ARMY
T M 5 - 6 1 1 5 - 6 1 2 - 34
MARINE CORPS TM 6115-34/8
AIR FORCE
TO 35C2-3-471-2
NAVY
AG-320B0-MME-000
10-2.
ENGINE
ELECTRONIC
CONTROL
MODULE (EECM). (cont)
Figure 10-5.
EECM Connectors (Back) Wire Connections
(c) Connect wiring to multiple
(e) Pull
contactor
out of
ground terminals. Remove tags.
cover.
Tag and disconnect wiring from
contactor.
(d) Place
bottom
cover
(3,
figure 10-2) on EECM and secure with
(f) Remove diode CR2 (8).
washers (2) and screws (1).
Torque to
10-12 inch pounds (1.1-1.4 Nm).
(g) Remove
grommet
(9) if
damaged.
g.
Contactor Replacement.
(1) Removal.
(2) Ins tallation.
(a) Place EECM so that bottom
(a) Press
grommet
(9)
into
cover faces up.
contactor cover (3).
(b) Remove screws (1, figure
(b) Install diode CR2 (8).
10-2), washers (2), and cover (3).
(c) Connect wiring to contactor
(c) Remove screws (1, figure
(7).
Remove tags.
10-7), washers (2), and contactor cover
(3).
(d) Position contactor in con-
(d) Remove screws (4), lock-
tactor cover and secure with washers
washers (5), and washers (6) that
(6), lockwashers (5), and screws (4).
secure contactor (7) in contactor cover.
Torque to 3-4 inch pounds (0.3-0.5 Nm).
10-21
