1401 7185 · PDF filead 1401 7185 __ ... table 3 identifies the testing and procedures...
Transcript of 1401 7185 · PDF filead 1401 7185 __ ... table 3 identifies the testing and procedures...
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.
THE AF PrZ~l COMP ANY
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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PREPARED BY Go, ______
SUPERVISED BY L -43
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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 [email protected]
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
metg2~
An~ ~.-e,~
1 0 0 0 a Q V
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wo 'J t- wa *.* 41
II.4.
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A 0
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00
4N4ADa:* W
00 w
00
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UX U0 nn 0.43 a
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0 -j ai )4 tJCl.0 a hi w~t
K 14 0' 0
*.0 w ILP- I
3 l 4 4 0 .4
4 rd V4 V 0 4 O
.- C4 44 04 N V
4r
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C.A. ~ ?4 , X, 4I
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-4 w
Cr t. LI- 0.4 IL&
z 40.L w
IL a w uz in a -a
0. 0
0 0V)f x F- V
4i A -Kt I-z
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THE PREA5SEMBLY TESTING REQUIACO FOR OGE PRIOR TO ASSEMMY IN THE
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MGE PRIOR TO ITS ENPLACEMENT IN THE SMSB 1 SPECIFIED IN TABLE 2.
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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.
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THE TEBTS REQUIRED AND DOCUMENTATION CONTAINING DETAILED TEST
PROCEDURES FOR CHECKOUT OF EQUIPMENT IN THE LAUNCH FACILITY
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THE TESTS REQUIRED AND DOCUMENTATION CONTAINING DETAILED 'rE3T
PROCEDURES FOR CHECKOUT Of EQUIPMENT 1IN THE SMSO ARE SPECIFIED
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THE TESTS REQUIRED AND DOCUMENTATION CONTAINING DETAILED TEST
PROCEDURES rOR FLIGHT, SQUADRON AND WING INTEGRATIONIEST4hG
ARE SPECITiED IN TABLE 6.
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