FM 10-450-4 MULTISERVICE HELICOPTER SLING LOAD: SINGLE-POINT LOAD RIGGING PROCEDURES (September 2003) - page 8

 

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FM 10-450-4 MULTISERVICE HELICOPTER SLING LOAD: SINGLE-POINT LOAD RIGGING PROCEDURES (September 2003) - page 8

 

 

FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-13. Roller, Towed, Vibrating
a. Applicability. The following item in Table 8-12 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-12. Roller, Towed, Vibrating
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Roller, Towed, Vibrating
4,830
10K
3/3
120
b. Materials. The following materials are required to
stowed or travel position and secure it with Type III nylon
rig this load:
cord.
(1) Sling set (10,000-pound capacity).
(b) Ensure the battery box cover, fuel cap, hoses,
and all loose items are secured. Tape or tie any loose
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
items as required.
roll.
(2) Rigging. Rig the load according to the steps in
(3) Cord, nylon, Type III, 550-pound breaking strength.
Figure 8-12.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(3) Hookup. The hookup team stands alongside 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 each
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) Lift the tongue and position the support leg in its
8-27
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 roller. Route
respective lift provision. Place the correct link from Table
outer sling legs 1and 2 to the front of the load (tongue
8-12 in the grab hook.
end). Route inner sling legs 3 and 4 to the rear of the load.
Sling legs 1 and 3 must be on the left side of the load.
3. Cluster and tie or tape (breakaway technique) the
sling legs together on top of the roller to prevent en-
2. Route the chain end of each sling leg through its
tanglement during hookup and lift-off.
Figure 8-12. Roller, Towed, Vibrating
8-28
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-14. Mk155 Launcher, Mine Clearing
a. Applicability. The following item in Table 8-13 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-13. Mk155 Launcher, Mine Clearing
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Mk155 Launcher, Mine Clearing
860
10K
3/3
80
b. Materials. The following materials are required to
(a) Ensure the launch rail is in the collapsed or stor-
rig this load:
age mode and not in its vertical position.
(1) Sling set (10,000-pound capacity).
(b) Ensure the storage box lid is closed and secured
with Type III nylon cord or tape.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(2) Rigging. Rig the load according to the steps in
Figure 8-13.
(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
launcher. The static wand person discharges the static
strength.
electricity 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 each
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).
8-29
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 launch rail.
ring on the other side of the storage box.
Route outer sling legs 1 and 2 to the front of the load .
Route inner sling legs 3 and 4 to the rear of the load. Sling
3. Loop the chain end of sling leg 3 through the left rear
legs 1 and 3 must be on the left side of the load.
lift ring. Place the correct link from Table 8-13 in the grab
hook. Repeat with sling leg 4 and the right rear lift ring.
2. Loop the chain end of sling leg 1 through the left
front lift ring located behind the left rear corner of the
4. Cluster and tie or tape (breakaway technique) the
storage box. Place the correct link from Table 8-13 in the
sling legs together on top of the launch rail to prevent
grab hook. Repeat with sling leg 2 and the right front lift
entanglement during hookup and lift-off.
Figure 8-13. Mk155 Launcher, Mine Clearing
8-30
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-15. M68A2 Line Charge, Demolition with or without Mk22 Rocket Motor
a. Applicability. The following items in Table 8-14 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-14. M68A2 Line Charge, Demolition
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
M68A2 Line Charge, Demolition, Inert
2,486
10K
3/3
70
M68A2 Line Charge, Demolition with
2,672
10K
3/3
70
Mk22 Rocket Motor
b. Materials. The following materials are required to
(d) Center the rocket motor box on top of the line
rig this load:
charge container.
(1) Sling set (10,000-pound capacity).
(e) Connect two CGU-1/B tie-down straps together
to form one long strap. Route the strap around the line
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
charge and rocket motor box lengthwise. Tighten the
roll.
strap securely.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(f) Route two CGU-1/B tie-down straps across the
rocket motor box and underneath the line charge con-
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
tainer. Position the strap at each end of the containers
strength.
approximately equal distance from the center. Tighten the
strap securely. Secure the excess tie-down strap with tape
(5) Tie-down strap, CGU-1B (4 each).
or Type III nylon cord.
c. Personnel. Two persons can prepare and rig each
NOTE: When rigging the line charge without the rocket
load in 20 minutes.
motor omit steps d (1) (c) through (f).
d. Procedures. The following procedures apply to this
(2) Rigging. Rig the load according to the steps in
load:
Figure 8-14.
(1) Preparation. Prepare the load using the following
(3) Hookup. The hookup team stands alongside the
steps:
line charge. The static wand person discharges the static
electricity with the static wand. The hookup person places
(a) Ensure the end of the load opposite the electrical
the apex fitting onto the aircraft cargo hook. The hookup
connectors and fuse storage area is designated as the
team then moves clear of the load but remains close to the
front of the load.
load as the helicopter removes slack from the sling legs.
When successful hookup is assured, the hookup team
(b) Ensure the storage box lid is closed and secured
quickly exits the area underneath the helicopter to the
with Type III nylon cord or tape.
designated rendezvous point.
(c) Ensure the rocket motor box is secured with metal
(4) Derigging. Derigging is the reverse of the prepa-
strapping.
ration and rigging procedures in steps d (1) and d (2).
8-31
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
3. Loop the chain end of sling leg 3 through the left rear
1. Position the apex fitting on top of the container.
lift ring. Place the correct link from Table 8-14 in the grab
Route outer sling legs 1 and 2 to the front of the load .
hook. Repeat with sling leg 4 and the right rear lift ring.
Route inner sling legs 3 and 4 to the rear of the load. Sling
legs 1 and 3 must be on the left side of the load.
4. Cluster and tie or tape (breakaway technique) the
2. Loop the chain end of sling leg 1 through the left
sling legs together on top of the launch rail to prevent
front lift ring. Place the correct link from Table 8-14 in the
entanglement during hookup and lift-off.
grab hook. Repeat with sling leg 2 and the right front lift
ring.
Figure 8-14. M68A2 Line Charge, Demolition
8-32
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-16. Mk155 Launcher with or without M68A2 Demolition Line Charge and Mk22 Rocket
Motor on M353 Trailer
a. Applicability. The following items in Table 8-15 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-15. Mk155 Launcher on M353 Trailer
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Mk155 Launcher
3,700
10K
3/3
90
Mk155 Launcher with M68A2
Demolition Charge and Mk22 Rocket
6,312
10K
3/3
100
Motor
b. Materials. The following materials are required to
(b) Ensure the storage box lid is closed and secured
rig this load:
with Type III nylon cord or tape (if installed).
(1) Sling set (10,000-pound capacity).
(c) Tie off hoses and safety chains and secure any
loose items with nylon cord or tape.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(d) Set the parking brake.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(e) Place and secure the Mk22 rocket motor box in-
side the aircraft using the CGU-1/B tie-down straps (if
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
required).
strength.
(2) Rigging. Rig the load according to the steps in
(5) Tie-down strap, CGU-1B (4 each).
Figure 8-15.
c. Personnel. Two persons can prepare and rig each
(3) Hookup. The hookup team stands on the trailer
load in 20 minutes.
chassis. The static wand person discharges the static
electricity 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) Ensure the launcher is securely attached to the
trailer chassis. Ensure the launch rail is in the collapsed
(4) Derigging. Derigging is the reverse of the prepa-
or storage mode and not in its vertical position.
ration and rigging procedures in steps d (1) and d (2).
8-33
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 launcher. Route
lift provision on the trailer chassis located aft of the trailer
outer sling legs 1 and 2 to the front of the trailer and the
left wheel. Place the correct link from Table 8-15 in the
inner sling legs 3 and 4 to the rear. Sling legs 1 and 3
grab hook. Repeat with sling leg 4 and the right rear lift
should be to the left side of the load.
provision.
2. Loop the chain end of sling leg 1 through the left
4. Raise the apex fitting above the launcher and tie or
front lift provision on the trailer chassis located aft of the
tape sling legs to the launch rail to prevent entanglement
left leveling wheel assembly. Place the correct link from
during hookup.
Table 8-15 in the grab hook. Repeat with sling leg 2 and
the right front lift provision.
5. Cluster and tie or tape (breakaway technique) all sling
legs above the launch rail to prevent entanglement during
3. Loop the chain end of sling leg 3 through the left rear
hookup and lift-off.
Figure 8-15. Mk155 Launcher on M353 Trailer
8-34
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-17. Mk155 Launcher with or without M68A2 Demolition Line Charge and Mk22 Rocket
Motor on M200A1 or Mobile-Trac System (MTS) Trailer
a. Applicability. The following items in Table 8-16 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-16. Mk155 Launcher on M200A1 or MTS Trailer
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Mk155 Launcher on M200A1 Trailer
3,330
10K
3/3
90
Mk155 Launcher, M68A2 Demolition
Charge, and Mk22 Rocker Motor on
5,620
10K
10/3
110
M200A1 Trailer
Mk155 Launcher, M68A2 Demolition
Charge, and Mk22 Rocker Motor on
7,172
10K
10/3
110
the Mobile-Trac System Trailer (MTS)
b. Materials. The following materials are required to
(b) Ensure the storage box lid is closed and secured
rig this load:
with Type III nylon cord or tape (if installed).
(1) Sling set (10,000-pound capacity).
(c) Tie off hoses and safety chains and secure any
loose items with nylon cord or tape.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(d) Set the parking brake.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(e) Place and secure the Mk22 rocket motor box in-
side the aircraft using the CGU-1/B tie-down straps (if
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
required).
strength.
(2) Rigging. Rig the load according to the steps in
(5) Tie-down strap, CGU-1B (4 each).
Figure 8-16.
c. Personnel. Two persons can prepare and rig each
(3) Hookup. The hookup team stands on the trailer
load in 20 minutes.
chassis or on the charge. The static wand person dis-
charges the static electricity with the static wand. The
d. Procedures. The following procedures apply to this
hookup person places the apex fitting onto the aircraft
load:
cargo hook. The hookup team then moves clear of the
load but remains close to the load as the helicopter re-
(1) Preparation. Prepare the load using the following
moves slack from the sling legs. When successful hookup
steps:
is assured, the hookup team quickly exits the area under-
neath the helicopter to the designated rendezvous point.
(a) Ensure the launcher is securely attached to the
trailer chassis. Ensure the launch rail is in the collapsed
(4) Derigging. Derigging is the reverse of the prepa-
or storage mode and not in its vertical position.
ration and rigging procedures in steps d (1) and d (2).
8-35
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 launcher. Route
lift provision on the trailer chassis located aft of the demo-
outer sling legs 1 and 2 to the front of the trailer and the
lition charge container. Place the correct link from Table 8-
inner sling legs 3 and 4 to the rear. Sling legs 1 and 3
16 in the grab hook. Repeat with sling leg 4 and the right
should be to the left side of the load.
rear lift provision.
2. Loop the chain end of sling leg 1 through the left
4. Raise the apex fitting above the launcher and tie or
front lift provision on the trailer chassis located aft of the
tape sling legs to the launch rail to prevent entanglement
lunette. Place the correct link from Table 8-16 in the grab
during hookup.
hook. Repeat with sling leg 2 and the right front lift provi-
sion.
5. Cluster and tie or tape (breakaway technique) all sling
legs above the launch rail to prevent entanglement during
3. Loop the chain end of sling leg 3 through the left rear
hookup and lift-off.
Figure 8-16. Mk155 Launcher on M200A1 or MTS Trailer
8-36
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-18. LRT-110, 7 1/2-Ton Crane
a. Applicability. The following item in Table 8-17 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-17. LRT-110, 7 1/2-Ton Crane
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
LRT-110 Crane
24,230
25K
3/3
120
b. Materials. The following materials are required to
(b) Ensure the wheels are pointing straight ahead.
rig this load:
Secure the steering wheel with nylon cord or tape.
(1) Sling set (25,000-pound capacity).
(c) Secure doors, tool box covers, and all loose equip-
ment with nylon cord or tape. Secure hook-block assem-
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
bly to the end of the boom mast with CGU-l/B cargo tie-
roll.
down or equivalent.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(d) Secure boom light power cable with nylon cord
or tape.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(e) Insert wooden cable wedges at the drum to pre-
vent the cable from unspooling if the cable becomes slack.
(5) Tie-down strap, CGU-1B (4 each).
Secure wedges with 1/2-inch tubular nylon.
(6) Webbing, tubular, nylon, 1/2-inch.
(f) Set the parking brake.
(7) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
(2) Rigging. Rig the load according to the steps in
substitute.
Figure 8-17.
c. Personnel. Two persons can prepare and rig each
(3) Hookup. The hookup team stands beside the left
load in 20 minutes.
and right side of the boom base. The static wand person
discharges the static electricity with the static wand. The
d. Procedures. The following procedures apply to this
hookup person places the apex fitting onto the aircraft
load:
cargo hook. The hookup team then moves clear of the
load but remains close to the load as the helicopter re-
(1) Preparation. Prepare the load using the following
moves slack from the sling legs. When successful hookup
steps:
is assured, the hookup team quickly exits the area under-
neath the helicopter to the designated rendezvous point.
(a) Fold side mirrors in toward cab and tie or tape, as
necessary. Tape or secure windshield wipers to wind-
(4) Derigging. Derigging is the reverse of the prepa-
shield.
ration and rigging procedures in steps d (1) and d (2).
8-37
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 directly above
3. Loop the chain end of sling leg 3 through the lift
the boom base. Route outer sling legs 1 and 2 to the front
provision located on the inboard side of the left rear
(cab end) of the crane and the inner sling legs 3 and 4 to
outrigger. Place the correct link from Table 8-17 in the grab
the rear. Sling legs 1 and 3 must be on the left (driver’s)
hook. Repeat with sling leg 4 on the right rear outrigger.
side of the load.
4. Pad the sling legs where they contact the crane cab.
2. Loop the chain end of sling leg 1 through the lift
provision located on the inboard side of the front left
5. Cluster and tie or tape (breakaway technique) all sling
outrigger. Place the correct link from Table 8-17 in the grab
legs together to prevent entanglement during hookup and
hook. Repeat with sling leg 2 on the right front outrigger.
lift-off.
Figure 8-17. LRT-110, 7 1/2-Ton Crane
8-38
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-19. LRT-110, 7 1/2-Ton Crane (Boom)
a. Applicability. The following item in Table 8-18 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-18. LRT-110, 7 1/2-Ton Crane (Boom)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
LRT-110 Crane (Boom)
8,600
10K
3/3
140
b. Materials. The following materials are required to
(b) Secure hook-block assembly to the end of the
rig this load:
boom mast with CGU-l/B cargo tie-down or equivalent.
(1) Sling set (10,000-pound capacity).
(c) Secure boom light power cable with nylon cord
or tape.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(d) Insert wooden cable wedges at the drum to pre-
vent the cable from unspooling if the cable becomes slack.
(3) Cord, nylon, Type III, 550-pound breaking strength.
Secure wedges with 1/2-inch tubular nylon.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(e) Secure the boom hydraulic hoses with tape or
strength.
nylon cord. Make sure the hoses are clear of the boom
base.
(5) Tie-down strap, CGU-1B (4 each).
(2) Rigging. Rig the load according to the steps in
(6) Webbing, tubular, nylon, 1/2-inch.
Figure 8-18.
c. Personnel. Two persons can prepare and rig each
(3) Hookup. The hookup team stands beside the
load in 20 minutes.
boom. 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) Sectionalize the crane according to instructions
in the operator’s manual.
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
8-39
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 directly above
3. Loop the chain end of sling leg 3 through the lift
the boom base. Route outer sling legs 1 and 2 to the front
provision located on the left side near the middle of the
(counterweight) end and inner sling legs 3 and 4 to the
boom. Place the correct link from Table 8-18 in the grab
rear (hook) end. Sling legs 1 and 3 must be on the left side
hook. Repeat with sling leg 4 on the right side.
of the boom.
4. Cluster and tie or tape (breakaway technique) all sling
2. Loop the chain end of sling leg 1 through the lift
legs together to prevent entanglement during hookup and
provision located on top of the boom left support arm
lift-off.
near the counterweight end. Place the correct link from
Table 8-18 in the grab hook. Repeat with sling leg 2 on the
right side support arm.
Figure 8-18. LRT-110, 7 1/2-Ton Crane (Boom)
8-40
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-20. LRT-110, 7 1/2-Ton Crane (Power Unit)
a. Applicability. The following item in Table 8-19 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-19. LRT-110, 7 1/2-Ton Crane (Power Unit)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
LRT-110 Crane (Power Unit)
15,600
25K
3/3
140
b. Materials. The following materials are required to
(a) Sectionalize the crane according to instructions
rig this load:
in the operator’s manual.
(1) Sling set (25,000-pound capacity).
(b) Fold side mirrors in toward cab and tie or tape, as
necessary. Tape or secure windshield wipers to wind-
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
shield.
roll.
(c) Ensure the wheels are pointing straight ahead.
(3) Cord, nylon, Type III, 550-pound breaking strength.
Secure the steering wheel with nylon cord or tape. En-
gage the parking brake.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(d) Secure doors, tool box covers, and all loose equip-
ment with nylon cord or tape.
(5) Tie-down strap, CGU-1B (4 each).
(2) Rigging. Rig the load according to the steps in
(6) Webbing, tubular, nylon, 1/2-inch.
Figure 8-19.
(7) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
(3) Hookup. The hookup team stands beside the left
substitute.
and right side of the boom base. The static wand person
discharges the static electricity with the static wand. The
c. Personnel. Two persons can prepare and rig each
hookup person places the apex fitting onto the aircraft
load in 20 minutes.
cargo hook. The hookup team then moves clear of the
load but remains close to the load as the helicopter re-
d. Procedures. The following procedures apply to this
moves slack from the sling legs. When successful hookup
load:
is assured, the hookup team quickly exits the area under-
neath 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).
8-41
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 base attach-
3. Loop the chain end of sling leg 3 through the lift
ing point. Route outer sling legs 1 and 2 to the front (cab
provision located on the inboard side of the left rear
end) of the crane and the inner sling legs 3 and 4 to the
outrigger. Place the correct link from Table 8-19 in the grab
rear. Sling legs 1 and 3 must be on the left (driver’s) side of
hook. Repeat with sling leg 4 on the right rear outrigger.
the load.
4. Pad the sling legs where they contact the crane cab.
2. Loop the chain end of sling leg 1 through the lift
provision located on the inboard side of the front left
5. Cluster and tie or tape (breakaway technique) all sling
outrigger. Place the correct link from Table 8-19 in the grab
legs together to prevent entanglement during hookup and
hook. Repeat with sling leg 2 on the right front outrigger.
lift-off.
Figure 8-19. LRT-110, 7 1/2-Ton Crane (Power Unit)
8-42
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-21. Truck, Forklift, MC-4000
a. Applicability. The following item in Table 8-20 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-20. Truck, Forklift, MC-4000
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Truck, Forklift, Rough Terrain,
8,600
15K
4/10
90
MC-4000, TAMCN B2565
b. Materials. The following materials are required to
(b) Secure the seat cushion and steering wheel with
rig this load:
Type III nylon cord. Engage the hand brake and place the
transmission in neutral.
(1) Sling set (15,000-pound capacity).
(c) Ensure the fuel tank is less than 3/4 full.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(d) Raise the fork tines 1 foot above the ground.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(2) Rigging. Rig the load according to the steps in
Figure 8-20.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(3) Hookup. The hookup team stands on top of the
engine deck. The static wand person discharges the static
c. Personnel. Two persons can prepare and rig each
electricity with the static wand. The hookup person places
load in 20 minutes.
the apex fitting onto the aircraft cargo hook. The hookup
team then moves clear of the load but remains close to the
d. Procedures. The following procedures apply to this
load as the helicopter removes slack from the sling legs.
load:
When successful hookup is assured, the hookup team
quickly exits the area underneath the helicopter to the
(1) Preparation. Prepare the load using the following
designated rendezvous point.
steps:
(4) Derigging. Derigging is the reverse of the prepa-
(a) Insert the articulating lock pin to keep the front
ration and rigging procedures in steps d (1) and d (2).
and rear sections from twisting while in flight.
8-43
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 engine
grab hook. Repeat with sling leg 4 and the right rear lift
hood or ROPS. Route outer sling legs 1 and 2 to the front
provision.
of the forklift and inner sling legs 3 and 4 to the rear of the
engine area. Sling legs 1 and 3 must be on the left side of
4. Pull the front sling legs up and tape or tie (breakaway
the load.
technique) the grab links to the front side of the upper
light brackets to ensure the sling legs do not become en-
2. Loop the chain end of sling leg 1 through the left
tangled.
front lift provision (not the tie-down provision) that is
located directly above the forward axle housing between
5. Pull the aft sling legs together on top of the engine
the left front tire and the hydraulic cylinder. Place the
compartment and tie or tape (breakaway technique) the
correct link from Table 8-20 in the grab hook. Repeat with
two grab links together.
sling leg 2 on the right front lift provision.
6. Cluster and tie or tape (breakaway technique) all
3. Loop the chain end of sling leg 3 through the left rear
sling legs together on top of the forklift to prevent en-
lift provision. Place the correct link from Table 8-20 in the
tanglement during hookup and lift-off.
Figure 8-20. Truck, Forklift, MC-4000
8-44
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-22. Truck, Forklift, RT4000
a. Applicability. The following item in Table 8-21 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-21. Truck, Forklift, RT4000
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Truck, Forklift, Rough Terrain,
10,860
15K
3/10
120
4000-pound capacity, TAMCN B2566
b. Materials. The following materials are required to
transmission in neutral.
rig this load:
(b) Ensure the fuel tank is less than 3/4 full.
(1) Sling set (15,000-pound capacity).
(c) Raise the fork tines 1 foot above the ground. Lift
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
the fork ends upward and secure to the lift cylinder frame
roll.
using the CGU-1B straps.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(d) Tape the end of the exhaust pipe.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(2) Rigging. Rig the load according to the steps in
strength.
Figure 8-21.
(5) Tie-down strap, CGU-1B (4 each).
(3) Hookup. The hookup team stands on top of the
falling objects protection system (FOPS). The static wand
c. Personnel. Two persons can prepare and rig each
person discharges the static electricity with the static
load in 10 minutes.
wand. The hookup person places the apex fitting onto
the aircraft cargo hook. The hookup team then moves
d. Procedures. The following procedures apply to this
clear of the load but remains close to the load as the heli-
load:
copter removes slack from the sling legs. When success-
ful hookup is assured, the hookup team quickly exits the
(1) Preparation. Prepare the load using the following
area underneath the helicopter to the designated rendez-
steps:
vous point.
(a) Secure the seat cushion and steering wheel with
(4) Derigging. Derigging is the reverse of the prepa-
Type III nylon cord. Engage the hand brake and place the
ration and rigging procedures in steps d (1) and d (2).
8-45
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 falling object pro-
grab hook. Repeat with sling leg 4 and the right rear lift
tection system (FOPS). Route outer sling legs 1 and 2 to
provision. Secure excess chain with tape or nylon cord.
the front of the forklift and inner sling legs 3 and 4 to the
rear of the engine area. Sling legs 1 and 3 must be on the
4. Pull the front sling legs up and tape or tie (breakaway
left side of the load.
technique) the grab links to the front side of the upper
light brackets to ensure the sling legs do not become en-
2. Loop the chain end of sling leg 1 through the left
tangled.
front lift provision (not the tie-down provision) that is
located directly above the forward axle housing between
5. Pull the aft sling legs together on top of the engine
the left front tire and the hydraulic cylinder. Place the
compartment and tie or tape (breakaway technique) the
correct link from Table 8-21 in the grab hook. Repeat with
two grab links together.
sling leg 2 on the right front lift provision.
6. Cluster and tie or tape (breakaway technique) all
3. Loop the chain end of sling leg 3 through the left rear
sling legs together on top of the FOPS to prevent en-
lift provision. Place the correct link from Table 8-21 in the
tanglement during hookup and lift-off.
Figure 8-21. Truck, Forklift, RT4000
8-46
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-23. MHE-270/MHE-271 Truck, Forklift, RT4000
a. Applicability. The following items in Table 8-22 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-22. MHE-270/MHE-271 Truck, Forklift, RT4000
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
MHE-270 without cab, NSN
11,700
25K
40/3
125
3930-01-330-8907
MHE-271 with cab, NSN
11,920
25K
40/3
125
3930-01-330-8906
b. Materials. The following materials are required to
disengaged. The tow bar must be free to rotate.
rig this load:
(d) Place the transmission in neutral and straighten
(1) Sling set (25,000-pound capacity).
the front wheels.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(e) Engage the parking brake.
roll.
(f) Secure the doors, chains, fire extinguisher, and all
(3) Cord, nylon, Type III, 550-pound breaking strength.
loose equipment with tape or Type III nylon cord.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(g) Tape all lights, windows and glass fixtures.
strength.
(h) Tape the windshield wipers to the windshield.
c. Personnel. Two persons can prepare and rig each
load in 15 minutes.
(2) Rigging. Rig the load according to the steps in
Figure 8-22.
d. Procedures. The following procedures apply to this
load:
(3) Hookup. The hookup team stands on the rear of
the forklift. The static wand person discharges the static
(1) Preparation. Prepare the load using the following
electricity with the static wand. The hookup person places
steps:
the apex fitting onto the aircraft cargo hook. The hookup
team then moves clear of the load but remains close to the
(a) Tilt the mast back as far as it will go.
load as the helicopter removes slack from the sling legs.
When successful hookup is assured, the hookup team
(b) Ensure the fuel tank is less than 3/4 full.
quickly exits the area underneath the helicopter to the
designated rendezvous point.
(c) Tilt the tow bar up as far as it will go. Ensure both
pins which hold the tow bar in an upright position are
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
8-47
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 rear of the
left rear lift provision located on the left side of the tow
forklift. Route outer sling legs 1and 2 to the mast and
bar. Place the correct link from Table 8-22 in the grab hook.
inner sling legs 3 and 4 to the tow bar. Sling legs 1 and 3
Repeat with sling leg 4 and the right rear lift provision.
must be on the left side of the load.
2. Loop the chain end of sling leg 1 through the left
4. Pull the front sling legs up and tape or tie (breakaway
front lift provision located at the top of the left mast. Place
technique) to the top of the mast to ensure the sling legs
the correct link from Table 8-22 in the grab hook. Repeat
do not become entangled.
with sling leg 2 and the right front lift provision.
5. Cluster and tie or tape (breakaway technique) all
3. Loop the chain end of sling leg 3 down through the
sling legs together on top of the forklift to prevent en-
tanglement during hookup and lift-off.
Figure 8-21. Truck, Forklift, RT4000
8-48
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-24. Truck, Forklift, MC-6000
a. Applicability. The following item in Table 8-23 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-23. Truck, Forklift, MC-6000
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
MC-6000 Forklift
19,800
40K
3/16
85
b. Materials. The following materials are required to
blocks and are tilted all the way aft.
rig this load:
(b) Ensure the fuel tank is less than 3/4 full. Place the
(1) Sling set (40,000-pound capacity).
transmission in neutral and engage the parking brake.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(c) Route two CGU-1/B cargo tie-down straps around
roll.
the rear access doors.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(d) Route two CGU-1/B cargo tie-down straps around
the engine access doors.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(e) Secure the tool box lid with tape or Type III nylon
cord.
(5) Tie-down strap, CGU-1B (4 each).
(2) Rigging. Rig the load according to the steps in
(6) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
Figure 8-23.
substitute.
(3) Hookup. The hookup team stands on top of the
c. Personnel. Two persons can prepare and rig each
engine deck. The static wand person discharges the static
load in 10 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) Position the forks so they are sitting on the travel
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
8-49
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 roll over protection
3. Loop the chain end of sling leg 3 through the left rear
system (ROPS). Route outer sling legs 1 and 2 to the front
lift provision located on the frame aft of the left rear tire.
of the forklift and inner sling legs 3 and 4 to the rear. Sling
Place the correct link from Table 8-23 in the grab hook.
legs 1 and 3 must be on the left side of the load.
Repeat with sling leg 4 and the right rear lift provision.
2. Loop the chain end of sling leg 1 through the left
4. Lift the sling leg and tie or tape (breakaway tech-
front lift provision mounted on the frame inboard of the
nique) the grab hooks to the ROPS. Cluster and tie or tape
left front tire. Place the correct link from Table 8-23 in the
(breakaway technique) all sling legs together on top of
grab hook. Repeat with sling leg 2 and the right front lift
the forklift to prevent entanglement during hookup and
provision.
lift-off.
Figure 8-23. Truck, Forklift, MC-6000
8-50
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-25. Extendable Boom Forklift (EBFL)
a. Applicability. The following item in Table 8-24 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-24. Extendable Boom Forklift (EBFL)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Extendable Boom Forklift, (EBFL),
25,640
40K
3/20
105
TAMCN B2561
b. Materials. The following materials are required to
(b) Raise the carriage 10 inches off the ground, re-
rig this load:
tract and raise the boom.
(1) Sling set (40,000-pound capacity).
(c) Set the parking brake.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(d) Place the gear selector lever in neutral.
roll.
(e) Tape the exhaust pipe end.
(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 8-24.
strength.
(3) Hookup. The hookup team stands on the falling
(5) Tie-down strap, cargo, CGU-1/B (as required).
objects protection system (FOPS). The static wand per-
son discharges the static electricity with the static wand.
c. Personnel. Two persons can prepare and rig each
The hookup person places the apex fitting onto the air-
load in 10 minutes.
craft cargo hook. The hookup team then moves clear of
the load but remains close to the load as the helicopter
d. Procedures. The following procedures apply to this
removes slack from the sling legs. When successful
load:
hookup is assured, the hookup team quickly exits the area
underneath the helicopter to the designated rendezvous
(1) Preparation. Prepare the load using the following
point.
steps:
(4) Derigging. Derigging is the reverse of the prepa-
(a) Secure the forks against the carriage using the
ration and rigging procedures in steps d (1) and d (2).
CGU-1/Bs.
8-51
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 falling object
3. Loop the chain end of sling leg 3 through the left rear
protection system (FOPS). Route outer sling legs 1 and 2
lift provision. Place the correct link from Table 8-24 in the
to the front of the EBFL and inner sling legs 3 and 4 to the
grab hook. Repeat with sling leg 4 and the right rear lift
rear of the EBFL. Sling legs 1 and 3 must be on the left side
provision. Secure excess chain with tape or Type III ny-
of the load.
lon cord.
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 8-24
legs together on top of the FOPS to prevent entanglement
in the grab hook. Repeat with sling leg 2 and the right
during hookup and lift-off.
front lift provision.
Figure 8-24. Extendable Boom Forklift (EBFL)
8-52
C3, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.3A
8-25.1. Extendable Boom Forklift (EBFL) (New Version)
a. Applicability. The following item in Table 8-24.1is certified for all helicopters with suitable lift capacity by the US
Army Soldier Systems Center:
Table 8-24.1. Extendable Boom Forklift (EBFL) (New Version)
MAX
RECOMMENDED
SLING
LINK COUNT
NOMENCLATURE
WEIGH T
AIRSPEE D
SET
FRONT / REA R
(POUNDS )
(KNOTS )
3/48 Cab Side
Extendable Boom Fork
i
28,400
40K
11
0
3/50 Boom Side
b. Materials. The following materials are required to
(e) Lower the boom and tilt the forks all the way
rig this load:
back.
(1) Sling set (40,000-pound capacity).
(f) Secure all latches on the windows with tape or
Type III nylon cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(g) Tape the windshield wipers to the windshield.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(h) Tape all lights and mirrors.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(i) Secure all equipment in the cab with tape or Type
strength.
III nylon cord.
(5) Tiedown strap, cargo, CGU-1/B (as required).
(j) Ensure the wheels are pointed straight ahead and
secure the steering wheel with Type III nylon cord.
c. Personnel. Two persons can prepare and rig this
load in 10 minutes.
(k) Secure the engine cover with Type III nylon
cord.
d. Procedures. The following procedures apply to this
load:
(2) Rigging. Rig the load according to the steps in
Figure 8-24.1.
(1) Preparation. Prepare the load using the following
steps:
(3) Hookup. The hookup team stands on the side of
the load. The static wand person discharges the static
(a) Secure the forks against the carriage using the
electricity with the static wand. The hookup person places
CGU-1/Bs.
the apex fitting onto the aircraft cargo hook. The hookup
team then moves clear of the load but remains close to the
(b) Set the parking brake.
load as the helicopter removes slack from the sling legs.
When successful hookup is assured, the hookup team
(c) Place the gear selector lever in neutral.
quickly exits the area underneath the helicopter to the
designated rendezvous point.
(d) Tape the exhaust pipe end.
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
8-52.1
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 vehicle. 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 EBFL and inner
lift provision. Place the correct link from Table 8-24.1 in
sling legs 3 and 4 to the rear of the EBFL. Sling legs 1 and
the grab hook. Repeat with sling leg 4 and the right rear
3 must be on the left side of the load.
lift provision. Secure excess chain with tape or Type III
nylon cord.
2. Loop the chain end of sling leg 1 through the left
front lift provision. Place the correct link from Table 8-24.1
4. Cluster and tie or tape (breakaway technique) all sling
in the grab hook. Repeat with sling leg 2 and the right
legs together on top of the vehicle to prevent entangle-
front lift provision.
ment during hookup and lift-off.
Figure 8-24.1. Extendable Boom Forklift (EBFL) (New Version)
8-52.2
C3, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.3A
8-25.2. Light Rough Terrain Forklift (LRTF)
a. Applicability. The following item in Table 8-24.2 is certified for all helicopters with suitable lift capacity by the US
Army Soldier Systems Center:
Table 8-24.2. Light Rough Terrain Forklift
M AX
RECOMMENDED
SLING
LINK COUNT
NOMENCLATURE
WEIGH T
AIRSPEE D
SET
FRONT / REA R
(POUNDS )
(KNOTS )
2
/
LightRoughTerrainFork
i
13,700
15K
11
0
3
/
b. Materials. The following materials are required to
(d) Tape the exhaust pipe end.
rig this load:
(e) Secure all latches on the windows with tape or
(1) Multileg sling set (15,000-pound capacity).
Type III nylon cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(f) Tape the windshield wipers to the windshield.
roll.
(g) Tape all lights and mirrors.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(h) Secure all equipment in the cab with tape or Type
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
III nylon cord.
strength.
(i) Ensure the wheels are pointed straight ahead and
(5) Tiedown strap, cargo, CGU-1/B (as required).
secure the steering wheel with Type III nylon cord.
c. Personnel. Two persons can prepare and rig each
(j) Secure the engine cover with Type III nylon cord.
load in 10 minutes.
(2) Rigging. Rig the load according to the steps in
d. Procedures. The following procedures apply to this
Figure 8-24.2.
load:
(3) Hookup. The hookup team stands on the side of
(1) Preparation. Prepare the load using the following
the load. The static wand person discharges the static
steps:
electricity with the static wand. The hookup person places
the apex fitting onto the aircraft cargo hook. The hookup
(a) Slide and secure the forks together in the middle
team then moves clear of the load but remains close to the
of the carriage using CGU-1/Bs.
load as the helicopter removes slack from the sling legs.
When successful hookup is assured, the hookup team
(b) Set the parking brake.
quickly exits the area underneath the helicopter to the
designated rendezvous point.
(c) Place the gear selector lever in neutral.
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
8-52.3
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 vehicle. 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 EBFL and inner
lift provision. Place the correct link from Table 8-24.2 in
sling legs 3 and 4 to the rear of the EBFL. Sling legs 1 and
the grab hook. Repeat with sling leg 4 and the right rear
3 must be on the left side of the load.
lift provision. Secure excess chain with tape or Type III
nylon cord.
2. Loop the chain end of sling leg 1 through the left
front lift provision. Place the correct link from Table 8-24.2
4. Cluster and tie or tape (breakaway technique) all sling
in the grab hook. Repeat with sling leg 2 and the right
legs together on top of the vehicle to prevent entangle-
front lift provision.
ment during hookup and lift-off.
Figure 8-24.2. Light Rough Terrain Forklift
8-52.4
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-26. Welding Shop on M200A1 Trailer
a. Applicability. The following item in Table 8-25 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-25. Welding Shop on M200A1 Trailer
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Welding Shop on M200A1
7,220
10K
3/17
120
b. Materials. The following materials are required to
(b) Secure the safety chains to tow bar of trailer with
rig this load:
tape or Type III nylon cord.
(1) Sling set (10,000-pound capacity).
(c) Secure rear outriggers in position by routing 1/2-
inch tubular nylon over rear deck and under engine hous-
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
ing and tie on outriggers below step plate.
roll.
(d) Secure engine doors and control panel cover by
(3) Cord, nylon, Type III, 550-pound breaking strength.
routing nylon cord around entire engine and tying cord.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(e) The front leg must be in full down position.
strength.
(2) Rigging. Rig the load according to the steps in
(5) Webbing, nylon, tubular, 1/2-inch.
Figure 8-25.
c. Personnel. Two persons can prepare and rig each
(3) Hookup. The hookup team stands on top of the
load in 20 minutes.
trailer. 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) Secure all compressed gas cylinders to trailer
with nylon cord. Ensure all the caps are properly installed.
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
8-53
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 welding shop. 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 trailer and inner
lift provision. Place the correct link from Table 8-25 in the
sling legs 3 and 4 to the rear of the trailer. Sling legs 1 and
grab hook. Repeat with sling leg 4 on the right rear lift
3 should be on the left side of the load.
provision. Secure excess chain with tape or nylon cord.
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 left front corner of the
legs together to prevent entanglement during hookup and
trailer. Place the correct link from Table 8-25 in the grab
lift-off.
hook. Repeat with sling leg 2 on the right front lift provi-
sion.
Figure 8-25. Welding Shop on M200A1 Trailer
8-54
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-27. 250 CFM Air Compressor
a. Applicability. The following item in Table 8-26 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-26. 250 CFM Air Compressor
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Compressor, Air, 250 CFM, LIN
7,425
10K
3/15
100
E72804
b. Materials. The following materials are required to
tape or nylon cord. Tie off hoses on reels to prevent
rig this load:
unrolling. Close and latch all doors and lids.
(1) Sling set (10,000-pound capacity).
(b) Ensure fuel cap is secure. Pad front corners of
shelter along bolt lines with felt and tape.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(c) Tape or tie the lift provisions in the UP position
to prevent fouling.
(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 8-26.
strength.
(3) Hookup. The hookup team stands on top of the
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
trailer. The static wand person discharges the static elec-
substitute.
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 each
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
(4) Derigging. Derigging is the reverse of the prepa-
steps:
ration and rigging procedures in steps d (1) and d (2).
(a) Engage parking brake. Secure light cables with
8-55
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Carefully place apex fitting on top of the compressor.
3. Loop the chain end from sling leg 3 through the left
Route outer sling legs 1 and 2 to the front of the trailer and
rear lift provision. Place the correct link from Table 8-26 in
the inner sling legs 3 and 4 to the rear. Sling legs 1 and 3
the grab hook. Repeat this procedure for sling leg 4. Tape
must be on the left side of the load.
or tie (breakaway technique) the sling legs to prevent foul-
ing the hose reels. Secure excess chain with tape or nylon
2. Loop the chain end from sling leg 1 through the left
cord.
front lift provision on the tongue of the trailer. Place the
correct link from Table 8-26 in the grab hook. Repeat this
4. Cluster and tie or tape (breakaway technique) all sling
procedure for sling leg 2 on the right side of the tongue.
legs together to prevent entanglement during hookup and
lift-off.
Figure 8-26. 250 CFM Air Compressor
8-56
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-28. Pneumatic Tool and Compressor Outfit / Hydraulic Pioneer Tool Outfit (PTO) on M353
Trailer
a. Applicability. The following items in Table 8-27 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-27. Tool Outfits on M353 Trailer
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Pneumatic Tool and Compressor,
8,040
10K
3/18
75
TAMCN B0395
Hydraulic Pioneer Tool Outfit (PTO)
6,740
10K
3/20
100
b. Materials. The following materials are required to
(b) Ensure fuel cap is secure. Secure all loose gear
rig this load:
and doors.
(1) Sling set (10,000-pound capacity).
(c) Secure the light cable to the drawbar with Type
III nylon cord or tape.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(d) Tape all lights, reflectors, and glass fixtures.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(e) Secure the two small wheels
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(2) Rigging. Rig the load according to the steps in
strength.
Figure 8-27.
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
(3) Hookup. The hookup team stands on top of the
substitute.
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 each
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) Engage both hand brakes.
8-57
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 through the lifting
outer sling legs 1 and 2 to the front of the trailer and inner
eye at the left rear corner of the trailer. Place the correct
sling legs 3 and 4 to the rear. Sling legs 1 and 3 must be on
link from Table 8-27 in the grab hook. Repeat with sling
the left side of the load.
leg 4 and the lifting eye at the right rear corner of the
trailer.
2. Loop the chain end of sling leg 1 through the lifting
eye located at the left front corner of the trailer. Place the
4. Cluster and tie or tape (breakaway technique) all sling
correct link from Table 8-27 in the grab hook. Repeat with
legs together on top of the air compressor to prevent en-
sling leg 2 and the lifting eye located at the right front
tanglement during hookup and lift-off. Ensure the rear
corner of the trailer.
sling legs are tied so they do not become entangled under
the hose reels.
Figure 8-27. Tool Outfits on M353 Trailer
8-58
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-29. Fuel Dispensing System, Tactical Airfield (TAFDS)
a. Applicability. The following item in Table 8-28 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-28. Fuel Dispensing System, Tactical Airfield (TAFDS)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Pump, 600 gallon per minute, TAFDS
3,500
15K
5/5
60
b. Materials. The following materials are required to
(b) Tape the engine intake and exhaust openings.
rig this load:
(c) Secure the canvas cover on the pump with Type
(1) Sling set (15,000-pound capacity).
III nylon cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(d) Engage one hand brake.
roll.
(2) Rigging. Rig the load according to the steps in
(3) Cord, nylon, Type III, 550-pound breaking strength.
Figure 8-28.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(3) Hookup. The hookup team stands on the pump
strength.
tires. 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 each
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) Secure the battery cover, inlet plugs, and outlet
plugs with tape or Type III nylon cord.
8-59
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 pump. 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 provision located on the left rear corner of the trailer.
legs 3 and 4 to the rear. Sling legs 1 and 3 must be on the
Place the correct link from Table 8-28 in the grab hook.
left side of the load.
Repeat with sling 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 provision located on the left front corner of the
legs together on top of the pump to prevent entanglement
trailer. Place the correct link from Table 8-28 in the grab
during hookup and lift-off.
hook. Repeat with sling leg 2 and the right front lift provi-
sion.
Figure 8-28. Fuel Dispensing System, Tactical Airfield (TAFDS)
8-60
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-30. Bath Unit Mounted on the M103 Trailer
a. Applicability. The following item in Table 8-29 is certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-29. Bath Unit on M103 Trailer
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Bath Unit on M103 Trailer
4,800
15K
16/30
45
b. Materials. The following materials are required to
(a) Ensure all tanks are empty. Secure all tank covers
rig this load:
and lids with tape or Type III nylon cord.
(1) Sling set (15,000-pound capacity).
(b) Raise and secure the jack mounts 1 foot off the
ground.
(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 8-29.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(3) Hookup. The hookup team stands beside the bath
unit. The static wand person discharges the static elec-
c. Personnel. Two persons can prepare and rig each
tricity with the static wand. The hookup person places
load in 15 minutes.
the apex fitting onto the aircraft cargo hook. The hookup
team then moves clear of the load but remains close to the
d. Procedures. The following procedures apply to this
load as the helicopter removes slack from the sling legs.
load:
When successful hookup is assured, the hookup team
quickly exits the area underneath the helicopter to the
(1) Preparation. Prepare the load using the following
designated rendezvous point.
steps:
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
8-61
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 bath unit. Route
3. Loop the chain end of sling leg 3 around the left rear
outer sling legs 1 and 2 to the front of the trailer and inner
jack mount. Place the correct link from Table 8-29 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 and the right rear jack
the left side of the load.
mount. Secure excess chain with tape or Type III nylon
cord.
2. Loop the chain end of sling leg 1 through the left
front steady jack eye and under the jack mount. Place the
4. Cluster and tie or tape (breakaway technique) all sling
correct link from Table 8-29 in the grab hook. Repeat with
legs together on top of the bath unit to prevent entangle-
sling leg 2 and the right front jack mount. Secure excess
ment during hookup and lift-off.
chain with tape or Type III nylon cord.
Figure 8-29. Bath Unit on M103 Trailer
8-62

 

 

 

 

 

 

 

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