(pi libraryofmichigan · 2019-02-21 · fm 10–536/to 13c7–16–8] chapter 1 introduction 1–1....
TRANSCRIPT
AIR FORCE TO 13C7–1 6–81
o), 2o’ \0 - 532\D\O\ , 2. ARMY FM 10–536
AIRDROP OF SUPPLIES AND EQUIPMENT
RIGG|NG
1/2–TON
PLATFORM TRUCKS
DEPARTMENTS OF THE ARMY AND THE AIR FORCE
DECEMBER 1973
TAGO 3242A
|||||||||||000 010 452 45
LIBRARY OF MICHIGAN
D\o\.;-10". \o-53¢.» ARMY FM 10-536AIR FORCE TO 13C7—16-81
AIRDROP OF SUPPLIES AND EQUIPMENT
RIGGING1/2—TON
PLATFORM TRUCKS
DEPARTMENTS OF THE ARMY AND THE AIR FORCEDECEMBER "I973
TAGO 3242A
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Digitized by GOOSIQ
*FM 10–536/TO 13C7–1 6–81
FIELD MANUAL DEPARTMENTS OF THE ARMY
NO. 10–536 AND THE AIR FORCE
TECHNICAL ORDER
NO. 13C7–16–81 WASHINGTON, D.C., 31 December 1973
AIRDROP OF SUPPLIES AND EQUIPMENT
RIGGING V2-TON PLATFORM TRUCKS
Paragraph Page
CHAPTER 1. INTRODUCTION
Scope . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1–1 1
Special Considerations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1–2 1
Recommended Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1–3 1
2. RIGGING TWO1/2-TON PLATFORM TRUCKS
Description of Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2–1 2
Preparing Trucks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2–2 2
Preparing Platform, Installing Suspension
Slings, and Load Spreader. . . . . . . . . . . . . . . . . . . . . . . . . 2–3 2
Stowing Accompanying Load . . . . . . . . . . . . . . . . . . . . . . . . . 2–4 5
Preparing and Positioning Honeycomb . . . . . . . . . . . . . . . 2–5 7
Positioning Trucks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2–6 8
Installing Lashings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2–7 8
Installing Load Cover . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2–8 11
Stowing Cargo Parachutes . . . . . . . . . . . . . . . . . . . . . . . . . . . 2–9 11
Installing Extraction System. . . . . . . . . . . . . . . . . . . . . . . . . 2–10 11
Installing Release System . . . . . . . . . . . . . . . . . . . . . . . . . . . 2–11 12
Installing Platform Retainer Strap . . . . . . . . . . . . . . . . . . . 2–12 12
Positioning Extraction Parachute . . . . . . . . . . . . . . . . . . . . 2–13 12
Marking Rigged Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2–14 12
Equipment Required . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2–15 13
APPENDIX REFERENCES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15
ILLUSTRATIONS
Page
Figure 2–1 Truck prepared . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
2–2 Platform prepared . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3
2–3 Ammunition stowed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
2–4 Honeycomb stacks positioned . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7
2–5 Front lashings installed . . . . . . . . .- - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 8
2–6 Side lashings installed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9
2–7 Rear lashings installed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10
2–8 Extraction system installed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11
2–9 Completely rigged load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13
*This manual supersedes TM 10–500–36/TO 13C7–16–81, 18 January 1971, including all changes.
*FM 10-536/TO I3C7-I 6-81
FIELD MANUAL DEPARTMENTS OF THE ARMYN0. 10—536 AND THE AIR FORCETECHNICAL ORDERN0. 13C7-16-81 WASHINGTON, D.C., .51 December 197.:
AIRDROP OF SUPPLIES AND EQUIPMENTRIGGING I/2-TON PLATFORM TRUCKS
I’a1';ip_i‘;iph
INTRODUCTIONScope . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .Special Considerations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..Recommended Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..
CHAPTER 1.,_.
»A;l\'Ji—l>—->-
2. RIGGING TWO‘/2-TON PLATFORM TRUCKSDescription of Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..Preparing Trucks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..Preparing Platform, Installing Suspension
Slings, and Load Spreader . . . . . . . . . . . . . . . . . . . . . . . ..Stowing Accompanying Load . . . . . . . . . . . . . . . . . . . . . . . ..Preparing and Positioning Honeycomb . . . . . . . . . . . . . ..Positioning Trucks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..Installing Lashings . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..Installing Load Cover . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..Stowing Cargo Parachutes . . . . . . . . . . . . . . . . . . . . . . . . . ..Installing Extraction System . . . . . . . . . . . . . . . . . . . . . . . ..Installing Release System . . . . . . . . . . . . . . . . . . . . . . . . . ..Installing Platform Retainer Strap . . . . . . . . . . . . . . . . . ..Positioning Extraction Parachute . . . . . . . . . . . . . . . . . . ..Marking Rigged Load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. ‘.-Equipment Required . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. '.- T
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APPENDIX REFERENCES . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..
ILLUSTRATIONSP
I“ l§_'I1l‘\* 2»1‘2—22432-4LBJ)
Truck prcpan-<l . . . . I . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..Platfurni pi‘:-pared ..............Ammunition S[()\\'t'(l . . . . . . . .H<mc)'uo|nl> stacks piisitioiicrl 4 . . I4 . . . . . . . . ..Front lashings installm-il . . . . ....Side lashings installed. .. ..,.Rear lashings installed . . . . . ....I-Ixtraction system installed ......(‘ompletely rigged load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 . . . , . . i . . . . . . ..
14$ZJT22—82-9
*This manual supersedes TM IO-500-36/TO l3C7—l6—8l, 18 January I971, including all changes.
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FM 10–536/TO 13C7–1 6–8]
CHAPTER 1
INTRODUCTION
1–1. Scope
This manual specifies and illustrates the equip
ment and procedures necessary to prepare and
rig two M274, 92-ton platform trucks for airdrop
from the C-130 and C-141 aircraft.
1–2. Special Considerations
Caution: Only ammunition authorized by
TM 10–500–53/TO 13C7–18–41 may be air
dropped.
a. This load may include a dangerous ma
terial. When included, it must be packaged,
marked, and labeled in compliance with AFM
71–4/TM 38–250.
b. When this load is dropped from the C-141
aircraft it must weigh at least 3,500 pounds.
c. The platform retainer strap is not required
for loads dropped from a C-141 aircraft.
d. Additional honeycomb is required on all
loads delivered on drop zones with ground eleva
tions of 6,000 to 10,000 feet.
e. A copy of this manual should accompany
the rigged load to the aircraft.
1–3. Recommended Changes
Users of this publication are encouraged to sub
mit recommended changes and comments to im
prove the publication. Comments should be
keyed to the specific page, paragraph, and line
of the text in which the change is recommended.
Reasons will be provided for each comment to
insure understanding and complete evaluation.
Comments should be prepared using DA Form
2028 (Recommended Changes to Publication) and
forwarded direct to the Commandant, US Army
Quartermaster School, ATTN: ATSM-CTD–TL,
Fort Lee VA. 23801. In addition Air Force units
should forward comments on AFTO Form 22 to
SAAMA (SANSTR) Kelly AFB, Texas 78241.
FM I0—536/TO I3C7-I6-81
CHAPTER I
INTRODUCTION
'I—'l. ScopeThis manual specifies and illustrates the equip-ment and procedures necessary to prepare andrig two M274, 1/2-ton platform trucks for airdropfrom the C-130 and C-141 aircraft.
‘I-2. Special ConsiderationsCaution: Only ammunition authorized by
TM 10-500-53/TO l3C7-18-41 may be air-dropped.
a. This load may include a dangerous ma-terial. When included, it must be packaged,marked, and labeled in compliance with AFM71—4/TM 38-250.
b. When this load is dropped from the C-141aircraft it must Weigh at least 3,500 pounds.
c. The platform retainer strap is not requiredfor loads dropped from a C-141 aircraft.
d. Additional honeycomb is required on all
loads delivered on drop zones with ground eleva-tions of 6,000 to 10,000 feet.
e. A copy of this manual should accompanythe rigged load to the aircraft.
I-3. Recommended ChangesUsers of this publication are encouraged to sub-mit recommended changes and comments to im-prove the publication. Comments should bekeyed to the specific page, paragraph, and lineof the text in which the change is recommended.Reasons will be provided for each comment toinsure understanding and complete evaluation.-Comments should be prepared using DA Form2028 (Recommended Changes to Publication) andforwarded direct to the Commandant, US ArmyQuartermaster School, ATTN: ATSM-CTD—TL,Fort Lee VA. 23801. In addition Air Force unitsshould forward comments on AFTO Form 22 toSAAMA (SANSTR) Kelly AFB, Texas 78241.
FM 10–53.6/TO 13C7–1 6–81
CHAPTER 2
RIGGING TWO W2-TON PLATFORM TRUCKS
2–1. Description of load
Two M274, '4-ton platform trucks, with an ac
companying load are rigged on an 8-foot modular
platform with one or two G-11A cargo para
chutes. Each unrigged truck weighs 900 pounds.
It is 118 inches long, reducible to 101 inches, 49
inches wide, and 49 inches high, reducible to 31
inches. The center of gravity of each truck is 48
inches from the rear edge of the cargo bed.
2–2. Preparing Trucks
Make certain that the fuel tank is not more than
three-fourths full. Disconnect brake, clutch, and
accelerator cables from connectors. Remove and
stow footrest under the right side of the truck.
Safety the footrest in place with type III nylon
cord as shown in figure 2–1. Remove the steer
ing wheel with the column and brace attached
and stow it under the right side of the truck
next to the footrest. Safety the steering wheel
with type III nylon cord. Remove and stow the
driver's seat as shown in figure 2–1. Secure the
engine access covers with type III nylon cord.
DRIVER'S
SEAL
Figure 2–1. Truck prepared.
2–3. Preparing Platform, Installing Sus
pension Slings, and Load Spreader
Prepare an 8-foot modular (type II) platform
(fig. 2–2) and install the suspension slings, and
load spreader as follows:
a. Inspecting Platform. Inspect, or assemble
and inspect the modular platform according to
procedures in TM 10–1670–208–23/TO 13C3–4–12.
b. Installing Suspension Slings. Form the
suspension slings with four 3-foot slings and four
12-foot (2-loop) sling. Place a tiedown clevis in
each end of the 3-foot sling and attach the
clevises to the platform. Repeat this procedure
for the other three slings. Starting at the front
of each rail, attach a clevis to the 3d and the 6th
clevis holes for the front slings and to the 12th
and 15th clevis holes for the rear slings. Tape
the loop of each 12-foot (2-loop) sling to the
center of each 3-foot sling as shown in A, figure
2–2.
FM 'l 0-536/TO I 3C7-I 6-8 I
CHAPTER 2
RIGGING TWO I/2-TON PLATFORM TRUCKS
2-I. Description of loadTwo M274, '15-ton platform trucks, with an ac-companying load are rigged on an 8-foot modularplatform with one or two G-11A cargo para-chutes. Each unrigged truck weighs 900 pounds.It is 118 inches long, reducible to 101 inches, 49inches wide, and 49 inches high, reducible to 31inches. The center of gravity of each truck is 48inches from the rear edge of the cargo bed.
2-2. Preparing TrucksMake certain that the fuel tank is not more than
1's. 1' ~*‘v »_,L.-- .- -.7»
#1:-I 5&-
three-fourths full. Disconnect brake, clutch, andaccelerator cables from connectors. Remove andstow footrest under the right side of the truck.Safety the footrest in place with type III nyloncord as shown in figure 2—1. Remove the steer-ing wheel with the column and brace attachedand stow it under the right side of the trucknext to the footrest. Safety the steering wheelwith type III nylon cord. Remove and stow thedriver’s seat as shown in figure 2—1. Secure theengine access covers with type III nylon cord.
DRlVIR'SSE/ll
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Figure 2-I. Truck prepared.
2-3. Preparing Platform, Installing Sus-pension Slings, and load SpreaderPrepare an 8-foot modular (type II) platform(fig. 2-2) and install the suspension slings, andload spreader as follows:
a. Inspecting Platform. Inspect, or assembleand inspect the modular platform according toprocedures in TM 10-1670-208-23/TO l3C3—4—12.
b. Installing Suspension Slings. Form the2
suspension slings with four 3-foot slings and four12-foot (2-loop) sling. Place a tiedown clevis ineach end of the 3-foot sling and attach theclevises to the platform. Repeat this procedurefor the other three slings. Starting at the frontof each rail, attach a clevis to the 3d and the 6thclevis holes for the front slings and to the 12thand 15th clevis holes for the rear slings. Tapethe loop of each 12-foot (2-loop) sling to thecenter of each 3-foot sling as shown in A, figure2-2
FM 10–536/TO 13C7–16–8]
pººſº ºn 3
**s—e.-
PLYWOOD
(3/4" x 48" x 96")
(10AD SPREADERS)
/N
prºmº
(2100P
A. Platform prepared
Figure 2–2. Platform prepared and honeycomb positioned.
FM “I-536/TO I 3C7-I 6-81
A. Platform preparedFigure 2-2. Platform prepared and honeycomb positioned.
3
Digitized by GOQSIQ
FM 10–536/TO 13C7–16–8]
TºmTºm.
3" x 36" x 96")
(2 FECES
-
HONEYCOMB
g"º",(2 PIECES)
B. Honeycomb positioned
Figure 2–2–Continued
FM I0-536/TO l3C7-I 6-Bl
. u1.11..‘
B. Honeycomb positioned
Fi u re 2-;2—Conti1Iued.9
Digitized by
FM 10–536/TO 13C7–1 6–81
c. Attaching Tiedown Clevises. Starting at the
front of each rail, attach tiedown clevises to the
1st, 2d, 4th, 5th, 7th, 11th, 13th, 14th, and 16th
clevis holes. Again starting at the front of each
rail, number the clevises attached to the right
rail from 1 through 13 and those attached to the
left rail 1A through 13A as shown in A, figure
2–2.
d. Positioning Plywood Load Spreader. Use
two pieces of 94- by 48- by 96-inch plywood for
the load spreader. Place one piece on each panel
of the platform as shown in A, figure 2–2.
e. Positioning Honeycomb. Prepare and posi
tion the honeycomb on the platform as shown in
B, figure 2–2.
2–4. Stowing Accompanying Load
Caution: Only ammunition listed in TM
10–500–53/TO 13C7–18–41 may be dropped.
When the load is dropped from the C-141 air
craft the minimum weight must be 3,500
pounds.
a. General. The accompanying load must meet
the requirements and restrictions as outlined in
TM 10–500/TO 13C7–1–5. Dangerous material
must be packaged, marked, and labeled in com
pliance with AFM 71–4/TM 38–250. The accom
panying load may consist of rations, spare parts,
ammunition, or similar items and they must be
evenly distributed on the platform.
b. C-130 Aircraft. This load may be rigged
with or without an accompanying load when
dropped from the C-130 aircraft. When there is
an accompanying load, it must not weigh more
than 1,700 pounds.
c. C-141 Aircraft. This load must have a
minimum accompanying load of 700 pounds when
dropped from the C-141 aircraft. The accom
panying load must not weigh more than 1,700
pounds.
d. Positioning Binding Lashings. Make four
30-foot lashings (tiedown straps) as outlined in
TM 10–500/TO 13C7–1–5 and use them for bind
ing lashings. Place two lashings on the front and
two on the rear pieces of honeycomb.
e. Positioning and Binding Ammunition.
Position seven boxes of ammunition on the front
and seven boxes on the rear of the platform as
shown in figure 2–3. Join each binding lashing
with two heavy-duty D-rings and a load binder.
f. Lashing Ammunition. To The Platform.
Position one piece of 3- by 36- by 96-inch hon
eycomb and one piece of 94- by 36- by 96-inch
plywood on top of the front ammunition boxes as
shown in figure 2–3. Repeat the above procedure
on the rear ammunition boxes. Using six 30-foot
lashings, 12 heavy-duty D-rings, and 6 load
binders, lash the ammunition boxes as shown in
figure 2–3.
c. Attaching Tiedown Clevises. Starting at thefront of each rail, attach tiedown clevises to the1st, 2d, 4th, 5th, 7th, 11th, 13th, 14th, and 16thclevis holes. Again starting at the front of eachrail, number the clevises attached to the rightrail from 1 through 13 and those attached to theleft rail 1A through 13A as shown in A, figure2-2.
d. Positioning Plywood Load Spreader. Usetwo pieces of %- by 48- by 96-inch plywood forthe load spreader. Place one piece on each panelof the platform as shown in A, figure 2-2.
e. Positioning Honeycomb. Prepare and posi-tion the honeycomb on the platform as shown inB, figure 2-2.
2-4. Stowing Accompanying Load
Caution: Only ammunition listed in TM10-500-53/TO l3C7-18-41 may be dropped.When the load is dropped from the C-141 air-craft the minimum weight must be 3,500pounds.
a. General. The accompanying load must meetthe requirements and restrictions as outlined inTM 10-500/TO 13C7-1-5. Dangerous materialmust be packaged, marked, and labeled in com-pliance with AFM 71-4/TM 38-250. The accom-panying load may consist of rations, spare parts,ammunition, or similar items and they must beevenly distributed on the platform.
FM 10-536/TO 'l3C7—l 6-Bl
b. C-130 Aircraft. This load may be riggedwith or without an accompanying load whendropped from the C-130 aircraft. When there isan accompanying load, it must not weigh morethan 1,700 pounds.
c. C-141 Aircraft. This load must have aminimum accompanying load of 700 pounds whendropped from the C-141 aircraft. The accom-panying load must not weigh more than 1,700pounds.
d. Positioning Binding Lashings. Make four30-foot lashings (tiedown straps) as outlined inTM 10-500/TO 13C7-1-5 and use them for bind-ing lashings. Place two lashings on the front andtwo on the rear pieces of honeycomb.
e. Positioning and Binding Ammunition.Position seven boxes of ammunition on the frontand seven boxes on the rear of the platform asshown in figure 2-3. Join each binding lashingwith two heavy-duty D-rings and a load binder.
f. Lashing Ammunition To The Platform.Position one piece of 3- by 36- by 96-inch hon-eycomb and one piece of %- by 36- by 96-inchplywood on top of the front ammunition boxes asshown in figure 2-3. Repeat the above procedureon the rear ammunition boxes. Using six 30-footlashings, 12 heavy-duty D-rings, and 6 loadbinders, lash the ammunition boxes as shown infigure 2-3.
5
FM 10–536/TO 13C7–1 6–81
30F001 PLYWOOD 30 FOOI
BINDING LASHINES (3/4" x 36" x 96") BINDING LASHINGS
HONEYCOMB
(3" x 36" x 96")
Lashing - lashing Iſedown - A363.3
No. Clewis No. Instructions N0. Clewis No. Instructions
l 1 to 1A Around front of boxes, through carrying handles M 8 to 8A | Around rear of boxes, through carrying handles
2 2 to 2A | Around fear of boxes, through carrying handles 5 13 to 13A | Around front of boxes, through carrying handles
3 4 to 4A Over top of boxes 6 11 to 11A Over top of boxes
Figure 2–3. Ammunition stowed.
FM ‘I0--536/TO I 3C7-‘I 6-8 I
_“-_-'..1*_'<.1.1';-. r-uni--_-1:._ . .- .. i .
lashing IIGIIOVIII T L . um Il0(IOVIl1 . we-3-3M (nevi; M lnsinltilnns M cmis M IIISIIUCIIOHS
1 7 I0 ll NOW lfllli OI B0195. Ill"!-Ell WIYIIE |Wll9$ 4 8 to 8A Around rear of boxes, through carrying handles2 2 to 2A Around rear of boxes, though marrying handles 5 13 in 13A Around front of boxes, through carrying handles3 4 to 4A Over top of boxes 6 ll to 11A Over l0p of boxes
Figure 2-‘I. Ammunition slowed.
6
Digitized by GOOSIQ
FM 10–536/TO 13C7–1 6–81
2–5. Preparing and Positioning Hon- Note. If the load is to be dropped on a drop zone with
eycomb ground elevation between 6,000 and 10,000 feet, add an ad
ditional layer of honeycomb to all of the stacks.
Prepare and position the honeycomb stacks as il
lustrated and described in figure 2–4. Paste hon
eycomb layers together.
(3" X 14"x 25")
º–
|º
===º-2 sº-sº ===C=2 *- -
ºf Tºº ºn 1
SIACK PIECES WIDIH LENGTH
N0. (NCHES) (NCHES)
l *5 18 25
2 14 9
l 14 25
2 Same as Stack No. 1 |
3 *5 12 25
2 8 25
4 Same 3S stack No. 3
*Add One additional piece of honeycomb when load is dropped on a
drop Zone with ground elevation between 6,000 and 10,000 feet.
Figure 2–4. Honeycomb stacks positioned.
2-5 Preparing and Posltronrng Hon Note If the load is to be dropped on a drop zone Wltlleycomb ground elevation between 6,000 and 10,000 feet, add an ad-dltlonal layer of honeycomb to all of the stacksPrepare and position the honeycomb stacks as ll-lustrated and described 1n figure 2-4 Paste hon-eycomb layers together
IA P S W Illll LEIEIIIl|IlCllE$)_ lllllilllsl
259
25Sameasstackllol
Z5
Z5
SameasstackNo3*Add one additional piece of honeycomb when load rs dropped on adrop zone with ground elevation between 6.11!) and 10.!!!) feet
Figure 2-it Honeycomb stacks positioned
Digitized by
FM I0-536/TO 'l3C7-'I 6-81
FM 10–536/TO 13C7–1 6–81
2–6. Positioning Trucks
Position the trucks on the honeycomb stacks.
The trucks overhang the front and rear of the
platform 3 inches.
2–7. Installing Lashings
Caution: Make sure that the lashings are
RIGHT TRUCK
not so tight that they cause the platform to
bow.
Lash the trucks to the platform with single Dac
ron lashings as shown in figures 2–5, 2–6, and
2–7. Pad all sharp edges that may come in con
tact with the lashings.
Note. If Dacron lashings are not available, use double
cotton lashings. DO NOT mix Dacron and cotton lashings.
LEFT TRUCK
Lashing A 365.3- ledown - Iſedown -
º ºº Instructions No. 1 Clewis No. Instructions
7 l Around engine protector frame of right truck 8 1A Around engine protector frame of left truck
Figure 2–5. Front lashings installed.
FM 10-536/TO l3C7-16-81
2-6. Positioning Trucks not so tight that they cause the platform toPosition the trucks on the honeycomb stacks. b°“’-The trucks overhang the front and rear of the Lash the trucks to the platform with single Dac-platform 3 inches. ron lashings as shown in figures 2-5, 2-6, and
2-7. Pad all sharp edges that may come in con-tact with the lashings.
2-7° lpstanlng Losiungs Note. If Dacron lashings are not available, use doubleCaution: Make sure that the l88hil1gS are cotton lashings. DO NOT mix Dacron and cotton lashings.
RIGHT TRUCK EFT TRUCK
._ ..___ __‘l
~~¢
-1" i ' ‘ii I _
. ~o\. ..¢|r ‘ “"41; ll"-'
*_',,l.>.. I...n ‘D ‘
L-Li ' —
~ .-1"" ' ‘
- —' i i n‘ l'd W‘? _ .Lashmg Instructions | Laiking @|:,;S0 lnstructrons A3653
Around engrne protector frame of rrght truck | 8 1A Around eflglfle DIOIBCIOI frame OT kill "HER
Figure 2-5. Front laslrirzgs installed.
8
Digitized by CIOOSIQ
FM 10–536/TO 13C7–1 6–81
Lashing | Tiêdown lashing ſiędown A 36.63
No. 1 Clewis No. Instructions No. 1 Clewis NO. Instructions
9 5 AſOUnd inside frame of left truck at rear of 13 4 Through rear lifting handle, right truck
frame bed support.
10 5A Around inside frame of right truck at rear of 14 AA Through rear lifting handle, left truck
frame bed support
11 10 AſOund inside frame of left truck at front of 15 11 Through front lifting handle, ſight truck
frame bed support
12 10A Around inside frame of right truck at front of 16 11A Through front lifting handle, left truck
frame bed support
Figure 2–6. Side lashings installed.
lashingNo
5=w
wnvvu s :6
‘":::w 5,/”~,
\
tiedownClevis No. Instructions
FM 10-536/TO 'l3C7-l 6-81
.__._,__.
EM
lashingNo.
tiedown A35Ciel/I8 N0- instructions
as
9 5
10 5A
ll 10
12 10A
frame bed support.
frame bed support
frame bed support
frame bed support
Around inside frame of left truck at rear of
Around inside frame of right truck at rear of
' Around inside frame of left truck at front of
Around inside frame of right truck at front of
13
14
15
15
4 Through rear lifting handle, right truck
4A I Through rear lifting handle, left truck
11 Through front lifting handle, right truck
11A through front lifting handle, left truck
Figure 2-6. Side lashings installed.
Digitized by C|OO8l€
FM 10–536/TO 13C7–1 6–81
LEFI IRUCK RIGHT IRUCK
TºII
|
º
|Tºº
- *-*.---
| "ºfºlºu
lashing | Iſedown - lashing - -
No. Clewis No. Instructions No. Clewis No. Instructions
17 13 Around inside frame, left truck 18 13A Around inside frame, right truck l
Figure 2–7. Rear lashings installed.
10
F'
FM 10-536/TO I 3C7—l 6-8 ‘I
I
lashing
-j — .4 _ l -.~ .!'.¢ r 1'_ L»
l
Hl TRUCK
‘-‘.5
i ~- ...
\ .lp..i.- ;_1 .__.L
Tiedown lashingNo.
tiedown
_ -QI-
' -0
W A‘ if lrli'iii- _lNl*iill\* l
clevis No InstructionsA7367-3
17 13
i No. Clevis No. Instructions
i
Around inside frame, left truck 18 13A
Figure 2-7. Rear lashings installed.
Around inside frame, right truck
Digitized by GOO8l€
FM 10–536/TO 13C7–1 6–81
2–8. Installing load Cover
Place a 3-year piece of cotton duck cloth over
the front of the trucks and tie it with type III
nylon cord.
2–9. Stowing Cargo Parachutes
Prepare two G–11A cargo parachutes as outlined
80 POUND COTION
WEBB/NG (DOUBLED)
(2100P)
12:00 SLING
(2100P)
DEPLOYMENT LINE
60 NCH
CONNECTOR
SIRAP
in TM 10–500/TO 13C7–1–5 and place them on
top of the load as shown in figure 2–8. Use a
12-foot (2-loop) sling as a deployment line. In
stall a 6-yard restraint strap according to TM
10–500/TO 13C7–1–5. Secure the ends of the
strap to the wheel clevises.
PLAIFORM
REIANERSIRAP
gFOOT STING
(2100P)
Figure 2–8. Eactraction system installed.
2–10. Installing Extraction System
a. Forming Eattraction Attaching Point. Use
a load tiedown clevis, two 9-foot (2-loop) slings,
and a large clevis assembly to form the extrac
tion attaching point. Place one end of a 9-foot
(2-loop) sling on a load tiedown clevis and attach
the clevis to the 17th clevis hole in the right
platform rail. Attach the second 9-foot (2-loop)
sling to the 17th clevis hole in the left rail in the
same manner. Place the free ends of the slings
on the large clevis assembly as shown in figure
2–8.
b. Installing Ea:traction Components. Using a
60-inch connector strap, install the extraction
System components to the extraction attaching
point according to procedures in TM 10–500/TO
13C7–1–5 and as shown in figure 2–8.
| I
2—8. Installing Load CoverPlace a 3-year piece of cotton duck cloth overthe front of the trucks and tie it with type IIInylon cord.
2-9. Stovving Cargo ParachutesPrepare two G-11A cargo parachutes as outlined
soeouiio COTl0N4 WEBBING (DOUBLED)\-
9-roor SllNG(2l00Pl ST12¥00l SLING
60 INCHCONNECTOR
BREAKAWAYAT C IN
FM 10-536/TO 'l3C7—l 6-81
in TM 10-500/TO 13C7-1-5 and place them ontop of the load as shown in figure 2—8. Use a12-foot (2-loop) sling as a deployment line. In-stall a 6-yard restraint strap according to TM10-500/TO l3C7-1-5. Secure the ends of thestrap to the wheel clevises.
l PLATFORMSTRAP9FO0T
A-3683
Figure 2-8. Extraction system installed.
2—'lO. Installing Extraction Systema. Forming Extraction Attaching Point. Use
a load tiedown clevis, two 9-foot (2-loop) slings,and a large clevis assembly to form the extrac-tion attaching point. Place one end of a 9-foot(2-loop) sling on a load tiedown clevis and attachthe clevis to the 17th clevis hole in the rightplatform rail. Attach the second 9-foot (2-loop)sling to the 17th clevis hole in the left rail in the
same manner. Place the free ends of the slingson the large clevis assembly as shown in figure2-8.
b. Installing Extraction Components. Using a60-inch connector strap, install the extractionsystem components to the extraction attachingpoint according to procedures in TM 10-500/TO13C7-1-5 and as shown in figure 2—8.
H
Digitized by GO()gl€
FM 10–536/TO 13C7–1 6–8 l
2–11. Installing Release System
Attach two 5,000-pound cargo parachute releases
to the suspension system according to proce
dures in TM 10–500/TO 13C7–1–5 and place them
on top of the load. Fold the slack in the suspen
sion slings and tape or tie the folds with
80-pound cotton webbing.
2–12. Installing Platform Retainer Strap
When the C-130 aircraft is used for airdrop, in
stall a platform retainer strap according to pro
cedures in TM 10–500/TO 13C7–1–5 and as
shown in figure 2–8.
Note. The platform retainer strap IS NOT used on loads
dropped from the C-141 aircraft.
2–13. Positioning Extraction Parachute
a. C-130 Aircraft. Place a 15-foot cargo ex
traction parachute (reefed with a 260-inch
reefing line) and a 60-inch nylon webbing strap
(shear strap) on the load for installation in the
aircraft.
b. C-141 Aircraft. Place a 15-foot cargo ex
traction parachute (reefed with a 260-inch
reefing line) on the load for installation in the
aircraft. The extraction parachute must be
equipped with an 85-inch pendulum line. In addi
tion, a type IV link assembly and a 60-foot
(2-ply) type X nylon extraction line must be
used to form a 120-foot extraction line. Form the
120-foot extraction line as outlined in TM
10–500/TO 13C7–1–5.
2–14. Marking Rigged Load
Mark the rigged load according to TM 10–500/TO
13C7–1–5 and as shown in figure 2–9. The rigged
load without an accompanying load weighs 2,800
pounds. The illustrated accompanying load
weighs 1,700 pounds. If the accompanying load
is varied, the weight, center of gravity, and
parachute requirements must be computed.
Note. When rigged for airdrop on a drop zone with
ground elevation of 6,000 to 10,000 feet, add 6 inches to the
height reflected on figure 2–9.
12
rm to-sac/to 1361-16-812-'l'l. Installing Release SystemAttach two 5,000-pound cargo parachute releasesto the suspension system according to proce-dures in TM 10-500/TO l3C7—1—5 and place themon top of the load. Fold the slack in the suspen-sion slings and tape or tie the folds with80-pound cotton webbing.
2—'l2. Installing Platform Retainer StrapWhen the C-130 aircraft is used for airdrop, in-stall a platform retainer strap according to pro-cedures in TM 10-500/TO 13C7—1-5 and asshown in figure 2—8.
Nolc. The platform retainer strap IS NOT used on loadsdropped from the C-141 aircraft.
2-13. Positioning Extraction Parachutea. C-1.10 Aircraft. Place a 15-foot cargo ex-
traction parachute (reefed with a 260-inchreefing line) and a 60-inch nylon webbing strap(shear strap) on the load for installation in theaircraft.
‘I2
b. C-141 Aircraft. Place a 15-foot cargo ex-traction parachute (reefed with a 260-inchreefing line) on the load for installation in theaircraft. The extraction parachute must beequipped with an 85-inch pendulum line. In addi-tion, a type IV link assembly and a 60-foot(2-ply) type X nylon extraction line must beused to form a 120-foot extraction line. Form the120-foot extraction line as outlined in TM10-500/TO 13C7—l—5.
2-14. Marking Riggecl loadMark the rigged load according to TM 10-500/TO13C7-1-5 and as shown in figure 2—9. The riggedload without an accompanying load weighs 2,800pounds. The illustrated accompanying loadweighs 1,700 pounds. If the accompanying loadis varied, the weight, center of gravity, andparachute requirements must be computed.
.\i'of1'. When rigged for airdrop on a drop zone withground elevation of 6,000 to 10,000 feet, add 6 inches to theheight reflected on figure 2-9.
FM 10–536/TO 13C7–1 6–81
RIGGED LOAD DAIA
Weight. *4,500 pounds *Height 74 inches
Width: 108 inches Length. 102 inches
OVerhäng: Front: 3 inches
Reaſ: 3 inches
Center of Gravity. 48 inches from the front edge of platform
*includes weight of illustrated accompanying load
*77 inches when load is rigged for drop on drop 10ne with ground
l elevation between 6,000 and 10,000 feet.
Figure 2–9. Completely rigged load.
2–15. Equipment Required
The equipment required for rigging this load is
listed in table 2–1. This table includes the
equipment required to rig the illustrated accom
panying load.
13
FM TO-536/TO l3C7-I 6-81
\ *<
RIGGED LOAD DATA
Weight; *4,500 pounds “Height; 74 inches
Width; 108 ‘inches Length; 102 inches
Overhang; Front: 3 inchesRear; 3 inches
Center of Gravity; 48 inches from the front edge of platform*lncludes weight of illustrated accompanying load**77 inches when load is rigged for drop on drop zone with ground
elevation between 6,000 and 10,000 feet.
Figure 2-9. Completely rigged load.
2-I 5. Equipment Required equipment required to rig the illustrated accom-The equipment required for rigging this load is Panying load-listed in table 2-1. This table includes the
13
Digitized by C|OOgl€
FM 10–536/TO 13C7–1 6–8 l
Table 2–1. Equipment Required
Federal
Stock No. Item Quantity
8040-273–8713 Adhesive, paste, 1-gal . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required
1377–958–1048 Cartridge, time-delay, 20-sec. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
1670–090–53.54 Clevis Assembly, suspension, large . . . . . . . . . . . . . . . . . . . . . . . . . . ............................ 5
8305–242–3593 | Cloth, cotton duck, 60-in. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ........................ 3 yd
4020–240–21.46 Card, nylon, type III, 550-lb. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required
1670–360–0328 Cover, clevis, large . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
8135–664–6958 Cushioning material, packaging, cellulose wadding ....................................... As required
1670–217–24.21 Link Assembly, connector, removeable (For C-141 aircraft) ............................. 2
1670–783–5988 Link Assembly, single, type IV (Add 1 for C-141 aircraft).............................. 1
1670–799–8596 Load Coupler, 8-spool . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1
1670–753–3928 | *Pad, energy dissipating, honeycomb, 3- by 36- by 96-in.: 11 sheets
3- by 9 by 14-in. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (4)
3- by 8- by 25-in. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (4)
*3- by 12- 25-in (add 2 for high elevation DX). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (10)
3- by 14- by 25-in . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (2)
*3- by 18- by 25-in (add 2 for high elevation DZ) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (10)
3- by 24- by 93-in . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (1)
3- by 36- by 96-in . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (6)
1670–269–1107 Parachute, cargo, 100-ft., G-11A. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
1670-052–1548 Parachute, cargo extraction, 15-ft (reefed with
260-in reefing line) (C-141 aircraft require
a 120-ft extraction line and an 85-in pendulum line.) .................................. 1
Platform, airdrop, modular, dual-rail system, 8-ft.:
1670–893–1631 Clevis, load tiedown . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 28
1670–893–1625 Rail, platform side, 8-ft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
5320–893–1632 Rivet, blind-drive type, 4-in. dia. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 32
NSN Plywood:
%- by 36- by 96-in. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
%- by 48- by 96-in (load spreaders). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2
1670–799–8494 Release, cargo parachute, 5,000-lb capacity .............................................. 2
Sling, cargo, A/D: (3-loop slings may be substituted for 2-loop
slings in accordance with TM 10–500/TO 13C7–1–5.)
1670–753–3788 3-ft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4
1670–753–3790 9-ft (2-loop). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ............... 2
1670–753–3792 12-ft (2-loop). . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .............. 5
1670–753–3794 20-ft (2-loop) (riser extensions) ........................................................ 2
1670–473–5115 Static Line, cargo parachute, breakaway type w/release knife and clevis ................ 2
1670–738–5879 Strap, connector, 60-in. . . . . . . . . . . . . . . . . . . . . . . . . . . . ....................................... 1
1670–998–01.16 Strap, parachute release, wifastener and release knife................................... 1
5340–181–1383 Strap, platform retainer (use with C-130 aircraft only) . . . . . . . . . . . . . . . . . . . . .............. 1
1670–368–7486 Strap, webbing, nylon, 60-in. (shear strap) (use with C-130 aircraft only)............... 1
7510–266–5016 Tape, adhesive, 2-in . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required
1670–937–0271 **Tiedown Assembly, 15-ft (Dacron) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 30
NSN Web, adapter (required w/120-ft extraction line, see TM 10–500/TO 13C7–1–5) .......... 1.
8035–268–2411 Webbing, cotton, 80-lb . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required
8305–263–3591 Webbing, nylon, type VIII (parachute restraint strap) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6 yd
8305–082–5752 Webbing, nylon, tubular, 4-in . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . As required
*When rigged for drop on drop zone with ground elevation between 6,000 and 10,000 feet, additional honeycomb is required.
**When this item is not available, the following items are required as replacements:
3990-360-0248
1670-360-0340
1670-360-05:40
Binder, load . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...------------
Fastener, strap, cargo tiedown, quick-fit . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Strap, tiedown, 15-ft. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ...-------------
14
FM 10-536/TO I 3C7-I 6-81
Table J-I. Equipment Required
Fr-<l¢~rulStock Nu. Item Quantity
8040-273-87131377-958-10481670-090-53548305-242-35934020—240—2l461670-360-03288135-664-69581670-2l7-2421l670-783-5988l670—799—85961670-753-3928
1670-269-1 1071670-052-I548
1670-893-16311670-893-16255320-893-1632N SN
1670-799-8494
1670-753-3788l670—753—3790l670—753—37921670-753-37941670-473-5115l670—738-58791670-998-01165340-l8l-13831670-368-74867510-266-5016l670—937—027lPJSN8035-268-24118305-263-35918305—082—5752
Adhesive, paste, 1-gal . . . . . . . . . . . . . . . . . . ..Cartrid re, time-delay, 20-sec . . . . . . . . . . . . ..
ssembly, suspension, large . . . . . ..L
Clevis A
Card, nylon, type lll, 550-lb. . . . . . . . . . . ..Cover, clevis, large . . . . . . . . . . . . . . . . . . . . . ..Cushioning material, packaging, cellulose wadding . . . . ..
Cloth, cotton duck, 60-in . . . . . . . . . . . . . . . . ..
sLink A.sembly, connector, removeable (For C-141 aircraLink Assembly, single, type lV (Add l for C-141 aircraLoad Coupler, 8-spool . . . . . . . . . . . . . . . . . . ..‘Pad, energy dissipating, honeycomb, 3- by 36- by 96-in
3- by 9- by 14-in . . . . . . . . . . . . . . . . . . . . . . ..3- by 8- by 25-in . . . . . . . . . . . . . . . . . . . . . . ..
*3- by 12- 25-in (add 2 for high elevation DX) . . . . . . . ..3- by l4- by 25-in . . . . . . . . . . . . . . . . . . . . ..
‘3- by 18- by 25-in (add 2 for high elevation DZ)3- by 24- by 93-in . . . . . . . . . . . . . . . . . . . . ..
3- by 36- by 96-in . . . . . . . . . . . . . . . . . . . . . . ..Parachute, cargo, 100-ft., G—llA . . . . . . . ..Parachute, cargo extraction, 15-ft (reefed with
260-in reefing line) (C-141 aircraft requirea 120-ft extraction line and an 85-in pendulum line.) .
PlatformIsClev1.,
%- by‘%- by
36- by 96-in .................... ..48- by 96-in (load spreaders).....
, airdrop, modular, dual-rail system, 8-ft.:load tiedown . . . . . . . . . . . . . . . . . . ..
Rail, platform side, 8-ft . . . . . . . . . . . . . . ..Rivet, blind-drive type, V4-in. dia . . . . . ..
Plywood:
Release, cargo parachute, 5,000-lb capacity . . . . . . . . . . . ..Sling, cargo, A/D: (3-loop slings may be substituted for
slings in accordance with TM 10-500/T0 13C7-1-5.)3-ft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .9-ft (2-loop) . . . . . . . . . . . . . . . . . . . . . . . . . . . ..l2-ft (2-loop) . . . . . . . . . . . . . . . . . . . . . . . . . . . .
Static Line, cargo parachute, breakaway type w/release20-ft (2-loop) (riser extensions) . . . . . . . . .
Strap, connecto 60-in . . . . . . . . . . . . . . . . . . ..Strap, parachute release, w/fastener and release knife..Strap, platform retainer (use with C-130 aircraft only).Strap, webbing, nylon, 60-in. (shear strap) (use with C-Tape, adhesive, 2-in . . . . . . . . . . . . . . . . . . . . ..“'l‘iedown Assembly, l5-ft (Dacron) . . . . ..Web, adapter (required w/120-ft extraction line, see TMWebbing, cotton, 80-lb . . . . . . . . . . . . . . . . . . ..Webbing, nylon, type Vlll (parachute restraint strap) .Webbing, nylon, tubular, '/&~in . . . . . . . . . . ..
ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . .ft) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
2-loop
knife and clevis
“ted Lit}-{Ari liiiiyi I I I II ........ ..
'ioL5b'oi'T'<5' iE;ciLiLisi' I I I I I I I I II
As required25
3 ydAs required
2As required
211
ll sheets(4)(4)
(lo)(2)
(10)(l)(6)
2
1
282
32
222
u-Ii-u-tOl\'iIUINiLl
As required30
1As required
6 ydAs required
‘When rigged for drop on drop zone with ground elevation between 6,000 and l0,000 feet. additional honeycomb is required.
"When thin item in not available. the following items are required as replacements:
3990-360-0248 liimler, loud . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..l670—360-0340 Flatt-ner, strap, cargo tieiluwn, quick-flt.T670-360-0540 Strap, tit-down, l5-ft . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ..
14
FM 10–536/TO 13C7–1 6–81
APPENDIX
REFERENCES
AFM 71–4/TM 38–250 Packaging and Handling of Dangerous Materials for Transporta
tion by Military Aircraft
TM 9–2320–213–10 Operator's Manual: Truck, Platform Utility, A-Ton, 4 × 4, M274
(2320–049–4804); M274A1 (2320–064–6363); M274A2 (2320–0.74–
1167); M274A3 (2320–782–5792);M274A4 (2320–782–5793)
TM 10–500/TO 13C7–1–5 Airdrop of Supplies and Equipment: General Information for Rig
ging Airdrop Platforms
TM 10–500–53/TO 13C7–18–41 Airdrop of Supplies and Equipment: Rigging Ammunition for Low
and High Velocity Airdrop
TM 10–1670–208–23/ Organizational and DS Maintenance Manual Including Repair
TO 13C3–4–12 Parts and Special Tools List for Platforms, Airdrop: Type II
and III Modular, 6,000-Pound Load (FSN 1670–260–0442), and
Combat-Expendable
TM 55–450–15 Air Movement of Troops and Equipment (Administrative)
By Order of the Secretary of the Army:
CREIGHTON W. ABRAMS
General, United States Army
Official: Chief of Staff
VERNE L. BOWERS
Major General, United States Army
The Adjutant General
Distribution:
Active Army, ARNG, USAR: To be distributed in accordance with DA Form 12–34, Section III,
requirements for Airdrop of Supplies and Equipment.
15
FM I 0-536/TO l3C7—I 6-81
APPENDIX
REFERENCES
AFM 71—4lTM 38—250 Packaging and Handling of Dangerous Materials for Transporta-tion by Military Aircraft
TM 9—2320—2l3—10 Operator’s Manual: Truck, Platform Utility, 1/é-Ton, 4 x 4, M274(2320-049-4804); M274A1 (2320-064-6363); M274A2 (2320-074-1167); M274A3 (2320—782—5792);M274A4 (2320—782—5793)
TM 10-500/TO 13C7—1—5 Airdrop of Supplies and Equipment: General Information for Rig-ging Airdrop Platforms
TM 10—500—53/TO 1307-18-41 Airdrop of Supplies and Equipment: Rigging Ammunition for Lowand High Velocity Airdrop
TM 10—1670-208—23/ Organizational and DS Maintenance Manual Including RepairTO 13C3—4—l2 Parts and Special Tools List for Platforms, Airdrop: Type II
and III Modular, 6,000-Pound Load (FSN 1670—260—0442), andCombat-Expendable
TM 55—450—15 Air Movement of Troops and Equipment (Administrative)By Order of the Secretary of the Army:
CREIGHTON W. ABRAMSGeneral, United States Army
Official: Chief of StaffVERNE L. BOWERSMajor General, United States ArmyThe Adjutant General
Distribution: -Active Army, ARNG, USAR: To be distributed in accordance with DA Form 12-34, Section III,
requirements for Airdrop of Supplies and Equipment.
I5
Digitized by GOOSIQ