TM 5-2410-240-23-1
0020
Table 2. Powertrain and Chassis Troubleshooting with Codes - Continued.
CID FMI CODE
Test or Inspection
Corrective Action
0096-04 Fuel Level Sensor
11. Using digital multimeter (WP
Continuity - Proceed to step 12.
Voltage Below Normal - Con-
0283), test for continuity between
No Continuity - Replace platform wir-
tinued
pin 21 on platform harness ECM
ing harness (WP 0150, WP 0155).
J1 connector PL-C4 (WP 0018,
Ensure all harness connectors are
Figure 217) and pin 5 on platform
reconnected. Verify proper operation
harness to fuel tank harness con-
of machine (TM 5-2410-240-10).
nector PL-C11 (WP 0018, Figure
221).
12. Using digital multimeter (WP
No Continuity - Replace machine
0283), test for continuity between
ECM (WP 0147, WP 0149). Ensure all
pin 30 on platform harness ECM
harness connectors are reconnected.
J1 connector PL-C4 (WP 0018,
Verify proper operation of machine
Figure 217) and all other pins on
(TM 5-2410-240-10).
platform harness ECM J1 connec-
Continuity - Replace platform wiring
tor PL-C4 (WP 0018, Figure 217).
harness (WP 0150, WP 0155).
Ensure all harness connectors are
reconnected. Verify proper operation
of machine (TM 5-2410-240-10).
N OT E
0133-03 Transmission Pilot
Pressure Solenoid Voltage
Always inspect harness connectors that are involved in circuit. Poor
Above Normal
connections can often be the cause of an electrical circuit problem.
Verify that all connections in circuit are clean, secure, and connections
are in good condition. If a problem with connection is found, correct
problem and verify diagnostic code is active before performing this
procedure.
Tag wiring harnesses to aid installation.
0133-03 Code Active - Proceed to
1. Connect MSD (WP 0016). Select
step 2.
machine control ECM and check
for diagnostic codes (WP 0013).
No Codes Active - The problem does
not exist at this time. Resume normal
operation.
2. Turn ignition switch and battery
disconnect switch to OFF position
(TM 5-2410-240-10).
3. Disconnect pump harness pilot
pressure supply solenoid connec-
tor PH-C2 (WP 0018, Figure 206)
from pilot pressure supply sole-
noid (WP 0132).
4. Disconnect pump harness to
engine harness connector PH-C1
(WP 0018, Figure 205) from
engine harness to platform har-
ness connector EN-C21 (WP
0018, Figure 137).