Главная Manuals FM 10-450-4 MULTISERVICE HELICOPTER SLING LOAD: SINGLE-POINT LOAD RIGGING PROCEDURES (September 2003)
|
|
|
C3, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.3A
1.5KW generator, with 5-gallon gas can attached, on the
electricity with the static wand. The hookup person places
opposite side of the reels. Place fuel hose carrying bags
the apex fitting onto the aircraft cargo hook. The hookup
in front of the reels. Secure the two carrying bags with the
team then moves clear of the load but remains close to the
remaining fire extinguisher together with Type III nylon
load as the helicopter removes slack from the sling legs.
cord. Secure the carrying bag to the reels.
When successful hookup is assured, the hookup team
quickly exits the area underneath the helicopter to the
(2) Rigging. Rig the load according to the steps in
designated rendezvous point.
Figure 14-1.
(4) Derigging. Derigging is the reverse of the prepa-
(3) Hookup. The hookup team stands along side the
ration and rigging procedures in steps d (1) and d (2).
load. The static wand person discharges the static
RIGGING STEPS
1. Inspect the net in accordance with FM 10-450-3.
2. Prepare and rig the net in accordance with FM 10-
450-3.
Figure 14-1. Forward Area Refueling Equipment (FARE)
14-2
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
14-3. Fire Extinguisher, Dry Chemical
a. Applicability. The following item in Table 14-2 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 14-2. Fire Extinguisher, Dry Chemical
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Fire Extinguisher, Dry Chemical, Self
3,000
15K
5/5
100
Contained, TAMCN C4765
b. Materials. The following materials are required to
(a) Tie hose reel and nozzle to the frame with Type
rig this load:
III nylon cord.
(1) Sling set (15,000-pound capacity).
(b) Secure or remove all loose attachments. Tape all
glass including the gages.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(2) Rigging. Rig the load according to the steps in
Figure 14-2.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(3) Hookup. The hookup team stands alongside 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 10 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).
14-3
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/web ring on top of the fire extin-
3. Loop the chain end of sling leg 3 through the left rear
guisher. Route outer sling legs 1 and 2 to the front of the
lift provision located at the top corner of the frame near
fire extinguisher and inner sling legs 3 and 4 to the rear
the hose reel. Place the correct link from Table 14-2 in the
end (hose reel). Sling legs 1 and 3 must be on the left side
grab hook. Repeat with sling leg 4 and the right rear lift
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 at the top corner of the frame
legs together on top of the fire extinguisher to prevent
near the pressure vessel. Place the correct link from Table
entanglement during hookup and lift-off. Pay close atten-
14-2 in the grab hook. Repeat with sling leg 2 and the
tion to the pipes and valves.
right front lift provision.
Figure 14-2. Fire Extinguisher, Dry Chemical
14-4
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
14-4. Rigid Raiding Craft
a. Applicability. The following item in Table 14-3 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 14-3. Rigid Raiding Craft
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Rigid Raiding Craft, Fiberglass,
3,200
40K
5/10
75
18-foot, TAMCN C5902
b. Materials. The following materials are required to
(c) Secure the console hatch with tape. Secure the
rig this load:
anchor to the deck and secure the loose end of the anchor.
(1) Sling set (40,000-pound capacity).
(d) Secure the running lights to an inner handrail
with tape or Type III nylon cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(e) Secure the base of the outboard motors tightly to
the bar directly above with Type III nylon cord.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(f) Tape the compass glass on top of the console.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(2) Rigging. Rig the load according to the steps in
Figure 14-3.
c. Personnel. Two persons can prepare and rig this
load in 15 minutes.
(3) Hookup. The hookup team stands alongside the
load. The static wand person discharges the static elec-
d. Procedures. The following procedures apply to this
tricity with the static wand. The hookup person places
load:
the apex fitting onto the aircraft cargo hook. The hookup
team then moves clear of the load but remains close to the
(1) Preparation. Prepare the load using the following
load as the helicopter removes slack from the sling legs.
steps:
When successful hookup is assured, the hookup team
quickly exits the area underneath the helicopter to the
(a) Tighten all straps on the anchor, paddles, cush-
designated rendezvous point.
ions, and loose equipment.
(4) Derigging. Derigging is the reverse of the prepa-
(b) Stow the boat utility bags in the console. Re-
ration and rigging procedures in steps d (1) and d (2).
move the anchor chain and line and stow in the console.
Protect the battery from the chain.
14-5
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 boat. Route outer
3. Loop the chain end of sling leg 3 through the left rear
sling legs 1 and 2 to the front (bow end) of the boat and
lift ring located on the inside of the hull. Place the correct
inner sling legs 3 and 4 to the rear end. Sling legs 1 and 3
link from Table 14-3 in the grab hook. Repeat with sling
must be on the left side of the load.
leg 4 and the right rear lift 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 ring located on the inside of the hull. Place the
legs together on top of the boat to prevent entanglement
correct link from Table 14-3 in the grab hook. Repeat with
during hookup and lift-off.
sling leg 2 and the right front lift provision.
Figure 14-3. Rigid Raiding Craft
14-6
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
14-5. 2.75-inch Rocket Fastpack Pallet
a. Applicability. The following items in Table 14-4 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 14-4. 2.75-inch Rocket Fastpack Pallet
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
PA 150 Pallet with Twelve (12)
2,200
10K
3/3
60
2.75-inch Rockets
PA 151 Pallet with Twelve (12)
2,000
10K
3/3
60
2.75-inch Rockets
b. Materials. The following materials are required to
(b) Secure the loose ends of any cables, bands, or
rig this load:
chains with tape or Type III nylon cord.
(1) Sling set (10,000-pound capacity).
(c) Ensure the 1-1/4-inch steel banding around the
pallet is in serviceable condition and the containers are
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
locked together.
roll.
(d) Tape the upper corners of the pallet from the top
(3) Cord, nylon, Type III, 550-pound breaking strength.
to the second row of rockets.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(2) Rigging. Rig the load according to the steps in
strength.
Figure 14-4.
c. Personnel. Two persons can prepare and rig this
(3) Hookup. The hookup team stands alongside the
load in 10 minutes.
load. The static wand person discharges the static elec-
tricity with the static wand. The hookup person places
d. Procedures. The following procedures apply to this
the apex fitting onto the aircraft cargo hook. The hookup
load:
team then moves clear of the load but remains close to the
load as the helicopter removes slack from the sling legs.
(1) Preparation. Prepare the load using the following
When successful hookup is assured, the hookup team
steps:
quickly exits the area underneath the helicopter to the
designated rendezvous point.
(a) Close the safety latches on the lids of the rocket
containers. Secure the lids with Type III nylon cord.
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
14-7
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 pallet. 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 pallet and inner sling
lift provision. Place the correct link from Table 14-4 in the
legs 3 and 4 to the rear end. Sling legs 1 and 3 must be on
grab hook. Repeat with sling leg 4 and 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 14-4
legs together on top of the pallet to prevent entanglement
in the grab hook. Repeat with sling leg 2 and the right
during hookup and lift-off.
front lift provision.
Figure 14-4. 2.75-inch Rocket Fastpack Pallet
14-8
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
14-6. Special Divers Air Support System (SDASS)
a. Applicability. The following item in Table 14-5 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 14-5. Special Divers Air Support System (SDASS)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Four SDASS Racks with Two Empty
Air Cylinders each in a 2X2
1,800
10K Cargo Net
N/A
70
Configuration
b. Materials. The following materials are required to
(1) Preparation. Prepare the load using the following
rig this load:
steps:
(1) Net, cargo (10,000-pound capacity).
(a) Inspect the cargo net in accordance with FM 10-
450-3.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(b) Prepare the plywood sheets and the dunnage.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(2) Rigging. Rig the load according to the steps in
Figure 14-5.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(3) Hookup. The hookup team stands alongside the
load. The static wand person discharges the static elec-
(5) Tie-down strap, cargo, CGU-1/B (4 each).
tricity with the static wand. The hookup person places
the apex fitting onto the aircraft cargo hook. The hookup
(6) Dunnage material.
team then moves clear of the load but remains close to the
load as the helicopter removes slack from the sling legs.
(7) Plywood 44 X 75 X 1/2-inch (2 each).
When successful hookup is assured, the hookup team
quickly exits the area underneath the helicopter to the
c. Personnel. Two persons can prepare and rig this
designated rendezvous point.
load in 20 minutes.
(4) Derigging. Derigging is the reverse of the prepa-
d. Procedures. The following procedures apply to this
ration and rigging procedures in steps d (1) and d (2).
load:
14-9
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Spread the cargo net on the ground.
4. Insert dunnage between the two stacks of racks and
secure the dunnage to the stacks with Type III nylon cord.
2. Position the bottom two racks on the plywood sheets.
Secure each rack to the plywood using CGU-1/B tie-down
5. Route two CGU-1/B tie-down straps around the lower
straps.
bottom racks and two CGU-1B tie-down straps around the
upper racks.
3. Place the remaining two racks on top of the bottom
racks, fitting together the feet at each of the five junction
6. Rig the net in accordance with FM 10-450-3.
points.
Figure 14-5. Special Divers Air Support System (SDASS)
14-10
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
14-7. Two Mobile Oversnow Transport (MOST) Snowmobiles with or without Two Sleds
a. Applicability. The following items in Table 14-6 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 14-6. Two Mobile Oversnow Transport (MOST) Snowmobiles with or without Two Sleds
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Polaris Indy Wide-Track Snowmobile
638 each
10K Cargo Net
N/A
70
Norwegian Pulk Sled, Model BN 2010C
381 loaded
10K Cargo Net
N/A
70
b. Materials. The following materials are required to
(b) Position the two MOSTs on level ground.
rig this load:
(c) Secure the canvas cargo cover over the sled.
(1) Net, cargo (10,000-pound capacity) (2 each).
(d) Secure the fuel cap on the MOST with tape.
(2) One sling leg from a sling set (10,000-pound capac-
ity).
(e) Remove the snap-off wind screen from the MOST,
pad it with felt, and secure it over the seat with Type III
(3) Cord, nylon, Type III, 550-pound breaking strength.
nylon cord.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(2) Rigging. Rig the load according to the steps in
strength.
Figure 14-6.
(5) Tape, adhesive, pressure-sensitive, 2-inch wide
(3) Hookup. The hookup team consists of four
roll.
people. The hookup team stands alongside the load. The
static wand person discharges the static electricity with
(6) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
the static wand. One hookup person places the apex fit-
substitute.
ting onto the aircraft cargo hook. The other two people
kneel, one on each side of the load, to ensure the net does
(7) Pad, energy dissipating, honeycomb (2 sheets).
not catch on the handle bars, tie-down points, or trailer
hitch as the load is lifted. As the first net is lifted off the
c. Personnel. Eight persons can prepare and rig this
ground, after successful hookup is assured, the hookup
load in 10 minutes. The large number of personnel is
team quickly exits the area underneath the helicopter to
required to lift and position the MOST.
the designated rendezvous point. This will ensure the
hookup team is not struck by the second cargo net as it is
d. Procedures. The following procedures apply to this
being lifted off the ground.
load:
NOTE: Brief the pilot to hover to the side after the sleds
(1) Preparation. Prepare the load using the following
are on the ground to lower the MOSTs to the ground.
steps:
Once the MOSTs are on the ground, the pilot must hover
to the side before releasing the apex fitting.
(a) Inspect the cargo net in accordance with FM 10-
450-3.
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
14-11
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
NOTES:
1. Two MOSTs are certified for sling loading without
the sleds.
2. One MOST and one sled is NOT certified for sling
loading. The load does not fly stable.
RIGGING STEPS
1. Lay out the first 10,000-pound cargo net. Place two
load and tape the net together every 3 feet from the apex
MOSTs side-by-side facing in opposite directions with
down (breakaway technique).
two sheets of honeycomb between them. Close the net to
the apex fitting of the cargo net. Gather the excess net
3. Attach the chain from the 10,000-pound sling leg to
above the load and tape the net together every 3 feet from
the apex of the cargo net holding the sleds. Insert link 4 in
the apex down (breakaway technique).
the grabhook. The end of the sling leg with the apex
attached is fed under the net holding the two MOSTs
2. Lay out the second 10,000-pound cargo net next to
along the axis of the honeycomb. It is passed through the
the first one and center the two sleds on the net side-by-
net at the center and pulled upward between the two sheets
side facing opposite directions. Close the net to the apex
of honeycomb and attached to the apex of the net using
fitting of the cargo net. Gather the excess net above the
the apex. This will allow the sleds to hang directly below
the MOST.
Figure 14-6. Two Mobile Oversnow Transport (MOST) Snowmobiles with or without Two Sleds
14-12
C3, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.3A
14-8. Container Roll-in/out Platform (CROP), Two Empty Platforms, Stacked
a. Applicability. The following item in Table 14-7 is certified for all helicopters with suitable lift capacity by the US Army
Soldier Systems Center:
Table 14-7. Container Roll-in/out Platform (CROP), Two Empty Platforms, Stacked
MAX
RECOMMENDED
SLING
LINK COUNT
NOMENCLATURE
WEIGH T
AIRSPEE D
SET
FRONT / REA R
(POUNDS )
(KNOTS )
Two CROPs, Empty, Stacked
7,300
10K
3
/
110
b. Materials. The following materials are required to
(b) Secure the A-frames in the down position.
rig this load:
(c) Stack the platforms with the A-frames at the same
(1) Sling set (10,000-pound capacity).
end and secure the platforms together with the straps
provided with the platform ( a minimum of two straps per
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
platform are required). Ensure the straps have operational
roll.
keepers on the hook ends. Secure the loose strap ends
with tape or 1/4-inch cotton webbing.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(2) Rigging. Rig the load according to the steps in
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
Figure 14-7.
strength.
(3) Hookup. The hookup team stands on the stacked
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
platforms. The static wand person discharges the static
padding.
electricity with the static wand. The hookup person places
the apex fitting onto the cargo hook. The hookup team
c. Personnel. Two persons can prepare and rig this
then carefully dismounts the platform and remains close
load in 10 minutes.
to the load as the helicopter removes slack from the sling
legs. When successful hookup is assured, the hookup
d. Procedures. The following procedures apply to
team quickly exits the area underneath the helicopter to
this load:
the designated rendezvous point.
(1) Preparation. Prepare the load using the following
(4) Derigging. Derigging is the reverse of the prepara-
steps:
tion and rigging procedures in steps d (1) and d (2).
(a) Ensure the load restraints are in the stowed
position.
14-13
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 top of the stacked plat-
rect link from Table 14-7 in the grab hook. Repeat with
forms. Route outer sling legs 1 and 2 to the front of the
sling leg 4 through the right rear lift provision on the top
platform and inner sling legs 3 and 4 to the rear (A-frame
platform.
end). Sling legs 1 and 3 must be on the left side of the
load.
4. Secure all excess chain with tape or Type III nylon
cord.
2. Loop the chain end of sling leg 1 through the left
front lift provision located on the top platform. Place the
5. Pad each chain where it contacts sharp edges on the
correct link from Table 14-7 in the grab hook. Repeat with
platform. Secure the padding with tape or Type III nylon
sling leg 2 through the right front lift provision on the top
cord.
platform.
6. Cluster and tie or tape (breakaway technique) all sling
3. Loop the chain end of sling leg 3 through the left rear
legs together on top of the platforms to prevent entangle-
lift provision located on the top platform. Place the cor-
ment during hookup and lift-off.
Figure 14-7. Container Roll-in/out Platform (CROP), Two Empty Platforms, Stacked
14-14
C3, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.3A
14-9. Special Operations Craft-Riverine (SOC-R) and Naval Special Warfare Rigid Inflatable
Boat (NSWRIB) Trailer
a. Applicability. The following items in Table 14-8 are certified for all helicopters with suitable lift capacity by the US
Army Soldier Systems Center:
Table 14-8. Special Operations Craft-Riverine (SOC-R) and Naval Special Warfare Rigid Inflatable Boat
(NSWRIB) Trailer
MAX
RECOMMENDED
SLING
LINK COUNT
NOMENCLATURE
WEIGH T
AIRSPEE D
SET
FRONT / REA R
(POUNDS )
(KNOTS )
Special Operations Craft-Riverine
3,716
15K
/
50
(SOC-R) Tra
l
Naval Special Warfare Rig
i
4,300
15K
/
50
Boat (NSWRIB) Tra
l
b. Materials. The following materials are required to
cables, and brake cables on top of the drawbar tape or
rig this load:
Type III nylon cord.
(1) Multileg sling set (15,000-pound capacity).
(d) Engage the parking brake and secure it in the
engaged position.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(e) Tape the rails on the trailer together to ensure the
slings do not become entangled.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(f) Tape all lights.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(2) Rigging. Rig the load according to the steps in
Figure 14-8.
c. Personnel. Two persons can prepare and rig this
load in 10 minutes.
NOTE: This load is flown with the lunette in front.
d. Procedures. The following procedures apply to this
(3) Hookup. The hookup team stands next to the
load:
trailer. The static discharge person discharges the static
electricity. The hookup person places the apex on the
(1) Preparation. Prepare the load using the following
cargo hook. The hookup teams then carefully dismount
steps:
the boat and remain close to the load as the helicopter
removes slack from the sling legs. When successful
(a) Secure the utility box lid with Type III nylon cord.
hookup is assured, the hookup teams quickly exit the area
underneath the helicopter to the designated rendezvous
(b) Lower the lunette close to the ground and secure
point.
it in place with a 5,000-pound tiedown strap and load binder.
(4) Derigging. Derigging is the reverse of the prepa-
(c) Secure safety chains, intervehicular electrical
ration and rigging procedures in steps d (1) and d (2).
14-15
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 top of the trailer.
Place the correct link from Table 14-8 in the grab hook.
Repeat this step with sling leg 4 on the right side of the
2. Loop the chain end of sling leg 1 around the main
trailer. Secure the excess chain with tape or Type III nylon
support frame in front of the tiedown provision on the left
cord.
side of the trailer . Place the correct link from Table 14-8 in
the grab hook. Repeat this step with sling leg 2 on the
4. Raise the apex fittings above the load. Cluster and tie
right side of the trailer.
or tape (breakaway technique) the sling legs in each sling
set together to prevent entanglement during hookup and
3. Loop the chain end of sling leg 3 around the frame
lift-off.
and through the lift provision on the left rear of the trailer.
Figure 14-8. Special Operations Craft-Riverine (SOC-R) and Naval Special Warfare Rigid
Inflatable Boat (NSWRIB) Trailer
14-16
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
CHAPTER 15
SUITABLE SINGLE-POINT RIGGING PROCEDURES FOR WHEELED VEHICLES
15-1. Introduction
This chapter contains rigging procedures for single-point
graphs 15-2 through 15-6 give detailed instructions for
lift of wheeled vehicles that are suitable for sling load.
rigging loads.
Each rigging procedure is found in a paragraph that in-
cludes 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 suitable loads. The suitable single-point rigging
procedures for wheeled vehicles are in this section. Para-
15-2. M342A2 2 1/2-Ton Dump Truck with Winch
a. Applicability. The following item in Table 15-1 is suitable for sling load by all ARMY helicopters with suitable lift
capacity:
WARNING
DO NOT LIFT THIS LOAD WITH THE ORIGINAL VEHICLE LIFT PROVISION
Table 15-1. M342A2 2 1/2-Ton Dump Truck with Winch
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Truck, Dump, 2 1/2-ton, M342A2
15,770
25K
3/30
85
b. Materials. The following materials are required to
d. Procedures. The following procedures apply to this
rig this load:
load:
(1) Sling set (25,000-pound capacity).
(1) Preparation. Prepare the load using the following
steps:
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(a) Modify the cargo bed. Secure the bed in the
down position.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(b) Place the transmission in neutral and engage the
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
hand brake.
strength.
(c) Secure the steering wheel and doors with Type
c. Personnel. One person can prepare and rig this load
III nylon cord.
( after modifying the bed) in 15 minutes.
15-1
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
(d) Tape the windshield wipers to the windshield.
static electricity with the static wand. The hookup person
places the apex fitting onto the aircraft cargo hook. The
(e) Secure the hood with Type III nylon cord routed
hookup team then moves clear of the load but remains
from the grill through the hood latches.
close to the load as the helicopter removes slack from the
sling legs. When successful hookup is assured, the
(2) Rigging. Rig the load according to the steps in
hookup team quickly exits the area underneath the heli-
Figure 15-1.
copter to the designated rendezvous point.
(3) Hookup. The hookup team stands in the cargo
(4) Derigging. Derigging is the reverse of the prepa-
bed of the truck. The static wand person discharges the
ration and rigging procedures in steps d (1) and d (2).
RIGGING STEPS
1. Position apex fitting on top of the forward end of the
3. Loop the chain end of sling leg 3 through the left hole
dump box. Route outer sling legs 1 and 2 to the front of
in the floor of the cargo bed, under the lifting pin on the
the truck and inner sling legs 3 and 4 to the rear end. Sling
spring shackle between the wheels, and back up through
legs 1 and 3 must be on the left side of the load.
the hole. Place the correct link from Table 15-1 in the grab
hook. Repeat with sling leg 4 and the right rear lift provi-
2. Loop the chain end of sling leg 1 through the left
sion.
front lift provision located on the left side of the front
bumper. Place the correct link from Table 15-1 in the grab
4. Cluster and tie or tape (breakaway technique) all sling
hook. Repeat with sling leg 2 and the right front lift provi-
legs together on top of the truck to prevent entanglement
sion.
during hookup and lift-off.
Figure 15-1. M342A2 2 1/2-Ton Dump Truck with Winch
15-2
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
15-3. M35A1/2 2 1/2-Ton Cargo Truck with Winch
a. Applicability. The following items in Table 15-2 are suitable for sling load by all ARMY helicopters with suitable lift
capacity:
WARNING
DO NOT LIFT THIS LOAD WITH THE ORIGINAL VEHICLE LIFT PROVISION
Table 15-2. M35A1/2 2 1/2-Ton Cargo Truck with Winch
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Truck, Cargo, 2 1/2-ton, M35A1, with
13,550
25K
13/3
90
Winch
Truck, Cargo, 2 1/2-ton, M35A2, with
13,570
25K
13/3
90
Winch
b. Materials. The following materials are required to
(b) Remove the cab tarpaulin, lower and secure the
rig this load:
windshield, and secure the tarpaulin over the windshield
with Type III nylon cord.
(1) Sling set (25,000-pound capacity).
(c) Secure the hood with Type III nylon cord routed
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
from the grill through the hood latches.
roll.
(d) Ensure the fuel cap, oil filler cap, radiator cap, and
(3) Cord, nylon, Type III, 550-pound breaking strength.
battery caps are properly installed and the battery com-
partment door is fastened.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(e) Secure the seats and doors with Type III nylon
cord.
(5) Padding, cellulose.
(f) Place the transmission in neutral and engage the
(6) Tie-down, cargo, CGU-1/B (as required).
hand brake.
c. Personnel. Two persons can prepare and rig this
(g) Straighten the front wheels and secure the steer-
load in 25 minutes.
ing wheel with Type III nylon cord.
d. Procedures. The following procedures apply to this
(2) Rigging. Rig the load according to the steps in
load:
Figure 15-2.
(1) Preparation. Prepare the load using the following
(3) Hookup. The hookup team stands in the cargo
steps:
bed of the truck. The static wand person discharges the
static electricity with the static wand. The hookup person
(a) Remove the bed tarpaulin and bows and secure
places the apex fitting onto the aircraft cargo hook. The
them in the truck bed with tie-down straps or Type III
hookup team then moves clear of the load but remains
nylon cord.
15-3
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
close to the load as the helicopter removes slack from the
(4) Derigging. Derigging is the reverse of the prepa-
sling legs. When successful hookup is assured, the
ration and rigging procedures in steps d (1) and d (2).
hookup team quickly exits the area underneath the heli-
copter to the designated rendezvous point.
RIGGING STEPS
1. Position apex fitting in the bed of the truck near the
the chain in the chain guide bracket with 1/4-inch cotton
cab. Route outer sling legs 1 and 2 to the front of the truck
webbing. Ensure the hook side of the grab hook faces
and inner sling legs 3 and 4 to the rear end. Sling legs 1
outward. Repeat with sling leg 4 and 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. Tie the rear grab hooks together across the bed of the
front lift provision located on the left side of the front
truck with 1/4-inch cotton webbing.
bumper. Place the correct link from Table 15-2 in the grab
hook. Repeat with sling leg 2 and the right front lift provi-
5. Pull the front sling legs up over the hood and secure
sion. Secure the excess chain with Type III nylon cord.
the grab hooks to the hood latch attachment with Type III
nylon cord.
3. Loop the chain end of sling leg 3 through the left
lifting pin on the spring shackle between the rear wheels.
6. Tape sling legs 1 and 2 to the top of the steering
Place the correct link from Table 15-2 in the grab hook.
wheel. Cluster and tie or tape (breakaway technique) all
Pull the grab hook up against the side of the truck and tie
sling legs together on top of the truck to prevent en-
tanglement during hookup and lift-off.
Figure 15-2. M35A1/2 2 1/2-Ton Cargo Truck with Winch
15-4
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
15-4. M54A2 5-Ton Cargo Truck with Winch
a. Applicability. The following item in Table 15-3 is suitable for sling load by all ARMY helicopters with suitable lift
capacity:
WARNING
DO NOT LIFT THIS LOAD WITH THE ORIGINAL VEHICLE LIFT PROVISION
Table 15-3. M54A2 5-Ton Cargo Truck with Winch
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Truck, Cargo, 5-ton, M54A2, with
20,782
25K
3/13
80
Winch
b. Materials. The following materials are required to
windshield, and secure the tarpaulin over the windshield
rig this load:
with Type III nylon cord.
(1) Sling set (25,000-pound capacity).
(c) Secure the hood with Type III nylon cord routed
from the grill through the hood latches.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(d) Ensure the fuel cap, oil filler cap, radiator cap, and
battery caps are properly installed and the battery com-
(3) Cord, nylon, Type III, 550-pound breaking strength.
partment door is fastened.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(e) Secure the seats and doors with Type III nylon
strength.
cord.
(5) Padding, cellulose.
(f) Place the transmission in neutral and engage the
hand brake.
(6) Tie-down, cargo, CGU-1/B (as required).
(g) Straighten the front wheels and secure the steer-
c. Personnel. Two persons can prepare and rig this
ing wheel with Type III nylon cord.
load in 25 minutes.
(2) Rigging. Rig the load according to the steps in
d. Procedures. The following procedures apply to this
Figure 15-3.
load:
(3) Hookup. The hookup team stands in the cargo
(1) Preparation. Prepare the load using the following
bed of the truck. The static wand person discharges the
steps:
static electricity with the static wand. The hookup person
places the apex fitting onto the aircraft cargo hook. The
(a) Remove the bed tarpaulin and bows and secure
hookup team then moves clear of the load but remains
them in the truck bed with tie-down straps or Type III
close to the load as the helicopter removes slack from the
nylon cord.
sling legs. When successful hookup is assured, the
hookup team quickly exits the area underneath the heli-
(b) Remove the cab tarpaulin, lower and secure the
copter to the designated rendezvous point.
15-5
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
RIGGING STEPS
1. Position apex fitting in the bed of the truck near the
webbing. Ensure the hook side of the grab hook faces
cab. Route outer sling legs 1 and 2 to the front of the truck
outward. Repeat with sling leg 4 and the right rear lift
and inner sling legs 3 and 4 to the rear end. Sling legs 1
provision.
and 3 must be on the left side of the load.
4. Tie the rear grab hooks together across the bed of the
2. Loop the chain end of sling leg 1 through the left
truck with 1/4-inch cotton webbing.
front lift provision located on the left side of the front
bumper. Place the correct link from Table 15-3 in the grab
5. Pull the front sling legs up over the hood and secure
hook. Repeat with sling leg 2 and the right front lift provi-
the grab hooks to the hood latch attachment with Type III
sion. Secure the excess chain with Type III nylon cord.
nylon cord.
3. Loop the chain end of sling leg 3 through the left
6. Tape sling legs 1 and 2 to the top of the steering
lifting pin on the spring shackle between the rear wheels.
wheel. Cluster and tie or tape (breakaway technique) all
Place the correct link from Table 15-3 in the grab hook.
sling legs together on top of the truck to prevent en-
Pull the grab hook up against the side of the truck and tie
tanglement during hookup and lift-off.
the chain in the chain guide bracket with 1/4-inch cotton
Figure 15-3. M54A2 5-Ton Cargo Truck with Winch
15-6
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
15-5. M52A2 or M818 5-Ton Tractor with Winch
a. Applicability. The following items in Table 15-4 are suitable for sling load by all ARMY helicopters with suitable lift
capacity:
WARNING
DO NOT LIFT THIS LOAD WITH THE ORIGINAL VEHICLE LIFT PROVISION
Table 15-4. M52A2 or M818 5-Ton Tractor with Winch
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Truck, Tractor, 5-ton, M52A2, with
18,430
25K
3/43
85
Winch
Truck, Tractor, 5-ton, M818, with
20,107
25K
3/43
85
Winch
b. Materials. The following materials are required to
(b) Straighten the front wheels and secure the steer-
rig this load:
ing wheel with Type III nylon cord. Secure the doors with
Type III nylon cord.
(1) Sling set (25,000-pound capacity).
(c) Place the air hoses in the brackets and 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 15-4.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(3) Hookup. The hookup team stands on the rear of
strength.
the hood. The static wand person discharges the static
electricity with the static wand. The hookup person places
c. Personnel. Two persons can prepare and rig this
the apex fitting onto the aircraft cargo hook. The hookup
load in 15 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) Place the transmission in neutral and engage the
hand brake.
15-7
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 spare tire. Route
lifting pin on the spring shackle between the rear wheels.
outer sling legs 1 and 2 to the front of the truck and inner
Place the correct link from Table 15-4 in the grab hook.
sling legs 3 and 4 to the rear end. Sling legs 1 and 3 must
Repeat with sling leg 4 and the right rear lift provision.
be on the left side of the load.
Secure the excess chain with Type III nylon cord.
2. Loop the chain end of sling leg 1 through the left
4. Pull the front sling legs up over the hood and secure
front lift provision located on the left side of the front
the grab hooks to the hood latch attachment with Type III
bumper. Place the correct link from Table 15-4 in the grab
nylon cord.
hook. Repeat with sling leg 2 and the right front lift provi-
sion.
5. Cluster and tie or tape (breakaway technique) all sling
legs together on top of the spare tire to prevent entangle-
3. Loop the chain end of sling leg 3 through the left
ment during hookup and lift-off.
Figure 15-4. M52A2 or M818 5-Ton Tractor with Winch
15-8
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
15-6. Crane, Self-Propelled, for Army Aircraft Maintenance and Positioning (SCAMP)
a. Applicability. The following item in Table 15-5 is suitable for sling load by all ARMY helicopters with suitable lift
capacity:
Table 15-5. Crane, Self-Propelled, for Army Aircraft Maintenance and Positioning (SCAMP)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Crane, Self-Propelled, Army Aircraft
14,600
25K
3/40
85
Maintenance and Positioning
b. Materials. The following materials are required to
(c) Secure the engine cover, tow bar, and tow wheels
rig this load:
in place with Type III nylon cord.
(1) Sling set (25,000-pound capacity).
(d) Secure all loose equipment, doors, or panels with
tape or Type III nylon cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(e) Place the transmission in neutral and engage the
parking brake.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(2) Rigging. Rig the load according to the steps in
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
Figure 15-5.
strength.
(3) Hookup. The hookup team stands between the
c. Personnel. Two persons can prepare and rig this
end of the boom and the engine cover. The static wand
load in 10 minutes.
person discharges the static electricity with the static
wand. The hookup person places the apex fitting onto the
d. Procedures. The following procedures apply to this
aircraft cargo hook. The hookup team then moves clear of
load:
the load but remains close to the load as the helicopter
removes slack from the sling legs. When successful
(1) Preparation. Prepare the load using the following
hookup is assured, the hookup team quickly exits the area
steps:
underneath the helicopter to the designated rendezvous
point.
(a) Attach the block and tackle to the front pintle
hook (the cable must be snug).
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
(b) Rotate the mirrors in toward the cab and tape all
the glass.
15-9
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 boom. Route outer
excess chain with Type III nylon cord.
sling legs 1 and 2 to the front of the crane and inner sling
legs 3 and 4 to the rear end. Sling legs 1 and 3 must be on
4. Cluster and tie or tape (breakaway technique) all
the left side of the load.
sling legs together on top of the crane to prevent en-
tanglement during hookup and lift-off.
2. Loop the chain end of sling leg 1 through the left
front lift provision located on the left front outrigger. Place
NOTES:
the correct link from Table 15-5 in the grab hook. Repeat
with sling leg 2 and the right front lift provision.
1. The rear sling leg routed on the exhaust must be
secured above the exhaust pipe to prevent entangling the
3. Loop the chain end of sling leg 3 through the left rear
sling.
lift provision located on the left rear outrigger. Place the
correct link from Table 15-5 in the grab hook. Repeat with
2. This load will fly with the boom low to prevent the
sling leg 4 and the right rear lift provision. Secure the
boom from striking the aircraft.
Figure 15-5. Crane, Self-Propelled, for Army Aircraft Maintenance and Positioning (SCAMP)
15-10
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
CHAPTER 16
SUITABLE SINGLE-POINT RIGGING PROCEDURES FOR TRAILERS
16-1. Introduction
This chapter contains rigging procedures for single-point
give detailed instructions for rigging loads.
lift of trailers that are suitable for sling load. Each rigging
procedure is found in a paragraph that includes a descrip-
tion of the load, materials required for rigging, and steps
NOTE: Reach Pendants may be used on all single point
to complete the procedure. An applicability paragraph is
loads. A static discharge person is not required when
also a part of each paragraph and identifies the suitable
using a Reach Pendant.
loads. The suitable single-point rigging procedures for
trailers are in this section. Paragraphs 16-2 through 16-13
16-2. M105 1 1/2-Ton Trailer
a. Applicability. The following item in Table 16-1 is suitable for sling load by all ARMY helicopters with suitable lift
capacity:
Table 16-1. M105 1 1/2-Ton Trailer
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Trailer, Cargo, 1 1/2-ton, M105 series
5,750
10K
4/30
45
b. Materials. The following materials are required to
load:
rig this load:
(1) Preparation. Prepare the load using the following
(1) Sling set (10,000-pound capacity).
steps:
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(a) Remove the top tarpaulin and bows.
roll.
(b) Remove the front and rear racks, stow in the slots
(3) Cord, nylon, Type III, 550-pound breaking strength.
provided on each side of the trailer, and secure them in
place with Type III nylon cord.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(c) Stow the bows and tarpaulin in the trailer bed and
secure them with Type III nylon cord.
(5) Tie-down, cargo, CGU-1/B (as required).
(d) Fasten the tailgate in the open position with the
c. Personnel. Two persons can prepare and rig this
chains on each side hooked through the keepers.
load in 25 minutes.
(e) Secure the cargo in the bed using the CGU-1/B
d. Procedures. The following procedures apply to this
cargo straps.
16-1
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
(f) Secure the light cable to the drawbar with tape or
(3) Hookup. The hookup team stands in the cargo
Type III nylon cord.
bed of the trailer. The static wand person discharges the
static electricity with the static wand. The hookup person
(g) Engage the parking brake.
places the apex fitting onto the aircraft cargo hook. The
hookup team then moves clear of the load but remains
(h) If the trailer has modified lift provisions, remove
close to the load as the helicopter removes slack from the
the push pin and rotate the provisions downward.
sling legs. When successful hookup is assured, the
hookup team quickly exits the area underneath the heli-
(2) Rigging. Rig the load according to the steps in
copter to the designated rendezvous point.
Figure 16-1.
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
RIGGING STEPS
1. Position apex fitting in the trailer bed. Route outer
lift provision located at the aft end of the trailer chassis
frame. Place the correct link from Table 16-1 in the grab
sling legs 1 and 2 to the front of the trailer and inner sling
hook. Repeat with sling leg 4 and the right rear lift provi-
legs 3 and 4 to the rear end. Route the rear chains between
the tailgate and the bed. Sling legs 1 and 3 must be on the
sion. Secure the excess chain with Type III nylon cord.
left side of the load.
4. Remove the slack from sling legs 3 and 4. Tape or tie
2. Loop the chain end of sling leg 1 through the lunette.
the grab hook or sling leg to the side rack.
Place the correct link from Table 16-1 in the grab hook.
Repeat with sling leg 2 on the lunette.
5. Cluster and tie or tape (breakaway technique) all sling
legs together on top of the trailer to prevent entanglement
during hookup and lift-off.
3. Loop the chain end of sling leg 3 through the left rear
Figure 16-1. M105 1 1/2-Ton Trailer
16-2
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
16-3. M270A1 Semitrailer, Wrecker
a. Applicability. The following item in Table 16-2 is suitable for sling load by all ARMY helicopters with suitable lift
capacity:
WARNING
DO NOT LIFT THIS LOAD WITH THE ORIGINAL VEHICLE LIFT PROVISION
Table 16-2. M270A1 Semitrailer, Wrecker
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Semitrailer, Lowbed, Wrecker, 12-ton,
17,500
25K
55/3
80
4-wheel
b. Materials. The following materials are required to
(1) Preparation. None required.
rig this load:
(2) Rigging. Rig the load according to the steps in
(1) Sling set (25,000-pound capacity).
Figure 16-2.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(3) Hookup. The hookup team stands on the trailer.
roll.
The static wand person discharges the static electricity
with the static wand. The hookup person places the apex
(3) Cord, nylon, Type III, 550-pound breaking strength.
fitting onto the aircraft cargo hook. The hookup team
then moves clear of the load but remains close to the load
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
as the helicopter removes slack from the sling legs. When
strength.
successful hookup is assured, the hookup team quickly
exits the area underneath the helicopter to the designated
c. Personnel. One person can prepare and rig this load
rendezvous point.
in 10 minutes.
(4) Derigging. Derigging is the reverse of the rigging
d. Procedures. The following procedures apply to this
procedures in step d (2).
load:
16-3
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 the trailer in the vicinity of the
3. Loop the chain end of sling leg 3 through the left lift
spare tire. Route outer sling legs 1 and 2 to the front of the
provision on the frame forward of the wheels. Place the
trailer and inner sling legs 3 and 4 to the rear end. Sling
correct link from Table 16-2 in the grab hook. Repeat with
legs 1 and 3 must be on the left side of the load.
sling leg 4 and the right rear lift provision.
2. Loop the chain end of sling leg 1 through the third
4. Cluster and tie or tape (breakaway technique) all
stake pocket on the left side from the forward end of the
sling legs together on top of the trailer to prevent en-
trailer . Place the correct link from Table 16-2 in the grab
tanglement during hookup and lift-off.
hook. Repeat with sling leg 2 on the right side. Secure the
excess chain with Type III nylon cord.
Figure 16-2. M270A1 Semitrailer, Wrecker
16-4
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
16-4. M172A1 Semitrailer, Lowbed
a. Applicability. The following item in Table 16-3 is suitable for sling load by all ARMY helicopters with suitable lift
capacity:
WARNING
DO NOT LIFT THIS LOAD WITH THE ORIGINAL VEHICLE LIFT PROVISION
Table 16-3. M172A1 Semitrailer, Lowbed
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Semitrailer, Lowbed, M172A1, 25-ton
16,500
25K
3/60
80
b. Materials. The following materials are required to
(1) Preparation. None required.
rig this load:
(2) Rigging. Rig the load according to the steps in
(1) Sling set (25,000-pound capacity).
Figure 16-3.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(3) Hookup. The hookup team stands on the trailer.
roll.
The static wand person discharges the static electricity
with the static wand. The hookup person places the apex
(3) Cord, nylon, Type III, 550-pound breaking strength.
fitting onto the aircraft cargo hook. The hookup team
then moves clear of the load but remains close to the load
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
as the helicopter removes slack from the sling legs. When
strength.
successful hookup is assured, the hookup team quickly
exits the area underneath the helicopter to the designated
c. Personnel. One person can prepare and rig this load
rendezvous point.
in 10 minutes.
(4) Derigging. Derigging is the reverse of the prepa-
d. Procedures. The following procedures apply to this
ration and rigging procedures in steps d (1) and d (2).
load:
1. Position apex fitting on the trailer in the vicinity of the
spare tire. Route outer sling legs 1 and 2 to the front of the
trailer and inner sling legs 3 and 4 to the rear end. Sling
legs 1 and 3 must be on the left side of the load.
2. Loop the chain end of sling leg 1 through the for-
ward lift provision on the left side of the trailer. Place the
correct link from Table 16-3 in the grab hook. Repeat with
sling leg 2 on the right side.
3. Loop the chain end of sling leg 3 through the aft lift
provision located on the left side of the trailer forward of
the wheels. Place the correct link from Table 16-3 in the
grab hook. Repeat with sling leg 4 and the right rear lift
provision. Secure the excess chain with Type III nylon
cord.
16-5
4. Cluster and tie or tape (breakaway technique) all
sling legs together on top of the trailer to prevent en-
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 the trailer in the vicinity of the
3. Loop the chain end of sling leg 3 through the aft lift
spare tire. Route outer sling legs 1 and 2 to the front of the
provision located on the left side of the trailer forward of
trailer and inner sling legs 3 and 4 to the rear end. Sling
the wheels. Place the correct link from Table 16-3 in the
legs 1 and 3 must be on the left side of the load.
grab hook. Repeat with sling leg 4 and the right rear lift
provision. Secure the excess chain with Type III nylon
2. Loop the chain end of sling leg 1 through the for-
cord.
ward lift provision on the left side of the trailer. Place the
correct link from Table 16-3 in the grab hook. Repeat with
4. Cluster and tie or tape (breakaway technique) all
sling leg 2 on the right side.
sling legs together on top of the trailer to prevent en-
tanglement during hookup and lift-off.
Figure 16-3. M172A1 Semitrailer, Lowbed
16-6
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
16-5. Trailer, Flatbed, Tilt Deck, 15-Ton, 8-Wheel
a. Applicability. The following item in Table 16-4 is suitable for sling load by all ARMY helicopters with suitable lift
capacity:
WARNING
DO NOT LIFT THIS LOAD WITH THE ORIGINAL VEHICLE LIFT PROVISION
Table 16-4. Trailer, Flatbed, Tilt Deck, 15-Ton, 8-Wheel
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Trailer, Flatbed, Tilt Deck, 15-ton,
9,000
10K
50/30
70
8-Wheel
b. Materials. The following materials are required to
drawbar with Type III nylon cord.
rig this load:
(b) Ensure the spare tire is securely attached.
(1) Sling set (10,000-pound capacity).
(c) Engage the parking brake.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(2) Rigging. Rig the load according to the steps in
Figure 16-4.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(3) Hookup. The hookup team stands on the trailer.
(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. Two persons can prepare and rig this
then moves clear of the load but remains close to the load
load in 10 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).
(a) Secure the air hoses and safety chains to the
16-7
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 the trailer bed. Route outer
3. Loop the chain end of sling leg 3 through the lift ring
sling legs 1 and 2 to the front of the trailer and inner sling
located on top of the trailer in the left rear corner. Place
legs 3 and 4 to the rear end. Sling legs 1 and 3 must be on
the correct link from Table 16-4 in the grab hook. Repeat
the left side of the load.
with sling leg 4 and the right rear lift provision. Secure the
excess chain with Type III nylon cord.
2. Loop the chain end of sling leg 1 through the first
hole on the side of the trailer on the left front corner. Place
4. Cluster and tie or tape (breakaway technique) all
the correct link from Table 16-4 in the grab hook. Repeat
sling legs together on top of the trailer to prevent en-
with sling leg 2 on the right side. Secure the excess chain
tanglement during hookup and lift-off.
with Type III nylon cord.
Figure 16-4. Trailer, Flatbed, Tilt Deck, 15-Ton, 8-Wheel
16-8
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
16-6. Trailer-Mounted Welding Shop
a. Applicability. The following item in Table 16-5 is suitable for sling load by all ARMY helicopters with suitable lift
capacity:
Table 16-5. Trailer-Mounted Welding Shop
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Welding Shop, Trailer Mounted
2,960
10K
10/65
110
b. Materials. The following materials are required to
III nylon cord. Secure the safety chains and intervehicular
rig this load:
cable to the trailer tongue with tape or Type III nylon cord.
(1) Sling set (10,000-pound capacity).
(b) Ensure all covers, doors, lids, and latches are
securely fastened.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(c) Engage the parking brake.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(2) Rigging. Rig the load according to the steps in
Figure 16-5.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(3) Hookup. The hookup team stands on the plat-
form to the rear of the trailer near the vise. The static wand
c. Personnel. Two persons can prepare and rig this
person discharges the static electricity with the static
load in 15 minutes.
wand. The hookup person places the apex fitting onto the
aircraft cargo hook. The hookup team then moves clear of
d. Procedures. The following procedures apply to this
the load but remains close to the load as the helicopter
load:
removes slack from the sling legs. When successful
hookup is assured, the hookup team quickly exits the area
(1) Preparation. Prepare the load using the following
underneath the helicopter to the designated rendezvous
steps:
point.
(a) Secure all tie-down handles on tanks with Type
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
16-9
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 center of the load.
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 trailer and
lift provision located on the left rear corner of the trailer.
inner sling legs 3 and 4 to the rear end. Sling legs 1 and 3
Place the correct link from Table 16-5 in the grab hook.
must be on the left side of the load.
Repeat with sling leg 4 and the right rear lift provision.
Secure the excess chain with Type III nylon cord.
2. Loop the chain end of sling leg 1 through the lunette
of the trailer. Place the correct link from Table 16-5 in the
4. Cluster and tie or tape (breakaway technique) all
grab hook. Repeat with sling leg 2 on the right side. Se-
sling legs together on top of the trailer to prevent en-
cure the excess chain with Type III nylon cord.
tanglement during hookup and lift-off.
Figure 16-5. Trailer-Mounted Welding Shop
16-10
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
16-7. LEB 300 Welding Machine on 2 1/2-ton Trailer Chassis
a. Applicability. The following item in Table 16-6 is suitable for sling load by all ARMY helicopters with suitable lift
capacity:
Table 16-6. LEB 300 Welding Machine on 2 1/2-ton Trailer Chassis
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Welding Machine, Arc, LEB 300, on 2
5,310
10K
28/3
100
1/2-ton Trailer
b. Materials. The following materials are required to
(b) Secure the brake hoses, safety hoses, and chains
rig this load:
to the trailer tongue with tape or Type III nylon cord.
(1) Sling set (10,000-pound capacity).
(c) Secure the OVE chock blocks on the trailer racks
with Type III nylon cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(d) Close and secure all lids, doors, and caps.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(2) Rigging. Rig the load according to the steps in
Figure 16-6.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(3) Hookup. The hookup team stands on the plat-
form to the rear of the trailer near the vise. The static wand
(5) Chock blocks (2 each) (addition to OVE blocks).
person discharges the static electricity with the static
wand. The hookup person places the apex fitting onto the
c. Personnel. One person can prepare and rig this load
aircraft cargo hook. The hookup team then moves clear of
in 10 minutes.
the load but remains close to the load as the helicopter
removes slack from the sling legs. When successful
d. Procedures. The following procedures apply to this
hookup is assured, the hookup team quickly exits the area
load:
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) Place chock blocks in front and behind the wheels.
16-11
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 apex fitting on top of the welding machine.
3. Loop the chain end of sling leg 3 around the rear
Route outer sling legs 1 and 2 to the front of the trailer and
crossmember and back up by the welder on the left rear
inner sling legs 3 and 4 to the rear. Sling legs 1 and 3 must
corner of the trailer. Place the correct link from Table 16-6
be on the left side of the load.
in the grab hook. Repeat with sling leg 4 and the right rear
corner of the trailer.
2. Loop the chain end of sling leg 1 down through the
left front lift provision on the LEB 300 arc welder, around
4. Cluster and tie or tape (breakaway technique) all
the trailer frame, and back up by the welder. Place the
sling legs together on top of the welder to prevent en-
correct link from Table 16-6 in the grab hook. Repeat with
tanglement during hookup and lift-off.
sling leg 2 on the right side. Secure the excess chain with
Type III nylon cord.
Figure 16-6. LEB 300 Welding Machine on 2 1/2-ton Trailer Chassis
16-12
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
16-8. Trailer-Mounted Compressor, Reciprocating
a. Applicability. The following item in Table 16-7 is suitable for sling load by all ARMY helicopters with suitable lift
capacity:
Table 16-7. Trailer-Mounted Compressor, Reciprocating
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Trailer-Mounted Compressor,
900
10K
10/15
90
Reciprocating
b. Materials. The following materials are required to
(b) Secure the brake hoses, safety hoses, and chains
rig this load:
to the trailer tongue with tape or Type III nylon cord.
(1) Sling set (10,000-pound capacity).
(c) Close and secure all lids, doors, and caps.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(d) Engage parking brake.
roll.
(2) Rigging. Rig the load according to the steps in
(3) Cord, nylon, Type III, 550-pound breaking strength.
Figure 16-7.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(3) Hookup. The hookup team stands along side the
strength.
trailer. The static wand person discharges the static elec-
tricity with the static wand. The hookup person places
c. Personnel. Two 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 the front leg in the down position.
16-13
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 apex fitting on top of the compressor. Route
3. Loop the chain end of sling leg 3 around the rear
outer sling legs 1 and 2 to the front of the trailer and inner
frame member to the left of the fuel tank. Place the correct
sling legs 3 and 4 to the rear. Sling legs 1 and 3 must be on
link from Table 16-7 in the grab hook. Repeat with sling
the left side of the load.
leg 4 and the right rear corner of the trailer. Secure the
excess chain with Type III nylon cord.
2. Loop the chain end of sling leg 1 through the lunette.
Place the correct link from Table 16-7 in the grab hook.
4. Cluster and tie or tape (breakaway technique) all
Repeat with sling leg 2 on the right side. Secure the ex-
sling legs together on top of the compressor to prevent
cess chain with Type III nylon cord.
entanglement during hookup and lift-off.
Figure 16-7. Trailer-Mounted Compressor, Reciprocating
16-14
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
16-9. Trailer-Mounted AN/MTC-10
a. Applicability. The following item in Table 16-8 is suitable for sling load by all ARMY helicopters with suitable lift
capacity:
Table 16-8. Trailer-Mounted AN/MTC-10
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
AN/MTC-10, Telephone Control
1,800
10K
3/3
70
Office Group on M416 Trailer
b. Materials. The following materials are required to
(b) Stow the accompanying load in the trailer bed
rig this load:
and secure with Type III nylon cord.
(1) Sling set (10,000-pound capacity).
(c) Tape all fittings on the trailer and tongue.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(d) Fold rear stand before hookup to helicopter.
roll.
(2) Rigging. Rig the load according to the steps in
(3) Cord, nylon, Type III, 550-pound breaking strength.
Figure 16-8.
(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
c. Personnel. Two persons can prepare and rig this
the apex fitting onto the aircraft cargo hook. The hookup
load in 30 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) Remove the tarpaulin and all external items; stow
in the bed of the trailer.
16-15
|
|