ARMY TM 9-6115-672-14
AIR FORCE TO 35C2-3-444-32
MARINE CORPS TM 09244A/09245A-14
c. Close engine compartment doors.
d. Release DCS control panel by turning two fasteners, and lower DCS control panel slowly.
e. Ensure FREQUENCY SELECT switch (10) is in required position.
Ensure VOLTAGE SELECTION switch (9) is set to match voltage requirements.
g. Raise and secure DCS control panel with two fasteners.
If software fails to boot properly, notify next higher level of maintenance.
h. Place MASTER CONTROL switch (12) in ON position. While DCS software is loading and running
its diagnostics on CIM, perform steps i through m.
Open output box access door (Figure 1-2).
Ensure voltage reconnection terminal board (27, Figure 1-30) is positioned to match voltage
requirements. If voltage reconnection board must be changed, notify next higher level of maintenance.
k. Close output box access door.
Ensure EMERGENCY STOP switch (2, Figure 2-8) is pulled out.
m. Ensure BATTLE SHORT switch (4) is in OFF position.
n. Ensure NETWORK FAILURE indicator (3) on DCS control panel goes out when DCS software has
finished loading and is displayed on CIM display screen as shown in Figure 2-2. If NETWORK
FAILURE indicator is still illuminated, use keypad to exit software, place MASTER CONTROL
switch (12) in OFF position and panel light switch (16) is in off position, and notify next higher level of
2.10.3 Self Test.
a. Place ENGINE CONTROL switch (6) in PRIME & RUN position.
b. Hold FAULT RESET switch (14) in ON position for two seconds. Release switch. FAULT
INDICATOR and MESSAGES portions of CIM display screen should be blank unless a fault condition
c. Use arrow buttons on keypad to move cursor to DISPLAY MODE portion of CIM display screen. Use
SELECT button to alternately click MAIN / FULL button to ensure MAIN screen and FULL screen
d. Push PRESS TO TEST pushbutton on NETWORK FAILURE INDICATOR (3). Ensure indicator
light illuminates. When pushbutton is released, indicator light should go out.