ML20125E631

Rev a to Seismic Test Plan of Four Motor-Driven Dampers & Three Control Boxes

ML20125E631
Person / Time
Site:	Hope Creek
Issue date:	05/23/1978
From:	Davies L, Jordan H WYLE LABORATORIES
To:
Shared Package
ML20125E587	List: ML20125E584 ML20125E614 ML20125E631 ML20125E662
References
541-0344-DK, 541-344-DK, NUDOCS 8506130183
Download: ML20125E631 (48)

Text

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• Report Mc. 44C57-1 TEST PROGDURE TEST PROCEDURE NO. 541/0344/ g i

EMM scamfis c samvicts anc svsrsus spour DATE:-

/ I' 8 8 0 sCs toos.aumiss%14LAeama m Revision A twa .sioi m:ns . *t.L*=ons ease somis

. SE:3MIC "'EST PLAN .

OF FOUR MOTOR-ORIVEN DAMPERS l AND

TERIZ CON"RCL BOXES A I

FOR POWERS PIGCI ATCR COMPANY SKOKII, ILI.INCIS jd * ^

APPROVED BY APPROVED BY: _-

1. e FOR: PROJECT MANAGER:

APPROVED BY: APPROVED BY FOR: QUAUTY ENGINEER-APPROVED SY: PREPARED BY 4 "I FOR: PROJECT ENGINEER:

REVISIONS ,o ,-.-.

ape'_ otscup't:= or cuancts  ;

Itav=c. i catz i = Gas asst:TE: i sv i I A I S-22-78 ; _l, 2 and 4  ;RT l Para.1.1 and 1.2 - Added one Cent: 1!

• l Box to test program i

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l4 lRT l MPara. 3.2 - Deleted 8 speci:nen accels l

1 4 i RT l M Para. 3.4 - Celeted 1 monitor channel!

l l4 l RT M Para. 2.6 - Deleted operation of l l l specimens during test l

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Test pitoegowg so, 541/0344/cx PAGE NO. 2 M MMO soewc sawcas ano sysvams Gaour Revision A 1.0 MOUN"'ING 1.1 Specimen orientation The seven (7) specimens, as described in Paragraph 1.2, shall be placed A

.on tihe Wyle Multiaxis Seismic Simulat=r Table such that one of their ,

horizontal axes are paral *,el to the longitudinal axis of the test table.

After completing the required tests, the specimens will be rotated 90 degrees in the horizontal plane and the required tests repeated. All specimens will be tested simultaneously.

1.2 Specimen Description Specimen Power Input /

Nun'ce Description Dimensions Control 1 Mote: een 30" High x 10" Diameter 120V AC/ Manual Damper Switch -

2 Motor-Driven 30" High x 10" Diameter - 120V AC/y.anual Damper Switch 3 Motor-Driven 30" High x 10" Diameter 120V AC/ Con-Damper trol Signal 4 Motor-Driven 30" High x 10" Diamatar 120V AC/ Con-Damper tec1 Signal 5 Centrol Box 6" Long x 8" Wide x 6" Deep 1207 AC/Ma.~.ual Switch 6 Control Box 6" Long x 6" Wide x 4" Deep 24V DC - 0.1" Column of Watar 7 Control Box 8" Long x 6" Wide x 4" Deep 12CV AC - RH A 1.3 Speci=en Tie-town -

The specimens will be mounted on the Wyle Laboratories' test fixtures which will secure them in a vertical orientation. "'he specimens will be attached to the fixtures by using commercially-available, or Customer-provideO hardware. The mounting will simulate the in-service =cunting configurations as closely as practical.

2.0 EXC*TATION 2.1 Resonant Search A low-level (approximately 0.2 g horizontally and vertically) single-axis sine sweep from 1 H: to 50 H: will be performed in each of the thrae orthogonal axes to determine equipment resonant frequencies. The sweep rate,will he one octave per minute. Transmissibility plots of the speci-men response accelerometers will he included in the est report.

Forrn NS 2 4ev 4/74

, , Repar- :c. 4405 -;,

TEST PROCEDuel NQ. 541/0244/ y, PAGE NO. 3 N MU v A#so SYSTEMS GAouP SCitwvC Ste icts l

1 2.1 Si:nultaneous Biaxial Excitation  !

l zach hori: ental axis will be excited separately, but each one will be excited simultaneously with the vertical axis (longitudinal simul.aneous with vertical, than lateral simultaneous with vertical). The hori:en.a1 and ver-ical input acceleration levels will be phase incoherent during the mult frequency tes a.

2.2 Multifrecuency Qualification Tests -

1 The specimens shall be subjected to 40-second duration simulta..eous horizontal and vertical inputs of random motion consisting of frequency  ;

bandwidths spaced one-third octava apart over the frequency range of 1.0 l Hz to 40 Hz as necessary to envelop the Required Response Spectra (RRS). l The amplitude of each one-third octave bandwidth will be independently {

adjusted in each axis until the Test Resp:nse Spectra (TRS) envelcp the i RRS within the limitations of the test machine, as shown in Figure 1.. The '

resulting table motion will be analy:ed at a damping of te per:ent (2%)

.using a spectrum analy=er, and plotted at one-third octave frequency intervals over the frequency range of interest. In addition to the required tes.s, calibration tes.s will be performed. The Zero Period Accelera.ica (::2A) as well as other areas of the RRS could be exceeded in order to mee the peaks of the spec. rum.

Five (5) cperating Basis Iare. quake (CEI) tests, followed by a Design Basis Earthquake (::3E) test, will be performed in each orientation. The CBE and 3BI RRS are shown in Figures 2 and 3, respectively.

2.3 Miche Level Multifrecuency Testing -

(CPTIONAL)

After ce=pletion of the seismic qualification tests described in Para-graph 2.2 above, the specimens can be subjected to higher level mul: - .

frequency testing. The testing will be the same as described in Para- I graph 2.2 except the test level will be increased until the limitations of the tas: =achine are reached (see Figure 1) in each orientation. It should he noted that the machine limit curve shown in Figure 1 exceeds c e RRS for flexibly-mounted instruments shown in Figure 4 at frequen:les abcve 4 Hm 3.0 INSTR::Mzh- AT::N 3.1 Excitation Cen r:1 Control accelerometers will be scunted on the table at locations near the o bases of the specimens.

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. . Pago No. 70 Reptre No. 44037-1 TEST PROCEDutE NO. 541/0344/::K

- PAGE NO. 4 E

sesurw e seawess Ano systaus onour Revisien A 3.2 Soecimen Response A total of four (4) uniaxial piezo-electric accelerometers will be A located on the specimens during the test. Placement of the accelero-meters will be as direeced by the Powers Regulator Technical Representative or the Wyle Test Engineer. TRS plots of the cont:cl and specimen response accelerometers at two percent (2%) damping of the SSE test in each axis and transmissibility plots will be provided in the test repert. Additional accelerometers, if required, are quoted as an cption.

3.3 Elec rical Power Electrical power of 120V AC, 60 Hz, single-phase, and 24V DC will be pro- A vided for operation of the specimens.

3.4 Electrical Moni:crine Cne channel of electireal monitoring will he recorded on an oscillograph 2 recorder to menitor the electrical operation of Specimen 5 during the test j program. This channel will be used to ascertain contact chatter, spurious operation, etc. The oscillograph recorder will contain galvancmeters capable of detecting a chatter duration of 1 millisecond or greater. Addi-tional electrical monitor channels are quoted as a separately-priced option.

3.! Water Pressurs A one-half-inch column of water will be provided for' operation of Speci-men 6.

2.6 ceeratine Conditions The specimens will be tested in the energi:ed condition. A 4.0 AC N_P"ANCE CR*TrtIA The acceptance criteria for qualification tests are that there be no instrument malfunction or failure that would inhibit the nuclear safet/-

related function of the inst:.: ment as determined by the Powers Regulater Technical Representative. Unrestricted acceptance shall require that the folicwing minimum conditions shall not occur, as applicable:

a. Less of output signal, e.g., open or short circuit.

b. Output variations greater than the published ace.::acy over the full range. ,

Form 'C54 2 Rm 4.74

Repor- No. 4405 -1 TEST PROCEDURE NO.

541/0344/::K '

PAGE NO. I N mmh sc:EmnAC Slavicts 440 SYS7 teas GacW

c. Spurious or , unwanted cutput, e.g., relay contact beunce.

NO*I: If contact bounce is detected, the specific data of the test shall be recorded and sub=itted to the Ar:hitect/Ingineer for written disposition of the deviation.

d. Drift of set point or trip setting greater than the published ace =acy over the full range.

e. Calibration shif greater than the published accuracy over the full ranger this parameter need not be determined during vibratory excitation.

f. Struct= al failure, e.g., broken componen s loosened parts or adverse permanent defer =ation whether or not -

device failure results.

g. Less of required performance characteristic, e.g., acility to change state.

h. Loss of pressure-boundary integrity, e.g., leakage.

5.0 IN-PFLVIs3 INSPIO"'ICN .

The records will be checked for quality of perfor=ance af ter each test.

The specimens will be examined for possible damage following all violent tests such as at a severe s rue:=al resonance.

All i=portant vibration effects will be logged.

Photographs wi1*. be taken of any noticeable physical damage that =ay occur, and of, all mounted accelerometers.

6.3 RIPORT Ten (10) copies of a certification-type report will be issued subsequen:

to ecmpletion of testing. This report will be signed by a Registered Professional Engineer and will su=narize the maxis = g levels, natual frequencies, de:sils and rece:mendations concerning deficiencies and repairs, photographs of test setups, acceleremeters, fail 1.res, etc.

The report will also contain a lis cf test equipment used, calibrati:ns, and Instruentatien Log Sheets.

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A PAGE NO.

76 SCIENTIFIC SERvlCES AND SYSTEMS GROUP REPORTNC 44057-1 l

E.WI3IT 1 PCWERS RICULA*CR COMPANY FUNCTIONAL OPERATION TIST PPICC URES AIC PISULT3 e

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1 Page No. 77  ;

Report No. 44057 1 1

I FtMCTIONAL OPERATION TESTS I

Functional Tests on the instruents are to. demonstrate the satisfactory

- operation before, during and after the Seismic Vibration Test. Tests-were conducted as follows:

1. BEFORE SEISMIC VIBRATION TEST 1.1 The instruments listed in this report were all bench tested in accordance with Powers Regulator Company's  !

Test Procedures ( Exhihi: 1 ). Functional l Tests, including proper instrument operation, cali- '

bration, electrical sonitoring, etc., were performed satisfactorily, in accordance with the procedure.

1.2 Test set-Up Each instrument was mounted on the shake-table in a l manner simulating field mounting configuration. -

Figure i shows the pneumatic and electrical inter-connections. It also shows the set-point, in-

. strument output, as applicable, and the necessary air and electrical power supplies.

2. DURING THE SEISMIC VIBRATION TEST -

2.1 Differential air pressure set at 0.5" w.c. was applied to the high side port of the Veltron Transmitter. All electrical power supplies were energi:ed as shown in

, Figure 1 . The damper actuator AH-91 was at half stroke (distance traveled by the shaft).

2.2 The damper actuator NH-95 is an On-Off actor controlled i by a control box, having a selector switch and a red I pilot light.

l 2.3 The_ damper actuator NH-91 was powered by 120 VAC power input. The control input coming from a Hygrotran Trans-mitter and Sensor Models L15-63713 and L15-1813D. The sensar senses the percent of relative humidity of the environment and amplification is produced to the trans-mitter to transmit a 4-20 sade current output.

~2.4 The damper. actuator NH-95 was controlled by an ordinary toggle switch. The actuator was activated during the Seismic Vibration Test.

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Page No. 73 Report No. 44057-1 em

3. AFTER THf SEISMIC VIBRATION TEST Esch instrument was functionally tested and performed satisfactorily

• in accordance with their individual specification. Post Seismic Test functional checks were performed as follows:

i' 3.1 Yeltron Transmitter 500/P232-1212 The input control differential pressure was varied be-tween the range span of 0-1"w.c. , and the output (4-20 ande) response was observed by visually sonitoring the distance traveled by the shaft of the AH-91 damper actuator. At 0" w.c. , the shaft was fully extended; at 0.5" w.c. , the shaft was at half stroke; and at 1" of w.c. , the shaft was fully retracted. The Veltron Transmitter functioned

, satisfactorily.

3.2 Desper Actuator 91

, As mentioned above, with the variation of input current between 4-20 made, the shaft moved proportionally to the ,

input signal. The damper actuator performed satisfactorily.

3.3 Control Box (IM43*H5006A)

The control box contains a red pilot light and a selecter switch interconnected to a terminal block. Electrical

wiring connections were made in such a way that the pilot light and a damper actuator could be controlled by a selector switch. By applying 120 VAC power and turning the selector knob clockwise, the damper actuator 101-95 and the red pilot light on the control box were activated. Observations revealed that the Seismic 3

Vibration Test did not affect the satisfactory perfotaance of the control box.

3.4 Hygrotran Transmitter and Sensor - 1.15-63718 and t.15-181SD Both instruments were tested together with a modulating damper actuator. The hygrotran sensor was tested by introducing steam to the sensor. The sensor sensed the

- increase of relative humidity in the environment and the transmitter immediately responded by transmitting a current output. The output was observed by visually inspecting the damper actuator (NH-91) shaft stroke.

Both transmitter and sensor performed satisfactorily.

3.5 Damper Actuator NH-91

. As stated above, the variation of input current to the damper actustor caused the accustor to retract the shaft.

The ITT control damper actustor was not affected by the seismic vibrations and performed satisfactorily.

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Page No. 79 j Report No. 44057-1 l l

3TDasineFATituator NH-95

.This actuator was functionally tested after the Seismic Vibration Test, together with the control j box. The On-Off selector switch controlled the vol- )

tage. The damper performed satisfactorily.

l 3.7 Dancer Actuator AH-95 The damper actuator was controlled by an ordinary toggle switch. With the switch at the "On" position, the actuator was activated (120 VAC input) and the shaft retracted as required. ,

4. CONCLUSION All instruments performed satisfactorily before, during and after the Seismic Vibration Tests. Each instrument did not deviate fren

'its proper functionir.g requirements. The only abeermality observed '

was the loosening of the shaft adaptor on the NH-91 actuator, which

• fell off due to a loose screw. Neverthless, all instruments were in satisfactory condition after the Seismic Vibration Tests.

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seeSPt CI soes Po6N1 sesE E T 8euMSE R tot sA48Pt E

, Covie .91.

l 30r FINAL.

i e' 4 n

sa usactenta *

.Ptc wunseen iocTii6Mg .g gg ner. se as n.~ isedav ano oAv vet I

POWERS RECul.ATOR COMPANY Sill-319 5440 N. FARCO NONE C Sjsalla i y 51EP CisARACT E RISTICS BNSFECTION PHOCE Dune nEStM.IS l

, 1 VISilAl.

i

} The control box shall be check- la. Visually inspect that all welds shall la. Does the hos comply with

! ed, inspected anel tested in be free of cracks and incomplete pene- Visual requirements stated in

, accordance with the general re- tration of welding materials by assur- Inspection Procedure Step laf

! quirement s of specification ing that the panel is smooth and has

! Sill-319. paragraph 2091. Page no signs of warping, nicking or Yes s/ No

! 1-41 and Paragraples 2249 on grinding on the final finished sur-Pages 1-44 and I-46. All in- face, struments and/or devices in-stalled sh.all have the highest Ib. Visually observe that all instruments Ib. Are all instruments properly availability and the highest are property' fitted on every hole fitted and installed 7 proven reliability. These and that proper tolerances are pro-inst rument s and/or devices vided for each replacement. Yes t/, No

) shoiId conform to the require- .

1 -

ments of the Applicable Nation- Ic. Assure lhet instruments are properly IC. Are the instruments located as

at Codes and Standards selected located as per drawing 8510-N-5049- per referenced drawingt i

~

as the best commerclally avall- IH43-DSPA.

j able that cosild perform satis- Yes [ No j factority under the operating i .ind environmental conditions Id. Observo that all electrical connections Id. Do all electrical connections as designed. This procedure are brought to termination on a ter- conform with Step Id? .

would then prove time compati- minal block. II '

bility of the control box to Yes [ No IT ,

perform the services properly ,') g uniler simulated cosiditions. le. Visually inspect that all wiring is le. Is there any presence of pre- g-i identified with pre-printed wrap-on printed wrap-on or slip-on e .=

) or slip-on markers located near both markers? g .

terminations of the wire. . S Yes No ,8 i

]::-.e,a.i...n..,.na.4,see i

! _0

, _ t . . _ . .

p (- f_ ev=<ns sw..an anm cimarany -

{T[p] -*/

nECORD Ol' INSPECTION CONTINUATION SIIEET Nui'l t An SYsit us t u*t~ftAI MWs ,

rant 4scnerinas cant seusseen re nw insesecutat seo. aneway son- -

. son attscuersion Sit 0Ri1LUt NilCI. EAR Potter STATION-lMIT I CONTROI. hept TEST IMIT TEST IMIT 2 .e 4 step CilARACTERIST6CS BNSs*ECIKW4 PROCEDURE RE SUt.TS If. Visisally verify that all internal if. Does all wiring conform with the power wiring is_No. 14 ANG mini- size requirements? j l amen and control wiring is No.18 .,

' AWG minimum. Yes t/ No- .

~

Ig. All wire terminations shall be Ig. Are all terminations properly l made of compression type ring wiredt g

- with pre-insulated sleeves.

Yes ./ No

~

. Ih. Verify that terminal blocks lh. Does the panel conform with thd

- are arranged in such a way that requirements of Step thf outgoing leads are connected to one stile of the Belocks and all ' Yes / No l

, leads to the other side. l

11. Visually inspect that all wisos 11. Is the wiring properly arrange 47 are arranged so that no more than two wires anil a jumper are Yes No  !

connected on the board side of .

the terminal block. ~

f

2. FIMCTIONAL -

This control box is an essential PREPARATl0N:

(safety-related) enclosure. It will i be checked. Inspected and tested in obtain the following instruments '

accordance with the contract spect- and/or devices to test the con- gy fication. Actual operation of the trol leox: , yj control box shall he sinislated by n ff j applying electrical ingnet s . linch I. One (1) Simpson 260 VON , ,

instrument's function (s) shall he or equivalent. , ,'

j observed and be the criteria of * ,

j acceptance. .2. 120 VAC power supply. 8 4

a 3

, e '.

J ns..n.ee .u. . .e. c.n a

'E

t . . _ - - . . . .

/ P. ns n, non Aio c. e Auv

( j[g7],

• 4.. .) flECOllD OF INSPECTION CONTINUATION SilEET .

( ',( nint An systete sa rnaison .

. sos adscsurrioN Pant >E5 CHIP ION rant #eutteEn PLAN 00es tnubM NI 800. $41Et r 800 l SilORfillAM NUCLEAR POWER STATION -CONTROI. BOX TEST IAllT TEST IfMIT 3 ., 4 STEP CH ARACTE RISTICS INSrEc tlON PROCEDURE HESul.15

~

i l

3. One (1) Insulatico Breakdown . J l I

I Tester. Noitel 1113-25 JtNI or ,

I espil va l ent . I

. i 2a. Us18'1 the Sinpaon 260 V0M, per- 2a. Does the electrical wiring i form a point-to-point verifica- ,

conform with referenced drawingt l tion of the electrical wiring with reference to drawing 8510- Yes / No l

N-5049-lH43-ilSWD.

~

. 2b. To find ooit if the switch and 2b. Did the control box conform pilot light are operating, do with the requirements of Step the following connection: 2bf ,,

n. Jaimper terminals: Yes No TR.-2 asal TR-7

• i Tu-3 and TR-8 ,

~

b. Connec't 120 VAC power across - l

,1  ;. terminals .

is , . .

TB-1 moul TR-2 ,

Energite 120 VAC and verify that the red pilot light is "0N". F7 Turn the selector switch clock- 11 wise to "RESliT" position and N g the !!aht stays on. Turn the g.

switch counter-clockwise aml ..

the red pilot light turns off. g" 8a j . . .. , , ~ ~ , . au.

i

-_a

p- POuwits IDEGen. Alan COMPANY -

gQ RECORD OF INSPECTION CONTINUATION SilEET.

y NuctE Att sYs f EMS f art nAlt0N rD 845CKerflota Pani lat senePTION PAntNutAGEn PLA80 ins tnUMENI 800, sufEF000, -

Sil0RI]LVI KUCLEAR STATION - taitT 1 CONTit01. DOK TEST teilT TEST if1tT 4

.e

'4' TEP CHARACTERISTICS : INSPECTION PROCEDURE RESULTS 8 i

l 2c. Ilsing the Vf4I, check that at "NEstiT" position, no continuity 2c.Doescontinuityexistacroy the mentioned terminalst b . .

I g exists across terminals: 1 .i Yes No /

• 1

- . TR-5 and TR-6 l s

2d. Nith the use of clie Insulatiose 24. Is there say breakdown? I Breakdown Tester, Model 103  :

JtEl, perform a high pot check Yes No V' l

~

from groesud to all terminals by .

i applying 1500 VAC for at least  !

one (I) minute, except to those 1 '

terminals traceable to electronic l

Instraments, if any. Breakdo n l e should not occur.* ,  !

2e. He control box mast conform with 2e. Check one

i

~ g the procedure requirements. In-I dicate the disposition of either ACCEPTED acceptance or' rejection. ,

, ,. , ll8JI!C11!D 19 518 t

55 11

'l N I N' l *2

. i 2  ;

. 3

. .i'..

,.....r.... '

4...

g

w 3 72. ,,,. A -

(. /.x_ etwns nEnin Asini enM. ANv p ## gHI RECORD OF INSPECTION meinese er MO TD1' h ' '. , NUCL E All SYSTEMS OPEnAleON

, yg '&

r o s.EsccerisoN on AWeNG NUMet n nE V. Pt.AN WesintAAENT No. Pani NUMet a sYsiE M NuMcE n SlKrl:llAM NilCl.1:AR POWER STATION . 510-Nr5049 N/A N/A -

, an0/P21L2 1212 N/A ragi oEsCCsPisoN P O. es M.T O. DNSP(CilON PO4NT steE E T NUMeE n Loi SAMPLE

!^ I .a 3 i i Feltron Transmi t t e r i waNufACiumEn SPE C. NUMGE n LOCATlON nEF.N M n. i8 esp. SV eso. DAY YA 1;

Ao Air Nuitor '. I Sill-319 OllCA00 SAI.l!S None 5 ,34 78 STEP CHARACTE RISTICS . INSPECTION PROCEDURE . RESUITS

1. VISUAL: Is. Verify that the unit js visually free la. Is the unit free of any visible

~

of :lsmage or evidence or poor workmanship, sign of slamage or evidence of poor workmanship, handling or storage?

lhe Yeltron Transmitter model hanslIlng or storage.

P132 shall be visually free of l l damage or evidence of poor work-  ! ,

Yes v' No ,

manship. handling or storage. i

• l l

The internal f. external views of Ib. Remove the cover hy loosening'the four Ib. Are all the parts'. mentioned in the Model P232 consists of th,e scrows located 'on the sides of.the unit. the visual characteristics presentf following: With cover removed, ve,ify r the internal and external views of the unit as stated Yes /

• No al Two h" threaded female hole in the visual characteristics. ,

for high and low Jifferential .

pressure inputs. . . .

b) A 3/4" threaded outlet for  : 4 .

electrical connections. .

c) An electronic printed cir- ,

cult that operates with 24 IIDC , ,

input and an output of 4-20 made proportional to the pneinna- ,

, g ,

t ic, ininst s.

d) A label stating the follow- .

ing: .

gi y 3 'E Hodel: p232 Range:

S/N:

Spec. No. 1222 I " 11 0 2725 ff *

e) Four (4) 5/16" dia. hole

• for mounting. e'.

- _ _ _ ___________ _ __ __ n

remwins maism Aisnt camowey '.

,- % IIEcollD OF INSPEC180N CON 11NUATION SilEET g

~

NUCe r AH SYSit ta5 (a'i'HAlnWe f ,

me wscnervio ranr msca.cium cani niemen run sie.ume=r no. some r no. .

Sik*l:llAM Nik'I.I!AR POIR R STATION Voltran Transmitter i 800/P232-1212 gj /A y , ,, 3 SIEP CilARACTERISTICS SHSPECilON PROCEDURE RE504.TS

2. FlNCTIONAI.: Obtaln the following:

I The velocity pressure transmit ter a. plffarenttal pressiere source. ' '

P232 is designed to dellter a 4-20 made h. One VitC power supply. i output depending on differential pres- c. One digital VOM or e<pelvalent.

' sure applied from 0-1" of 1920. * -

f Connect wirings as shown belowl Pannes IRAAfJil1[w fjag ,

Joosn~ ** _,_

4, . .

~

• t**Prf.

L L I'

.. . I g4 yo.

vaw *

.. T. * ..

2b. I!nergine the power supply. Walt 2b. Record output reading.

for at least five minutes to warm up.

- Now with no differenttal pressure d. . O madc.

applieel, verify that the oestput reads 4 + .2 made.

2c. Slowly increase clie differential 2c. Record output reading.

pressure to approx. 25" 11,0. Verify that the output increases to 12 + .2 12. .L made.

made. ,

2d. Again slowly increase the dif- 2d. Record outpist reading.

ferenttal pressure to approx. .52" [g, 112 0. Verify that the new output read-16.O made, ga lug now reads 15 + .2 made. dg g'

2

- t O

~

. e. .a.e ,. / . .. g . gist g

~

/ I rimwr ses stl 64:3 AIeNt ENIMPMlY t

(\

' r

,7

) IIECOllD OF INSPfiCTION CONTINUATION SilEET HisCI E All SY:'It MS (2*t'8tATION

L. * ' .

De (Jt SCMePilOta PAllI In hCeter flON pan t NUMeE n PLAN INSinUMENI No. SetE E T 880 -

Silsmi.IIAM NIN lJiAR P00ft:R STATifM4 4 STEP CHARACTERISTICS INSPECT N)N PilOCEDURE REsut.TS

! 2e. Increase again the differential 2e. Record output reading.  ;

j g pressiere to I" 18 20. Vert fy tinat the ,

output read {ng noet reads 20 t .2 gedc.

~

j l 20.0 medc.

l I

2 f. Turn power off and remove all 2f. Check one:

connection after observation. Secure ar.d replace cover. -

Accept / Reject I

I i

l 4

I i

5 i 12 e

. .t*y N'

.m 2

.9 e 6 -'

j es.. sy 4 as e f .ne G/4 3 5

aw.177 ee , A

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• g POwEns nt GutATO64 COMPANY 7gg necono or insrEcTion NUCLE AH SYSTEMS OPinATION

-~~ > e 7-

[g g -* g-[ 7g ,

w on AWGNG NUMSE n nE V. PL AN IN51RuMEN T NO. PANT NuneeE n sYsIE M NuMSE n .

kJaas oE7,CpeePIsON SiluHl.llAH NilCI. EAR l'UWiiR STATION S10-N-5049 N/A N/A

' .. _ .l.15_6321R_A115. .1818 D N/A 4*ei nisCf.sPTiON PO w M TO. thsPE CT EON POeNT sutkT NUMSEn LOT SAMPLE (lygtetr.an p

Transmitter (Surface mounted) FINAL.

.N/A 1 *83 I I pilt_llig[95tilsor & Cable iPEC.NUMef n L OCA TION nEF. N M n. spese SY esO. DAY vfl star.uf ACiuRE n i A>lERICAN INSTRIDIENT CO. 3,,, , ,L 19 ClllCAc0 SAI.lis _

None _

/p 5 JD 78

! STEP CilAR ACTE RISTICS I INSPECTION PHOCEDURE RESULTS I PACKAGING ne flygrotran Transmitter is la. Visibly assure that the shipping con- Is. Is the shipping container free packaged in a corrugated carton. tainer is free from visihte damage due from visible damage?

n e package must be free of to handling or storage.

visilite damage due to handling .

Yes / No or storage. The Ilygrosensor is packaged in a separate box from the transmitter. .

2 VISilAI. .

The flygrotran Transmitter is 2a. Verify that both the flygrotran Trans- 2a. Are both instruments properly identified by a llanufacturer's mitter and the flygrosensor are properly identified?

label showing the following: identified as specified in Step 2 echaracteristics. '

Yes / No YOLT RATING: 115

• SERI AL NO.: (TBD) ,

Record the following: .

A)lPS : 0.2 .

CYCili: 60 llZ @erial 8 of XTER 4 0 66 3 l'l Pil SE: 1 Hodel of Sensor 1 5 -i e,se p yy It has two (2) 1"xt" angle bars 'g g fastened by six (6) screws. con- Cable Model 9 0 - 301- 3'3 y .a taining four (4) 3/8" inside g .0 diameter. for mount ing purposes. ..

The flygrosensor is identified a by its model number stamped

• cn the sensor liousing. A Model e $

lits 8- 301 - 33 Cabic should accom- e'.

pany the sensor.

is s.., o. . t w . eis 2 sesto I

PomERs MEGesLATon coneANY ,

py , RECERD CF INSPECTION CONTINUATION SHEET

~-

NUCLE All SYs1LMG OPEnAT80N ,

os osscn8 Piton PANT DEsculf 88094 flygrut riell Transmit ter Pant tsumeEn Pt.AN Ofes1MUMENT NO. SleEET MO SilCI:llMI Nili'lJiAR l'OWiilt STATION (Surface mounted) willi Ilygrosensor f. Cal le 1.15-6371R 4 1.15 18150 2g 2 STEP CilARACTERISTICS , INSl*ECIlON PHOCEDURE RESul.TS 2b. a) thiscrew the tour (4) screws 2b. Are all connectors properly located at the riglit side of secured? J j

[ t .the transmitter. Connect a l.to VAC power source to ter, Yes No i

minals marked "Il0T", "NfilnRAlf e anti a grointil wire to the ter-minal marked "GNH" DO NOT ENiiRGIZli POWER YliT.

b) Plug the cable to the sensor, c) At the right of the transmit-ter is a terminal block marked A, R, GND, C, and 11 At the end of the cable are multi-

- colored wires, having slip-on markers stellar to the marking s on the terminal block. Con-nect the wires accordingly. .

2c. Now, energize the 120 VAC power. 2c. Record the current reading, lising a digital VOM, measure the current (MAllC) across terminals (Q. 9 MADC -

8 and 9 of the terminal block.

It should be witliin 4-20 made.

2d. Ilsing a sling thermometer, mes- 2d. Record: F 5

sure the wet bulb and dry bulb , n termperatiere of the surrousmilng Wet bulb F 66 dF a t mosplie re. F*

Dry bulb *F 7> *3 3

• y e'

t..a.e, As.m see f osses. ei74 8 F

POmEnt nEcutATOn CObe'ANY

• p RECOfD CF INSPECTION CONTINUATION SHEET

-Y NUCL E An SVSTEMS Ot*tnA100N me exscasenson rant adscneesuwe Pant NumeEn PLAN ensinumawr no. sneer mc Ilygs nt ran Transelt ter SINClillAll Nill:1.liAM Inn!N STATI(#4 (Surface mounteil) witle llygrosensor 4 Cal. le 1.15-63713 4 1.15 18180 3 .e 3 STEP CilARACTERISTICS INSPECTIOM PflOCEDURE RE5ul.TS 2e. liith the aid of a Psychometric 2a. '71  % R.ll. . - ;

g Clia rt , look for the % relative ,

I hussidity based on the wet semi dry

. hulb temperature.

2f. Now, verify that the hygrosensor 2f. Are both Instruments functioning asul transmitter are functioning property?

proporly by comparing the relative

'lusmidity measured by the sensor, Yes / No sind Ril measured lay the use of the-sling thermometer. The transmit-ter gives an outpist of 4-20 made, based on a relative humidity of l .

0-100%. Therefore, the value pe 1% R.ll. Is equal to 0.16 madc.

To check if both readings are correct, divide the current read-ing messiered by 0.16 to get the .

. relative humidity value from the transmitter. .

FF

'a i 1

. ay

• 3 O

.  ?

e m s.e y A en. 4..a e f .,ees. a 74 g

w,I -

ennens accin m enn conne4=v a l572 ,A m j RECORD Cf INSPECTION nu se A O

-- soucttan svsis us net na100N Q 7 ,

i ce scc.e s.ow onaswas muues n ne v ei en wasemu utse eso cane sounsean sestau seuwee a p raise caseary' erarwas uu.vs e d er is ne ses.si.oes eo O/A as : o

_ N/A ensetciease pones IB191 - - - - - - - -

seu ei asuesas a toe MA saueta HiblW EITOR ACTUATOR y/g _ i, 3 ,_ ,

ipsc sounsetn (UCAil00s ~ nGI $$l4 R ekse s'V eAP,. DaT vfl

<usacsunen i IT CENEIUll. 00* Hit 01.S 1-259e AL AGAth A MeUS (llln4g* 5 l 85 l78f I

IEP CHAR ACT ERISTDCS INSPECitON PROCEDURE Af5ULTS W

PACKAGil:G  ;

D.

The ITT Ceneral Controls Hydra- la. Verify that the llydrametor shipping la. Is the leydremotor shipping con-motor Actuator is packaged in container is free of visible damage toiner free of visible damage o corrugated container with from poor handling or storage. from poor handling or storageT.

sufficient insulation. I.abel co carton states as a minimum, Yes / Ile the following:

nill 91

• lb. Verify presence of identifying label Ib. Is label informatten as stated '

HYDRAHOTOR ACTUATOR stating, as a minimous:

la Step lbf 1YPE Wil91 VOLTACE 120 AC Wil91 Yes / Ble INPtif 4-20 MADC. HYpitAM010R ACTilATOR 3 20 VtH.TS 4-20 MADC INPUT -

2. VISUAL <

The leydramotor Actuator ccenststs 2a. Remove Hydramotor from shipping centale - 2a. Is the nameplete informaties af the Actuator Assembly, Yoke er senal locate ITT General Controls name -

correct?

cad Valve Sten Assembly. It is plate. It shall have the following gy '

identifled by a nameplate that Informatlon: Yes / Ile 11 has the following information: "g,.

- ITT GlihP.RAI. CONTIt00.5 g g. '

IIYDRAN01HR VALVP. ..

ITT CENERAL CONTit01.S "

HYDRA.WTOR VALVE . .

ACTUATOR NO.W H91 Actuator No. tutSt ,

8 Serial No. Gil Type Mit y Voltage r ,

o.. 2,. ..e,.. s . ~ s a z .s n. .

I

- . - . . ... - . _ . . . .. - .< , . - , . . . ~ . . - - . m ._ . .

. . ~ . . . , ,

Pimens nrslutaton CfWPANY

[ff ,

HECORD CF INSPECllON CONTINUATION SilEET eartt An sysit ar Urs nAs um

1. ' A I D 5 M8F3 8 N PAntNuneeta PL AN aNsinuuf MI NO. sHEt t NG INllYli aurlY STATION tlNITS I fe 2 IlYI)I&ggTfM Af*'lllATult W141 N/A y et 3

• STEP CIIARACTERISTICS INSPECilON PDOCEDUllE RESULTS .'

The unit shall.be free of fraces of 2b. Visually check for traces of ot t 2b. Is the Hydramotor free of visible oil leniks and shall have proper iden. Isaks, proper IJentification of damage or evidence of poelt work-tification of terminals. W!rlog terminals and general appearance manship, handling or storaget and general appearances Jhall be nest. of the inolt. Wiring must be neat 1 Foreign bodies must be absent in asul foreign bodies minst be absent Yes [ No  !

unit. In tlie unit.

3. FIACTIONAl. *-.

With 120 VAC applied to the hydramoton , 3a. Remove the terminal plate cover

• 3a. Did the actuator operate smoothl*

and 4-20 HADC current, the stem oper- (turn CCW) and connect 120 VA' to when the current input signal ,

ating pull-type shall move proportion- the Ilne terminals 4 and L2. was appliedt i al to the input current signal it Connect a 4-20 MADC to low voltage 3 receives. At 4 HADC the stem shall terminals covered by an lasulation Yes / No j start to move and reaches the complett< barrier. .

stroke at 20 MADC. *

• Now apply 120 VAC power and pro-portionally apply the 4-20 MADC input signal. The stem shall start to move at 4 MADC. It shall be smooth and consistent. -

3b. Slowly increase the input signal 3b. Have the requirements of Step ,

to approximately 12 MADC. Verify 3b been confiramit l that the stem has traveled 1 3/4.

or half the complete stroke. Yes / No ,

3c. Increase further the input signal 3c. Record the distance traveled:

to 20 MADC. Check that the E *,

hydramotor has completed a full S bz " 3T power stroke. Distance traveled U y

. shosId he 3 I"t s 3/g". Record the input signal: g-

@. 2 MADC y 8

- ,1 ses.eg Faseaser innene. rete 8

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.l j M

8 2g'*

T 8

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E nW A e-t P he .

C t r N fr O oe I

T E ne oc R

YAN U in N UN I

D t a A E it P

MINIA C sp oe OT Mf O R

pc '

CNP se .

P nOO N ie d

O C SM f

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T hh 2

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i D

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tt i

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nC M A S t n sE A l

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nP L T I cri t S L C iet dtc N A OI NE t

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P N l

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N 3 D 4 5 A R ia R O l De .i , . ,- ,'

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A 9 ,

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7 .

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• 5 73 ** A .

TM , RECORD CF INSPECTION ,,,, & g/f7

- ' ' wuctsau sysuus orananow / ._ e

" ..v_yt.1'Iob07 j

• is os sca.e sion onawee+o wousen ne v etau m sunumeur n o rans numee n sysseu muuesa '

~~~~~~~*

_LA s Atr e ceoup s womed vomsig U/A M/A ,

M/A INbl$[lN5bRACTUATOR 4/A Mpene j pet pec. I es 3 8. s u u5 Aclu Ea , iPE C. NUuSE n 1OCA HON nEF.N he A. msP. SV MO. DAY YIL 11T CENERAL CON'IROI.S J tr9. _ Atayana uoue cowe. s lss;he LIEP CHAR ACTERISilCS I INSPECTION PROCEDURE RESut.T5

1. PACKAGING The ITT General Controls llydra- la. Verify that the Ilydramotor shipping a. Is the Ilydramotor shipping motor Actuator is packaged in . container is free of, visible damage container free of visible damage o corrugated shipping container from poor handling or storage. from poor handling or storaget uith sufficient insulation. '

1.ahel on carton states as a min-

~

! Yes # No inum, the following: l Nil 95 REVERSE lb. kerify the presence of identifying Ib. Is label information as stated ilYDRM10 TOR AC1UATOR label stating, as a alnimum: in Step lbf Pull. TYPE 120V 60/50 CY  ;

• Nil 95 REVERSE . Yes / No 3 IlYDRMIOTOR ACTUATOR

' Pul.I.1YPl! 120 V 60/50 CY

2. VISUAL.

I The IlyJramotor Actuator consist: 2a. henove IlyJramotor from shipping contain - 2a. Is the nameplate information of the Actuator Assembly. Yoke er and locate ITT Ceneral Controls correct?

cnd Valve Sten Assembly. It is nameplate. It shall have the following identified by a nameplate that jnformation: Yes / No has the following information:

ITT CliNERAI. CON 11t01.S E' I ITT CI'NERAL CONTROL.S llYDRAFEllDR VAI.Vi!

• 3$

I el g IlYDRM10 TOR val.VE Actuator No. N! IDS g.

ACTUATOR NO. Nil 95 Sorial No. Oil Type Mit . .

VOI.TAGE VAC

• Hol.HING AHl'S Voltage VAC

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-lhilding_ N 15 AHl'S AT 120 VAC _AH1'S 15 Mll'S AT 250 VAC AM!'S at 120 VAC ,8 AN1'S nt 240 VAC e-.

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som s4scasevipse Pant adscneP300N PAny NunesEn et Age geestatutagNT peo. SeeEE r MS.

I ..Sa I ie Count y St at ion thii t s I f. 2 3gygytANOTUll ACrllATolt Nil 95 1118 9 5 2 .e 3 STEP CilARACTERISTICS INSPECTION PROCEDURE . RESUL.YS Thp unit shall~ be free of traces of 2b. Visually clieck for traces of oil 2b. Is the flydramotor free ofj visible  ;

oil leaks and shall have proper iden- leaks, proper identification of damage or ovidence of pepr work-*

tification of terminals.y Wiring and terminals and general appearance manship, handling or storage?

g'eneral appearances shall be nest. of the unit. Wiring must be neat , t Foreign bodies must be absent in unit. and foreign bodies unest be absent Yes / No in unit.

3. FINJCTIONAL Alimitswitchislocatedwithih 3a. Remove the terminal plate cover 3a. Did the actuator operate smoothlf actuator motor housing. With 120 VAC (Turn ccw) and apply 120 VAC frasp with power applied and reture to, applied to the Ilydramotor actuador, a regulated power supply to the ' normal relaaed position upon pow-the stem operating pull-type shall liydramotor "line" terminals, and er failure?

complete a power stroke. At this observe the stem and spring motion .

point, the limit switch will de-ener. It shall be sanocth and consistent. Yes # llo -

gize tiie piump motor and the stem shall When power rietyly has been removed ,

remain in full pull position. When stem shall return to full eatended the llydreotor is de-activated, the position. .

sten shall return to normal position. l With 85% of full power,102 VAC, the 3b. Now, asyly 102 VAC, 85% of norant 3b. With 85% of normal voltage, did l actuator stem shall move in a smooth voltage, and verify that the the stem move without stalling nonerratic manner without stalling, actuator stem neoves thru the re- , or erretic behavior? ,

and the actuator relay shall not spaired stroke without stalling have a "hus" evident from a distance or operating in an erratic manner. Yes llo o f 12" . Maintain power, l'*

3c. With 85% of normal voltage, there 3c. Was a " hum" evident with the 'g j shall be no similble relay hun at voltage dropped 85% normalf g

. a distance of 12" from the actua- E tor. Yes No 7 f *,

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p3 exscar: sow ranisssenerIHos Pani DetmesEn PLAs0 seesfautetdef eso, seWEf 884 t S. IIe Couisty Stat ion linit s I 4. 2 flygigtAMirtDR AC11ANIDit M195 Mt95 3 es 3

STEP CHARACTERISTICS INSPECTION PROCEDURE RESUI.TS g 9

The stem travel of the ta195 Actuator 3d. Noting the position of the stem 3d. Itecord shaft travel:

with 6" scale, activate the actus-

/

is to be set'at 38"81%. i 3 %, inches. t I tor with a 120 VAC and measure ,

stem travel at full stroke. It shall be 3'a"13/8".

z Itemove power. Return actisator i to shipping container.

4. ACCESSORIES AND INSTIttA.*T100tS 1

Included with Hydremotor ActuatM is 4a. Verify the Bulletin for Installa- 4a. Is the proper Sistleting present?

the Installation, Calibration and tion, Calibration and Adjustment Adjustment Manual for the M195 Actua- of the Nil 95 Actuator is inclieded Yes # IIe

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t or, with shipment of flydramotor Actus-

- tor.

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! *- Indicate disposition of Acceptance ACCEPTED #

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• or Rejection.

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{ uae.ufAC1unEn SPEC peuteeE A iOC510'Oes REF. N to R. 18:5P. eV M

! ITT GENERAL CONTROLS

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INSPECTION PROCEpuRE RESutTS

s l 1. PACKAGING ,

The ITT General Controls la. Verifr t that the Hydramotor la. Is the Hydramotor shipping i Hydramotor Actuator is eshippang container is free of , container free of visible packaged in a corrugated l ivisible damage from poor hand- damage from poor handling j

or storage?

shipping container with . ling or storage.

sufticient insulation. .

Label on carton states as a Yes / No minimum, the following:

lb. Verify presence of identifying Alt 95 label stating gas a minimum: lb. Is label information as i HYDRAMOTOR ACTUATOR stated in si.ep lb?

PULL TYPE 120V 60/50 CY AH95

' HYDRAMOTOR ACTUATOR Yes / No l

PULL TYPE 120 V 60/50 CY l .

i .

2. VISUAL: 2a. Remove Ilydramotor from shipping ,2 a . Is the namsplate informa-j container and locate ITT General tion correct?

i The Hydramotor Actuator Controla nameplate. It shall

}' consists of the Actuator have the following information: Yes / No ge Assembly; Yoke and Valve ag.E*

, Stem Assembly. It is iden- ITT GENERAL CONTHOLS n tified by a nameplate that HYDRANOTOR VAINE I has the following informa- E' tion: Actuator No. A1195 .

j Serial No. Oil Type N1) [

. ITT GENERAL CONTROLS Voltage VAC 3 l.

j' _.. IlYDRAMOTOR VALVE Running AMt*S .

! ACTl1ATOR NO. KH95 lloiding AMPS o . .., e. .. .. . e . e. n 2 . . n .

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.SAI.ll! 00lWlY STATION llNITS I 4 2 HYDRAMOTOlt ACTUATOR _ Al(' i N/A l . ., '

f INSPEC110N PROCEDURE RESULTS fvI CIIARACTERISTICS i I

2. VOLTAGE VAC ,

2a. (continued) t RUlillING AMPS ilOLDIllG AMPS ~

Amps at 120 VAC 15 AllPS AT 120 VAC Amps at 240 VAC 15 AMPS AT 240 VAC The unit shall be free of traces 2b. Visually check for traces of 2b. Is the Hydrassotor free of of oil leaks and shall have pro- oil leaks, proper identifi- visible damage or evidenc's

• per identification of terminals. cation of terminals and gen- of poor workmanship, hand- -

Wiring and general appearances eral appearance of the unit. ling or storage?  :

chall be neat. Foreign bodies wiring must be neat and for-

• must be absent in unit. eign bodies must be absent Yes / No

3. FUNCTIONAL: in unit. f A limit switch is located within cctuator motor housing. With 3a. Remove the terminal plate 3a. Did the actuator operate e 120V AC applied to the Hydra- cover (Turn ccw) and apply smoothly with power applied motor actuator, the stem opera- 120V AC from a regulated and return to normal relaxed ting pull-type shall complete power supply to the Hydra- position upon poiter failure?

o power stroke. At this point, motor "line" terminab, and the limit switch will de-energina r observe the stem and spring Yes / No the pump motor and the stem shal' motion. It shall be smooth remain in full pull position. and consistent. When power l When the flydramotor is de-acti- supply has been removed, , i vated, the stem shall return to ,

stem shall return to full ,

normal position. ,

extended position. . ,

Nith 85% of full power, 102V AC, 3b. Now apply 102V AC, 85% of 3b. With 854 of norinal voltage F ;

t.he actuctor stem shall move in nomal voltage, and verify did the stem move without 1 1 a smooth non-erratic manner that t.he actuator stem stalling or erratic behavi,'i without stalling and the actua- moves thru the required tor relay shall not have a " hum" stroke without stalling or Yes No .E* E ovident from a distance of 12". operating in an errati manner. Maintain popea. k U

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• NUCLEAR SYSTEedS OPERATION

, ",7 PARIpgUMSER PLAN IN518tubMNT feO. 86EET No. i l JOD id 5CAstitON PAAF DESCR8PilON IlYDRANOTOR ACTUATOR AH95 N/A 3 ,, 3 I 1.asalle umuty Stat ion linits 1 4 2 CHARACTERISTICS INSPECTION PROCEDURE RESULT 3 I STEP 3c. With 85% of normal voltage, 3c. Was a " hum" evident with the 5

there shall be no audible voltage dropped 854 ndrinal?

1 relay hum at a distance of '

j 12" from the actuator. Yes No /

rhe stem travel of the AH95 Act-I i nator is to be set at 3 1/2"114. 3d. Noting the position of the 3d. Decord shaf t - travels

.. stem with a 6" scale, acti-j .

+ vate the actuator with a S h ,, inches.

120V AC and measure stem l

travel at full stroke. It shall be 3 1/2" t 3/8".

l

. Remove power. Return actua-tor to sh1pping container, f 4. ACCESSORhES AND INSTRUCTIONS: .

I Included with Hydramotor Actua- 4a. Verify that Bulletin for 4a. Is the-proper Bulletin.

l tor is the Installation, Cali ,

Installation, Calibration present?

l aration and Adjustment Manual and Adjustment of the AH95

• for the NI95 Actuator, Actuator is included with Yes g No ~

l shipment of flydramotor Aot-untor. .

l Indicate disposition of '

Acceptance or Dejection. Accept / Reject F .,,

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' INSPECTION PROCEDURE RESULTS

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l 1. PACKACING  :

l i The 11T Ceneral Controls llydre- la. Verify that the llydramotor shipping la. Is the Hydramotor shipping con-4 motor Actuator is packaged in container is free of visible damage toiner free of visible damage

, a corrugated container with from poor handling or storage.

from poor handling or storage 7 sufficient insulation. Label on carton states as a minimum, ,

Yes / Ito the following: ,

l i Nil 91 . . . Ib. Vprify presence of identifying label Ib. Is label luformattom as stated i llVDRAnt1 TOR ACTUATOR sltating, as a minimium: l An Step lbf I

i 1YPE Nil 91 REVERSE '

l VOLTAGE 120 AC Nil 91 REVERSE , ,

Yes [ Ho i INPiff 4-20 MADC. IlYDIIANDToll ACTUATOR I

j 120 V01.TS j 4-20 MADC INPUT l

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! 2. VISilAL

! The flydramotor Actitator consists 2a. Remove Ilydraanotor from shipping contain - 2a. Is the nameplate information l of the Actuator Assembly. Yoke er and locate ITT Ceneral Controls name -

correct?

l and Valve Sten Assembly. It is plate. It shall have the following 2' I

! identified by a nameplate that infonimation: Yes- No ]I l has the following information: et g l ITT GENERAL. CONTROIS g-ITT GENERAL. CONTROLS IIVIHtANIFIOlt VAI.VE g

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IlVDRAMOTOR val.VE ,

l AC1UATOR HO. Nil 91 Actinator No. 18895 ,

,3 i Serial Nu. Oil Type Mil  ?

! Voltage

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sus tescnie ioes rant isEsenerisose rany poussesa et AN 000sInua4ENI feo, sH(1i 880 1.aSaIIe Cousity Station thiits i 4 2 N/A 2 ,, 3

. STEP CilARACTERISTICS INSPECTION PHOCEDURE RE5utTS-11 e unit shall be free of ' traces of 2b. Vissially check for traces of oil 2b. Is the flydramotor free of visible oil leaks and steell.have proper iden- leaks. proper identification of damage or evidence of peer work-Wirl4:3 terminals and general appearance manship. handling or stgrage?

tification and general ofappearances terminals., shall be nest. of the unit. Wiring must be neat Foreign bodies must be absent tai and forolgn bodies must be absent Yes [ No I l

unit. in the unit. .

3. FUNCTIONAL -

f l

With 120 VAC applied to the hydramotor . 3a. Remove the terminal plate cover . 3a. Did the actuator operate smoothly and 4-20 MADC current, the stem oper- (turnCCW)andconnect120VACty when the current input signal -

ating pull-type shall move proportion- the line terminals 4 and L2. . was applied? I at to the input current signal it Connect a 4-20 MADC to low voltage receives. At 4 MADC the stem shall terminals covered by an insulatten Yes / lio start to move and reaches the comple ei; barrier. l'

• stroke at 20 MADC. I Now apply 120 VAC power and pro-portloosally apply the 4-20 MADC input signal. H e stem shall j start to move at 4 MADC. It shall be smootle avid consistent. .

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3b. Slowly increase the input signal 36. Ileve the registrements of Step to approximately 12 MAIIC. Verify 3h been confirmedt that the sten has traveled 1 3/40 or half the complete stroke. Yes [ Ito 3c. Increase further the inpist signal Sc. Record the distance traveled: y; to 20 MARC. Check that the 'gj hydramotor has completed a full Sh "

g power stroke. Distance traveled should be 3 I"t n 3/en, secord the input signal: 5 y.E o

a, e 20.0 MADC $

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j D' RECORD CF INSPECTION CONTINUATION SHEET

• NUCLt AM Sysyf teS OPf RATOON joe IM 5CR4PT80N PART 84SCRIPy40N PART 9euteeEA PLAgetoestWUteENT000. El8EET 000 l.asAI.lj! OMNIY STATIOff IINITS I 4 2 IlYllRANDTOR ACTilATUR 18893 N/A 3 ,, 3  !

STEP CHARACTERISTICS INSPECTION PROCEOuftE RESUt.TS i

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!.  ! Recorddistencetravelojat 20 NADC 3 4

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1 3d. Indicate the disposition of the 3d. Check ene: 3

' Gotor, either ecceptance or re- l

. jection. ACCEPTED [ .

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1-i I-k ATTACHMENT II ,

Response to SQRT Equipment Specific Open Item B.1 -

' Approximation of Instructure RRS Using Input Response

-Spectra and-Transmissibilities Obtained from Test, prepared

by General Electric Company, May 1985.

DJDadb

' OP 07l03/04A E'

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