Главная Manuals FM 10-450-4 MULTISERVICE HELICOPTER SLING LOAD: SINGLE-POINT LOAD RIGGING PROCEDURES (September 2003)
|
|
|
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
NOTE: Brief the aircrew to hover to
the side of the load and relax sling
leg tension before releasing the apex
fitting to prevent damage to the mis-
sile pedestal.
RIGGING STEPS
1. Position the apex fitting on top of the crew compart-
3. Route the chain end of sling leg 3 through the left
ment. Route outer sling legs 1and 2 to the front of the load
rear lift provision located on the upper structure of the left
(lunette end). Route inner sling legs 3 and 4 to the rear of
rear stabilizer. Place the correct link from Table 7-2 in the
the load. Sling legs 1 and 3 must be on the left side of the
grab hook. Repeat with sling leg 4 on the right rear lift
load.
provision.
2. Route the chain end of sling leg 1 through the left
4. Cluster and tie or tape (breakaway technique) the
front lift provision located on the upper structure of the
sling legs together on top of the crew compartment to
left front stabilizer. Place the correct link from Table 7-2 in
prevent entanglement during hookup and lift-off.
the grab hook. Repeat with sling leg 2 and the right front
lift provision. Secure the excess chain with Type III nylon
cord.
Figure 7-2. M85 Towed Chaparral Missile System
7-4
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
7-4. Continuous Wave Acquisition Radar (CWAR)
a. Applicability. The following items, components of the HAWK Missile System, in Table 7-3 are certified for all
helicopters with suitable lift capacity by the US Army Natick Research, Development, and Engineering Center:
Table 7-3. Continuous Wave Acquisition Radar (CWAR)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
CWAR, Phase II, on M514 Trailer
4,898
25K
3/14
75
CWAR, Phase III, on M514 Trailer
4,840
25K
3/14
75
b. Materials. The following materials are required to
(b) Extend the rear leveling jack so the CWAR is
rig this load:
level.
(1) Sling set (25,000-pound capacity).
(c) Secure all doors and vents with tape or Type III
nylon cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(d) Secure all safety chains and hoses to the trailer
frame with tape or Type III nylon cord.
(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 7-3.
strength.
(3) Hookup. This load does not use a ground crew to
c. Personnel. Two persons can prepare and rig this
connect the load to the aircraft cargo hook. As the heli-
load in 20 minutes.
copter hovers over the load, the flight engineer hooks the
apex fitting with the helicopter cargo loading pole, lifts the
d. Procedures. The following procedures apply to this
apex fitting up, and places it on the aircraft cargo hook.
load:
The ground crew stands by the trailer and checks to make
sure the sling legs do not become entangled as the heli-
(1) Preparation. Prepare the load using the following
copter removes slack from the sling legs. When success-
steps:
ful hookup is assured, the hookup team quickly exits the
area underneath the helicopter to the designated rendez-
(a) Prepare the CWAR for general travel according
vous point.
to the operator's manual. Secure the shipping cover over
the radar.
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
7-5
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 the apex fitting on top of the radar antenna.
excess chain with Type III nylon cord.
Route outer sling legs 1and 2 to the front of the trailer
(lunette end). Route inner sling legs 3 and 4 to the rear of
4. Pull the front sling legs up and tape or tie (breakaway
the load. Sling legs 1 and 3 must be on the left side of the
technique) the chains together at the top of the leveling
load.
jack bracket. Tape or tie (breakaway technique) the front
sling leg grab hooks to the back of the front compartment
2. Route the chain end of sling leg 1 down through the
so the chains do not become entangled during hookup
opening between the left front leveling jack bracket and
and lift-off.
the trailer A-frame, under the short cross members, and
back up through the opening between the leveling jack
bracket and the front of the trailer chassis. Place the cor-
5. Pull the aft sling legs up and tape or tie (breakaway
rect link from Table 7-3 in the grab hook. Repeat with sling
technique) the grab hooks to the base of the antenna
leg 2 on the right side of the trailer A-frame.
support so the chains do not become entangled in the rear
support leg.
3. Route the chain end of sling leg 3 through the left
rear lift provision located on the left rear corner of the
6. Position the apex fitting so that it sits vertically on
trailer chassis outboard of the support rod. Place the
top of the radar antenna. Tape in place (breakaway tech-
correct link from Table 7-3 in the grab hook. Repeat with
nique) so the helicopter aircrew can pick it up using the
sling leg 4 on the right rear lift provision. Secure the
helicopter cargo loading pole.
Figure 7-3. Continuous Wave Acquisition Radar (CWAR)
7-6
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
7-5. M192E1/M192-1 Zero Length Launcher
a. Applicability. The following items, components of the HAWK Missile System, in Table 7-4 are certified for all
helicopters with suitable lift capacity by the US Army Natick Research, Development, and Engineering Center:
Table 7-4. M192E1/M192-1 Zero Length Launcher
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
M192E1, Guided Missile Launcher,
4,482
25K
53/53
90
Zero Length
M192-1, Guided Missile Launcher,
4,500
15K
47/50
60
Zero Length
b. Materials. The following materials are required to
(d) Load the launcher section control box inside the
rig this load:
helicopter.
(1) Sling set (25,000 or 15,000-pound capacity).
(e) Engage the brakes.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(2) Rigging. Rig the load according to the steps in
roll.
Figure 7-4.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(3) Hookup. The hookup team stands on the launcher
on each side of the pedestal. The static wand person
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
discharges the static electricity with the static wand. The
strength.
hookup person places the apex fitting onto the aircraft
cargo hook. The hookup team then moves clear of the
(5) Webbing, nylon, tubular, 1/2-inch (20' length).
helicopter but remains close to the load as the helicopter
removes slack from the sling legs. When successful
c. Personnel. Two persons can prepare and rig this
hookup is assured, the hookup team quickly exits the area
load in 20 minutes.
underneath the helicopter to the designated rendezvous
point.
d. Procedures. The following procedures apply to this
load:
Due to the relatively small clearance between the
top of the load and the helicopter during hookup, it may
(1) Preparation. Prepare the load using the following
be desirable for the helicopter flight engineer to make the
steps:
hookup using the cargo loading pole (shepherd's hook).
Place the apex fitting on top of the center launch boom,
(a) Prepare the launcher for general travel according
with the pin facing up. Ground crew must stand by to
to the operator's manual.
ensure the sling legs do not become entangled on the
load.
(b) Secure all doors and vents with tape or Type III
nylon cord.
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
(c) Secure all safety chains and hoses to the trailer
frame with tape or Type III nylon cord.
7-7
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 the apex fitting on top of the launch stand
lon, repeat the procedure until there are at least 5 lengths
pedestal. Route outer sling legs 1and 2 to the front of the
of nylon (2 1/2 wraps) between the potted eyes of the two
launcher (lunette end). Route inner sling legs 3 and 4 to
sling legs. Tie the ends of the tubular nylon together with
the rear of the load. Sling legs 1 and 3 must be on the left
a square knot and an overhand knot in each running end.
side of the load.
NOTE: Do not route the tubular nylon between the chains
2. Route the chain end of sling leg 1 through the left
or grab hooks. Failure to attach the tubular nylon be-
front lifting provision located aft of the leveling cylinder
tween the sling leg potted eyes may result in damage to
outboard end. Place the correct link from Table 7-4 in the
the missile launch booms or failure of the load.
grab hook. Repeat with sling leg 2 on the right front lift
provision. Ensure the chain is routed from the inside of
4. Route the chain end of sling leg 3 through the left
the lifting provision to the outside so the hook on the
rear lift provision located above the taillight. Place the
grab hook faces outboard when you insert the chain in
correct link from Table 7-4 in the grab hook. Repeat with
the grab hook. Secure the excess chain with Type III
sling leg 4 on the right rear lift provision. Secure the
nylon cord.
excess chain with Type III nylon cord.
3. Route one end of the tubular nylon through the pot-
5. Pull the sling legs up and tape or tie (breakaway tech-
ted eye of sling leg 1. Route the same end of the tubular
nique) the grab hooks to the boom supports. Cluster and
nylon through the potted eye of sling leg 2. Position the
tape or tie (breakaway technique) all sling legs together
potted eyes of the two sling legs 39 inches apart so the
above the center launch boom to prevent entanglement
sling legs cannot contact the two outer launch booms or
during hookup and lift-off.
the center boom. Using the remainder of the tubular ny-
Figure 7-4. M192E1/M192-1 Zero Length Launcher
7-8
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
7-6. M501E3 Loader-Transporter, Guided Missile
a. Applicability. The following items, components of the HAWK Missile System, in Table 7-5 are certified for all
helicopters with suitable lift capacity by the US Army Natick Research, Development, and Engineering Center:
Table 7-5. M501E3 Loader-Transporter, Guided Missile
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
M501E3 Loader-Transporter, Guided
5,650
25K
3/13
100
Missile
M501E3 Loader-Transporter, Guided
5,300
15K
8/3
80
Missile
b. Materials. The following materials are required to
(b) Secure the super structure arms in the opera-
rig this load:
tional position by engaging the lock pins. THE SUPER
STRUCTURE CANNOT BE ALLOWED TO MOVE.
(1) Sling set (25,000 or 15,000-pound capacity).
(c) Secure all safety chains and hoses to the adja-
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
cent structure with tape or Type III nylon cord.
roll.
(d) Secure all doors and vents with tape or 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 7-5.
c. Personnel. Two persons can prepare and rig this
(3) Hookup. The hookup team stands on the loader-
load in 20 minutes.
transporter on each side of the center of the vehicle. The
static wand person discharges the static electricity with
d. Procedures. The following procedures apply to this
the static wand. The hookup person places the apex fit-
load:
ting onto the aircraft cargo hook. The hookup team then
moves clear of the helicopter but remains close to the load
(1) Preparation. Prepare the load using the following
as the helicopter removes slack from the sling legs. When
steps:
successful hookup is assured, the hookup team quickly
exits the area underneath the helicopter to the designated
(a) With the loader-transporter engine ON, raise the
rendezvous point.
super structure about 3 feet using the EXTENSION lever.
Using the ROLL/ELEVATION, AZIMUTH, and EXTEN-
(4) Derigging. Derigging is the reverse of the prepa-
SION levers, position the super structure in the OPERA-
ration and rigging procedures in steps d (1) and d (2).
TIONAL READY position. Shut the engine down and
place the transmission in neutral.
7-9
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 the apex fitting on top of the loader arm at
hook. Repeat with sling leg 2 on the right front lift provi-
the center of the vehicle. Route outer sling legs 1and 2 to
sion clevis.
the front of the vehicle (driver's compartment). Ensure the
sling legs are routed inboard of the outer two upper hoist-
4. Route the chain end of sling leg 3 through the left
ing beams and outboard of the two lower super structure
rear lift provision clevis inboard of the left rear fender.
arms.
Place the correct link from Table 7-5 in the grab hook.
Repeat with sling leg 4 on the right rear lift provision cle-
2. Route inner sling legs 3 and 4 to the rear of the load
vis. Secure the excess chain with Type III nylon cord.
(engine compartment). Ensure the sling legs are routed
inboard of the outer two upper hoisting beams. Sling legs
5. Pull the sling legs up and tape or tie (breakaway tech-
1 and 3 must be on the left side of the load.
nique) the grab hooks to the hoisting beams. Cluster and
tape or tie (breakaway technique) all sling legs together
3. Route the chain end of sling leg 1 through the left
above the hoisting beams to prevent entanglement dur-
front lift provision clevis located inboard of the left front
ing hookup and lift-off.
wheel. Place the correct link from Table 7-5 in the grab
Figure 7-5. Guided Missile Loader-Transporter
7-10
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
7-7. M1E2 Loading and Storage Missile Pallet
a. Applicability. The following item, component of the HAWK Missile System, in Table 7-6 is certified for all helicop-
ters with suitable lift capacity by the US Army Natick Research, Development, and Engineering Center:
Table 7-6. M1E2 Loading and Storage Missile Pallet
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
M1E2 Loading and Storage Missile
4,670
15K
3/35
100
Pallet on M390C Trailer Chassis
b. Materials. The following materials are required to
6 3/4-ton shackles (NSN 4030-00-278-0699). Ensure the
rig this load:
shackles are properly pinned.
(1) Sling set (15,000-pound capacity).
(c) Secure all cables, safety chains, and hoses to the
adjacent structure with tape or Type III nylon cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(d) Engage the parking brake.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(e) Adjust the forward and aft leveling jacks so the
pads are located just above ground level.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(2) Rigging. Rig the load according to the steps in
Figure 7-6.
c. Personnel. Two persons can prepare and rig this
load in 10 minutes.
(3) Hookup. The hookup team stands on the missile
pallet. 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 helicopter but remains close
(1) Preparation. Prepare the load using the following
to the load as the helicopter removes slack from the sling
steps:
legs. When successful hookup is assured, the hookup
team quickly exits the area underneath the helicopter to
(a) Prepare the missile pallet for general travel in
the designated rendezvous point.
accordance with the operator's manual.
(4) Derigging. Derigging is the reverse of the prepa-
(b) Ensure the 3 1/4-ton shackles initially provided
ration and rigging procedures in steps d (1) and d (2).
with the M390C trailer chassis have been replaced by the
7-11
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position the apex fitting on top of the missile stor-
3. Loop the chain end of sling leg 3 through the open-
age racks. Route outer sling legs 1and 2 to the rear of the
ing aft of the lunette and of the landing wheel on the left
missile pallet and inner sling legs 3 and 4 to the front of the
side of the tongue. Place the correct link from Table 7-6 in
missile pallet (lunette end).
the grab hook. Repeat with sling leg 4 on the side of the
tongue.
2. Route the chain end of sling leg 1 through the left
rear lift provision located on the corner of the trailer above
4. Cluster and tie or tape (breakaway technique) the
the taillight. Route the chain from the inside to the out-
sling legs together on top of the missile storage racks to
side of the lift provision. Place the correct link from Table
prevent entanglement during hookup and lift-off.
7-6 in the grab hook. Repeat with sling leg 2 on the right
rear lift provision. Secure the excess chain with Type III
nylon cord.
Figure 7-6. M1E2 Loading and Storage Missile Pallet
7-12
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
7-8. Pedestal-Mounted Stinger (Avenger)
a. Applicability. The following items in Table 7-7 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 7-7. Pedestal-Mounted Stinger (Avenger)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Stinger, Pedestal-Mounted on M998
8,513
10K
50/5
90
(Avenger)
Stinger, Pedestal-Mounted on M1097
9,087
10K
50/5
90
(Avenger)
(d) Secure all equipment inside the vehicle with tape,
b. Materials. The following materials are required to
nylon cord, or tie-downs. Close and secure the doors (if
rig this load:
installed).
(1) Sling set (10,000-pound capacity).
(e) Ensure the fuel tank is not over 3/4 full. Inspect
the fuel tank, oil filter, and battery caps for proper installa-
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
tion.
roll.
(f) Place the transmission in neutral and set the park-
(3) Cord, nylon, Type III, 550-pound breaking strength.
ing brake.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(g) Ensure the front wheels are pointed straight
strength.
ahead. Secure the steering wheel using the securing de-
vice attached under the dashboard.
c. Personnel. Two persons can prepare and rig this
load in 15 minutes.
(2) Rigging. Rig the load according to the steps in
Figure 7-7.
d. Procedures. The following procedures apply to this
load:
NOTE: Hookup of this load presents substantial risk of
damage to the load or injury to the hookup personnel.
(1) Preparation. Prepare the load using the following
Use of a reach pendant is recommended for this load.
steps:
(3) Hookup. The hookup team stands on top of the
(a) Fold the mirrors in front of the windshield and tie
fire unit. The static wand person discharges the static
together with Type III nylon cord.
electricity with the static wand. The hookup person places
the apex fitting onto the aircraft cargo hook. The hookup
(b) Ensure the Avenger fire unit is secured to the
team then moves clear of the helicopter but remains close
truck. Secure all equipment inside the fire unit with tape,
to the load as the helicopter removes slack from the sling
tie-downs, or nylon cord; close and secure the door.
legs. When successful hookup is assured, the hookup
team quickly exits the area underneath the helicopter to
(c) Disconnect the standard vehicle mounted
the designated rendezvous point.
launcher connectors from the missile pods and secure
them to the fire unit with tape or nylon cord.
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
7-13
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position the apex fitting on top of the fire unit. Route
3. Loop the chain end of sling leg 3 through the left rear
outer sling legs 1and 2 to the front of the vehicle and inner
lift provision located on the rear bumper. Place the correct
sling legs 3 and 4 to the rear of the load. Ensure sling legs
link from Table 7-7 in the grab hook. Place the sling leg in
1 and 3 are on the left side of the load.
the sling guide on top of the fire unit. Repeat with sling
leg 4 on the right rear lift provision.
2. Route the chain end of sling leg 1 through the left
front lift provision that protrudes through the hood. Place
4. Cluster and tie or tape (breakaway technique) the
the correct link from Table 7-7 in the grab hook. Repeat
sling legs together on top of the fire unit to prevent en-
with sling leg 2 on the right front lift provision. Secure the
tanglement during hookup and lift-off.
excess chain with Type III nylon cord.
Figure 7-7. Pedestal-Mounted Stinger (Avenger)
7-14
C3, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.3A
7-9. Pedestal-Mounted Stinger on M1097/M1097A1/M1097A2 HMMWV (Avenger) with
ECU/PPU and an Aluminum Airlift Bumper with or without Bustle Box Stowed on the Roof
a. Applicability. The following items in Table 7-8 are certified for all helicopters with suitable lift capacity by the US
Army Soldier Systems Center:
Table 7-8. Pedestal-Mounted Stinger (Avenger) with Aluminum Airlift Bumper
M AX
RECOMMENDED
SLING
LINK COUNT
NOMENCLATURE
WEIGH T
AIRSPEE D
SET
FRONT / REA R
(POUNDS )
(KNOTS )
S
i
10K
4
/
ECU/PPU on M1097 HMMW V
9,800
70
15K
3
/
(Avenger)
S
i
10K
4
/
ECU/PPU on M1097A 1
9,800
70
15K
3
/
HMMWV (Avenger)
S
i
10,000
10K
4
/
ECU/PPU on M1097A 2
10,300
15K
3
/
70
HMMWV (Avenger)
10,300
25K
3
/
CAUTION
These sling load rigging procedures are for Avengers that have the Aluminum Airlift Bumpers ONLY. Lift provisions
on Steel Airlift Bumpers do not allow for adequate sling clearance.
b. Materials. The following materials are required to
(3) Tape, adhesive, pressure-sensitive, 2-inch wide
rig this load:
roll.
(1) Sling set (10,000-pound capacity).
(4) Cord, nylon, Type III, 550-pound breaking strength.
(a) Chain length, part number 38850-00053-101,
(5) Webbing, cotton, 1/4-inch, 80-pound breaking
from a 10,000-pound capacity sling set (4 each).
strength.
(b) Coupling link, part number 577-0415, from a
(6) Strap, cargo, tiedown, CGU-1/B (2 each, or more
10,000-pound sling set (4 each).
as required to secure cargo).
or
c. Personnel. Two persons can prepare and rig this
load in 15 minutes.
(2) Multileg sling set (15,000-pound capacity).
d. Procedures. The following procedures apply to this
(a) Chain length, part number 34080-4 from a
load:
15,000-pound capacity sling set (8 each).
(1) Preparation. Prepare the load using the following
(b) Coupling link, part number 31611, from a
steps:
15,000-pound sling set (8 each).
7-15
C3, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.3A
(a) Fold the mirrors inward and tie together with
(i) Tape the zippers on the missle pod covers (if
Type III nylon cord.
applicable).
(b) Ensure the Avenger fire unit is secured to the
(j) Extend the sling leg chains by connecting one
truck. Secure all equipment inside the fire unit with tape,
additional chain length to each chain on a 10,000-pound
tiedown straps, or Type III nylon cord; close and secure
capacity sling set with coupling links and two chain
the door.
lengths to each chain on a 15,000-pound capacity sling
set with coupling links.
(c) Disconnect the standard vehicle mounted
launcher connectors from the missile pods and secure
(2) Rigging. Rig the load according to the steps in
them to the fire unit with tape or Type III nylon cord.
Figure 7-8.
(d) Secure all equipment inside the vehicle with tape,
NOTE: Hookup of this load presents substantial risk of
Type III nylon cord, or tiedown straps. Roll up the win-
damage to the load or injury to the hookup personnel.
dows. Close and secure the doors (if installed).
Use of a reach pendant is recommended for this load.
(e) Ensure the fuel tank is not over 3/4 full. Inspect
(3) Hookup. The hookup team stands on top of the
the fuel tank, oil filter, and battery caps for proper installa-
fire unit. The static wand person discharges the static
tion.
electricity with the static wand. The hookup person places
the apex fitting onto the aircraft cargo hook. The hookup
(f) Place the transmission in neutral and set the park-
team then moves clear of the helicopter but remains close
ing brake.
to the load as the helicopter removes slack from the sling
legs. When successful hookup is assured, the hookup
(g) Ensure the front wheels are pointed straight
team quickly exits the area underneath the helicopter to
ahead. Secure the steering wheel using the securing de-
the designated rendezvous point.
vice attached under the dashboard or Type III nylon cord.
(4) Derigging. Derigging is the reverse of the prepa-
(h) Secure the bustle box to the box rack on the roof
ration and rigging procedures in steps d (1) and d (2).
of the vehicle CGU-1/B tiedown straps (if needed).
7-16
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 fire unit. Route
rear sling guide. Loop the chain through the left rear lift
outer sling legs 1and 2 to the front of the vehicle and inner
provision located on the rear bumper. Route the chain
sling legs 3 and 4 to the rear of the load. Ensure sling legs
back through the left sling guide. Place the correct link
1 and 3 are on the left side of the load.
from Table 7-8 in the grab hook. Pull the chains tight and
secure both sides of the chain to the sling guide with
2. Route the chain end of sling leg 1 through the left
Type III nylon cord. Repeat with sling leg 4 using the
front lift provision that protrudes through the hood. Place
right rear lift provision and sling guide.
the correct link from Table 7-8 in the grab hook. Repeat
with sling leg 2 on the right front lift provision. Secure the
4. Cluster and tie or tape (breakaway technique) the
excess chain with Type III nylon cord.
sling legs together on top of the fire unit to prevent en-
tanglement during hookup and lift-off.
3. Route the chain end of sling leg 3 through the left
Figure 7-8. Pedestal-Mounted Stinger on M1097/M1097A1/M1097A2 HMMWV (Avenger) with ECU/PPU and
an Aluminum Airlift Bumper with or without Bustle Box Stowed on the Roof
7-17
C3, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.3A
CHAPTER 8
CERTIFIED SINGLE-POINT RIGGING PROCEDURES FOR ENGINEER EQUIPMENT
8-1. INTRODUCTION
This chapter contains rigging procedures for single-point
procedures for engineer equipment are in this section.
lift of engineer equipment that has been certified for sling
Paragraphs 8-2 through 8-41 give detailed instructions for
load. Each rigging procedure is found in a paragraph that
rigging loads.
includes a description of the load, materials required for
rigging, and steps to complete the procedure. An applica-
NOTE: Reach Pendants may be used on all single point
bility paragraph is also a part of each paragraph and iden-
loads. A static discharge person is not required when
tifies the certified loads. The certified single-point rigging
using a Reach Pendant.
8-2. T-3 Tractor, Crawler
a. Applicability. The following items in Table 8-1 are certified for all helicopters with suitable lift capacity by the US
Army Soldier Systems Center:
Table 8-1. T-3 Tractor, Crawler
M AX
LINK COUNT
RECOMMENDED
NOMENCLATURE
WEIGH T
SLING SET
FRONT /
AIRSPEE D
(POUNDS )
REAR
(KNOTS )
Tractor, Full-Tracked, JD550 wih
Roll Over Protection System
16,662
25K
1
/
90
(ROPS), Towing Winch and
Hydraulic Angle Blade
b. Materials. The following materials are required to
load:
rig this load:
(1) Preparation. Prepare the load using the following
(1) Sling set (25,000-pound capacity).
steps:
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(a) Secure the operator's seat cushion to the seat
roll.
frame with tape or Type III nylon cord.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(b) Remove both canopy lights, wrap in padding,
and store in the toolbox.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(c) Secure all loose covers and panels with tape.
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
(d) Place the transmission in neutral and start the
substitute.
engine. Raise the blade 12 inches above the ground and
align the blade at a 90 degree angle to the tractor. Turn the
c. Personnel. Two persons can prepare and rig this
engine off and tape the ignition key in place.
load in 10 minutes.
(2) Rigging. Rig the load according to the steps in
d. Procedures. The following procedures apply to this
Figure 8-1.
8-1
C3, FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.3A
(3) Hookup. The hookup team stands on the engine
moves slack from the sling legs. When successful hookup
cowl in front of the ROPS. The static wand person dis-
is assured, the hookup team quickly exits the area under-
charges the static electricity with the static wand. The
neath the helicopter to the designated rendezvous point.
hookup person places the apex fitting onto the aircraft
cargo hook. The hookup team then moves clear of the
(4) Derigging. Derigging is the reverse of the prepa-
load but remains close to the load as the helicopter re-
ration and rigging procedures in steps d (1) and d (2).
RIGGING STEPS
1. Position the apex fitting on top of the ROPS. Route
3. Route the chain end of sling leg 3 through the left
outer sling legs 1and 2 to the front of the load. Route
rear lift provision located forward of the left track rear
inner sling legs 3 and 4 to the rear of the load. Sling legs 1
wheel. Place the correct link from Table 8-1 in the grab
and 3 must be on the left side of the load.
hook. Repeat with sling leg 4 on the right rear lift provi-
sion located on the right track.
2. Route the chain end of sling leg 1 through the left
front lift provision located just aft of the front of the left
4. Cluster and tie or tape (breakaway technique) the
track. Place the correct link from Table 8-1 in the grab
sling legs together on top of the crew compartment to
hook. Repeat with sling leg 2 and the right front lift provi-
prevent entanglement during hookup and lift-off.
sion located on the right track. Secure the excess chain
with Type III nylon cord.
Figure 8-1. T-3 Tractor, Crawler
8-2
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-3. D5B Tractor, Dozer
a. Applicability. The following items in Table 8-2 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-2. D5B Tractor, Dozer
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
D5B Tractor, Dozer, Type II, Power
18,915
25K
47/8
70
Section without ROPS
D5B Tractor, Dozer, Type II, Track
13,735
25K
21/3
90
Section
b. Materials. The following materials are required to
(c) Remove the pre-air cleaner and secure it on the
rig this load:
seat with Type III nylon cord.
(1) Sling set (25,000-pound capacity) (2 each).
(d) Secure the operator's seat cushion to the seat
frame with tape or Type III nylon cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(e) Tape all lights and gauges.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(f) Place the transmission in neutral and secure the
safety lock lever with Type III nylon cord.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(2) Rigging. Rig the load according to the steps in
Figure 8-2.
c. Personnel. Four persons can sectionalize the dozer
in 2 1/2 hours and two persons can prepare and rig this
NOTE: Hookup of this load presents substantial risk of
load in 10 minutes.
damage to the load or injury to the hookup personnel.
Use of a reach pendant is recommended for this load.
d. Procedures. The following procedures apply to this
load:
(3) Hookup. The hookup team stands on top of the
power or track section. The static wand person discharges
(1) Preparation. Prepare the load using the following
the static electricity with the static wand. The hookup
steps:
person places the apex fitting onto the aircraft cargo hook.
The hookup team then moves clear of the load but re-
(a) Sectionalize the dozer in accordance with the
mains close to the load as the helicopter removes slack
operator's manual. Do not remove the winch or the winch
from the sling legs. When successful hookup is assured,
pump.
the hookup team quickly exits the area underneath the
helicopter to the designated rendezvous point.
(b) Remove the exhaust stack and secure it on top of
the winch 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).
8-3
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
RIGGING STEPS
TRACK SECTION
POWER SECTION
1. Position the apex fitting on top of the section. Route
1. Position the apex fitting on top of the section. Route
outer sling legs 1and 2 to the front of the load (blade end).
outer sling legs 1and 2 to the front of the load (radiator
Route inner sling legs 3 and 4 to the rear of the load. Sling
end). Route inner sling legs 3 and 4 to the rear of the load.
legs 1 and 3 must be on the left side of the load.
Sling legs 1 and 3 must be on the left side of the load.
2. Route the chain end of sling leg 1 through the left
2. Route the chain end of sling leg 1 through the left
front lift provision. Place the correct link from Table 8-2 in
front lift provision located by the left headlight. Place the
the grab hook. Repeat with sling leg 2 and the right front
correct link from Table 8-2 in the grab hook. Repeat with
lift provision. Secure the excess chain with Type III nylon
sling leg 2 and the right front lift provision. Secure the
cord.
excess chain with Type III nylon cord.
3. Route the chain end of sling leg 3 through the left
3. Route the chain end of sling leg 3 through the left
rear lift provision. Place the correct link from Table 8-2 in
rear lift provision located beside the fuel tank. Place the
the grab hook. Repeat with sling leg 4 on the right rear lift
correct link from Table 8-2 in the grab hook. Repeat with
provision.
sling leg 4 on the right rear lift provision.
4. Cluster and tie or tape (breakaway technique) the
4. Cluster and tie or tape (breakaway technique) the
sling legs together on top of the section to prevent en-
sling legs together on top of the section to prevent en-
tanglement during hookup and lift-off.
tanglement during hookup and lift-off.
Figure 8-2. D5B Tractor, Dozer
8-4
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-4. Tractor, Full Tracked, MC1150E
a. Applicability. The following item in Table 8-3 is certified for all helicopters with suitable lift capacity by the US Army
Natick Research, Development, and Engineering Center:
Table 8-3. Tractor, Full Tracked, MC1150E
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Tractor, Full-Tracked, MC1150E
24,062
40K
5/35
75
b. Materials. The following materials are required to
steps:
rig this load:
(a) Elevate the blade two feet off the ground. Using
(1) Sling set (40,000-pound capacity).
the tie-down chains, secure the blade in the UP position.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(b) Twist the lights on the cab inward. Tape the
roll.
lights, glass fixtures, and exhaust pipe opening.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(c) Ensure all caps, lids, and doors are securely fas-
tened.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(d) Place the transmission in neutral and engage the
hand brake.
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
substitute.
(2) Rigging. Rig the load according to the steps in
Figure 8-3.
(6) Chain, 8-foot length from 40,000-pound capacity
sling set with coupling links (2 each).
(3) Hookup. The hookup team stands on top of the
engine deck or cab. The static wand person discharges
(7) Tie-down chain assembly (10,000-pound capac-
the static electricity with the static wand. The hookup
ity), MB-1.
person places the apex fitting onto the aircraft cargo hook.
The hookup team then moves clear of the load but re-
c. Personnel. Two persons can prepare and rig this
mains close to the load as the helicopter removes slack
load in 30 minutes.
from the sling legs. When successful hookup is assured,
the hookup team quickly exits the area underneath the
d. Procedures. The following procedures apply to this
helicopter to the designated rendezvous point.
load:
(4) Derigging. Derigging is the reverse of the prepa-
(1) Preparation. Prepare the load using the following
ration and rigging procedures in steps d (1) and d (2).
8-5
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
rear lift provision located near the base of the cab. Using
1. Position the apex fitting on top of the cab. Route
the coupling link add the additional chain length to the
outer sling legs 1and 2 to the front of the load. Route
sling leg chain. Place the correct link from Table 8-3 in the
inner sling legs 3 and 4 to the rear of the load. Sling legs 1
grab hook. Repeat with sling leg 4 on the right rear lift
and 3 must be on the left side of the load.
provision.
2. Route the chain end of sling leg 1 through the left
NOTE: Add the additional chain length after the sling
front lift provision located on the left front corner of the
leg chain is routed through the lift provision. The link
engine deck. Place the correct link from Table 8-3 in the
coupling does not fit through the lift provision.
grab hook. Repeat with sling leg 2 and the right front lift
provision. Secure the excess chain with Type III nylon
4. Cluster and tie or tape (breakaway technique) the
cord.
sling legs together on top of the crew compartment to
prevent entanglement during hookup and lift-off.
3. Route the chain end of sling leg 3 through the left
Figure 8-3. Tractor, Full Tracked, MC1150E
8-6
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-5. Tractor, Wheeled, Industrial, Case Model 580
a. Applicability. The following item in Table 8-4 is certified for all helicopters with suitable lift capacity by the US Army
Natick Research, Development, and Engineering Center:
Table 8-4. Tractor, Wheeled, Industrial, Case Model 580
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Tractor, Case, 580
10,500
15K
30/54
80
b. Materials. The following materials are required to
toward the rear.
rig this load:
(b) Position the rear backhoe arm with the backhoe
(1) Sling set (15,000-pound capacity).
in the up position and secure with the tie-down straps to
prevent the backhoe arm from swinging freely. Route the
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
straps from each stabilizer to the backhoe arm.
roll.
(c) Ensure all caps, lids, and doors are securely fas-
(3) Cord, nylon, Type III, 550-pound breaking strength.
tened.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(d) Tape all lights, glass fixtures, and the exhaust cap
strength.
closed.
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
(e) Place the transmission in neutral and engage the
substitute.
hand brake.
(6) Chain, 6-foot length from 15,000-pound capacity
(2) Rigging. Rig the load according to the steps in
sling set with coupling links (2 each).
Figure 8-4.
(7) Tie-down strap, cargo, CGU-1B (2 each).
(3) Hookup. The hookup team stands on top of the
engine deck or ROPS. The static wand person discharges
c. Personnel. Two persons can prepare and rig this
the static electricity with the static wand. The hookup
load in 20 minutes.
person places the apex fitting onto the aircraft cargo hook.
The hookup team then moves clear of the load but re-
d. Procedures. The following procedures apply to this
mains close to the load as the helicopter removes slack
load:
from the sling legs. When successful hookup is assured,
the hookup team quickly exits the area underneath the
(1) Preparation. Prepare the load using the following
helicopter to the designated rendezvous point.
steps:
(4) Derigging. Derigging is the reverse of the prepa-
(a) Elevate the front bucket halfway and tilt the bucket
ration and rigging procedures in steps d (1) and d (2).
8-7
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 the apex fitting on top of the cab. Route
provision. Secure the excess chain with Type III nylon
outer sling legs 1and 2 to the front of the load. Route
cord.
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. Using the
3. Route the chain end of sling leg 3 through the left
coupling links, add the additional chain length to sling
rear lift provision located on the left rear corner of the
legs 1and 2.
ROPS. Place the correct link from Table 8-4 in the grab
hook. Repeat with sling leg 4 on the right rear lift provi-
2. Route the chain end of sling leg 1 through the left
sion. Secure the excess chain with Type III nylon cord.
front lift provision located on the left front corner of the
engine hood. Place the correct link from Table 8-4 in the
4. Cluster and tie or tape (breakaway technique) the
grab hook. Repeat with sling leg 2 and the right front lift
sling legs together on top of the crew compartment to
prevent entanglement during hookup and lift-off.
Figure 8-4. Tractor, Wheeled, Industrial, Case Model 580
8-8
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-6. Small Emplacement Excavator (SEE)
a. Applicability. The following item in Table 8-5 is certified for all helicopters with suitable lift capacity by the US Army
Natick Research, Development, and Engineering Center:
Table 8-5. Small Emplacement Excavator (SEE)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Listed in Rigging
Small Emplacement Excavator (SEE)
16,240
25K
95
Steps
b. Materials. The following materials are required to
closed.
rig this load:
(d) Fold the side mirrors inboard and tie or tape as
(1) Sling set (25,000-pound capacity).
required. Tape the windshield wipers to the windshield.
Secure the engine compartment hood with Type III nylon
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
cord.
roll.
(e) Place the transmission in neutral and engage the
(3) Cord, nylon, Type III, 550-pound breaking strength.
hand brake.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(f) Tie or tape the hydraulic lines and hoses in close
strength.
proximity to the forward lift provisions to prevent pos-
sible entanglement during hookup.
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
substitute.
(2) Rigging. Rig the load according to the steps in
Figure 8-5.
c. Personnel. Two persons can prepare and rig this
load in 30 minutes.
NOTE: Hookup of this load presents substantial risk of
damage to the load or injury to the hookup personnel.
d. Procedures. The following procedures apply to this
Use of a reach pendant is recommended for this load.
load:
(3) Hookup. The hookup team stands on top of the
(1) Preparation. Prepare the load using the following
falling objects protection systems (FOPS). The static wand
steps:
person discharges the static electricity with the static
wand. The hookup person places the apex fitting onto the
(a) Elevate the bucket halfway and tilt the bucket
aircraft cargo hook. The hookup team then moves clear of
toward the rear. Ensure the front end loader assembly
the load but remains close to the load as the helicopter
travel locks, located at the ends of both front end loader
removes slack from the sling legs. When successful
boom cylinders, are properly pinned in place.
hookup is assured, the hookup team quickly exits the area
underneath the helicopter to the designated rendezvous
(b) Secure the steering wheel, doors, and all loose
point.
equipment with tape or Type III nylon cord.
(4) Derigging. Derigging is the reverse of the prepa-
(c) Tape all lights, glass fixtures, and the exhaust cap
ration and rigging procedures in steps d (1) and d (2).
8-9
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 the apex fitting on top of the FOPS. Route
frame. Insert link 5 in the grab hook.
outer sling legs 1and 2 to the front of the load. Route
inner sling legs 3 and 4 to the rear of the load (backhoe
4. Route the chain end of sling leg 4 through the right
bucket end). Sling legs 1 and 3 must be on the left side of
rear lift provision located (closest to the backhoe bucket)
the load.
on the top right between the right rear wheel and frame.
Insert link 10 in the grab hook. Secure the excess chain
2. Route the chain end of sling leg 1 through the left
with Type III nylon cord.
front lift provision located on the front bumper inboard of
the front end loader left support arm. Insert link 3 in the
5. Place felt padding around all the chains. Secure the
grab hook. Repeat with sling leg 2 and the right front lift
padding with tape or Type III nylon cord.
provision inboard of the right support arm.
6. Cluster and tie or tape (breakaway technique) the
3. Route the chain end of sling leg 3 through the left
sling legs together on top of the crew compartment to
rear lift provision located (closest to the backhoe opera-
prevent entanglement during hookup and lift-off.
tors seat) on the top left between the left rear wheel and
Figure 8-5. Small Emplacement Excavator (SEE)
8-10
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-7. High Mobility Materiel Handler (HMMH)
a. Applicability. The following item in Table 8-6 is certified for all helicopters with suitable lift capacity by the US Army
Natick Research, Development, and Engineering Center:
Table 8-6. High Mobility Materiel Handler (HMMH)
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
High Mobility Materiel Handler
15,650
25K
3/56
115
b. Materials. The following materials are required to
(d) Fold the side mirrors inboard and tie or tape as
rig this load:
required. Tape the windshield wipers to the windshield.
Secure the engine compartment hood with Type III nylon
(1) Sling set (25,000-pound capacity).
cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(e) Place the transmission in neutral and engage the
roll.
hand brake.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(f) Tie or tape the hydraulic lines and hoses in close
proximity to the forward lift provisions to prevent pos-
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
sible entanglement during hookup.
strength.
(2) Rigging. Rig the load according to the steps in
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
Figure 8-6.
substitute.
NOTE: Hookup of this load presents substantial risk of
c. Personnel. Two persons can prepare and rig this
damage to the load or injury to the hookup personnel.
load in 30 minutes.
Use of a reach pendant is recommended for this load.
d. Procedures. The following procedures apply to this
(3) Hookup. The hookup team stands on top of the
load:
falling objects protection systems (FOPS). The static wand
person discharges the static electricity with the static
(1) Preparation. Prepare the load using the following
wand. The hookup person places the apex fitting onto
steps:
the aircraft cargo hook. The hookup team then moves
clear of the load but remains close to the load as the heli-
(a) Ensure all travel locks are properly pinned in
copter removes slack from the sling legs. When success-
place.
ful hookup is assured, the hookup team quickly exits the
area underneath the helicopter to the designated rendez-
(b) Secure the steering wheel, doors, and all loose
vous point.
equipment with tape or Type III nylon cord.
(4) Derigging. Derigging is the reverse of the prepa-
(c) Tape all lights, glass fixtures, and the exhaust cap
ration and rigging procedures in steps d (1) and d (2).
closed.
8-11
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position the apex fitting on top of the FOPS. Route
rear lift provision located on the frame inboard of the rear
outer sling legs 1and 2 to the front of the load. Route
wheel. Place the correct link from Table 8-6 in the grab
inner sling legs 3 and 4 to the rear of the load. Sling legs 1
hook. Repeat with sling leg 4 on the right rear lift provi-
and 3 must be on the left side of the load.
sion. Secure the excess chain with Type III nylon cord.
2. Route the chain end of sling leg 1 through the left
4. Place felt padding around all the chains. Secure the
front lift provision located near the front bumper out-
padding with tape or Type III nylon cord.
board of the forklift frame. Place the correct link from
Table 8-6 in the grab hook. Repeat with sling leg 2 and the
5. Cluster and tie or tape (breakaway technique) the
right front lift provision.
sling legs together on top of the FOPS to prevent en-
tanglement during hookup and lift-off.
3. Route the chain end of sling leg 3 through the left
Figure 8-6. High Mobility Materiel Handler (HMMH)
8-12
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-8. Ditching Machine
a. Applicability. The following item in Table 8-7 is certified for all helicopters with suitable lift capacity by the US Army
Natick Research, Development, and Engineering Center:
Table 8-7. Ditching Machine
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Ditching Machine
3,340
15K
3/20
100
b. Materials. The following materials are required to
(b) Ensure the fuel tank is not over 3/4 full. Inspect
rig this load:
the fuel tank cap, oil filter cap, and the battery caps for
proper installation.
(1) Sling set (15,000-pound capacity).
(c) Place the transmission in neutral and engage the
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
parking brake.
roll.
(d) Ensure the front wheels are pointed straight ahead
(3) Cord, nylon, Type III, 550-pound breaking strength.
and tie the steering wheel in place with Type III nylon
cord.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(e) Secure the hood latches with type III nylon cord.
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
(2) Rigging. Rig the load according to the steps in
substitute.
Figure 8-7.
c. Personnel. Two persons can prepare and rig this
(3) Hookup. The hookup team stands on the hood of
load in 15 minutes.
the vehicle. 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) Raise the blade on the front of the vehicle and
the digging chain on the rear of the vehicle.
(4) Derigging. Derigging is the reverse of the prepa-
ration and rigging procedures in steps d (1) and d (2).
8-13
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS
1. Position the apex fitting on the hood of the vehicle.
sling leg 4 on the right rear lift provision. Secure the
Route outer sling legs 1and 2 to the front of the load
excess chain with Type III nylon cord.
(blade 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
4. Place felt padding around all the chains where they
load.
contact the vehicle. Secure the padding with tape or
Type III nylon cord.
2. Route the chain end of sling leg 1 through the left
front lift provision located at the front bottom of the frame.
5. Raise the apex fitting above the hood of the vehicle.
Place the correct link from Table 8-7 in the grab hook.
Ensure the front slings are in front of the exhaust stack
Repeat with sling leg 2 and the right front lift provision.
and the rear slings are in front of the rollover bar.
3. Route the chain end of sling leg 3 through the left
6. Cluster and tie or tape (breakaway technique) the
rear lift provision located below the rollover bar. Place the
sling legs together on top of the FOPS to prevent en-
correct link from Table 8-7 in the grab hook. Repeat with
tanglement during hookup and lift-off.
Figure 8-7. Ditching Machine
8-14
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-9. 950BS Scoop Loader
a. Applicability. The following items in Table 8-8 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-8. 950BS Scoop Loader
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Loader, Scoop, 950BS (Type II), Work
15,830
25K
10/5
100
Section
Loader, Scoop, 950BS (Type II), Power
16,110
25K
10/20
90
Section
b. Materials. The following materials are required to
(1) Preparation. Prepare the load using the following
rig this load:
steps:
(1) Sling set (25,000-pound capacity).
(a) Sectionalize the loader according to the instruc-
tions provided in the operator's manual.
(2) Chain, 8-foot length from a 25,000-pound capacity
sling set with coupling links.
(b) Secure the bucket lift arm assembly to the work
section housing with two MB-1 chain tie-down assem-
(3) Cord, nylon, Type III, 550-pound breaking strength.
blies. Pass a chain around the left side of the bucket
control group arm crosstube through the lift point on the
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
housing, and secure the running ends with an MB-1
strength.
tensioning device. Repeat this procedure on the right
side of the crosstube.
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
substitute.
CAUTION
Chains must be tight to prevent sagging of
(6) Tape, adhesive, pressure-sensitive, 2-inch wide
the hydraulic system during flight.
roll.
(c) Cover all hitch pins and pivot holes with plastic
(7) Tie-down assembly, 15-foot dacron (2 each).
and tape to prevent contamination by dust and dirt.
(8) Tie-down assembly, chain, MB-1 (2 each).
(d) Secure tool basket lid, located in the bucket, with
nylon cord. Tape all lights.
(9) Plastic bags (4 each).
(e) Secure all hoses and cables located on front of
c. Personnel. Four persons can sectionalize the scoop
the power section, with nylon cord to prevent damage.
loader in 2 1/2 hours. Two persons can prepare and rig
this load in 20 minutes per section.
(f) Secure the floating axle in level position with two
15-foot tie-down assemblies. On the left side, pass the
d. Procedures. The following procedures apply to this
running end of a 15-foot tie-down strap down through the
load:
tie-down provision aft of the axle, under the axle, and up
8-15
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
through the tie-down provision forward of the axle. Se-
(k) Tape all lights and instruments.
cure the running ends of the strap using a D-ring and load
binder on top of the axle. Repeat this procedure on the
(l) Secure all doors and covers with tape or nylon
right side. Fold and secure excess webbing and loadbinder
cord.
with cotton webbing or tape.
(m) Place controls in neutral and release brakes.
(g) Install the low-velocity airdrop suspension pro-
visions on the left and right sides of the operator’s plat-
(2) Rigging. Rig the load according to the steps in
form. (These provisions are used as forward lift points for
Figure 8-8.
sling loading.) Torque mounting bolts to 640 + 80 foot-
pounds.
(3) Hookup. The hookup team stands on the wheels
or fender of the work section and on the operator's plat-
(h) Remove exhaust stack and stow on the compo-
form of the power section. The static wand person dis-
nent tray, mounted in the work section bucket. Cover
charges the static electricity with the static wand. The
opening of exhaust stack with tape.
hookup person places the apex fitting onto the aircraft
cargo hook. The hookup team then moves clear of the
(i) Remove the pre-air cleaner and pad with cellu-
load but remains close to the load as the helicopter re-
lose padding and stow in the stowage compartment lo-
moves slack from the sling legs. When successful hookup
cated behind the operator’s seat. Cover opening of pre-
is assured, the hookup team quickly exits the area under-
air cleaner with tape.
neath the helicopter to the designated rendezvous point.
(j) Fold the back of the operator seat down and
(4) Derigging. Derigging is the reverse of the prepa-
secure in place with nylon cord. Secure the seat belt over
ration and rigging procedures in steps d (1) and d (2).
the seat back.
8-16
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS (WORK SECTION)
1. Lay out a 25,000-pound sling set and connect the
grab hook. Repeat with sling leg 2 on the right front lift
additional
8-foot chain sections to sling legs 1 and 2
provision on the right side of the bucket. Secure the ex-
using the proper coupling links.
cess chain with Type III nylon cord.
2. Position apex fitting on top of the hydraulic cylinder.
4. Loop the chain end of sling leg 3 through the left rear
Route outer sling legs 1 and 2 to the bucket end of the
lift provision, located on top of the control group left sup-
load and the inner sling legs 3 and 4 to the aft end. Sling
port arm. Place the correct link from Table 8-8 in the grab
legs 1 and 3 should be on the left side of the load.
hook. Repeat with sling leg 4 on the right rear lift provi-
sion on the right arm.
3. Pass the chain end of sling leg 1 through the left
front lift provision, located on the left side of the back of
5. Cluster and tie or tape (breakaway technique) all sling
the bucket. Place the correct link from Table 8-8 in the
legs together to prevent entanglement during hookup and
lift-off.
Figure 8-8. 950BS Scoop Loader
8-17
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS (POWER SECTION)
1. Lay out a 25,000-pound sling set and connect the
8-8 in the grab hook. Repeat with sling leg 4 on the right
additional
8-foot chain sections to sling legs 3 and 4
rear lift provision. Secure the excess chain with Type III
using the proper coupling links.
nylon cord.
2. Position apex fitting on the engine hood. Route outer
sling legs 1 and 2 to the front of the load (operator’s seat)
WARNING
and inner sling legs 3 and 4 to the rear of the load (bumper
end). Sling legs 1 and 3 should be on the left side of the
DO NOT ATTACH SLING LEGS 3 AND 4
load.
TO FRAME LIFTING PROVISIONS LO-
3. Loop the chain end of sling leg 1 through the left
CATED ON THE FRAME. SLINGS AT-
front lift provision located to the left of the operator’s seat
TACHED TO THESE PROVISIONS MAY
above the fuel tank. Place the correct link from Table 8-8 in
CAUSE LOSS OF THE LOAD IN FLIGHT.
the grab hook. Repeat with sling leg 2 on the right front
lift provision.
5. Pull sling legs up on top of the engine hood and
4. Loop the chain end of sling leg 3 through the left rear
secure together with cotton webbing. Cluster and tie or
lift provision located on the forward edge of the battery
tape (breakaway technique) all sling legs together to pre-
box aft of the left wheel. Place the correct link from Table
vent entanglement during hookup and lift-off.
Figure 8-8. 950BS Scoop Loader (continued)
8-18
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-10. 130GS Grader
a. Applicability. The following items in Table 8-9 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-9. 130GS Grader
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
130GS Grader, Front Section with
Scarifier and ROPS and Low-Velocity
16,120
25K
3/77
100
Airdrop (LVAD) suspension
provisions removed
130GS Grader, Rear Section
14,270
25K
46/56
100
b. Materials. The following materials are required to
(a) Sectionalize the loader according to the instruc-
rig this load:
tions provided in the operator's manual.
(1) Sling set (25,000-pound capacity).
(b) Remove ROPS and LVAD suspension provisions
mounted on the front bolster.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
roll.
(c) Ensure the fuel tank is not over 3/4 full.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(d) Use a tie-down assembly to secure each side of
the front axle to front tie-down points on the front end.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(e) Loosen front headlight bar, rotate forward 180
degrees, and retighten. Pad lights with padding and tape.
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
substitute.
(f) Tape work lights on forward edge of operator’s
platform.
(6) Tie-down, cargo, CGU-1B (2 each).
(g) Secure steering wheel to horizontal control bar
(7) Plastic bags (4 each).
with nylon cord on both sides. Secure seat with nylon
cord.
(8) Posts, wooden, 4- x 4- x 48-inch (2 each).
(h) Cover all pivot points in the articulated hitch
c. Personnel. Two persons can prepare and rig each
group with plastic bags or a suitable substitute and tape
load in 20 minutes after the ROPS and LVAD suspension
securely to prevent fouling by sand and dirt.
provisions are removed and the grader is sectionalized.
(i) Remove throttle handle and secure in toolbox.
d. Procedures. The following procedures apply to this
load:
(j) Pad instrument panel with cellulose padding and
tape.
(1) Preparation. Prepare the load using the following
steps:
(k) Remove air cleaner and exhaust stack and secure
8-19
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
to top rail with nylon cord.
(3) Hookup. The hookup team stands on top of each
section. The static wand person discharges the static
(l) Tie 4- x 4- x 48-inch posts to inside rear guardrail
electricity with the static wand. The hookup person places
on the rear section with nylon cord.
the apex fitting onto the aircraft cargo hook. The hookup
team then moves clear of the load but remains close to the
(m) Pad and tape rear working light and taillights.
load as the helicopter removes slack from the sling legs.
When successful hookup is assured, the hookup team
(n) Secure doors with one loop of nylon cord hori-
quickly exits the area underneath the helicopter to the
zontally around the body of the unit.
designated rendezvous point.
(2) Rigging. Rig the load according to the steps in
(4) Derigging. Derigging is the reverse of the prepa-
Figure 8-9.
ration and rigging procedures in steps d (1) and d (2).
FRONT SECTION
REAR SECTION
RIGGING STEPS (REAR SECTION)
1. Position the apex fitting on top of the engine com-
3. Loop the chain end of sling leg 3 through the left rear
partment. Route outer sling legs 1 and 2 to the front (for-
lift provision located aft of the left rear wheel. Place the
ward wheel) end and inner sling legs 3 and 4 to the rear
correct link from Table 8-9 in the grab hook. Repeat with
(radiator) end of the rear section. Sling legs1 and 3 should
sling leg 4 on the right rear lift provision.
be on the left side of the load.
4. Cluster and tie or tape (breakaway technique) all sling
2. Loop the chain end of sling leg 1 through the left
legs together to prevent entanglement during hookup and
front lift provision located inboard of the left front wheel
lift-off. Ensure the sling legs are located outside of the 4-
Place the correct link from Table 8-9 in the grab hook.
x 4- x 48-inch posts.
Repeat with sling leg 2 on the right front lift provision.
Figure 8-9. 130GS Grader
8-20
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS (FRONT SECTION)
1.
Position apex fitting on top of the front section.
3. Loop the chain end of sling leg 3 through the left rear
Route outer sling legs 1 and 2 to the front (wheel end) of
lift provision above the blade. Place the correct link from
the section and inner sling legs 3 and 4 to the rear end.
Table 8-9 in the grab hook. Repeat with sling leg 4 on the
Sling legs 1 and 3 should be on the left side of the load.
right rear lift provision. Secure excess chain with tape or
nylon cord.
2. Loop the chain end of sling leg 1 through the left
front lift provision by the left wheel. Place the correct link
4. Cluster and tie or tape (breakaway technique) all sling
from Table 8-9 in the grab hook. Repeat with sling leg 2 on
legs together to prevent entanglement during hookup and
the right front lift provision.
lift-off.
Figure 8-9. 130GS Grader (continued)
8-11. 613BS Scraper, Elevating
a. Applicability. The following items in Table 8-10 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-10. 613BS Scraper, Elevating
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
613BS Scraper, Elevating, Work
16,330
25K
3/40
110
Section
613BS Scraper, Elevating, Power
Listed in Rigging
16,860
25K
110
Section
Steps
b. Materials. The following materials are required to
c. Personnel. Four persons can sectionalize the scraper
rig this load:
in 1 hour. Two persons can prepare and rig each load in 20
minutes.
(1) Sling set (25,000-pound capacity).
d. Procedures. The following procedures apply to this
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
load:
roll.
(1) Preparation. Prepare the load using the following
(3) Cord, nylon, Type III, 550-pound breaking strength.
steps:
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
(a) Sectionalize the scaper according to the instruc-
strength.
tions provided in the operator's manual.
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
(b) Secure the operator's seat with Type III nylon
substitute.
cord.
(6) Plastic bags (4 each).
(c) Secure all covers and doors with tape or Type III
nylon cord.
(7) Plywood, 3/4- x 8- x 46-inch (2 each).
8-21
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
(d) Secure auxiliary fuel tank in place with Type III
an L-shaped protector. Drill two 1/2-inch holes in each
nylon cord.
corner for restraint. Plywood will protect the top edge of
the radiator grill where it meets the hood.
(e) Stow elevator motor hoses and hanger arms on
elevator flights in the bowl, and secure with nylon cord.
(o) Place felt padding over the headlights and tape in
place.
(f) Secure hydraulic cylinders up in a stowed posi-
tion with doubled nylon cord.
(p) Position the plywood protector on the hood and
secure in place at four corners with nylon cord.
(g) Secure loose hoses and cables with Type III
nylon cord.
CAUTION
Plywood hood protector is essential to pre-
(h) Fold and secure the steps located on outside of
vent hood damage by sling leg chains.
the bowl.
(2) Rigging. Rig the load according to the steps in
(i) Tape all lights.
Figure 8-10.
(j) Cover all hitch pins and pin holes with plastic and
(3) Hookup. The hookup team stands on top of each
tape to prevent contamination by dirt and dust.
section. The static wand person discharges the static
electricity with the static wand. The hookup person places
(k) Secure toolbox lid closed with nylon cord.
the apex fitting onto the aircraft cargo hook. The hookup
team then moves clear of the load but remains close to the
(l) Ensure that steering wheels are aligned.
load as the helicopter removes slack from the sling legs.
When successful hookup is assured, the hookup team
(m) Install front bumper lift provision. Ensure that
quickly exits the area underneath the helicopter to the
pin safety clip is installed. If clip is missing, secure the pin
designated rendezvous point.
in place with nylon cord.
(4) Derigging. Derigging is the reverse of the prepa-
(n) Fabricate a hood protection from two pieces of 3/
ration and rigging procedures in steps d (1) and d (2).
4- x 8- x 46-inch plywood. Nail plywood together forming
8-22
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
POWER SECTION
WORK SECTION
RIGGING STEPS (WORK SECTION)
RIGGING STEPS (POWER SECTION)
1. Place apex fitting on top of rockguard and route outer
1. Position apex fitting on top of the engine hood. Route
sling legs 1 and 2 to forward end of load and inner sling
outer sling legs 1 and 2 to the center of the power section
legs 3 and 4 to aft (bumper) end. Sling legs 1 and 3 must be
by the main wheels. Route inner sling leg 3 forward to the
on the left side of the load.
front bumper and the other inner sling leg 4 to the arm
assembly frame.
2. Loop the chain end of sling leg 1 through the left
front lift provision located on the left front corner of the
2. Loop the chain end of sling leg 1 through the left
bowl. Place the correct link from Table 8-10 in the grab
center lift provision to the left of the operator’s seat and
hook. Repeat with sling leg 2 on the right front lift provi-
insert link 40 in the grab hook. Repeat with sling leg 2 on
sion on the right front corner.
the right center lift provision.
3. Pull both sling legs aft and secure (breakaway tech-
3. Loop the chain end of sling leg 3 through the front
nique) to elevator and rockguard with cotton webbing or
bumper lift provision located in the center of the bumper
tape.
and insert link 3 in the grab hook. Pull the sling leg up
over the hood protector and tape or tie (breakaway tech-
4. Loop the chain end of sling leg 3 through the left rear
nique) the sling leg to the ROPS mount.
lift fitting located on the aft deck above the left wheel.
Place the correct link from Table 8-10 in the grab hook.
4. Loop the chain end of sling leg 4 through the lift
Repeat with sling leg 4 on the right rear lift provision.
provision located on the center top of the draft arm as-
Secure excess chain with tape or nylon cord.
sembly frame and insert link 24 in grab hook. Tape or tie
(breakaway technique) the sling leg to the top of the draft
5. Pull both sling legs forward and secure (breakaway
arm. Secure excess chain with tape or nylon cord.
technique) to rockguard with tape or cotton webbing.
5. Cluster and tie or tape (breakaway technique) all sling
6. Cluster and tie or tape (breakaway technique) all sling
legs together to prevent entanglement during hookup and
legs together on top of the rockguard to prevent entangle-
lift-off.
ment during hookup and lift-off.
Figure 8-10. 613BS Scraper, Elevating
8-23
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
8-12. 613WDS Water Distributor
a. Applicability. The following items in Table 8-11 are certified for all helicopters with suitable lift capacity by the US
Army Natick Research, Development, and Engineering Center:
Table 8-11. 613WDS Water Distributor
MAX
RECOMMENDED
LINK COUNT
NOMENCLATURE
WEIGHT
SLING SET
AIRSPEED
FRONT/REAR
(POUNDS)
(KNOTS)
Distributor, Water, Work Section
15,400
25K
3/45
110
Listed in Rigging
Distributor, Water, Power Section
16,960
25K
110
Steps
b. Materials. The following materials are required to
cord.
rig this load:
(c) Secure all covers and doors with tape or Type III
(1) Sling set (25,000-pound capacity).
nylon cord.
(2) Tape, adhesive, pressure-sensitive, 2-inch wide
(d) Secure auxiliary fuel tank in place with Type III
roll.
nylon cord.
(3) Cord, nylon, Type III, 550-pound breaking strength.
(e) Secure the distribution control panel and cable in
place on top of the tank with nylon cord.
(4) Webbing, cotton, 1/4-inch, 80-pound breaking
strength.
(f) Ensure that the tank manhole cover is closed and
secured.
(5) Felt sheet, cattle hair, Type IV, 1/2-inch or suitable
substitute.
(g) Close and secure the toolbox and hose stowage
compartment covers with nylon cord.
(6) Plastic bags (4 each).
(h) Secure the hose nozzle and reel with nylon cord.
(7) Plywood, 3/4- x 8- x 46-inch (2 each).
(i) Tape all lights.
c. Personnel. Four persons can sectionalize the dis-
tributor in 1 hour. Two persons can prepare and rig each
(j) Cover hitch pins and pin holes with plastic and
load in 20 minutes.
tape to prevent contamination by dust and dirt.
d. Procedures. The following procedures apply to this
(k) Ensure the steering wheels are aligned.
load:
(l) Install front bumper lift provision. Ensure that
(1) Preparation. Prepare the load using the following
pin safety clip is installed. If clip is missing, secure the pin
steps:
in place with nylon cord.
(a) Sectionalize the distributor according to the in-
(m) Fabricate a hood protection from two pieces of
structions provided in the operator's manual.
3/4- x 8- x 46-inch plywood. Nail plywood together form-
ing an L-shaped protector. Drill two 1/2-inch holes in each
(b) Secure the operator's seat with Type III nylon
corner for restraint. Plywood will protect the top edge of
8-24
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
the radiator grill where it meets the hood.
(2) Rigging. Rig the load according to the steps in
Figure 8-11.
(n) Place felt padding over the headlights and tape
in place.
(3) Hookup. The hookup team stands on top of each
section. The static wand person discharges the static
(o) Position the plywood protector on the hood and
electricity with the static wand. The hookup person places
secure in place at four corners with nylon cord.
the apex fitting onto the aircraft cargo hook. The hookup
team then moves clear of the load but remains close to the
(p) Secure lift cylinders to the draft arms with a
load as the helicopter removes slack from the sling legs.
doubled length of nylon cord.
When successful hookup is assured, the hookup team
quickly exits the area underneath the helicopter to the
CAUTION
designated rendezvous point.
Plywood hood protector is essential to pre-
(4) Derigging. Derigging is the reverse of the prepa-
vent hood damage by sling leg chains.
ration and rigging procedures in steps d (1) and d (2).
POWER SECTION
WORK SECTION
Figure 8-11. 613WDS Water Distributor
8-25
FM 10-450-4/MCRP 4-23E, VOL II/NWP 3-04.12/AFJMAN 11-223, VOL II/
COMDTINST M13482.2
RIGGING STEPS (WORK SECTION)
RIGGING STEPS (POWER SECTION)
1. Place the apex fitting on top of work section tank.
1. Position apex fitting on top of the engine hood. Route
Route outer sling legs 1 and 2 to the forward end of the
outer sling legs 1 and 2 to the center of the power section
water tank and inner sling legs 3 and 4 to the aft (wheel)
by the main wheels. Route inner sling leg 3 forward to the
front bumper and the other inner sling leg 4 to the arm
end of the work section. Sling legs 1 and 3 must be to the
assembly frame.
same side of the water tank.
2. Loop the chain end of sling leg 1 through the left
2. Pass chain end of sling leg 1 through the forward left
center lift provision to the left of the operator’s seat and
lift provision located on left forward corner of the water
insert link 40 in the grab hook. Repeat with sling leg 2 on
tank. Place the correct link from Table 8-11 in the grab
the right center lift provision.
hook. Repeat this procedure for sling leg 2 on the lift
provision on the right forward corner of the water tank.
3. Loop the chain end of sling leg 3 through the front
bumper lift provision located in the center of the bumper
3. Pass chain end of sling leg 3 through the aft left lift
and insert link 3 in the grab hook. Pull the sling leg up
provision located on the aft deck by the left wheel. Place
over the hood protector and tape or tie (breakaway tech-
the correct link from Table 8-11 in the grab hook. Repeat
nique) the sling leg to the ROPS mount.
this procedure for sling leg 4 on the lift provision by the
right wheel. Secure excess chain with tape or nylon cord.
4. Loop the chain end of sling leg 4 through the lift
provision located on the center top of the draft arm as-
4. Cluster and tie or tape (breakaway technique) all sling
sembly frame and insert link 24 in grab hook. Tape or tie
legs together on top of the tank to prevent entanglement
(breakaway technique) the sling leg to the top of the draft
during hookup and lift-off.
arm. Secure excess chain with tape or nylon cord.
5. Cluster and tie or tape (breakaway technique) all sling
legs together to prevent entanglement during hookup and
lift-off.
Figure 8-11. 613WDS Water Distributor (continued)
8-26
|
|