FM 10-450-4 MULTISERVICE HELICOPTER SLING LOAD: SINGLE-POINT LOAD RIGGING PROCEDURES (September 2003) - page 11

 

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FM 10-450-4 MULTISERVICE HELICOPTER SLING LOAD: SINGLE-POINT LOAD RIGGING PROCEDURES (September 2003) - page 11

 

 

C3, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.3A
RIGGING STEPS
1. Position the apex fitting on the roof of the container.
3. Loop the chain end of sling leg 3 through the left rear
Route outer sling legs 1 and 2 to the front of the container
lift provision located on the left rear corner of the con-
and inner sling legs 3 and 4 to the rear. Sling legs 1 and 3
tainer. Place the correct link from Table 11-11 in the grab
must be on the left side of the load.
hook. Repeat with sling leg 4 through the right rear lift
provision.
2. Loop the chain end of sling leg 1 through the left
front lift provision located on the left front corner of the
4. Secure all excess chain with tape or Type III nylon
container . Place the correct link from Table 11-11 in the
cord.
grab hook. Repeat with sling leg 2 through the right front
lift provision.
5. Cluster and tie or tape (breakaway technique) all sling
legs together on top of the container to prevent entangle-
ment during hookup and lift-off.
Figure 11-11. Quadcons
11-22
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
CHAPTER 12
CERTIFIED SINGLE-POINT RIGGING PROCEDURES FOR RADAR AND
SATELLITE EQUIPMENT
12-1. Introduction
This chapter contains rigging procedures for single-point
equipment are in this section. Paragraphs 12-2 through
lift of radar and satelite equipment that has been certified
12-12 give detailed instructions for rigging loads.
for sling load. Each rigging procedure is found in a para-
graph that includes a description of the load, materials
NOTE: Reach Pendants may be used on all single point
required for rigging, and steps to complete the procedure.
loads. A static discharge person is not required when
An applicability paragraph is also a part of each para-
using a Reach Pendant.
graph and identifies the certified loads. The certified
single-point rigging procedures for radar and satellite
12-2. AN/TPQ-37 Artillery-Loading Radar Set (Firefinder)
a. Applicability. The following item in Table 12-1 is certified for all helicopters with suitable lift capacity by the US
Army Soldier Systems Center:
Table 12-1. AN/TPQ-37 Artillery-Loading Radar Set (Firefinder)
M AX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGH T
SLING SET
AIRSPEE D
FRONT/REA R
(POUNDS )
(KNOTS )
AN/TPQ-37 Artillery-Loading Radar
10,800
24K
68/5
90
Set (Firefinder)
b. Materials. The following materials are required to
c. Personnel. Two persons can prepare and rig this
rig this load:
load in 30 minutes.
(1) Sling set (25,000-pound capacity).
d. Procedures. The following procedures apply to this
load:
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(1) Preparation. Prepare the load using the following
steps:
(3) Cord, nylon, Type III, 550-pound breaking strength.
(a) Antenna unit should be configured for march
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
order. If the antenna unit is mounted on its transport
strength.
trailer, it must be removed for sling loading. If the trailer is
to accompany the unit, it must be rigged and moved as a
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
separate load.
substitute.
(b) Ensure the maintenance tent frame and cover are
(6) Ladder.
stowed and secured in their proper position.
12-1
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
(c) Ensure all cover panels, cabinet doors, and vents
(3) Hookup. The hookup team remains close to the
are installed and secured.
load as the helicopter removes slack from the sling legs.
When successful hookup is assured, the hookup team
(d) Secure all loose items with Type III nylon cord.
quickly exits the area underneath the helicopter to the
designated rendezvous point.
(e) Ensure the rear door is closed and secured with
the locking handle. Door rods must be secured in their
NOTE: Hookup is accomplished by the flight engineer
clips.
using a cargo-hook loading pole (Shepard's Hook). En-
sure the helicopter crew is informed of this in advance.
(f) Ensure the antenna transport cover is secured
tightly to the lacing brackets with bungee cord. If neces-
(4) Derigging. Derigging is the reverse of the prepa-
sary, secure the antenna with additional nylon cord.
ration and rigging procedures in steps d (1) and d (2).
(2) Rigging. Rig the load according to the steps in
NOTE: Advise the pilot to hover to one side before releas-
Figure 12-1.
ing the apex fitting from the cargo hook .
CAUTION
Do not stand on top of the load. Use the
ladder to connect the sling legs to the load.
12-2
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Open the access holes in the antenna transport cover
provision. Secure the excess chain with Type III nylon
as necessary to reach the lifting rings.
cord.
2. Rotate the antenna tie-down bolt ratchet handles
5. Loop the chain end of sling leg 3 through the left rear
toward the center of the trailer to prevent sling interfer-
lift ring. Ensure the chain is routed through the slot on the
ence.
top of the corner post. Place the correct link from Table
12-1 in the grab hook. Repeat with sling leg 4 on the right
3. Position apex fitting on top of the load. Route outer
rear lift ring. Pad the chain legs where they contact the
sling legs 1 and 2 to the front of the unit and inner sling
top of the corner post. Secure the padding with tape or
legs 3 and 4 to the rear (door end). Sling legs 1 and 3 must
Type III nylon cord.
be on the left side of the load.
6. Close and securely fasten the opening in the rear of
4. Loop the chain end of sling leg 1 through the left
the antenna transport cover.
front lift ring. Place the correct link from Table 12-1 in the
grab hook. Repeat with sling leg 2 on the right front lift
7. Cluster and tie or tape (breakaway technique)
all sling legs together on top of the unit to prevent en-
tanglement during hookup and lift-off.
Figure 12-1. AN/TPQ-37 Artillery-Loading Radar Set (Firefinder)
12-3
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
12-3. AN/TMQ-31 Radio Direction Finder
a. Applicability. The following item in Table 12-2 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 12-2. AN/TMQ-31 Radio Direction Finder
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
AN/TMQ-31 Radio Direction Finder,
5,010
10K
3/22
90
Pedestal Mounted on M103A3 Trailer
b. Materials. The following materials are required to
intervehicular cable to the tongue of the trailer with tape
rig this load:
or Type III nylon cord.
(1) Sling set (10,000-pound capacity).
(c) Engage the trailer hand brakes.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(d) Remove the canvas cover and secure it on top of
roll.
the ladder with Type III nylon cord.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(e) Fold the canvas bows down and secure them to
the trailer deck with Type III nylon cord.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(2) Rigging. Rig the load according to the steps in
Figure 12-2.
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
substitute.
(3) Hookup. The hookup team stands on the plat-
form to the rear of the radar. The static wand person
c. Personnel. Two persons can prepare and rig this
discharges the static electricity with the static wand. The
load in 30 minutes.
hookup person places the apex fitting onto the aircraft
cargo hook. The hookup team then moves clear of the
d. Procedures. The following procedures apply to this
load but remains close to the load as the helicopter re-
load:
moves slack from the sling legs. When successful hookup
is assured, the hookup team quickly exits the area under-
(1) Preparation. Prepare the load using the following
neath the helicopter to the designated rendezvous point.
steps:
(4) Derigging. Derigging is the reverse of the prepa-
(a) Place the radar set in the travel mode.
ration and rigging procedures in steps d (1) and d (2).
(b) Secure the air hoses, safety chains, and
NOTE: Advise the pilot to hover to one side before releas-
ing the apex fitting from the cargo hook .
12-4
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position apex fitting on top of the trailer. Route outer
3. Loop the chain end of sling leg 3 through the left rear
sling legs 1 and 2 to the front of the trailer and inner sling
lift ring located on the left rear corner of the trailer. Place
legs 3 and 4 to the rear. Sling legs 1 and 3 must be on the
the correct link from Table 12-2 in the grab hook. Repeat
left side of the load.
with sling leg 4 on the right rear lift ring. Secure the excess
chain with tape or Type III nylon cord.
2. Loop the chain end of sling leg 1 through the left
front lift ring located on the front left corner of the trailer.
4. Cluster and tie or tape (breakaway technique)
Place the correct link from Table 12-2 in the grab hook.
all sling legs together on top of the unit to prevent en-
Repeat with sling leg 2 on the right front lift provision.
tanglement during hookup and lift-off.
Figure 12-2. AN/TMQ-31 Radio Direction Finder
12-5
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
12-4. AN/TPQ-36 Firefinder Antenna Radar Set
a. Applicability. The following item in Table 12-3 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 12-3. AN/TPQ-36 Firefinder Antenna Radar Set
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
AN/TPQ-36 Firefinder Antenna Radar
4,110
10K
16/11
110
Set on M103A1 Trailer
b. Materials. The following materials are required to
(b) Close and secure the doors with Type III nylon
rig this load:
cord.
(1) Sling set (10,000-pound capacity).
(c) Place the radar set in the travel mode.
(2) Multiloop line, 9-foot, Type XXVI, nylon (4 each).
(d) Secure the cover on the antenna.
(3) Tape, adhesive, pressure-sensitive, 2-inch wide
(e) Attach a medium clevis to each rear lift points.
roll.
(2) Rigging. Rig the load according to the steps in
(4) Cord, nylon, Type III, 550-pound breaking strength.
Figure 12-3.
(5) Webbing, cotton, 1/4-inch, 80-pound breaking
NOTE: The radar panels cannot support any extra weight.
strength.
(3) Hookup. The hookup team stands on the fend-
(6) Clevis assembly, medium (2 each).
ers of the unit. The static wand person discharges the
static electricity with the static wand. The hookup person
(7) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
places the apex fitting onto the aircraft cargo hook. The
substitute.
hookup team then moves clear of the load but remains
close to the load as the helicopter removes slack from the
c. Personnel. Two persons can prepare and rig this
sling legs. When successful hookup is assured, the
load in 20 minutes.
hookup team quickly exits the area underneath the heli-
copter to the designated rendezvous point.
d. Procedures. The following procedures apply to this
load:
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
(1) Preparation. Prepare the load using the following
steps:
NOTE: Advise the pilot to hover to one side before releas-
ing the apex fitting from the cargo hook .
(a) Engage the trailer hand brakes.
12-6
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Connect a 9-foot multiloop line to the left rear clevis.
4. Loop the chain end of sling leg 1 through the multiloop
Place the multiloop line in the sling guide of the antenna,
line attached to the left side of the tongue. Place the
pull up until tight, and tape the line to the sling guide.
correct link from Table 12-3 in the grab hook. Repeat with
Repeat the procedure on the right side.
sling leg 2 on the right front lift provision. Secure the
excess chain with tape or Type III nylon cord.
2. Wrap the left side of the A-frame, aft of the lunette,
with padding and secure it in place with tape. Choker-
5. Loop the chain end of sling leg 3 through the multiloop
hitch a 9-foot multiloop line around the padded area. Re-
line attached to the left rear lift provision. Place the cor-
peat the procedure on the right side.
rect link from Table 12-3 in the grab hook. Repeat with
sling leg 4 on the right rear lift provision. Secure the
3. Position apex fitting on top of the trailer (not on top
excess chain with tape or Type III nylon cord.
of the radar panel). Route outer sling legs 1 and 2 to the
front of the trailer and inner sling legs 3 and 4 to the rear.
6. Cluster and tie or tape (breakaway technique)
Sling legs 1 and 3 must be on the left side of the load.
all sling legs together on top of the unit to prevent en-
tanglement during hookup and lift-off.
Figure 12-3. AN/TPQ-36 Firefinder Antenna Radar Set
12-7
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
12-5. AN/TPQ-36 Firefinder II
a. Applicability. The following item in Table 12-4 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 12-4. AN/TPQ-36 Firefinder II
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Firefinder II, AN/TPQ-36 Block II
9,673
25K
11/3
120
b. Materials. The following materials are required to
matching similar sections to form a long (117-inch) and a
rig this load:
short (91.8-inch) spreader bar.
(1) Sling set (25,000-pound capacity) with four addi-
(b) Prepare the Firefinder II for transport in accor-
tional chain lengths and coupling links.
dance with operator’s manual.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(c) Secure all loose equipment on the pallet with tape
roll.
or nylon cord.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(d) Ensure all latches, doors, and panels are secured
with tape or nylon cord.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(e) Using the two tie-down straps, secure the an-
tenna cover to the antenna array. Route the tie-down
(5) Tie-down straps, cargo, CGU-1/B (2 each).
straps from front to rear.
(6) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
(f) Place the long (117-inch) spreader bar on top of
substitute.
the shelter roof. Position the bar (parallel with the side of
the shelter) between the edge of the shelter that is adja-
(7) Spreader bar assemblies, 117 inches and 91.8 inches
cent to the antenna array and the radio mount on the
in length (components of the Firefinder II).
shelter roof. Secure the spreader bar loosely in place (al-
low adequate slack for movement) with nylon cord to pre-
c. Personnel. Two persons can prepare and rig this
vent the spreader bar from rolling off the shelter roof.
load in 30 minutes.
(g) Place the short (91.8-inch) spreader bar through
d. Procedures. The following procedures apply to this
the opening in the antenna array support arms directly
load:
below the antenna array as indicated in the illustration.
Secure the spreader bar loosely in place with nylon cord
(1) Preparation. Prepare the load using the following
to prevent the spreader bar from sliding out of the open-
steps:
ings in the support arms.
NOTE: Do not stand on the surface of the antenna array
(2) Rigging. Rig the load according to the steps in
at any time.
Figure 12-4.
(a) Assemble the two spreader bar assemblies by
(3) Hookup. The hookup team stands on top of the
12-8
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
shelter. The static wand person discharges the static elec-
(4) Derigging. Derigging is the reverse of the prepa-
tricity with the static wand. The hookup person places
ration and rigging procedures in steps d (1) and d (2).
the apex fitting onto the aircraft cargo hook. The hookup
team then moves clear of the load but remains close to the
NOTE: Brief the helicopter crew to relax sling leg ten-
load as the helicopter removes slack from the sling legs.
sion, lower the spreader bars onto the shelter roof and
When successful hookup is assured, the hookup team
antenna array support arms, and hover to the side of the
quickly exits the area underneath the helicopter to the
load when releasing the sling set.
designated rendezvous point.
Figure 12-4. AN/TPQ-36 Firefinder II
12-9
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position apex fitting on top of the shelter. Route
below the generator engine and back up through the
outer sling legs 1 and 2 to the front (shelter end) of the
spreader bar end fitting. Pull the chains tight to remove
load and inner sling legs 3 and 4 to the rear (generator
slack. Place the correct link from Table 12-4 in the grab
end). Sling legs 1 and 3 must be on the left side of the
hook. Install the retaining pin in the end of the spreader
load.
bar. Repeat with sling leg 4 through the right end fitting
on the spreader bar and lift provision on the right side of
2. Using the proper coupling links, add the chain exten-
the pallet frame.
sions to each sling leg chain assembly.
NOTE: The chain links do not lock in the end fittings on
3. Route the chain end of sling leg 1 through the fitting
the short spreader bar like they do on the long spreader
on the left end of the long spreader bar and down the side
bar.
of the shelter. Insert link 10 (counting down from the grab
hook coupling link) in the spreader bar end fitting. Route
5. Tape the two loops of the chain legs together every 1
the chain end through the lift provision located on the left
to 2 feet. Secure all excess chain with tape or nylon cord.
side of the pallet frame, back up to the spreader bar, and
Place padding around the grabhooks and secure with tape
insert link 23 in the end fitting. Secure the chain in the end
or nylon cord to prevent damage caused by the grabhooks
fitting by installing the retaining pin in the end of the
when the sling is released.
spreader bar. Place the correct link from Table 12-4 in the
grab hook. Repeat with sling leg 2 through the right end
6. Pull the rear sling legs 3 and 4 tight over top of the
fitting on the spreader bar, and lift provision on the right
antenna array to remove slack from the sling legs. Cluster
side of the pallet frame.
and tie or tape (breakaway technique) the sling legs to-
gether to prevent the chains and grabhooks from fouling
4. Route the chain end of sling leg 3 through the fitting
on the antenna array during hookup and lift-off.
on the left end of the short spreader bar and down the side
of the antenna array assembly. Route the chain end through
7. Cluster and tie or tape (breakaway technique) the
the lift provision located on the left side of the pallet frame
front sling legs 1 and 2 together on top of the shelter to
prevent entanglement during hookup and lift-off.
Figure 12-4. AN/TPQ-36 Firefinder II (continued)
12-10
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
12-6. OE-361/G Quick Reaction Satellite Antenna
a. Applicability. The following item in Table 12-5 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 12-5. OE-361/G Quick Reaction Satellite Antenna
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Antenna, Satellite, Quick Reaction
4,830
10K
3/30
80
(QRSA), OE-361/G
b. Materials. The following materials are required to
available material to prevent possible damage from the
rig this load:
apex clevis at load release. Tape or tie the padding se-
curely to prevent it from being dislodged during flight.
(1) Sling set (10,000-pound capacity).
(d) Ensure the ladder, box covers, and any other
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
loose items are properly secured. If the tie-down straps
roll.
are missing or worn, replace with nylon cord.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(2) Rigging. Rig the load according to the steps in
Figure 12-5.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(3) Hookup. The hookup team stands on top of the
load between the stacked antenna panels and either side
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
of the center post. The static wand person discharges the
substitute.
static electricity with the static wand. The hookup person
places the apex fitting onto the aircraft cargo hook. The
c. Personnel. Four persons can prepare and rig this
hookup team then moves clear of the load but remains
load in 30 minutes.
close to the load as the helicopter removes slack from the
sling legs. When successful hookup is assured, the
d. Procedures. The following procedures apply to this
hookup team quickly exits the area underneath the heli-
load:
copter to the designated rendezvous point.
(1) Preparation. Prepare the load using the following
(4) Derigging. Derigging is the reverse of the prepa-
steps:
ration and rigging procedures in steps d (1) and d (2).
(a) Install the spreader bar assembly which is stored
CAUTION
on the load. After hooking the spreader bar assembly to
Brief the helicopter crew to relax sling leg ten-
the lift rings, tape the keepers securely with tape.
sion, lower the spreader bars onto the shelter
roof and antenna array support arms, and
(b) Pad both spreader bars with felt or other cush-
ioning material to prevent damage to the antenna panels
hover to the side of the load when releasing
during load release. Tape or tie the padding securely to
the sling set.
prevent it from being dislodged during flight.
(c) Pad the uppermost stacked antenna panel with
12-11
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position the apex fitting on top of the load. Route
the right lift eye on the rear spreader bar. Secure excess
outer sling legs 1 and 2 to the front (ladder end) of the load
chain with tape or nylon cord.
and inner sling legs 3 and 4 to the rear. Sling legs 1 and 3
must be on the left side of the load.
4. Wrap felt padding or other suitable cushioning mate-
rial around each grab hook assembly to protect the an-
2. Loop the chain end of sling leg 1 through the left lift
tenna when the sling set is released. Tape or tie the pad-
eye of the front spreader bar. Place the correct link from
ding securely to prevent it from being dislodged during
Table 12-5 in the grab hook. Repeat with sling leg 2 and
flight.
the right lift eye on the front spreader bar.
5. Cluster and tie or tape (breakaway technique) all sling
3. Loop the chain end of sling leg 3 through the left lift
legs together on top of the antenna to prevent entangle-
eye of the rear spreader bar. Place the correct link from
ment during hookup and lift-off.
Table 12-5 in the grab hook. Repeat with sling leg 4 and
Figure 12-5. OE-361/G Quick Reaction Satellite Antenna
12-12
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
12-7. AS-3471/TPN-22 Antenna Pallet (USMC)
a. Applicability. The following item in Table 12-6 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 12-6. AS-3471/TPN-22 Antenna Pallet (USMC)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Antenna Pallet, AN-3471/TPN-22
5,700
40K
3/5
80
TAMCN Q2115
b. Materials. The following materials are required to
steps:
rig this load:
(a) Secure all handles.
(1) Sling set (40,000-pound capacity) with four addi-
tional chain lengths and coupling links.
(b) Secure the crank handle at the base of the pallet.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(c) Add the additional chain length to each leg of the
roll.
sling set using the coupling links.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(2) Rigging. Rig the load according to the steps in
Figure 12-6.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(3) Hookup. The hookup team stands on the pallet.
The static wand person discharges the static electricity
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
with the static wand. The hookup person places the apex
substitute.
fitting onto the aircraft cargo hook. The hookup team
then moves clear of the load but remains close to the load
c. Personnel. Four persons can prepare and rig this
as the helicopter removes slack from the sling legs. When
load in 15 minutes.
successful hookup is assured, the hookup team quickly
exits the area underneath the helicopter to the designated
d. Procedures. The following procedures apply to this
rendezvous point.
load:
(4) Derigging. Derigging is the reverse of the prepa-
(1) Preparation. Prepare the load using the following
ration and rigging procedures in steps d (1) and d (2).
12-13
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position the apex fitting on top of the load. Route
space between the channel beams at the left rear base of
outer sling legs 1 and 2 to the front (supply box end) of the
the antenna. Place the correct link from Table 12-6 in the
load and inner sling legs 3 and 4 to the rear (leveling disk
grab hook. Repeat with sling leg 4 on the right rear base of
end). Sling legs 1 and 3 must be on the left side of the
the antenna.
load.
4. Tie or tape (breakaway technique) all chains loosely
2. Loop the chain end of sling leg 1 through the small
to the straps at the bumpers to prevent the chains from
space between the channel beams at the left front base of
moving off the protective bumpers.
the antenna. Place the correct link from Table 12-6 in the
grab hook. Repeat with sling leg 2 on the right front base
5. Cluster and tie or tape (breakaway technique) all sling
of the antenna.
legs together on top of the antenna to prevent entangle-
ment during hookup and lift-off.
3. Loop the chain end of sling leg 3 through the small
Figure 12-6. AS-3471/TPN-22 Antenna Pallet
12-14
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
12-8. Antenna Pallet Transit Frame
a. Applicability. The following items in Table 12-7 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 12-7. Antenna Pallet Transit Frame
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
SM-F 973604-1 used with
1,970
10K
30/3
75
AN/TSC-93B
SM-F 973604-21 used with
2,107
10K
30/3
75
AN/TSC-85B
b. Materials. The following materials are required to
(a) Secure all equipment with the eight ratchet straps
rig this load:
supplied. Use tape or Type III nylon cord if additional
security is required.
(1) Sling set (10,000-pound capacity).
(b) Remove and stow the protective cover. Secure
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
with Type III nylon cord.
roll.
(2) Rigging. Rig the load according to the steps in
(3) Cord, nylon, Type III, 550-pound breaking strength.
Figure 12-7.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(3) Hookup. The hookup team stands on the frame.
strength.
The static wand person discharges the static electricity
with the static wand. The hookup person places the apex
c. Personnel. Four persons can prepare and rig this
fitting onto the aircraft cargo hook. The hookup team
load in 10 minutes.
then moves clear of the load but remains close to the load
as the helicopter removes slack from the sling legs. When
d. Procedures. The following procedures apply to this
successful hookup is assured, the hookup team quickly
load:
exits the area underneath the helicopter to the designated
rendezvous point.
(1) Preparation. Prepare the load using the following
steps:
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
12-15
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position the apex fitting on top of the load. Route
cord.
outer sling legs 1 and 2 to the front (opposite the antenna
segments) of the load and inner sling legs 3 and 4 to the
3. Loop the chain end of sling leg 3 through the left rear
rear . Sling legs 1 and 3 must be on the left side of the load.
lift provision. Place the correct link from Table 12-7 in the
grab hook. Repeat with sling leg 4 on the right rear lift
2. Loop the chain end of sling leg 1 through the left
provision.
front lift provision located on the top left corner of the
frame. Place the correct link from Table 12-7 in the grab
4. Cluster and tie or tape (breakaway technique) all sling
hook. Repeat with sling leg 2 on the top right corner of the
legs together on top of the frame to prevent entanglement
frame. Secure the excess chain with tape or Type III nylon
during hookup and lift-off.
Figure 12-7. Antenna Pallet Transit Frame
12-16
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
12-9. Digital Group Multiplexer (DGM), Digital Antenna Mast Program (DAMP), 2 and 3
Antenna Pallet Configurations
a. Applicability. The following items in Table 12-8 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 12-8. Digital Group Multiplexer (DGM), Digital Antenna Mast Program (DAMP)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
DGM, DAMP Pallet, 2 Antenna
4,300
10K
3/3
90
Configuration
DGM, DAMP Pallet, 3 Antenna
5,500
10K
3/3
90
Configuration
b. Materials. The following materials are required to
steps:
rig this load:
(a) Secure the grating on the cable reels side with
(1) Sling set (10,000-pound capacity).
Type III nylon cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(b) Secure the cable reels with Type III nylon cord.
roll.
(c) Wrap the tie-down straps and turnbuckles with
(3) Cord, nylon, Type III, 550-pound breaking strength.
padding and secure the padding with tape. Secure them
to the pallet with the rubber straps provided.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(2) Rigging. Rig the load according to the steps in
Figure 12-8.
(5) Webbing, tubular, nylon, 1/2-inch, 1000-pound
breaking strength.
(3) Hookup. The hookup team stands on the pallet.
The static wand person discharges the static electricity
(6) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
with the static wand. The hookup person places the apex
substitute.
fitting onto the aircraft cargo hook. The hookup team
then moves clear of the load but remains close to the load
c. Personnel. Four persons can prepare and rig this
as the helicopter removes slack from the sling legs. When
load in 20 minutes.
successful hookup is assured, the hookup team quickly
exits the area underneath the helicopter to the designated
d. Procedures. The following procedures apply to this
rendezvous point.
load:
(4) Derigging. Derigging is the reverse of the prepa-
(1) Preparation. Prepare the load using the following
ration and rigging procedures in steps d (1) and d (2).
12-17
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position the apex fitting on top of the load. Route
3. Loop the chain end of sling leg 3 through the left rear
outer sling legs 1 and 2 to the front (cable reel end) of the
lift provision. Place the correct link from Table 12-8 in the
load and inner sling legs 3 and 4 to the rear. Sling legs 1
grab hook. Repeat with sling leg 4 on the right rear lift
and 3 must be on the left side of the load.
provision.
2. Loop the chain end of sling leg 1 through the left
4. Cluster and tie or tape (breakaway technique) all sling
front lift provision located on the top left corner of the
legs together on top of the frame to prevent entanglement
frame. Place the correct link from Table 12-8 in the grab
during hookup and lift-off.
hook. Repeat with sling leg 2 on the top right corner of the
frame.
Figure 12-8. Digital Group Multiplexer (DGM), Digital Antenna Mast Program (DAMP)
12-18
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
12-10. Digital Group Multiplexer (DGM), Auxiliary Equipment Transportation Container
(AETC), 2 and 3 Mast Configurations
a. Applicability. The following items in Table 12-9 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 12-9. Digital Group Multiplexer (DGM), Auxiliary Equipment Transportation Container (AETC)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
DGM, AETC, 2 Mast Configuration
3,028
10K
3/3
100
DGM, AETC, 3 Mast Configuration
4,014
10K
3/3
100
b. Materials. The following materials are required to
(a) Secure all loose equipment inside the AETC with
rig this load:
tape or Type III nylon cord.
(1) Sling set (10,000-pound capacity).
(b) Remove and stow the AETC cover. Secure the
cover with Type III nylon cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(2) Rigging. Rig the load according to the steps in
Figure 12-9.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(3) Hookup. The hookup team stands on the AETC.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
The static wand person discharges the static electricity
strength.
with the static wand. The hookup person places the apex
fitting onto the aircraft cargo hook. The hookup team
c. Personnel. Four persons can prepare and rig this
then moves clear of the load but remains close to the load
load in 15 minutes.
as the helicopter removes slack from the sling legs. When
successful hookup is assured, the hookup team quickly
d. Procedures. The following procedures apply to this
exits the area underneath the helicopter to the designated
load:
rendezvous point.
(1) Preparation. Prepare the load using the following
(4) Derigging. Derigging is the reverse of the prepa-
steps:
ration and rigging procedures in steps d (1) and d (2).
12-19
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position the apex fitting on top of the load. Route
3. Loop the chain end of sling leg 3 through the left rear
outer sling legs 1 and 2 to the front of the load and inner
lift provision. Place the correct link from Table 12-9 in the
sling legs 3 and 4 to the rear. Sling legs 1 and 3 must be on
grab hook. Repeat with sling leg 4 on the right rear lift
the left side of the load.
provision.
2. Loop the chain end of sling leg 1 through the left
4. Cluster and tie or tape (breakaway technique) all sling
front lift provision. Place the correct link from Table 12-9 in
legs together on top of the AETC to prevent entangle-
the grab hook. Repeat with sling leg 2 on the top right
ment during hookup and lift-off.
corner of the frame.
Figure 12-9. Digital Group Multiplexer (DGM), Auxiliary Equipment Transportation Container (AETC)
12-20
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
12-11. Lightweight Generator Frame Assembly (AN/TSC-93B Reconfiguration) Satellite
Communications Terminal
a. Applicability. The following items in Table 12-10 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 12-10. Lightweight Generator Frame Assembly (AN/TSC-93B Reconfiguration)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
AN/TSC-98B Satellite
Communications Terminal without
3,644
10K
3/3
110
ALTA
AN/TSC-98B Satellite
3,957
10K
3/3
110
Communications Terminal with ALTA
b. Materials. The following materials are required to
(b) Remove and stow the cover. Secure the cover
rig this load:
with Type III nylon cord.
(1) Sling set (10,000-pound capacity).
(2) Rigging. Rig the load according to the steps in
Figure 12-10.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(3) Hookup. The hookup team stands on the frame
corners, diagonally across from each other. The static
(3) Cord, nylon, Type III, 550-pound breaking strength.
wand person discharges the static electricity with the static
wand. The hookup person places the apex fitting onto the
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
aircraft cargo hook. The hookup team then moves clear of
strength.
the load but remains close to the load as the helicopter
removes slack from the sling legs. When successful
(5) Tie-down strap, cargo, CGU-1/B (3 each).
hookup is assured, the hookup team quickly exits the area
underneath the helicopter to the designated rendezvous
c. Personnel. Four persons can prepare and rig this
point.
load in 10 minutes.
CAUTION
d. Procedures. The following procedures apply to this
Brief the helicopter crew to relax the sling leg
load:
tension and hover to the side of the load when
releasing the apex fitting.
(1) Preparation. Prepare the load using the following
steps:
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
(a) Secure all loose equipment with CGU-1/B tie-
down straps, tape, or Type III nylon cord.
12-21
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position the apex fitting on top of the load. Route
3. Loop the chain end of sling leg 3 through the left rear
outer sling legs 1 and 2 to the front of the load and inner
lift provision. Place the correct link from Table 12-10 in the
sling legs 3 and 4 to the rear. Sling legs 1 and 3 must be on
grab hook. Repeat with sling leg 4 on the right rear lift
the left side of the load.
provision.
2. Loop the chain end of sling leg 1 through the left
4. Cluster and tie or tape (breakaway technique) all sling
front lift provision. Place the correct link from Table 12-10
legs together on top of the load to prevent entanglement
in the grab hook. Repeat with sling leg 2 on the top right
during hookup and lift-off.
corner of the frame.
Figure 12-10. Lightweight Generator Frame Assembly (AN/TSC-93B Reconfiguration)
12-22
C1, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
12-12. Secure Mobile Anti-Jam Reliable Tactical Terminal (SMART-T) Pallet
a. Applicability. The following item in Table 12-11 is certified for all helicopters with suitable lift capacity by the US
Army Soldier Systems Center:
Table 12-11. Secure Mobile Anti-Jam Reliable Tactical Terminal (SMART-T) Pallet
M AX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGH T
SLING SET
AIRSPEE D
FRONT/REA R
(POUNDS )
(KNOTS )
Secure Mobile Anti-Jam Reliable
2,440
10K
3/30
100
T
actical Terminal (SMART-T) Pa
l
b. Materials. The following materials are required to
nylon cord. Ensure the fuel cans at the end of the pallet
rig this load:
are locked in position.
(1) Sling set (10,000-pound capacity).
(b) Secure the antenna dish.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(2) Rigging. Rig the load according to the steps in
roll.
Figure 12-11.
(3) Cord, nylon, Type III, 550-pound breaking strength.
NOTE: The fuel can brackets are on the rear of the load.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(3) Hookup. The hookup team stands beside the
strength.
pallet. The static wand person discharges the static elec-
tricity with the static wand. The hookup person places
c. Personnel. Four persons can prepare and rig this
the apex fitting onto the aircraft cargo hook. The hookup
load in 10 minutes.
team then moves clear of the load but remains close to the
load as the helicopter removes slack from the sling legs.
d. Procedures. The following procedures apply to this
When successful hookup is assured, the hookup team
load:
quickly exits the area underneath the helicopter to the
designated rendezvous point.
(1) Preparation. Prepare the load using the following
steps:
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
(a) Secure all loose equipment with tape or Type III
12-23
C1, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position the apex fitting beside the pallet. Route
3. Loop the chain end of sling leg 3 through the left rear
outer sling legs 1 and 2 to the front of the load and inner
lift provision. Place the correct link from Table 12-11 in the
sling legs 3 and 4 to the rear. Sling legs 1 and 3 must be on
grab hook. Repeat with sling leg 4 on the right rear lift
the left side of the load.
provision. Secure excess chain with tape or Type III ny-
lon cord.
2. Loop the chain end of sling leg 1 through the left
front lift provision. Place the correct link from Table 12-11
4. Cluster and tie or tape (breakaway technique) all sling
in the grab hook. Repeat with sling leg 2 on the top right
legs together on top of the load to prevent entanglement
corner of the frame.
during hookup and lift-off.
Figure 12-11. Secure Mobile Anti-Jam Reliable Tactical Terminal (SMART-T) Pallet
12-24
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
CHAPTER 13
CERTIFIED SINGLE-POINT RIGGING PROCEDURES FOR GENERATOR SETS
13-1. Introduction
This chapter contains rigging procedures for single-point
graphs 13-2 through 13-7 give detailed instructions for
lift of generator sets that have been certified for sling
rigging loads.
load. Each rigging procedure is found in a paragraph that
includes a description of the load, materials required for
NOTE: Reach Pendants may be used on all single point
rigging, and steps to complete the procedure. An applica-
loads. A static discharge person is not required when
bility paragraph is also a part of each paragraph and iden-
using a Reach Pendant.
tifies the certified loads. The certified single-point rigging
procedures for generator sets are in this section. Para-
13-2. Aviation Ground Power Unit (AGPU)
a. Applicability. The following item in Table 13-1 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 13-1. Aviation Ground Power Unit (AGPU)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Aviation Ground Power Unit
4,190
10K
3/3
90
b. Materials. The following materials are required to
c. Personnel. Two persons can prepare and rig this
rig this load:
load in 10 minutes.
(1) Sling set (10,000-pound capacity).
d. Procedures. The following procedures apply to this
load:
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(1) Preparation. Prepare the load using the following
steps:
(3) Cord, nylon, Type III, 550-pound breaking strength.
(a) Stow and secure the towbar with 1/2-inch tubular
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
nylon.
strength.
(b) Close all doors, secure handles with tape, and
(5) Tie-down strap, cargo, CGU-1/B (4 each).
attach four CGU-1/B tie-down straps.
(6) Webbing, nylon, tubular, 1/2-inch,1000-pound
(c) Route one tie-down strap horizontally around
breaking strength.
the power unit. Position it approximately 16 inches down
from the top of the power unit. Repeat using another tie-
13-1
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
down strap positioned approximately 8 inches higher than
(g) Ensure that fuel tank is not more than 3/4 full.
the first tie-down strap.
Inspect fuel tank cap, oil filler caps, and battery caps to
ensure they are secure.
(d) Route another tie-down strap through the forklift
lift provisions and then vertically around the power unit.
(h) Engage the parking brake.
Repeat this procedure using another tie-down strap
through the other lift provision.
(2) Rigging. Rig the load according to the steps in
Figure 13-1.
(e) Secure all equipment inside the unit with nylon
cord or tape.
(3) Hookup. The hookup team stands on top of the
power unit. The static wand person discharges the static
(f) Secure exhaust cover closed with tape.
electricity with the static wand. The hookup person places
the apex fitting onto the aircraft cargo hook. The hookup
CAUTION
team then moves clear of the load but remains close to the
load as the helicopter removes slack from the sling legs.
Pay careful attention to securing the exhaust
When successful hookup is assured, the hookup team
cover closed to preclude possible damage dur-
quickly exits the area underneath the helicopter to the
ing flight. If cover cannot be adequately se-
designated rendezvous point.
cured, it should be removed.
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
13-2
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position apex fitting on top of the unit. Route outer
3. Loop the chain end of sling leg 3 through the left rear
sling legs 1 and 2 to the front (tongue) of the trailer and
lift ring. Place the correct link from Table 13-1 in the grab
inner sling legs 3 and 4 to the rear. Sling legs 1 and 3
hook. Repeat with sling leg 4 on the right rear lift ring.
should be on the left side of the load.
4. Cluster and tie or tape (breakaway technique) all sling
2. Loop the chain end of sling leg 1 through the left
legs together on top of the unit to prevent entanglement
front lift ring. Place the correct link from Table 13-1 in the
during hookup and lift-off.
grab hook. Repeat with sling leg 2 on the right front lift
ring.
Figure 13-1. Aviation Ground Power Unit (AGPU)
13-3
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
13-3. Aviation Direct Current Generator Set (ADCGS)
a. Applicability. The following item in Table 13-2 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 13-2. Aviation Direct Current Generator Set (ADCGS)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Aviation Direct Current Generator Set
1,100
10K
3/3
90
b. Materials. The following materials are required to
hold-down latch on rear cable rack.
rig this load:
(b) Cover cable receptacles. Secure door latches
(1) Sling set (10,000-pound capacity).
and tape exhaust stack cover down.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(c) Route a single length of Type III nylon cord
roll.
under and through the frame, over the exhaust stack cover
and instrument cover, and tie to secure both covers. Tape
(3) Cord, nylon, Type III, 550-pound breaking strength.
the fuel tank gage.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(d) Set the wheel brakes in the ON position.
strength.
(2) Rigging. Rig the load according to the steps in
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
Figure 13-2.
substitute, 30- x 36-inch (4 sheets).
(3) Hookup. The hookup team stands on the side of
c. Personnel. Two persons can prepare and rig this
the load. The static wand person discharges the static
load in 20 minutes.
electricity with the static wand. The hookup person places
the apex fitting onto the aircraft cargo hook. The hookup
d. Procedures. The following procedures apply to this
team then moves clear of the load but remains close to the
load:
load as the helicopter removes slack from the sling legs.
When successful hookup is assured, the hookup team
(1) Preparation. Prepare the load using the following
quickly exits the area underneath the helicopter to the
steps:
designated rendezvous point.
(a) Fold and tape ground cable to the inside of the
(4) Derigging. Derigging is the reverse of the prepa-
tongue frame. Roll rear cable in the rack provided. Tape
ration and rigging procedures in steps d (1) and d (2).
13-4
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position apex fitting on top of the generator set. Route
3. Loop the chain end of sling leg 3 through the left rear
outer sling legs 1 and 2 to the front (tongue) of the trailer
lift provision. Place the correct link from Table 13-2 in the
and inner sling legs 3 and 4 to the rear. Sling legs 1 and 3
grab hook. Repeat with sling leg 4 on the right rear lift
should be on the left side of the load.
ring.
2. Loop the chain end of sling leg 1 through the left
4. Cluster and tie or tape (breakaway technique) all sling
front lift provision. Place the correct link from Table 13-2 in
legs together on top of the unit to prevent entanglement
the grab hook. Repeat with sling leg 2 on the right front
during hookup and lift-off.
lift ring.
Figure 13-2. Aviation Direct Current Generator Set (ADCGS)
13-5
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
13-4. Skid Mounted Generators
a. Applicability. The following items in Table 13-3 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 13-3. Skid Mounted Generators
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
MEP-004AAS with Acoustic
4,031
10K
3/3
40
Suppression Kit, 15KW
MEP-005AAS with Acoustic
4,556
10K
3/3
65
Suppression Kit, 30KW
MEP-103A with Acoustic Suppression
4,230
10K
3/3
40
Kit, 15KW
MEP-104A with Acoustic Suppression
4,830
10K
3/3
40
Kit, 30KW
MEP-113A with Acoustic Suppression
4,230
10K
3/3
40
Kit, 15KW
MEP-114A with Acoustic Suppression
4,830
10K
3/3
40
Kit, 30KW
b. Materials. The following materials are required to
steps:
rig this load:
(a) Remove two sling legs from the sling set.
(1) Sling set (10,000-pound capacity).
(b) Secure all lids, doors, and caps with tape or Type
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
III nylon cord.
roll.
(2) Rigging. Rig the load according to the steps in
(3) Cord, nylon, Type III, 550-pound breaking strength.
Figure 13-3.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(3) Hookup. The hookup team stands on top of the
strength.
load. The static wand person discharges the static elec-
tricity with the static wand. The hookup person places
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
the apex fitting onto the aircraft cargo hook. The hookup
substitute, 30- x 36-inch (4 sheets).
team then moves clear of the load but remains close to the
load as the helicopter removes slack from the sling legs.
c. Personnel. Two persons can prepare and rig this
When successful hookup is assured, the hookup team
load in 15 minutes.
quickly exits the area underneath the helicopter to the
designated rendezvous point.
d. Procedures. The following procedures apply to this
load:
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
(1) Preparation. Prepare the load using the following
13-6
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position apex fitting on top of the generator set. Route
grab hook. Repeat with the right sling leg on the right lift
the left sling leg to the left lift provision and the right sling
provision.
leg to the right lift provision.
3. Cluster and tie or tape (breakaway technique) all sling
2. Loop the chain end of left sling leg through the left
legs together on top of the unit to prevent entanglement
lift provision. Place the correct link from Table 13-3 in the
during hookup and lift-off.
Figure 13-3. Skid Mounted Generators
13-7
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
13-5. MEP112A Generator Pallet
a. Applicability. The following items in Table 13-4 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 13-4. MEP112A Generator Pallet
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
MEP813 TQG, Generator Pallet,
1,600
10K
7/3
70
Sentinel Radar System
MEP112A, Generator Pallet
2,150
10K
7/3
100
b. Materials. The following materials are required to
(a) Secure all chains and hoses with tape or Type III
rig this load:
nylon cord.
(1) Sling set (10,000-pound capacity).
(b) Secure all lids, doors, vents, and caps with tape
or Type III nylon cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(2) Rigging. Rig the load according to the steps in
Figure 13-4.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(3) Hookup. The hookup team stands on top of the
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
load. The static wand person discharges the static elec-
strength.
tricity with the static wand. The hookup person places
the apex fitting onto the aircraft cargo hook. The hookup
c. Personnel. Two persons can prepare and rig this
team then moves clear of the load but remains close to the
load in 15 minutes.
load as the helicopter removes slack from the sling legs.
When successful hookup is assured, the hookup team
d. Procedures. The following procedures apply to this
quickly exits the area underneath the helicopter to the
load:
designated rendezvous point.
(1) Preparation. Prepare the load using the following
(4) Derigging. Derigging is the reverse of the prepa-
steps:
ration and rigging procedures in steps d (1) and d (2).
13-8
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position apex fitting on top of the generator set. Route
3. Loop the chain end of sling leg 3 through the left rear
outer sling legs 1 and 2 to the front of the pallet and inner
lift provision. Place the correct link from Table 13-4 in the
sling legs 3 and 4 to the rear. Sling legs 1 and 3 should be
grab hook. Repeat with sling leg 4 on the right rear lift
on the left side of the load.
ring.
2. Loop the chain end of sling leg 1 through the left
4. Cluster and tie or tape (breakaway technique) all sling
front lift provision. Place the correct link from Table 13-4 in
legs together on top of the unit to prevent entanglement
the grab hook. Repeat with sling leg 2 on the right front
during hookup and lift-off.
lift ring.
Figure 13-4. MEP112A Generator Pallet
13-9
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
13-6. NATO Air Base Satcom (NABS) Power Pallet AN/TSC-85(V)2
a. Applicability. The following item in Table 13-5 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 13-5. NATO Air Base Satcom (NABS) Power Pallet AN/TSC-85(V)2
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
AN/TSC-85(V)2 Power Pallet
8,630
10K
3/3
120
b. Materials. The following materials are required to
(c) Remove the cargo cover and store it on the prime
rig this load:
mover.
(1) Sling set (10,000-pound capacity).
(2) Rigging. Rig the load according to the steps in
Figure 13-5.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
NOTE: The Required Individual Equipment (RIE) case is
designated as the forward end for rigging purposes.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(3) Hookup. The hookup team stands on top of the
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
load. The static wand person discharges the static elec-
strength.
tricity with the static wand. The hookup person places
the apex fitting onto the aircraft cargo hook. The hookup
c. Personnel. Two persons can prepare and rig this
team then moves clear of the load but remains close to the
load in 20 minutes.
load as the helicopter removes slack from the sling legs.
When successful hookup is assured, the hookup team
d. Procedures. The following procedures apply to this
quickly exits the area underneath the helicopter to the
load:
designated rendezvous point.
(1) Preparation. Prepare the load using the following
CAUTION
steps:
Brief the pilot to relax sling tension and hover
to the side of the load when releasing the apex
(a) Secure all loose equipment and cables on the
fitting to prevent damage to the pallet.
pallet with tape or Type III nylon cord.
(4) Derigging. Derigging is the reverse of the prepa-
(b) Close and secure all access covers, vents, and
ration and rigging procedures in steps d (1) and d (2).
doors. All exhaust covers must be taped.
13-10
C3, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.3A
RIGGING STEPS
leg 2 on the right front lift ring.
1. Position apex fitting on top of the generators. Route
outer sling legs 1 and 2 to the front of the pallet and inner
3. Loop the chain end of sling leg 3 through the left rear
sling legs 3 and 4 to the rear. Sling legs 1 and 3 should be
lift provision. Place the correct link from Table 13-5 in the
on the left side of the load.
grab hook. Repeat with sling leg 4 on the right rear lift
ring.
NOTE: Do not use the lift provisions on the generators.
2. Loop the chain end of sling leg 1 through the left
4. Cluster and tie or tape (breakaway technique) all sling
front lift provision located on the pallet. Place the correct
legs together on top of the unit to prevent entanglement
link from Table 13-5 in the grab hook. Repeat with sling
during hookup and lift-off.
Figure 13-5. NATO Air Base Satcom (NABS) Power Pallet AN/TSC-85(V)2
13-11
C3, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.3A
13-7. Skid Mounted Tactical Quiet Generator Sets
a. Applicability. The following items in Table 13-6 are certified for all helicopters with suitable lift capacity by the US
Army Soldier Systems Center:
Table 13-6. Skid Mounted Tactical Quiet Generator Sets
M AX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGH T
SLING SET
AIRSPEE D
FRONT/REA R
(POUNDS )
(KNOTS )
MEP831, 3KW, 60HZ Generator Set
325
10K
/
80
MEP802A, 5KW, 60HZ Generator Set
890
10K
/
50
MEP812A, 5KW, 400HZ Generator Set
900
10K
/
50
MEP803A, 10KW, 60HZ Generator Set
1,180
10K
/
50
MEP813A, 10KW, 400HZ Generator Set
1,280
10K
/
50
MEP804A, 15KW, 50/60HZ Generator Set
2,125
10K
/
70
MEP814A, 15KW, 400HZ Generator Set
2,240
10K
/
70
MEP805A, 30KW, 50/60HZ Generator Set
3,005
10K
/
70
MEP805B, 30KW, 50/60HZ Generator Set
3,040
10K
/
70
MEP815A, 30KW, 400HZ Generator Set
3,015
10K
/
70
MEP815B, 30KW, 400HZ Generator Set
3,060
10K
/
70
MEP806A, 60KW, 50/60HZ Generator Set
3,760
10K
/
80
MEP806B, 60KW, 50/60HZ Generator Set
4,042
10K
/
80
MEP816A, 60KW, 400HZ Generator Set
3,850
10K
/
80
MEP816B, 60KW, 400HZ Generator Set
4,240
10K
/
80
b. Materials. The following materials are required to
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
rig this load:
strength.
(1) Sling set (10,000-pound capacity).
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
substitute.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
c. Personnel. Two persons can prepare and rig this
load in 20 minutes.
(3) Cord, nylon, Type III, 550-pound breaking strength.
d. Procedures. The following procedures apply to this
load:
13-12
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
(1) Preparation. Prepare the load using the following
(3) Hookup. The hookup team stands on top of the
steps:
load. The static wand person discharges the static elec-
tricity with the static wand. The hookup person places
(a) Close, lock, and secure all doors and panels with
the apex fitting onto the aircraft cargo hook. The hookup
tape.
team then moves clear of the load but remains close to the
load as the helicopter removes slack from the sling legs.
(b) Close and secure the exhaust cover with tape.
When successful hookup is assured, the hookup team
quickly exits the area underneath the helicopter to the
(c) Close vents on the fuel cap.
designated rendezvous point.
(2) Rigging. Rig the load according to the steps in
(4) Derigging. Derigging is the reverse of the prepa-
Figure 13-6.
ration and rigging procedures in steps d (1) and d (2).
RIGGING STEPS
1. Position apex fitting on top of the generator. Route
lift provision located at the rear of the generator and in-
outer sling legs 1 and 2 to the front of the generator and
side the skid. Place the correct link from Table 13-6 in the
inner sling legs 3 and 4 to the rear. Sling legs 1 and 3
grab hook. Repeat with sling leg 4 on the right rear lift
should be on the left side of the load.
provision.
2. Loop the chain end of sling leg 1 through the left
4. Secure the lift provision in the up position with tape
front lift provision located at the front of the generator
and pad the slings where they contact the generator.
inside of the left skid. Place the correct link from Table 13-
6 in the grab hook. Repeat with sling leg 2 on the right
5. Cluster and tie or tape (breakaway technique) all sling
front lift provision.
legs together on top of the unit to prevent entanglement
during hookup and lift-off.
3. Loop the chain end of sling leg 3 through the left rear
Figure 13-6. Skid Mounted Tactical Quiet Generator Sets
13-13
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
THIS PAGE INTENTIONALLY LEFT BLANK
13-14
C3, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.3A
CHAPTER 14
CERTIFIED SINGLE-POINT RIGGING PROCEDURES FOR MISCELLANEOUS
EQUIPMENT
14-1. Introduction
graph and identifies the certified loads. The certified
This chapter contains rigging procedures for single-point
single-point rigging procedures for miscellaneous equip-
lift of miscellaneous equipment that has been certified for
ment are in this section. Paragraphs 14-2 through 14-9
sling load. Each rigging procedure is found in a para-
give detailed instructions for rigging loads.
graph that includes a description of the load, materials
required for rigging, and steps to complete the procedure.
NOTE: Reach Pendants may be used on all single point
An applicability paragraph is also a part of each para-
loads. A static discharge person is not required when
using a Reach Pendant.
14-2. Forward Area Refueling Equipment (FARE)
a. Applicability. The following item in Table 14-1 is certified for all helicopters with suitable lift capacity by the US Army
Soldier Systems Center:
Table 14-1. Forward Area Refueling Equipment (FARE)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGH T
SLING SET
AIRSPEE D
FRONT/REA R
(POUNDS )
(KNOTS )
Generator, 1.5KW, Fuel Hoses wih
Reels and Carrying Bags (2 each),
820
5K Cargo Net
/
60
Assembly Pump, Fire Extinguishers
(3 each)
b. Materials. The following materials are required to
c. Personnel. Two persons can prepare and rig this
rig this load:
load in 15 minutes.
(1) Net, cargo (5,000-pound capacity).
d. Procedures. The following procedures apply to this
load:
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(1) Preparation. Prepare the load using the following
steps:
(3) Cord, nylon, Type III, 550-pound breaking strength.
(a) Secure the two fire extinguishers to the inside
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
frame of the fuel hose reels with 1/2-inch tubular nylon
strength.
webbing. Secure the two fuel hose reels together with
Type III nylon cord.
(5) Tiedown strap, cargo, CGU-1/B (4 each).
(b) Spread a 5,000-pound capacity cargo net on the
(6) Webbing, nylon, tubular, 1/2-inch, 1000-pound
ground. Center the two fuel hose reels on the net. Place
breaking strength.
the pump assembly on either side of the reels. Place the
14-1

 

 

 

 

 

 

 

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