Главная Manuals AIRDROP OF SUPPLIES AND EQUIPMENT: RIGGING MILITARY UTILITY VEHICLE (M-GATOR) (June 2001)
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FM 4-20.108/TO 13C7-2-491
20A
10
9
20
Lashing
Tiedown
Instructions
Number
Clevis Number
Pass lashing through :
9
20
Front right tiedown poin t
10
20A
Front left tiedown poin t
Figure 2-13. Lashings 9 and 10 Installed
2-15
FM 4-20.108/TO 13C7-2-491
9A
11
Lashing
Tiedown
Instructions
Number
Clevis Number
Pass lashing through :
11
Tiedown-ring 9A
Left rear tiedown point
12
Tiedown-ring 9B
Right rear tiedown point
Figure 2-14. Lashings 11 and 12 Installed
2-16
FM 4-20.108/TO 13C7-2-491
13
15
16
12
Lashing
Tiedown
Instruction s
Number
Clevis Number
Pass lashing through :
13
16
Front left tiedown poin t
14
16A
Front right tiedown poin t
15
12
Right rear tiedown point
16
12A
Left rear tiedown point
Figure 2-15. Lashings 13 and 14 Installed
2-17
FM 4-20.108/TO 13C7-2-491
POSITIONING M-GATOR BOXES
2-12. Position M-Gator boxes as shown in Figure 2-16.
Position the front box over the front M-Gator aligning the bottom front edge of the box with the
front edge of the platform.
Position the rear box over the rear M-Gator aligning the bottom front edge of the box with the
rear edge of the platform.
Figure 2-16. M-Gator Boxes Positioned
2-18
FM 4-20.108/TO 13C7-2-491
LASHING M-GATOR BOXES
2-13. Lash the M-Gator boxes to the platform according to FM 10-500-2/TO
13C7-1-5 and as shown in Figure 2-17.
18
17
4
3
FRONT
Route a lashing through clevis 3 and back through it’s own D-ring, and pull strap taut.
Repeat the same steps for clevis 4. Bind to clevises 3A and 4A.
Lashing
Tiedown
Instructions
Number
Clevis Number
Pass lashing through :
17
3 and 3A
Front lower cutouts of front bo x
18
4 and 4A
Front upper cutouts of front bo x
Figure 2-17. M-Gator Boxes Lashed
2-19
FM 4-20.108/TO 13C7-2-491
20
19
6
2
Route a lashing through clevis 2 and back through it’s own D-ring, and pull strap taut.
Repeat the same steps for clevises 2A, 6, and 6A.
Lashing
Tiedown
Instructions
Number
Clevis Number
Pass lashing through :
19
2 and 2A
Over top of box and bind on right side of box.
20
6 and 6A
Over top of box and bind on right side of box.
Figure 2-17. M-Gator Boxes Lashed (continued)
2-20
FM 4-20.108/TO 13C7-2-491
21
22
17
18
REAR
Route a lashing through clevis 17 and back through it’s own D-ring, and pull the strap taut.
Repeat the same steps for 17A, 18, and 18A. Bind to clevises 17A and 18A.
Lashing
Tiedown
Instructions
Number
Clevis Number
Pass lashing through :
21
17 and 17A
Front upper cutouts of rear box.
22
18 and 18A
Front lower cutouts of rear box.
Figure 2-17. M-Gator Boxes Lashed (continued)
2-21
FM 4-20.108/TO 13C7-2-491
24
23
19
15
Route a lashing through clevis 15 and back through it’s own D-ring, and pull strap taut.
Repeat the same steps for clevises 15A, 19, and 19A.
Lashing
Tiedown
Instructions
Number
Clevis Number
Pass lashing :
23
15 and 15A
Over top of box and bind on left side of box.
24
19 and 19A
Over top of box and bind on left side of box.
Figure 2-17. M-Gator Boxes Lashed (continued)
2-22
FM 4-20.108/TO 13C7-2-491
INSTALLING SUSPENSION SLINGS
2-14. Install four 16-foot (2-loop), type XXVI nylon slings as suspension slings
according to FM 10-500-2/TO 13C7-1-5 and as shown in Figure 2-18.
1
2
3
1
Attach a 16-foot (2-loop), type XXVI nylon sling to each of the four suspension links using a
large clevis.
2
Raise the slings above the load and install the deadman’s tie as outlined in FM 10-500-2/TO
13C7-1-5.
3
Felt and tape each sling where they make contact with the boxes.
Figure 2-18. Suspension Slings Installed
2-23
FM 4-20.108/TO 13C7-2-491
STOWING CARGO PARACHUTES
2-15. Prepare, stow, and restrain two G-11 cargo parachutes according to FM
10-500-2/TO 13C7-1-5 and as shown in Figure 2-19.
3
1
2
1
Place two G-11 cargo parachutes on the front edge of the rear M-Gator box.
2
Restrain the parachutes with type VIII nylon webbing to clevises 18 and 18A.
3
Install the parachute release strap according to FM 10-500-2/TO 13C7-1-5.
Figure 2-19. Cargo Parachutes Stowed
2-24
FM 4-20.108/TO 13C7-2-491
INSTALLING EXTRACTION SYSTEM
2-16. Install the Extraction Force Transfer Coupling (EFTC) according to FM
10-500-2/TO 13C7-1-5 and as shown in Figure 2-20.
3
2
1
1
Install EFTC actuator mounting brackets using rear mounting holes.
2
Install a 20-foot cable.
3
Attach a 9-foot (2-loop), type XXVI nylon sling for the deployment line.
Figure 2-20. Extraction System Installed
2-25
FM 4-20.108/TO 13C7-2-491
INSTALLING PARACHUTE RELEASE
2-17. Prepare and install an M-1 cargo parachute release system according to
FM 10-500-2/TO 13C7-1-5 and as shown in Figure 2-21.
1
2
3
4
1
Cut one piece of honeycomb to fit between the lashings and two pieces to fit outside the
lashings on top of the equipment box. Each piece will be 25 1/2-inches wide.
2
Cut a 58 1/2-inch by 25 1/2-inch piece of honeycomb and place it on top of the three pieces
previously placed on top of the equipment box. Tape the outer edges and secure with type
III nylon cord.
3
Place the M-1 release on the equipment box and safety it to convenient places on the load.
4
Fold and secure any slack in the suspension slings.
Figure 2-21. Parachute Release Installed
2-26
FM 4-20.108/TO 13C7-2-491
POSITIONING EXTRACTION PARACHUTE
2-18. Select the extraction parachute and extraction line needed using the
extraction line requirements table in FM 10-500-2/TO 13C7-1-5. Place the
extraction parachute and extraction line on the load for installation inside
aircraft.
INSTALLING PROVISIONS FOR EMERGENCY RESTRAINTS
2-19. Select and install provisions for emergency restraints according to the
emergency aft restraint requirements in FM 10-500-2/TO 13C7-1-5.
2-27
FM 4-20.108/TO 13C7-2-491
MARKING RIGGED LOAD
2-20. Mark the rigged load according to FM 10-500-2/TO 13C7-1-5 and as shown
in Figure 2-22. Complete the Shipper’s Declaration for Dangerous Goods. If the
load varies from the one shown, the weight, height, CB, and must be recom-
puted.
EQUIPMENT REQUIRED
2-21. The equipment required to rig this load is listed in Table 2-1.
CAUTION
Make the final rigger inspection required by FM 10-500-2/
TO 13C7-1-5 before load leaves rigging site.
CB
RIGGED LOAD
Weight
8,520 pounds
Height
78 inches
Width
108 inches
Overall Length
258 inches
Overhang: Front (Box)
2 1/2 inches
Rear (EFTC)
18 inches
Center of Balance (from front edge of platform)
124 inches
Figure 2-22. M-Gator Rigged on a 20-Foot Platform for Low-Velocity Airdrop
2-28
FM 4-20.108/TO 13C7-2-491
Table 2-1. Equipment required for rigging M-Gator on a 20-foot platform for low-velocity airdrop
National Stock
Item
Quantity
Number
8040-00-273-8713
Adhesive paste, 1-gal
As required
1670-01-035-6054
Bridle, extraction line bag (C-17
)
1
4030-00-090-5354
Clevis, suspension, 1-in (large
)
5
4020-00-240-2146
Cord, nylon, type III, 550-lb
As required
1670-00-434-5783
Coupling, airdrop, extraction force transfer with cable, 20ft
1
Cover:
1670-00-360-0328
Clevis, large
2
1670-01-183-2678
Leaf, extraction line (line bag
)
2
Line, drogue (for C-17)
1670-01-064-4452
60-ft (1-loop), type XXV I
1
Line, extraction
:
1670-01-062-6313
For C-130: 60-ft (3-loop), type XXV I
1
1670-01-107-7651
For C-141: 140-ft (3-loop), type XXV I
1
1670-01-107-7652
For C-5: 160-ft (1-loop), type XXV I
1
1670-01-107-7651
For C-17: 140-ft (3-loop), type XXV I
1
Link assembly:
Two-point, 3 3/4-in
1
5306-00-435-8994
Bolt, 1-in diam, 4-in long
(2
)
5310-00-232-5165
Nut, 1-in, hexagonal
(2
)
1670-00-003-1954
Plate, side, 3 3/4-in
(2
)
5365-00-007-3414
Spacer, large
(2
)
Two-point, 3 3/4-in (for C-1
7)
1
5306-00-435-8994
Bolt, 1-in diam, 4-in long
(2
)
5310-00-232-5165
Nut, 1-in, hexagonal
(2
)
1670-00-003-1954
Plate, side, 3 3/4-in
(2
)
5365-00-007-3414
Spacer, large
(2
)
/
Link, towed mechanized release (H-Block) C-17
aircraft
1
Lumber:
5510-00-220-6146
2- by 4-in
As required
5510-00-220-6148
2- by 6-in
As required
5315-00-010-4659
Nail, steel wire, common, 8d
As required
1670-00-753-3928
Pad, energy dissipating, honeycomb, 3- by 36- by 96-in
20 sheets
2-29
FM 4-20.108/TO 13C7-2-491
Table 2-1. Equipment required for rigging M-Gator on a 20-foot platform for low-velocity airdrop
(continued)
National Stock
Item
Quantity
Numbe r
Parachute:
1670-01-016-7841
Cargo, G-11B
2
1670-01-063-3716
Cargo, extraction, 22-ft (for C-130 and C-17
)
1
1670-01-063-3715
Drogue, 15-ft (for C-17
)
1
Platform, airdrop, type
V, 20-foot:
1670-01-353-8425
Bracket assembly, couplin g
(1
)
1670-01-162-2372
Clevis assembly, type V
(40
)
1670-01-353-8424
Extraction bracket assembly
(1
)
1670-01-162-2381
Link, tandem, suspension link assembly
(2
)
1670-01-247-2389
Link, suspension
(4
)
5530-00-128-4981
Plywood, 3/4- by 48- by 96-in
9
sheets
1670-01-097-8816
Release, cargo parachute, M-1
1
Sling, cargo airdrop
For suspension:
1670-01-063-7761
16-ft (2-loop), type XXVI nylon webbing
4
For deployment:
1670-01-062-6304
9-ft (2-loop), type XXVI nylon webbin g
1
For riser extention
:
1670-01-062-6302
20-ft (2-loop), type XXVI nylon webbing
2
7510-00-266-5016
Tape, adhesive, 2-in
As required
1670-00-937-0271
Tie-down assembly, 15-ft
46
Webbing:
8305-00-268-2411
Cotton, 1/4-in, type I
As required
8305-00-082-5725
Nylon, tubular, 1/2-in
As required
8305-00-261-8585
Type VIII
As required
2-30
FM 4-20.108/TO 13C7-2-491
CHAPTER 3
Rigging One Military Utility Vehicle (M-Gator) and an A-22
Cargo Bag on a 12-Foot Platform for Low-Velocity Airdrop
DESCRIPTION OF LOAD
3-1. This load consists of one John Deere Diesel, which has been named the M-
Gator and one A-22 cargo bag. The minimum the A-22 cargo bag can weigh is
800 pounds and the maximum weight is 1,000 pounds. It is rigged on a 12-foot
platform. The load shown has a rigged weight of 4,630 pounds. It has an overall
length of 162 inches, width of 108 inches, and height of 78 inches, with a center
of balance of 68 inches. The load is rigged with one G-11 cargo parachute.
PREPARING PLATFORM
3-2. Inspect, or assemble and inspect, a 12-foot platform as outlined in TM 10-
1670-268-20&P/TO 13C7-52-22. Prepare a 12-foot platform using 22 tiedown
clevises as shown in Figure 3-1.
BUILDING M-GATOR BOX
3-3. Build the M-Gator box as outlined in chapter 1, paragraph 1-7.
PREPARING M-GATOR
3-4. Prepare the M-Gator according to chapter 1, paragraph 1-4 and chapter 2,
paragraph 2-5.
3-1
FM 4-20.108/TO 13C7-2-491
CLEVISES
11A THROUGH 1 A
LEFT
REAR
FRONT
RIGHT
CLEVISES
11 THROUGH 1
Step:
1. Install a tandem multi-purpose link to the front of each platform side rail using holes 1,2,
and 3.
2. Install a tandem multi-purpose link to the rear of each platform side rail using holes 22, 23,
and 24.
3. Install a clevis on bushings 1 and 3 of each front tandem link.
4. Install a clevis on bushing 2 of each rear tandem link.
5. Starting at the front of each platform side rail, install clevises on the bushings bolted on
holes 6, 7, 9, 15, 17, 18, 19, and 20.
6. Starting at the front of the platform number the clevises 1 through 11 on the right side and
1A through 11A on the left side.
7. Label the tie-down rings according to FM 10-500-2/TO 13C7-1-5.
8. Route a lashing through tie-down ring 1A and back through it’s own D-ring, repeat for tie-
down rings 1B, 3A, and 3B.
Figure 3-1. Platform Prepared
3-2
FM 4-20.108/TO 13C7-2-491
BUILDING HONEYCOMB STACKS
3-5. Refer to paragraph 1-3 for building honeycomb stack 1. Build honeycomb
stack 2 as shown in Figure 3-2.
Stack
Width
Length
Pieces
Material
Instructions
Number
(inches
)
(inches
)
2
2
51
36
Honeycomb
Glue and place one on top of the other.
Figure 3-2. Honeycomb Stack Prepared
POSITIONING HONEYCOMB STACK 1
3-6. Position honeycomb stack 1 centered left to right and 47 1/2 inches
from the front edge of the platform and as shown in Figure 3-3.
47 1/2”
Figure 3-3. Honeycomb Stack 1 Positioned
3-3
FM 4-20.108/TO 13C7-2-491
POSITIONING LOAD
3-7. Use four 12-foot (2-loop), type XXVI, nylon suspension slings to lift and
position the M-Gator. Attach large clevis assemblies to each sling. Using two
front and two rear lifting points, attach one clevis to each lifting point. Position
the M-Gator with the rear of the vehicle facing the front of the platform. Align
the rear edge of the M-Gator frame with the front edge of the honeycomb stack
and center. Each tire will be centered over a cutout in the honeycomb stack as
shown in Figure 3-4.
Figure 3-4. M-Gator Positioned
3-4
FM 4-20.108/TO 13C7-2-491
POSITIONING HONEYCOMB STACK 2
3-8. Temporarily place the pre-positioned lashings from deck-rings 3A and 3B
over the tailgate. Position honeycomb stack 2 on the front edge of the platform,
centered left to right ensure the 51 inch length is across the platform as shown
in Figure 3-5.
Figure 3-5. Honeycomb Stack 2 Positioned
3-5
FM 4-20.108/TO 13C7-2-491
RIGGING AND POSITIONING THE A-22 CARGO BAG
3-9. Rig the A-22 cargo bag as described in FM 10-500-3/TO13C7-1-11. The A-22
cargo bag weight limitations are 800 pounds minimum to 2,000 pounds maxi-
mum of unit specific equipment. Position the A-22 container on stack 2. Place
the A-22 container against the tailgate of the M-Gator so there is no overhang as
shown in Figure 3-6.
Figure 3-6. A-22 Cargo Bag Postitioned
3-6
FM 4-20.108/TO 13C7-2-491
LASHING THE A-22 CARGO BAG
3-10. Lash the A-22 cargo bag to the platform according to FM 10-500-2/TO
13C7-1-5 and as shown in Figure 3-7.
1
2
3
2
1
1
Route the pre-positioned lashings under the A-22 cargo bag webbing, tie-down ring 1A
load binds to tie-down ring 3A, tie-down ring 1B load binds to tie-down ring 3B, and load
bind on top of A-22 cargo bag.
2
Route a lashing through clevis 1 and back through it’s own D-ring, route it through the
rear middle webbing on the A-22 cargo bag and load bind to clevis 1A.
3
Route a lashing through clevis 2 and back through it’s own D-ring, route it through the
rear lower webbing on the A-22 cargo bag and load bind to clevis 2A.
Figure 3-7. A-22 Cargo Bag Lashed
3-7
FM 4-20.108/TO 13C7-2-491
5
4
3
4
4
Route a lashing through clevis 3A and back through it’s own D-ring. Route it through
the front lower webbing on the A-22 cargo bag and load bind to clevis 3.
5
Route a lashing through clevis 4A and back through it’s own D-ring. Route it through
the front middle webbing on the A-22 cargo bag and load bind to clevis 4.
Figure 3-7. A-22 Cargo Bag Lashed (Continued)
3-8
FM 4-20.108/TO 13C7-2-491
LASHING M-GATOR
3-11. Lash the M-Gator to the platform according to FM 10-500-2/TO 13C7-1-5
and as shown in Figures 3-8 through 3-10.
NOTE: Place all load binders near the platform in case adjustments to the
lashings are needed.
2
3
1
7
11
Lashing
Tiedown
Instruction s
Numbe r
Clevis Numbe r
Pass lashing through :
1
11
Front right tiedown poin t
2
11A
Front left tiedown poin t
3
7
Front left tiedown poin t
4
7A
Front right tiedown poin t
Figure 3-8. Lashings 1,2,3, and 4 Installed
3-9
FM 4-20.108/TO 13C7-2-491
5
5A
Lashing
Tiedown
Instructions
Number
Clevis Number
Pass lashing through :
5
Tiedown-ring 5A
Left rear tiedown point
(do not tighten)
6
Tiedown-ring 5B
Right rear tiedown point (do not tighten)
Figure 3-9. Lashings 5 and 6 Installed
3-10
FM 4-20.108/TO 13C7-2-491
7
5
Lashing
Tiedown
In stru ction s
Numbe r
Clevis Numbe r
Pass lashing through
:
7
5
Rear right tiedown point
(d o n o t tig h ten )
8
5A
Rear left tiedown point
(d o n o t tig h ten )
Tighten lashings 5 and 6 and then 7 and
8
Figure 3-10. Lashings 7 and 8 Installed
3-11
FM 4-20.108/TO 13C7-2-491
POSITIONING M-GATOR BOX
3-12. Position M-Gator box as shown in Figure 3-11.
Position the box on the platform, aligning the front bottom edge of the box with the platform
rear edge.
Figure 3-11. M-Gator Box Positioned
3-12
FM 4-20.108/TO 13C7-2-491
LASHING M-GATOR BOX
3-13. Lash the M-Gator box to the platform according to FM 10 500-2/TO 13C7-
1-5 and as shown in Figure 3-12.
BOX FRONT
BOX LEFT SIDE
1
2
8
10
Route a lashing through clevis 8A and back through it’s own D-ring, and pull the strap
taut. Repeat the same steps for clevis 10A.
Lashing
Tiedown
Instructions
Number
Clevis Number
Pass lashing through :
1
8A and
8
Top rear cutouts of box
2
10A and
10
Bottom rear cutouts of box
Figure 3-12. M-Gator Box Lashed
3-13
FM 4-20.108/TO 13C7-2-491
4
3
9
6
Route a lashing through clevis 6 and back through it’s own D-rig, and pull strap taut.
Repeat the same steps for clevises 6A, 9, and 9A.
Lashing
Tiedown
Instructions
Number
Clevis Number
Pass lashing :
3
6 and 6A
Over top of box and bind on left side of box.
4
9 and 9A
Over top of box and bind on left side of box.
Figure 3-12. M-Gator Box Lashed (Continued)
3-14
FM 4-20.108/TO 13C7-2-491
INSTALLING SUSPENSION SLINGS
3-14. Install four 16-foot (2 loop), type XXVI nylon slings as suspension
slings according to FM 10-500-2/TO 13C7-1-5 and as shown in Figure 3-13.
1
2
3
1
Attach a 16-foot (2-loop), type XXVI nylon sling to each of the four suspension links using a
large clevis.
2
Raise the slings above the load and install the deadman’s tie as outlined in FM 10-500-2/TO
13C7-1-5.
3
Felt and tape each sling where they may make contact with the box or load.
Figure 3-13. Suspension Slings Installed
3-15
FM 4-20.108/TO 13C7-2-491
STOWING CARGO PARACHUTE
3-15. Prepare, stow, and restrain one G-11 cargo parachute on the front edge of
the M-Gator box according to FM 10-500-2/TO 13C7-1-5 and as shown in Figure
3-14.
Figure 3-14. Cargo Parachute Stowed
3-16
FM 4-20.108/TO 13C7-2-491
INSTALLING EXTRACTION SYSTEM
3-16. Install the Extraction Force Transfer Coupling (EFTC) according to FM
10-500-2/TO13C7-1-5 and as shown in Figure 3-15.
2
1
3
1
Install EFTC actuator mounting bracket using front mounting holes.
2
Install a 12-foot cable.
3
Attach a 9-foot (2-loop), type XXVI nylon sling for the deployment line.
Figure 3-15. Extraction System Installed
3-17
FM 4-20.108/TO 13C7-2-491
INSTALLING PARACHUTE RELEASE
3-17. Prepare and install an M-1 cargo parachute release system
according to FM 10-500-2/TO 13C7-1-5, and as shown in Figure 3-16.
2
1
1
Place the M-1 release on the M-Gator box, and safety it to a convenient place on the load.
2
Fold and secure any slack in the suspension slings.
Figure 3-16. Parachute Release System Installed
3-18
FM 4-20.108/TO 13C7-2-491
POSITIONING EXTRACTION PARACHUTE
3-18. Select the extraction parachute and extraction line needed using the
extraction line requirements table in FM 10-500-2/TO 13C7-1-5. Place the
extraction parachute and extraction line on the load for installation inside
aircraft.
INSTALLING PROVISIONS FOR EMERGENCY RESTRAINTS
3-19. Select and install provisions for emergency restraints according to the
emergency aft restraints requirements in FM 10-500-2/TO 13C7-1-5.
3-19
FM 4-20.108/TO 13C7-2-491
MARKING RIGGED LOAD
3-20. Mark the rigged load according to FM 10-500-2/TO 13C7-1-5 and as
shown in Figure 3-17. Complete the Shipper's Declaration for Dangerous Goods.
If the load varies from the one shown, the weight, height, tip-off curve, CB, and
parachute requirements must be recomputed.
EQUIPMENT REQUIRED
3-21. The equipment required to rig this load is listed in Table 3-1.
CAUTION
Make the final rigger inspection required by FM 10-500-2/
TO 13C7-1-5 before load leaves rigging site.
CB
RIGGED LOAD
Weight
4,630 pounds
Height
78 inches
Width
108 inches
Overall Length
162 inches
Overhang: Front
0 inches
Rear (EFTC)
18 inches
Center of Balance (from front edge of platform)
68 inches
Figure 3-17. M-Gator and CDS Rigged on a 12-Foot Platform For Low- Velocity Airdrop
3-20
FM 4-20.108/TO 13C7-2-491
Table 3-1. Equipment required for rigging M-Gator and CDS on a 12-foot platform for low-velocity
airdrop
National Stock
Item
Quantity
Numbe r
8040-00-273-8713
Adhesive paste, 1-gal
As required
1670-01-035-6054
Bridle, extraction line ba g
1
1670-00-587-3421
Bag, cargo, aerial delivery, A-2
2
1
4030-00-090-5354
Clevis, suspension, 1-in (large
)
5
4020-00-240-2146
Cord, nylon, type III, 550-lb
As required
1670-00-434-5783
Coupling, airdrop, extraction force transfer with cable, 12-ft
1
Cover:
1670-00-360-0328
Clevis, large
1
1670-01-183-2678
Leaf, extraction line (line bag
)
2
Line, drogue (for C-17
)
1670-01-064-4452
60-ft (1-loop), type XXV I
1
Line, extraction
:
1670-01-064-4452
For C-130: 60-ft (1-loop), type XXV I
1
1670-01-107-7652
For C-141: 160-ft (1-loop), type XXV I
1
1670-01-107-7652
For C-5: 160-ft (1-loop), type XXV I
1
1670-01-107-7652
For C-17: 160-ft (1-loop), type XXV I
1
Link assembly:
Two-point, 3 3/4-in
1
5306-00-435-8994
Bolt, 1-in diam, 4-in long
(2
)
5310-00-232-5165
Nut, 1-in, hexagonal
(2
)
1670-00-003-1954
Plate, side, 3 3/4-in
(2
)
5365-00-007-3414
Spacer, large
(2
)
Two-point, 3 3/4-in (for C-1
7)
1
5306-00-435-8994
Bolt, 1-in diam, 4-in long
(2
)
5310-00-232-5165
Nut, 1-in, hexagonal
(2
)
1670-00-003-1954
Plate, side, 3 3/4-in
(2
)
5365-00-007-3414
Spacer, large
(2
)
/
Link, towed mechanized release (H-Block) C-17
aircraft
1
Lumber:
5510-00-220-6146
2- by 4-in
As required
5510-00-220-6148
2- by 6-in
As required
5315-00-010-4659
Nail, steel wire, common, 8d
As required
1670-00-753-3928
Pad, energy dissipating, honeycomb, 3- by 36- by 96-in
9
sheets
3-21
FM 4-20.108/TO 13C7-2-491
Table 3-1. Equipment required for rigging M-Gator and CDS on a 12-foot platform for low-velocity
airdrop (continued)
National Stock
Item
Quantity
Numbe r
Parachute:
1670-01-016-7841
Cargo, G-11B
1
1670-01-063-3715
Cargo, extraction, 15ft
1
1670-01-063-3715
Drogue, 15ft (for C-17
)
1
Platform, airdrop, type
V, 12-foot:
1670-01-353-8425
Bracket assembly, couplin g
(1
)
1670-01-162-2372
Clevis assembly, type V
(22
)
1670-01-353-8424
Extraction bracket assembly
(1
)
1670-01-162-2381
Link, tandem, suspension link assembly
(4
)
5530-00-128-4981
Plywood, 3/4- by 48- by 96-in
6
sheets
1670-01-097-8816
Release, cargo parachute, M-1
1
Sling, cargo airdrop
For suspension:
1670-01-063-7761
16-ft (2-loop), type XXVI nylon webbing
4
For deployment:
1670-01-062-6304
9-ft (2-loop), type XXVI nylon webbin g
1
For riser extention
:
1670-01-062-6301
3-ft (2-loop), type XXVI nylon webbin g
1
7510-00-266-5016
Tape, adhesive, 2-in
As required
1670-00-937-0271
Tie-down assembly, 15-ft
24
Webbing:
8305-00-268-2411
Cotton, 1/4-in, type I
As required
8305-00-082-5725
Nylon, tubular, 1/2-in
As required
8305-00-261-8585
Type VIII
As required
3-22
FM 4-20.108/TO 13C7-2-491
Glossary
AFB
Air Force Base
AFTO
Air Force Technical Order
AFSOC
Air Force Special Operations Command
ALC
Airlift Logistics Center
AMC
Air Mobility Command
CB
center of balance
CDS
container delivery system
d
penny
DC
District of Columbia
diam
diameter
EFTC
extraction force transfer coupling
FM
field manual
ft
foot/feet
gal
gallon
HQ
headquarters
in
inch
lb
pound
M-Gator
military utility vehicle
No
number
TRADOC
US Army Training and Doctrine Command
USA
United States of America
TM
technical manual
TO
technical order
Glossary-1
FM 4-20.108/TO 13C7-2-491
References
AFR 55-40/AR59-4
Joint Airdrop Inspection Records, Malfunction Investigations and
Activity Reporting. 1 May 1998.
*AFJMAN 24-204/
Preparing Hazardous Materials for Military Air Shipments.
TM 38-250
25 November 1994.
FM 10-500-2/TO 13C7-1-5
Airdrop of Supplies and Equipment: Rigging Airdrop Platforms.
1 November 1990.
FM 10-500-3/TO 13C7-1-11/
Airdrop of Supplies and Equipment: Rigging Containers.
FMFM 7-47
26 September 1996.
FM 10-500-53/MCRP No 4-
Airdrop of Supplies and Equipment: Rigging Amunition.
3.8/TO 13C7-18-41
19 August 1996.
TM 10-1670-268-20&P/
Organizational Maintenance Manual With Repair Parts and Special
TO 13C7-52-22
Tools List: TypeV Airdrop Platform. 1 June 1986.
TM 10-1670-278-23&P/TO
Unit and Intermediate DS Maintenance Manual Including Repair
13C5-26-2/NAVAIR 13-1-27
Parts and Special Tools List for Parachute, Cargo Type, 15-ft Diam,
/TM 01109C-23&P/1
Extraction. 6 November 1989.
TM 10-1670-279-23&P/TO
Unit and Intermediate DS Maintenance Manual Including Repair
13C5-27-2/NAVAIR 13-1-28
Parts and Special Tools List for Parachute, Cargo Type, G-11A,
G-11B, and G-11C. 5 August 1991.
TM 10-1670-280-23&P/TO
Unit and Intermediate DS Maintenance Manual Including Repair
13C5-31-2/NAVAIR 13-1-31
Parts and Special Tools List for Parachute, Cargo Type, 22-ft Diam,
Extraction. 30 August 1989.
*AFJMAN 24-204/TM 38-250 has superseded AFR 71-4/TM 38-250 (15 January 1988).
Refences-1
FM 4-20.108/TO 13C7-2-491
TM 10-1670-286-20/ Unit Maintenance Manual for Sling/Extraction Line Panel (Includ-
TO 13C5-2-41
ing Stowing Procedures). 1 April 1986
TM 10-1670-296-20&P/ Unit Maintenance Manual Including Repair Parts and Special Tools
TO 13C7-49-2
List for Ancillary Equipment for Low-Velocity Airdrop System
(LVADS). 15 September 19995
AFTO Form 22
Technical Order Publication Improvement Report
DA Form 2028
Recommended Changes to Publication and Blank Forms. February
1974.
*Shipper’s Declaration Locally Procured Form.
for Dangerous Goods
*Shipper’s Declaration for Dangerous Goods has superseded DD Form 1387-2 (February
1982).
References-2
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