TM
55-1730-229-12
AG
320AO-OMM-000
TO
35C2-3-473-1
TM
1730-12/1
(4) Hookup is as follows: Hookup
team should kneel on top of load. Assistant
hookup person discharges static electricity
with the static probe. Hookup person then
places apex on the aircraft cargo hook. If per-
forming dual-point hookup, the front sling leg
apex should be hooked first to aircraft cargo
hook No. 1 and the rear sling leg apex should
be hooked to aircraft cargo hook No. 3. Both
persons carefully dismount but remain close
to the load as helicopter removes slack in sl-
ing legs. When successful hookup is assured,
hookup team briskly exits the area
underneath the helicopter.
AFTER
MOVEMENT.
Refer to paragraph 4-2.
Figure 4-2A. Airlift Hookup
Section III. REPAIR PARTS; SPECIAL TOOLS; SPECIAL TEST;
MEASUREMENT AND DIAGNOSTIC EQUIPMENT (TMDE); AND SPECIAL SUPPORT EQUIPMENT
pair parts and equipment are listed and
tools, TMDE or support equipment re-
illustrated in the repair parts and
quired for organizational maintenance of
special tools list manual TM 55-1730-
the AGPU is as follows:
229-24P covering organizational main-
Oil drain fitting/hose, part
tenance for the AGPU.
number DB 75-108 (TEDESLO)
LUBRICATION INSTRUCTIONS
Section IV.
4-8. GENERAL. Army personnel should
a. Engine Oil Change. (See figure
refer to DA Pam 310-1 and Marine Corps
personnel to SL-1-3 to ensure the latest
edition of LO is used.
(1) Start and operate engine for
15 minutes, then shutdown engine and
Lubrication instructions for the AGPU
proceed with oil change while oil is
are contained in LO 55-1730-229-12.
hot.
