ARMY TM 9-6115-672-14
AIR FORCE TO 35C2-3-444-32
MARINE CORPS TM 09244A/09245A-14
4-103
4.8.16 Computer Interface Module (CIM).
a. Inspection.
(1)
Shut down Generator set, Paragraph 2.11.2
(2)
Remove DCS control box top panel, paragraph 4.7.2.
(3)
Inspect CIM (3, Figure 4-14) for cracks, corrosion, dents, or other damage.
(4)
Install DCS control box top panel, paragraph 4.7.2.
b. Removal.
(1)
Shut down generator set, paragraph 2.11.2.
(2)
Open BATTERY ACCESS door (Figure 1-2), and disconnect negative battery cable.
(3)
Remove DCS control box top panel, paragraph 4.7.2.
CAUTION
CIM has two multi-pin electrical connectors. Pins can be damaged or broken if
connectors are pulled from or inserted in CIM sockets at an angle. Use care
when connecting or disconnecting wiring harnesses from CIM. Failure to
comply can cause damage to equipment and malfunction of the CIM.
NOTE
CIM has two connectors from the CIM wiring harness. The smaller connector
provides power to the CIM. The large connector is for data exchange. Both
connectors are secured in place with fasteners.
(4)
Loosen two screws, and disconnect power connector (25, fig 4-14) from CIM.
(5)
Loosen two thumbscrews, and disconnect data connector (24) from CIM.
CAUTION
CIM is mounted in DCS control panel frame suspended by mounting
hardware. If mounting hardware is removed without support being provided
for the CIM, the CIM and frame may be damaged. Have an assistant support
CIM during removal. Failure to comply can cause damage to equipment.
(6)
While providing adequate support for CIM, remove bolts (2) and CIM (3) from DCS control panel
frame (4).
(7)
If necessary, drill out rivet nuts (1) from DCS control panel frame.
c. Installation.
(1)
If removed, install rivet nuts (1, Figure 4-14) with rivet gun.
