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

I imggRoiQ‘-E so?2&1QWLE zkli

#1(piOi

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

[ON l\'J>—I

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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.

Pain

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Digitized by GOOSIQ

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

’/ -'1‘ wit iii!‘-" Elli--<i~--- .. . R.-. = -'-""~t" ‘ ‘RD’ _.4:.a 1. __, __ _,___,;_'~' -— - CU .;__,

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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