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Figure 5. Front Cover.
Figure 6. Splash Shield and Retaining Hardware.

Field Maintenance Manual For Military 621G Scraper -2 Page Navigation
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TM 5-3805-296-23-2
0070
Table 1. 1275 Bowl Up Proportional Solenoid Diagnostic Codes Continued.
070
CID FMI
TEST OR INSPECTION
CORRECTIVE ACTION
1275-5 Bowl Up Solenoid Current
5. At MSD, check for active
1275-06 Bowl Up Solenoid
Below Normal Becomes Active
diagnostic code 1275-6 Bowl Up
Current Above Normal
Replace bowl up solenoid (WP 0436).
Solenoid Current Above Normal
Continued
Proceed to Test Step 6.
(WP 0008).
1275-6 Bowl Up Solenoid Current
Above Normal Remains Active
Proceed to Test Step 2.
Test Step 2. Test for Shorted
Implement Wiring Harness.
1. Turn ignition switch and battery
disconnect switch to OFF position
(TM 5-3805-296-10).
2. Disconnect connector F-C8
(WP 0012, Figure 146)
from connector AE-C5
(WP 0012, Figure 145).
3. Using digital multimeter
Continuity Replace implement wiring
(WP 0540), test for continuity
harness (WP 0349).
between connector F-C8
Proceed to Test Step 6.
terminal 6 (WP 0012, Figure 146)
No Continuity Proceed to step 4.
and all other terminals
in connector F-C8
(WP 0012, Figure 146).
4. Using digital multimeter
Continuity Replace implement wiring
(WP 0540), test for continuity
harness (WP 0349).
between connector F-C8
Proceed to Test Step 6.
terminal 6 (WP 0012, Figure 146)
No Continuity Proceed to Test
and ground.
Step 3.
Test Step 3. Test for Shorted Draft
Frame and Bowl Side Wiring
Harness.
1. Disconnect connector AE-C1
(WP 0012, Figure 144)
from connector E-C2
(WP 0012, Figure 143).
2. Using digital multimeter
Continuity Replace draft frame and
(WP 0540), test for continuity
bowl side wiring harness (WP 0348).
between connector AE-C1
Proceed to Test Step 6.
terminal 6 (WP 0012, Figure 144)
No Continuity Proceed to step 3.
and all other terminals
in connector AE-C1
(WP 0012, Figure 144).
3. Using digital multimeter
Continuity Replace draft frame and
(WP 0540), test for continuity
bowl side wiring harness (WP 0348).
between connector AE-C1
Proceed to Test Step 6.
terminal 6 (WP 0012, Figure 144)
No Continuity Proceed to Test
and ground.
Step 4.
0070-13


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