TM 55-3810-01-165-14
LEGEND: C-130 AIRCRAFT
10,000-POUND-CAPACITY TIEDOWN FITTING
25,000-POUND-CAPACITY TIEDOWN FITTING
NOTE: FLOOR TIEDOWN FITTINGS ARE LOCATED IN ROWS A THROUGH G AND COLUMNS 1 THROUGH 25.
THE RAMP HAS 5 ADDITIONAL COLUMNS. THIS IS A TYPICAL TIEDOWN PROCEDURE AND ONLY
COLUMNS 1 THROUGH 25 ARE SHOWN. ITEM BEING SHIPPED CAN BE TIED DOWN AT ANY
LOCATION APPROVED BY THE LOADMASTER.
4-l. Tiedown diagram for the 7-ton rough-terrain cranein C-130 aircraft.
Figure
g. For airdrop of the Koehring 7-ton type II
available, use the crane's lifting device. All lifting
crane, rig the crane acording to FM 10-548/TO 13C7-
device components (mast, post, lift arms, and truss
24-21. Then the 7-ton type II crane can be suc-
rods) are stowed on the type II crane with pin con-
cessfully delivered by LAPES and LVAD from a C-
nection (figs 2-2, 4-2, and 4-3). All tools, extension
130 and by LVAD from a C-141B.
hoses, and accessories required for disassembly and
reassembly are stowed in the carrier tool box on the
left-hand side (fig 4-3). When the type II crane is
sectionalized into two separate loads, the weight of
WARNING
each section should be according to paragraph 2-4.
Any additional components, when added to the car-
Use extreme caution during the removal and
rier, that will affect the total weight or flight charac-
installation of the upper structure from and
teristics may affect helicopter transport.
onto the carrier. The lifting apparatus (part
of the sectionalization equipment) allows
Sectionalization and rigging of crane must follow the
procedures given in the Koehring Commercial Oper-
free rotation of the upper structure after
ation Instructions. This manual contains all sec-
lifting it from the carrier. During this rota-
tion, the upper structure should be under
tionalized instructions. The maintenance manual is
control; if not under control, it can cause
separate and is entitled "Koehring Commercial Main-
injury to personnel and damage to the
tenance Instructions". The type II crane, when sec-
crane.
tionalized for helicopter transport, is within the
For helicopter external air transport (EAT) of the
lifting capability of the CH-47 helicopter. The carrier
type II crane, remove the boom assembly (upper
unit or upper structure can be transported by CH-47
as a single- or dual-point load, as shown in figures 4-4
3). If a suitable size crane (l0-ton or larger) is not
through 4-7.
