ARMY
TM 5-6115-612-34
MARINE CORPS TM 6115-34/8
AIR FORCE
TO 35C2-3-471-2
NAVY
AG-320BO-MME-OOO
3-10.
ENGINE HOUSING. (cont)
c.
Installation. (cont)
(18) Install
exhaust
plenum
access cover and secure with turnlock
fasteners.
(19) Install
engine
housing
access cover and secure with turnlock
fasteners.
(20) Close
inlet
air
housing
access door.
(21) Connect battery cable plug
connector to battery.
(22) Fill
oil
reservoir
(paragraph 4-8b, TM 5-6115-612-12).
3-11.
ENGINE SUPPORT ASSEMBLY.
a.
Removal.
(1) Ensure that MASTER SWITCH is
in OFF position.
WARNING
To prevent injury, ensure that
battery is
disconnected before
performing maintenance on elec-
trical components.
(2) Disconnect battery cable plug
connector from battery.
(3) Remove engine in accordance
with paragraph 2-7a.
Do not disconnect
lifting device.
(4) Maintain
light
strain on
lifting device.
(5) Remove capscrew (1, figure
3-2),
self-locking nut (2),
washers
(3), resilient mount (4), spacer (5),
and resilient mount (6) to free engine
support (7) from engine mount plate
(10).
(6) Remove capscrews (8), lock-
washers (9),
engine mount plate (10),
and rear spacer (11) from bottom of
combustion chamber case.
(7) Remove capscrew (12), nuts
(13), washers (14), ground strap (15),
resilient mounts (16), spacers (17),
and
resilient mounts (18) to free
engine support (19) from engine mounts
(22).
(8) Remove
capscrews
(20),
lockwashers (21), and engine mounts
(22) from sides of gearbox.
b. Repair.
(1) Weld cracks and holes.
(2) Remove dents and straighten
bent sections.
(3) Remove corrosion and chipped
paint.
Prime and
repaint
affected
areas.
(4) Replace resilient mounts if
dry or cracked, or if damaged by fuel/
oil contamination.
c.
Installation.
(1) Install engine mounts (22) on
sides of gearbox and secure with lock-
washers
(21),
and
capscrews
(20).
Torque
to 100-140
inch
pounds
(11.3-15.8 Nm).
3-12
