
2.11. SPOTLIGHT. .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .440
2.12. STOP, TAIL, TURN AND HAZARD SIGNAL LIGHTS WITH FLASHER. . . . . . . . . . . . . . . . . . . . . . . . .440
2.13. WORK LIGHT WITHOUT SLEEPER.. .. . .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .440
2.14. WORK LIGHT WITH PRO SLEEPER. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .441
3. TROUBLESHOOTING. .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .441
3.1. BACK-UP LIGHTS. .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . .. .441
3.2. CAB AND TRAILER LIGHTS SWITCH AND RELAYS WIRING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .442
3.3. CAB CLEARANCE AND IDENTIFICATION LIGHTS. .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .445
3.4. CAB DOME, READING, AND COURTESY LIGHTS. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .447
3.5. DAYTIME RUNNING LIGHTS (DRL) MODULE WIRING- STANDARD USA AND CANADA.. .453
3.6. FOG LIGHTS.. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .456
3.7. HEADLIGHT SWITCH AND DIMMER SWITCH WIRING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .458
3.8. HEADLIGHTS. .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .462
3.9. PANEL LIGHTS. . . .. . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . .. . . .. . . .464
3.10. PARK/TURN/MARKER LIGHTS . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . .467
3.11. SPOTLIGHT. .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .470
3.12. STOP, TAIL, TURN AND HAZARD SIGNAL LIGHTS WITH FLASHER. . . . . . . . . . . . . . . . . . . . . . . . .471
3.13. WORK LIGHT WITHOUT SLEEPER.. .. . .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .477
3.14. WORK LIGHT WITH PRO SLEEPER. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .479
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1. DESCRIPTION
1.1. BACK-UP LIGHTS
The vehicle back-up lights are a set of lamps that come on when the vehicle transmission is shifted into reverse.
NOTE – Fog lights will only function if headlight switch is in the on position, dimmer switch is in low
position, and the fog light switch is in the on position.
1.8. HEADLIGHTS
The 5000i, 9100i, 9200i, 9400i, and 9900i model trucks use a two headlamp system. Each lamp contains a low
beam element and a high beam element.
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1.11. SPOTLIGHT
The spotlight circuit provides power for two spotlights. The switches for these spotlights are built into the lights.
1.12. STOP, TAIL, TURN AND HAZARD SIGNAL LIGHTS WITH FLASHER
This set of circuits contains the turn signal switch, stop light switch, flasher unit (turn signal/hazard), right and
left turn relays, stop light relay, and right and left stop, turn, and tail light assemblies for the rear of the vehicle.
The turn indicators located in the instrument cluster are also included.
2. OPERATION
Refer to the LIGHT SYSTEMS circuit diagrams in CTS-5298 or S08225.
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coil and ground circuit 58-G. This allows power to flow through circuits 14H, 14B, fuse F3-C, circuit 68,
through cab and trailer tail lights relay, and through circuit 68E. From this point it flows through circuit 68B
to the trailer socket. It also flows through circuit 68D, fuse F8-C, and circuit 68C to supply mirror lights, tail
lights, clearance lights, panel lights, and park lights.
The dome light switch is illuminated by circuits 62A, 62S, 62AP, and 63F coming from the panel light switch.
The ground circuit is 62-GF, 11-GAB and 11-GB to right dash panel ground stud. When the dome light switch is
set to on, power flows from (B2) battery stud through circuits 14AG, 14T, fuse F2-B, and circuit 63. From this
point power flows to left courtesy light through circuit 63V, or right courtesy light through circuits 63X and 63V,
or right dome light through circuits 63Z, 63, and 63S, or left dome light through circuits 63Z, 63, and 63M.
The ground path for the left courtesy light is circuits 63H, 63A, dome light switch, circuits 63-GD, 11-GAB, and
11-GB to right dash ground stud. The ground path for the right courtesy light is circuits 63H, 63Y, 63A, dome
light switch, circuits 63-GD, 11-GAB, and 11-GB to right dash ground stud.
The ground path for the right dome light is circuits 63Y, 63A, dome light switch, circuits 63-GD, 11-GAB, and
11-GB to right dash ground stud. The ground path for the left dome light is circuit 63N, dome light switch,
circuits 63-GD, 11-GAB, and 11-GB to right dash ground stud. If the dome light switch is set to automatic
operation, the ground path for all the courtesy and dome lights becomes circuit 63B, and circuit 63C to ground
when a door is opened.
When the park brake is released, the DRL park brake switch opens and the voltage that the DRL module
senses at connector (513) terminal E goes to 12 ± 1.5V. This tells the module to power the low beam elements
of the headlights at 50% of normal low beam brightness, which is 75% to 84% of battery voltage. When the
headlight switch is turned on, the brightness will go to 100%.
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438 12 LIGHT SYSTEMS
The fog light switch (440) is used to enable the fog light system by energizing the fog light relay (148). The
switch receives power from the dimmer switch (only in low beam position) or Daytime Running Lights module,
on circuit 64C. Closing the switch applies power through circuit 64A to the control coil of the fog light relay,
which energizes the relay.
Accessory power from A3 flows through circuit 12P, fuse F10-A, and circuit 64 to fog light relay (148). With the
fog light relay energized, power flows through the relay, and circuit 64B to circuits 64C and 64D delivering
power to the fog lights.
If the headlight switch is placed in on (ignition) position, power is available from (B2) battery stud, through
circuit 14H, 14B, fuse F3-D, and circuit 50A to the headlights switch (465). If the headlight switch is on,
current will flow through the switch and circuit 50B to energize the headlight relay (462-R4). Circuits 50-GB
and 11-G complete the ground circuit.
With the headlight relay energized, current flows from (B2) battery stud, through circuits 14H, 14D, fuse F8-B,
circuit 51, headlight relay (462-R4), and circuit 51A, to dimmer switch (42). With the dimmer switch in the
low position, current will flow through circuit 53B to a splice. From the splice power will flow through circuit
53D to the left headlight and 53C to the right headlight. Then the current will flow through circuits 52–GE,
52–GF, and 11–GF to ground stud at left dash panel. With the dimmer switch in the high position, current will
flow through circuit 52F to a splice. From the splice power will flow through circuit 52D to the left headlight
and 52E to the right headlight. Then the current will flow through circuits 52–GE, 52–GF, and 11– GF to
ground stud at left dash panel.
With the standard USA and Canadian DRL system, with the headlight switch off, power flows from the DRL
module through circuits 66B, 64C, and 53B to a splice. From the splice power will flow through circuit 53D to
the left headlight and 53C to the right headlight. Then the current will flow through circuits 52–GE, 52–GF, and
11–GF to the ground stud at the left dash panel.
2.8. HEADLIGHTS
These models utilize a two headlight system, one on each side. The lamps receive power in the low beam
mode on circuit 53B with the power split up on 53C for the right lamp and 53D for the left lamp. The lamps
receive power in the high beam mode from circuit 52F, with power split up on 52E for the right lamp and 52D
for the left lamp.
Circuits 52–GE, 52–GF, and 11–GF provide the ground path for the left headlight to left dash panel ground
stud. Circuits 52–GA and 64–GC provide the ground path for the right headlight to J7 cab ground.
Circuits 52–GD, 52–GB, and 52–GA provide the ground path for the left headlights to J7 cab ground. Circuits
52–GH, 52–GF, 52–GE, 52–GF, and 11–GF provide the ground path for the right headlights.
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12 LIGHT SYSTEMS 439
From the panel light switch power flows through circuits 62A, 62S, 62M, panel lights feed adapter (503), and
circuit 62AQ to the analog clock lamp. The ground path is circuit 62-GAQ and 11-GAV to ground adapter (454).
From the panel light switch power flows through circuits 62A, 62S, 62M, panel lights feed adapter (503), and
circuit 62AB to the air restriction gauge lamp. The ground path is circuit 62-GAB to ground adapter (506).
From the panel light switch power flows through circuits 62A and 62D to the speedo/tach module panel lights
and through circuits 62-GD and 11-GF to ground stud at left dash panel.
From the panel light switch power flows through circuits 62A and 62C to the left gauge cluster panel lights and
through circuits 62-GC and 11-GF to ground stud at left dash panel.
From the panel light switch power flows through circuits 62A and 62B to the right gauge cluster panel lights
and through circuits 62-GB and 11-GF to ground stud at left dash panel.
From the panel light switch power flows through circuits 62A and 62T to the cigar lighter light and directly
to ground.
From the panel light switch power flows through circuits 62A, 62S, and 62P to the heater control (105) light and
through circuits 62-GP and 11-G to ground stud at right dash panel.
From the panel light switch power flows through circuits 62A, 62S, and 62P to the heater control (105) light and
through circuits 62–GP and 11–G to ground stud at right dash panel.
The turn signal switch provides power on circuit 56D to the left side turn light element and circuit 56 to the
left/park/turn/marker light high element.
The turn signal switch provides power on circuit 57D to the right side turn light element and circuit 57 to the
right/park/turn/marker light high element.
The ground path for the park/turn/marker lights was mentioned above. The ground path for the left side turn
light is circuit 56-GA and 11-GD to ground stud at left dash panel. The ground path for the right side turn light is
circuit 57-GA, and 11-GB to ground stud at right dash panel.
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440 12 LIGHT SYSTEMS
2.11. SPOTLIGHT
(B2) battery stud supplies power through circuits 14H, 14Y, fuse F1-D, circuits 63P, and 64E. The power is
available at this point to circuit 64H and the left spotlight and switch assembly, or circuit 64F and the right
spotlight and switch assembly. The lights are grounded through their mounting brackets.
2.12. STOP, TAIL, TURN AND HAZARD SIGNAL LIGHTS WITH FLASHER
When the brakes are applied, stoplight switch (640) closes and power flows from (B2) battery stud through
circuits 14H and 14E to fuse F3-B. From the fuse, power flows through circuit 70, stoplight switch, and circuit
70A, to turn signal switch and circuit 70D to stoplight relay (464)/R10.
This energizes the stoplight relay through ground path circuits 70-G, 56-G, 57-G, and 11-G to ground stud at
right dash panel. This allows power to flow from (B1) battery stud through circuits 14K, and 14F to fuse F7-D.
From the fuse, power flows through circuit 70E, stoplight relay (464)/R10 and circuit 70C to the trailer socket.
From the turn signal switch power flows through circuit 56B to bright element of the left rear stop, tail, and turn
light, and the four wheel trailer connection. Power also flows from the turn signal switch on circuit 57B to bright
element of the right rear stop, tail, and turn light, and the four wheel trailer connection. Circuit 11-GV is the
ground path for the left and right rear stop, tail, and turn light.
When the turn signal switch is moved to the left turn position, power flows from (B1) battery stud through
circuits 14K, 14R, fuse F2-D, and circuit 55 to the flasher unit. From the flasher unit power flows through
circuit 55A, and the turn signal switch.
From the turn signal switch power flows through circuit 56D to the left side turn light, and 56E to the left
turn relay (464)/R11. The left turn relay is energized through ground path circuits 56-G, 57-G, and 11-G to
ground stud at right dash panel. Power also flows from the turn signal switch through circuit 56B to the four
wheel trailer connection and the bright element of the left rear stop, tail, and turn light. Circuit 11-GV is the
ground path for the left rear stop, tail, and turn light.
With the left turn relay energized, power flows from (B1) battery stud through circuits 14K, 14L, fuse F7-B, and
circuit 56H to the left turn relay. Power then flows through circuit 56C to the trailer socket, and circuits 56A and
56R to the left turn indicator. The ground path is circuit 62-GD and 11-GF to ground stud left dash panel.
When the turn signal switch is moved to the right turn position, power flows from the turn signal switch, through
circuit 57D to the right side turn light, and circuit 57E to the right turn relay (464)/R12. The right turn relay is
energized through ground path circuits 57-G, and 11-G to ground stud at right dash panel. Power also flows
from the turn signal switch through circuit 57B to the four wheel trailer connection and the bright element of
the right rear stop, tail, and turn light. Circuits 11-GV and 11–GV make up the ground path for the right
rear stop, tail, and turn light.
With the right turn relay energized power flows from (B1) battery stud through circuits 14K, 14L, fuse F7-C, and
circuit 57H to the right turn relay. Power then flows through circuit 57C to the trailer socket, and circuits 57A
and 57R to the right turn indicator. The ground path is circuits 62-GD and 11-GF to ground stud left dash panel.
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3. TROUBLESHOOTING
Refer to the LIGHT SYSTEMS circuit diagrams in CTS-5298 or S08225.
A. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of
charge (SOC) or higher. This represents an open circuit voltage (OCV) of 12.4 volts. Batteries
with an OCV of 12 volts or less are either completely discharged or have a dead cell.
B. Before beginning these test procedures, check any light or indicator lamp filaments that are
suspected of being open (burned out). This is done to avoid unnecessary extensive circuit checks.
C. Before beginning these test procedures, inspect all connectors for loose or damaged pins,
wires, etc. Refer to TEST EQUIPMENT AND CONNECTOR REPAIR section in GROUP 08 —
ELECTRICAL in the CTS-5000 Master Service Manual.
D. When the technician determines that a fuse is blown, while checking its condition, he is directed
to locate the cause of the overload condition and to repair it. While no further instruction on this
procedure is listed in the diagnostic tables, the common procedure is as follows: isolate sections
of the circuit by disconnecting connectors, and measure the resistance to ground to find the circuit
that is shorted to ground. Then locate the damaged spot in the wire or connector and repair.
E. Diagnostics for circuits that are malfunctioning by sticking in the on position are generally not
covered in detail. It is assumed that the technician knows to check for a malfunctioning switch,
relay, or solenoid.
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12 LIGHT SYSTEMS 443
Table 141 Cab and Trailer Lights Switch and Relays Wiring (cont.)
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF
POINTS SPEC. SPEC.
5. Off With headlight switch (466), 62AR 11 ± 1.5 Go to next Locate cause of
on and panel light to gnd. volts. step. low or no voltage in
switch adjusted for full circuit 62A, 62AS,
brightness, at connector or 62AR from panel
(466) measure voltage to light switch, then
ground at circuit 62AR. repair.
6. Off At conn. (466) with (466), 62AR 11 ± 1.5 Go to next Locate open or
headlight switch on to 62- GAR. volts. step. poor connection
and panel light switch in ground circuit
adjusted for full 62-GAR, 11-GK,
brightness, measure or 11-GD going to
voltage from circuit 62AR ground stud at left
to 62-GAR. dash panel, then
repair.
7. Off Reconnect conn. (466), (464-R9), 12 ± 1.5 Go to next Locate cause of
and remove cab and 58P to gnd. volts. step. low or no voltage
trailer tail lights relay in circuit 58P, then
(464-R9). With the cab repair.
and trailer lights switch in
the on position, measure
voltage at relay socket
(464-R9) circuit 58P to
ground.
8. Off Measure voltage at relay (464-R9), 12 ± 1.5 Go to next Locate open or poor
socket (464-R9) circuit 58P to 58-G. volts. step. conn. in circuits
58P to 58-G. 58-G, 70-G, 58-G,
57-G, and 11-G to
ground stud at right
dash panel, then
repair. Re-install
relay.
9. Off Check fuse F3-C. F3-C. <1 ohm. Go to next Locate cause of
step. overload condition,
then repair. Replace
fuse.
10. Off Replace fuse F3-C. At F3-C, 14B to 12 ±1.5 Go to next Locate cause of
F3-C measure voltage gnd. volts. step. low or no voltage in
from circuit 14B to ground. circuit 14H or 14B,
then repair.
11. Off Measure voltage at relay (464-R9), 68 12 ±1.5 Go to next Locate cause of
socket (464-R9) circuit 68 to 58-G. volts. step. low or no voltage
to 58-G. in circuit 68, then
repair. Re-install
relay.
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444 12 LIGHT SYSTEMS
Table 141 Cab and Trailer Lights Switch and Relays Wiring (cont.)
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF
POINTS SPEC. SPEC.
12. Off At relay socket (464-R9) Go to next
with test lead jumper step.
connect circuit 68 to 68E.
13. Off Remove and check fuse F8-C <1 ohm. Go to next Locate cause of
F8-C. step. overload condition,
then repair. Replace
fuse.
14. Off Re-install fuse F8-C. F8-C, 68D to 12 ±1.5 Go to next Locate cause of
At fuse F8-C measure gnd. volts. step. low or no voltage
voltage from circuit 68D in circuit 68E or
to ground. 68D, then repair.
Re-install relay.
15. Off Remove test jumper, F8-C, to gnd. 12 ±1.5 Go to next Replace cab and
and re-install cab and volts. step. trailer tail lights
trailer tail lights relay. relay.
Turn headlight switch on
and cab and trailer lights
switch on. At fuse F8-C
measure voltage from
circuit 68D to ground.
16. Off With headlight switch Trailer 12 ±1.5 Go to next Locate cause of
and cab and trailer socket, 68B volts. step. low or no voltage
lights switch still on, at to gnd. in circuit 68B, then
trailer socket measure repair.
voltage from circuit 68B
to ground.
17. Off Park, panel, clearance, Go to next
and mirror lights, and step.
trailer tail lights power
feed circuit checks good.
18. Off Remove trailer marker (463-R8), 12 ±1.5 Go to next Locate cause of
lights relay from socket 58C to gnd. volts. step. low or no voltage in
(463-R8). With headlight circuit 58C or jumper
switch and cab and trailer between 58C and
lights switch still on, 58P, then repair.
measure voltage from
circuit 58C to ground.
19. Off With headlight switch (463-R8), 12 ±1.5 Go to next Locate cause of
and cab and trailer lights 58C to volts. step. low or no voltage
switch still on, measure 58-GA. in circuit 58-GA or
voltage from circuit 58C 11-G, then repair.
to 58-GA.
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12 LIGHT SYSTEMS 445
Table 141 Cab and Trailer Lights Switch and Relays Wiring (cont.)
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF
POINTS SPEC. SPEC.
20. Off Remove and check fuse F3-A. <1 ohm. Go to next Locate cause of
F3-A. step. overload condition,
then repair. Replace
fuse.
21. Off Re-install fuse F3-A. F3-A, 14E to 12 ±1.5 Go to next Locate cause of
At fuse F3-A measure gnd. volts. step. low or no voltage in
voltage from circuit 14E circuits 14H or 14E,
to ground. then repair.
22. Off At (463-R8) measure (463-R8), 12 ±1.5 Go to next Locate cause of
voltage from circuit 58D 58D to gnd. volts. step. low or no voltage
to ground. in circuit 58D, then
repair.
23. Off At (463-R8) use test lead Trailer 12 ±1.5 Go to next Locate cause of
to jumper circuit 58D to socket, 58S volts. step. low or no voltage in
58R. At trailer socket to gnd. circuit 58R or 58S,
measure voltage from then repair.
circuit 58S to gnd.
24. Off Remove test jumper Trailer 12 ±1.5 Trailer Replace defective
and re-install trailer socket, 58S volts. marker trailer marker lights
marker lights relay. With to gnd. lights relay.
headlights and cab and circuits
trailer lights switched on, check
at trailer socket measure good.
voltage from circuit 58S
to gnd.
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3.5. DAYTIME RUNNING LIGHTS (DRL) MODULE WIRING- STANDARD USA AND
CANADA
Table 144 Daytime Running Lights (DRL) Module Wiring-Standard USA and Canada
STEP KEY ACTION TEST SPEC. YES NO - OUT OF SPEC.
POINTS - IN
SPEC.
1. Off Remove fuse F10-B and F10-B. <1 ohm. Go to Locate cause of
check for open condition. next overload condition,
step. then repair. Replace
fuse.
2. Off Re-install fuse F10-B. At F10-B, 14BL 12 ±1.5 Go to Locate cause of low
F10-B measure voltage to gnd. volts. next or no voltage in circuit
from circuit 14BL to step. 14BL to (B1) battery
ground. adapter, then repair.
3. Off Remove connector (513) (513), 66A to 12 ±1.5 Go to Locate cause of low
from DRL module, and gnd. volts next or no voltage in circuit
measure voltage from step. 66A, then repair.
circuit 66A to ground.
4. Off Check fuse F10-A for F10-A. <1 ohm. Go to Locate cause of
open condition. next overload condition,
step. then repair. Replace
fuse.
5. Off Turn ignition key on F10-A, 13BL 12 ±1.5 Go to Locate cause of low
and at F10-A measure to gnd. volts. next or no voltage in circuit
voltage from circuit 13BL step. 13BL from I2 ignition
to ground. adapter, then repair.
6. Off Measure voltage from (513), 66D to 12 ±1.5 Go to Locate cause of low
circuit 66D to ground. gnd. volts. next or no voltage in circuit
step. 66D, then repair.
7. Off Remove connector (468) (468), 44-GB <1 ohm. Go to Locate open or poor
from DRL park brake to gnd. next connection in circuit
switch and measure step. 44-GB or 66-G, then
resistance from circuit repair.
44-GB to ground.
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454 12 LIGHT SYSTEMS
Table 144 Daytime Running Lights (DRL) Module Wiring-Standard USA and Canada (cont.)
STEP KEY ACTION TEST SPEC. YES NO - OUT OF SPEC.
POINTS - IN
SPEC.
8. Off With park brake applied, Across DRL <1 ohm. Go to Replace defective
measure resistance park brake next DRL park brake
across DRL park brake switch. step. switch.
switch.
9. Off Chock vehicle wheels Across DRL >100K Go to Re-apply park brake.
and release park brake. park brake ohms. next Replace defective
Measure resistance switch. step. DRL park brake
across DRL park brake switch.
switch.
10. Off/On Reconnect (513). When Go to Go to next step.
ign. key is moved/held Step 17.
to start position, does
park brake indicator
illuminate?
11. Off Check fuse F4-A for open F4-A. <1 ohm. Go to Locate cause of
condition. next overload condition,
step. then repair. Replace
fuse.
12. Off At F4-A measure voltage F4-A, 13B 12 ±1.5 Go to Locate cause of
from circuit 13B to to gnd. volts next low or no voltage in
ground. step. circuit 13 or 13B from
ignition key switch,
then repair.
13. Off/On Remove conn. (420) (420), 28C to 12 ±1.5 Go to Locate cause of low
With key in on (ign.) gnd. volts. next or no voltage in circuit
position at conn. (420) step. 13V or 28C to ign. key
measure voltage from switch, then repair.
circuit 28C to ground.
14. Off Check filament of park Go to Replace lamp, and
brake lamp for open next reconnect (420).
condition. Lamp OK? step.
15. Off With park brake applied, (420), 44 to < 1 ohm. Go to Locate open or poor
at connector (420) gnd. next connection in circuit
measure resistance from step. 44, 44A or 44B to DRL
circuit 44 to ground. park brake switch and
circuits checked in
steps above, then
repair.
16. Off/On Reconnect conn. (420), Go to Replace defective
move key to start (crank) next ignition key switch.
position. Does lamp step.
illuminate?
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12 LIGHT SYSTEMS 455
Table 144 Daytime Running Lights (DRL) Module Wiring-Standard USA and Canada (cont.)
STEP KEY ACTION TEST SPEC. YES NO - OUT OF SPEC.
POINTS - IN
SPEC.
17. Off Park brake lamp circuits Go to
check good. next
step.
18. Off Remove connector (513) (513), 66-GA <1 ohm. Go to Locate open or poor
from DRL module. to gnd. next connection in circuit
At (513) measure step. 66-GA, then repair.
resistance from circuit
66-GA to ground.
19. Off With park brake applied, (513), 66-E to <1 ohm. Go to Locate open or poor
at (513) measure gnd. next connection in circuit
resistance from circuit step. 66-E, then repair.
66-E to ground.
20. Off Remove connector (440) (440), 64C to <1 ohm. Recon- Locate open or poor
from fog light switch, and (513) 64D. nect connection in circuit
measure resistance from (440). 64C or 64D, then
circuit 64C at (440) to Go to repair.
circuit 64D at connector next
(513). step.
21. Off Move headlight switch (513), 66B to 12 ±1.5 Go to Locate cause of low
to on and dimmer switch gnd. volts. next or no voltage in circuit
to low beam position. At step. 64C or 66B, then
(513) and circuit 66B, repair.
measure voltage to
ground.
22. Off With headlight switch on (513), 66F to 12 ±1.5 Go to Locate open or poor
and dimmer switch in gnd. volts. next connection in circuit
high position, measure step. 66F, then repair.
voltage at connector
(513) circuit 66F to
ground.
23. Off Daytime running light
circuits check good. If
system does not operate
properly, replace DRL
module. Reconnect
connectors (468) and
(513).
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3.8. HEADLIGHTS
Table 147 Headlights
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF SPEC.
POINTS SPEC.
1. Off With headlight switch off, (1), 52F 12 ±1.5 Go to next Locate cause of low
disconnect conn. (1). Then to gnd. volts. step. or no voltage in circuit
turn headlight switch on 52F, then repair.
and place dimmer switch in
high beam position, and at
(1) measure voltage from
circuit 52F to ground.
2. Off With headlight switch on (1), 53B 12 ±1.5 Go to next Locate cause of low
and dimmer switch in to gnd. volts. step. or no voltage in circuit
low beam position. At 53B, then repair.
(1) measure voltage from
circuit 53B to gnd.
3. Off With headlight switch off (1), <1 ohm. Switch Locate open or poor
at (1) measure resistance 52-GE to circuits connection in circuit
from circuit 52-GE to gnd. check 52-GE, 52-GF, or
ground. good. Go 11-GF to ground stud
to next at left dash panel,
step. then repair.
4. Off Turn off headlight switch. (296), 12 ±1.5 Go to next Locate cause of low
Reconnect connector (1), 53D to volts. step. or no voltage in circuit
and disconnect connector gnd. 53B or 53D, then
(296). Turn headlight repair.
switch on and place
dimmer switch in low beam
position. Measure voltage
at (296) from circuit 53D to
gnd.
5. Off With headlight switch still (296), 12 ±1.5 Go to next Locate cause of low
on, place dimmer switch 52D to volts. step. or no voltage in circuit
in high beam position. gnd. 52F or 52D, then
Measure voltage at (296) repair.
from circuit 52D to gnd.
6. Off With headlight switch still (296), 12 ± 1.5 Go to next Locate open or poor
on and dimmer sw. in high 52D to volts. step. conn. in circuit
beam position, measure 52-GE. 52-GE, then repair.
voltage at (296) from circuit
52D to 52-GE.
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3.11. SPOTLIGHT
Table 150 Spotlight
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF SPEC.
POINTS SPEC.
1. Off Remove fuse F1-D and F1-D. <1 ohm. Go to Locate cause of
check for open condition. next overload condition
step. and replace fuse.
2. Off At F1-D measure voltage F1-D, 14Y 12±1.5 Go to Locate cause of low
from circuit 14Y to ground. to gnd. volts. next or no voltage in circuit
step. 14H or 14Y from
battery stud (B2), then
repair.
3. Off With fuse re-installed, (428), 63P 12±1.5 Go to Locate cause of low
disconnect connector to gnd. volts. next or no voltage in circuit
(428), and at circuit 63P step. 63P, then repair.
measure voltage to ground.
4. Off Reconnect connector (428) 64H to gnd. 12±1.5 Go to Locate cause of low
and disconnect left spot volts. next or no voltage in circuit
light at circuit 64H. At 64H step. 64P, 64E or 63H then
measure voltage to ground. repair.
5. Off Repair or replace left Go to
spotlight and switch next
assembly. step.
6. Off Disconnect right spot 64F to gnd. 12±1.5 Go to Locate cause of low
light at circuit 64F. At 64F volts. next or no voltage in circuit
measure voltage to ground. step. 63P, 64E, or 63F then
repair.
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3.12. STOP, TAIL, TURN AND HAZARD SIGNAL LIGHTS WITH FLASHER
Table 151 Stop, Tail, Turn and Hazard Signal Lights With Flasher
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF SPEC.
POINTS SPEC.
1. Off Do some or all of the Go to Go to next step.
stop lights illuminate Step 8.
when the brake pedal is
depressed?
2. Off Remove fuse F3-B and F3-B. <1 ohm. Go to Locate cause of
check for open condition. next step. overload condition,
replace fuse.
3. Off At F3-B measure voltage F3-B, 14E 12±1.5 Go to Locate cause of low
from circuit 14E to to gnd. volts. next step. or no voltage in circuit
ground. 14E or 14H from battery
stud (B2), then repair.
4. Off With fuse re-installed, (640), 70 12±1.5 Go to Locate cause of low or
disconnect connector to gnd. volts next step. no voltage in circuit 70,
(640), and at circuit then repair.
70 measure voltage to
ground.
5. Off With stop light switch Across <1 ohm. Go to Replace defective stop
disconnected, measure stop light next step. light switch.
resistance across sw.
switch with brake pedal
depressed.
6. Off With stop light switch Across >100K Go to Replace defective stop
disconnected, measure stop light ohms. next step. light switch.
resistance across sw.
switch with brake pedal
released.
7. Off Disconnect connector (4), 70A 12±1.5 Go to Locate cause of low
(4), and at circuit 70A to gnd. volts. next step. or no voltage in circuit
measure voltage to 70A, then repair.
ground.
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472 12 LIGHT SYSTEMS
Table 151 Stop, Tail, Turn and Hazard Signal Lights With Flasher (cont.)
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF SPEC.
POINTS SPEC.
8. Off Remove stop light (464-R10), 12±1.5 Go to Locate cause of low
relay from relay socket 70D to volts. next step. or no voltage in circuit
(464-R10), and at circuit gnd. 70D, then repair.
70D measure voltage to
ground with brake pedal
depressed.
9. Off At connector (464-R10) (464- 12±1.5 Go to Locate open or poor
measure voltage from R10), volts. next step. connection in circuit
circuit 70D to 70-G with 70D to 70-G, 56-G, 57-G, or
brake pedal depressed. 70-G. 11-G to ground stud at
right dash panel, then
repair.
10. Off Remove fuse F7-D and F7-D. <1 ohm. Go to Locate cause of
check for open condition. next step. overload condition,
replace fuse.
11. Off At F7-D measure voltage F7-D, 14F 12±1.5 Go to Locate cause of low
from circuit 14F to to gnd. volts. next step. or no voltage in circuit
ground. 14F or 14K from battery
stud (B1), then repair.
12. Off With fuse re-installed, at (464- 12±1.5 Go to Locate cause of low
relay socket (464-R10), R10). volts. next step. or no voltage in circuit
measure voltage at circuit 70E to 70E, then repair.
70E to gnd. gnd.
13. Off At relay socket Go to
(464-R10), install a test next step.
lead jumper wire between
circuits 70E and 70C.
14. Off At trailer socket (112), (112), 12±1.5 Go to Locate cause of low
measure voltage at circuit 70C to volts. next step. or no voltage in circuit
70C to ground. gnd. 70C, then repair.
15. Off Remove test jumper and (112), 12±1.5 Go to Replace defective stop
re-install stop light relay. 70C to volts. next step. light relay.
At trailer socket (112), gnd.
measure voltage at circuit
70C to ground with brake
pedal depressed.
16. Off Remove fuse F7-B and F7-B. <1 ohm. Go to Locate cause of
check for open condition. next step. overload condition,
replace fuse.
17. Off Re-install fuse F7-B. At F7-B, 14L 12±1.5 Go to Locate cause of low
F7-B measure voltage to gnd. volts. next step. or no voltage in circuit
from circuit 14L to ground. 14L or 14K from battery
stud (B1), then repair.
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12 LIGHT SYSTEMS 473
Table 151 Stop, Tail, Turn and Hazard Signal Lights With Flasher (cont.)
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF SPEC.
POINTS SPEC.
18. Off Remove relay (464-R11) (464-R11), 12±1.5 Go to Locate cause of low
and measure voltage to 56H to volts. next step. or no voltage in circuit
circuit 56H to ground. gnd. 56H, then repair.
19. Off At relay socket (464-R11), Go to
install a test lead jumper next step.
wire between circuits 56H
and 56C.
20. Off At trailer socket (112), (112), 12±1.5 Go to Locate cause of low
measure voltage at circuit 56C to volts. next step. or no voltage in circuit
56C to ground. gnd. 56C, then repair.
21. Off With test jumper still in Go to Go to next step.
place does the left turn Step 26.
indicator illuminate?
22. Off With test jumper still (422), 12±1.5 Go to Locate cause of low
in place, disconnect 56R to volts. next step. or no voltage in circuit
connector (422), and gnd. 56R or 56A, then repair.
measure voltage at circuit
56R to gnd.
23. Off With test jumper still (422) 56R 12±1.5 Go to Locate open or poor
in place, disconnect to (421) volts. next step. connection in circuit
connector at (421), and 62-GD. 62-GD or 11-GF, then
measure voltage from repair.
circuit 62-GD to 56R of
(422).
24. Off Reconnect (422) and Go to Replace defective
(421). Does left turn next step. indicator lamp.
indicator illuminate?
25. Off Remove test jumper and Go to
re-install left turn relay. next step.
26. Off Remove fuse F7-C and F7-C. <1 ohm. Go to Locate cause of
check for open condition. next step. overload condition,
replace fuse.
27. Off Re-install fuse F7-C. At F7-C, 14L 12±1.5 Go to Locate cause of low
F7-C measure voltage to gnd. volts. next step. or no voltage in circuit
from circuit 14L to ground. 14L or 14K from battery
stud (B1), then repair.
28. Off Remove relay (464-R12) (464-R12), 12±1.5 Go to Locate cause of low
and measure voltage at 57H to volts. next step. or no voltage in circuit
circuit 57H to ground. gnd. 57H, then repair.
29. Off At relay socket Go to
(464-R12), install a test next step.
lead jumper wire between
circuits 57H and 57C.
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474 12 LIGHT SYSTEMS
Table 151 Stop, Tail, Turn and Hazard Signal Lights With Flasher (cont.)
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF SPEC.
POINTS SPEC.
30. Off At trailer socket (112), (112), 12±1.5 Go to Locate cause of low
measure voltage at circuit 57C to volts. next step. or no voltage in circuit
57C to ground. gnd. 57C, then repair.
31. Off With test jumper still in Go to Go to next step.
place does the right turn Step 36.
indicator illuminate?
32. Off With test jumper still (422), 12±1.5 Go to Locate cause of low
in place, disconnect 57R to volts. next step. or no voltage in circuit
connector (422), and gnd. 57R or 57A, then repair.
measure voltage at circuit
57R to gnd.
33. Off With test jumper still (422), 12±1.5 Go to Locate open or poor
in place, disconnect 57R to volts. next step. connection in circuit
connector at (421), and (421), 62-GD or 11-GF, then
measure voltage from 62-GD. repair.
circuit 62-GD to 57R of
(422).
34. Off Reconnect (422) and Go to Replace defective
(421). Does right turn next step. indicator lamp.
indicator illuminate?
35. Off Remove test jumper and Go to
re-install left turn relay. next step.
36. Off Remove fuse F2-D and F2-D <1 ohm. Go to Locate cause of
check for open condition. next step. overload condition,
replace fuse.
37. Off Re-instal fuse F2-D. At F2-D, 12±1.5 Go to Locate cause of low
F2-D measure voltage 14R to volts. next step. or no voltage in circuit
from circuit 14R to gnd. 14R or 14K from battery
ground. stud (B1), then repair.
38. Off At flasher connector Flasher 12±1.5 Go to Locate cause of low or
measure voltage from conn., 55 volts. next step. no voltage in circuit 55,
circuit 55 to ground. to gnd. then repair.
39. Off Install a test lead jumper Go to
in place of the flasher next step.
unit.
40. Off Disconnect connector (4) (4), 55A 12±1.5 Go to Locate cause of low
at turn signal pigtail, and to gnd. volts. next step. or no voltage in circuit
at circuit 55A measure 55A, then repair.
voltage to ground.
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12 LIGHT SYSTEMS 475
Table 151 Stop, Tail, Turn and Hazard Signal Lights With Flasher (cont.)
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF SPEC.
POINTS SPEC.
41. Off With connector (4) (4), BK to <1 ohm. Go to Replace defective
disconnected, move OR. next step. switch.
switch to left turn position
and measure resistance
from black wire to orange
wire.
42. Off With switch in left turn (4), BK to <1 ohm. Go to Replace defective
position, measure YL. next step. switch.
resistance from black
wire to yellow wire.
43. Off Move switch to right turn (4), BK to <1 ohm. Go to Replace defective
position and measure GN. next step. switch.
resistance from black
wire to green wire.
44. Off With switch in right (4), BK to <1 ohm. Go to Replace defective
turn position, measure BL. next step. switch.
resistance from black
wire to blue wire.
45. Off Move switch to neutral (4), RD to <1 ohm. Go to Replace defective
position and measure YL. next step. switch.
resistance from red wire
to yellow wire.
46. Off With switch in the (4), RD to <1 ohm. Go to Replace defective
neutral position, measure GN. next step. switch.
resistance from red wire
to green wire.
47. Off Remove left turn relay at (464- 12±1.5 Go to Locate cause of low
(464-R11). Reconnect R11), 56E volts. next step. or no voltage in circuit
connector (4) and move to gnd. 56E, then repair.
turn signal switch to
left turn position. At
(464-R11) measure
voltage from circuit 56E
to ground.
48. Off Re-install left turn relay. Go to Replace defective left
Move turn signal switch next step. turn relay.
to left turn position. Do
left turn lamps illuminate?
49. Off Remove right turn relay (464- 12±1.5 Go to Locate cause of low
at (464-R12). Move turn R12), volts. next step. or no voltage in circuit
signal switch to right turn 57E to 57E, then repair.
position. At (464-R12) gnd.
measure voltage from
circuit 57E to ground.
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476 12 LIGHT SYSTEMS
Table 151 Stop, Tail, Turn and Hazard Signal Lights With Flasher (cont.)
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF SPEC.
POINTS SPEC.
50. Off Re-install right turn relay. Go to Replace defective right
Move turn signal switch next step. turn relay.
to right turn position.
Do right turn lamps
illuminate?
51. Off Disconnect connector (3). (3), 56B 12±1.5 Go to Locate cause of low
Move turn signal switch to gnd. volts. next step. or no voltage in circuit
to left turn position, and at 56B, then repair.
(3) measure voltage from
circuit 56B to ground.
52. Off Move turn signal switch to (3), 57B 12±1.5 Go to Locate cause of low
right turn position, and at to gnd. volts. next step. or no voltage in circuit
(3) measure voltage from 57B, then repair.
circuit 57B to ground.
53. Off Reconnect connector (127), 12±1.5 Go to Locate cause of low
(3), and disconnect 56B to volts. next step. or no voltage in circuit
connector (127). Move gnd. 56B, then repair.
turn signal switch to left
turn position, and at (127)
measure voltage from
circuit 56B to gnd.
54. Off Move turn signal switch (127), 12±1.5 Go to Locate cause of low
to right turn position, and 57B to volts. next step. or no voltage in circuit
at (127) measure voltage gnd. 57B, then repair.
from circuit 57B to gnd.
55. Off With the turn signal switch (127), 12±1.5 Go to Locate open or poor
in the right turn position, 57B to volts. next step. connection in circuit
at (127) measure voltage 11-GV. 11-GV, then repair.
from circuit 57B to 11-GV.
56. Off Reconnect connector Go to Replace defective left
(127). With turn signal next step. turn lamp or socket.
switch in left turn position,
do the left turn lamps
illuminate?
57. Off Disconnect connector (128), 12±1.5 Go to Locate cause of low
(128). Move turn signal 57B to volts. next step. or no voltage in circuit
switch to right turn gnd. 57B, then repair.
position, and at (128)
measure voltage from
circuit 57B to gnd.
58. Off With the turn signal switch (128), 12±1.5 Go to Locate open or poor
in the right turn position, 57B to volts. next step. connection in circuit
at (128) measure voltage 11-GN. 11-GN, then repair.
from circuit 57B to 11-GN.
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12 LIGHT SYSTEMS 477
Table 151 Stop, Tail, Turn and Hazard Signal Lights With Flasher (cont.)
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF SPEC.
POINTS SPEC.
59. Off Reconnect connector Go to Replace defective right
(128). With turn signal next step. turn lamp or socket.
switch in right turn
position, do the right turn
lamps illuminate?
60. Off Remove test jumper Go to Replace defective turn
and re-install turn signal next step. signal flasher.
flasher. Do lamps flash
when turn signal switch is
moved to a turn position?
61. Off Stop, tail, turn, and
hazard signal lights
circuits check good.
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478 12 LIGHT SYSTEMS
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12 LIGHT SYSTEMS 479
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480 12 LIGHT SYSTEMS
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12 LIGHT SYSTEMS 481
4. COMPONENT LOCATIONS
B1 Battery Stud.. . .. .. . .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . . . . . Power Distribution Panel
B2 Battery Stud.. . .. .. . .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . . . . . Power Distribution Panel
J7 Junction Point. . . . . . . .. . . . . . . . . . . . . . .. . . . . . . . . . . . . . .. . . . . . In Dash Panel Left Side
(1) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Left Side of Engine Cowl
(2) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Right Side of Engine Cowl, Above Conn. 3
(3) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Right Side of Engine Cowl, Below Conn. 2
(4) Turn Signal Connector. . . . .. . . . . . . .. . . . . . . .. . . . . . .. . . . . . On Steering Column
(42) Headlight Dimmer Switch. . . . . . . . . . . . . . . . . . . . . . .. . . . . . Behind/Below Lt Instrument Panel
(43) Truck Body/Trailer Feed. .. .. . .. .. .. . .. .. .. . .. .. .. . . . . . Left Back of Cab, "B" Pillar
(65) Left Fog Light. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . . . . . Left Inner Bumper
(66) Right Fog Light.. . . . .. . . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . . . Right Inner Bumper
(71) Right Headlight. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . . . . . Hood Harness
(76) Horn (Inline). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Front End Harness, At Lower Left of Radiator
(77) Left Headlight. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Hood Harness
(84) Left Headlight Upper Unit. . . . . . . . . . . . . . . . . . . . . . .. . . . . . Front End Harness
(85) Left Headlight Lower Unit. . . . . . . . . . . . . . . . . . . . . . .. . . . . . Front End Harness
(86) Right Headlight Upper Unit. . . . . . . . . . . . . . . . . . . . .. . . . . . Front End Harness
(87) Right Headlight Lower Unit. . . . . . . . . . . . . . . . . . . . .. . . . . . Front End Harness
(93) Sleeper Box (Inline). .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. . . . . . In Left Luggage Compartment
(94) Back-Up Light Switch. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . . . . . On Transmission
(100) Left & Right Door Courtesy Light. . . . . . . . . . . . .. . . . . . Inside Door
(115) Right Cab Dome Light. . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Right Roof Area
(116) Left Cab Dome Light. . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Left Roof Area
(127) Lt Stop, Tail, Turn & Back-Up Lt. . . . . . . . . . . . . .. . . . . . Left Outer Socket
(127A) Lt Stop, Tail, Turn & Back-Up Lt.. .. . .. .. . .. .. . . . . . Left Inner Socket
(128) Rt Stop, Tail, Turn & Back-Up Lt. . . . . . . . . . . . . .. . . . . . Right Inner to Left Light Inner Socket
(148-R19 Fog Light Relay.. . . . . . . . . . . . . .. . . . . . . . . . . . .. . . . . . Power Distribution Panel
(170) Turn Signal Light Left Side. . . . . . . . . . . . . . . . . . . .. . . . . . Behind Instrument Panel Left Side
(171) Turn Signal Light Right Side. . . . . . . . . . . . . . . . . .. . . . . . Behind Instrument Panel Right Side
(180) Front Left and Right Turn Lights. . . . . . . . . . . . . .. . . . . . Behind Turn Light Assembly
(211) Right Headlight Connector. . . . . . . . . . . . . . . . . . . .. . . . . . Crossmember Harness to Headlight
(296) Front End/Hood (Inline). . . .. . . . . . .. . . . . . .. . . . . .. . . . . . Base of Hood
(311) Right Reading Light. . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Roof Near Light )
(312) Left Reading Light. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . . . Roof Near Light
(314) Work Light Inline. .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . . . . . Rear Center of Cab
(318) W/Stop, Tail & Turn (Inline). . .. . . . . . . . .. . . . . . . .. . . . . . Cab Wiring to Chassis Wiring
(420) Right Gauge Cluster. . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Gauge Cluster
(421) Speedo./Tach. Gauge Cluster . .. . .. . .. . .. . .. .. . . . . . At Speedo Gauge
(422) Speedo./Tach. Module. .. . . .. . . .. . . .. . . .. . . .. . .. . . . . . Behind Speedo./Tach. Gauge
(423) Left Gauge Cluster. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Left Gauge Cluster
(425) Panel Lights Switch . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Switch Cluster
(427) Speakers. . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Left Rear of Cab, “B” Pillar
(428) Roof Connector #2. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Behind Rt Instr. Panel/Roof Conn. to Cab Harn.
(429) Roof Connector #1. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Behind Rt Instr. Panel/Roof Conn. to Cab Harn.
(431) Windshield Wiper Motor Switch. . .. . . . . .. . . . . .. . . . . . At Switch Cluster
(432) Windshield Washer/Delay Switch. . .. .. . .. . .. .. . . . . . At Switch Cluster
(440) Fog Lights Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Switch Cluster
(441) Work Light Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Switch Cluster
(442) Dome Light Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Switch Cluster
(450) Lt Mirror Light. . . . . .. . . . . . . . . .. . . . . . . . . .. . . . . . . . .. . . . . . At Switch Cluster
(451) Rt Mirror Light.. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. . . . . . At Switch Cluster
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482 12 LIGHT SYSTEMS
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12 LIGHT SYSTEMS 483
Figure 137 Stop, Tail And Turn Light Wiring 9100i, 9200i, 9400i And 9900i
NOTE: CONNECTOR NUMBERS SHOWN IN PARENTHESES
1. 22-WAY DASH CONNECTOR (3)
2. CHASSIS HARNESS
3. WIRING TO REAR OF VEHICLE
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484 12 LIGHT SYSTEMS
Figure 138 Stop, Tail And Turn Light Wiring 9400i And 9900i, No Chassis Skirts
1. WIRING TO REAR OF VEHICLE
2. WIRING TO FRONT OF VEHICLE
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12 LIGHT SYSTEMS 485
Figure 139 Stop, Tail And Turn Light Wiring 9100i, 9200i, 9400i And 9900i
1. WIRING TO FRONT OF VEHICLE
2. WIRING TO REAR OF VEHICLE
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486 12 LIGHT SYSTEMS
Figure 140 Stop, Tail And Turn Light Wiring 9100i, 9200i, 9400i, And 9900i
1. STOP AND TAIL LIGHT HARNESS
2. RIGHT TAIL LIGHT (128)
3. LEFT TAIL LIGHT (127), (127A) INSIDE
4. CHASSIS HARNESS—STOP, TAIL AND TURN LIGHT WIRING HARNESS
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12 LIGHT SYSTEMS 487
Figure 141 Relays, Fuses And Circuit Breakers 9100, 9200, 9400 And 9900
1. (B1) BATTERY STUD
2. (B2) BATTERY STUD
3. (148) FOG LIGHT RELAY
4. TURN SIGNAL FLASHER
5. OPTIONAL ALARM
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488 12 LIGHT SYSTEMS
Figure 142 Fixed Steering Column Wiring 9100i, 9200i, 9400i And 9900i
1. HORN BUTTON ASSEMBLY
2. TURN SIGNAL SWITCH
3. GROUND
4. CONDUIT, CONVULATED TUBING
5. GROUND
6. TURN SIGNAL 6-WAY CONNECTOR (4)
7. MAIN CAB HARNESS
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12 LIGHT SYSTEMS 489
Figure 143 Tilt-Telescope Steering Column Wiring 9100i, 9200i, 9400i and 9900i
1. TURN SIGNAL SWITCH
2. CIRCUIT 85C
3. TURN SIGNAL 6-WAY CONNECTOR (4)
4. MAIN CAB HARNESS
5. HORN CIRCUIT 85C
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490 12 LIGHT SYSTEMS
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12 LIGHT SYSTEMS 491
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492 12 LIGHT SYSTEMS
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12 LIGHT SYSTEMS 493
Figure 147 Cab, Clearance, Identification, Dome And Reading Lights (Day Cab without Sun Shade)
1. ROOF CONNECTOR (429)
2. RIGHT READING LAMP (311)
3. DOME LIGHT LEFT (116) & RIGHT (115)
4. LEFT READING LAMP (312)
5. IDENTIFICATION AND CLEARANCE LAMPS
6. CAB ROOF HARNESS
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494 12 LIGHT SYSTEMS
Figure 148 Cab, Clearance, Identification, Dome And Reading Lights (Day Cab with Sun Shade)
1. RIGHT READING LAMP (311)
2. DOME LIGHT LEFT (116) & RIGHT (115)
3. LEFT READING LAMP (312)
4. CLEARANCE LIGHT CONNECTOR (345)
5. CAB ROOF HARNESS
6. IDENTIFICATION AND CLEARANCE LAMPS
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12 LIGHT SYSTEMS 495
Figure 149 Cab, Clearance, Identification, Dome And Reading Lights (With Low And High Roof Pro
Sleepers)
1. ROOF CONNECTOR (429)
2. RIGHT READING LAMP (311)
3. DOME LIGHT LEFT (116) & RIGHT (115)
4. LEFT READING LAMP (312)
5. CLEARANCE LIGHT CONNECTOR (345)
6. CAB ROOF HARNESS
7. IDENTIFICATION AND CLEARANCE LAMPS
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496 12 LIGHT SYSTEMS
Figure 150 Cab, Clearance, Identification, Dome And Reading Lights (With Sky Rise Pro Sleepers)
1. RIGHT READING LAMP (311)
2. DOME LIGHT RIGHT (115)
3. LEFT READING LAMP (312)
4. DOME LIGHT LEFT (116)
5. CAB ROOF HARNESS
6. IDENTIFICATION AND CLEARANCE LAMPS
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12 LIGHT SYSTEMS 497
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498 12 LIGHT SYSTEMS
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500 12 LIGHT SYSTEMS
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12 LIGHT SYSTEMS 501
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502 12 LIGHT SYSTEMS
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12 LIGHT SYSTEMS 503
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504 12 LIGHT SYSTEMS
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12 LIGHT SYSTEMS 505
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506 12 LIGHT SYSTEMS
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12 LIGHT SYSTEMS 507
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508 12 LIGHT SYSTEMS
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13 SLEEPER LIGHTING AND ACCESSORIES 509
Table of Contents
1. DESCRIPTION. . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . ..511
1.1. AUXILIARY CIRCULATION FAN (LOW ROOF, HIGH ROOF & SKYRISE). . . . . . . . . . . . . . . . . . . . . .511
1.2. AUXILIARY RADIO CONTROLS.. .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. .. . .. .. .. .. .. .. . .. .. .. .. ..511
1.3. BUNK FLUORESCENT AND READING LIGHTS . .. . .. . . . . . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . . .. . ..511
1.4. BUNK SPEAKERS .. . .. .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .. . .. . .. . .. . .. . ..511
1.5. LUGGAGE COMPARTMENT LIGHTS .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. .. .. . .. .. .. . .. .. .. .. . .. .. .. . .. .. ..511
1.6. POWER SALEM VENT . . . .. . . .. . .. . . .. . .. . . .. . . .. . .. . . .. . .. . . .. . . .. . .. . . .. . .. . . .. . . .. . .. . . .. . .. . . .. . . ..511
1.7. POWER SOURCE (SLEEPER) . . . .. . .. . . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . . ..511
1.8. REFRIGERATOR WIRING . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . . . . . .. . . . . .. . . . . . .. . . . . .. . . . . .. . . . . . .. . . . . .. . .511
1.9. TV/VCR WIRING . .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. ..511
1.10. OVERHEAD CABINETS, ACCENT LIGHTS WIRING . . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. .. . .. ..511
2. OPERATION.. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .512
2.1. AUXILIARY CIRCULATION FAN (LOW ROOF, HIGH ROOF & SKYRISE) . .. .. .. . .. .. .. . .. .. .. .512
2.2. AUXILIARY RADIO CONTROLS .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .512
2.3. BUNK FLUORESCENT AND READING LIGHTS .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .512
2.4. BUNK SPEAKERS. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .512
2.5. LUGGAGE COMPARTMENT LIGHTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .512
2.6. POWER SALEM VENT . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .513
2.7. POWER SOURCE (SLEEPER) . . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. .. . .. . .. . .. . .. .. . .. . .. . .. .513
2.8. REFRIGERATOR WIRING . .. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . .513
2.9. TV/VCR WIRING. . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . .513
2.10. OVERHEAD CABINETS, ACCENT LIGHTS. .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .513
3. TROUBLESHOOTING. .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .513
3.1. AUXILIARY CIRCULATION FAN (LOW ROOF, HIGH ROOF & SKYRISE). . . . . . . . . . . . . . . . . . . . . .514
3.2. AUXILIARY RADIO CONTROLS .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .515
3.3. BUNK FLUORESCENT AND READING LIGHTS .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .516
3.4. BUNK SPEAKERS . . .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .520
3.5. LUGGAGE COMPARTMENT LIGHTS. . .. . . . . . .. . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . .522
3.6. POWER SALEM VENT . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .524
3.7. POWER SOURCE (SLEEPER). .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .525
3.8. REFRIGERATOR WIRING.. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . . .. . .. . .. . .. . .. . .. . .. . .. . .. . .526
3.9. TV/VCR WIRING. . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . .. . . .. . . .. . . .. . .528
3.10. OVERHEAD CABINETS, ACCENT LIGHTS WIRING. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. .529
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1. DESCRIPTION
1.1. AUXILIARY CIRCULATION FAN (LOW ROOF, HIGH ROOF & SKYRISE)
The auxiliary circulation fan is a small fan that is located in the PRO SLEEPER (LOW ROOF, HIGH ROOF &
SKYRISE) to provide a means of circulating the air. It has two speeds of operation.
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2. OPERATION
Refer to the SLEEPER LIGHTING AND ACCESSORIES circuit diagrams in CTS-5298 or S08225.
2.1. AUXILIARY CIRCULATION FAN (LOW ROOF, HIGH ROOF & SKYRISE)
When the auxiliary circulation fan is switched to high or low position, power flows from the (B2) battery stud
through circuits 14AK, 14AV, 30A fuse F10–D, and circuit 14AX to 5A fuse 582–B. From there power flows
through circuits 76L and 76K to the fan switch and fan motor. The ground path consists of circuits 76–GK,
76–GL, 11–GAC, 11–GAD, 11–GAG, 11–GBC, 11–GBD to ground adapter (454).
When the lower bunk reading light switch is turned on, current will flow from battery stud (B2), through circuit
14AK, 14AP, fuse F8 – D, circuits 63AA, and 63AP, 63AS and 63W to the reading light switch and lamp. The
ground circuit is 63–GW, 11–GAD and 11–GBD to ground adapter (454).
When the upper bunk reading light switch is turned on, current will flow from battery stud (B2), through
circuits 14AK, 14AP, fuse F8–D, circuits 63AA, 63AP, 63AS and 63U to the reading light switch and lamp.
The ground circuit is 63–GU, (switch [220] and circuit 63GX with the Sky-Rise) 11–GAD and 11–GBD to
ground adapter (454).
In the Sky-Rise model switch (220) is opened when the upper bunk is raised. This will inhibit the upper bunk
reading light from illuminating.
When the under cabinet light switch is turned on, current will flow from battery stud (B2) through circuits 14AK,
14AP, fuse F8 – D, circuit 63AA, 63AP, 63AS and 63AR to the under cabinet light switch and lamp. The ground
circuit is 63–GR, 11–GAD and 11–GBD to ground adapter (454).
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power flows through circuits 63AK, and 63AL to the left lamp. If the right luggage compartment light switch is
closed, power will also flow through 63AB, but additionally it will flow through circuit 63AD to the right luggage
compartment light switch. Then power flows through circuit 63AE to the right lamp. The ground path for the left
light is circuits 63–GAK, 11–GAF, 11–GBC, 11–GBD and 11–GBE to ground adapter (454). The ground path
for the right light is circuits 63–GD, 11–GAG, 11–GBC, 11–GBD and 11–GBE to ground adapter (454).
3. TROUBLESHOOTING
Refer to the SLEEPER LIGHTING AND ACCESSORIES circuit diagrams in CTS-5298 or S08225.
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514 13 SLEEPER LIGHTING AND ACCESSORIES
A. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of
charge (SOC) or higher. This represents an open circuit voltage (OCV) of 12.4 volts. Batteries
with an OCV of 12 volts or less are either completely discharged or have a dead cell.
B. Before beginning these test procedures, check any light or indicator lamp filaments that are
suspected of being open (burned out). This is done to avoid unnecessary extensive circuit checks.
C. Before beginning these test procedures, inspect all connectors for loose or damaged pins,
wires, etc. Refer to TEST EQUIPMENT AND CONNECTOR REPAIR section in GROUP 08 –
ELECTRICAL in the CTS – 5000 Master Service Manual.
D. When the technician determines that a fuse is blown, while checking its condition, he is directed
to locate the cause of the overload condition and to repair it. While no further instruction on this
procedure is listed in the diagnostic tables, the common procedure is as follows: isolate sections
of the circuit by disconnecting connectors, and measure the resistance to ground to find the circuit
that is shorted to ground. Then locate the damaged spot in the wire or connector and repair.
E. Diagnostics for circuits that are malfunctioning by sticking in the on position are generally not
covered in detail. It is assumed that the technician knows to check for a malfunctioning switch,
relay, or solenoid.
3.1. AUXILIARY CIRCULATION FAN (LOW ROOF, HIGH ROOF & SKYRISE)
Table 154 Auxiliary Circulation Fan (LOW ROOF, HIGH ROOF & SKYRISE)
STEP KEY ACTION TEST SPEC. YES – IN NO – OUT OF SPEC.
POINTS SPEC.
1. Off Remove fuse F10–D and F10–D. <1 ohm. Go to Locate cause of
check for open condition. next step. overload condition,
then repair. Replace
fuse.
2. Off Re-install fuse F10-D and F10 – D, 12 ± 1.5 Go to Locate cause of low
measure voltage at circuit 14AV to volts. next step. or no voltage in circuit
14AV to ground. gnd. 14AK or 14AV from
battery stud (B2), then
repair.
3. Off Remove fuse 582-B and 582-B. <1 ohm. Go to Locate cause of
check for open condition. next step. overload condition,
then repair. Replace
fuse.
4. Off Re-install fuse 582-B and 582-B, 12 ± 1.5 Go to Locate cause of low
measure voltage at circuit 14AX to volts. next step. or no voltage in circuit
14AX to ground. gnd. 14AX from fuse F10 –
D, then repair.
5. Off Disconnect connector (611) (611) or 12 ± 1.5 Go to Locate cause of low
or (1305) and measure (1305), volts. next step. or no voltage in circuit
voltage from circuit 76K or 76K to 76K or 76L from fuse
76L to ground. gnd. 582-B, then repair.
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13 SLEEPER LIGHTING AND ACCESSORIES 515
Table 154 Auxiliary Circulation Fan (LOW ROOF, HIGH ROOF & SKYRISE) (cont.)
STEP KEY ACTION TEST SPEC. YES – IN NO – OUT OF SPEC.
POINTS SPEC.
6. Off At connector (611) or (611) or 12 ± 1.5 Go to Locate open or
(1305), measure voltage (1305), volts. next step. poor connection in
from circuit 76K or 76L to 76K to circuit 76-GK or 76L,
76 – GK or 76 – GL. 76-GK or 11-GAG, 11-GAD,
76 – GL. 11-GBC or 11-GBD to
gnd. adapter (454),
then repair.
7. Off Circuits to fan check good. Fan and Repair or replace
Reconnect connector (611) circuits defective fan
or (1305). Does fan run in check assembly.
low and high position? good.
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516 13 SLEEPER LIGHTING AND ACCESSORIES
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4. COMPONENT LOCATIONS
B2 Battery Stud.. . .. .. . .. . .. .. . .. . .. .. . .. .. . .. . .. .. . .. .. . . . . . Power Distribution Panel
(43) Truck Body/Trailer Feed. .. .. . .. .. .. . .. .. .. . .. .. .. . . . . . Left Back of Cab, "B" Pillar
(117) Sleeper Box Control Panel. . . . . . . . . . . . . . . . . . . .. . . . . . Behind Sleeper Control Panel (Volume Control)
(118) Sleeper Box Control Panel. . . . . . . . . . . . . . . . . . . .. . . . . . Behind Sleeper Control Panel (Volume Control)
(220) Reading Light Ground Switch. . . . . . . . . . . . . . . . .. . . . . . Upper Bunk, Driver Side, Stop
(322) Left Bunk Jumper.. .. .. . .. .. .. .. .. .. . .. .. .. .. .. .. . . . . . Left Bunk
(323) Right Bunk Jumper.. . . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . . . Right Bunk
(426) Radio Connector #1. . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . . . Radio Pigtail to Cab Harness
(427) Radio Connector #2. . .. . . .. . . .. . . . .. . . .. . . .. . . .. . . . . . Radio Pigtail to Cab Harness
(428) Roof Connector #2. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Behind Right Instrument Panel/Roof Connector to Cab
Harness
(429) Roof Connector #1. . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Behind Right Instrument Panel/Roof Connector to Cab
Harness
(441) Work Light Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Switch Cluster
(454) G2 Ground Adapter. . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Behind Instrument Panel
(463) F8 Fuseblock. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . At Fuse Panel
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534 13 SLEEPER LIGHTING AND ACCESSORIES
Figure 162 Auxiliary Fan Wiring With 51” Low Roof PRO SLEEPER
1. (611) SLEEPER ROOF HARNESS CIRCUITS 76L AND 76-GL TO CONNECTOR
2. SEE THE NEXT FIGURE FOR VIEW OF ARROW C
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13 SLEEPER LIGHTING AND ACCESSORIES 535
Figure 163 Auxiliary Fan Wiring With 51” Low Roof PRO SLEEPER
1. AUXILIARY CIRCULATION FAN
2. (611) CONNECTOR AUXILIARY FAN HARNESS
3. LEFT “B” PILLAR TRIM PANEL
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536 13 SLEEPER LIGHTING AND ACCESSORIES
Figure 164 Auxiliary Fan Wiring With 72” PRO SLEEPER & HIGH ROOF
1. CIRCUITS 76K AND 76-GK
2. (611) CONNECTOR
3. AUXILIARY CIRCULATION FAN
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Figure 165 Auxiliary Fan Wiring With PRO SLEEPER & SKYRISE
1. AUXILIARY CIRCULATION FAN
2. (611) RIGHT SIDE JUMPER HARNESS CIRCUITS 76K AND 76-GK CONNECTOR
3. SKYRISE ROOF JUMPER HARNESS
4. (323) CONNECTOR RIGHT SIDE ROOF JUMPER HARNESS TO SLEEPER ROOF
HARNESS
5. SLEEPER WIRING FOR PRO SLEEPER
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538 13 SLEEPER LIGHTING AND ACCESSORIES
Figure 166 Radio Wiring With Low Roof and High Roof Bunk Speakers PRO SLEEPER
1. AM/FM CASSETTE RADIO
2. (529) RADIO SPEAKER
3. (575) AND (574) BUNK SPEAKERS
4. SLEEPER CONTROL PANEL (SEE FIGURES 169 & 170)
5. SLEEPER WIRING HARNESS
6. (642) ROOF HARNESS CONNECTOR
7. (531) RADIO SPEAKER
8. (906) CAB HARNESS TO SLEEPER HARNESS CONNECTOR
9. (530) RADIO SPEAKER
10. (528) RADIO SPEAKER
11. ANTENNA MULTIPLEXER
12. CAB BASE HARNESS
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13 SLEEPER LIGHTING AND ACCESSORIES 539
Figure 167 Radio Wiring With High Roof And Upper Bunk Speakers PRO SLEEPER
1. (575) BUNK RIGHT SPEAKER CIRCUITS 86AY, 86AZ
2. ROOF HARNESS
3. (574) BUNK LEFT SPEAKER CIRCUITS 86AW, 86AX
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540 13 SLEEPER LIGHTING AND ACCESSORIES
Figure 168 Radio Wiring With SKYRISE Bunk Speakers PRO SLEEPER
1. AM/FM CASSETTE RADIO
2. (529) RADIO SPEAKER
3. (575) AND (574) BUNK SPEAKERS
4. SLEEPER CONTROL PANEL (SEE FIGURES 169 & 170)
5. SLEEPER WIRING HARNESS
6. (642) ROOF HARNESS CONNECTOR
7. (531) RADIO SPEAKER
8. CAB HARNESS TO SLEEPER HARNESS CONNECTOR (906)
9. (530) RADIO SPEAKER
10. (528) RADIO SPEAKER
11. ANTENNA MULTIPLEXER
12. CAB BASE HARNESS
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Figure 169 Radio Wiring With PRO SLEEPER (With Headset Jack)
1. HEADSET ADAPTER
2. SLEEPER CONTROL PANEL
3. SLEEPER CONTROL PANEL
4. (118) CONNECTOR CIRCUITS 86AT, 86AU, 86AY, 86AZ
5. (117) CONNECTOR CIRCUITS 86AR, 86AS, 86AW, 86AX
6. (577) CONNECTOR
7. SLEEPER WIRING HARNESS
8. (576) CONNECTOR
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542 13 SLEEPER LIGHTING AND ACCESSORIES
Figure 170 Radio Wiring With PRO SLEEPER (Without Headset Jack)
1. SLEEPER CONTROL PANEL
2. SLEEPER CONTROL PANEL
3. (118) CONNECTOR CIRCUITS 86AT, 86AU, 86AY, 86AZ
4. (117) CONNECTOR CIRCUITS 86AR, 86AS, 86AW, 86AX
5. SLEEPER WIRING HARNESS
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Figure 171 Fluorescent Light And Reading Light High Roof and Low Roof PRO SLEEPER
1. (603) FLUORESCENT LIGHT
2. (607) TV/VCR CONNECTOR
3. (606) TO AUXILIARY FAN
4. (720) READING LIGHT
5. (604) READING LGHT (HIGH ROOF ONLY)
6. UNDER CABINET LIGHT
7. SLEEPER ROOF HARNESS
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544 13 SLEEPER LIGHTING AND ACCESSORIES
Figure 172 Fluorescent Light and Reading Light Wiring with High Roof PRO SLEEPER and Upper
Bunk
1. TO FLUORESCENT LIGHT
2. TO TV/VCR AND AUXILIARY FAN
3. (720) UPPER READING LIGHT
4. (604) LOWER READING LIGHT
5. (605) UNDER CABINET LIGHT
6. SLEEPER BOX ROOF HARNESS
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Figure 173 Fluorescent Light And Reading Light SKYRISE PRO SLEEPER
1. TO TV/VCR AND AUXILIARY FAN
2. (603) FLUORESCENT LIGHT
3. (604) READING LGHT
4. (322) SLEEPER ROOF JUMPER
5. (220) READING LIGHT GND SWITCH
6. (720) READING LIGHT
7. (605) UNDER CABINET LIGHT CIRCUIT 63–AR, 63–GR
8. SLEEPER ROOF HARNESS
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546 13 SLEEPER LIGHTING AND ACCESSORIES
Figure 174 Wiring and Luggage Compartment Lights PRO SLEEPER With High Roof, Low Roof
and SKYRISE
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Figure 175 Wiring, Luggage Compartment Lights And Right Aux. Power Source PRO SLEEPER With
High Roof, Low Roof and SKYRISE
1. SLEEPER HARNESS (DRIVER SIDE WIRING)
2. SLEEPER HARNESS (PASSENGER SIDE WIRING)
3. CONNECTOR (609)
4. LUGGAGE COMPARTMENT SWITCH (MERCURY)
5. SLEEPER HARNESS
6. (588) LUGGAGE COMPARTMENT LIGHT
7. TO SLEEPER HARNESS ON LEFT SIDE OF SLEEPER
8. (789) RIGHT AUXILIARY POWER SOURCE
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Figure 176 Fuse and Relay Wiring PRO SLEEPER With High Roof, Low Roof and SKYRISE
1. 5 AMP REFRIGERATOR FUSE
2. 10 AMP AUXILIARY BLOWER FUSE
3. 20 AMP TV FUSE
4. MAIN SLEEPER HARNESS
5. MEDIUM SPEED RELAY
6. HIGH SPEED RELAY
7. LABEL
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Figure 177 Bunk Light Wiring PRO SLEEPER With High Roof, Low Roof and SKYRISE
1. CONTROL PANEL
2. BUNK LIGHT SWITCH
3. (594) CONNECTOR CIRCUITS 63-GE, 63-GF, 63-GJ, 63-GK, 63–GZ AND 62Z
4. SLEEPER HARNESS
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Figure 178 Refrigerator Wiring PRO SLEEPER With High Roof Or Low Roof W/118” Sleeper Only
1. CONTROL PANEL
2. SLEEPER WIRING HARNESS
3. (612) REFRIGERATOR POWER SOURCE
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Figure 179 Refrigerator Wiring PRO SLEEPER With High Roof Or Low Roof W/118” Sleeper Only
1. SLEEPER CONTROL PANEL
2. (613) REFRIGERATOR ON/OFF SWITCH
3. SLEEPER WIRING HARNESS CIRCUITS 62X, 62–GX, 86–GK, 86AV AND 86AG
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Figure 180 TV and Antenna Installation PRO SLEEPER With 72” High Roof W/Upper Bunk
1. (607) TV/VCR POWER SOURCE CIRCUITS 86AP, 86–GP
2. TV ANTENNA
3. SLEEPER TV/VCR WIRING HARNESS
4. SEE FIGURE 184 FOR VIEW OF ARROW D
5. SEE FIGURE 184 FOR VIEW OF CIRCLE C
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Figure 182 TV And Antenna Installation Sky—Rise PRO SLEEPER No Upper Bunk
1. (607) TV/VCR POWER SOURCE CIRCUITS 86AP, 86-GP
2. TV ANTENNA
3. SLEEPER CONTROL PANEL SEE FIGURE 181
4. SLEEPER HARNESS
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Figure 183 TV And Antenna Installation Sky-Rise PRO SLEEPER With Upper Bunk
1. (607) TV/VCR POWER SOURCE CIRCUITS 86AP, 86–GP
2. TV ANTENNA
3. SLEEPER TV/VCR WIRING HARNESS
4. SEE FIGURE 184 FOR VIEW OF ARROW D
5. SEE FIGURE 184 FOR VIEW OF CIRCLE C
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Figure 184 TV And Antenna Installation 72 Inch High Roof, Sky-Rise PRO SLEEPER With Upper Bunk
1. (607) TV/VCR POWER SOURCE CIRCUITS 86AP, 86-GP
2. SLEEPER TV/VCR HARNESS
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Figure 185 Overhead Cabinets, Accent Lights Installation High Roof And EAGLE PRO SLEEPER
1. (1313) RIGHT ACCENT LIGHTS
2. (1312) CENTER ACCENT LIGHTS
3. (1311) LEFT ACCENT LIGHTS
4. (310) CONNECTOR ACCENT LIGHTS CIRCUITS 62BB, 62–GBB
5. SLEEPER HARNESS TO ACCENT LIGHTS ON/OFF SWITCH (1289)
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14 HEATER AND AIR CONDITIONER 559
Table of Contents
1. DESCRIPTION. .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .. . . .. . .. . .. . .561
1.1. HVAC CONTROL-CAB. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. .. . .. .. . .. .. .561
1.2. HEATER-BUNK WITH STANDARD TEMPERATURE CONTROL. . . . . . .. . . . . .. . . . . . .. . . . . . .. . . . . .561
1.3. HEATER-BUNK WITH THERMOSTAT TEMPERATURE CONTROL. .. .. .. . .. .. .. .. .. . .. .. .. .. .. .561
2. OPERATION.. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. . .. .. .. .. .561
2.1. AIR CONDITIONER-CAB . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . .561
2.2. BLOWER-CAB . . .. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . .562
2.3. AIR DISTRIBUTION-CAB.. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .. . .. .. . .. .. . .. .. . .. .. . .. .. . .. .. .563
Temperature Control.. . . . . .. . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .563
Air Distribution Selection. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .563
Recirculation. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. . .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .. .563
2.4. HEATER-BUNK WITH STANDARD TEMPERATURE CONTROL. . . . . . .. . . . . .. . . . . . .. . . . . . .. . . . . .564
2.5. HEATER-BUNK WITH THERMOSTAT TEMPERATURE CONTROL. .. .. .. . .. .. .. .. .. . .. .. .. .. .. .565
3. TROUBLESHOOTING. .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . . .. . . .. . . .. . . . .. . . .. . . .566
3.1. AIR CONDITIONER-CAB . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . .567
3.2. BLOWER-CAB . . .. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . . .. . . .572
3.3. TEMPERATURE CONTROL-CAB . . . . . .. . . . . . . . .. . . . . . . . .. . . . . . . . .. . . . . . . . .. . . . . . . . .. . . . . . . .. . . . . . . . .578
3.4. AIR DISTRIBUTION MOTOR-CAB . . . . . . . . . .. . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . .. . . . . . . . . . . . . . . . . . .579
3.5. RECIRCULATION MOTOR-CAB . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .579
3.6. HEATER-BUNK AUXILIARY BLOWER . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . .. . . . .. . . . .580
3.7. HEATER-BUNK WITH STANDARD TEMPERATURE CONTROL . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .585
3.8. HEATER-BUNK WITH THERMOSTAT TEMPERATURE CONTROL .. . . . . .. . . . .. . . . . .. . . . . .. . . . .587
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1. DESCRIPTION
Refer to Truck Service Manual S16023 AIR CONDITIONER – HEATER SYSTEM: 9100i, 9200i, 9400i, 9900i
MODELS for information on removal and installation of components.
The blower control knob on the left side of the control allows the operator to select one of four blower speeds.
The temperature control knob in the center of the HVAC control module controls a stepper motor in the heater
box allowing the operator to determine the mixture of hot and cold air available at the air ducts in the cab.
The mode control knob on the right side allows the operator to control air distribution. This is performed by a
stepper motor in the air ducts. The operator may select air flow to the defrost duct (when defrost is selected
the AC compressor will be activated), mixed lower duct and defrost duct, lower heat duct, mixed lower and
upper duct, and upper duct. The MAX position controls a recirculation stepper motor which will recirculate air
to speed up cooling of the cab. Air flow may be turned off by selecting OFF.
The BUNK button will shut off the bunk blower and all sleeper HVAC controls.
2. OPERATION
Refer to the HEATER AND AIR CONDITIONER circuit diagrams in CTS-5298 or S08225.
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If the vehicle is equipped with a sleeper A/C On/Off switch, A/C control relay (144) can also be energized when
the bunk heater blower switch (593) is not in the off position and the sleeper A/C switch (905) is on. The switch
will illuminate when it is on. Power flows from switch (593) on circuits 77L, 77AB and 77AC through switch
(905) to circuits 77M and 77K to energize the relay.
Power from fuse F1–B will flow through the relay on circuit 77H to connector (162) of the heater box pigtail.
From (162) it can flow through circuit 77C and 77P to feed the low pressure safety switch, circuits 77C and
77N to feed the high pressure safety switch, and 77B to feed the thermal switch. If the refrigerant pressure is
greater than the low pressure cut off switch, and less than the high pressure cut off switch, circuit 77R will not
have power applied. Thus, A/C relay (463–R6) normally closed (N.C.) contacts remain closed and while the
thermal switch contacts remain closed, power will flow from the thermal switch through circuit 77F, A/C relay
(463–R6) contacts, and circuit 77C to energize the refrigerant compressor clutch.
When the evaporator temperature cools to below 30° ± 2° (-1° ± 1°C), the thermal switch contacts will open
cutting off the flow of power to the compressor clutch. This will keep the evaporator from freezing over. If
either of the safety pressure switches close, the A/C relay will energize and its contacts will open breaking
power to the compressor clutch.
With the air conditioning relay (463–R6) energized, power is interrupted to the refrigerant compressor
clutch. Thus, the compressor is shut down, and will not restart until the refrigerant pressure is back within
operating range.
2.2. BLOWER-CAB
Power is supplied to (B2) battery stud, circuits 14H, 14Z, fuse F1–C and circuit 75A to the main control
relay (463–R5). When the ignition switch is on, power is applied to circuit 62P of HVAC control connector
(1057). When the HVAC control is not in the OFF position, 12 volts is applied to the coil of main control relay
(463–R5). The ground path for the main control relay is circuits 13–GT, 77–G, 58–GA and 11–G to right dash
panel ground stud. This energizes the main control relay (463–R5) and allows power to flow through the relay
contacts and circuit 75B to blower control switch (1056).
When the blower control switch (1056) is moved to the low position, there is no input from the switch to resistor
block (27). Power from main control relay (463–R5) will be applied through circuit 75BL, 75C, connector
(162), 75C to resistor block (27) terminal C. Power from the resistor block will be applied through circuit 75T,
connector (161), circuit 75T, high speed relay (462–R2) N.C. contacts, circuit 75F, connector (161) and circuit
75F to the blower motor. This causes the blower motor to run at low speed. The blower motor ground path
is through circuit 75–G, connector (161), circuits 75–G and 75–GL to connector (1057) of the HVAC control
module. Power flows through these circuits when the blower switch is in any position other than HIGH, as long
as the middle knob of the HVAC control module is not in the OFF position.
When the blower control switch (1056) is moved to the medium low position, power will flow through the
switch, circuit 75BH, connector (161), circuit 75M to resistor block (27) terminal A. Power from the resistor
block, terminal B, will be applied through circuit 75T, connector (161), circuit 75T, high speed relay (462–R2)
N.C. contacts, circuit 75F, connector (161) and circuit 75F to the blower motor. This causes the blower motor
to run at medium low speed. The blower motor ground path is through circuit 75–G, connector (161), circuits
75–G and 75–GL to connector (1057) of the HVAC control module.
When the blower control switch (1056) is moved to the medium high position, power will flow through the
switch on circuit 75N to the coil of medium high speed relay (462-R3). This energizes the medium high
speed relay (462–R3) which is grounded through circuits 75–GC, 50–GB and 11–G to the right dash panel
ground stud. Power from main control relay (462–R2), on circuit 75BL and 75D, will be applied to heater box
pigtail connector (1060) on circuit 75M. Power will be applied to the resistor block from connector (1060) on
circuit75BH. Power from the resistor block will be applied through circuit 75T, connector (161), circuit 75T, high
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speed relay (462–R2) N.C. contacts, circuit 75F, connector (161) and circuit 75F to the blower motor. This
causes the blower motor to run at medium high speed. The blower motor ground path is through circuit 75–G,
connector (161), circuits 75–G and 75–GL to connector (1057) of the HVAC control module.
When the blower control switch (1056) is moved to the high position, power will flow through the switch on
circuit 75H to the high speed relay (462–R2). This energizes the high speed relay (462–R2) which is grounded
through circuits 75–GB, 75–GC, 50–GB and 11–G to the right dash panel ground stud. This allows power to
flow from (B2) battery stud through circuits 14H, 14X, fuse F1–A, circuit 75, high speed relay (462–R2) N.O.
contacts, circuit 75F, connector (161), and circuit 75F to the blower motor. This causes the blower to run at
high speed. The blower motor ground path is through circuit 75–G, connector (161), circuits 75–G and 75–GL
to connector (1057) of the HVAC control module.
Cab temperature is controlled by a stepper motor in the heater box which controls the mixture of hot and cold air.
12 volts is supplied from fuse F9-D on circuit 75BC, circuit 75BJ, terminal A of connector (162), and 75BJ to
the stepper motor
The stepper motor ground path is through circuit 75–GL, connector (161), circuits 75–G and 75–GL to terminal
12 on connector (1057) of the HVAC control module.
The control voltage from the HVAC control module originates on terminal 3, circuit 75BE and is applied to
heater box connector (1060) and the stepper motor.
Cab air distribution is controlled by a stepper motor in the cab duct work which directs air flow to the desired
vents. The air distribution motor is located behind the instrument panel in front of the driver.
12 volts are supplied from fuse F9-D on circuit 75BC and circuit 75BK to the stepper motor.
The stepper motor ground path is through circuit 75–GM and circuit 75–GL to terminal 12 on connector (1057)
of the HVAC control module.
The control voltage from the HVAC control module originates on terminal 6 of (1057), circuit 75BF and is
applied to the stepper motor.
Recirculation
Recirculation of cab air is controlled by a stepper motor in the cab duct work which directs air flow between
internal and external air. The recirculation motor is located below the kick panel in front of the passenger seat.
12 volts is supplied from fuse F9-D on circuit 75BC and circuit 75BM to the stepper motor
The stepper motor ground path is through circuit 75–GK and circuit 75–GL to terminal 12 on connector (1057)
of the HVAC control module.
The control voltage from the HVAC control module originates on terminal 7, circuit 75BG and is applied to
the stepper motor.
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564 14 HEATER AND AIR CONDITIONER
When the bunk heater blower switch (593) is moved to the low speed position, power flows through circuit
75AC, connector (49), circuit 75AC, resistor and thermofuse assembly, circuit 75AT, connect (48), circuit
75AT, sleeper high speed relay (584) N.C. contacts, circuit 75AF, connector (48) and circuit 75AF to the
sleeper blower motor (1053).
This causes the blower motor to run at low speed. The blower motor ground path is circuit 75–GA, connector
(48), circuits 75–GA, 11–GBD, and 11–GBC to ground adapter (454).
When the bunk blower switch (593) is moved to the medium speed position, power flows through circuit 75AN
to the sleeper medium speed relay (585). The ground path for the sleeper medium speed relay (585) is circuits
75–GN, 11–GBD, and 11–GBC to ground adapter (454). This energizes the sleeper medium speed relay (585)
and allows power to flow from (B2) battery stud through circuits 14AK, 14AU, fuse F10–A (location may vary),
circuits 75AW, 75AB, sleeper medium speed relay (585) N.O. contacts, circuit 75AM, connector (48), circuit
75AM, resistor and thermofuse assembly (N/L), circuit 75AT, connector (48), circuit 75AT, sleeper high speed
relay (584) N.C. contacts, circuit 75AF, connector (48), and circuit 75AF to sleeper blower motor. This causes
the blower motor to run at medium speed. The blower ground path is circuit 75–GA, connector (48), circuit
75–GA, 11–GBD, and 11–GBC to ground adapter (454).
When the bunk blower switch (593) is moved to the high speed position, power flows through the switch, circuit
75AH to the sleeper high speed relay (584). The ground path for the sleeper high speed relay (584) is circuits
75–GH, 75–GN, 11–GBD, and 11–GBC to ground adapter (454).
This energizes the sleeper high speed relay (584) and allows power to flow from (B2) battery stud through
circuits 14AK and 14AU, 30A fuse F10–A (location may vary), circuit 75AW, connector (942), circuits 75AW,
75AD, sleeper high speed relay (584) N.O. contacts, circuit 75AF, connector (48) and circuit 75AF to sleeper
blower motor. This causes the blower motor to run at high speed.
The blower ground path is circuit 75–GA, connector (48), circuits 75–GA, 11–GBD and 11–GBC to ground
adapter (454).
When the key switch (40) is moved to the ignition position and the blower switch (593) is not off, power is
also made available by the auxiliary bunk relay (147) to circuit 75AS, connector (906), circuit 75AS, switch
(592), and circuit 75AL to sleeper temperature control connector (592). The ground path for the sleeper
temperature control is through connector (592), circuit 75-GS, 11–GAE to sleeper ground stud (746), circuit
11–GAN, connector (942) and circuit 11–GAN to B-pillar ground stud.
When the bunk heater blower switch (593) is moved to the high, medium or low positions, power flows through
circuit 77L, connector (905) and 75AL to sleeper temperature control (592). This allows the voltage from the
sleeper temperature control to control the heater box flat pack.
Power is made available by fuse F-9D to circuits 75BC and 75BJ, connector (162) and circuit 75BJ to the
heater box damper flat pack (stepper motor). The heater box damper flat pack is grounded through circuit
75–GL, connector (161), circuits 75–G and 11–G to right dash panel ground stud. The flat pack receives a
variable voltage from the sleeper temperature control through connector (592), circuit 75K, connector (906),
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circuit 75K, connector (162) and circuit 75K. Thus, the damper blends hot and cold air as selected by the
sleeper temperature control.
When cooling is required in the sleeper and the cab A/C switch is not in the on position, the cab switch must
be moved to the on position by the driver or sleeper occupant. Thus, the A/C compressor will engage (the
compressor will cycle with the thermal switch) and cooling will be available for the sleeper blower.
NOTE – This is the standard manual temperature control. The output of the system does not change
with changes in temperature.
When the bunk heater blower switch (593) is moved to the low speed position, power flows through circuit
75AC, connector (49), circuit 75AC, resistor and thermofuse assembly, circuit 75AT, connect (48), circuit
75AT, sleeper high speed relay (584) N.C. contacts, circuit 75AF, connector (48) and circuit 75AF to the
sleeper blower motor (1053).
This causes the blower motor to run at low speed. The blower motor ground path is circuit 75–GA, connector
(48), circuits 75–GA, 11–GBD, and 11–GBC to ground adapter (454).
When the bunk blower switch (593) is moved to the medium speed position, power flows through circuit 75AN
to the sleeper medium speed relay (585). The ground path for the sleeper medium speed relay (585) is circuits
75–GN, 11–GBD, and 11–GBC to ground adapter (454). This energizes the sleeper medium speed relay (585)
and allows power to flow from (B2) battery stud through circuits 14AK, 14AU, fuse F10–A (location may vary),
circuits 75AW, 75AB, sleeper medium speed relay (585) N.O. contacts, circuit 75AM, connector (48), circuit
75AM, resistor and thermofuse assembly (N/L), circuit 75AT, connector (48), circuit 75AT, sleeper high speed
relay (584) N.C. contacts, circuit 75AF, connector (48), and circuit 75AF to sleeper blower motor. This causes
the blower motor to run at medium speed. The blower ground path is circuit 75–GA, connector (48), circuit
75–GA, 11–GBD, and 11–GBC to ground adapter (454).
When the bunk blower switch (593) is moved to the high speed position, power flows through the switch, circuit
75AH to the sleeper high speed relay (584). The ground path for the sleeper high speed relay (584) is circuits
75–GH, 75–GN, 11–GBD, and 11–GBC to ground adapter (454).
This energizes the sleeper high speed relay (584) and allows power to flow from (B2) battery stud through
circuits 14AK and 14AU, 30A fuse F10–A (location may vary), circuit 75AW, connector (942), circuits 75AW,
75AD, sleeper high speed relay (584) N.O. contacts, circuit 75AF, connector (48) and circuit 75AF to sleeper
blower motor. This causes the blower motor to run at high speed.
The blower ground path is circuit 75–GA, connector (48), circuits 75–GA, 11–GBD and 11–GBC to ground
adapter (454).
When the key switch (40) is moved to the ignition position and the blower switch (593) is not off, power is
also made available by the auxiliary bunk relay (147) to circuit 75AS, connector (906), circuit 75AS, switch
(592), and circuit 75AL to sleeper temperature control connector (592). The ground path for the sleeper
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566 14 HEATER AND AIR CONDITIONER
temperature control is through connector (592), circuit 75-GS, 11–GAE to sleeper ground stud (746), circuit
11–GAN, connector (942) and circuit 11–GAN to B-pillar ground stud.
When the bunk heater blower switch (593) is moved to the high, medium or low positions, power flows through
circuit 75AL to the auto temperature control module (592). This allows the voltage from the auto temperature
control module to control the heater box flat pack (stepper motor).
Power is made available by fuse F-9D to circuits 75BC and 75BJ, connector (162) and circuit 75BJ to the
heater box damper flat pack (stepper motor). The heater box damper flat pack is grounded through circuit
75–GL, connector (161), circuits 75–G and 11–G to right dash panel ground stud. The flat pack receives a
variable voltage from the sleeper temperature control through connector (592), circuit 75K, connector (906),
circuit 75K, connector (162) and circuit 75K. Thus, the damper blends hot and cold air as selected by the
sleeper temperature control.
When the key switch (40) is in ignition position and the bunk heater blower switch (593) is in low, medium or
high position, power is applied to circuit 77L and the sleeper A/C On/Off switch (905). When the switch is
moved to the on position, the switch indicator lamp illuminates. The ground path for the lamp is through circuits
75–GBB, 75–GBA and 77–GL to the sleeper ground stud. When the switch is moved to on position, power is
also supplied to the A/C control relay (144) by way of connector (905), circuit 77M, connector (906) and circuit
77M. Thus, the A/C compressor will engage, if it is not already running (the compressor will cycle with the
thermal switch), and cooling will be available for the sleeper blower.
NOTE – This is the optional thermostat temperature control circuit. The output of the system changes
with changes in temperature to maintain the temperature of the sleeper at the thermostat setting.
3. TROUBLESHOOTING
Refer to the HEATER AND AIR CONDITIONER circuit diagrams in CTS-5298 or S08225.
A. Before beginning these test procedures, make sure the vehicle batteries are at 75% state of
charge (SOC) or higher. This represents an open circuit voltage (OCV) of 13.4 volts. Batteries
with an OCV of 12 volts or less are either completely discharged or have a dead cell.
B. Before beginning these test procedures, check any light or indicator lamp filaments that are
suspected of being open (burned out). This is done to avoid unnecessary extensive circuit checks.
C. Before beginning these test procedures, inspect all connectors for loose or damaged pins,
wires, etc. Refer to TEST EQUIPMENT AND CONNECTOR REPAIR section in GROUP 08 —
ELECTRICAL in the CTS-5000 Master Service Manual.
D. When the technician determines that a fuse is blown, while checking its condition, he is directed
to locate the cause of the overload condition and to repair it. While no further instruction on this
procedure is listed in the diagnostic tables, the common procedure is as follows: isolate sections
of the circuit, by disconnecting connectors, and measure the resistance to ground to find the circuit
that is shorted to ground. Then locate the damaged spot in the wire or connector and repair.
E. Diagnostics for circuits that are malfunctioning by sticking in the on position are generally not
covered in detail. It is assumed that the technician knows to check for a malfunctioning switch,
relay, or solenoid.
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3.2. BLOWER-CAB
Table 165 Blower-Cab
STEP KEY ACTION TEST SPEC. YES - IN NO - OUT OF SPEC.
POINTS SPEC.
1. On When the ignition is on Go to Step Go to next step.
and the mode select 19.
switch is not off, does the
blower run in low speed
position?
2. Off/ On Remove main control (463-R5), 12 ± 1.5 Go to step Go to next step.
relay (463-R5). Insure 13BH to volts. 4.
the HVAC control mode ground.
switch is not off and turn
ignition on. Measure
voltage between circuit
13BH and ground.
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4. COMPONENT LOCATIONS
(B1) Battery Stud. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . . Power Distribution Panel
(B2) Battery Stud. . . . . .. . . . .. . . . . .. . . . .. . . . . .. . . . .. . . . .. . . . . . Power Distribution Panel
J7 Junction Point/Ground Stud. . . . . . . . . . . . . . . . . . . . . .. . . . . . At Dash Panel Left Side
(1) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Left Side of Engine Cowl
(2) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Right Side of Engine Cowl, Above Connector 3
(3) Dash Panel Connector. . .. .. . .. . .. .. . .. .. . .. .. . .. .. . . . . . Right Side of Engine Cowl, Below Connector 2
(27) Heater Resistor & Thermofuse. . . . . . . . . . . . . . . . .. . . . . . In Heater Box
(28) Heater Resistor & Thermofuse/Box Sleeper
. . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . . . . . .. . . . . . . .. . . . . . .. . . . . . .. . . . . . In Heater Box
(40) Key Switch.. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. . .. .. . .. .. . . . . . Instrument Panel to Left of Steering Column.
(43) Truck Body/Trailer Feed . .. . . . . . . . . . .. . . . . . . . . . .. . . . . . Left Rear of Cab, "B" Pillar
(48) Sleeper Blower Motor Connector/Pro
Sleeper.. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . .. . . . . . At “B”– Pillar, Right Side
(147) Auxiliary Bunk Blower Relay/Pro Sleeper . . . . . . . . . Power Distribution Panel
(147) Heater Control Motor #2/Box Sleeper. . . . . . . .. . . . . . Power Distribution Panel
(161) Heater Box Connector. . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Pigtail at Right Front of Cab
(162) Heater Box Connector. . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Pigtail at Right Front of Cab
(196) Resistor and Thermofuse Assembly/Pro
Sleeper.. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . . .. . . . . .. . . . . . Inside Blower Assembly
(227) Fan Solenoid.. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. . .. .. . . . . . At Front of Engine
(228) A/C High Pressure Switch/Pro Sleeper. . . . . .. . . . . . At A/C Compressor, on Engine
(454) G2 Ground Adapter. . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . . Behind Instrument Panel
(462) R2 High Speed Fan #1 Relay. . . . . . . . . . . . . . . . .. . . . . . Power Distribution Panel
(462) R3 High Speed Fan #2 Relay. . . . . . . . . . . . . . . . .. . . . . . Power Distribution Panel
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14 HEATER AND AIR CONDITIONER 591
Figure 186 Cab Heater And Air Conditioner Wiring (Dash Panel)
1. WIRING TO REAR OF CAB OR PRO SLEEPER
2. CIRCUIT 11-GB
3. CIRCUIT 11-G
4. NO BUS BAR WITH 3+1 BATTERY SYSTEM
5. TO HEATER
6. (3) ENGINE HARNESS CONNECTOR
7. (2) CHASSIS HARNESS CONNECTOR
8. RIGHT HAND DASH GROUND STUD
9. FUSE BLOCK GROUND STUD
10. (B2) BATTERY STUD
11. (B1) BATTERY STUD
12. KEY SWITCH
13. LEFT HAND DASH GROUND STUD
14. (1) FRONT END HARNESS CONNECTOR
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592 14 HEATER AND AIR CONDITIONER
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14 HEATER AND AIR CONDITIONER 593
Figure 188 Cab Heater And Air Conditioner Wiring (Pro Sleeper)
1. TO WIRING AT DASH
2. SLEEPER BOX HARNESS
3. SLEEPER CONNECTOR #1 (906)
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594 14 HEATER AND AIR CONDITIONER
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14 HEATER AND AIR CONDITIONER 595
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596 14 HEATER AND AIR CONDITIONER
1. 150A MEGAFUSE
2. CIRCUIT 14A TO (B1), (B2) BATTERY STUDS
3. CIRCUIT 14
4. STARTER MAGNETIC SWITCH
5. CIRCUIT 2
6. CIRCUIT 17C
7. CIRCUIT 17B
8. CIRCUIT 14A
Figure 191 Typical Engine Wiring to Air Conditioner Compressor (Caterpillar 3406E Shown)
1. (190) ELECTRONIC ENGINE CONNECTOR
2. (3) CHASSIS HARNESS CONNECTOR
3. (2) CAB/ENGINE HARNESS CONNECTOR
4. RIGHT HAND DASH PANEL GROUND STUD
5. TO ENGINE HARNESS
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Figure 192 Typical Engine Wiring to Air Conditioner Compressor (Caterpillar 3406E Shown)
1. AIR CONDITIONING COMPRESSOR
2. ENGINE HARNESS TO DASH WIRING
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Figure 193 Typical Engine Wiring To A/C Compressor (Caterpillar 3406E Shown)
1. CIRCUIT 77C
2. ALTERNATOR
3. ENGINE HARNESS
4. INLINE CONNECTOR
5. AIR CONDITIONER HIGH PRESSURE SWITCH (228)
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Printed in the United States of America