ARMY
TM 5-6115-612-12
MARINE CORPS TM 6115-12/7
AIR FORCE
T0 35C2-3-471-1
NAVY
AG-320B0-0MM-000
4-28. WIRING HARNESS. (cont)
e.
Installation.
(1) Feed wiring harness through
bulkhead and secure with grommet
plate. Refer to figure 4-48 for
grommet plate detail.
(2) Connect
connector P1 to
terminal J1 on GECM.
(3) Connect
connector
P16 to
terminal J16 on generator.
(4) Close
control
panel
and
secure with turnlock fasteners.
(5) Check for continuity between
negative (-) pin on J18 through wire
V102AK0 to
feedthrough
terminal.
Reading should show continuity and low
resistance.
(6) If readings do not show con-
tinuity,
r e p l a c e
slave
receptacle
(paragraph 4-29b).
(7) Install output/slave housing
access
cover
(3) and secure with
washers (2) and screws (1).
Torque to
24-36 inch pounds (2.7-4 Nm).
(8) Stow power cable on cable
support assembly.
(5) Close control panel access
door.
b. Removal.
(6) Install engine housing access
cover
secure
with
turnlock
fasteners.
WARNING
(7) Connect battery cable plug
connector to battery.
4-29. SLAVE RECEPTACLE.
Maintenance
of the slave receptacle (figure 4-16)
consists of testing and replacement.
a. Test.
(1) Remove power cable from cable
support assembly.
(2) Remove screws (1), washers
(2), and output/slave housing access
cover (3).
(3) Set multimeter to OHMS scale.
(4) Check for continuity between
positive (+) pin on slave receptacle
(J18)
through
wire
P103D0
to
feedthrough terminal.
Reading should
show continuity.
To prevent
battery is
performing
injury,
ensure that
disconnected before
maintenance
on
electrical components.
(1) Disconnect battery cable plug
connector from battery.
(2) Remove power cable from cable
support assembly.
(3) Remove screws (1), washers
(2),
and output/slave housing access
cover (3).
(4) Tag slave receptacle leads
(4).
Remove nuts (5), washers (6), and
leads from feedthrough terminals (7).
(5) Remove screws (8), washers
(9), self-locking nuts (10), and slave
receptacle
(11)
from
output/slave
housing (12).
4-72
