NASA Saturn S-1 Stage, Saturn SA-1 Handling, Transporting And Erection Instructions

HANDLING,

TRANSPORTING

AND

ERECTION

SATURN

INSTRUCTIONS

S-l

STAGE,

SA-1

,

J

:

....

GEORGE

."

C.

MARSHALL

SPACE

HTTP://HEROICRELICS.ORG

HUNTSVILLE

FLIGHT

ALABAMA

CENTER

TITLE

Handling, T

Erect

ion

ranspor ing,

Inst

ructions, Sat urn S

Stage

~

SA

=1

And

T

ABLE

=1

OF CONTENTS

GEORGE

MARSHALL

SPACE FLIGHT

PROCEDURE DATE PAGE

1 1

OF

c.

CENTER

147

Paragraph LIST

INTRODUCTION

10

OF

CHAPTER

PREPARING

ILLUSTRATIONS

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Installing

and

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ECTI.NG

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Removing

T

hrus t Ring

REMOVING

Bumper

Two

Cable Asse mblies (J=1 Procedu BOOSTER

Transpor t

Booster

BOOSTER

Assembly (D=

re

Rear Ring Sec

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er

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302

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Trans

303 304

Installation Removing

and

CHAPTER

10

PREPARING

1

01

Preparing 102 103

Positioning

Insta

(J

ing

Booster for

Booster from Towe

porter

Bumper

Two Cable

II

TRANSPORTATION,

BOOSTER

Servi ce St ruct

Tran

lli

ng

Beam

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(D=1

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35

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47

47 47 47

EORGE C.

PROCEDURE

MARSHALL

EP=141

SPACE

PAGE

FLIGHT

CENTER

OF

2 1

47

TABLE

OF

CONTEN

TS

(Con

o)

Paragraph Page 104 105 Removal

:2

2

,2

30 40

4

4~2

Remova

0

EREC

TING

01

Posit

2

Removing

0

REMOVING REMOVING

RING DET

.1

Removing

front Trans porter

Preservi

l Procedure Forward Ri

Procedure Rear Ring Secti

BOO STER

ioning

Booster

BOOSTER

RING

AILS Forwa

ng

Forward and Rear Ring Deta

I)

0 0 0 0 0 0 0 0 0 0 0 0 8 0 0 0

Transport er and A

from Transpor t

FROM

LAUNCH

SECTIONS

AND ATT

WITH

ACHING

rd and Rear Ring Sect i ons w

I)

0 0

(.)

0 0 0 0 0 0 0 0 0 0 0 0

ng

Sectio

tta

er

PEDESTAL

ns (J=AF=12

ons (J=AF=1

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ching Cab

and

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oning on Launch

FIN I IDENTIFICATION

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0 0

82

CHAPTER III

GENERAL

INSTRUCTIO

NS

FOR THE

8=1

T

RANSPORTER 0000

0000

000

0000

00

83

LIST

OF

ILLUSTRATIONS

PAGE

OF

EP-141 3 147

Figure

1.

2"

3. 40

Positioning

Removing Doors and

Installing Bumpers Positioning

Equipment at

Horizontal

5. Removal of Rear Ring Sec

6.

7.

8.

9Q Erect

100

11

• Connect

2.

1

Rear Ring Sect Removal

of

Identification

ion

Attaching

ion Attaching

Rear Ri

of

Beam

Ins t

Erection

ng Fin

allation

ing Aft Cable Assembly

Forward Support Clamps

Static

Plates

oooe

and Cable

Pla

tform and

ti

ons

Section

Line

and Out

Beam

and Cable Assemblies 0' 0000'

o.

0 0 • 0 0 • 0 • 0 0 0 0

Title

Test

Tower 0000

o o o

oooo

o

ooocooooooo

Assemblies

0.000 •• 0

Personnel

(J=AF=12004-2~0

Poin

ts

•••

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at Outrigger

rigger

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Page

8

12 13

18 19

21

27

13 0

14. Boost

15. 16

0

17.

18.

19.

20.

21.

22. 23

. Forward Ring Section Removal

24 .

Lifting

Boost

Positioning Boost

Preparing

Boost

er

Stabilization

er

in

er

Vert

Serv

ice Structure

off

Transporter

ical

Position

er

on

Preparatory

Positioning Equipment at Preparing Installa

ti

Boost on

of

er

Beam

for

Erection 0 0 •• • •• 0 • •• 0

Weldmen Removing Forward Ring Sect Forward Ring

Attaching Aft

Section Attaching

and Forward

0 •• 0 • •

0000000

t o

Lifting

••••

000

..• 0 .•.•

0. 0 •• •• •• 0. 0. 0.0 0.· •

Support Bracket s 0.00 . 0

for

Erection

Firing Sit e 0

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•••. 000. 0

•.

t and Forward

ions

(J=AF-12004~3~0) .~

Poin

t s

Procedures

Sling

Assemblies .000

•••

Sling

0 .

.0 .0

.... 00. 0 ••

••••

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off

Transporter

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00

48 49

52 53 55

57 65

GEORGE

C.

PROCEDURE

MARSHALL SPACE FLIGHT CENTER

EP

,·,1

41

PAGE

4

OF

147

Figure

Connec 26 27 28

0

. .

L

8-1

Removing

29. Booster-

30.

31 0 Rear Ri ng Support Cl

P

ti

ng

ifti

ng Boost

Stage

Af t Cable Assembly and

Pedestal

to-

ositioning

Erect

ing

er

off

Cen'ter-or-Gravi

0

III

0 .

000

Launch

Boost

LIST OF

Beam Transpor

••

0.0

ILLUSTRATIONS

Ti t

le

and Forward

er

0

•• 0 ••••

ty Di agram

Positioni

Q 0 • • " 0 • • 0 e • • 0 II 0 . 0 0 0 .

(Con

Sling Assemblies

• 0 • • 0

•••••• ng

o)

• 0 • • 0 • • Booster

....

Pedestal Orientation Diagram..

er

on

Support A

amp

s Q. 0 0 • 0 0 • ·0 u •

rms

and Holddown

••

0

••

0 •

III

0 • 0

••

0 •

•••••

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III

•••

0 • • • • • • 81

Page

• • • 69

••

• • 71

00

. 75

..

68

77 78

ER

Thi s

manual provide

erecting

and

chapt

II

ta

ers 0 Chapter

con

tai

ns

i ns

opera

ins

t i ng

Chapter I consi st s

sections,

va

tion

of

t he

Chapter

rear

pedes t

position of tooling rear ring sect i ons t o t he

II

ring

sections, posi t i oning and

al,

and

A complet e

T

ransporter

and Int

roducti

Equipmen

t ower and

por

t e

r, towing tractor

ranspor

t handling

and i ncluding a

t e

at t he Cape Canaveral f

tat i on ring pl a t forms .

of

t he Boost er d

s t he necessary in

t he Saturn S

=I

Booste r

I cont ai ns instructi

t ruct i ons at t he

ins

t ructions

of

st ep=by=st ep procedures

i ng and erecting the

, pos

iti

oning

cons i st s

preserva

man

ual

of t i on con

taini

st ep=by=st ep of tool

on i s inserted i n

ssential

t o proper ha

, gant

urin

INTRODU

~

ef

Cape Canaveral

for

t he Sat

t he Boost

Booster aft

erecting 'the Boost

i ng

ng ge

separa

neral inst

t e Tab l e

thi

s manual

ndling of

irin

g site i

ry

cra

ne, mobil

Sp

eci

al

g r e

mov

al

CTI

ON

st r uct i ons fectivity SA ons at t he

f i ri

urn

S=I T

ransporter

Boost

er

on t he t

er

i n t he

er sta

procedures

for shipp ing.

ructions

of

Con

t ent s ,

as

Chap

t he Boost

nclu

des t he fol

e c

rane, fork

hardware

and

erection.

assures

for transporting,

=1

and

is divided int o t

static tes

ng sit e.

t tower.

Chapter

.

for

r e

moving

t he

static test t ower ,

ransp

or t

er,

and

t i c test

for

firing

removi ng t he

er

from t he

t he Sat

List of

t er

III

.

er

at t he

lowing: trans l i f t , safe

horizontal

and

handling

Chapter

III

rear ring reassembly

.

forward

launch

urn

S=I

Ill

ustrati

static tes

efficient

hree

con=

pres

and

ons,

t = and

,

er -

Divi

T

his

sions

publ

0

i cat i

on

i s a

com

bin

ed

effort

of

t he M=

LOD, M=T

EST,

and M-

F&AE

PROCEDURE

PAGE

OF

CHAPTER

I

1.

PREPARING

1.1

1

Pos

1.1.

1.

.2

Installing

and

1.

1.2.2

TRANSPORTATION,

BOOSTER

iti

oning

1 Pos

r i ght

FOR

Transporter

iti

on transporter

angle

bridging

1.2

area

Lock t

around

(See

figure 1 for

ransporter

Bumper

Two

Cable Assemblies

2.1

Move tractor

boos t

Using

er

fork

personnel

(D-10426438) , t (J-10424771) . (See

HANDLING,

TEST T

ERECTION

0

(J=AF=12004

on nort h

t o

deflector pit

at a di stance which

t he t

ransporter

the rel ative

brakes

and chock wheels .

Assembly (D-10426438).

(J-10424771~

and t

ow

bar

.

lift,

raise transpor

to a height necessary

wo

bumpers (D-10426434

figure 2.)

AND OWER

)o

for

clear

ERECTION

side

of

and

aline

will

provi de

t he mobile

positions

Two

of the

tat

ion

for att

AT

STATIC

sta

tic tes

wit h

sufficien

of

Bumpers

forward

ring

aching

),

and

t t ower at a

deflector pit

t working

crane

and

fork

t he equipment. )

(D-1042643~

end

of

t he

pla

t form and bumper assembly

cable

assemblies

)

lift

!

.

1.

2.1 .1

1.

2. 1. 2

1.201

.3

1.201.4

Remove attached adapter

doors

t o int

~o

gain assembly attac I=beams

Remove att fairing for

shown

NOTE: and st boost

No.3,

aching

t o second stage adapt

bumper

in

All

figure

assemblies

doors

oredo Th

er

has been

figure 2 for Install

bump

wi t h detai l Install

B

~

bumpers (D-10426434)

figure

3.

(D-10411708) and pl at

er

st age

access

hing

4,

fairing t o bumper and

poi

nt s . Attaching

5,

6,

and 7.

hardware t hat

er

es

and second st

secures int

at at

and forward sli ng

2. and a

i s hardwar e wi

erec

list of attaching

tta

t ed

ching

in

hardware t o be packaged

ll

be

t he test t ower. See

hardware.

er assembly (D-10426438)

A,

figure

3. in

accordance

(D-10411753)

age

forward

poin

t s

ers

sling

are

tage

taching poi nt s

assemblies

installed aft

in

accordance

wi

t h

at

as

er the

detail

PROCEDURE

EP

=141

PAGE

OF

8 1

47

FIG.I POSITIONING EQUIPMENT

AT

STATIC

TEST

TOWER

-----

--,--

--

---------------

---

---_._-._----------

...

_-----

[I

--

L

---------

-------

--------

"~?,-.-

1%2'\

----

E§

--

---

7\

-

__

U

(C-10411722)

(I)

NUT J_

NAS-1022

(I)

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REQ'O

~

REQ'O I

U

D

~------SCREW

/ 7513-1032 -12A

i

~

S>

~

I /

I)

~

I

l1

i ' 1

Q '

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I I

.r-PLATE

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(0-10411753)

(~~~~1I723)

~

REQ'O

'1

~

I I

~

I

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r-~~J-1022-C8

~

,

~

,,1,

.....

~

I-----SCREW

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{f)-~OE4J!621l

(I)

REQ'O

LOCK

PLATE

(C-10411724)

(Il

REQ'O

AN501AC416-8

(I)

REQ

' O

(0-10411708)

7513

-1032-12A

(10)

REQ' 0

-0

DETAIL

A

FIG.2 REMOVING

DOORS

AND PLATES

REF.

OWG

10411701

.

GEORGE PROCEDURE

C.

EP=141

MARSHALL

SPACE

PAGE

10 147

FLIGHT

OF

CENTER

ill

R

BUMPER

UNSCREW

SEATED

BRACKET.

AGAINST

[~

.

~-jJ~ ,-~:~ =-i-~.:-

~~

IS

BOTH

SECURED

BOLTS

BOLT

BUMPER

BY

BOLT

AN12-14,

(AN8-6A)UNTIL

HOLDING

(D~0426438)(REF)

EACH

SHROUD

IS

TO

_-~-=~1r'

---Q--

~

"

BOLT

AN8-6A

TANI2-14

WASHER

NOTE:

WHENEVER

BOLTS,WASHER,AND

TO

BE

DISCARDED

NOTE: WIPE OFF

CLEAN RAGS

WITH

ASSEMBLIES

TOROUE LUBRICATE BEFORE

2-

22-WASHER NASI43-16C,RFF.

2-

HEAD

INSTALLATION

CABLE

ASSY

BOLT

NAS156-68,

WASHER

NAS~3-I.'R?

CABLE

.

ALL

OF

BOLT

THREADS,

(J-1042477il,

NUTS

SHANK

REF

AT

(NAS

fi

ASSEMBLY

SHALL

LUBRICANT FROM BOOSTER PARTS

TIME

156-68) OF

WITH

R

_

~

1042477

BY

INSTALLED,USED

OF

REMOVAL

TO

BOLT,

AND

MOLYKOTE

_

6000

EACH

TYPE INSTALL

PULL

IS

ATTACHED,NEW

HARDWARE

OF

SLING

INC

LBS(500FT

SIDE

OF

"G'.'

LUG

OF

IN

CABLE-

WASHERS

LINE

. LBS.).

OF

SEE

A-A

BOLT

AN14-14

WASHER

FIG

AN945-14

. 3 .

INSTALLING

2-NUT(A-10424915),

BUMPERS

AND

~

R

~

CABLE

ASSEMBLIES

1020105 Install

w

ith instructI

assemblie

cab l e

s toget

assemblie

s (J=10424771)

ons i n deta

her

t o prevent damage to boos

il

C~

f i g

ure

in acc

30 T

ordan

ie

tero

cabl

ce

e

1

1.

03

302

2

1

0

01

Posi t i on m abov e t he r e

mov

r e

Using m and p ring so t hat for

ti

ono (See f i

comple

WARNIN

(J=,10424771) i s ext,remel

washers

shank and si de

Gg

Cor

~

and nut s sha

thr

of t he

rect

eads

wash

el~

inst

allat

ion

y importa.nto New

ll

be used o

of t he bol t s (

s

(

NAS

143=16 and

of

cab

le

assemblies

Lubricatin

NAS

156=68) and ea eh

NAS14J=16C obtaining a torque va l ue of 600=inch pounds (500 foot po sh

10

6 Q

ti r e

al

of a 1 r e

obile

er

son

removal

te

t he

unds) f r

earin

uality

on of cord

obile

ar rin

crane~

nel

the

of

followi ng p

om

the

hea d

g of

the

attac

Control Divisio

the

cab

le assemblies (.T=1

the

tor

que val ues

cra

ne so t hat t he two

g" The

ar

ring section

raise and

on t,op

t he re

gur

pla e

tf o

4,,

of

t he boos

rm

ar

r i ng sec

) W

i s res

orkin

rocedure

hin

crane

pos

g f

of bol

t s i s

mandatory

g hardware du

n sha

ll insp

ect

0424771 ) , check and

of bolt

boom

crane

can n

s (

NAS156=68

hooks

ow

s o

ition

t he

hori ter just forward ting firmly tio

n with F

rom

t he horizont

in

in s g

ring

t he installa

are directly

be

maneuvered for

zontal

of

prop

III

identifica

al

bolt

s,

g t he

) and

t o preven't

erectiono

)0

pla

t form

the

rear

er

position

platform

=

~

1

.3.3

10

302

'~

.302

10

30203 Di

Using pla

t f

1 Connect ri ng

0

wi

th

F

in

.2

Lower 1ine and p

loosenin

fork

orm

and perso

(See f i g

5

~

scon

(S

ee

lift~

ure

crane hook

s o Connect choker

ut sli

deta

il

nect

g s

fi. gur e 6

ra

handling 'bra

III

iden

59

ght

A 0 )

tee et scre

0)

i se and p

nnel

as at 'the rear rlng separat,;i f i g

ure 40) Working from

c

omplete

wi

t h Fi n I II

10303

t he following proce

identif

01

Disconnect t ee re

ar

ri ng by removing

base

of

each t ee

ica

t iong

t i fica t,

detail

s ,

to

ion wit

A 0 )

work area and conne

line

ten

si on on

bracket fro

ws

and re

osition

nece

ssary on and t he t

tee attachment point

ransportation ring

dures

bracket

s at o four bol

bracket

cket s t o

rear

ring

sec t

h nuts and bolt s 0

ct

to

s t o

ring handling

crane

cable

s o (See figu

m outrigger Noo 5 by

moving conn ecting pino

t he t

ransportati

on each si de of

on the s o (See

p

latf orm

to remov

utri

e re

ggers

ar

ring sectio

4

No

o

and 6 from

t s and washers t hrough

to

t he ringo (See f i

ion

choker

brackets

re

ring

booster

~

n

gure 60)

GEORGE C. MARSHALL SPACE FLIGHT CENTER

PROCEDURE

EP

=141

PAGE

OF

12 147

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4.

POSITIONING

HORIZONTAL PLATFORM

AND

PERSONNEL

PROCEDURE

EP=141

FLIGHT

OF

13 147

.

CHOKER

CENTER

LINE

CHOKER

TYPICAL

LINE

\ I

~

;

)""-IJ-AF-12004-2-01

ASSEMBLY

HANDLING

IJ-I04244401

F.:OR

BRACKET

ALL

REAR

RING

RING SECTIONS

FIG

. 5 REMOVAL

AFT

VIEW LOOKING

OF

TRANSPORTER

FORWARD

REAR RING SECTIONS

GEORGE

PROCEDURE

C.

EP

MARSHALL

-141

SPACE FLIGHT CENTER

PAGE

OF

14 147

(J"AF-12004 -2"17)

SCREW

ROTATED

180·

) B(AF-12004-2"3)

,

~

C6~~ECTING

~

---

·TEE

BRACKET

D(AF"12004-2"2)

TYPICAL

FIG.6 REAR

DETAIL

AT

OUTRIG

RING

SECTION ATTACHING

A

GERS NO

.2.4.6

POINT

AND

S

8

1.303.2

Remove holes holes

t he 4!= of each on opposi

screws t o

di sco

l ocat

of

are rear r i and

nnectin

NO

TEg

or (A=AF=1

each ring

c

onn

ring

ng

at

locators

One 4!=

ect,ed~

each splic

sections o

inch

scr

ews

ring sectiony inser

te

si de

of

pull locato

g pos

inch

rs

(A=AF=1

iti

ono (See fi g

screw (J=AF=1

2004=2=14)

section; t

herefore,

one screw i s on t he

and one s cr ew i s

e j o

into

(A=AF=1

2004=2=14) rema

(J=AF=

12004=2=18) from

t t

hese

ring sections

2004=2=14) t o t he

ure 60)

2004=2-18) and one

are

loca

t ed

when

forward

on

t he aft

Screws

(J=AF=1200

in wit h t he

screws

in

, and t i ght en

in

t he end

t he

ring

sections

side

side of

of

t he

4~2~18)

ring

end

hole

t he

rear

1

.3.4

103.3.3 Dis

connect

ti

on from 6 by remov six

screws (J=AF=1

5 and 60)

1

0303

04

Co

nne.d tag

iden

t ifica

work

ing areao Use tag line

men

t 0 (See f i

10

3.3.5 Disconnect r

ion wit h F

t lines

10

30306 Using

p

Us

ing

fork

and

personne section wit h from t he t pro

cedur es g

10

3.4

.1

Con Fin

f i g

from mobile cra mob

er

sonnel

lif

t , raise

l t o a hei ght

Fin

ranspor

nect

IV

ure

rear

ring sectio rear rin in

g t

wo

g s barrel 2004=2=17) at

line

tio

to

r e

n and hoi st

gure 50

ing handling

in

III

i dent i f

ile

crane, lower

t o

the

gro

und 0

and posi t

as

nece

IV

i d

entification.

tation ring pla

ring

handling

identification

5. )

n with Fi n

ecti

ons at out ri nut s (J=AF=1

ar ring secti

off

of

t o cont

)

brackets icatio

ne hooks .

horizon

ion transporta

ssary

for

(See

tform, compl

bracke with

t s t o r ear

bolts

III

identific

ggers

No

. 4 and

2004=2=6) and

each

boost,er

end. (See

on w

ith Fin III

and lower i nt o

rol

swinging

from

rear

ring

figures

move

sec

n and remove choker

tal

pl at form and

t i

on

ring

removal

figure 4.)

ete

t he

pla

of

rear

Work

following

i ng

ring sectio

and

nut

s.

(See

a-

-

=

tform ring

n with

1

.3.4.2

1.3.4

Using mobil e to

work

03

Connect

ri

ng sect i on wit h F

t

ension

area

cho

on

crane wit

and con

ker

l i

crane

h t

wo

nect

nes

t o ring hand

in

IV

hooks,

t o choker

i d

enti

lower lineso

ling

bracke

fication and put

cables. (See figure 5.)

crane

t s on

hooks

rear

sligh

t

GEORGE C.

PROCEDURE

MARSHALL

EP=141

SPACE FLIGHT CENTER

PAGE

1

.3.4.4

OF

16 1

Disconnect

47

outrigger t

ee.

Remove

at out ri gger No. 8. (See

tee

No.7

two

bracket

from

by removing

bol

t s only from base

rear

ring

four

bolts

figure 6.)

section

from base

of

t ee

bracket

at

of

1

.3.4.5

10

304.6

1.3.

4.7

1.3.4.8

1.3.4.9

NOTEg The

t ee

bra

until

erection

forces

Disconnect

t

ion

by performing

in

paragraphs 1

Connect tag

wi

t h

Fin

Lower personnel and t

fork

lif

hoisting

Wi

t h

personnel lift rear of

t he bOOster and lower int o working

crane. Disconnect

ti

on

and remove choker

remaining t

wo

cket at outrigger

are

cables

obtained rear

ring

are

from t he t

section

the

.3.3

.2 and 1

line

to

lower end

rv

identification.

ransportation

t and

rear

clear ring

immediat e

section

positioned

ring

(See

section wit h

figure

ring

handling

5. )

bol

t s t hrough t he base

No

0 8

connect ed and

with

applicable

.3.3.3.

(See

free

t o

maintain a taut tag

Fin

brackets

lines

from mobile crane hooks.

will

remain

ower

and

Fin procedures

of

rear

figure

ring

area

preparatory

of

booster

IV

identification

from

of

t he

installed

slight lifting

gantry

IV

identifica-

cranes.

outlined

ring

section

5.)

platform wit h

t o

.

line,

free

area with mobile

rear

ring

sec-

1

.3.5

103.4.10 Using and

fork

lif

personnel t ee bracket s from out se

t screws and removing connecting

6. )

1.

3.4.

11

Lower transportati

t he ground with f ork lift.

Using fork lift, raise form and ring Working following

1.3. 5

1.

3.5

personnel

section wit h

t o a hei ght

Fin

from t he t ranspor t ation ring

.1

procedu

Connect

wi

th

figure

Fin

5.)

res

ring

II

:

.2 Using mobile crane wi

t o work

area

t , rai t o a

and

II

se transpor

height as

riggers

on ring

position

as

necessary Noo 6 and 7

pla

tform and pereonnel

transportation

neceSSary

identification.

platform

handling

bracket s t o

identification wit h

th two

hooks, lower crane hooks

and connect choker

tat

ion

(See

rear

bolts

lines.

ring

pins.

pla

and

disconnect

by

(See

tform

loosening

ring

for

removal

figure

4.)

, complet e t he

ring

and

nuts.

(See

section

figure

to

platof

rear

(See

5. )

T

CENTER

147

1.3.5.3

1.

3. 5

1.

3.5. 5 Disconnect r ear ring sect

Connect choker lines t o ring s

ension

t

04

Disconnect t ee out r i of

by

ecti

on

crane

ggers NOe

each t ee

bra

performing

wi t h F

t he app

in

cables.

brackets 2 and 3 by removing cke

t.

paragraphs 103.3.2 and 10303.

1.3.5.6

1.

3. 5.7

figure 8 for numbers

.)

Connect tag l i ne t o lower end

Fin

II

ide

Inser

t t

section wit

and

secure tee

bol

t s . (See

NO

TEg The t

bracke

t at out r i

t he er ection

for

ces

are obtaine

identification

ntifica

wo

barrel nut h Fi n I

brack

fig

wo bol

cables are connecte

t iono (See

identification at out r i

ur e 6

t s t hrough t he

gger

d from t he t ower and gant

ring handling bra

II identification

(See f i gu

from

rear ring sections at

re 5.)

four

(See f i

gure 6.)

ion wit h Fi n

licable

pro ced 30

of

Fin

of

ure

(See

Li nes and outrigger

rear ring

figure

s (J=AF=12004=2=6)

et

t o

rear ring

0) base

Noo 2 w

ill

r emai n d and

cket s on

and put

bol

II

identification

sligh

t s at

s outlined figure 70)

section wit h

5.

)

in

rear

ring

gger No. 2

section wit h t

of

t he t ee

installed unt

slight

lifting

ry

cranes

rear

t

base

in

(See

wo

il

o

1.

305.8 Lower pe fork lif t a

hois

t i ng

10

30509

Wi

t h pe lift rear ring sec of boos t crane

1.

3. 5010 Disconnect t

ion

10

3050

11

Using pe

rso bracke screws

1.

305.12

Low

er pe

wi

t h

ransporter ont o t he

t NO

TEg The aft end

hree

t

ring

No

o 2 and 8 at out

are sti

wo

of

t

sections stHl

rsonn

el and trans

nd cle

rear

rso

nne l positioned t o maintain

ar

ring sec

t i on with Fin

er

and lower i nt o worki

imme

t i

portat

dia

t e

on

free

ion

ring

area

preparatory

of

boos tero

II

i d

ng

area wit h mobile

0 (See figur e 50)

ring handling bracket

s from

and remove choker lines from mobi

fork

lif

t~

raise t

nnel

t o a hei ght

t s from out ri ggers

and r e

fork

points

moving conn

rsonnel

l i ft and

~

and t

t ee

brackets Noo

section with Fin I identifica

riggers

ll

connect ed t o t

t he four bolt

install

ransportati

as

necessary

Noo 3 and 4 by

ectin

g pins o (See

ransportation ring

clear

the

area

deflector pit

of

t he boost

er 1,

No

o 2 and 8,

heir

out

rigg

s t hrough t

ed o Tee

heir bracket Noo 1

on r i

and di sconnect t

preparatory

bridgingo

is 2 and 8 t i on o Tee

er beams and have base

pla

t form wit h

t o

a taut t ag l i

enti

fication

rear

l e

crane

ng

ring sec

hooks

pla

tform

loosening set

figure 60)

pla

t form

to

now

resting

of

t he bracke

respe

ctively

t o t he ri

is

ne,

free

·=

and

ee

moving

on rear

t s

y

ng

inta

o

ct

GEORGE

PROCEDURE

C.

EP

MARSHALL

~141

SPACE FLIGHT CENTER

PAGE OF

18 1

47

TEE BRACKET

(D-AF-12004-2-2)

(J-AF-12004-2-8)

SCREW

-~

,

WASHER

(J-AF-12004-2-7)

NOTE: OUTRIGGER 8 CONNECTING

PIN OMITTED

FOR

CLARITY

.

SET

SCREW...::...J

(J-AF-12004-2-10l

l-

lrl1!

~

FIG. 7. REMOVAL

OF

REAR

RING

SECTION

AT

OUTRIGGER NO.2

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PAGE

OF

19 147

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FI

G.

8 I

DE

NTIFICATION

OF

FIN LINE AND

OUT

RiGGER

NUMBERS

GEORGE C.

PROCEDURE

MARSHALL

EP

=141

SPACE FLIGHT CENTER

PAGE 2 OF 1

0

47

20

10306

10307

10

308

ERECTING

2

01

Pos 2

0101

and wil l not be

connec t ed and th

e t

ower

and gant

t o be t

adap t

Clean mating

wi

t h

dry~cleaning

owed

er

is directl

surfaces

solven

accordance wit h paragraph 302

MIL-P=11

cation

Immerse attaching preserv

Move ring

or

BOOSTER

iti

oning T

Using gant pla

6 and

MIL

-C=1

ati

ve

details

equivalen

o

ransporter

ry

t form

of

apply

6173, t o mat

hardware

lubricating oil ,

t o adequat e st orage

t , and cover w

and A

crane

static

~

t es t t

disconnected unt

slight

t o a

lifting

ry

crane 0

position

y under t he t

of

P-3

rear

t~

corrosion

ring

Federal

01

ing

surfaces

for

of

rear

Military

ith

a t

arpaulin

tta

ching Erect

place erection

ower

o

il

erection

forces

are

Transporter

where t he second

ower

crane

cables

obtained

is

now

stage

o

segment s and tee bracke t s

Specification

Military

prevent

ive,

p-s=66

1,

Specification

Military

Specifi-

o

ring

segment s

Specification

area,

place

in

P-9

MIL-L

on

cross ties,

0

ion

beam

Cab1es

(J~10427055)

g

on

load

are

from

ready

in

=6440

10

2 Using t

2

0

t he l oad t he 100=t st de

20103 Place

cra

2

0104 Using t owing t

boost

ower

pla on

op

(C=10423817) , and screw

tail

Bo)

defl

ne

o

er

as

deflector pit

t

ractor

portero

it from l

et out

in

Position towing tractor

i n a dl

def

lect

sufficient slack of transporter , and pos bridging

as

crane, t form and connect sister

lower 1

00=ton

block and

sister

the

sister

(MS3530

ect

or pit

ractor,

close

bridgingo After

horizontal

bridging

as

poss

over

position

ibl

e t o and

pos

ition

t he t locking

, disconnect

on

rect line with transporter

or pito Secure towi

in

ng tractor with chock

winch

ition transporter

follows

Using t owing onto deflect second d

irectly under t

g

stage

t

ractor

or pit

bridging

adapter i s

he tower

winch,

block

erection

hook wit h 1=11

1) 0 (See

deflector pit

ransporter in

alinement wit h t he

the

t he south

at a

and

sister

beam

(J=10427055)

pin (C=1

figure

using

carrying

drawbar it

from

side

on the

of

convenient

0423816),

gant

t he towi

deflector

dis

blocks,

cable, attach

on

carefully t o a

24 inches

cable

deflector pit

pull transporter

position

short of

where t he

being

t o

crane 0 (See fi gure 10)

hook t o

9,

ry

t he

trans-

t ance. fron

to

ng

t

NO

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hori zon

Use

tal

gant

ry

crane t o hold t

position.

ransporter

drawbar

in

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~424

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PAGE

21 147

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OF

THE

--

-

---------------

-----.

BOOSTER

,

TOWER

CRANE CABLES SHALL

SO

THAT THE SISTER

8

HOOK

GEORGE

PROCEDURE

C.

MARSHALL SPACE FLIGHT CENTER

EP

=141

PAGE

22

OF

"1

47

20105

2010402 When tran

fig

ure

1,

Position

c

ran

e hook.

2010403

Disconnect t owing remove chocks from t owing remove towi

Due to ot prepa'rations dures

2

0"10501

her

the

high

hardwar

mus

t be

Pos

shear e, at'ta for

adhered

ition mobi personnel booster.

2

010502 Lower

100=ton

point in

l

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03

assemb

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ra

lies

ct

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ning a slight

ise the

against bum

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sporter i s

lock

and

lock

tran

drawbar

positioned

sporter

tract

ng t

ractor

l oads imposed

chi

ng

the

erecting the

to

closelyz

l e

crane

on south

(See

side

figure 100

sister

front of

booster

erection beamo

(J=1

0424771 ) from second

to

erection

per

beam

assemblies

or

from t

cables

booster.

with

of

)

hook

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beam

o (See

tension

until

on

bridging

brakes

rigidly

winch

and chock and remove

cable

tractor,

est

tower

on

attaching

is a critical

The

horizontal deflector

block where

and

personnel

figure

wind

following

pit

erection

100)

stage

as

from area

transporter,

up

cable,

o

bolts

part

platform

in

can

Untie

adapter

figure 30)

on

the

cable

erection

assemblies,

beam

(D-10426434). (See

shown

all

wheels.

gantry

and

of

the

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beam

to

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and

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figure

in

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Ng

The

contact bum

per negative ang l e between horizontal res

ul t in

centerl

damage stage adapter darnage9 maintain a visi sister

(See f i

hook gure 9 for

block, bumper

504

Mov

e mobile

t o nor t h

side

line with outriggerso

.5

Using m o

utrigger Noo 5

assembly

tioning

ca

F

in

ble

Line

obUe

to

pla

tform and

assemblyo

s and out

100=ton si

ster

hook

assembly (D-10426438)

the

t ower

ine

of the boostero This would

t o

the

bumper assembly and

ringo

block

assembly,

crane,

of

crane,

at

outrigger

) (See

To

insure

ble

space between

and t he bumper assembly

t he

desired

and tower

horizontal

deflector

position

Fin

pit adjacent

(See

figure

horizontal

Line

III

Noo 50

figure

11

figure 8 for

rigger

numberso )

block

crane

as

cables

must

this

not

creates

the

against this type

the 100

at

all

relative

platform,

crane

position

cables.)

and

personnel

to

booster

100) platform

and

(See

attach

figure

aft

10

for

connecting

identification

and

second

of

=to

times

of

near

cable

aft

a

the

n

o

the

in

posi=

of

STATIC TEST

TOWER

PROCEDURE

EP-141

PAGE

23

STATIC TEST TOWER

FT

ASSEMBLY

OF

CABLE

147

TOWING TRACTOR

(M-

26)

DEFLECTOR

PIT BRI DGING

TRANSPORTER

DEFLECTOR

HORIZONTAL PLATFORM

MOBILE

HORIZONTAL PLATFORM

SATURN BOOSTER

TRANSPORTER

DEFLECTOR PIT BRIDGING

CRANE

FIG.

STEP I

ATTACHING

10

ATTACHING ERECTION BEAM AND CABLE ASSEMBLIES

CABLE

ASSEMBLIES

TO

ERECTION

BEAM

ATTACHING

AFT

CABLE ASSEMBLY

STEP

2

TO

OUTRIGGER

NO.5

~

GANTRY BLOCK

CRANE

ASSEMBLY

- - - -

---

-

---

CONNECTING

---

PIN~

~

--------AFT

.

~

...

-----

CABLE

ASSEMBLY

(0-10423292)

COTTER

CONNECTING

(0-10424657)

NUT

OUTRIGGER-------.y-

LINK

(DOG

BONE)

~

.

~

FIG. II. CONNECTING

@;

AFT

~

CABLE ASSEMBLY

CONNECTING

A

PROCEDURE

EP-141

PAGE

26 147

OF

201.5

2.1.5

2

.1.

508 Using

2.105

2.1.50

.6 Lower gan t

assembly

NOTE:

lifting

ry

gant

forces

t he boos t

ry

t o

Prior

forces cranes should not,

er

ware yet t o be r e

07

Remove

aft se

set Connecting

figure

ring of

.9

Remove two

bracke

large

t screws

screw t hrough

60

)

fork

pla

lif

t form and

t he boos t

rema

t at out ri

10 Disconnect t ee

loosening

(See

figure

set

crane

block

to

as

Bal~lok

er

block

assembly

assembly. (See f

t he

following

must be

obtained

t o support t he

however, be

t hi s would

moved

in

t ee

base

remains

t ,

raise

cause

from t he

and

bracke

of

t he t ee

in

out

and

position

personnel

at outriggers ini

ng bol

ggers

brackets

t s t

No

2 and 8.,

o

from outriggers

and at

igure 100)

proceduresy substantial

from t he tower and

booster

great

.

enough t o binding forward

loosen

t at out

rigg

t he

rigger

is

t o remain

er Noo

t he transportation

as

necessary

No.2

hro

ugh b

and 8

ase

(See f

screws and removing connecting

60

)

tach aft

The

lifting

of

t he

and

rear

forward

No.1.

10

(See

on

each

of

rear

of

each tee

igure 60)

No

2 and 8 by

o

lif hard-

fixed

pins.

cable

t

rings

and

The

.

side

ring

o

.

NOTE: lower

porter.

2.1

05.11 At

tach two

NOTE~

equal,

201.5.12

Place

Lower

201.5.

13

fork Remove

lif

porter

2.1.5.14

Clean mat brackets wit h tion

p=s=661,

Military

corrosion

MIL=C=

01.5.1 5 Immerse at

2

bracke Specification

Boost

section

approximately

tee personnel

er retai

tag

Tag

lines

bracke

t and cle

of

rear

lines

t o be

t s on t

and t

ar

ns

ring

t o

75

ransportati

immediat e

support clamps from

. (See

ing

figure

surfaces

dry

cleaning

in

accordance

12

of

Specification

preventive,

161

73,

taching

t s'

in

t o mati

P-9

preservative

MIL

Military

ng

hardware

=L=644.

the

horizontal remains attached

each

outrigger

1=i

nch diamet

feet

long

o

ransportation

on

area

forward

0) support

clamps and

solvent,

with

paragraph

MIL

=P-116 and

Specification

surfaces

for

0

support

lubricating

position

Noo 3 and 70

er

hemp

ring ring near

ring

pla rear

and

Federal

apply

clamps and

oil,

and

t o t

rans=

pla

rope,

tformo

or

tform wit h

ring

o

trans=

tee

Specifica=

3.2.1

of

P=3

tee

Military

GEORGE C.

_-

________ . (J-AF-12004-3-0)

FORWARD

RING

HOLDDOWN

(J-AF-12004

FORWARD

ROLLER -

- 4-36)

--1

V

=

VIEW

LOOKING

DETAIL A

AFT

-HOLOOOWN BRACKET

(J-AF-12004-4-31l

Y/~

CAP

~

(J-

1----

SCREW

i-II

NC 8 REa'o

8

AF-12004-4-32)

TRANSPORTER

FIG.12

FORWARD

SUPPORT CLAMPS

GEORGE C. MARS

PROCEDURE

202

Removing Boost

L SPACE

PAGE

201

0

FLIGHT

28

5016

er

CENTER

OF

147

Move

storage c

ov

from

support clamps and t ee

area,

er

with a tarpaulin

Transporter

place

and

on

Positioning

bra

cross ties,

0

cket s t o adequat e

or equivalent, and

on

Tow

er Th

rus

t Ringo

2.201

Have ment of figure

bar

20

20102

2020103 Using t

202

02 With tower

booster ring

20203

Using towing

Clean and

ou

tl

men

hold

boost

13

0)

Using t ower

lifting

above t he

rear Gonne:c

using tow

the

free

This st. of

crane

off transporter

section

o

preserve transporter

ined

in

paragraphs

each

er

as

of

it

force

bottom set scr ew

out

rigger

t towing t

bar

rac

t orjl

connecting

In t he

l9.b.ilizes

transporter

and

gantry cra

(See

figure

tractor,

t he

four

is

raised

cra

ne and gant

t o

tag

from t he

raise boo

lin

ry

ster

es

to transporter o (See

crane~

approximately t=inc

located

No

10

o

ractor

0

(See f i

t o t he aft end

move transporter pin

in

out

slot of

t ee

booster

prepara

bracket

rigger

gur

es 13 and 140)

f orward No at out

t ory t o liftin

o tSee f i gur es 13 and 14

ne lif t i ng

to

a hei gh't that wi

sim

ll cle

130)

remove tran

10205

sporter f rom

us i ng app

and

10

2060

licab

prevent undue move=

appl y a

slig

ht

h

in tee

bra

of

t ransporter

cket

at

or aft unt i l

0 1 i s

floating

rigger Noo

10

g clear

0)

ultane ous

ar

stat

le specifi ca

ly~

hoist

t he r e

ar

i c test ar ea

tion

s

o

20204

Wi

t h

the

booster still

t

ransportery remove

out

rigger

No

20205 Using tower

202.6

202,.7

20

2.8

gantry maneuver

Using mobile outrigger, at No

Lower

'

crane

Using tower main vertically lines position

Fin

if

5

o

horizontal and

load

to

crane

0 (S

Line

conditions

horizontal

platform,

personnel i t a few

in

horizont,a

in

out

rigger

0 1

if

crane

t o

ee

crane

cond! t

~

hois

sta

bi lize booster and take up sl ack

figure

and hori zontal pl at form t o gai n

ions

t boost

150)

warra er into

disconnect aft cable ass

1110 (See f i

gure

150) A

warranto

pl at form

pla

craney hoist booster

move

over

opening

on main

fee

t above t

using mobile c

tform from stat i c test H

t o a he

boost

of

er hori zon

main

load

load pla

hrus

l

posi

t.i

on~

but free

No

10

At

o

nt

0 (See f i g

vertical positi

tach tag line t o

ure

14

0)

ono

duri

access

embly from outrigg

er Noo 5

ttach tag line t o outr i gg

ran

e'. Re

ight suffici tall

pla

tform, transfer tag

t form; lower boost

move mobile

rea

o

ent

y t o a posiUon

er

t ringo (See f i gur e

of t,he

Use

ng

t o

to cle

and

150

)

er

ar

TOWER CRANE

HOIST

PROCEDURE

EP-14f

AGE

29

OF

stATIC TEST TOWER

147

PRIOR

TO

LIFTING THE BOOSTER

FROM

TRANSPORTER STABILIZE THE BOOSTER

SO

THAT THE

IS

FLOATING

THROUGH

IN

THE RECESS

OUTRIGGER

OF

TEE

BRACKET.

STABILIZING BOOSTER

STEP

PREPARATORY

I

TRANSPORTER

FIG.13

LIFTING

BOOSTER OFF TRANSPORTER

THE

NO.1

TO

LIFTING OFF

STEP 2

LIFTING BOOSTER

OFF

TRANSPORTER

OUTFllGCiER

[\10.

1

PIN CONNEC

(B-AF-12004-2-3)

FIG.14. BOOSTER

TING

STABILIZATION

PREPARATORY

TO

LIFTING

OFF

TRANSPORTER

PROCEDURE

PAGE

OF

GANTRY CRANE

TOWER CRANE HOIST -

IOO-TON BLOCK

AND

SISTER HOOK

ERECTION

BEAM AFT

CABLE

ASSEMBLY -

NO

.5 OUTRIGGER

--------1+-f---+!I

.......,.

....

~~~~~~

~

~~

PROCEDURE

OUTRIGGER

TEST

TOWER

~

ASHE

~<9

~

~\

~

NUT

A TYPICAL 8 PLACES

~

TIEROD

EP_1~GE

33

OF

SUPPORT BRACKET

NUl)

WASHE~~

D

147

DETACHING

STEP I

AFT

OUTRIGGER

CABLE ASSEMBLY FROM

NO

.5

MOBILE

CRANE

o

STEP 2

POSITIONING BOOSTER

ON

TEST

TOWER

FIG.

15

BOOSTER

IN

VERTICAL

P{)SITION

CENTER

20209 Us

tower

2020

'W

Remove tag

on outrig

202

011

Inser t t est t ower pins (

accordance wit h inst ructions from M

202012 Us

'tower

202.13 202

Remove ga

014

Disconnect cable

adapt

cl e CAUTION

blies t o prevent

202

015

The removal of bumper

(D=10426434)

I=>beams No

insi~ructions

(See fi gur es 3 a

in

g tag

t o t,h

in

g gant

er 0 Ra

ar

lines

support

rus

t ringy usi

gers

ry

area

0

~

brac

lin

es

int

o suppor t

crane,

aline

ket s

and lower booster through main

ntry crane

assem

i se

erection

of

boost

er

and lower t o t he groundo (See

g Care must be

damage

an

d t he

0 3

~

4)

5)

as

out nd

boost er out r i

o

ng p

bracke figure

remove

(See f i

ersonnel

defl

gure

t s o (See

16)

ect

or pit

from test t ower

blie

s (

J=1

0424771) from

beam

with

exer

ci sed

in

t o t he second

assembly

installation

(D=1042643

of

6 ~ and 7 1s essenti

line

d i n

paragraphs

4

0)

ggers wit h

15

0)

t o s

tea

dy

booster

figure

in

support

=TEST

LAB

o

bridging

area

o

cable

assemblies atta

disconnecting

stage

adapter o

8) and bumpers

original

ally

1020101

respective

load

pla

and

)

16

0

bracke

t s

from test

se

cond

stage

figure

cable

hardware at

t he

reverse

thr

ough 1

tes

tform guide

in

ohed

3

0)

asseffi=

of

2

1

0

t

40

30

202016 C

REl10VI NG

.3

0 1

Pr

epar i

30

101

3

010

3

0103

3

0104

0105

3

le

ar

t,est t ower

BOOSTER

FROM

ng BOQ,ster

Pla ce

deflect

crane 0

< U

sing

t owing t possi bl e t o and A

ttac

h gant

horizo

ntal Di sconnec t t

so

uth

si de of and i n

lin

Attach wi nch pos

,ition on t he

When transport

as shown

wh

eel

so

area

TEST TOWER

for

Rem

or pit

ractor

in alinemen

ry cra

ne t o drawbar and support t he drawbar

positio

ractor

the

e

with

the transporter 0 (See fig

to tra

defl

er

i s posi t i oned on

in

f igure

,

o

ovaL

bridging ov

, p

osi

t i on t he t

t with t he

no

from t ransport

def

lector pit

nsport

er

draw

ect or pi t b

1j

l ock tran

er deflect

ransporter

deflector pit

er

and move t he t

with

bar

ridgin

the tractor

and winch t

go (See

deflector

sporter

brakes

or pit

as clo

ure

1

ransporter int o

figure

pi t br idgin

and chock

using

bridging

ractor

wi nch

0)

gant

se

in

facing

10

)

g

ry

as

o

a

t o t he

all

GEORGE C. MARSHALL SPACE FLIGHT CENTER

PROCEDURE

EP~141

PAGE

36

OF

1

47

NOTE:

SHROUD

NOT

SHOWN

A TYPICAL 8 PLACES

FOR

CLARITY

FIG. IS-POSITIONING BOOSTER

OUTRIGGER

------~--.-

ON

-

SUPPOR

T BRACKET

.---~--

.

..

--

- ----.

MARSHALL

SPACE FLiOH

PAGE

37

OF

1

47

301.6 Lock

Move tractor

of t

30

107

010

3

30'09

.3

0 10 '

Uslng tower cra

wi

t h

to

a position

8 R

emove doors

4

~

5,

Install

A

~

fi gure

10

Ins

tall

f i gur e 30

30'

;11

Low a

nd washers, f i gure 30

WARNING

i s ext remely impor 'U

sedo Lu and each si de of t he obtaining from a

tta and posi t i oning

dra~bar

in t o nor'th

ransporter o

erection

and

6

~

a

nd 7 as outlined in

bumper assem

.3

0

bumpers (0=,1042

er er

ection beam with

i ns

tall cable

and

nuts

g Corr

bricating the

a torq

th

e head

chme

nt

hardware

rigid

ne, low

beam

pos

iti

on

side

of test t ower and at

er 100=ton si st

and

cable

assemblies

and disconnect gant

tach

er block and

(J=1

0424771)

directly above t he second st age adapt

necessary fli

ght hardware at out

riggers

paragraphs1020L1 and 10201.20

bly

ect

of

(D=104

6434)

assem

blies (J=1042477

in

accordance wit h

ins

tal

lati

tan

to

shanks and t hreads

~ashers

ue

value

bolts

is

durin

on

trans

port ero

in

cable

26438)

accordance wit h

assemblies attached

in

accordance

1)

using

detail

new

instructions

on

of cable assemblies

Ne

w bol t s, washers, and nut s

of

bol

t s

(

NAS

143=16 and

of

6000

inc

h pounds (500 foot pounds)

mandat ,ory t o preve

g removal

of

boost

NAS143= nt

shearing

er

from test t ower

ry

crane.

t o

aft

sister

er

a

tta

0

hook,

ched~

No

with

detail

B,

in

position

bolts,

in

detail

(J=1042

4771

sheil

(NAS156-68)

16c) and

of

ehd

o

C,

be

t he

3

~

)

.30101:2 Qua

30101

.3 0 '1014

.3 G 10

.3

02 Hemo

30201

lit

y Cont

cable ass

valUes of bolts (

3 Re

mova

l of test

~il

l

be performed i n

LAB

0

Use

per sonn

rol

emblies

el

to steady boost

Division

(

J=10424771

NAS156=68)o

t ower pins f r

accorda

thrust ring support bracket so

15 AJl;,t

ving Boost,er from T

.ach t wo t ag

7, and one e

NOTEg

approximat

Tag

ely

ach

lines ,to

75

Prior t o remoYi

following

t he

par

lin

es t o outrigg

to outrigg

be 1=inch diameter

feet longo

owe

r Thrust Ring and Posi t

ng

boo

s'ter f

t s

are

shall inspect t he

) ~

check and

om

t hrust ring support bracket s

nce wit h

instructions

er and t o guide out ri

ers

No 0 .3 ~ t

er s

No

o

an

d 5 i f conditions warranto

1

rom tower thrust ri

ava

ilableg

installation

record the t

wo

t o

hemp rope,

ionin

g on T

ng, check that

of

orq

ue

from M=TES

ggers

free

outriggers

or

equal,

ransporter o

t he

T

of

No

0

GEORGE C.

PROCEDURE PAGE OF

MARSHALL

EP=141

SPACE

302.

FLIGHT

38

101

Rear id

CENTER

147

ring

ent

ifi cati

section with Fin I

on

(1)

required

NOTE

30201. 2

302

010

3

302

010

4

g Rear

is

attached

Rear

rIng

i

dentification

Rear

rIng

identifi Rear

ring

ring section wit h Fin I to

transporter 0

sec

t i on wit h

sect

ion wIt h

ca

t i

on

section wit h

identification

3020105

installed

NOTE

sec bracket is attac F

in

3

020106 Screw

brackets wit h s

(J=AF=12004=2=

~

One

t ee

t i

on wIt h

III

identifica

(J=AFr=12004=2~".s

Fin I id

et

bra

cket

ent

hed t o r e

tion

)

Tee

3020107 Screw (J=AF=12004=2=13) 3

02

0108 Screw (J=AF=12004=2=17)

Fin

II

Fin

III

Fin

IV

screws

2)

is attached

ification

ar

ring

o

identification

(1 )

(1

)

(1 )

(6)

t o

rear

ring

and one t ee

sec

t i

on wit h

(32) (8)

(32)

required

requi

red

requ.ired

required

020109 Barrel

3 30201 3020101

01

0 Connect i

1 Washer 30201012 Bal= 302

01013 Bal= 302 3020

302. 302 3020 3020

30201.

302

14

01

0

'01

5 Screw

1016 Bo

01017

101

8 Washer

1019

20

01021

Bracket

l t (J=AF=12004=4-33)

Washer (J=

Roller Tubing (J=AF=12004 Hex Nut

nut

(J=AF=12004=2=6)

ng

(B=AF~.1

(J=AF=12004~2=5)

lok pin (J=AF=12004 lok pin

(J-AF=1200

(J=AF=12004=2

(J=AF=

12004=4=31)

4=4~32)

AFd12004=4=34)

(J~AF~'12004='4 =35)

(D=AF=120

04~4=36

=4=37)

(J=

AF=12004~4=38)

2 004<'>2=3)

.'3

2=9)

=24.

)

(8)

req¢.red (8) required (8)

required

(8)

required (8) required (4)

required

(1

6)

require (2) required (4)

required

(4

.)

required

(2)

required

(2)

required

(2)

required

d

302

302 302

302

02

Cl

ean mat

support

ven

t~

ing

cla

F

ederal

paragraph

a l

igh

t coat

Spec

ification

hardware 0

03

Raise boost er to a

04

Usi

ng tower cra

05

vertica

Have boos

l ly over t he

men hol d each t ag

te

r o (See

surfaces

mps

302

01

of

MIL

of

, and at

taching

Speci f icat

of Milita

P=9 pre

=L=

644, to

heig

ne,

move bo

def

fig

ure

150

all

GEORGE

PROCEDURE

rear

ring

C.

MARSHALL

EP=141 PAGE 39 OF

sections,

hardware with

ion

p=s=661,

ry

Specification

in

accordance

MIL=P

servative lubricating

all mating surfaces

ht

of a

few

fee

t above

ost

er

horizontally

lect

or pit b

line

t o prevent undue

ridging

o (See

)

SPACE FLIGHT

tee

brackets,

dry~cleaning

sol-

with

=11

6 and

oil,

Military

and at

thrust

t o a

position figure

movement of

apply

taching

ringo

150) t he

147

30206 Lower

cable

boost assembl yo (See fi g

30207 Using mobi

cable 110 ri

3

020

8 Lower h

mobile c

30209 Using t

t o a f ig

302

01

0 Load

sma transp

NOTEg

302011 Usin

p

at

assem

) (See f ig

gger

number orizonta

rane

ower crane

horizontal

ure

'13

tee bracket

l l a

nd

ortation

The

g f o

rk lif t , rai

latform

tee att

er

t o a

height sufficie

ure 150)

l e crane, pos

bly

(0=1

ure

iti

on

0423292) t o outrigger

8 f

or

identi

s o)

l platform and personnel t o the ground and

and hor i zontal

and gant

pos

iti

on

ry

dire

0 )

s f

lar

ge Bal=l

or out

riggers

ok pin

ri ng plat formo

tee brackets are matc

se

and position

and personn

achment point s

el

as

nece

of

horizontal

fication

pla

tform

crane, ctl

y above t

Noo 2 and

s f

or out

h=marked

ssary

outri

ggers Noo

nt t o

allow att

platform

No

o 50 (See

of Fin

clear

of transporter

simultaneously

ransporter

8,

riggers

t he t on

each

No

for

proper

ransportation

side

1~

achment

and

Lines

conne

1,

o

of the

2,

and 80

of

af'

attach

aft

figure

and out=

move

ares

lower boost

o (See

cti

ng

pins

2,

and 8

location

r i

on

o

ng

boost

o

er

,

er

012 Install

302

No

o

connec

1~ 2~

pinso See fi g

302013 lns

t,a

ll

tee

la

rge Bal=lok

302014 Lover tran

an

d clear

302

015

Lower boos

so t ha t t he c the

tee

bracket

tin

g pi n

and 80 Secu

throu

re connecti

ure 6 for pin

brackets to out rigger

pinso See fi g

sportation of

the

t,er to reaso

onn

rin

g plat f

area

o

nable

ect

ing pin in outrigger

on

the bott

om

gh o

utri

gger bus

ng

pi ns wit h

location

ure

height d

s N

6 f

orm

s

oo

or

and pe

irect

rear ring se

o

2 and 80

locations o

rsonnel

ly

Noo 1

cti

hin

gs at out

sma

l l

B~

Se

cure v

t o the gr.ound

over t he t

is

directly

ono

rigger

l=l

ok

ith

ransporter

above

GEORGE C.

PROCEDURE

EP-141

MARSHALL

SPACE FLIGHT CENTER

PAGE

40

OF

147

3.2.16

3.2.17

3.2.18

3.2.19

3.2.20

3.2.21

Using towing porter, position

and

ring

Lower

rigger ring

NOTE:

Install

move

in

the

section.

booster

No.

section.

The

two

the

outriggers

(See

figure

Adjust

to

8

(See

Install

set

center

figure

all

transporter. Using mobile

necessary

outrigger

to

Noo

tractor transporter

connecting

center

of

(See

onto

1

into

slot

(See

forward

bolts

No.

only

2 and 8

7.)

screws

in

connecting

60)

support

(See

crane, disconnect

5.

(See

that

is

forward

in

the

tee

figure

14.)

transporter;

of

tee

figure

ring

is

14.) now

through to

secure

tee

brackets

in

clamps

figure

raise

that

12.) horizontal

aft

cable

figure

attached

or

outrigger

bracket

guide

bracket

in

position

base

tee

at

center

secure

assembly (0=10423292)

11

)

0

to

the

aft

as

No.

slot

on

connecting

at

Fin

of

each

brackets

outriggers of

tee

the

platform

aft

end

necessary

1

directly

the

bottom

Line I of

on

transporter.

tee

b!'acket

to

ring

No.1,

bracket

forward

and

personnel

of to

at

section.

notch.

ring

trans-

above rear

out=

rear

at

2,

and

to

_from

the

as

3.3

3

2.22

0

Lower mobile

3.2.23

Using in

(See

3.2.24

Disconnect

Tie

(See

3.2.25

Using the

3.2.36

Haiae

Installation

3.3.1

Using towing

static with sufficient

crane

3.3.2

Lock

horizontal

crane

gantry

front

of

figure

cable

figure

gantry

ground.

erection

Procedure

test

deflector

and

transporter

platform

and

horizontal

crane,

booster

10.)

two

cable

assemblies

3.) crane,

beam Rear Ring

tractor~

tower

at a right

pit

working

fork

lift.

brakes

and

personnel

platform

position

horizontal

in a position

to

the

clear

of

platform

disconnect

assemblies (J=10424771) from

together

lower

to

clear

Sections

position

bridging

area

around

(See

and chock

to

prevent

horizontal

booster.

(J=AF=12004=2=0).

transporter

angle

to

at a distance

the

transporter

figure

10)

wheels.

damage

platform

on

deflector

which

ground and

transporter

and

personnel

erection

to

booster.

and

personnel

north

pit

side

and

will. provide

for

the

move area.

beamo

beam.

to

of aline

mobile

303.3

3.

3.4 Att

Connect

section

ach

5

0)

ring

with

tag

handling Fin

line

brackets

II

identification.

to

lower

portion

and choker

(See

of

ring

lines figure

section.

to

5,

rear

detail

(See

ring

A.)

figure

30305 Using mobile

wi

t h

Fin

II

swinging moti

303.6

303

303.8

Load ring

NOTEg

07

Using pla

make

Fit attached sections

30308.1 Ut

two

tee

p1atformo

Tee bracke t s

fork

lif

tform and

ring

rear

splice

ring

to

as

ilizing

locator

section, t o section. (See

30

308.2

Install bracket

crane wit h t

wo

identification

on wit h bracke

t,

personnel

section

transporter

tag

t s and

are

raise

connect

line.

match-marked

and as

ion

with

in

fo110ws g

the 4 1/2""inch screw (J-AF-12004-2-18) and

(A-AF-12604=2

aline

ring

insert locators

figures

remaining at out

rigger

hooks,

position

opposite

(See

attaching

position

necessary

at

outrigger

Fin

II

identification

approximate

~

14)

in

sections

into

matching

6 and 7

two

bol

t s t hrough

Noo 2.

rear

Fin

II

on

booster.

figure

50)

hardware on

for

outriggers

the

transportation

to a height

Noo 2.

location.

end

holes

by

tapping

holes

0) base

(See

figure 6.)

ring

section

Control

transportation

No.

3 and 4,.

ring

sufficient

(See

figure

to

ring

Connect

of

each

to

section

ring

screw heads

of

opposite

of

tee

4.)

ring

303.

8.3

303.8

04

3.3.8. 5

3.30806

3.

3.8

07

Install tig

No 0

four 8-inch

ht en

2.

(See fi

t,o

Remove two section

with

and remove

section. Install the

a t orque

of

Remove two install

Tighten

each screw screws

figure 70)

Install two

7

0)

screws (J-AF-12004-2-17) and

secure

bol

rear

gure

t s that

ring

70) secure

Fin I identification

two

barrel

(See

figures

remaining 700

foot

4

1

/2~inch

nuts (J-AF-12004=2-6) from

6 and 70)

screws and t

poundso (See

screws (J-AF-12004-2-18) and

in

opposite

to a torque

barrel

nuts

(J-AF=12004-2-6)0 (See

sections

tee

side

of

700

at

bracket

at

outrigger

ighten

figure

of

foot

outrigger

to

rear

ring

No.2

ring

all

screws

70)

rear

ring.

pounds. (See

figure

to

GEORGE C.

PROCEDURE

MARSHALL

EP=141

SPACE FLIGHT CENTER

PAGE

OF

42 147

3.3.9

3.3.10

3.3.

11

3.3.12

3.3.13

3.3.14

3.3.15

Position

No.

a t

outrigger

figure

outrigger Install

and Adjust

notch

NOTE:

3 and

6.)

connect

4. set

of

It

and

4;

numbers.)

(See

tee

may

connection

Remove ring

.

Connect section

Attach

ring

section

ring with

tag

5. )

Using mobile

wi

th

Fin

IV

swinging

motion

install install

No.3,

(See

ing

figure

screws

brackets.

be

with

ring

handling

with handling

Fin

line

to

crane

identifi

with

tee

brackets

tvlO

bolts

and

two

figure 8 for

pins

and

6.)

in

tee

bracket~

(See

necessary

to

section

brackets

Fin

II

identification.

brackets

IV

identification.

lower

with

cat

tag

portion

two

ion

line.

opposite

to

ring

at

outrigger

bolts

at

outrigger

identification

B

al~lok

t o

pins

center

figure 6.)

readjust set

with

Fin

III

and choker and

and choker

(See

of

ring

hooks,

position

Fin

(See

figure

section

No.2,

at

four

No.4.

of

Fin

Line

at out

riggers

connecting

screws t o

identification

tag

lines

to

rear

figure 5.)

section. (See

rear

ring

IV

on boos

ter.

5.)

outriggers

bolts

(See

and

No.3

in

make

.

from

ring

figure

section

Contro.l

3.3.16

3.3.17

3.3.18

Load

ring

two

platform. NOTE: Using

pla make

Fit

fork

tform and

ring

rear

attached

sections

3.3.18.3

tee

Tee

brackets lift1

splice

ring t o t

as

Utilizing locator section, to ring

Install of

Remove install Tighten

figure

brackets

are

raise

personnel

connection at

section

ransporter

follows&

t he 4 1!2=

(A=AF=

aline

insert

locators

section.

the

700

foot

two 4 1!2=inch

each screws

6.)

and attaching

match=marked

and

position

as

necessary

outrigger

with

Fin

in

approximat e

IV

identification

inch

12004-2=14)

ring

sections by

into

matching

(See

figure 6.)

remaining

screws and

pounds. (See

screws (J=AF=12004-2=18) and

screw

in

opposite

to a torque

hardware on

for

outriggers

the transportation to a height

No.8

location.

transportation

No.6

ring

sufficient

. (See

to

figure

ring

Connect

and

to

4.)

section

ring

screw (J=AF=12004=2-18) and

in

end

figure

of

700

holes

tapping

holes

ti~hten

6. )

side

foot

of

each

screw heads

of

opposite

to

a t orque

of

rear

ring

pounds. (See

ring

.

7.

30301804

Install

two

figure 60)

barrel

nuts

(J~AF=12004~2-6)

(See

303019

Posi

tion

No

6 a

o

at

outrigger

nd

and

7;

figure 60) (See

303020

303021

outrigger Install

70 (See

and Adjust set screws

notch NO

TEg

of

It

co

tee

numberso) nnec

may

connection

303022

Rem ring

ove

ring

section with

303023 Using mobile

and p for

figure

ersonnel

ring

so that

installation

40)

install in

sta

ll

No

0 7 ~ and t

figure 8 for

ting pins

figure 60)

brackets

be

necessary

with

ring

handling

Fin

crane~

on top

the

pla of

tee

brackets

two

bolts wo

and Bal=l

in

tee

brackets

(See

o

section wit h

brackets

IV

identificationo

raise

of

and

t he tform t he upper

to

at

outrigger

bol

tsa t outrigger

identification

ok

to

figure

to

readjust

Fin

and choker and

position

booster

is

resting

section

ring

pins

center

60) set

III

the

just

firmly

of

section

Noo

at

outriggers

at

8,

No

0 6 0 (See

of

Fin

four

Line

connecting

screws

to

identificationo

tag

line

horizontal

forward

in

the

of

proper

rear

ringo (See

the

outriggers

bolts

and

No

6

o

in

make

from

platform

rear

position

303024

Connect ring

handling

identification

3

030

25 Using m

NOTEg Rear c

enter

tee obile

ri

ng s

ecti

ring

bracket

crane with

on

and connect t o choker

303026 Connect choker

ring secti tee

bracket

swinging

igure 50)

f

303027 303028

Install

Lower

connectin

s

ectiono

303029 Using a

pla

tform and personnel

tee

at tachment

40

)

on

with

is

movement of

connecting

rear

ring

g p

in in

(See

fork 1if t9 raise

brackets

with

nut s and

section with

attachedo

lines

Fin

to

III

directly

rear

in out

section

outrigger

figure

50)

as

poin

t s

of out

to

ring

bolts

Fin

III

two

hooks,

ring

handling brackets

identification

above out

ring

rigger

section wit h

rigger

with

Fin

III

No

5

as

o

and

position

necessary

riggers

section

and

attach

identification

IDwer

crane hooks

lineso

t o a

Noo 50

tag

Noo

50

(See fi gure 60)

identification

a guide t o

t he t

ranspor on No

each

o

side

4 and

with

F;in

tag

lineso

o

Raise

position

Control

lineso

utilizing

position

tat

of

booster

90

(See

has

to

rear where

ion

figure

III

rear

(See

ring

at

GEORGE

PROCEDURE

C.

MARSHA

EP

=141

3.3.

3.3

LL SPACEFLIGHT

PAGE

44

OF

30

Conne ri

ct

ng sect

rear

accor dnace wit h pro

t hrough 3.

respe

031

Install two bol No

cti

vely

o 4 and

CENTER

1

47

ring section with Fin

ions with Fin

II and F

cedures outlined in

3.8.7

and

paragr

.

t s 'through

6.

(See f i

gure 60)

III

i den

in

IV

identificati

paragra

tificati

phs

on t o

ons

in

3.3.801

aphs 3.3018.1 t hrough 3.3.18.4

base

of tee b

ra cket

s at o

utr

iggers

rear

303.32

303033

303034 Using

303035 Lower

304 Bemov

Two

3

0401

Adjust set screws

not ch

of tee brack

Remove ring hand re

ar ring secti

mobile

from t

op perso

u

sing

fork

ing

Bump

er Assembly

Cab

l e

A ssemblie

Prior

t o r emoving b

(D=1042643

following

t he 3040101 3040102

304.103

in et

ling bracket

on wit,h F

cra

ne~

of

t he booster o

nnel and tran lif

t o

(D=10426~J8)

s.J.~T

='104

4) j and t par

t s a

Door (0=

s,'

Pl

cr

S

,10411708)

te

(D=

104'l'J753)

(7513~~·u

ew

t ee

brac

ket s t o

o

(See f

igure

s and choker and

in

III

re

move horizontal

spor

tation

,

24771JI'

ump

er assembly

wo

cab

le

assemblie

re

ava

ilableo

032=

']

2A)

cent

er

60)

,id

enti

f,icationo

platform

ri

ng p

lat

T}[Q

~Jlll1P,J!r

:?~D-

(D=1042643

s (J=10424771) , check t hat

(See fig

(5)

C')

).

(60)

connecting pin

in

tag lines from

and p

ersonn

el

form t o the ground

~1Q

4?&4}41,i,

8) , two ure

20)

re

qu.ir ed

bumper

and,

s

requlred

required

30

40104 3040'1.5 .3

040106

304010'1

30401.8 3

04010

30402 Using

plat

f o

bumper

304.3

Remove by removing fi

gur

P

in (C=104'H721 ) in

P

N

ut Bolt Lock P

Screw

9

fork rm

and pe

and

lif

cable

bumper

bolt (AN

e 3, deta,

( G= 10411722)

(

NAS=1022

'~C8

((,-:,104°11723)

late

(AN

t~

rsonnel

asse

(G=104'~17

501AC416

raise

and pos to

assem

mbly

blieso

(D=1

I2=14) a

il

A 0 )

)

2

,)

~-8)

ltl

on

a hel ght nece

(See f

0426L~38

nd

washer

igure

)

from secon

the

(2)

require requI

(2)

required

(4)

(4

)

require

(.2)

req\.L\red

(2)

required

t r

ansportation rin

ssary

3

0)

red

f or removal

d stage adapt er

(AN

960=1216

)0

d

g

of

(See

EP=141

30404

Remove

places

(See f i gure

30405

30406

040

3

Un

tie

adap t

Install all

3.4

1c·1

0

7 Using

nel

er

to the

30408 St ore b

wo

cable

t

NOTEJ

from the test t

bumper

by

and re

0 (See

t hrough 304

(D=

10426434) from second

removing

3,

detail

mov

e cabl e assembl i

figure

fligh

bolt (AN14=

B

~)

14) and washer

3, detail C

t hardware that

010

90 (See f igure 20)

es

fork lif t9 lower transport at

groundo

ump

er

Tran

assembly (D=

assem

blie

sporter

ower area

s (J=10414771

and boost

10416438) , t

er

are

o

stage

(J=1

042477

o)

is

called

ion

ring

wo

) , and at

now

ready

adapter

(AN945=14P)0

1)

out

pla

bumpers

taching

to

at

two

from second

in

paragraphs

stage

tform and person=

(D=

10426434),

hardwareo

be

moved

GEORGE C. MARSHALL SPACE FLIGHT CENTER

PROCEDURE

PAGE

OF

CHAPTER

II

10

PREPARING

NOTE~

when recommend shows

TRANSPORTATION,

BOOSTER

The

actua

the

wind speed is slowesto

erec

loads imparted

TABLE

l time

tion at

I -

EFFECTS

WI

ND

(

MPH)

FOR

ERECTIONo

wind speeds

to

SPEED

5

10

15

20 25 30 35 40 45

HANDLING,

of

erection

the

booster

OF WIND

AND

ERECTION

should

The

procedures

of

15

at

SPEED

be

scheduled

MPH

or

different DURING

ERECTION

AT GAPE

outlined

lesso

The

wind speedso

WIND

BOOSTER

1250 2250 3200 4375 5700 7200

CANAVERAL

at

the

time

in

this

chapter

following

OF

BOOSTER

FORCE

ON

(LBS)

100 350 800

of

table

day

10

1

10

2 Pos

Preparing 10101 101

Position bridge crane

02

Lower 60-to

(

J~1

the

03

101

Lower 40-t assembly (D-104 and

itio

ning Transp

1

0201 Us

vicinity of and with adequate maneuver fork

0202

1

Lock transp

Service

Structure

for

Erectiono

at

l60-foot

n bl ock from bridge

0423l94)o

Raise

60-ton

work areao (See figure 170)

on block from

aft

cable

ort

ing towing

23292

assembly er

P-AF~1 20 04

tractor

launch

pedestalj out

bridge

)0 (See

clear

j pos it

ion

clearance

lift

and mobile craneo (See

ort

er

brakes and chock wheelso

levelo

crane

block and

crane and figure of

L

on

the

trans

of

all

sides

170 work areao

porter way

(See

and

attach

erecting

attach

) Raise

of

figure

erecting

beam

aft

40-ton

and boos other

trans

equipment porter

figure

clear

cable

ter

180)

170) beam

of

block

in

to

PROCEDURE

EP=141

SERVICE

STRUCTURE

~-

~::=~~~

~-#

~

-+Il

""::""4llJ.

BRIDGE SO IN IS

~~-....!·BRIDGE

-:u...--

~~II----

CRANE

THAT

THE RETRACTED POSITION

160 FEET FROM

60-TON

ERECTING BEAM

(J-10423194)

40-TON

CRANE

BLOCK

MUST

HOOK

BE

SET

HEIGHT

GROUND

.

SUPPORT ARMS

HOLDDOWN

ARMS

FIG. 17.

PREPARING

SERVICE

~

f¥.i'III~~~t;.!

STRUCTURE

FOR

II---AFT

ASSEMBLY

( D-

I0423292)

ERECTION

CABLE

PROC£

DU~

E EP-141

PItOrE

49

OF

147

SERVICE

STRUCTURE

----I~hrul

-BRIDGE SO

THAT

IN

THE

IS

160 FEET

CRANE

RETRACTED POSITION

MUST

CRANE

ABOVE

BE

HOOK

THE

SET

HEIGHT

GROUND.

SUPPORT ARMS

FORWARD

ASSEMBLY

1I!'!1t:~=ln

60-TON

BLOCK

(J-l042666B)---~H-_~..,..;W'&'

SLING

TOWING

TRACTOR

(M-26)

1ftW1tfHIr~::-ftt---40-TON

~

~~~~~--AFT

~

ASSEMBLY

(

0-10423292)

I4---tSATURN

BLOCK

CABLE

BOOSTER

TRANSPORTER

TRANSPORTATION

(J-1042597I)

ORIZONTAL

PLATFORM

(J-10426476)

RING

FORK

PLATFOR

LIFT

FIG.IS POSITIONING EQUIPMENT

AT

FIRING

SITE

10203

Disconnect

tow

bar

to

tow

bar

allow

from

adequate

transporter

clearance

and on

move

all

towing

sides

tractor

of

transportero

and

103

Installing

(J

-10426668) 0

10301

103.2

10303

10304

Using sonnel

(

J-I0426675)

(See

Remove interstage 3, sling

Remove e.ttaching

second forward

I

nstall stage and 20,

Beam

fork

to a height

figure

doors

4,

6, assembly

stage

sling

mounting

adapter nuts detail

Weldment

lift~

and forward

19,

fairing

and

7,

adapter

(AN325-14 )

Eo

(J-I0426675)

raise

necessary

step

(D-I041l708) and

and second

to

gain

attaching

hardware

assemblies

brackets (J-l0427014

using

transportation

sling

1

0)

access

points

that

at

attaching

as

shown

two

bolts

for

each mounting

and Forward

for

attaching

assemblies

plates stage

to o (See

secures

(AN14C-32), washers (AN960-14l6),

(D-I04l1753)

adapter

beam

points in

figure

Sling

ring

platform beam

(J-I0426668)0

at weldment and forward figure

interstage

for

and

J-I0427097)

bracket

Assemblies

weldment

outriggers

20)

beam

2.

as

shown

and

per-

attached

fairing

weldment and

on second

in

to

Noo

to

figure

103

.5

10

3.6

10307

Using mobile beam

weldment (J-I0426675 )

ment

detail

Attach adapter

Figure

WARNING

nuts

i ng hardwareo Attachment

cable

Qua sling

values

to

(

AN16C-54)

Eo

forward

(

NAS143-

20,

; Corr

(J-

10426668) shall

in

detail

o

lity Contr

assemblies (J-I0426668

of

mounting

at

crane

and

Fin

l6 and

detail

is extremely

be

A,

figure

ol Division

bolts (NAS156-68

and

brackets

nuts (AN325-

sling Lines

NAS143-16C) ~ and

Ao

ect

attachment

used.

20

two

assemblies II

and

Lubrication

are

sling

into

(J-

I0427014 and

16)

as

IV

using

of

important

mandatory

lug

must

sha

l l

inspect

)0

assemblies

position

shown

(J-

I0426668)

nuts

the

forward

.

and

be

Check and

and

J-I0427097)

in

figures

bolts (NAS156-68),

(C-424316)

New

bolts,

torque

to

avoid

in

same

the

installation

record

(10427036),

attach

to

sling

values

shearing line

beam

19 and 20,

second

as

shown

assemblies

washers,

as

of

the

torque

raise

weld-

with

defined

pull

bolts

stage

washers

in

and

of

attach-

as

of

the

10308 Ti e forward sl

wire

to

avoid

ing

assembly

damaging second

cables

stage

to

beam

adapter.

weldment

with

rope

or

GEORGE

PROCEDURE

C.

MARSHALL

EP=141

SPACE FLIGHT CENTER

PAGE OF

52

1

47

a:,.{

~

.'/"~

,

'~ ' ··:~

.

~

CONNECTING

FORWARD SLING ASSEMBUES,

SLlNG

ASSEMBLY

BEAM

WELDO<ENT (J-1

-'7f,~~

:J.-

---

STEP I

(10427036)

0426675

---

AND

-----":=

BEAM

WELDMENT

===

SATURN BOOSTER

==--

TRANSPORTER

MOBILE

FORWARD UPPER SECTION

RING

MOBILE

CRANE

HORIZONTAL

PLATFORM

ON

SHROUD

REMOVING

----

HORIZONTAL ON

STEP

2

FORWARD

~~::::---

PLATFORM

TANKS

....

(J-10426476)

FORK

LIFT

REAR RING UPPER SECTION

SATURN BOOSTER

~~

::s."?"I

FIG.

IJ.t~"'

''''-'--~

REMOVING

19

PREPARING BOOSTER

-'-

STEP 3

REAR RING

TRANSPORTER

FOR

ERECTION

SATURN BOOSTER

TRANSPORTATION

PLATFORM

FORK

LIFT

RING

I,

. /1

SLING ASSEMBLY

. - -_, ,

,

~

--

<,:::-...

':

,'

' .' i (J-10426668) .J

\~

~"

..

FORWARD

;;

SLING ASSEMBLY

''\i'

TO

BRIDGE

AT

160 FT. LEVEL

\,t

/

'/

,.

.

~

""

\

tJ

CRANE

..

60-TON

[]

-

1

BLOCK

\----

F'-'-'=

E

FLIGHT

53

NOTE : WIPE OFF ALL LUBRICANT

FROM BOO STER PARTS

WITH

CLEAN

TIME

OF

SLING ASSEMBLIES

____

-L"o

~

--

:..:

-

~

RAGS AT I

REMOVAL

CENTER

OF

147

'''1

II

DF

IT\

"]

- BEAM ASSEMBLY

(10426675)

I

i

---

-----

I

I.

TORQUE LBS

. BO

WITH NOTE: WHENEVER

WASHER

--

HEAD

OF

BOLT

(NASI56-68)

(500

FT.

LBS), WBRICATE THREADS, SHANK

LT a EACH

MOLYKOTE TYPE "G",

SLING

WASHER(NASI43~16C

NUT

SIDE

OF

WASHER

ARE NUTS SHALL

TO

8E(}lSCARDED,

ASSY

BOLT {NASI56-68)REF.

~NAS

(C-424316IREF.

SLING 'ASSt:MBLIES

AT:rACHED,

143-16)

NEW

BE

INSTALLED, USED

PULL

(J- 10426668)REF.>

)REF

.

REF.--\

Yfj

INSTALL LUG

ti

BOLTS, 'WASHERS,

OF

-1

--...,/j

uv

TO

6000

INCH

OF

BEfORE INSTALLATION

(J-I0426668)

CABLE-SEE

HARDWARE

IN

LINE

A-A

AND

1

".~--

\"

OF

"-....

~

__

-'

---MOUNTING

.hOLT

l

0-

(J-104270141-

(J-104210971-

,M

/ /

{ANI4C-321

f------

--

BRACKET

SHOWN

0PPO

bJ

.~

-

--

,-------

--

BEAM (J.-I0426675)

r--S_IT_E_S_I_DEL-...."

BOL~

_ _ _

-

----

..

_."

- -

WELDMENT

(AN'6C-,547

1

~,

----.J

-,

~

l

~uT

(.AN.325-16)

'.

__

._ _____

...

_____ ....

______

FIG, 20,' IN'

________

__

._.

SlALLAtl0N

____

OF

BEAM

._

,j

A.

WELDMENT

..

AND

FOWARO

SLING

ASSEMBI".IES

GEORGE C. MARSHALL SPACE FLIGHT CENTER

PROCEDUREEP

1

- 1 4 l PAGE 5 4

.4

Removal

OF

147

Procedure Forward Ring

Sections (J-AF

-12004-3-0).

1. 4. 1

1

.4.2

Position above so

the

mobile crane so

the

forward

boom

can

be

ring.

maneuvered

operations. Using mobile

and personnel so

tha

t the

tanks.

Working from the

crane

on

pla

tform

~

top

following procedures

1.

4.2.

1 Connect r i

1

.4.2.2

10402. 3

with Fin figure

Lower

l

ines.

Co

nnect choker

ng

III

210

crane hooks

slight tension

l

ower

A. )

pos

i t i

that The

mobile crane

raise

of

is

and

the

booster just

resting

horizontal

8 (See

figure

handling identification

)

to

lines

on

crane cabl

on

of

ring

the

two

for

all

posi

tion

firmly

platform

19,

brackets

with

work

area

t o

ring

es.

sect ion . (

crane hooks

is

now

forward

the

aft

on

ring

horizontal

of

top

of

complete the

step

2.)

to

forward

nuts and

and connect

handl ing

brackets

Attaoh

See figure 21,

are

directly

in a position

disassembly

platform

the

forward

two

70-inch

ring

section

bolts.

to

choker

and

tag

line

to detail

ring

(See

put

1. 4.204 Di soonneot beam No. 5 by

and key Leave

10

403 Using fork l if t , rai

form and personnel

at

r i

ng

seotion beams Noo 4 and for

identification

10

404 Disoonnect tee braokets f

6

by

removing

so

rew

and key at each t ee

1.4.

5 Disoo

nneo

i

dentifio

1.4.5. 1

t and

atio

Remove forw

reta

tee

bracket

as

separation

6. of Fin Lines and I -beams ).

four

bolts

remove

n as fol

two 4 l/2-inoh

ard ring these screws i n opposite pull loc

ators

tee

braoket

removing

from forward four

bolts,

ining sorew and key. (See

se

and posi

necessary

(See

figure

rom

~

nuts, braoket.

forward

lows

: (See f i gure 23. )

se ct ions

to

the disconneot posi

bolted

and

forward

to

the I-beam.

tion

transportation

on

each

tee

attachment

19,

Step

ring

sied

2.)

at

and washers and key

(See f

ring

section wit h Fin

scre

ws

at

I -

beams

holes

igure 22.)

(J-

AF-l2004-3-l2) from

No.

and t ighten screws

ring

nuts,

figure

of

the locations (See

I-beams

4 and

tion.

seotion

at

and washers

22.)

ring

plat-

booster

at

1-

figure

reta

No.4

i ning

22

and

III

60

Insert

to

1-

CHOKER LINE

FIG

. .

21

REMOVING

FORWARD RING SECTIONS

(J-AF-12004-3-0)

GEORGE

PROCEDURE

C.

EP-141

56

147

- -

FORWARD

RING

(GMT -12004-3-0)

-------

BARREL

(J-AF-12004-

NUT~

-

--~----

3-6)

ROTATED

I

~

-.--

---

:?':

LOCATOR

(A-AF-12004-3-71

0

180

-

._------_.

FIG. 22. FORWARD

CAP

/ -

'"

(JAFI2004-8'21

BO~"

~--":"SCREW

'\

l'

SHOULDER

(J-AF-12004-8-~)

SCREW

--------

RING

SECTION

--

ATTACHING

.....

PAD

( D'AF-12004-8-3)

~

UT

(J'AF-12004-8-22)

--

PLATE.

NUT

( B-AF-12004-8-12)

"""

~

....

"

-SCREW

~

~~lCKET

(D-AF-12004'8-2)

. -

...

.

-~-

..

----~-

-

....

-- '

POINTS

_-----

'?lO

~

(B-AF-12004-8-24

" (J-AF-12004iH2)

WASHER

'

:;:.,

SC~tW

,IjI

IJ-

.--_

.....

,

-...

120~

1~1

..

-

SCREW

(J-AF-12004-3-20)

SPACE FLIGHT

PAGE OF

TEE BRACKET

(F-AF - 12004

WASHER

(J-AF- 12004

-3-2)

57

-3-9)

147

SCREW

(J-AF-12004-3-8) ...

J~

--'.~--->~-

~~~~--~.--~~~=,~--~~---

SCREW

(J-AF-12004-3-12 )

----

----~--

--.

------

--~

FIG,23.

FORWARD RING SECTION REMOVAL PROCEDURES

GEORGE

PROCEDURE

C.

MARSHALL

EP-141

SPACE FLIGHT CENTER

PAGE

58

OF

NOTEg The

locators

ring

1040502

Remove end

tion

1040503 Using mobile

Fin I

to

1040504

Disconnect section

10406

Disconnect nut

plate

j

10407 Thread rope

rope t o

10408 Using

mobile

the ground 0

4 1/2-

inch

(A-AF-12004-3-7) remai n

sectionso

six

8-inch

of

forward r i

ng

o

crane

II identification

contr

ol swinging moti

ring

handl

with

Fin

III

tee

bracket

and

nuts

through l-i

crane hook

from

(See figure

o

nch di

and l ow

cranej lower hor i zo

screws

(J~AF-

12004-3-12)

with

scre

ws

(J-AF-12004-3-8) from

section

wit

h Fi n

, lower forward r i ng

to

the ground 0

ono

ing

brackets

identifi

I~

beam

Noo 5 by

23

det ai l Ao)

ameter hole

er

bracket

ntal

platform

cat

fr om fo

iono

removing four

of

tee to

and

the

forward

each

III identifica

section Use tag

rwa.rd

with

line

ring

bolts,

bracketo Attach

the ground 0

and

personnel

-

to

10409 Using

fork

personnel

1

040

10 Connect

II

ring

identificat

Ao)

104011 Lower

crane

104012 Connect cho

1

04013

tension

of

ring

Disconnect

on section

7 by removing four screw and keyo (See

104014

1

04015

Remove I-

two

beam Noo Bo

Disconnect ficati

on

as fol lows g (See fi gure 230)

lift

j lower

to I-beam

handl

ion

ing

with

hooks t o work

ker lines crane

cables

transportation r i ng

Noo 70 (See figure 1

brackets

nuts

area

to forward r i

and

bolts

and connect t o

t o r ing handling bracket s and

o

Atta

ch t ag lines

o

tee

bracke t f rom forward r ing sect

bolts,

and

remove

bolts

nutsj and w

j nut s j and w

figure 22j

ashers

forward r i ng

deta

platform

9,

ste

p 20)

ng secti

and

on wi

o (See figure 21j deta

choker lines

put sli

to low

er porti

ion at I-beam Noo

ashers

i l

f rom base

sec

tio

Ao)

n w

and key

of

tee

ith Fin

retaining

bracket

II ident

th

o

ght

on

Fin i l

at

i-

1040150 1

Remove

two 4

forward r i

1/2-inch screws (J-AF-1

ng

sec

t i ons at I-beam

2004-3=12) from

Noo

80 I

nsert

these

screws i n opposi

locators

to

t he disconne

te holes and tighten

ct

posi t i

ono

screws

t o

pull

NOTEg The loca se

10

401502

Remove fo

beam

1

0401

503

Low

ground and

1

0401504 Using mobile

II

t rol swinging mot

10401505 Disconne

fo

104016 Repo

104017 Thread a ro

s i t i on fork lif

er

sonnel t o I -beams

p

br

ackets Noo

ctio

t o

4 1/ 2

rs

(A-AF-12004-3-7 ) remai n

nso

-i

nch

scre

si x S-i nch screws (J-AF-

rward r i ng sec

Noo

So

tion

wi th Fin II

er transport ation ri ng

move

crane~

i

dentificat

ct

i on

r i ng handl i ng

rward r i ng sect

t, rai

Noo

pe

t hrough t he

fork

se transportation 6 and 70

lift

lower forward

to

the

ion

o

ion wi

l ~inch

6 and 70

ws (J-AF

platform

clear

ground 0

brackets

th Fin

di

II

ameter holes

-12004-3-12) and

with

12004-3-

the

S)

forward

from end

identification

and p

of

ring

ring Use

and

i

dentificationo

ri ng

ersonnel areao

section with

tag

line

tag

line

platform

in

base

ring

at

to

con-

from

and

of

tee

of

1-

the

Fin

040

1B Disco nnect tee

1

fo

ur bolts, nut

lower t ee br

10

4019 Reposi t i on fork

ers

10

40

p

20

Remo accordan

onnel

ve f orward r i ng sect ion wi

to

ce wi

104010 throu

02

1 Usi ng f ork

104

t o t he groundo

104022 Clean and p

wa

re

in

acc

N

Of,Eg The

points

ri ng se

, t

ctio

ee

bracket f rom

p

late~

ackets

I -

th the

gh

lif

t t lower transportatio

reserve ordan

f orward

bra

t o

lif

t, rai

beam Noo 30 (See f

applica

10401So

f orward

ce wi th

end of

cket s

and nut s

the grou

se transportation

bl e proc

ring comp

paragraph 4020

the booster

at

I -

beams Noo

n wi th Fi n I iden

I ~Bea

ms

N

oo

6 and 7 by remov ing

at

eac h t

nd

0 (See figure 210)

igure

th Fin IV

19,

identificati on

edures

n ri ng pl a

onent s and attachi ng hard-

i s now

l~ 2

~

tificati

ono

Tee

ee

bracket and

r i ng

platform

step

20)

out

l i ned i n

tfo

rm and

resting on t

and

8,

of· the

bra

cket s

and

in

paragr

personnel

hree

forward

at

I -

beams

aphs

GEORGE C.

PROCEDURE

10

5

MARSHALL

EP

-141

1040

23

~ova

1

0501

1

050

2

SPACE

Noo

t he

FLIGHT

OF

2 and 8 four bol

CENTER

147

are still

t s throu stalledo Tee bracke disconnected

li

fti

ng forc

Move or

l

ri ng de

equ

ivalent~

P

rocedure

Position

above t

he

removal

Us

i ng

mobile form and p rear ring so position fo i

dentifica

p

latform

until

es

obt ai nedo

tails to

a

nd cover

Rear Ri ng Se

mobile c

rear rin

of

al l

rear ring se

c

rane

ers

onnel on t hat

r removal

tio

no

, complete

conn

ecte

gh

t he i r base

t at I-beam Noo

erection cabl

adequate

with a ta

ctions (J

rane

go

so

The

that

cra

ctio

~

raise and pos

top

of the bo

the

platf

orm i s

of the

(See figure

the follow

d t o the I-beams

to the r ing sectio

1 is i

es are

ntact and.

conne

cted

storage area, place

rpau

lino

the

ne

-AF-120

boom

04-2-0)0

two crane

can

now

hooks

ns o

ition

t he

hor

oster just forw

resting firm

rea

r ring section

40

) Worki.ng .from t he

i ng procedu

res

g

and hav e two

n s

will not

and s

lig

on cro

are direc

be

maneuvered for

izo

ntal plat

ard

of

ly

in

pr o

with Fin

hor

izo

till

ht

ss ties

tly

-

the

per

III

nt al

of

in-

be

,

10503

'1

0502. 1 Conne

ct

with Fin

(See figure 5j det

1

050

202 Lower C

l.i

nes 0 Conne

et s and

re

f'igu

1050203 Disconne

se t screws and rem

60

)

Us

i ng

fork platform at outriggers transportat to

remove

10

5030

1 Disconne

lif

tj rai

and p

ersonne Noo 4 a

ion ring pla

rear

e

ach

ri ng secti

rin t ee

r i ng handl

III

iden

rane

hooks t o wo

ct

put sli

5 s detail

ct tee

se

bracket

and pos l as necessary nd

60

tform9

ct

tee

bracke

g by remo

bra

cket

ing

tificatio

ail

cho

ker

ght

Ao

ovi

on

with

ving

to

bracket s

Ao

)

rk lin

tension

n

area es

to

with bolt

and conne

to rin

on

crane cable

rear ring se

g handling

)

f rom

ng connec

ition

(See figu

complet e the

t s at

four bolt

the

outrigger Noo

tin

g pino (See figure

the tra on

re

nsportatio

each

side

40) Working fol

Fin

III ide

out

ntificationo

r i

ggers Noo

s and wash

ri ngo (See figure 60)

ction

s a

nd

nut s o

ct

to

chok

er

brack

-

s o (See

5 by

loo

sening

n ri ng

of

t he boo

fr om

ster

the

lowing procedures

4 and 6 f r om

ers through

1050302

Remove t he 4

oles of

h

each ring sec

1/2-inc

h screws

(J-AF-12004-2-1

tiono Insert these

8) fr om end

scre

ws

in

holes

screws

to

disconnect

NOTE

~

One 4 l/2-inch

locator

of

each are rear

ring and sections

(A-AF-

ring

connected

ri ng and one at

each

locators

.

PROCEDURE

on

opposite

pull

locators

position.

side

of

(A-AF-l2004-2-l4)

(See

figure

screw (J-AF-12004-2-1B) and one

l2004-2

section;

, one

-l4) are located therefore,

screw

is

on

splice joint.

(A-AF-12004-2-14) remain

ring

sections

and

to

tighten

the

6.)

in

the

end

hole

on

when

the

forward

aft

side

ring

side of

sections

of

the

rear

Screws (J-AF-l2004-2-1S)

with

the

ring

the

1.504

1.50303

Disc o from

nne rear

removing

(J

-AF-12004-2-l7)

(See figure S

r i

gger

1050304 Connect

iden

tifi worki ng men

to (See figure 50)

105

0305

Disc onnect r i ng

t i on

with Fin

l i nes from mobile c

1050306

Us

i ng mobile

personnel

Us

ing fork

fo

rm

and p

r i ng sectio

Worki ng from

fol

lowi ng proc

lift,

ersonnel to

n wit h

the transportat

edures

ct

rear

ring

two

barrel

for identificat

numbers.)

tag

line

cation

and hoi s t

areao Use

III identification

crane~

to

the

raise

and

a he i

Fin

IV

g

r i ng secti

sections

nuts

at each

to

rear

on

at

(J-AF-12004-2-6) and

end.

ring off

tag

line

handling

rane

hooks.

lower

brackets

horizontal

ground.

position ght

as

necessary

identificationo

i on r i ng pla

with

Fin

III

outriggers

(See

i on

of

section

of

booster

No

figures

finglines

with

to control

from

and remove

platform

transportation

for

(See

figure

tform, complete

identification

o 4 and 6 by

six

5 and

and

Fin

III

and

lower

swinging

rear

move

ring secchoker

and

ring

removal

platof

40) the

screws

6.)

out

-

into

~

rear

1050401 C

with Fin IV i den

fi

05040

1

2 Using

work

1050403 C

ri ng secti

onnect

gure 50)

mobile crane

area

onnect

r i ng handling

brackets

tificatio

with tw

and

connect

to

choker lines t o

on

with Fi

n IV i den

to

rear

n with bo

lts

o hooks , lower c

choker

ring

lineso

handling tific

ation

r i ng

section

and

nuts.

rane

brackets

and

put

(See

hooks

on

rear

slight

to

PROCEDURE

t

ensi

on on

crane

cableso

(S

ee

figure

50)

1050404 Di

sconnect

r

igg

er

Noo

Rem

ove t

wo

r i

gger

Noo

N

OTEg The rema

tee

bracket

until

forces

erection

are

1050405 Disconnect

by

performing

paragraphs

1 050406 Connec t

Fin

fo

er

rk

1050407 Low

ing

1050408 With

lift of

crane

tag

IV

identification

personnel and transporta

lift

rear

personne rear

boo

ster

0 (See f

tee bracke

7 by removing

bol

t s

only

80

(See

ining two

at

outrigger Noo 8 will

cables

obtain

ed from t

rear ring

the

applicab

1050302

lin

and

ring

and '1. 5

e t o

clear section f

l positi

r i ng

section with Fin

and l ower

igure

t fr om

rear ring

four bolts f r

f r

om

base

of tee bracket

figure

60)

bolts through t he base

remai n

are

connected

he

service structureo

and slight

section wi t h Fin IV

l e

procedures

03030

low

er

end

of

rear

(See f

igu

re 50)

t i on r i ng

immediate area

ree

of

preparatory

boostero

oned to maintai n a

IV

identificatio

into working area

50)

section om

base

at

of

at

of

installed

lifting

identification

outlined

r i ng

sec tion with

platform

to

taut tag line,

n

wit

h m

obile

outteeo

out-

t he

in

with

hois

free

t-

10

50409

105040 10

Disconnect ring

section

Positio pla

disco

and remove choker l

n f o

t form and

nnect

(See figure 199 st ep 30

1

05040

11

Thread a rope t of

tee

brackets

ropes t o

10504 . 12 Loosen set

riggers No.6

105.4013 Lower t gr

ound

ransporta with fork

handling

rk

lift~

per

sonnel

tee brackets

hro

at

mobile

scre

crane hookso

ws and remove co

and 70

tio

lift

bracket s from

ines

ra

ise the

to a height

fr om

out

ugh the

l~i

nch

out riggers Noo

Low

er tee bracket s t o t

n r ing

platform

0

rear rin

f r

om

mobile

t ransp

or tati on r

as nece

riggers Noo

diamet

6 and

er holes

70 Attach

nnecting pins

and

personnel

cran

ssary

6 and

at

he

g

e hookso

ing

to

70

in

outground.

to the

base

105.5 Using

and

personnel

section

Working from

following

1

05050

050

105

fork

lift,

to a height

with

Fin the

procedures

1 Connect

with

Fin

figure

raise

II

identificationo

transportation

g

ring

II

identification

50)

2 Using mobile c

to

work

5. )

area

and

position

as

handling

rane

with

and

connect

transportation

necessary

ring

brackets

two hooks, lower

choker

for

(See

platform,

to

with

removal

figure

rear

bolts

lineso

ring

of

rear

19,

step

complete

ring

and

nuts.

crane

(See

sec

figure

platform

ring

3.)

the

tion.

(See

hooks

105. 503 Connect

ring

section

tension

1050504

10

50505

1050506

1050

Disconnect outriggers of

Disconnect by perfoTming paragraphs

Connect

Fin II ident

507

I

nsert section and

bolts

NOTE

at erection are

each

secure

0 (See

~

The

outrigger

obt ai ned from

choker

on

crane

tee Noo

tee

rear

1050302

tag

two

barrel

with

tee

two

cables

lines

with

brackets 2 and 3 by removing

bracket

the

line ific

ationo

Fin I identification

bracket

figure

bolts

Noo 2 will

are

Fin

cables

o (See

ring

applicab

and

to

lower end

nuts

70

through

connected

the

to

ring

handling

II

identification

o (See

from

rear

figure

section

with

l e

procedures

10503030

of

(See f i gure

(J -AF-12004-2-6)

to

rear

)

the

remain

and

service

structureo

figure

ring

four

60)

Fin

(See

rear

50)

at

outrigger

ring

section

base

of

installed

slight

brackets

and

put

50)

section

bolts

II

outlined

figure

ring

in

the

at

identification

70)

section

rear

with

~ee

until

lifting

on

rear

slight

at

base

in

with

ring

No.

2

two

bracket

the

forces

105050

8 Lower

1050509

personnel

f o

rk

lif

hoisting

Wi

th

pers

l i

ft

rear

of boost

crane

. (See

and

transportati

t and cl

rear

onnel posi t i oned

r i ng

er

and low

ear

r ing

section

figure

immediate

section

er into

50)

to

with

working

on

ring

area

preparatory

free

of

booster.

maintain a taut

Fin

II

identification

area

platform

with

mobile

tag

with

to

line,

free

GEORGE C.

PROCEDURE

MARSHALL

SPACE

PAGE

FLIGHT

CENTER

64 OF 147

10505010

Disconnect section hooks 0

10505011

Perform 10504010 outriggers

10505012 Lower

fork transporter.

1

05050

13 Cl

ean

hardware

NOTE~

three ring Noo are two section and

will connected the be

towed

ring

and remove

applicable

through 10504012

Noo

personnel

lift

and

clear

and

preserve

in

accordance

The

aft

points,

seGtion

2 and 8 still of

the

with

at

co

nnected

four

still

not

be

and

slight

service

struoture.

into

positiono

handling

choker

brackets

lines

procedures

to

3 and

end

tee

4.

and

transportation

t he

rear

with

of

the

brackets

area

ring

paragraph

booster

Noo

Fin I identificationo

outriggers

to

bolts

installedo

Noo

their

through

Tee

disconnected

lifting

Transporter

from

rear

from mobile

outlined

remove

preparatory

tee

ring

in

paragraphs

brackets

platform

to

components and

4020

is

now

resting

1,

2 and

S,

Tee

2 and 8,

outrigger

their

bracket until forces

respectively, beams

base

to

Noo 1 is

erection

are

obtained

is

now

ring

crane

moving

attaching

on

of

the

brackets

and have

the

ring

intact

cables

from

ready

from

with

rear

are

to

20

ERECTING

201

10505014

Move

cross

BOOSTERo

Positioning

20101

Using towing 5 24,

Transporter

is

directly

step 10)

20102 Using mobile

platform on

pIa

20103 Lower

connect

figure

is

tformo

aft

cable

aft

110

20104 Using mobile

from

boostero

ring

ties,

tractor,

under

crane,

stable

details

and

the

place

and

or

Attaching

position

to

equivalent,

bridge

horizontal

outrigger

assembly (D-I0423292)

cable

crane,

assembly

remove

to

horizontal

adequate

and

Cables.

transporter crane

40-ton

platform

Noo 5

outrigger

storage

cover

so

blocko (See

is

accessible

with

40-ton

Noo 5 as

platform

area,

place

on

with a tarpaulino

that

outrigger

figure

on

booster

block

shown

and

personnel

so

to

personnel

and

in

that

Noo

PROCEDURE

EP-141

PAGE65

OF

147

SERVICE STRUCTURE

+--H'-I+------BRIDGE

JI\'4HI!IlE'!IINt---H--+t------4

MIN.

HOOK

160 FT.

0-

TON

CRANE

HEIGHT

FROM

BLOCK

GROUND

SERVICE

STRUCTURE

--

off

.-..--#'#---BRIDGE

\tW1----

40-TON

CRANE

BLOCK

ERECTING

(J-10423194)

SUPPORT

HOLDDOWN

TOWING

BEAM

ARMS

ARMS---~~~~~~~~:...J~

TRACTOR

(M-26)

---«

......

.

I,~~

'

HORIZONTAL PLATFORM

(J-10426476)

STEP I

ATTACHING

AFT

I-

BEAM

CABLE ASSEMBLY AT

NO.5

N';~'F--+t------AFT

/joIf--

TRANSPORTER

CABLE

ASSEMBLY (0-10423292)

- MOBILE CRANE

SUPPORT

60-TON

ARMS

BLvL"-_

ERECTING BEAM (J-10423194)

-----~m-!:::::::::::=--:--b)::::~::1t

HORIZONTAL (J-10426476)

ATTACHING

PLATFORM

STEP

FORWARD

ERECTION

2

SLING ASSEMBLY

BEAM

l----EiATURN

BOOSTER

TO

FIG.24

ATTACHING

AFT

AND

FORWARD

SUNG

ASSEMBLIES

2

0105

Us

i ng

towi

t

er

en boest

ble

ck

ef briage craneo (See figure 2

NOTE

g Al lew sl ack mevement al

ready

been

ng

tracter

er

i s directly

of booster

cennectedo

~

back transper t

benea t h and

te

be rele

wit

h t

ransport

ased

er

49

by 40 er

as a

until secen

~

n

l i

ne

wit

step 20 )

-te

n b

leck te

ft

cable

d st age adaph 60

-te

n

perm

it

assembly

has

20106

20107

2010S

09

201

2010

20

1011 Us

Us

ing mebi le secend stag assemblies (J-I

Att

ach two lines

by

me

n en t

ada

ptero

Grane

e adapt

042666S)

he grou

er

to

~

nd

posi t

her

Untie forward sling asse

(J-I042319

te

ere

cti

4)

with 60-ten

ng

beam

. (See f i gure

Using bridge crane ~ slo

tens

estab

ion is

l i shed betwe

exer

ted en forw

en

beam weldment (3-1

sling assemblies (J-I042666S

10

Remove m f erward e

ing

sh

own

boes t

obile

nd

towin

g tractor9 position transporter

in figure

er

in rel at

crane

ef t

~

rans

perter

269 st ep ion

to 60 and

ien

her

izon

in

pos

itien

as shewn

izontal platfe

in

o

rder

to

mbly

cabl

bleck

o Att ach f erward sli

250

wly raise

ard sling

t al pla to attac in

figu

rm and mai

avoid

es; lew

)

60~to

assembly and

h ferw

re 249

damage

er

n

blo

tfe

ere

ck unt i l slight

0426675) and forward

)0

herizont al platferm, and

o

and bo

10

(See

40~ t

figure

on

27 fer pes ition

heoks o)

rm

i n frent

ard sli

ste

ntain

to

sec

ng

p 20

tau

ond s tage

cting beam

ng

assemblies

contac

t i s

persennel

ester

as

ef

t l ines

fr em

of

NOTEg During thi

60- t on bloc

crane unt

k and t aken by the 4

il

201012 With transpor t

t he

er

s movemen

booster

in corre

check al l wheel s en t rans

201013 Using ferk lift9 rai

te

201014

t he nece

ri

gger Noo

NOTEg Tag appreximately

Lewe

r t

and move fork

t he

area

rans

o

ssar

y height and att ach t we t

3 and

lin

per ta

70

es are

75

feet

tion ring platfo

lift

se tra

(See f

to

len

and t

t s

lack

0-ton

is in

ct

lift-eff

porter

co~rect

o

nspo r t

igu

re

be

I-inc

go

ransport a

will

have

block

te

fr em t he bridge

lift-off pos

pesitien

ation ring pla

ag

lines

269 st ep

h diamet

rm

and p

tien

lo)

er

hem

ers

onnel

r ing platfe

be let

~

le

tfo

ck

rm to

iti

ono

brakes

and each

by the

and

persennel

eu~

p r ep99 lOr equa1

te the greu rm clear

of

1

nd

GEORGE

PROCEDURE

C.

EP-141

MARSHALL

SPACE FLIGHT CENTER

PAGE OF

68

147

ERECTING

(J

-10433194)

FORWARD

ASSEMBLY

BEAM (J-104266751

BEAM

SLING

(J-I0426668)

WELDMENT

--~

\~~--

-

60HOOK

TON

BLOCK

CONNECTING PIN-__

~

_

TYPICAL

TWO PLACES

FIG. 25. CONNECTING ERECTING BEAM

ERECTING

(J-104231941

ly

L--

Ir

---

CO

BEAM

TT

E R

A

AND

FORWARD SLING ASSEMBLIES

PROCEDURE

EP-141

PAGE

BRIDGE

CRANE

~~~~~ij~~~~~~!!!!;~iii=~'~'---SERVICE

STRUCTURE

SET

SERVICE

SCREW

STRUCTURE----.

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PRIOR THE BOOSTER IN

THE

TO

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BLOCK

BEAM

TRACTOR

THE

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THAT

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STABILIZING BOOSTER PREPARATORY

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THE

TEE BRACKET. SEE

FROM

FIG.26 LIFTING

THE TRANSPORTER. STABELIZE

THROUGH

FIGURE

OUTRIGGER

14.

STEP I

BOOSTER

1.J:(JtItii~~~+---AFT

(0-10423292)

SEE

FIGURE

TRANSPORTER

NO. I IS

TO

LIFTING OFF TRANSPORTER

OFF

14

FLOATING

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CABLE

SATURN

ASSEMBLY

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60-TON

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(J-10423194)

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PROCEDURE

2.2

Removing

NOTEg must forces the

Booster

Prior

be

obtained

should

transporter

2.201 Using

personnel forward

2.202

Remove each

2.203

Remove 2 and

platformo

2.204

Lower Move

clear

from

Transporter

to

the

following

from

not,

or

fork

the

howeverj be

cause

lift

j

to a height

ring

at I-beams

two

boltsj

tee

bracket

four

bolts,

80

Remove

transportation

fork

of

lift,

area

o

and

proceduresj sUbstantial

bridge

to

great

binding

raise

of

transportation

necessary

Noo 2 and

and

key

retaining

at

I~

beams

nut

tee

plates,

brackets

ring

platformj

transportation

Positioning

support

enough

the

hardware

to

80

Noo

2 and

and

place

ring

on Launch

the

boostero

to

lift

the

yet

to

ring

platform

disconnect

screw and

tee

key

80

nuts

from

on

transporation

personnel,

platformjl and

Pedestal.

lifting

The

forces

lifting booster be

removedo

and

brackets

from base

each I-beam

and

tee

bracketso

tee

brackets

from

No

ring

of

o

2.205

2.2.6

20207

2.?.8

2.209

2.2.10

202011

Remove tee

Remove

Remove fication

Remove in through

Using as

8

of

Remove Noo

Disconnect set

four

bracket

four

Bal-lok

tee

fork

necessary

rear

two

bolts at

bolts,

tee

bracket

and

bracket

base

lift,

ringo

bolts

I -

move

pin at

of

tee

on

each

2 and 8.

tee

brackets

screws and removing co

and

key

beam

No

o

nut

plate

from forward

tee

bracket

and

loosen

outrigger

bracket

Tai

se

transportation

side

through

base

from

retaining

10

and

j

ring

clear

the

No

. 1

are

to

of

the

of

outriggers

nnecting

screw and

nuts

section

of

forward of

rear

remain

ring

booster

each

tee

pinso

from I-beam

with

area

o

and ring fixed.

platform

at

outriggers

bracket

2 and

No

o

key

from base

Fin I identi-

aft

set

.

The

and

at

8 by

of

NOolo

screws

set

screws

personnel

Noo

2 and

outriggers

loosening

202012

Place

tee

personnel

clear

immediate

brackets and

transportation

area

on

transportation

near

rear

ring

platform

o

platform

with

fork

o Lower

lift

and

NOTE

~

The

ti

me for t

er

boost portero

t

he booster

pin through out

he

purpo

se

in the

The

t ransport

i n outr i

has been

r i

of

us ing er befo

gger

hoisted

PROCEDURE

gger Noo

it

as

re

it

Noo 1

clear

1 i s not removed at

a gui de

i s

will

of

t he t

to stabilize

hoisted from the trans

be

removed

ransp

or tero

aft

thi

t he

er the

s

-

202013 Have

ment

through out

in the tee t he t notcho (See f i gure 140)

202014

Wi t h bridge si mult aneouslYj hoist boost co

ndit

20)

NOTE of

202

015

Using

2

02016 Us

i ng

t o a

bl i

202

017

Remove connecting

t o out r i

men hold

of booster

ransp

i on complet

g Boost

the

f orward and

towi fork

he

i ght

es

o

gger Noo 1 if

each

of the

fou

o (See figure

rigger Noo I as a gu

bra

or t

cket

er

cran

at outrigger Noo

so t

he

i s float

e 60-ton bloc

er off transp

ely clear

er retai ns i

ng

tractor~

lif

t~

raise transp

rear rin

of t

ts

hor gs rema

remove t

necessary for inst

fr om outr i cond

itio

r t

ag

269 st

ide

lines

ep

in rel at

19

ing i n t he cent

t o

1.0

stab

preven

)

Us ionshi p iliz

t undue move-

i ng t he p

to the notc

e the boost

er

of

k and 40- t on block lifting

or t

er

i n its st

ransp

izo

ransp

or t at i on r i ng pla

alla

or ter. (See figure

nt al pos

in

ort

tion

ition

attached

er

f r om fir

of holddown bloc

and l ow

t o t he t

ing site ere

tfor

m and

269 st ep

er secti ransp

gger Noo 1 and attach t

ns

warran

t o

in

h

er

in

the

abilized

ons

or t er o

so

per

sonnel

k assem-

ag line

Low

202018

er trans

Remove fork lift

site areao

202019 Using bridge

it

pos

slack

s t a

CAUTION

iono Use

during

bil

iz8

~

t i on wi

Ex cables from complete

vertical pos

erection cabl e at t hi s po

several degrees

202020 Using

mobile

outrigger Noo 5 and

step

28,

wa

rran

10) A

t o

portation ring pla

and t

ransport ation ring

crane 60- t on

blo

40-t on bl ock

maneuver o

ll

be maint

t reme

care

slapping t

Du

r ing t hi s mov

ai ned by tag

must

he boo

itiono

int let s t

of

arc

o

crane9 raise

disc

tta

ch tag line

hor

onne

tfo

rm

and personnel

ck9 hoist boost

to

stab

ilize bo

emen

Hnes

be

t aken

ster

A

sma

izo

ct aft

to

prevent

as

the

boost

l l a

mou

he

boo

nt al

pla

t fo

cable assembly

outrigger Noo 5

pla

tfo

rm from

er

into ver

ost

er

t 9

additional

0

t he

er

mov

nt of mov

ster

rm

swing

and

to

t he ground 0

firing

tic

al

and take up

rear hoistin

es

to

t he

ement of

the

through

pers

onnel

to

o (See figure

if

condi t

ion

s

g

GEORGE

PROCEDURE

C.

MARSHALL

EP-14l

SPACE FLIGHT CENTER

PAGE

74

OF 147

2.2.21

Lower to

the

aft

cable

202022 Using

launch vertically

2.2.23

Transfer booster figure

2.2.24

Using Line I

2.2.25

2.2.26

Remove

Install

riggers

(D-I0418915) on

300)

horizontal

ground 0

assembly from

60-ton

block,

pedestal

over opening

tag

lines

to a position

28,

step 2.)

tag

lines,

as

shown

tag

lines

outboard Noo 2,

4,

platform

Remove

mobile

firing

hoist

and

move

of

to

personnel

a few

orientate

in

figures

.

holddown

6,

and S and

outriggers

~

personnel,

crane,

site

booter

and

aft

horizontal platform,

areao

to a height

booster horizontally

launch

feet

booster

8 and

block

Noo

pedestal.

on

launch

pedestal

above holddown arms. (See

Fin

Line I

290

assemblies

inboar~

l~

3,

holddown

5,

and 70 (See

cable

assembly

sufficient

to a position

and lower

with

launcher

(D-I0418916)

blo

ck

assemblies

figure

to

on

and

clear

Fin

out-

202027

2. 2028

2.2.29

2.2030

202031

2.2.32

Install

230)

and washers (MS35333-32)

outriggers Retract

support

Ascertain

10)

Using with

eighth

down

bridge

holddown

inch

arm bi

Carefully billet Lock

with

Place support

and lower

the

four

retractable

anvil

inboard

Noo

that

crane

block

above

llets

position

base

of

set

screws,

so

guide

l~

arms

plates (B-I

3,

5~

o

and 70 (See

holddown arms

60-ton

block,

assemblies

respective

o

Adjust

each

booster

each

support

that

suppo

block

until block two

through

arms

it pic

0418920)

at

each

are

uncockedo (See

lower bo

attachedj are

retractab

rt

arms

assembly

weight

assembly

each

in

support

ks

up

the

end

figure

oster

l e

support

as

in

rests

to

its

side

block

using

of

bolts (MS3529S

connecting

300)

figure

until

outriggers,

approximately

arm and

necessary

exact

o

center

of

on holddown armso

respective

of

the

position

assemblies

billet

billet.

and

adjust

.

30

~

hold-

its

-

on

step

one-

202.33

CAUTION~

support Position

(See

figure

Check

arms and

holddown arms

300)

to

that

assure

block

to

that

assembli

secure

weight

es

boost

is

distributed

are

centered

er

to

launch

on

all

in

billet.

pedestalo

PROCEDURE EP-141 PAGE 75 OF 147

rl$~:t--BRIDGE

rrnI~~~

~~--tt--

60-

TON

~m~~~~-ERECTING

(J-10423194)

O-TON

CRANE

BLOCK

BEAM

BLOCK

SERVICE

60-TON

ERECTING

(J-10423194)

STRUCTURt:.--......,f//

BLOCK

BEAM

--~~~~~~r'

114~:'ItitIflt----iJO-llt--

SUPPORT ARMS

HOLDD)(O~W~N~-l~~~~~~~~

ARMS-

r'nK'''~

O~I

DETACHING

FIG.

28

REMOVING

POSITIONING

\zAG

AFT CABLE ASSEMBLY

AFT

BOOSTER

LINES

STEP I

FROM

CABLE ASSEMBLY AND

ON

LAUNCH PEDESTAL

OUTRIGGER

SATURN

AFT CABLE

ASSEMBLY

(J-10423292)

HORIZONTAL

PLATFORM

'

__

BOOSTER

MOBILE

NO.5

CRANE

SUPPORT

HOLDDOWN

ARMS

---.",...,

ARMS-----~~~~~~~~~

POSITIONING

__

"

BOOSTER

STEP 2

ON

LAUNCH PEDESTAL

_

________ ... °

-

--

/

00

FIG. 29- BOOSTER

TO

LAUNCH

PEDESTAL ORIENTATION

DIAGRAM

GEORGE C. PROCEDURE

EP=141

MARSHALL

SPACE

PAGE

FLIGHT

78

OF

CENTER

1

47

1,3,5 AND 7

OUTRIGGERS

4':Jt:':t

':

'(~

A

_. I 0 0

BOLT

~

(MS35298-230

BLOCK ASSEMBLY

(?N~OO~~~15)

HOLD

DOWN

ARM

(10435650)

~..

\~!

'<':\0

I )

/

;,1

(

(I

<

-;;

-:~.A'

GUIDE

\i

~

('0 ' ,

:;,.,

' (B-10418920)

1.1'

;' ',.

.,

-f',' '\ ' : ,0

r

fl

o

!\,

.-----

WASHER

\)

(MS35333-32)

PLATE

'/

GUIDE BRACKET

(J-10435895)

I

OUTRIGGER

1,3,5 AND 7

OUTRIGGERS

HOLDDOWN ARM . 4

(

10435650)

I--_

,_-:--

--I

__

T~Y

.-:...

P~IC~AL

I

fJJ

STEP

~~

~

:

\

rn

~

,

®]

'

~I

'

; HOLD

~

~-

;)

/

,1/1

./

~il

,

~y,:;

Ii)

2

F~UR_~LACES

-

C

~

i 1

/'

•.

;;;.~

/

>

"'

'-

/~/,.

;

:/

HOLDDOWN BLOCK

ASSEMBLY

. INBOARD

. (0-10418915)

2,4,6

OUTRIGGERS

BLOCK ASSEMBLY

OUTBOARD

GUIDE

PLATE

(J-10435895)

AND 8

DOWN

04IB916)

r--

J

l!

__

"

___

..

_.~_

.~~

__ ~ ..

_._

-__

..

_. ____

FIG.30

SUPPORT ARM

(10435500)

___ .. __

...

_ _ ____ _ _ ._

POSITIONING

BOOSTER

ON

SUPPORT ARMS AND HOLDDOWN ARMS

SUPPORT (10435500)

ARM \

-1

,

TYPICAL

_._~

_ ____ ' ____ _ '

"",

'~

FOUR PLACES

___

"'.

' _M_~

rs--

J

__

·

202034

Remove

guide

brackets

from holddown armso

NOTEg holddown

35

2020

Disconnect forward nuts

202036 Using

and forward ponents

202037 Disconnect

(J

nuts

202038 Using

Before

block

and

bolts

bridge

sling a.ssemblies

to

work

beam

-l0427014 and J-l0427097) by removing (AN325-l6 )0 (See

bridge

(10427036), ra.ise

and lower

to

202039 Disconnect and

J-l0427097) from second

Bo)

vehicle

assemblies

sling

that

attach

crane 60-

area

o

weldment

crane

40=ton

beam

work

area

remove

is

to

be

launched~

remove

(D-l04189l5 and D-l04l89l6)0

assemblies

erection

ton

block,

clear

(J"-

lugs

raise

of

10426668) by removing to

second

erecting

booster

(J-l04266675) from mounting

bolts (AN16C-54)

figure

weldment (

o

mounting

stage

20

~

detail

block

and

J-l0426675)

brackets

adaptero (See

two

Bo)

sling

(J-

l04270l4 and

clips

stage

from

adaptero

beam (J-l0423l94)

and lower

com

brackets

and

assemblies

clear

figure

of

20,

booster

detail

-

202040

30

REMOVING Removing

of

erecting

BOOSTER the

installing

WARNINGg extremely

Corect

importanto Lubricating (NAS156-68) and each taining a torque of

the

bolts

during

that

supports strict

removal

upon

replacing

(J-AFA-12053)

the forward end

Install forward

(J-

NO!Eg

ing

the sling

l0426675

The

the

installation

FROM

booster

procedures

forward

from

sling

installation

side

valve

in

mandatory

of

booster

the

original

flight

assemblies

)0

(See

figure 20)

booster

LAUNCH

the

~

paragraph 20 Spec i

assembly

is

now

of

the

PEDESTALo

launch

on

of

forward

the

of

the

washers (

of

6000 to from

booster are of

prevent

to

the

inch

launch

on

the

be

connected

booster

pounds (500

hardware removed

(3-

10426668) and

erected

upper

pedestal

the

shank and

on

the

stages

is

essent

al

care

boostero (See sling

assembly (3-10426668)

threads

NAS143-16

foot

shearing

pedestalo

of

the

It

trans.porter

but

not

from

rotating

for

beam

weldment

launch

pedestal

o

ial

ly

must

be

exercised

figure

of

the

and

NAS143 pounds) from attachment

should

that

be

the

forward clamp

tightened

during

transportationo

installation

await

the

reverse

in

200) is

bolts

- l6C) and the

head

hardware

noted

so

as

also

to re-

of

-

ob-

PROCEDURE

4.

REMOVING DETAILS

RING

AND

SECTION

ATTACHING

WITH FIN I IDENTIFICATION HARDWARE

.

AND

PRESERVING

ALL

RING

4.1

Removing Forward and Rear Ring

Transporter. NOTEg The

are

to

4

.1

.1 Connect

401.2

4.

1.3

40104

forward and

be

removed

after

ring

rear

firing

handling

Fin I identification Position

above Lower

Connect choker tension

Remove from forward bolt

mobile crane so

the

forward

crane hooks

lines

on

crane

two

forward

cradle

(J-AF-12004-

cables

4-33)

(J-AF-12004-4-32)

cradle.

(See

figure

ring

brackets

with

ring to

work

to

support

by removing one

that

120)

Sections

sections

of

the

bolts

that

with

Saturn

to

forward

and

the

two

Fin I Identification

with

Booster o

nuts.

crane

section.

area

and connect

ring

handling

brackets

.

clamps,

reference

nut from each clamp. attach

two

brackets

Fin I identification

ring

hooks

to

section

choker

and

are

put

with

directly

lines.

slight

J-AF-12004-4-0

(J-AF- 12004-

Remove

eight

4-38)

screws

(J-AF-12004-4-31)

from

j

and

to

40105

Using mobile and lower

4.1

06 Disconnect choker

forward

401.7 Connect

ring

identification

40108

4.1

09

Position above

Lower

the

crane

mobile

Connect choker

4.1.10

tension

Remove

on

all

identification

(See

figure

4.1

.11 Using mobile

and lower

crane~

to

the

section handling

with

rear

hooks crane clamps

310)

crane,

to

the

ground 0

lines

crane

ring

to

lines

cables.

that

to

rear

groundo

hoist

and

with

brackets

bolts

so

section

work

to

ring

secure cradle

hoist

forward

remove

Fin I identification

and

that

to

nuts

the

ring

section

ring

rear

ring

o

two

crane hooks

from

handling

o

section

transporter

brackets

with

are

directly

o

area

and connect

handling

rear

ring

brackets

to

section

choker

and

put

with

lineso

Fin

. (Reference drawing J-AFA-12053.)

rear

ring

section

from

transporter

from

Fin

slight

I

4.1012

Disconnect choker

lines

and

remove

ring

handling

brackets

from

REAR

(J-AFA-

RING --- -

12004-

~

2-0)

TRANSPORTER

--

CLAMP(J-AFA-12053)

___

---.1

CLAMP SUPPORTS

(J-AFA-

12053)--_

AFT VIEW LOOKING

FORWARD

CLAMP SUPPORTS

(J-AFA-

12053)---~

ROTATED

90

DEGREES

FIG.

ROTATED

31

REAR RING SUPPORT

90

DEGREES

CLAMPS

ROTATED

90

DEGREES

PROCEDURE

40·2

4.1012 (Con. rear

Preserving

NOTEg The after

disassembly

necessary

40

201 Clean mating

)

ring

Forward and Rear Ring

following pro

o

clamps,

Specification

Military preventive, surfaces

4.202

Clean

attaching

support Federal 302

01

of

P-9

preservat

L~6440

section

with

cedures

and

should

surfaces

and

tee

bracke t s

P-S-66lj in

Specification

Military

0

hardware

clamps,

and t ee

Specificat

Military

Specifica

ive

lubricating oil , Milit

Fin I identification

Details

should

be

repeated

of

forward

with

accordance

MIL

-P-

116 and

Specif

ica

for

forward

brackets

ion

P-S-

66l,

tio

o

and

Attaching

be

performed

at

30~day

and

rear

dry-cleaning

with

apply

tion

MIL-C-16l73~

and

with

dry-cleaning

i n

accordance

as

intervals

ring

solvent,

paragraph

P-3

rear

with

n MIL-P-116 and i

ary

Speci

Hardwareo

soon

sections,

Federal 30201

corrosion

to

mating

ring

sections solvent,

paragraph

mmerse

fic

ation

as

possible

-if

parts

support

of

9

in

MIL

~

TER

EP=141

147

CHAPTER

GENERAL INS

FOR

SA

TURN

S=1

III

TRUCTIONS THE

TRANSPORTER

GEORGE

C.

PROCEDURE

MARSHALL

SPACE FLIGHT CENTER

PAGE

OF

EP

=141

85

147

Paragraph LIST

1 0

OF

ILLUSTRATIONS

INTRODUCTION

DESCRIPTION

1.1

1.2

2.

201

2

203

204

De

. s

cr

i p

ti

Leading

OPERATING

General

02

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Start

ing

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06

Operating the Brakes Tire

INSTALLATION

Installa

01

Removal

02

SHIPMENT

Description

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02

Tie-Down Arrangement

Unloading at

SATURN

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the

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GEORGE C. MARSHAL.L. SPACE

PROCEDURE

PAGE

n'-141

FLIGHT

OF

86

CENTER

147

Paragraph

503

504

5.5

5 0 6

507

5 G B

5.9

Power

Positioning

Electrical Positioning

Lifting

storage

To

Requirements

Booster

and Mechanical Checkout 1

Jacks under Jack Pad

0 0 0 0 0 0 0 0 0

..

0 • 0 0 0 0 0 0 0 0 • 0 0 • 0 " 0 0 0 0 • 0 •

Replace Cradles

5.10 Emergency Use:

50

11

Lubrication

PREPARATION

60

Instructions

OF

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Dolly

DOLLIES

Repairs,

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GEORGE C. MA

PROCEDURE PAGE OF

EP

:..

141

88

14

1

Figure

55

56

57 58

LIST

OF

ILLUSTRATIONS

Title Assembly Packaging Truss

Fixture AF=1

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2004 Breakdown

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ions

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41 43 45

The

primary

for

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cedures

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ves

to sup tains

l y by

tions

paragraphs.

particulars

to

instructions for por t

information for

main l pro Pa dollies gi Paragraph

dol

of

necessary

30 cont

or

removing

5.

contains

fixtures

either

shipping

INTRODUCTION

purpose

the

Paragraph

ains

pertaining

motor

t he

of this

Saturn

of its major components.

for

complete

installation

the shipment

information

and

cargo

freight or

fixture

chapter

3-1 '

transporter

10

cont

operation

and removal

dollies

of ent

for

if stored

t o t he

railroad,

assembly by commercial means .

is

to

provide

o

This

ains a description

Paragraph

and

from

the

assembly

ire

transporter

operation

on a

hardstand

preparation

and

chapter

cont

rol

procedures

of

portable

for

shipment

paragraph

the

necessary

is

presented

of

the

transporter

20

presents

of

t he

transporter

for

installing

fixture.

with

area. Paragraph

7.

Paragraph

cargo

storage

of

a complete

contains

by

information

in

seven

and

operating

.

the

4.

barge

jacks

.

used

90

instruc-

con

~

The transporter

from one

tio

no The

prime mo

sea

t ed hand the

prime mover

location

ver

on

appearing

transporter

o St

eering

each

dolly in

facing

is

specifically

to

anot

her

consists

of

t he t

o

Unless otherwise

t hi s chapt

forward

and

provide

of

ransporter

er

refer

o

designed

complete

three

major

st at

t o t he

to

transport

maneuverability

assemblies

is

accomplished

ed,

the

left

and

t erms

right

the

Saturn

and

is

by

two

left=hand and

of a person

booster

at

each towed by a operators,

loca

right

seated

=

one

=

in

GEORGE C.

PROCEDURE

MARSHALL

SPACE FLIGHT CENTER

PAGE

OF

1.

DESCRIPTION

10

1

AND

LEADING

Descriptiono

PARTICULARS

o

GEORGE C.

PROCEDURE

MARSHALL

EP=141

SP

91

147

10101

The Sat

Boost

t

wo dollies whi ch i s t

Becau

t he onl y removal and i nst

for shi

t

ransporter

101

Each

2

0

assembly hydraul by

an

101.

3 The frame and

consisting

beam. Each walki

equi pped with a cas t si on t owing. (See

1.1

.4

The

opera Power wh

i ch ut

generator

ar

st

engine

obtained

The

cont

(f i

gure

power un

harge

c

nect ed from t he voltmet

battery

limit switches,

preven

eering

st

urn

8=1 transporter

er

consi st s

se the Sat

mention

pmen

t by

when

of

t he dolli

, drawbar,

i c

system

ai r

over

of a left=hand walki ng

is used

t o connect t he tran

24-volt DC

t e

an

elec

is

supp

lie

ilizes

is a seri

t t he

gasol

i s

operating.

from t

pow

er un

it

rol

panel, 34 ) , it.

or

A

t he batter er

loca

voltage

t t he

cont

hydraul

rols

essentially

owed

urn

Boost

of

allation

er

t he assembly

of

commercial

complet ely assemb

es

is composed

an

operator

. (See f i

hydraul

runn

i ng

ng

beam has t

i c

gear

brak

gure 34.)

er wheel t o

figure

elec t ri c mot

35. )

t ri

cal

system

or whi ch

utilized

of by a prime mover . (See f i gu is

assembled on

t he dol l i

carrier

is sea

i ng assemb

wo

t o t

ranspor

an

assembl y

fixture will

es

and

o For

led

and

of

a f r

ame

t , a st

Braki ng a

system ly

beam

is

.

an and a

wheelso suppor sporter

t i

t o t he pri

(figure

drives

t he

d by a power unit, Model No. 0

a gasoline engi ne t o drive a

es=shu

i ne engi ne and wo

12=

may

be star t ed

nt wou

as a generator

Pow

er t o star t t he

vol

t st

orage batterie

and

nd

uni

t, acti

st opped from t he

located on t he operatoris cont

from t he generat

reverse cur

ies

sys

t em when t he

as ne

r ent r e

cessary

t ed on the elect

when t he batteries l ocat ed on t he

i c

pump mot

are

in

t he

or

cont

rol

lay

enables

o The batteries

dolly

rical

i s not

cont

are

connect ed.

operator

or

from

HOLD

opera

position

rol

' s cont

t t he

fixture

the

assembl y f i xt

be

during

dimensions

loaded,

and

running

eering

cti

Saturn

suppor t ed

re

dur

i ng t he

preparation

of

t he

see

figure

gear

system,

on

is

provided

32

and a

all steel structure

right-hand walki

The

drawbar

to

The drawbar exten-

36 )

provides

hydraulic

6AK

=224RV/1658E,

me

is

mover

pow

pumps

er t o

.

generator. The ng

as a motor

when

gasol

i ne

t he engine

s connect ed

rol

assembly

panel,

t he

loca

generator

elec

t o

gasoline

is

in

series

t ri

cal

t ed on t he

can be di

in

useo A

panel i ndi

DC

cates

Pump mot

rol

assembly,

t i

ng

when

the

o

0)

ure,

33

ng

for

t o scon

or

by

0

.

=

1.1.

5

The

fron

(figures

st

eering

such

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locking

Normallyy all

rating

ope

t do

lly

and r e

37 and 38) provi de

t he

dollies

allow

t o be st

eered

of one

four

pressure

or

wheel,

wheels for each

ar

dolly

each operator wit

independent

t he

rear

locked

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independently,

are steered

system

hydraulic st

ly

0 The

system

wheels and

ly;

is not

simultaneously

is

1500

eering

systems

h a means

is

fron

t wheels of

however, st

possible

psi

.

Th

of

connect ed i n

each

eering

.

. Normal

i s

pressure

GEORGE

PROCEDURE PAGE OF

C.

MARSHALL SPACE

EP-141

JL

FLIGHT

92

SATURN BOOSTER

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147

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PROCEDURE

MARSHALL

EP-141

SPACE

PAGE

FLIGHT

OF

96

CENTER

147

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INDICATING LIGHT - 24 VOLT - AMBER

"OFF" -WHEN "ON" -WHEN

- DOUBLE STACKED - HAND

RELIEF

VALVE

LOCKED IN

UNLOCKED

-'SOO

LOCKED IN

WAY, OPEN

PSI

SETTING

CENTER

OPERATED

PROCEDURE EP-141

PAGE

101

OF

147

CYLINDER

CYLINDER NO. 1

STEERING CONTROL VALVES (CENTER-LOCK) -

U - UNLOCK L - LOCK

o - OPEN

STEERING CONTROL VALVES (RIGHT

L -

LEFT R - RIGHT U - UNLOCK

CENTER

STEER

(HOLD)

NO.2

(HOLD)

AND

LEFT)

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FIG.38 REAR DOLLY STEERING SYSTEM

PUMP

t

NO.1

PUMP

.....

NO.2

PUMP

+-

- -

t

NO.3

PUMP

NO."

t

INLET

-

/ STEERING CONTROLS

REAR

Q SWITCH - INDICATING LIGHTS

II

...

)J,...

~_u~

INDICA TING LIGHT - 24 VOLT - GREEN

~

.'

~

"ON" -WHEN

INDICATING LIGHT - 24 VOLT - A.YBER

,

"OFF" -WHEN "ON" -WHEN

CONTROL VALVE - 4

DOUBLE STACKED - HAND

RELIEF

CHECK VALVE

VALVE -

LOCKED

LOCKED IN

UNLOCKED

WAY,

'500

PSI SETTING

IN

CENTER

OPEN

CENTER

OPERATED

is

obtained

from

motor o These

center=lock

Ro

tat

ion

t o t

he steering wheels. be

applied

tion

of

pressure

center

position

cont

of

t he s'

Ro

tat

to

pressure

allows

four

pumps

rols are

teering

cylinders

ion

of

or

rsleased f

unlocks t,he when

GEORGE PROCEDURE

hydraulic pumps,

operate

only

rotated

c;ont

rols

(figure

t he

cen

't'

er~lock

rom

t,he

t he

steering

cyH

nder

s t o mechani,::ally

t he wheels

are straight

C.

MARSHALL

driven

when

t he

out

of

their

allows

34),

causing

cont r

center-lock

cylinders

by one

steering

HOLD

pressure

movemen

ols

all

pi

lock onl y i n t he

o

SPACE FLIGHT

PAGE

1

03

OF

147

electric

controls or

positiono

t o be

applied

t of the

ows

pressure

ston. Applica-

and

rele

ase

to

of

10106

1 02 Lead

102

The

brake

Normal

air

suppl y

auxiliary

has an ently mover

individ

of

.

ing Parlliulars

01

The

leading

porter

are

system

(figure pressure for for

t,he system

source

ual

when

braking

the other;

o

part,iculars

cont

ained

however,

in

--------------------------------._------

TRANSPORTER

LENGTH (Ov

(Be

HEIGHT

(Loaded)

era

11)

tween

.:)

0 0 0 0

Sllpp

I)

r)

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TABLE

orts

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(l

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{}

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()

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)

~)

I)

0 0 0 u 0 0 0 0 0 u V

(; 0 ()

0 0 0 0 0

(1

39)

is

an

t he

system

is

furnish

loading

on

barge wit h wincho Each

system which can be

both

may

for the rnajor Table

IIo

PARTICULARS

\}

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() 0 ()

n

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air

over

is

from 90 t o

ed by

be

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<)

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000

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hydra

the

prime mover operated

operated

ents

I)

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f)

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ulic syst

100

psi.

independ

from

of 'the

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o

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or

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re Diameter)

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GEORGE C.

PROCEDURE

MARSHALL

EP=

141

SPACE

PAGE

FLIGHT

OF

1

04

CENTER

1

47

TREA.D

WHEELBASE

TIRES

TIRE

PRESSURE Front Rear

ELECTRICAL

OUTPUT V OLTAG

POWER

GASOLINE

OIL

oo()oa

TABLE

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0

o 0 0 0 0 0 Q 0 0 0

0000000000000000 0

11

0

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II

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0 0 0 (. 0 0 0 u 0 0

(Loaded)

Tires

SYSTEM

UNIT 0 0 0

00000

oooco

0

00000000000

o 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 '

0 0 0

00000000000000000000

E 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 a 0 0 0 v 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 a 0 0 0

0000

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x 16, Type

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60

Plus

80

+ PSI

coo

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Regular

er

grade,

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00

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ylon

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t s

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en

omotive

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BATTERY

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HYDRAULIC

OPERATING

TESTING HYDRAULIC HYDRAULIC

AIR

OVER

NORMAL HINIMUM

BRAKE

DOLLY

0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 a 0 0 0 0 0 0 0 0 0 0 0 U 0 0 0 0 0 0 0 0 0 0 0 0 0 0 0 2

MOTOR

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SYSTEM

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PRESSURE

PRESSURE FLUID 000 FLUID AIR

LEVEL

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00

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M=

26A

1

PROCEDURE

EP-141

PAGE

105

OF

147

AIR HOSE

ASSEM

BLY

LOCATED

ON

FRONT

DOLLY

LOCATED

ON

REAR

•

-AIR

~~~--~----~----------~~~--~r----------------;I

~--------------~~------~------.-------------~I

FILTER

SERVICE LINE

EMERGENCY

...-.

DOLLY AIR

TANK

UNE

------1------.4

EXHAUST

. I

I I

..

DOLLY

"

~

RELAY QUICK-RELEASE EMERGENCY VALVE

POWER

FIG. 39.

OPERATOR'S

BRAKE

CLUSTER

AIR

OVER

CONTROL ASSEMBLY

APPLICATION

TWO-WAY

ASSEMBLY (AIR OVER HYDRAULIC)

HYDRAULIC

VALVE

CHECK VALVE

---------

FRONT

BRAKE

-------_

AXLE ASSEMBLY

SYSTEM

----...;.:---...

__

r-------------------l

~-

-

.

-

.-

-- - -

_______

r

....

-

r-------

I

,

I

,

L.

_ _ _ _ _ _ _ _ _ _ _ _ _

REAR AXLE ASSEMBLY

.J

:

I

-----

t

~-~---·-OPERATOR

__

.;;-

__

."./,;

/'

....

's

ASSEMBLY

-

-,

I

.J

CONTROL

2.

OPERATING

2.

PROCEDURES

1 Genera,.L.

.

2.1.1

2.2

Preoperational

2.2.1

Operation

one

operator

assembly

of the t

(figure

independently

Check.

Before

should

operating eit

be accomplishedg

2.2.1.1 Check

2. 2.1.2

2.2

.1.

2.2

.1.

Check ba

3 Check t o

t o

battery

4 Check battery

elec

on read

2.201.5

Check of

hydraulic flui

I

I.

ransporter

seated

on

each

40). Each

of

t he ot

el

ect ttery for

t r

i ng should be at

hydraulic

her

o

her

of

t he

rical

wiri

proper wate

se

e t hat battery box connec t

vol

tage r eading on

ica

l cont

r e

rol

servo

d. For

is

performed by t dolly dolly

dollies

ng

for

at

the

is

operated

, t he

damage and

r l

out put

operator's

evel

cables

ions.

DC

pane

l.

(S

ee

least 22 volts DC

i r (fi

prop

gur er

e 3

lev

wo

operators,

control

separately

following

and

checks

security.

.

are

connect

voltmeter

loca

t ed

fi gur e 40.) Volt

.

4)

for

el ,

proper

refer

t o

level

Table

ed

age

2.2

.1.

6

Check

.1.

2.2

2. 2

7 Check t

.1.

8

for

Drain

corre

2.2.1.9 Check proper level Table II.

2.2.1 .10 Using

ai r

lines

2.2

.1.

11

Check releasing

2.2

.1.1

2 C

heck dolly

CAUTION carry, may

result i f

gasol

i ne and oi l l evel

ires

f or proper ai r

ct

t:ire pressure.

all

condensatio

master

cylind of brake fl

p~im

e

mover

(f i

gure

for

damage and

brakes

for

n from ai r

er

as sour

3

5)

securi

proper

of

uid

for

operation by

in

press

power c

. For

ce

of

leakage

ty .

.

for

proper

g Because

of

lubrication.

t he

loads

t he t

damage t o t he equipmen t and

prop

er

lubrication i s not

power

ure.

tank luster

prop

air

pressure

. V

ransporter

improper

uni

t .

Refer

and a

t o T

ir

assembly

er

level

isu

ally

applying

(See

figure

operation

observed.

able

filters

for

see

~

check

and

is

41

t o

II

.

air

. )

'TJ

~

p

o

."

(TI

::0

~

o

::0

CJ)~

(')

o

Z

-I

::0

o

r

STEERING CONTROL (REAR WHEELS) - STEERING CONTROL (FRONT WHEELS)

" -

..

""

"\,

-

t:<:J

~

I

....

.t--

....

0

00

--'

.t--

-.J

"'TI

r

G'>

::I:

-i

I§

m

::0

»

CJ) CJ)

(TI

~

m

~

CENTER-LOCK CONTROL

(REAR WHEELS) '

FRONT

ASSEMBLY

mp',,

\ J

_

....

CENTER-LOCK CONTROL (FRONT WHEELS)

FRONT ASSEMBLY

e e

@O.

"'

e

\ I

\ \ \

EP-141

14

7

~

"

~~

e

~

~~~

~ ~.

,

e

/l1JJ

, ,

" ,

..

;

,

I ,

Uf

e

FIG.

41.

LUBRICATION CHART (SHEET I OF

2)

GEORGE

PROCEDURE PAGE OF

C.

MARSHALL

EP=141

1

KINGPIN

2-

BRAKING

SPACE FLIGHT CENTER

11

0 147

AND

THRUST

MECHANISM

KEY

BEARING

WHEEL

3

BRAKE

4

BUSHING

5

6

STEERING BUSHING

7

a

BUSHING

APPLICATION

n(

~

IDENTIFICATION

\)

BEARING

CYLINDER

Cn.INDER

SYMBOLS OIL ZERK

HAND

(SEE

CAN

GUN

LETTER

NOTE

4)

TABLE

OF

LUBRICANTS

LUBROICATION

FREQU::::H:~:::SAFTER

~

TYPE

OF

LUBRICANT

EACH

TRIP

SEMIANNUALLY

GAA

HB

1

CLEAN SPECIFICATION

:2

IF

CLIMATE

MORE

OFTEN

WILL

TAKE

3

LUBRICATE

4

RFMOVE

FITTINGS

OR

TO PRE

RE'

.M!!:D

BROKEN

CLEAN

FIG.

41.

BEFORE

p-s-661. OPERA'l'ING

IAL

AND

LUBRICATION

LUBRICATING,

VEN'l' \{EAR

ACTION

ARROVI

REPACK

LUBRICATION

DRY

BEFORE

CONDITIONS

OIt

DETERIORATION,

AS REQ

ITFJ-lS

ON

WHEEL

BEARINGS.

GREASE

MILITARY

HYDRAULIC AUTOMOTIVE

UIRED.

BOTH

IN

STRUCTIONS (SH

AUTOMOTIVE

SPECIFICATION MIL-G-I0924

BRAKE

NOTES

WITH

DRY-CLEANING

LUBRICATING. REQUIRE

SIDES

'IHE

OF

FLUID,

DOLLY

PERSONNEL

DOLLY.

AND

ARTILLERY

HEAVY

SOLVENT,

TO

BE

LUBRICA'l'ED RESPONSIBLE

EET 2 OF

DUTY

FEDERAL

2)

NASA Saturn S-1 Stage, Saturn SA-1 Handling, Transporting And Erection Instructions

Specifications and Main Features

Frequently Asked Questions

User Manual