UNCLASSIFIED

AD 1401 7185 __

DEFENSE DOCUMENTATION CENTERFOR

SCIENTIFIC AND TECHNICAL INFORMATION

CAMERON STATION. ALEXANDRIA. VIRGINIA

UNCLASSIFIED

NOTICE: Ven goverment or other drawings, speci-fications or other data are used for any purposeother than in connection with a definitely relatedgovernment procurement operation, the U. S.Government thereby incurs no responsibility, nor anyobligation whatsoever; and the fact that the Govern-ment may have formulated, furnished, or in any waysupplied the said drawings, specifications, or otherdata is not to be regarded by implication or other-wise as in any manner licensing the holder or anyother person or corporation, or conveying any rightsor permission to manufacture, use or sell anypatented invention that my in any way be relatedthereto.

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CODE IDENT NO. 81205

NUMBER ~ -2~VL

TITLE -JIILV -Lk T~ f~ ATN E I EI -P, ~ IN -UL,

MODEL NO. 4~-133A CONTRACT NO. a'04(694)-107

ISSUE NO. Jý ISSUED TO _________

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TABLE OF CONTENTS

1.0 INTRODUCTION

1.1 PURPOSE AND ScoPC

1.2 ORGANIZATION OF DOCUMENT

1.3 DEFINITIONS

1.4 GENEKAL REQUIRENENTS

1.5 SPECIAL REGUIREMENT3

1.6 EQUIPMENT NOT REQUIRING FUNCTIONAL TESTING

2.0 PROCESSING OPERATION

2.1 CSA ACTIVATION TABLE 1

2.2 PREASSEMBLY TESTING OF OGE AND TABLE 2MGE

3.0 LAUNCH CONTROL FACILITY TESTING TABLE 3

4.0 LAUNCH FACILITY TESTING TABLE 4

5.0 STRATEGIC MISSILE SUPPORT BASE TESTING TABLE 5

6.0 FLIGHT AND FLIGHT-TO-FLIGHT INTEGRA- TABLE 6.TION TESTING

7.0 INTERIM PROCEDURES

iEW VYi . ii., ii 2-9262 VOL.. X. IREV..

S1.0 INTRODUCTION

1.1 PURPOSE AND SCOPE

THE PURPOSE OF THIS DOCUMENT IS TO SPECIFY THE ACCEPTANCE TESTS

REQUIRED FOR THE CHECKOUT OF EQUIPMENT A5SEMBLED INTO A MINUTEMAN

MISSILE SYSTEM BY THE bOEING COMPANY AT WARREN AFB PREPARATORY TO

THE EVENTAUL ACCEPTANCE OF THE FLIGHTS, SQUADRON & THE ENTIRE WING.

PROCEDURE DOCUMENTS REQUIRED FOR THE CERTIFICATION OF ASSEMBLY AND

CHECKOUT (ACO) TEST EQUIPMENT AS WELL AS THE DOCUMENTS REQUIRED

FOR CHECKOUT OF OGE AND MGE EQUIPMENT ARE CALLED OUT HEREIN.

1.2 ORGANIZATION OF DOCUMENT

THE INFORMATION CONTAINED IN THIS DOCUMENT ýS CATEGORIZED AS TO

TYPE AND PRESENTED UNDER MAJOR PARAGRAPHS AS FOLLOWS:

PARAGRAPH 1.0 IS THE INTRODUCTION AND THE SUB-PARAGRAPHS UNDER IT

CONTAIN THE DESCRIPTION OF THE PURPOSE AND SLOPE Oý THE DOCUMENT,

DEFI I TION OF TERMS PARTICULARLY APPLICABLE TO IHE ASSEMBLY AND

CHECKOUT TASK, THE GENERAL REQUIREMENTS CONTAINING GROUND RULES

GOVERNING DURING THE CHECKOUT PROCESS, AND THE CONDITIONS THAT ARE

APPLICABLE DURING TESTING.

THE RLMAINING MAJOR PARAGRAPHS CONlAIN TIHE VARIOUS tABLES IN WHICH

THE RLQUIRED TESTING AND DOCUMENTATION IS IDENTIFIED. THE TABLES

CONTAIN EACH TEST TO BE PERFORMED AND IDENTIFY THE PROCEDURES TO BE

USED.

PARAGRAPH 2.0 CONTAINS TABLES 1 ANo 2 WHICH COVERS ALL THE TESTING

AND DOCUMENTATION REQUIRED FOR ACTIVATION OF THE CONTRACTOR SUPPORT

AREA (CSA) AND THE PREASSEMOLY TESTING OF OGE AND MGE.

TABLE 1 IDENTIF;E3 THE TESTING AND PROCEDURE DOCUMENTn REQUIRED TO

ACTIVATE THE CSA. ALL Or THE TESTING OF ACO EQUIPMENT IS COVERED

IN THIS TABLE. SOME OF THE ACO EQUIPMENT IS ASSEMBLED AND UTILIZED

IN THE CSA AND IS IDENTIFED AS SUCH. OTHER ACO EQUIPMENT iS USED

AT THE LF, LCF & SMSB BUT THE TESTING AND CERTIFICATION OF IT IS

ACCOMiLISHED AT THE CSA.

TABLE 2 IDENTIFIES THE PREASSEMBLY TESTING AND PROCEDURES REQUIRED

FOR THE OGE XND MGE BEING PROCESSED THROUGH THE CSA AND/OR THE SMS3.

TABLE 3 IDENTIFiES THE TESTING AND PROCEDURES REQUIRED FOR THE CHECK-

OUT OF EQUIPMENT ASSEMBLED WITHIN THE LCF. THIS TESTING INCLUDES THE

POSTASSEMBLY CHECKOUT Or END-I TEMS AND THE INTEGRATION TESTING OF

SUBSYSTEMS AND SYSTEMS BUT DOES NOT INCLUDE ANY INTEGRATION TESTING

INVOLVING ITEMS NOT ASSEMBLED WITHIN THE LCF.

us 4 M4 ftEV. /6/6 a-ta-

REV sYm_____. 0" 2-9262 VOL. v

i-. iP,,,

1.2 (CoNT.)

TABLE 4 IDENTIFIES THE TESTING AND PROCEDURES REQUIRED FOR THE CHECK-

OUT OF EQUIPMENT ASSEMBLED WITHIN THE LF. THIS TESTING INCLUDES THEPOSTASSEMBLY CHECKOUT OF END-ITEMS AND THE INTEGRATION TESTING OF

SUBSYSTEMS AND SYSTEMS BUT DOES NOT INCLUDE ANY INTEGRAT ON TESTING

INVOLVING ITEM3 NO1 ASSEMBLED WITHIN THE L.F.

TABLE 5 IDENTIFIES THE TESTING AND PROCEDURES REQUIRED FOR THE

CHECKOUT OF EQUIPMENT ASSEMBLED W THIN THE SMSB.

TABLE 6 IDENTIFIES THE TESTING AND PROCEDURES REQUIRED FOR THEINTEGRATION OF LF AND LCF EQUIPMENT WITHIN A FLIGHT. AND FOR THE

INTEGRATION OF EQUIPMENT BETWEEN TWO OR MORE FLIGHTS.

1.3 DEFINITIONS

ASSEMBLE

THE ACT OF RECEIVING EQUIPMENT AND MATERIAL AT THE WORK SITE ANDPERFORMING SU'CH FURTHER WORK AS I, NECESSARY TO EMPLACE AND IN ER-CONNELT THE EQUIPMENT IN ACCORDANCE WI[H ASSEMBLY DRAWINGS AND

DOCUMENTATION. THE TERM "ASSEMBLE" IS APPROPRIATE EVEN WHEN THE

UNIT I5 COMPLETELY PORTABLE AND DOES NOT REQUIRE PERMANENT CONNEC-TION TO FACILITIES OR OTHER EQUIPMENT.

ASSEMULY AND CHECKOUT EQUIPMENT (ACO)

THE CATEGORY OF TEST EQUIPMENT CONSISTING OF SPECIAL FACILITIES

CONTRA.:T EQUIPMENT, (SFC/OH) AND BASE ACTIVATION TEST EQUIPMENT

(BATE) USED IN ASSEMBLY AND CHECKOUT AND TRANSFERABLE FROM SJTe TOSITE DURING SYSTEM ASSEMBLY.

BASE ACTIVATION TEST EQUIPMENT (BATE)

EQUIPMENT USED DURING ASSEMBLY AND CHECKOUT AND REQUIRING SPECIALDESIGN THAT IS PECULIAR TO THE MINUTEMAN ASSEMBLY AND CHECKOUT TASK.

MAINTENANCE GROUP EQUIPMENT (MGE)

THE EQUIPMENT REQUIrEO TO MAINTAIN THE MINUTEMAN MISSILE AND THE

OGE IN A CONDITION SUCH THAT THE WEAPON SYSTEM IS CAPABLE OF PER-

FORMING ITS MISSION. THE TERM "MAINTAIN" INCLUDES SUCH FUNCTIONS

AS "TEST", "REPAIR" AND "TRANSPORT."

OPERATIONAL GROUND EQUIPMENT (OGE)

EQUIPMENT REQUIRED TO SUPPORT THE MINUTEMAN MISSILE IN THE DIRECT

PERFORMANCE OF ITS MISSION. THIS INCLUDES THE EQUIPMENT REQUIRED

TO READY THE MISSILE DURING THE LAUNCH SEQUENCE AND CO INITIATE

LAUNCH.

U

OWIl BMW RV. 6/U1 1"taa-I

REV SYM, ,_IN D2-9262 VOL. XIV

,CT . iPAGK C

1.3 (CONT.)

END- ITEM

SMALLEST ASSEMBLY OF EQUIPMENT IDENTIFIED BY A FIGURE A NUMBER OR

ACO NUMBER RELEIVED OR ASSEMBLED ON THE BASE SITE. THESE 'ITEMS

HAVE PREVIOUSLY UNDERGONE (1) AN ACCEPTANCE TEST PRIOR TO SHIPMENT

FROM A VENDOR'S PLANT, AND (2) RELEIVING INSPELTION AT THE BASE

SITE.

,UIk-5YS TEM

A COMBINATION OF TWO OR MORE ENO-ITEMS 'WHICH ARE COMBINED AT THE BASE

SIrE AND WHICH, AFTER COMBINATION, PERFORM AN INDIVIDUAL FUNCTION.

SYSTEM

A COMBINATION OF ALL SUBSYSTEMS THAT ARE NECESSARY rO SUPPORT AMAJOR PART OF iHE MINUTEMAN WEAPON SYSTEM AT THE BASE SITE.

PREA5SEMBLY TESTING

PREASSEMBLY TEST;NG IS A CONFIDENCE CHECK PERFORMED ON (CRITICAL

ITEMS OF EQUIPMENT TO ENSURE THAT ONLY PROVEN EQUIPMENT 15

ASSEMBLED. THIS REDUCES POSTASSEMBLY MALFUNCTION, AND SUBSEQUENTFAULT ISOLATION TO EQUIPMCNT ASSEMDLY RATHER THAN INTERNAL BREAK-

DOWN. GENERALLY, THIS TESTING IS RESTRICTED TO ITEMS OF ELECTRONICEQUIPMENT AND SENSITIVE UNITS OF MELHANICAL EQUIPMENT,

PO$TA.SEMSLY TESTING

POSTASSEMBLY TESTING FOLLOWING T'HE ASSEMBLY OF EQUIPMENT IS PER-FORMED WITH THE SAME TYPE OF PORTABI.L TEST SETS NORMALLY USED IN

ORGANIZATIONAL MAINTENANCE. IN INSTANCES WHERE A UNIQUE FUNý,TIONMUST BE PERFORMED, SPECIAL TEST EQUIPMENT (BATE) is USED.

INTEGRATION TESTING

INTEGRATION TESTING IS THE POSTASSEMBLY CHECKOUT OF TWO OR MOREEND-ITEMS ASSEMBLED INTO A SUB-SYSTEM OR SYSTEM.

FLIGHT INTEGRATION

FLIGHT INTEGRATION IS THE PROCESS BY WHICH THE TEN LF's COMMON TOAN LCF ARE PROGRESSIVELY CONNECTED INTO THE SYSTEM AFTER ASSEMBLY

AND CHECHED OUT AS INDIVIDUAL FACILITIES.

FILIGHT-TO-FLIGHT INTEGRATION

THIS TESTING COMMENCES WITH DELIVERY OF THE SECOND FLIGHT AND ISA JOINT AIR FORCE-BOEING OPERATING. THIS TESTING CONSISTS OF

LINE EQUALIZATION VERIFICATION ON THE INTER-FLIGHT LINES AT THE

AFFELTED LAUNCH FACILITIES$ FOLLOWED BY LAUNCH NET VERIFICATIONTEST CONDUCTED FROM BOTH LAUNCH CONTROL FACILITIES.

us i m o REv. 111i ISiIi .S

RE 'ym Io 'D. 2-9262 VOL. x IVREVWW_____ _ _ _ _ _IPIII

"+"- ! X (CONT.)

. + .....-. -. : ... ,, . ,

A VafttIa: OINc Vif!ON THAT:IAJ~tL,.5', 4cM'iVt IN,.'^ EN-•l-Em, T[M

SY$t4, -EW SYt04, A-l' A3S:4MBLICV, 0O ENISURIC CO01PLIANýi' WVI-" tNAU 1OCt47 Afl' b PEC . ANLE SPICIFICATIONS.

1.4 GENRAlIREQUIREMLNTS

ký TNHE "OLLOW NG OCNERAL REQUIREMENTS ARE APPLItAbLC TO ALL PARA-

.'.A" Vo 7,4S VOLUME.

1.4'.1 CALIBRATION-CERTIFICATION

BEFORE PERFORMING ANY TEST SPECIFLD HEREIN; ACIO EOUIP•#4N' MJUST

BEAR A VALID QUALIrY CONTROL CERTIF-CAfT;OlN ,.AIL 101 ACCOROA•c-.

WITH rHL REQUIREMENTS SPECIFIED IN D2-12075, "CALIORATION.:

CERTII, IATION, AND TEST DOCUMENTATION INDEX".

1.4.2 UN3CHE DULED EVENTS

ANY UNS'HEDIJLED EVENT THAT OLCURS DURING TESTING SHALL &E*RE"CRIED,

TO THE BOEING LIAI',ON ENGINEER FOR NECESSARY AC1iON. tl"oll RUCIONl -m

THAT MAY BL CONTAINED IN INDIVIDUAL PROCEDURES CONCt*N'ING MALFUNC"

IIONz OR OTIICR UNSLHEOULED EVENTS SHALL NOT BE PERFQAMCD UNLESS

SO DIRECTED BY THE LIAISON ENGINEER. THE ACTION TA"N+CM1BALL BE

COORDINATED WITH THE BOZING (QUALITY CONTROL DePARTMt4E1T.

CAUTION .4

ALL ELECTRON,C MALFUNCTIONS IN THE LF AND LCF SHALL DC ISOLATED iBY THE USE OF STANDARD MINUTEMAN TEs-T EQUIPMENT APPLIED TO PRE.-,

SLRIBED TEST POINTS. THE USE OF TESI LQUIPMCNT 10 TAKE VOLTAGE

REAOING. AT NON-SIANDARD POINTS IN ELECIRONIC CHASSIS PFOR MAL-

FUNClION ISOLATION, REFERRED TO AS PROBING, IS PROBITED.

1.4.3 TEST ORDER

THIS DOCUMENT DOES NOT PROVIDE THE ORDER OF TEST SEQUENCING.

TEST SEQUENCES MUST BE DERIVED FROM THE PREREQUISITES GIVEN IN A.

THE INDIVIDUAL TEST PROCEDURES.

1.4.4 SAFETY PRECAUTIONS

COMPLIANCE WITH THE SAFETY PRECAUIIONS PROVIDED IN USAI BSDEXHIBIT 62-16, "MINUTEMAN WEAPON SYSTEM SAFETY STANDARD",

AND THE WARREN AFB SUPPLEMENT TO EXHIBIT 62-16 Is MAMDATORY.

D2-9262 Vo,.. XIV

KV. S-'

1.4.4 (ONT.)

P*IOR TO THE START OF AND DURING THE CONDUCT OF ANY SITE ACC4PT"

AlCE TESTS, CONPLIANCE WITH ALL APPLICABLE SAFETY RESTRAINTS SIT

FORTH IN D2-9262, VOL. XIV AND THE DOCUMENTS REFERENCED IN TABLLSI THROUGH 6 Is MANDATORY. THESE SAFETY RESTRAINTS AOL ALSLO SETFORTH IN A CONVENIENT CHECK LIST FORM IN Ua-14863-3 "SAFETT CNLCKLIST FOR FLIGHT AND SQUADRON ACCEPTANCE TESTS". THESE CHECK LISTS

PRESENTED IN D2.14863-3 SHALL BE USED ONLY AFTER IT HAS BErDETERMINED THAT ThEY DO NOT CONFLICT WITH THE SAFETY RESTRAINTS

SPECIFIED'IN THIS DOCUMENT. IN CASE OF CONFLICT. THE REQUIRCMENTS

OF THIS DOCUMENT SHALL GOVERN.

1.4.5 FACILITY ACCEPTANCE

ALL REAL PROPERTY AND REAL PROPERTY INSTALLED EQUIPMENT (RPIE)SHALL NAVE BEEN ACCEPTED IN ACCORDANCE WITH THE VALIDATION PRO-

CEDURES PER CONTRACT DA..O4-548,ENG-98, SPECIFICATION SERIAL No.ENG-04,548-63-5, VOL. IV, "SPECIFICATIONS FOR MINUTEMAN FACILITIES

AT WARREN AIR FORCE BASE".

1.4.6 COOLING AIRFLOW ADJUSTMENT

NO POWER SHALL BE APPLIED TO ANY EQUIPMENT REQUIRING COOLING AIRPRIOR TO THE COMPLETION OF THE REQUIRED ADJUSTMENTS TO THE COOLING

AIR PROVIDED FOR THE EQUIPMENT.

{ 1.4.7 VOLUME IDENTIFICATION

To ACHIEVE CONSISTENT DOCUMENT NUMBERING WITHIN THIS DOCUMENT,

VOLUMES OF TEST PROCEDURE DOCUMENTS ARE DENOTED BY DASH NUMBERS,I.E., D2-xxxx-6.

1.4.8 ASSEMBLY REQUIREMENTS

PRIOR TO POSTASSEMBLY TESTING, THE EQUIPMENT TO BE CHECKED OUTSHALL HAVE BEEN ASSEMBLED AND INSPECTED IN ACCORDANCE WITH THE

FOLLOWING APPLICABLE ASSEMBLY DRAWINGSt

LAUNCH CONTROL FACILITY ASSE.MBLY - 24-3405WARREN AFB

LAUNCH FACILITY ASSEMBL -. 24-3404WARREN AFB

MINUTEMAN STRATEGIC MISSILE SUPPORT 24-3404BASE ASSEMBLY- WARREN AF1B

Cus mu a a. Wa -4

RE ,, D2 -26 VOL.' xiv

++.1

+•,*1.5 SPECIAL RE QUI RENTS

1. ".5.1 ENVIRONMENTAL CONTROL SYSTEM OPERATION

THE ENVIRONMENTAL CONTROL SYSTMS IN THE LAUNICHER EQUIPMENT Room orTHE LAUNCH FACILITY AJND IN THE LAUNCH CONTROL CENTER SMALL NOT BE

OPERATED UNTIL THE AMBIECT AIR TEMPERATURE 15 AS SPECIFIED IN PARA-

"GRAPH 1.5.3. THE AMBIENT AIR REQUIREMENTS SHALL BE INITIALLY

ESTABLISHED IN ACCORDANCE WITH THE.LF PREHEAT PROCEDURES .OF O¢CUMgNT

D2-40027.

1.5.2 PREHEAT OPERATION

THE PREHEAT OPERATION SHALL BE INITIATED, MAINTAINEDj AND TERMINATED

IN THE LAUNCH CONTROL CENTER AND LAUNCH FACILITY IN ACCORDANCE WITH

D2-10027. THE PREHEAT EQUIPMENT IN THE LAUNCH FAC-LITY SHAtL NOT BE

REMOVED UNTIL THE COMPLETION OF THE SINGLE-THREAD COMMAND & MONITOR

TEST REQUIRED BY D2-14556-5.

1.5.3 LAUNCH CONTROL CENTER, LAUNCH EQUIPM4ENT AND SMSB ENVIRONMENT

AT THE BEGINNING AND END OF EACH TEST PERIOD, OR AT THE BEGINNING

OF THE TEST DAY AND EACH 12 HOURS T.HEREAFTER DURING WHICH ELEC-

TRONIC EQUIPMENT 15 OPERATING (ELECTRICAL POWER APPLIED), THE

FOLLOWING AMBIENT AIR CONDITIONS SHALL BE MEASURED AND RECORDED,

AND SHALL BE AS SPECIFIED.

A) TEMPERATURE - THE TEMPERATURE IN THE LAUNCH CONTROL CENTER SHALL

BE WITHIN THE LIMITS OF 69*F AND 78*F.

THE TEMPERATURE IN THE LAUNCHER EQUIPMENT RooM SHALL BE

WITHIN THE LIMITS OF 60*F AND 80eI.

THE TEMPERATURE IN THE SMSB DURING PERIODS OF EQUIPMENT

OPERATION SHALL BE BETWEEN 701F AND 74*F.

B) RELATIVE HUMIDITY - THE RELATIVE WMIDITY IN THE LAUNCH CONTROL

CENTER SHALL NOT EXCEED THE UPPER PERCENT LIMIT SET BY A

STRAIGHT LINE ON A. PSYCHROMETRIC CHART CONNECTING 69*F AT

557 RELATIVE HuMI.DITY AND 78*F AT 457 RELATIVE HUMIDITY.

THE RELATIVE NUAIDITY IN THE LAUNCHER EQUIPMENT ROOM SHALL

NOT EXCEED THE UPPER PERCENT LIMIT SET BY A STRAIGHT LINE

ON A PSYCHROMETRIC CHART CONNECTOmG 60*F AT 607 RELATIVEHUMIDITY AND 80OF AT 45% RELATIVE HUMIDITY.

THE RELATIVE HUMIDITY OF THE AIR IN THE SMSB SHALL NOT EXCEED

607 AT 72 DEGREES ORY BULB.

NOTE

THE FOLLOWING TEST EQUIPMENT IS NECESSARY TO SATISFY THESEREQUIREMENTS1

A. THERMOMETER .SELF-INDICATING, LIQUID IN GLASS, ACO0.3023.-

L 'B* SLING PSYCHROMETER, ACO-316.

.•24262 VoL. XIV

a151 syO

14.4 EQUIPMENT COOLING AIR REQUIREMENT$

t AT THE SEIONIRIN OF EACH TE3T PELRIOO* Ao EACH 1wous mazArTeRDURING WHICH ELECTRONIC EQUIPMENT SEOUl NG DUCTED COOLING AIR ISOPERATING (ELECTRILAL POWER APPLIED), TH( TEMPERATURE AT THE DUCTEDEQUIPMENT COOLtNG AIR SHALL-BE MEASURED AND RkCOROCO. 'THE MEASURE-MENT PROCEDURES AND RESPONSES SHALL BE A SPECIFIED IN THE APPLIC-ABLE PORTION or D2-14553-5.

1.5.5 CONTROL oF ACCESS TO LAUNCHER

DURING THE ASSEMBLY AND CHECKOUT PERIOD, THE. LAUNCHER CLOSURE ANDTHE PERSONNEL ACCESS HATCH SHALL BE KEPT IN A CLOSED POSITIONUNLESS OTHERWISE AUTHORIZED BY THE SENIOR FIELD SUPERVISOR AT THELAUNCH FACILITY. IN THE EVENT THAT THE PERSONNEL HATCH MUST BEOPENED, THE ACO-4267 "VEHICLE TO ACCESS SHAFT PROTECTIVE COVER"SHALL BE USED WHENEVER POSSIBLE.

1.5.6 SCN CCMMAND LINE CONNECTIONS STATUS

ACHECK SHALL BE MADE TO ENSURE THAT NO SCN COMMAND LINES ARE

CONNECTED AT THE INTERCONNECTING BOX BEFORE ANY OF THE FOLLOWINGINTEGRATION TESTS ARE PERFORMED:

LAUNCH FACILITY START-UP TEST PER D2-14550-5

LAUNCH FACILITY END-TO-END TEST PER D2-14551-5

TEST AND ADJUSTMENT OF SECURITY SYSTEM PER D2-11276-5

LF - MISSILE INTEGRATION TEST PEc D2-14560-5

GROUNDING AND ORDNANCE CIRCUIT TEST PER D2-14552-5

1.5.7 ELECTRICAL POWER REQU.IREMENTS

BEFORE ELECTRICAL POWER CONNECTIONS ARE MADE TO A PIECE OF EQUIP-

MENT, ASSURANCE SHALL BE RECEIVED THAT THE POWER SHALL BE OF THE

PROPER TYPE AND QUALITY AND THAT THE EQUIPMENT HAS BEEN GROUNDED

IN ACCORDANCE WITH REQUIREMENTS OF THEIR ASSEMBLY DRAWINGS.

1.5.8 LAUNCH CONTROL SYSTEM SAFETY REQUIREMENTS

PR4OR TO THE BEGINNING OF AN INTEGRATION TEST AND DURING THE

PERFORMANCE OF ANY INTEGRATION TEST$ THE FQLLOWING CONFIGURATION

SHALL BE MAINTAINED EXCEPT WHERE THE TEST PROCEDURE SPECIFICALLY

AUTHORIZES OTHERWISE%

A) LCF I ALL TEN (10) LAUNCH ENABLE SWITCHES IN TH4 COMMUNICA..TIONS CONTROL CONSOLE SHALL BE IN THE "SAFE" POSITION.

B) LF - (1) IN THE MAIN DISTRIBUTION BOX, THE SAFETY-CONTROLSWITCH SHALL BE MECHANICALLY POSITIONED AND

LOCKED IN THE "SAFE" POSITION.

l Ilme m tV. vef *-rnu4

D2-9262 VOL. XIV

Illin .*A

1.5., (CONT.)•" ) CONT.

(2) ACO-172 MUST BE INSTALLED IN T1E P/G CAVIY' WHEN

THE MISSILE IS IN PLACE AND CONNECTED TO THE GCUMBILICAL AND SKIRT UMBILICAL CABLES.

1.5.9 MISSILE SAFETY REQUIREMENTS

PRIOR TO THE BEGINNING OF ANY INTEGRATION TEST AND DURING THE PER-FORMANCE OF ANY INTEGRATION TEST, THE FOLLOWING CONFIGURATION OF THE

MISSILE ORDNANCE SYSTEMS SHALL BE MAINTAINED UPON ANY MISSILE WHICH

MAY HAVE BEEN EMPLACED ;N AN LF IN A FLIGHT EXCEPT WHERE THE TESY

PROCEDURE SPECIFICALLY AUTHORIZES OTHERWISE;

A) SAFING PINS SHALL BE INSTALLED IN THE FOLLOWING ORDNANCE

DEVICE3:

(1) FIRST-STAGE IGNITOR AT THE REAR END OF THE SECOND-

STAGE ENGINE.

(2) SECONO-STAGE IGNITOR AT FORWARD END OF THE FIRST-STAGE

ENGINE.

(3) THIRD-STAGE IGNITOR AT AFT. END OF THIRD-STAGE ENGINE.

( (4) FIRST AND SECOND STAGE SEPARATION3 DEVICE AT INTER-STAGE A.

(5) SECOND AND THIRD STAGE SEPARATIONS DEVICE AT INTERSTAGE B.

(6) THRUST TERMINATOR AT THE FORWARD END OF THE THIRD-STAGE

ENGINE.

B) THE G&C UMBILICAL CABLE (W548) SHALL NOT BE CONNECTED TO THEMISSILE UNTIL THE SINGLE THREAD COMMAND AND MONITOR TEST HAS

BEEN COMPLETED.

c) THE SKIRT UMBILICAL (W510) SHALL NOT BE CONNECTED IN THE MISSILE.

1.5.10 LAUNCH FACILITY ORDNANCE SYSTEM SAFETY REQUIREMENTS

PRIOR TO THE BEGINNING OF AND DURING THE PERFORMANCE OF-ANY INTEGRA-

TION TESTO THE FOLLOWING CONFIGURATION OF THE LF ORDNANCE SYSTEM

SHALL BE MAINTAINED:

A) W550 FROM THE GUIDAN(.E AND CONTROL UMBILICAL CABLE RETRACTOR

SHALL BE DISCONNECTED.

9) W551 FROM THE LAUNCHER CLOSURE ACTUATING AND LOCKING MECHANISM

SHALL BE DISCONNECTED.

( c) W716 FROM THE GW UMBILICAL PLUG SHALL BE DISCONNECTED.

as -m euw. • ..au

NmD-96 VOL. xIvMY 5ymMMNM@WWA-W.W

1.5.11 COWAND LINE CONNECTIONS

PPRIOR TO THE BEQINNING AND DURING THE PFRrq*NANCE or AflI(iWTEGRATION

TEST, THE COMMAND LINE LINKS IN THE LCF'ANo LF INTERCONN44icIiG boICs

IN THE AFFECTED FACILITIES SHALL HAVE BEEN REMOVED AND STOtED AT A

LOCATION CONVENIENT TO THE sox. THESE CONNECTING LINKS 4AY 'BEREINSTALLED ONLY WITH THE PERMISSION OF TH4E SENIOR FIELD SUPcRVISOR,AT THE LCF EVEN THOUGH INSTALLATION IS REQUIRED AS PART OF A TEST

PROCEDURE.

1.5.12 LCF AND LF SHUTDOWN AND START-UP PROCEDURES

1.5.12.1 ASSEMBLY THE ACO-545.5 LCF'SHUTDOWN/STARTUP PROCEDURE PLACARD TO THE

WALL OF tHE LAUNCH CONTROL CENTER BENEATH THE EMERGENCY ESCAPE HATCH.

THE PLACARD SHALL BE POSITIONED SO THAT IT WILL BE VISIBLE TO THE

OPERATOR SEATED AT THE LAUNCH CONTROL CONSOLE. THE ATTACHMENT HARDWARE1I PROVIDED AS PART OF ACO-545.3. EFFECTIVITY OF THE PLACARD IS

SPECIFIED IN 25-39271.

1.5.12.2 ASSEMBLE THE ACO-544.5 LF SHUTDOWN/STARTUP PROCEDURE PLACARD TO THE

EQUIPMENT ROOM SIDE or THE LAUNCH TUBE LINER IN THE LOWER LAUNCHER

EQUIPMENT Room, OPPOSITE THE FIG. A 1283 MOTOR GENERATOR SET. THE

ATTACHMENT HARDWARE IS PROVIDED Ab PART OF ACO-544.5. EFFECTIVITYOF THE PLACARD IS'SPECIFIED IN 25-39270.

1.5.12.3 DURING ASSEMBLY AND CHECKOUT AND PRIOR TO THE DELIVERY OF A FLIGHT,

ALL SHUTDOWNS AND STARTUPS OF THE LAUNCH CONrROL FACILITY SHALL BE IN

ACCORDANCE WITH THE PROC-EDURES PROVIDED ON THE ACO-545.5 PLACARD ANDALL SHUTDOWNS AND SlARTUPS OF THE LAUNCH FACILITIES SHALL BE IN

ACCORDANCE WITH THt PROCEDURES PROVIDED ON THE ACO-5,,.5 PLACARDUNLESS OTHERWISE SPECIFIED IN THE TEST PROCEDURES REFERENCED IN

THIS DOCUMENT.

1.5.12.4 FOLLOWING COMPLETION OF THE LAST CHECKOUT TEST AND PRIOR TO DELIVERY

OF THE FLIGHT TO THE AIR FORCE, THE ACO-544.5 AND ACO-545.5 PLACARDSSHALL BE REMOVED FROM EACH LAUNCH FACILITY AND THE LAUNCH CONTROL

FACILITY RESPECTIVELY.

1.5.13 INTERIM SECURITY REQUIREMENT

AS EARLY AS PRACTICALBE, INTERIM SECURITY EQUIPMENT SHALL BE ASSEM-BLED AND CHECKED OUT IN EACH LAUNCH FACILITY.

THE EQUIPMENT REQUIRED, THE DETAILED DESCRIPTION OF INSTALLATION,CHECKOUT AND THE REMOVAL OF THE EQUIPMENT SHALL BE IN ACCORDANCEWITH D2-15006-3, "INSTALLATION, CHECKOUT, AND USE OF LF INTERIM

SECURITY SYSTEM."

THE NORMAL OPERATIONAL FUNCTIONING OF SWITCH CIRCUITRY OF EACH OUTER'

ZONE SWITCH, THE ACCESS HATCH CLOSURE (PRIMARY DooR) SWITCH AND THE-.VAULT DOOR COMBINATION LOCK SWITCH VILL HAVE BEEN VERIFIED DURINGCHECKOUT OF THE INTERIM SECURITY SYSTEM PER D2-15006-3. THE*EFUNCTIONS NEED NOT BE REVERIFIED.

Cvs m an ams. w"

UIV $YM~ iW. D2-2624 YOt. X I V

• .1.6 faut TT ROQY 2 ,qutINa FuricTiONAL TESTINGt

TASLES I THROUGH 6 OF THIS DOCUMENT INCLUDE ONLY THOSE ITEJMSREQUIRING FUNCTIONAL TESTING. THE Fia. A AND ACO ITEMS LISTEDBELQV 00 NOT REQUIRE FUNCTIONAL TESTING$ HOWEVER, SOME Of THESEITEMS DO REQUIRE CALIBRATION, SERVICING OR PROOF-LOAO TESTING.FOR SUCH ITEMS, REFER TO D2-12075, "CALIBRATION, CERTIFICAT4ON

AND TEST DOCUMENTATION INDEX".

1.6.1 FIGURE.A ITEMS NOT REQUIRING FUNCTIONAL TESTING"

FIG. AITE O

602.2 COLLIMATOR SET604.4 COUPLER, GUIDANCE CONTROL

1246 CABLE ASSEMBLY SET, LAUNCH CONTROL

1248 CABLE ASSEMBLY SET, LAUNCHER1252.2 ADAPTER, RING, MISSILE SUPPORT1268 DECODER, COMMAND SI-GNALS

1334 SEAT, OPERATOR'S1335 SEAT, OPERATOR'S1370 LIGHTING EQUIPMENT, SURVIVAL

1375 DAMPER SET, FLUE, ELECTRONIC COOLING1385 DISTRIBUTION Box, POWER AND COMMUNICATION1409 ARRESTER SET, ELECTRICAL SURGE

FIG. AITEM G

553 TRANSFORMER, RATIO, GERTSCH RT MODEL 529554 SHIFTER, PHASE GERTSCH

555 PRECISION DC VOLTAGE STANDARD

559 4 00-CYCLE OSCILLATOR

560 AC - DC CONVERTER565 TRUCK, HAND, AUTONAVIGATOR

575 TRIPOO., THEODOLITE, WILD IVA580 INDICATOR, PRESSURE583 KIT, MODULE CONNECTOR ALIGNMENT585 SET, TRAVERSE TARGET590 VOLTMETER, PRECISION, D. C.593 RESISTANCE BOX, DECADE617 SUPPORT RING, AUTONAVIGATOR H&A631 MIRROR AZIMUTH ALIGNMENT

(I

wIS 1S 3 mU. em as.

v gym ... 0..96 VOL. AV

i 1.6.1 (CiNY.)

FIG. At~mL

637 S141PPING AND STORAGE CONTAINER, MISStILE

GUIDANCE SET

642 OPTICAL ALIGNMENT SET

648 THEODOLITE

657 FIXTURE,- TRANSFER AUTONAVIGATOR

660 MOUNTj THEODOLITE'

675 MIRROR, AZIMUTH ALIGNMENT

684 COVER, PROTECTIVE

687 COVER, ASSEMBLY, DUST

719 OPTICAL ALIGNMENT GROUP

3009 PULLER, PRINTED CIRCUIT

3022 TRIJCK, DOLLY

3037 HOIST, CHAIN

3046 BATTERY FILLER, GRAVITY

3048 SLING, BEAM TYPE

3050 SLING, BEAM TYPE

3052 SLING, MULTIPLE LEG

3053 CLAMP, RESTRAINING, HYDRAULIC ACTUATOR

3066 TRUCK, HAND, LIFT

3067 VOLTMETER

C 3096 SHIPPING AND STORAGE CONTAINER

3119 ADAPTER ASSEMBLY, SPANNER WRENCH

3140 INDICATOR, DIGITAL DISPLAY

4001 MULTIMETER4004 OSCILLOSCOPE

4006 OSCILLATOR, AUDIO FREQUENCY

4025 CONTAINER, SAfE-ARM PINS

4028 ADAPTER, HOISTING, W SECTION

4038 BARRIER SET, LAUNCHER-OPENINGj SAFETY

4041 TE'STER, GAS, PORTABLE

4047 WRENCH, ASSEMBLY, SOCKET SAFING PIN

4053 ADAPTER, HOISTING, STABILIZING RING

4069 CLAMP SET, ADAPTER RING TO MISSILE SKIRT

4095 SHIPPING AND STORAGE CONTAINER, BALLISTIC

MISSILE

4102 TRUCK, HAND, LIFT

4103 GRIP SET, UMBILICAL CABLE

4104 HOIST, CHAIN

4107 LEVEL SET, MISSILE BASE SUPPORT

4117 HOISTING UNIT

4125 ATTENUATOR, VARIABLE

4127 POWER SUPPLY

4141 DOLtY, GgAftCASEMNOTOR,

4143 HARNESS, BALLISTIC ACTUATOR

4144 HEADSET

4145 ADAPTER, HOISTING, MOTOR-GENERATOR

ov t)2wM%*2 VOL. X IV

£ 1.6.1 (CON 7)

FIG. A

4146 PLATE, LEVELING4149 TRUCK, HAND, LIFT

4160 WIRE WRAPPING KIT

4167 LOAD BANK, ELECTRICAL

4172 PLUG-IN UNIT, OSCILLATOR

4175 JACK-SET, TRANSLATING

4179 CASE, ENCODER

4188 JACK SET, LEVELING

4191 TANK, 4IQUID STORAGE, METAL

4192 BRIDGE, RESISTANCE

4206 SUPPORT RAMP4217 SUPPORT SET, T1E

4218 SCALE, DIAL INDICATING

4263 BARRIER, LAUNCH TUBE ACCESS DOOR, SAFETY

4264 CABLE AND REEL ASSEMBLY, GROUNDING MISSILE

4265 COVER SET, SLING ROD ENDS

4267 SHELTER, ENVIRONMENTAL, ENTRANCE HATCH

4270 PLUMB BOB SET, TRANSPORTER-ERECTOR

4274 SUPPORT CRADLEt, ROCKET MOTOR CARRIAGE,

3RD STAGE

4277 SLING, GEARCASE MOTOR

4278 SHELTER, ENVIRONMENTAL, TRANSPORTER -

ERECTOR TO LAUNCHER

4280 POSITIONING KIT, CARRIAGE, ROCKET MOTOR

KMU-116/E4281 SUPPORT, CRADLE, ROCKET MOTOR CARRIAGE,

2BD STAGE4282 HOIST, GEARCASE-MOTOR

4289 Roo ASSEMBLY; L-AUNCHLR CLOSURE LOCK REMOVAL

4290 ADAPTER, HOISTING, MULTIPLYING LINKAGE

4291 CLAMP, BALLISTIC ACTUATOR ROD4292 COVER, ENVIRONMENTAL, LAUNCHER OPENING

4305 CYLINDER/VALVE, COMPRESSED GAS

4306 PLATE SET, TRANSPORTER - ERECTOR, HINGE TO

PYLON

4307 RESTRAINT ROD, BASE'ADAPTER RING TO

TRANSPORTER-ERECToR4308 SLING, GUIDANCE & CONTROL, SHIPPING

CONTAINER4319 ADAPTER SET, CONNECTOR

4337 TRUCK, DOLLY, MOTOR-GENERATOR

4339 OHMMETER

4343 BRIDGE, IMPEDANCE

U SR ll V. S, Ba 8-RU4

;D. 2-9262 VOL. X IV

-"T IP Co

1.:6.1 (CONT.)

FIG. A

4370 TEST STAND, GEARCASE MOTOR4375 STEP, DOOR ACTUATOR4378 SLING, CHILLER UNIT AND PUMP

4382 CORD ASSEMBLY, ELECTRICAL4386 WRENCH SET, ELECTRICAL CONNECTORS

4388 TEST SET, TELEPHONE EQUIPMENT

4394 SLING, GAS GENERATOR, LAUNCHER CLOSURE440 HOOK, HOIST, SUPPORT"4405 SUPPORT, HOIST, UMBILICAL CABLE

4406 WRENCH, TORQUE"415 SLING, TRANSPORTER - ERECTOR ACTUATOR

4440 PLATES, MOUNTING, THEODOLITE441" PROTRACTOR STRIPSET, AUTOCOLLIMATOR BENCH

RAIL"4442 CASE, DECODER, COMMAND SIGNAL

4443 TOOL, CODE CHANGE4"5 CONTROL, MISSILE ERECTION

4446 COVER, PERSONNEL ACCESS, LAUNCHER4447 INSTALLATION - REMOVAL KIT, CARRIAGE

VERTICAL RESTRAINT

4448 EXTENSION, MISSILE BASE ADAPTER RING"4451 CONTROLLER, POWER AZIMUTH DRIVE4452 TRAVERSE PLATE, LAUNCH TUBE ACCESS

DOOR

"346 FREQUENCY CONVERTER

"4459 MULTIMETER, ELECTRONIC4461 AMMETER"4468 THERNOMETER, ARMORED, STAINLESS - STEEL

GROUND SPIKE4471 MICROWAVE POWER METER4472 GENERATOR, SIGNAL

4476 TESTER, PYROMETER AND THERMOCOUPLE

4479 OSCILLOSCOPE, DUAL BEAM

4•83 KIT, SAFEJY PIN INSTALLATION AND REMOVAL-484 TOWBAR,'MOTOR VEHICLE4521 ALIGNMENT KIT, OPTICAL4535 ALIGNMENT SET, MISSILE TRANSFER4341 MAINTENANCE PLATFORM, LAUNCH CONTROL

FACILITY

"AM me3 - v ISV.SM 4l

- " V IN0 D2-9262 VoL. XIVI- VIPAU..

t 1.6.2 ANO ttS'-NOT REQUIRNG FunCTIo•NA6 TL'STIN

ACO

104 KIT, ADAPTER, INTRASITE CAOLE, LF

105 KIT, ADAPTER, INTRAs3TE CABLE, LCF112 JUNCTION BOX & CABLE SET, MISSILE

SIMULATION KIT

115 HF SYSTEM TEST BREAKOUT BOX

116 CABLE EXTENSION

118 POWER CONTROL UNIT

119 CABLE KIT, C53C120 CABLE, POWER, PROGRAMMER, TEST

123 JUNCTION Box, TEST, SCN/CSA125 ADAPTER, LF/DDG CABLE

126 ADAPTER, LCF/DOG CABLE

129 POWER SUPPLY SCN TEST, CSA130 CABLE KIT, LCF/SCN TEST, CSA

131 CABLE, POWER, SECURITY RACK TEST

132 CABLE KIT, LF/SCN TEST, CSA133 DUmmY LOAD, R/V139 ADAPTER, SCN, FRONT PANEL

149 UHF SYSTEM TEST BREAKOUT BOX

151 POWER CABLE SET, CSA DRAWER TEST AREA

160 CABLE SET, HF/UHFS161 PANEL, DISTRIBUTION

162 CABLE POWER, HVC/SIN166 PLUG, CAVITY, ENCODER

168 CIRCUIT CARD, FAULT SIMULATION

G&C COUPLER

170 LF/SIN CHECKOUT ADAPTER

171 LCF/SIN CHECKOUT ADAPTER

172 PLUG, DECODER CAVITY

173 SIMULATOR, LF/SCN INTERFACE

176 FILTER, BOND PASS, E-1178 TEST PLUG, E-I180 TEST LEADS

181 CABLE SET, AC POWER (120V, 60 CPS)182 CIRCUIT CARD, FAULT SIMULATION,

PROGRAMMER GROUP

184 DiSCONNEýT, LF BATTERY, MG SET

187 CABLE, SECURITY, SITE ACTIVATION

189 GENERATOR, PULSE

194 TRANSCEIVER,' PORTABLE

195 CABLEf INTERCONNECTING, BATTERY CHARGER,

POWER SUPPLY

197 CABLE SET, INTERCONNECTING BATTERY

200 ADAPTER, FLOW, G&C UM13ILICAL

D2-9462 VOL. XIV

S.. . . .. .

C 1.6.2 (CONT.)

ACO

201 MANIFOLD, TvsT, DRYER-AIR COMPRESSOR204 ADAPTER, MANOMETER TO C40B RACK AIR DUCT211 PLUG, PRESSURE, BALLISTIC ACTUATOR

ASSEMBLY'

215 FIXTURE) HOLE LOCATING, MISSILE 5USPENSLON'

SYSTEM$ SPRING CAN

216 FIXTURE, MISSILE SUSPENSION SYSTEM

LOADING

217 SET', FIXTURE, LIFTING, MAIN J-BOX

220 DRILL JIG, ADAPTER PLATE

229 TRUCK, 16' FLAT BED, W/HYDRAULIC CRANE231 CABLE SET, CHOKE, LCF M-G SET

232 PLATFORM, WORK, LCF233 ADAPTER, TORQUE, AZIMUTH DRIVE INSTALLATION

235 REMOVAL EQUIPPENT, SNOW AND ICE

245 BEAM-TYPE SLING

248 SLING, DOOR, VAULT, SECURITY PIT

270 CABLE, MISSILE GROUNDING

274 INDICATOR, PHASE SEQUENCE (400 CYCLE)277 LCF/HVC CHECKOUT ADAPTER278 LF/IVC CHECKOUT ADAPTER

279 Bl DIRECTIONAL POWER MONITOR281 ADAPTER TEST MISSILE SIMULATOR KiT

282 ADAPTER, TEST, SCN INTERFACE S1IULATOR

283 ADAPTER, TEST, ACO INCODER284 TEST SET , CACLE SYSTEM

287 HANDLE , CT S

289 BREAKOUT BOXT CABLE SYSTEM

290 ADAPTER, COAZIAL CABLE292 CABLE ASSEMBLY, GROUND CONNECTION

301 SCAFFOLDING, PORTABLEj LF AND LCF306 PLUMB BoB308 MANOMETER31 FILTER, WATER, 10 MICRON313 SAFPLING BOW e313 SPOTTING SCOPE315 MICROSCOPE31 PSYCHROMETER, SLING

317 BENCHR TEST, ELECTRONIC

.318 METER, AUDIO FREQUENCY PONER

320 DuMmy LOAD, UHF320 GENDRATORD SIGNAL322 Dummy LOAD SINLF

337 VOLTMETER, VACUUM TUBE341 FLOOR POLISHER

347 AMMETER, 500 A4P

REVWN............... .nfM, D24 ,3•2 YoL. *XIv

KY~ VIMr. I" I962VL XIV

. (CONT.)

( ACO

352 LEAD, ELECTRICAL (GROUNDING)

355 TEST SET LCF POWER SUPPLY356 TEST SET LF POWER SUPPLY359. CONVERTER, HF

360 METER, RF POWER362 MEGOHMMETER367 OSCILLOSCOPE

368 OSCILLATOR, AUDIO FREQUENCY370 -THERMOMETER CONTACT

371 PUMP, CENTRIFUGAL, PORTABLE

375 SHELTER, MOBILE

379 HAND SET, SOUNDPOWERED

387 SPRAYER, PAINT, PORTABLE392 TRANSIT393 POWER SUPPLY

394 MILLINETER, SLIP-ON DC396 TEST SET, INSULATION BREAKDOWN"

404 MOTOp-GENERATOR

405 HOIST, POR'iABLE

407 BREATHING APPARATUS SELF CONfAINED

409 CABLE TESTER, PORTABLE410 TESTER, COBUSTIBLE GASES

411 TELEPHONE SET, FIELD412 CAMERA, POLORO•IO, FLASH

413 TESTER, OXYGEN DEFICIENCY

414 TESTER, GAS, CARBON MONOXIDE

416 CAMERA, OSCILLOSCOPE420 TRUCK, 91 VAN w/HoisT & HEAT

421 REPAIR KIT, VAPOR SEAL ENVELOPE

422 VOLTMETER, DIFFERENTIAL, AC-DC424 METER, FREQUENCY426 TACHOMETER427 PUMP, CENTRIFUGAL, PORTABLE

430 HEATER, PORTABLE431 TRUCK, ORDNANCE, HANDLING AND SUPPORT432 TANK, DEIONIZED WATER

433 FAN, CIRCULATiNG435 MONITOR, CURRENT RECORDING

439 KIT, PH METER440 GENERATOR, SIGNAL

"441 BUS TRAVEL-ALL446 METER, FREQUENCY

474 TRUCK, 9' VAN475 TRUCK, 9' VAN W/HEAT

476 TRUCK, 12' VAN W/HOIST & HEAT477 TRUCK, 7 1/2' PANEL W/HCAT478. TRUCK, 7 1/2' PANEL

" m.v. em

.. ... . ,r, ... ....... .. . .•0 4. .. 262. VOL .. X UV

(. . (CONeT.)

ACOI.TEH

482 RECEIvER, HF443 1MPEDANCE BRIOGE, PF

485 DECADE, CAPACI'TANtE

486 GENERATOR, FREQUENCY

48-7 VARIAC488 INTERRUPTER, CIRCUIT

489 MEGOHMNETER

490 ANEMOMETER

491 PITOT TUBE492 DRAF"T GAUGE

494 DETECTOR,- LAND LINE

512 SLING SET, ROCKET MOTOR CARRIAGES

513 INVERTER DC TO AC

514 VACUUM TUBE VOLTMETER516 TEMPLATE, DRILL, ESA PANEL

517 ADAPTER, SIN REMOVE RINGING

518 TRUCK, CABLE MAINTENANCE

521 POWER CABLE SET

523 CUTOFF DEVICE,,H. V. W POWE SUPPLY524 CABLE, INTERIM(OUTER ZONE SECU•iTY

525 PLUG, SCS526 TR,iPOO, THEODOLITE527 CHUCK & FOOT ADAPTER

528 KIT, INSTALLATION, LAUNCHER CLOSURE

ACTUATOR

529 GENERATOR, GASOLINE DRIVEN

530 WRENCH, "T" HANDLE

534 MONITOR & RECORDER, G&C COUPLER

INGERFACE535 HF BREAKOUT BOX

536 ELECTRONIC LOUNTER537 FIXTURE, LOCATING, LF ACCESS CENTER LINE

538 JIG, DRILL, INTRASITE CABLE FEED THROUGH

539 JIG, LOCATING LF, AUTOCOLLIMATORMIRROR MOUNl

540 DECK REMOVABLE, PERSONNEL ACCESS SHAFT

541 KIT, LOCAriNo, LF MAiN "J" BOX542 VARIATOR, PRESSURE - VACUUM543 VOLTMETER, PRECISION, DC

544.2 PLACARD, LF SHUTDOWN/START-UP PROCEDURE

545.2 PLACARD,'LCF SHUTDOWN/START-UP PROCEDURE

546 POWER SUPPLY

601 ALIGNMENT PIN, ROCKER ARM TO UPPER

BRACKET

604 SLING606 COVER PROTECTIVE, ELECTRONIc RACK

low D2-9262 Vot. * X I +

- Ipam 2.

aI1.6.2 (CoNT.)

ACO

608 ENvIRONMENTAL ENCLOSURE - LCF609 5PANNER, LOWER

610 MARKER, AZIMUTH, INDICATOR

612 LIFT BASKET

613 ALIGNMENT PIN, PENDULUM ROD TO ROCKER

ARM

614 SAFETY BARRIER, LF PERSONNEL ACCESS

SHAFT

624 JIG625 JIG

629 COVER, PROTECTIVE, LCC FLOOR

632 RAMP-ACCESS, PORTABLE LCC

"0 FLOOR, WIRE-MESH643 LOAD NG PLATFORM - PORTABLE LCF645 DOLLY, LIFT,"TILTING, LCF652 RAILING, GUARD, SUPPORT BUILDING ACCESS

(PORTABLE HANDRAILS)

653 RAILING, HAND, LCC ENTRANCE

654 KIT, PURGE & DRY

655 LEVELING FRAME, SUPPORT AND SUSPENSONSYSTEM, UPPER BRACKETS

656 ADAPTER, HOIST TO BEAM

658 SEMITRAILER, VAN, LF AND LCFASSEMBLY

659 COVER, PROTECTIVE, UMBILICAL CABLE HEAD

670 CONTAINER, ORDNANCE STORAGE

671 HOIST & SUPPORT ASSEMBLY

672 CABLE ASSEMBLY, LF AND LCF PREHEAT

674 CONDUCTIVITY CELL

675 LIFT PLATE

676 SLING

680 SUPPORT, HOIST, EMP R&CK. EMPLACEMENT

683 CRADELE, BALLISTIC GAS GENERATOR

690 CANOPY, ENVIRONMENTAL, LF ACCESS HATCH691 SHELTER, ENVIRONMENrAL

692 BRUSH, ELECTROPLATING

694 STRAP WRENCH696 DENINERALrZATION UNIT, ION EXCHANGE,

TRUCK MOUNTER

697 FIXTURE, TRACK ALIGNMENT

698 CHECKING TOOLi, SIGHT TUBE

699 COVER, END-Q&C SECTION

706 GENERATOR, RINGING707 ELEVATOR & WORK CAGE

708 SUPPORT FRAME, ROLLING

717 BARRIER, SAFETY LAUNCMER OPENING

02-9262- vo.a

.W WfA bosom___._,__,_,____

1.6.2 (CON.)

ACO

730 POWER SUPPLY, D. C.741 TEST SET, PROGRAMMER GROUP

(INTERIM MODEL)

775" ATTENUATOR, VIDEO778 ADAPTER, TEST, G&C COUPLER907 RESISTRo, DECADE914 PROBE, AC CURRENT929 ýTEST SET, POWER SUPPLY

935 TEST TOOL-TEST SET, EXPLOSIVE SCTCIRCUI TRY

0553 TRANSFORMER, RATIO

0554 SHIFTER, PHASE0555 STANDARD, VOLTAGE0558 OSCILLATOR, WIDE RANGE

0559 OSCILLATOR, 400-CYCLE0560 AC - DC CONVERTER, MODEL 100 A CSC0583 KIT, MODULE CONNECTOR, ALIGNMENT

0584 TIME INTERVAL UNIT0585 TRAVERSE TARGET SET0590 VOLTMETER, PREC'ISION, DC, CSC, 200 AR

.0593 RESISTANCE BOX, DECODE0599 SIMULATOR, LOAD

0642 OPTICAL ALIGNI4ENT SET0719 ACCESSORY KIT, OPTICAL ALIGNMENT0721 CABLE SET, OPERATIONAL TARGETING

VEHICLE0722 CASE, HANDLING TAPE0820 SIMULATOR, TEST SET, R/V

3009 PULLER, PRINTED CIRCUIT CARD3022 TRUCK, DOLLY3023 THERMOMETER, SELr INDICATING

3039 FREON LEAK DETECTOR3046 BATTERY FILLER, GRAVITY3059 STOP WATCH3067 VOLTMETER, D. C.3074 TAPE, FISH, STEEL3078 TRUCK, FORK, LIFT3080 TRUCK, TRANSPORTER

3096 SHIPPING AND STORAGE CONTAINER,

ELECTRONIC EQUIPMENT.3119 ADAPTER, SPANNER3126 DITCHING MACHINE, CRAWLER-MOUNTERj

LADDER TYPE3136 AMMETER, 0. C.

- 3140 INDICATOR, DtaiTAL DISPLAY

(1986W ,USV .1W.... " -0"1W

iVOL. XIV

low* aZ

S1.6.2 (CONT.)

(• ACO

4001 MULTINETER4004 OSCILLOSCOPE4006 OSCILLATOR, AUoIO.FREQUENCY4024 SEMITRAILER, G&C - R/V4031 TRUCK, MECHANICAL MAINTENANCE4038 BARRIER, SAFETY, LAUNCHER OPENING4047 WRENCH, SATING PIN4053 ADAPTER HOISTING, STASLIZING RING4054 CRANE, TRUCK MOUNTED4059 SEMITRAILER, T-E AND TxUCK4062 TRUCK, TARGETING4063 TRUCK, ELECTRONIC MAINTENANCE4069 CLAMP ASSEMBLY, MISSIL*E SKIRT TO BASE4075 TRACTOR, T-E4105 TRACTOR, LAUNCHER CLOSURE4107 LEVEL SET, MISSILE BASE SUPPORT4116 TRUCK, TRACTOR (R/V - G&C MAINTENANCE)

4119 TRUCK, T-E SUPPORT4127 POWER SUPPLY4129 TRAILER, BALLISTIC MISSILE4130 TRACTOR, BALLISTIC MISSILE-4141 . TRUCK, DOLLY, TRACTOR, LAUNCHER CLOSURE4144 HEADSET, INTERPHONE, SIN/LCF - LF4146 PLATE, SURFACE

4147 LEVEL, PRECISION, MASTER4160 WRAPPING KIT, SOLDERLESS4172 PLUG-IN UNIT, OSC LLOSCOPE4191 TANK, LIQUID STORAGE, METAL4192 BRIDGE, RESISTANCE4220 TEST SET, RELAY424 HOLDING FIXTURE, HOISTING UNIT4258 WRENCH, TORQUE4263 BARRIER, SAFETY, LAUNCH TUBE ACCESS

DOOR4264 CABLE AND REEL ASSEMBLY, GROUNDING

MISSILE4265 PAD, CUSHIONING, MISSILE SLING ROD ENDS4267 COVER, PROTECTIVE, VEHICLE TO ACCESS SHAFT4270 PLUMS BO0 SET, T-E4271 COVER, FITTED, T-E4278 SHETTER, ENVIRONMENTAL, T/E TO LAUNCH

TUBE4285 HEATER, DUCT TYPE, PORTABLE4286 DRAIN UNIT COOLANT4292 COVER, ENVIRONMENTAL, LAUNCHER OPENI.NG4305 CYLINDER & VALVE ASSEMBLY4306 PLATE, AoJUSTABLE, T/E HINGE TO PYLON

us .m 0" mv. #ia s.44

REV sy . .f D2-9262, VOL. XJV. " A2

3.6,2 (CONT.)

ACO

4307 RESTRAINT SET, BASE ADAPTER RING TO T/f4319 LEAD SET, TEST4337 ADAPTER, MOTOR.GENCRATOR SET TO DOLLY TRUCx4349 TESTING KIT, PRESSURE, SCN CABLE SYSTEM4369 COUNTER, ROTATING, HAND HOLD

4370 TEST STAND, TRACTOR, LAUNCHER CLOSURE4381 OHMMETER

4382 CORD ASSEMBLY, ELECTRICAL4386 WRENCH SET, ELECTRICAL

4388 TEST SET, TELEPHONE EQUIPMENT

4416 METER, AIR'VELOcITY

4445 STAND ASSEMBLY, T/E CONTROL PANEL4447 KIT, INSTALLAfION REMOVAL, VERTICAL

RESTRAINT MKU-117/E4448 EXTENSIONp MISSILE BASE ADAPTER RING

4451 CONTROLLER, PORTABLE HAND POWERED

AZIMUTH DRivE SYSTEM

4452 TRAVERSE PLATE, LAUNCH TUBE ACCESS DOOR

4456 CONVERTER FREQUENCY

4458 VOLTMETER, VACUUM TUBE4460 AMMETER4461 AMMETER, AC/DC4471 POWERI METER, MICROWAVE

4472 GENERATOR, FUN'_TION, LoW FREQUENCY

4476 TESTER, PYROMETER AND THERMOCOUPLE4478 THERMISTOR MOUNT, COAXIAL

4480 ATTENUATOR (0-12 06)4484 TOWBAR, MOTOR VEHICLE

4524 WRENCH# PORTABLE ELECTRIC

4525 STOP, RAILCAR WHEEL

4533 TESTER, TORQUE WRENCH AND TENSIOMETER

4534 TORQUE TESTER4535 ALIGNMENT ,SET, MISSILE TRANSFER4537 TESTER, DEAD WEIGHT, HYDRAULIC PRESSURE

GAGE

4552 INDICATOR, PHASE SEQUENCE (60 CYCLE)

4623 TEST, KIT, CHRONRATE

4634 TOOL ASSEMBLY - RESETTING LAUNCHER

CLOSURE ACTUATOR

7600 COVER, END, G&C SECTION7665 KIT, ABLATIVE MATERIAL REPAIR

10700 POTENTIOMETER) DECADE

10701 RECORDER

10702 BRIDGE, IMPEDANCE

10706 PLUG-INUNIT, VIDEO AMPLIFIER10707 PLUG-IN UNIT, OSCILLOSCOPEI' DIFFERENTIAL

10708 POWERSTATO 3-PHASE VARIABLE TRANSFORMER

-02-9262# VOL. iV ..

1203

Vi

F 2.0 PROCESSING OPERATIONS

2.1 CSA ACTIVATION

THE TESTS REQUIREO AND OOCUNMNTATIOIN CONTAINING DETAILED TEST

PROCCOU'RES IOR THE ACTIVATION .OF THE CSA ARC SPECIFIED IN TApe 1.THIS TABLE CO0¥'RS TESTING REQUIRED FOR CERTIFICATION OF ALL ACOEQUI PMENT.

49V D"-9262 V.OL. X .v

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4 rd V4 V 0 4 O

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2.2 PRCAsjsVHLY Tc•rINA '

THE PREA5SEMBLY TESTING REQUIACO FOR OGE PRIOR TO ASSEMMY IN THE

OPERATING CONFIGU.RATION AfULP THE TESTING REQUIREDO FOR PORTASLE

MGE PRIOR TO ITS ENPLACEMENT IN THE SMSB 1 SPECIFIED IN TABLE 2.

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3.0 LAUNCH CONTROL FACILITY TESTING'

THE TES-rS REQUIRED AND DOCUMENTATION CONTAINING DETAILED TEST

PROCEDURES FOR CHECKOUT or EQUIPMENT IN THE LAUNCH CON.TROI.FACILITY ARE SPECIFIED IN TABLE 3.

LV WMA W6 02-9262 V*L. xiV

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4.0 LAUNCH FACILITY TESTING

THE TEBTS REQUIRED AND DOCUMENTATION CONTAINING DETAILED TEST

PROCEDURES FOR CHECKOUT OF EQUIPMENT IN THE LAUNCH FACILITY

ARE SPECIFED IN TABLE 4.

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v s. [0. D2.-9262 VOL. X IV

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SS.0 SMSB TESTING

THE TESTS REQUIRED AND DOCUMENTATION CONTAINING DETAILED 'rE3T

PROCEDURES FOR CHECKOUT Of EQUIPMENT 1IN THE SMSO ARE SPECIFIED

IN TABLE 5.

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mvIYM a Io. D2.9262 VOL. XIVHI __ - * ~IsaT 0A= l l '4IIII

r~e 4 r4 P4 V4

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- ~6.0 INTEGRATION. TESTS

THE TESTS REQUIRED AND DOCUMENTATION CONTAINING DETAILED TEST

PROCEDURES rOR FLIGHT, SQUADRON AND WING INTEGRATIONIEST4hG

ARE SPECITiED IN TABLE 6.

V I I II I I II I.g o 4 w w e m v. a/m" N -

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VOL xiv No096

us 4w w

2.U U.i '.

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-J 1-4 a1 0J

04-

w4 4 W) 0'00

4J 4 1- 4 -4..w4

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FRO I- XI-O0296

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k(..7.0 INTERIM PROCEDURES

ALL INTERIM PROCEDURES, APPLI. CABLE '0 THIS VOLUME, WILL BEDOCUMENTED AS A PART OF PARAM.R/PH 7.0. THESE INTEPIM PRO-

f4EDURES WILL BE IDENTIFIED AtAD COLLATED NUMLRICALLY BYTHEIR IP NUMBERS.

Sin" Re-v. w.'v

REV SYD2-9262. VOL. XI1V

IPAGR4