Text

Cycle 4 Startup Physics Test Rept
	ML20073K138
Person / Time
Site:	North Anna
Issue date:	03/31/1983
From:	Ford C, Lozito E, Snow C; VIRGINIA POWER (VIRGINIA ELECTRIC & POWER CO.)
To:	;
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ML20073K035	List: ML20073K032; ML20073K138;
References
	VEP-NOS-2, NUDOCS 8304190542
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VEp-NOS-2 s

NORTH ANNA UNIT 1,

CYCLE 4 STARTUP PHYSICS TEST REPORT BY C.

Alan Ford Reviewed by:

Approved b :

c.1 La E

ork C.

T.

Snow, Supervisor Lo=i/6 L Director Nuclear Fuel Operation Subsection lear Fub2 Operation Subsection Nuclear Fuel Operation Subsection Nuclear Operations Department Virginia Electric and Pouer,Co.

Richmond, Va.

March, 1983 OCK o!hjg p

PDR

CLASSIFICATION / DISCLAIMER The data,. techniques, information, and conclusions in this report have been ' prepared. solely for use by the Virginia Electric and power Company (the-Company),

and they may not be appropriate for use in situations othar' than those for which they were specifically prepared. The Company therefore makes no claim or warranty whatsoever, express or implied,as-to.their

accuracy, usefulness, or applicability. In particular, THE COMPANY MAKES MO WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR

PURPOSE, NOR SHALL ANY WARRANTY BE DEEMED TO ARISE FROM COURSE OF DEALING OR USAGE OF TRADE, with respect to this report or any of the

data, techniques, information, or conclusions in it. By making this report available, the Company does not authori=e its use by others, and any such use is expressly forbidden except with the prior written approval of the Company.

Any such.uritten approval shall itself be deemed to incorporate the disclaimers of liability and disclaimers of warranties provided herein.

In no event shall the Company be liable, under any legal theory whatsoever (whether contract, tort, warranty, or strict or absolute liability),

for any property damage, mental or physical injury or

death, loss of use of property, or other damage resulting from or arising out of the use, authori=ed or unauthorized,'of this report or the data, techniques, information, or conclusions in it.

9 s

i

- ACKNOWLEDGEMENTS.

The author would'like to acknowledge the cooperation of the North Anna power-Station personnel in performing the tests documented in this report.

Also, the author would like to express his gratitude to Mr.

C.

T.

Snow and Dr.

E..J.

Lozito for their aid and guidance in preparing this report.

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f TABLE OF CONTENTS SECTION TITLE PAGE NO.

Classification / Disclaimer..................

i l

Acknowledgements...........................

ii List of Tables.............................

iv List of F1gures............................

v Preface....................................

vi 1

Introduction and Summary...................

1 2

Control Rod Drop Time Measurements.........

10 3

Control Rod Bank Worth Measurements........

15 4

Boron Endpoint and Worth Measurements......

21 5

Temperature coefficient Measurements.......

25 6

Power Distribution Measurements............

29 7

References.................................

38 APPENDIX StartuP Physics Test Results and Evaluation Sheets..........................

39 s

I e

iii

LIST OF TABLES TRBLE.

TITLE PAGE NO.

1.1 Chronology cf Tests................................

4 2.1 Hot Rod Drop Time Summary..........................

12 3.1 Control Rod Bank Worth Summary.....................

18-4.1 Boron Endpoints Summary............................

23 5.1 Isothermal Temperature coefficient Summary.........

27 6.1 Incore Flux Map Summary............................

31 G.2 Comparison of Measured Power Distribution Param-eters With Their Techn:r a specifications Limits...

32 iv

4 LIST OF FIGURES 4

FIGURE TITLE PAGE NO.

1.1 Core Loading Map.........................................

5 i

1.2 Beginning of Cycle Fuel Assembly Burnups.................

6 1.3 Incore Instrument 4 tion Locations.........................

7 1.4 Burnable Poison and Source Assembly Locations............

8 f.5 Control Rod Locations....................................

9 2

2.1 Typical Rod Drop Trace...................................

13 2.2 Rod Drop Time - Hot Full Flon Conditions.................

14 3.1 Bank B Integral. Rod Worth -

HZP..........................

19 3.2 Bank B Differential Rod Worth - HZP......................

20 4.1 Boron Worth Coefficient..................................

24 5.1 Isothermal Temperature Coefficient - HZP, AR0............

28 4

6.1

. Assembly Power Distribution - HZP, AR0...................

33 6.2 Assembly Power Distribution - 29%

P0WER..................

34 I

6.3 Assembly Power Distribution - 52%

POWER..................

35

6. 4 '

Assembly Power Distribution - 96%

P0WER..................

36 6.5-Assembly Power. Distribution - HFP, Eq. Xenon.............

37 i.

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PREFACE The purpose of_ this report is to present the analysis and ovaluation of the physics tes ts which were performed to verify that the North Anna 1,

Cycle 4

core could be operated safely, and to make an initial evaluation of the performance of the core.

It is not the intent of this report to discuss the particular methods of testing or to present the detailed data taken. Standard test techiques and methods of data analysis were used.

The test. data, results and evaluations, together with the detailed startup procedures, are on file at the North Anna power Station.

Therefore, only a cursory discussion of these items is included in this report.

The. analyses presented includes a brief summary of each test,.

a comparision of the test results with design predictions, and an evaluation of the results.

The. North Anna 1,

Cycle 4

Startup physics Tests Results and Evaluation Sheets have been included as an appendix to provide additional information on the startup test results.

Each data sheet provides the following information:

1) test identification, 2) test conditions (design),

3) test conditions (actual), 4) test results,.5) cceeptance. criteria, and 6) comments concerning the t'e s t.

These sheets provide a.

compact summary of the startup test results in a consistent format.

The design test conditions and design values of the measured parameters were completed prior to startup physics testing.

The entries for the design values were based on the calculations performed by Vapco's Nuclear Fuel Engineering Group 1 During the tests, the data chsets were used as guidelines both to verify that the proper test v1

conditions were met and to facilitate the preliminary comparison between measured and predicted test

results, thus enabling a

quick identification of possible problems occuring during the tests.

The Appendix to this report contains the final completed and approved version of the Startup Physics Tests Results and Evaluation Sheets.

vii

Ssction 1 INTRODUCTION AND

SUMMARY

On M a'y 17, 1982, Unit No.

1 of the North Anna power Station was shut down for its third refueling.

During this shutdown, 69 of the 157.

fuel assemblies in the core were replaced with fresh fuel assemblies.

The core loading pattern and the design parameters for each batch are shown in Figure 1.1.

Fuel assembly burnups are given in Figure 1.2.

The incore instrumentation locations are identified in Figure 1.3.

Figure 1.4 identifies the location and number of burnable poison rods and source as s emblie.s in the Cycle 4

core.

Figure 1.5 identifies the location and number of control rods in the Cycle 4 core.

On November 18, 1982, at 4:49 p.m.,

the fourth cycle core achieved initial criticality.

Following criticality, startup physics tests were parformed as outlined in Table 1.1.

A summary of the results of these tasts follows:

1.

The drop time of each control rod was confirmed to be within the 2.2 second limit of the North Anna Technical Specifications 2 2.

Individual control rod bank worths for all control rod banks were measured using the rod swap technique 3 and were found to be within 10.3% of the design predictions.

The sum of the individual control rod bank worths was measured to be within 6.6% of the design prediction.

These results are within the design tolerance of 215% for individual bank 1

worths (!10% for the rod swap reference bank worth) and the design tolerance of 110% for the sum of the individual control rod bank worths.

3.

Critical boron concentrations for two control bank configurations were measured to be within 6 ppm of the design predictions.

These results were within the design tolerances and also met the accident analysis acceptance criterion.

4.

The boron worth coefficient was measured to be within 2.2%

of the design predication, which is within the design tolerance of 110% and met the accident analysis criterion.

5.

Isothermal temperature coefficients for the all-rods-out configuration was measured to be within 1.7 pcm/*F of design prediction.

This result is within the design tolerance of 13 pcm/*F and also meets the accident analysis acceptance criterion.

6.

Core power distributions for various HZp and at power conditions were. generally within 6% of the predicted power l

distributions.

For all maps, the hot channel factors were measured to be within the limits of the Technical Specifications.

Generally, all measurament parameters met their respective design value tolerances.

All I

measurement parameters met their respective accident analysis acceptance criteria.

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In

summary, all startup' physics test results are acceptable.

Datailed

results, together with specific ~ design tolerances and

-acceptance

-criteria for each measurement, are presented -in the appropriate sections of this report.

.3

Table 1.1 NORTH ANNA 1 - BOL CYCLE 4 PHYSICS TESTS CHRONOLOGY OF TESTS a

i l

l l

l Referencel l

Test i

Date l Time'l Power l Procedurel l

I I

I

-l Hot Rod Drops-Hot Full Flow 111/17/821 2200 i HSD 1 1-PT-17.21 l Flux Map-ARO 111/19/821 0537 1 4%

-l 1-PT-21.11 l Reactivity Computer Checkout 111/19/821.0824 l HZP l 1-PT-94.21 l Boron Endpoint-ARO 111/19/821 1129 I HZP l 1-PT-94.31 1 Temperature Coefficient-ARO 111/19/821 1327 i HZP l 1-PT-94.41 l Bank B Worth 111/19/821 1516 I HZP l 1-PT-94.51 l Boron Endpoint-B In 111/19/821 2035 i HZP l 1-PT-94.31 l Bank C Worth --Rod Swap 111/19/821 2332 l HZP l 1-PT-94.71 l Bank A Worth - Rod Swap 111/20/821 0024 I HZP l 1-PT-94.71 l Bank SB Worth - Rod Swap 111/20/821 0106 i HZP l 1-PT-94.71 l Bank SA Worth - Rod Swap 111/20/821 0149 i HZP l 1-PT-94.71 l Bank D Worth - Rod Swap 111/20/821.0312 i HZP l 1-PT-94.71

! Flux Map - I/E Calibration 1 3/14/831 1223 1 29%

i 1-PT-22.21 1 Flux Map - I/E Calibration 1 3/14/831 1609 l 29%

1 1-PT-22.21 1 Flux Map - I/E Calibration I 3/14/831 1810 1 29%

i 1-PT-22.21 l Flux Map - I/E Calibration 1 3/17/831 0913 l 52%

1 1-PT-22.21 1 Flux Map - HFP, Eq. Xenon 1 3/24/831 1241 l 100%

i 1-PT-21.11 1

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Figure 1.1 NORTH ANNA UNIT 1 - CYCLE 4 CORE LOADING MAP' s

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FUEL ASSEMBLY DESIGN PARAMETERS 4A2 SA 6A Initial Enrichment (w/o U235) 3.21 3.40 3.59.

Burnup at BOC-4 (MWD /MTU) 26,211 14,868 0

Assembly Type 17x17 17x17 17x17 Number of Assemblies 24 64 69 l

Fuel Rods per Assembly 264 264 264 5

Figure'1.2 NORTH ANNA UNIT 1 - CYCLE 4 BEGINNING OF CYCLE FUEL ASSEMBLY BURNUPS E

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i Section 2

{

' CONTROL' ROD DROP TIME MEASUREMENTS

,I W

_The drop time of each control rod-uas measured-at hot RCS

. conditions in order to confirm satisfactoryJoperation and.to verify.that the rod drop-times were less than the maximum allowed by the Technical Specifications.

The hot. control rod drop time measurements were run 4

with the RCS at hot,' full flow conditiens ( 547

'F, 2235 psig).and are i

_ described below.

The rod drop time measurements were performed by first withdrawing a' ~ rod bank to its. fully withdrawn position, and then re, moving the-movable gripper coil fuse and stationary gripper coil fuse for the test rod.

This allows the rod to drop into the core as it would in a normal plant. trip.

The data. recorded' during this test are, the stationary 1

gripper coil

voltage, the LVDT (Linear Variable Differential i

Transformer) primary _. coil voltage and a 60Hz timing. trace which'are recorded using a visicorder.

The rod drop time to the dashpot entry and L

to the bottom of the dashpot are determined from this data.

Figure 2.1 1

j provides an example of the data'that is recorded during'a rod drop time I

[

'msasurement.

l-As shown in Figure 2.1, the initiation of the rod drop is indicated-i by the decay of the stationary gripper coil voltage when the stationary 4

i coil ' fuse is. removed.

A voltage is then induced in the LVDT primary I

f

. coil-as the rod drops.

The magnitude of this voltage is a function of thn-rod. velocity.

Whe'n the. rod enters the dashpot section of its guide 3

i 10

..a-

1

tube, the velocity -slous. causing 1a voltage decrease in the LVDT coil.

The LVDT voltage then reaches a minimum as the rod reaches the bottom of the dashpot.

Subsequent variations in the trace are caused by the rod bouncing.

This procedure was repeated for each control rod.

The measured drop times for each control rod are recorded on Figure 2.2.

The

slowest, fastest,.and average drop times are summari=ed in a

Table 2.1.

Technical specification 3.1.3.4 specifies a maximum rod drop time from loss of stationary gripper coil voltage to dashpot entry of 2.2 seconds with the P.C S at hot, full flow conditions.

All test results met this limit.

J L

i h.

11

Table 2.1 NORTH ANNA UNIT 1 - CYCLE 4 BOL PHYSICS TEST HOT ROD' DROP TIME

SUMMARY

ROD DROP TIME TO DASHPOT ENTRY l

. SLOWEST ROD I

FASTEST ROD l

AVERAGE TIME l

l 1

l i

I I

l B-06, 1.82 sec.

l H-02, 1.55 sec.

I 1.67 sec.

I I

I ROD DROP-TIME TO BOTTOM OF DASHPOT l

SLOWEST ROD l

FASTEST ROD l

AVERAGE TIME I

l-1 I

I I

I l

B-06, 2.48 sec.

I H-02, 2.09 sec.

1 2.25 sec.

I l

l I

I I

I G

4 s

12

4 Figure 2.1 HORTH AHMA UNIT 1 - CYCLE 4 BOL PHYSICS TEST TYPICAL ROD DROP TRACE w

m I',.

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Figure 2.2 NORTH ANNA UNIT 1 - CYCLE 4 BOL PHYSICS TEST ROD DROP TIME - HOT FULL FLOW CONDITIONS a

P w

n L

x J

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14

Section 3 CONTROL ROD BANK WORTH MEASUREMENTS Control rod bank worth measurements were obtained for all control end shutdown banks using the rod suap technique.

The first step in the rod swap procedure was to dilute the most reactive control rod bank (hereafter referred to as the reference bank) into the core and measure

~

its reactivity worth using conventional test techniques.

The reactivity changes resulting from the reference bank movements were recorded continuously by the reactivity computer

and were used to determine the differential and integral worth of the reference bank (control Bank B).

At the completion of the reference bank reactivity worth measurement, the reactor coolant system temperature and boron concentration were stabili=ed such that the reactor was critical with

~

the reference bank near full insertion.

Initial statepoint data for the rod swap maneuver were obtained by moving the reference bank to its fully inserted position and recording the core reactivity and moderator tamperature.

At this

point, a

rod swap maneuver was performed by withdrawing the reference bank while one of the other control rod banks

( i.. e.,

a test bank) was inserted.

The core was kept nominally critical throughout this rod swap and the maneuver was continued until the test bank was fully inserted and the reference bank was at the position at

-which the core was just critical.

This measured critical position (MCp) of the reference bank with the test bank fully inserted is the major parameter of interest and was used to determine the integral reactivity worth of the test bank.

Statepoint data (core reactivity, moderator 15

temperature, and the differential worth of the reference bank) were rocorded with the reference bank at the MCp.

The rod swap meneuver was then performed in reverse order such that the reference bank once again ucs near full insertion and the test bank uns once again fully withdrawn from the core.

The rod suap process was then repeated for all of the other control rod banks (control and shutdoun).

The procedure given above uns modified during the measurement of the control bank D worth.

Although control bank B was predicted to have the largest worth of all the banks, the measured worth of control bank D exceeded the worth of control bank B.

The measured critical position for control bank D

was B

bank fully withdrawn and D bank partially inserted to 58 steps.

Therefore, the worth of the last 58 steps of D bank was measured using the boron dilution method.

The measured worth of control bank D is the sum of the worths determined by rod swap and the dilution of the last 58 steps.

A summary of the results for these tests is given in Table 3.1.

As shown by this table and the Startup physics Tests Results and Evaluation Sheets given in the Appendix, the individual measured bank worths for c11 of the control and shutdown banks were within the design tolerance (210%

for the reference bank and 15% for the test banks). The sum of the individual rod bank worths was measured to be within 6.6% of the dasign prediction.

This is well within the design tolerance of 10% for the sum of the individual control rod bank uorths.

The integral and differential reactivity worths of the reference benk (Control Bank B) are shown in Figures 3.1 and 3.2, respectively.

16

The design predictions and the measured data are plotted together in order to illustrate their agreement.

In summary, all measured rod worth vclues are satisfactory.

6 4

17

Table 3.1 NORTH ANNA UNIT 1 - CYCLE 4 BOL PHYSICS TEST CONTROL ROD BANK WORTH

SUMMARY

l l

MEASURED l

PREDICTED l

PERCENT DIFFERENCE l

l l

WORTH I

l l

BANK I

(PCM) l (PCM) l (M-P)/P X 100 l

l l

1 1

I I B-Reference Bank l

1188 l

1187 l

0.1%

l l D 1

1294 1

1181 1

9.6%

l l C l

843 1

764 l

10.3%

l l A l

562 1

524 1

7.3% (38 pcm)I I SB l

1023 l

965 l

6.0%

1 1 SA i

1094 l

1011 1

8.2%

l l Total Worth l

6004 1

5632 1

6.6%

i l

i I

I I

9 18

FIGURE 3.1 NORTH ANNA 1 CYCLE 4 BOL PHYSICS TEST BANK. 8 INTEGRAL ROD NORTH - HZP i

B BANK WITH ALL OTHER RODS OUT PREclCTED M MEASURED o

O IN

- - - _. j l

l 6

v 1

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0 40 80 120 160 200 2dB BANK POSITION (STEPS) 19

t-FIGURE 3.2 NORTH ANNA 1 - CYCLE 4 BOL PHYSICS TEST BRNK B DIFFERENTIAL ROD WORTH - HZP B BANK WITH RLL OTHER RODS OUT

-- PREDICTED M f1EASURED o

o.

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0 40 80 120 160 200 228 BANK POSITION (STEPS) 20

Soction 4 BORON ENDp0 INT AND WORTH MEASUREMENTS Baron Endpoint With the reactor critical at hot =ero power, reactor coolant system boron concentrations were measured at selected rod bank configurations 9

to enable a

direct comparison of measured boron endpoints with design predictions.

For each measurement, the RCS conditions were stabili=ed with the control banks at or very near a selected endpoint position. The critical boron concentration was then measured.

If necessary, an cdjustment to the measured critical boron concentration was.made to account for off-nominal core conditions, i.e.,

for rod position and moderator temperature.

The results of these measurements are given in Table 4.1.

As shoun in this table and in the Startup physics Test Results and Evaluation Sheets given in the

Appendix, all measured critical boron endpoint values were within their respective design tolerances.

All measured values met the accident analysis acceptance criterion.

In summary, all results are satisfactory.

Boron Worth Coefficient The measured boron endpoint values provide stable statepoint data from which the boron worth coefficient was determined.

A plot of the boron concentration as a

function of integrated reactivity can be constructed by relating each endpoint concentration to the integrated 21

rod uorth present in the core et the time of the endpoint measurement.

The value of the boron coefficient, over the range of boron endpoint concentrations, is obtained directly from this plot.

The boron worth plot is shown in Fig'tre 4.1.

As indicated in this figure and in the Appendix, the boron uorth coefficient of reactivity was measured to be -8,25 pcm/ ppm.

The measured boron worth coefficient is within 2.2%

of the predicted value of -8.07 pcm/ ppm and is well within the design tolerance of !10%.

The measurement result also met the accident analysis acceptance criterion.

In summary, this result is satisfactory.

I 1

1 1

l e

f 22

Table 4.1 NORTH ANNA UNIT 1 - CYCLE 4 BOL pi!YSICS TEST BOROM ENDPOINTS

SUMMARY

l l

Measured i

predicted l

Difference 1 l

Control Rod l

Endpoint l

M-p l

l Configuration 1

(ppm)

I (ppm)

I (ppm) l l

l l

1 I

I I

I

~

3 l

l ARO 1631 l

1628 1

l i B Bank In l

1488 l

1482 1

6 l

l l

l 1

I nThe predicted endpoint for the B Bank in configuration has been adjusted for the difference between the measured and predicted values of the endpoint taken at the ARO configuration as shown in the boron endpoint Startup physics Test Results and Evaluation Sheets in the Appendix.

I a

23 N

FIGURE 4.1 NORTH RNNA UNIT 1 - CYCLE 4 BOL PHYSICS TEST BORON WORTH COEFFICIENT

^

G ENDPolNT F1EA50REf1ENTS 1200 g \\ \\

- - -8.25 pcm/ ppa

\\

8 1000

\\

N s-800 N

y E

N s

\\ s 600

\\

N w

u N

C s

x

$ 400

\\

\\ \\

200

\\

\\'N

\\.N 0

1480 1500 1520 1540 1560 1580 1600 1620 1640 BORON CONCENTRATION IPPM)

d Saction 5 TEMPERATURE COEFFICIENT MEASUREMENT The isothermal temperature coefficient measurement was accomplished by controlling the RCS heat gains / losses with the steam dump valves to the condenser, establishing a constant and uniform heatup/cooldoun rate, and then monitoring the resulting reactivity changes on the reactivity computer.

The measurement uns. performed at a very lou power level in order to minimi=e the effects of non-uniform nuclear heating, thus, the moderator and fuel were'approximately at the same temperature (between 543-549

'F) during the measurement.

To eliminate the boron reactivity effect of outflow from 'the pressuri=er, the pressuri=er level was maintained constant or slightly increasing during the measurement.

Reactivity measurements were taken at the all-rods-cut configuration for both RCS heatup and cooldoun ramps during which the RCS temperature varied approximately 6*F.

Reactivity was determined

- using the reactivity computer and was plotted against the RCS temperature on an x-y recorder.

The temperature coefficient was then determined from the slope of the plotted lines. The x-y recorder plots of reactivity changes versus RCS temperature for the measurement is shown in Figure 5.1.

The predicted and measured isothermal temperature coefficient values are compared in Table 5.1.

As can be seen from this summary and from the Startup physics Test Results and Evaluation Sheets given in the

Appendix, the measured ARO isothermal temperature coefficient value was 25

within the design tolerance of 13 pcm/*r and met the accident analysis acceptance criterion. In summary, the measured result is satisfactory.

26

Table 5.1 MORTH ANNA UNIT 1 - CYCLE 4 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COEFFICIENT

SUMMARY

l l

1 l ISOTHERMAL TEMPERATURE COEFFICIENTI 1

l l

l (PCM/'F)~

l l

BANK lTEMPERATUREI BORON I

i IPOSITION l RANGE lCONCENTRATIONI l COOL l l

l DIFFER. l l

l

(*F) 1 (PPM) lHEATUPl DOWN LAVER.lPRED.l (M-P) l I

I I

I l

i I

I I

l l

ALL l-543.75 l

l l

RODS I

to l

1634 l -5.401'-4.431-4.921-3.301 -1.62 l

l OUT l

549.2 l

l l

l I

I I

I e

=

0 27-

Tigure 5.1 NORTH AHMA UNIT 1 CYCLE 4 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COEFFICIENT HZP, ARO H

l;p

~~

VERTICAL SCALE 10.0 pe=/ inch a,

t.

3;

,ji,

.d!i

,!j HORIZONTAL SCALE l' F/ inch

D.;;*!

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f-i!'

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TEMPERATURE (*F) 28

Section 6 POWER DISTRIBUTION MEASUREMENTS The core power d'istributions were measured using the incore movable detector flux mapping system.

This system consists of five fission detectors which traverse fuel assembly instrumentation thimbles in 50 core locations (see Figure 1.3).

For each traverse, the detector output is continuously monitored on a strip chart recorder.

The output is also scanned for 61 discrete axial points by the PRODAC P-250 process computer.

Full

core, three-dimensional power distributions are then determined by analy=ing this data using the Westinghouse computer

program, INCORE5 INCORE couples the measured flux map data with predetermined analytic power-to-flux ratios in order to determine the power distribution for the whole core.

A list of all the flux maps taken during the test program together with a

list of the measured values of the important power distribution parameters is given in Table 6.1.

The measured power distribution parameter values are compared uith their Technical Specifications limits in Tabl'e 6.2.'

Flux Map 1 was taken at =ero power.

This flux map serves as the base case design check.

Figure 6.1 shows the resulting radial power distribution associated with this flux map. Flux Maps 2 through 7 were taken over a

wide range of power levels and control rod configurations.

Flux maps 3 and 4 were quarter-core maps used only to provide incore/excore calibration data for the nuclear instrumentation system.

Flux maps 2,

5, 6,

and 7 were taken to check the at-power design predictions and to measure core power distributions at various

'l 29

" operating. conditions.

These maps also provide incore/excore calibration

~

data for the nuclear-instrumentation system.

The radial power distributions for maps 2, 5,

6, and 7 are given in Figures 6.2 through 6.5.

These-figures show that the measured relative assembly power values are generally within 6% of the predicted values.

In conclusion, all power distribution measurement results were considered to be acceptable with respect to the design tolerances, the accident analysis acceptance criteria, and the Technical Specification limits.

It is therefore anticipated that the core will continue to operate safely throughout cycle 4.

30

TABLE 6.1 HORTH At&4A UNIT 1 - CYCLE 4 BOL PHYSICS TESTS INCORE FLUX NAP

SUMMARY

l i

I i

i 1

1 2

1 3 1 1

1 1

1 I

i l

IBURHI l

l F-Q(T) HOT I F-DH(H) HOT l CORE F(Z) l l

5l l

l l

l UP l lBAta( l CHAl#4EL FACTOR I CHHL. FACTOR l

HAX l

41 QPTR I AXIALI NO.1 l

l HAP 1

lHAPI DATE INWD/IPWRI D l l

l lF(XYll i OFF l OF I I

I DESCRIPTION lHO.1 lHTU l(%)lSTEPSI l

lAXIALI i

i l

lAXIAll i NAX l 1

i SET lTHIH1 l

l l

l

'i 1

1 IASSYlPINIPOINTl F-Q(T)lASSYlPIHlf-DH(N)lPOINTl F(Z)l l NAX lLOCl (%) IBLESl l

l l_1 I

l_1 I

l_I 1

I l_1 1

1 I

I l_I I

I l

1 1

I i

1 1

1 i

i i

i I

i i

i l

i I

I l

lARO l 1111-19-821 01 01 228 1 J101 AQl 13 l 2.687 i K091 QAl 1.475 l 13 11.72211.596l1.0121 NEl 40.291 48 l l

1 1

I I

I i

1 1

1 1.

1 1

IPOWER DIST. VER.I 21 3-14-831 131 291 180 l B061 CEl 22 l 1.946 l J04l IJl 1.428 l 22 11.31011.66011.0061 SWI 4.401 48 l I

l i

I I

i l

1 I

I I

IPOWER DIST. VER.I 51 3-17-831 All 521 188 l K091 QAl 21 l 1.882 l J04l IJl 1.425 1 21 11.27711.51211.005l SWI 3.421 49 l 1

1 I

I I

l i

i i

I I

IPOWER DIST. VER.I 61 3-18-831 611 961 228 l B061 del 29 l 1.708 l K091 JII 1.388 l 29 11.170ll.51511.006l HEl 0.641 48 l 1

1 1

I I

I l

i I

I I

lHFP EQ. XEH0H l 71 3-24-831 30511001 221 l B06l del 29 l 1.765 l K091 JIl 1.393 l 29 11.17611.51311.0091 NEl -1.161 45 l NOTES: HOT SPOT LOCATIONS ARE SPECIFIED BY GIVING ASSEMBLY LOCATIONS (E.G. H-8 IS THE CENTER-OF-CORE ASSET 10LY).

l FOLLOWED BY THE PIN LOCATION (DEHOTED BY THE "Y" COORDINATE WITH THE SEVENTEEN ROWS OF FUEL RODS l

LETTERED A THROUGH R AllD THE "X" C00RDIllATE DESIGNATED IN A SINILAR NAl#lER).

IN THE "Z" DIRECTION THE CORE IS DIVIDED INTO 61 AXIAL POINTS STARTING FRON THE TOP OF THE CORE.

1.

NAPS 3 At3D 4 WERE QUARTER-CORE NAPS USED FOR CALIBRATION OF THE EXCORE DETECTORS.

2.

F-C'. T ) INCLUDES A TOTAL LUCERTAINTY OF 1.05 X 1.03.

3.

F-DH(H) INCLUDES A NEASUREMENT UNCERTAINTY OF 1.04.

4.

F(XY) IHCLUDES A TOTAL UNCERTAINTY OF 1.05 X 1.03.

5.

QPTR - QUADRANT POWER TILT RATIO.

l l

\\

Table 6.2 NORTH ANNA UNIT 1 - CYCLE 4 BOL PHYSICS TESTS COMPARISION OF MEASURED POWER DISTRIBUTION PARAMETERS WITH THEIR TECHNICAL SPECIFICATION LIMITS I

I I

l l

F-9(T) HOT I

F-DH(N) HOT l

F(XY) MAX 3 l

l l

CHANNEL FACTORT l

CHANNEL FACTOR 2 l

[

l MAPL I

l l

IMO.l MEASl LIMITlMARGINI MEASl LIMITIMARGINI MEASIAXIALI LIMITIMARGINI l

l l

l

(%) i i

I

(%>

l IPOINTI I

(%) l l

l__

l l

I I

i i

l I

i i

1 2 1 1.951 4.30 1 54.8 1 1.431 1.77 l 19.2 l 1.661 10 1 1.95 1 14.9 I i 5 l 1.881 4.12 1 54.4 l 1.431 1.69 1 15.4 1 1.511 13 l 1.80 1 16.1 I I 6 l 1.711 2.29 l 24.7 1 1.391 1.56 l 10.9 1 1.521 10 1 1.66 I 8.4 l l 7 l 1.771 2.18 l 18.8 l 1.391 1.55 l 10.3 1 1.511 10 1 1.65 1 8.5 l I

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1 1 The technical specification limit for the heat flux hot channel factor, F-2(T) is a function of core height. The value for F-9(T) listed above is the maximum of F-2(T) in the core. The technical specification limit listed above is evaluated at the plane of maximum F-2(T). The minimum margin values listed above are the minimum percent difference between the measured values of F-9(T) and the technical specifications limit for each map. All measured F-2(T) hot channel factors include 5% measurement uncertainty and 3% engineering uncertainty.

2 The measured values for the enthalpy rise hot channel factor, F-DH(N) includes 4% measurement uncertainty.

3 All measured FfXY) MAX values include 5% measurement uncertainty and 3% engineering uncertainty.

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. 0. 31. 0.79. 1. 0 7. 1.19. 1.2 9. 1.f 4 1.27. 1.17. 1.00. 0.00. 0.32.

4

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. 0.31. 0.64 1.06. 1.11. 1.22. 1.06. 1.20. 1.04 1.21. 1.12. 1.07. 0.09. 0.35.

5

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6

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1.0. 5.3.

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7 0.6. 1.1. 1.1. -0. 3. -1. 9. -1. 5.

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11 1.0.

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12 3.0.

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. 0.32. 0.90. 1.16. 1.20. 1.21. 1.22. 1.16. 0.06. 0.31.

13 2.4

2. 9.

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14 2.9

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Sfapcato 0.44. 0.72. 0.44 AVERAGE Olv!ATIQH 0.44. 0.77. 0.46.

.PC7 01FFEREPCt.

15

=1.775

7. 9. 6.2.

4.5.

a 2.0

SUMMARY

MAP H0t H1 5 DATE: 3/17/83 PCWER:

52%

CONTROL R00 POSITIONS:

F-Q(T) = 1.882 QPTRt D BANK AT 188 STEPS F-DHtH) a 1.425 HW 1.001 1 NE 1.004

-l..........

F(Z)

= 1.277 SW 1.005 l SE 0.990 F(XY) a 1.512 BURNUP a 41 MWD /MTU A.O s 3.42(%)

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s

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tt

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s oe* t e * -t** * -t.

.................................'s

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e*63

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t os

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e tS

e*es

t*ts

t*tt

t*te

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16*

- t

t*t *

- 6*

e*4

t * * * -e

...............................................'t sAreerac

e*64

e* 44

s'04

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e te

e*et

e**e *

*d31 eiddasama*

ts et ttt

* *

t 3s*

e t*3

............'s S045bY51 WVd H08 HT-t-1 aY138 t/29/91 dom 3Mt 100X 30H1M0l* 500 dosIIIOHS d-blA( n t*195 0d1H8 0 SY4M Y1 321 S13dE d-QHIN( m 1*t61 ieP 0*66$ l N3 I*006

..g...

d12(

a T*t19 stP I*004 l S3 0*662 A1X1(

a t*SII SENnd m 105 4se W 1R V*0 a

-t*2 )%(

CL

\\

l l

l Section 8 REFERENCES 1.

A.

p.

Main, T.

W.

Schleicher, " North Anna Unit 1,

Cycle 4,

Design Report," NFE Technical Report No. 231, Vepco, June, 1982.

2.

North Anna Unit 1 Technical Specifications, Sections 3.1.3.4, 3/4.2.

3.

T.

K.

Ross, W.

C.

Beck, " Control Rod Reactivity Worth Determination By The Rod Swap Technique," VEp-FRD-36A, December, 1980.

4.

" Technical Manual for Westinghouse Solid State Reactivity Computer,"

Westinghouse Electric Corporation.

^

5.

W.

Leggett and L.

Eisenhart, "The INCORE Code," WCAp-7149, December, 1967.

38

APPENDIX STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEETS 39

1-PT-91. 0 Page 1 of 35

^/

ATTACIC S T 6.9 10-29 *

. PCWI2 STAT CM UNIT 1 CYC'I 4 MCP.TM AMMA ST A ?.TU F FMYSIC3 TIST IIS U:.T S AMD IVA'U1!!CM SHIET

'll l

Tast

Description:

Reac :vity Computa: Checkout Rada:anca l

?:oc Mo /Section: 1 - ? T - 7 7 / A T T.-0 Saquance Step Mot 5 v

W.2 II 3ank Positions (Staps)

I ?.C S Tanpe=atu a ('T): 547 Test l

I ?cuar 2aval (% T.P.): C Conditions!

SDA: 223 S33: 223 CA: 223 I O tha: -( specif y ) :

(Design) l C3: 228 CC: 223 CD: 8 1 3alou Nuclea: Maating i

l =At the just c:it. positic 1

1 III I

3ank Positions (Staps)

I 2CS Tampa:atura (*T): 5 r5 5 Test 1

I ?cua: *avel ( *: T.P.): o Conditions!

SDA: 218 303: 228 CA: 228 1 0-ha: (Specidy):

(Aetual) l C3 228 CO8 228 038 206 I

b...l.., Mq l

a l

Oata/Ti=a !ast Pa:do::ad:

I l

I

// - / 9 - 82 0 624 l

l Measu:ad Parameta: I fc = Maas. Ranctivty using/ -conput Indar:ad Raaet from acet pa:i IV i

(:ase:4stion)

I /e 8

=

l l

1 A = -2 '7 3 17.6 32.o I

1 i:aasured value i

Be = -2 8.9

' B. 3 32 5-Tast i

I 3D = ~ _ 3,eg

_ g,7

. p,'$

Results i

1 1

Design value 1

l ( /t - /*, ) /AI x ~ 10 0:: 5 4.0%

1 (Actual canditions) I %D =

i I

1 Oasign value 1

' r, !

l t /c - A )

/

x 100% i

4. c::

1 (Design Conditions) I :D =

1 I

l Rada:anca l WCAP 79c5. ?.a v.

1, Table 3.s i

I I

I V

I TSA2/ Tech Spec

.I Mot Applicable Acceptancel l

C itaria l l

Rada:ance i Mot Applicabla 1

I i

l Casign Tolerance i: met X TIS MC 4

X TIS M O*

VI I Acceptanca C itaria is =a Co==ents l l'

l Alleuah's aang f

.7. 3 ** 3 2.0

~

c.

I b

b Completed 3y:

/M..

Ivaluatad 3y: R /[9M i

' Tas: ~ Ing:..a a:

/

Recommended do:

C. I A;;: eval 3y

?

Mr In;:.n a a :

5 A.1

1-PT-94.0 ATTACliMINI 6.9 Page 2 of 35 10-29-82 MOR~H ANNA P C'*Il S T A2 0N 'JN!!

C'?CLI

'4

..a.~.~..'

a'.'.'-

.'. l a'.'. '.' a' '. ~ '..'(

' h'.. '. '.

S~s.',2".'J'.

- - 'a'~.'.

~. ~. a~ ~. '~

..... a I

1 Tast Desc: p:Lon: C:1:ical 3eron Concent:stion - A2C Rade:enca l P:oc No /Saction: 1 - ? ! - :, A.'.' ':

Saquanca Stap No : [

w.3 I

3ank Positions (Staps)

,1 ACS Tamperatura ('T): 547 Tast-l 1 ? cue: Level (:( T.?.): 0 Conditionsi SDA: 223 323: 223 CA: 223

! Othe: (specify):

( 7,a sign ) l C3 223 CC: 203 C3 223 1 3alow Nuclaa: Heating i

i II:

I 3ank Positions (Staps)

! ?.CS Te=;a:atu:e ('T): 5431

ast I

I Power Level C :' T.P.): O Conditions!

S3A: 221 S:3: 21F a: 227 1 Otha: (Specify):

.(Actual) 1 C3: 111 00: 218 CO: 117 1 3 e f,w ft/g g fw //g4f,1 i

I Oa a/!ina Tas: Pa: o::a :

i 1

11 /19 / 7 7-112 9' l

1 I naas ?a:::ata: I IV l (Desc:iption) 1 (Cg )m: C:itical 3oron Cone - 120 I

I I

I M

l Measu:sd Valua I (CsI

/[*3I ff m m

Test l

l Results I

l

'De sign value i

lb 2 3 P P '"

~

I

(' Actual Cond) l C 5

l l

i Oasign Value 1

l (Design Cond) l C3

= 15*3 :

50 7;m i

I Rade:en=a i VI?-720-MTI-231. June. 1932 I

I I

V I TSAR /0ach Spec ! "C x C S 24,000 pcs 3

S Acceptancel I

C:staria I Rede:L. c e

! TSAA Section 15.2.4 I

1 l Das:.7n Tola:ance is =et X IIS MO I Accept:nca C:::a ::.a :.s ca X IIS MC I

7:

Com=ents,I C

~S'07 20'??" IC 7 *1i i00 Y

^ 178i 5

1 I cAc

.for 9,

,f. poly 3;3 5 = - 3. 7.5' pcm /

m f/

c-Completad 3y:

/

Ivaluatad 3y:

<2as: :=-. ue:

Racomntnied io:

A; proval 3y C-i MIO 5.*.$ '.~.a a :

'A. 2

1-PT-94.0 A TACHMENT 6.9 Pegs 3 of 35 2

10-29-82 XORTM AMMA PC'.;IR OTAT 0M UNIT 1 CY C 2.I 4 STARTUP PHYSICS TIST RISC:. S AND IVALUA!!CN SMII l

Test Oasc=1; tion Iso:ha==al Tamparatu:a Coaddiciant - A20 i

Kada:ance 1

?:oc Mo /Saction: 1 -? !-

' /1.' ?. :

Sequence Stap Mos y

'94A II l

3ank ?csitions (Staps) l ACS Tamperatu:a ('T): 347 Tast I

I Pcus: !.aval (% T.?.): O Conditionsi SDA: 228 333: 223 CA: 203 i Ctha:-(s;4cidy):

(Design) l C3 200 CC: 228 C3: 223 1 3alow Muclea: Maating i

i II l

3ank Pes:tions (Sta;s) l 2C3 !a=paratu:a (87): 546.3 Test I Pous: Laval (% T.?.):

o Condi-ionsi SDA: 228 533: 2.7. 8 CA: 21B l Otha: (Specidy):

(Actual) I C 3 : p.g g CC: 2,28 CD: 211 I 38102 M20 *E: E6'ti'7 I

~

l Ca a/Tiss Tast Pa:do::ad:

I 1

I l

//-/9-82

/327 l

l Maas Pa:n= eta: I y.r e IV I,

(Descriptien) l

("T 3 mo Iso Tamp Coadd - A20 A

1 I

I I

as' I

Measu:2d 7alus I (x[*1

- g g cM P

(C 3 = lf 34 p -

=

p 3

l Design value i

I

( Ac tual. Cont.s )

l (d?*)eaa = -3 '3c r3.o *// cs 1.'si s 1

I Oasien value I ( d :S e )g,

-- 3.33 : 3.0 yen /*T r

l (Design Cond) l (C 3=

1G23 ;pm)

I l

Rada:ance i VIP-T20-MTI-231. June. 1932 I

I i

l so Dor V

I TSAZ/ Tach S;ac 1 4f 5-2.11 pcm/'T 4

= -2.11 p:=/*T 7

Accep ancel I

C:ita:La l i

I Rada:ance 1

25 3.i.1.4 VI?-TED-MTI 231 1

l I

I Design Tole: nce is =st I ?IS MO V

l Acca; nnea Crata:i: is =at

)(_Y S NO Com=en s i

~

/

[b

/

Completad 3y:

A#

/

IV:lus:4d 37: PdY M

'3:a:: i..g

.de~= ~ ~

/

O 2aco: Sanded do:

a;;: eval 27 C-PTO Infinal:

A.3 e

bii im

-i i ii i ii-

1-PT-94.0 ATTAC10ENT 6.9 Page 4 of 35 10-29-82

. ( 0 3..,,.

A M.-( A 2 O.,g ? 3 S.a._aX UM. 1 C v. a.

s.......... - i.,..,-.

....,.,.. C 3 S,-

s.

.a

.auwa.ws 2

I Tast Descri? tion : M/3 Tlux Map - HI?, A10 lede:ence !

?:oc Mo / Section: 1-?T-21.1 Caquenca Sta? Xo: la I:

I 3ank Positions (Sta?s)

.I RCS Tam?eratu:e (87):733, 21 Test i

! Poue:

a tal ( **. T. P. 3 : ~ f.

Conditions!

00A: 223 SD3: 223 CA: 203

! Othe: '(s?acify)

("asign) 1 C3 2 223 CC 223 CD: 223 i Must have 1 33 thishlas l

1 1

3cnX ?ositions (Sta?s) i RCO Tas?arstu:a('T)? 547.2.

Test i

l Poue: Level (% T.P.):'f%

Conditions!

32A:228 533:226 CA: 110

! Cther (S?ecify):

.(.4::ual) i C3 :2?.8 CC 2228 CO:2. ?,8 V S en w 'jo n g g ;,4/cr i Data / Time Tast: f j / li/FP.

i I ?s:fo::ad:

i g

l i

l

.==. A.S.

3..?

6

= +.

.. e.t r.=

?..y. u. t

.e. t..s=-

.==.*.=3

,...

at S.

s e.

y w.a...

aw4..

.n a

4 a

../

I s.a a s S.

_.. m at. a_ _* i.. a'" V.

f) ' '.3 l

3.

S ?_

U. A *. l ? ? '.' *.?.

V.. C.

l O f* * * ?. S.

.*..P.*.*

.u

, a s._. <,. u. o ) I

.. 3

??.

! - u..s X

.? a. C.

l, u.

s.

.?,.,,,..

c..,.. 0

...s I

I (M-?)/?

T-dH(X) i T-2(!)

I 2?!2 I

l.

15.7 % rw Ga't.16 e -

l. N lb

1l*000 i $. 0 0 2.

sst.

I Measuzad 111uallgo,g f r Pg 0.61 Results i

4 1

Design Valua i m...,, g,, I

~

l -~

l ('asign Conds)I'u: f a r 71 *. 8 1,4,. n;y.,. !..! r'. :: s s.a i :::i:

5 1.C2 t p s..,,,.,.,, s -...

1 i

i iUCA?-7923 i

';C A?-7 9 3 5 i

?.ade:ance

?.2 7. I 1

MOMI i

MOM:

?.I 7. 1 i

1 i.

i.

1 I

l 7

i TSA?./ Tach S?aci MOMI I

MA i

MA I

MA Acceptancel l

I I

C:sta:ia i I

l 1

1 I

lade:ence McMI I

S 3.2.3 i TS 2.2.2 i :: 2.2.4 I

l I-i i

l l

I x

I Oasign Tolerance is set Y ?IS

'I C l Acceptance C:ita::.a is est X ?I:

'! O 7

I Co.mentr'l I

T s'

. /.

Cc= plated 2y:

Ivaluated 37:

McA_

"Tas: In?inai:

.'.s e c.?.m e n d e d do:

AP?: eval Oy C.

Mr:

-n?.n..:

n.4 m.

1-PT-94.0 ATTACEENT 6.9 Page 5 of 35 10-29-82

'HORTM'AMha PCtIII STATION "M:7 1 CTCLI a S.

,J ? ? H,.,,a,. b.

S.

.,,SU

.S aMD

.la.. U a,.

.,N S...n-..

i 1

Tas- :escription:Cn:1 2nnk 3 Me: h' Mans. 2 d Sung Red. S a n:-

?.ede:ence !

?:oc Mo /Section: 1 - ? '* - 7 1 ' A T T.

Sequence Sta? Mo:~~[

M.f II i

3ank Fcsiticas (Staps)

I ?.C S Ca=;e:stura (*T): 547 l ?oua: Laval (% T.?.): 0 Test I

Conditions!

SOA: 220. Sas: 223 CA: 223 i Cther-(specidy):

4 (Design) 1 C3_: Moving CC: 223 CD: 223 1 3elou Mucian: Heating 3

_I 1

3ank Positions (Staps) 1-2C5 Temperatu:2 ('T): 5 4F. 6

.I l ? owe: Laval (% T.P.): O Test Conditions!

S O A : 217 333: Z17 C A : 2.7.9 1 Other (Spacidy):

g

- ='eu Mu:;a:: H e at:.ng C3 :/ evig 00:221 00:Z22 tf (A :ual) I t,

1 1

Date/ Time 742 Pe:dorsed:

I lll19 l1'L IS'I &

I Kr#

I l

Measu:ed Ps:aseta: I I

'I^t*7 "1 I#C*th *5 Onti 3^^k 3'

3 l

(Descriptica) l All Othe: ?.ods Cut

_I IV I

I I

~

1 0

=

wr

//Fg gem

.. 'casu:ed Value 3

Tast 1;

)

I Results I

I

')asign value~

l

// T 7

Il9 fe" I (Actual conditions)-l s

I 1

I Dazagn value tar l ~ ( De sign ( :.nditions ) 1 I II37 III

?*

s i

I 1

Eada:ence

! VI?-TRD-MTI-231, "una, 1932 i

l i~;d esign Tolerance is a :<. c a e d e d. SMS l

1 sha'!.1~evalusta :. pact ed tas: :ssult.

I l

TSAR / Tach Spec 1 on sada:7 analysis. SMSOC ::y spacii V

I I that additional testing he ye:do==ad'

.I A C C s. ! ? *=n c e I I

C:iteria i i

22derance

! VI?-T13-3GA I

I K_ ?IS MO I Des:.;n 'cle: nee :.s =e:

X YIS NO V

1 Acceptanca C::.ta::.a is met Co=ments i 1

/

I

~

Aka sr/. lst

~zu a,a 1, :

C=.

e,a 2,:

..-..w Race =cendad do:

C App: val 3y NFC Ing :.n s a A.5

1-PT-94.0 s.

o

...9 Page 7 of 35 10-29-82

.e...,... S..,. - n.g,3 M -.,,..,,... g y C.,.

a.

M,..

w..

S. n.,.,.,,

...., 5 S

.S.

. S.J..

aM, -

Ja..-.y-...S:

I i

Tas-3ase:1ption: 0::: cal 3c:en Concent:stion - 3 3ank In Zada:anca i

?:oc Mo /5 action: 1 - ; T - E /.'..-~' 0 Secuanca.Ita; Moi 8 M. 3 I

3ank Fositions (Staps)

,1 2C5 Tampe:atu:a ('T): 347 Tasc l

l Foua: :avel (% T.?.): 0 Conditionsi SDA: 223 SD3: 223 CA: 223 i Other'.(specify)r (pasi.Jn) i C3:

o CC: 223 Cs: 223 1 3alou Nuclaa: saating I

l II:"

l 3ank Positions (Staps) 1 2CS !anperatura ('?): TY4.I Tast I

I Poua: "avel (% T.P.): C Conditions!

S O A : 217 003:217 C A : 22 7 i Ctha: (Specify);

.CActual) !

03: o CC U7

: 7.23 I gdm Mder 4de'n3 l

a:a/ isa as: 7e:do::ad:

i I

i ll /19 /g 2.

2. o 3,5-l l

I Maas pa:a=e:a: 1 M

IV

! (Description) l (Cg). : Critical 3cron Cen: - 3 3cnk In I

l I

I M

i Maasu:ad Valua I (C 3 3 3 U*

Tast I

l Results i

i 1

Oasi;n Valua i

I (Acuual Cond)

I C 3=

Mh t.Mrpm 5.

. -- ~ i v 1

I l

O a s :. ;n 1ua pegg l C asign

nd)

! C

=

'4 3

aC 3

3

C:2

0.7/ide3: );;=

I 2ada:anca i VI?-T23-NTI-23*, Juna..332 l

l I

I V.

I TSA2/ Tach Spac I "as xCS S 24.000 pen Acceptancel l

C*itaria-l Rada:anca l TSAA Saction 15.2.4 I

I I Design 7:ler:nce is me:

25 YIS NO I Acceptance Criteria is =st X ?IS NC I

y.

C.: =ents I CS

= -8.07 ;cm/;ps de: 3:alinin::7 analysis I

pg,y g 3,3

=,. -, y 6.* 3 w s,m -

dcg

/. 2S'[

[P fe bk Ah*If 5 8'S Complatad 3y:

/ _/

d Evaluated 37:

-,, a s znganse:

Zace==andad de:

C.

>g J

A;;:: val 37 MT0 E.7 n a:

. A. 6

-.,n.

~w4

-,-,e

1-PT-94.0

- .9 Fage 6 of 35 10-29-82 N O 1s.e g 4Nyg

. O.. ?..S.

S. 4 - a N eJ g(=.= =. I u=.p e., ?.

4 g

g ga w.

..a S. a. 3..,.,.a

.n.u. v. a C a<-

. e S.-

e

.e..r. a ].?.. a.i.sl3

e. < a *.:J a.. v M

.e.u. v e.-

i a

a s

I Tes: 0 ascription:

HI? So:ca 'Jo: h Coaddican: Maasuracan:

Rada:anca'I

?:oc l(o /Saction:

1-PT-

'.1.'?-.

Saquanca Stap 2(o s @

W.C II l

3ank Positions (Staps) l RCS Tamparatura ('T): 347 Tast I

i ?cuar *avel (% T.P.): 0 Conditionsi SOA: 223 SO3: 223 CA: 223 I Otha:.(spacidy):

~

(Design) l C3: Moving CC: 03 CO: 223 1 3alou Nuciaa: Haating I

l 3ank Fos:. ions (Staps) i RCS Tampe:atu:a (*T): 5'W. I, Test i

I Poua: Laval (% T.?.): O Co.d:.

ons!

S3A:225 S:3: 229 CA: 22 3

! Othe: (Specidy).

(Ac nal) !

03 :Afovius CC: 225 C J : 2 21' l

Below p'acleae Meas.

I f

i I. sta/ Tina Cas:'?a:de:nad:

i ll /19[71.

2 o'35-I Maasured Pa:nsata: I d

'IV l

(Cascription)

I es, Didda:ential 3c::= IJo th I

I I

I

-I. 2 I P C *** /ffm I

Measu:..d Valua CS

Test I

l I

assults.I i

~

l Design valta 1

1 (Actual Censitions) I

cs=-8.07 1 0.31 pcea / ppm -

1 1

I 3arign Vclua 1

e I (Design conditi:ns) !

43 = -3.07 :

0.3*

pe= / pyn l

I I

'=4$

anca l VIP -T RO -!(T I-2 31, Juna. 19C I

I l

e l

TSA2/ Tach 0;ac l

C xC3 1 24,000 pen g

V I

Acceptancal, l

C:ita:ia l Rada:ance l T3Al action 15.2.'4 I

l

+

1

! *:asign ' To la:anc e is st X TIS

!(0 V

1 Acceptanca C::.ta:ia is =at

>f T I3 fic Cc=ments !

1 I

I

-l '

/

- e

/

e Complated 3y:

N# [

d Ivaluated By:

!ast IF.g :.'ic o :

7.2ComOended 50:

j A??:3vC1 37*

S.~ 0 E..

inea:

. A.7

1-pT-94.0 Attachssnt 6.9

~

page 9 of 35 10-29-82 N C.,.. u..

aXX 7 0..r.3 a.. _ m. ( Ln.(_.

C,.,.. r

~

a. a 2.,J,

.o H v. S

.S

.cS.

R _r.e,J u-. a-a.s(0

.r /. J_ ~. C.r(

S.u..- r.

I 1

"ast Oasw:iption: Cn 1 3:nk 3 Mo:th "a su:a:ent-p.ed Sus?

Raderanca i

?:ce No.*Saction:

1-pT-7'c1'T.:

Saquanca Stap No.{O H."7 II i

3ank.7ositions (Staps) l 2CS !a=parctu:a

('T)-

347 T a s t' I

I pecar.Laval (%

.~.?.):

0 Conditionsi S3A: 223 SD3 200 Ca. 223 i C he:~(specidy):

(Dasign) i C3: Moving CC: 228 CO Moving,1 3elou Mucian: Hanting g

g g

3..

o s _4 _4.o.....

..e_.,s)

[

3.. -a

...e.....a

,, r,. : Syd.4

... r Test 1

I peca: *aval (% T.p.): O Conditionsi SDA: 2 2.2 503: 2.2.3 CA:

'2.'2. 7 i Otha: 'Spacidy)t

. gt % c n g - -. 2 2 g

..It\\a D an, *

~..'.-.'(..'.._-

. =.. -... '.,

, e e..u.._.._,

n.,.

_, s I

"I I

Data / Tina Test pa:do==ed:

I g

\\ \\ /'2A[82.

0312.

g g

i Maas Pa:c:ata: I IU ; Int Morth of Catl.22n% 0-Rod Scan l ( C a s c : i c. t i e n )

1 I

i v

i i

tad 5 naas. C:

. asi 3t=2 l19y gcq position = 4A sjaps)

Test i Mansusad Valua i I,

=

Rasults I

! Desi n Valus I

(Adj. Meas. C:it. Rai 3ank

!(Actual Cond) 1 I" = l \\ 8( t\\17 un position = N A saaps) f a

l I

I I

M

~

1 Dasign Value i I

=

1131- : 177 pc= (C:iticci Zed 3ank 3

IfDasign Cond)

I positica = 2i? staps)

I l

i 1

3.. a a. a....

i

- r. s _ r, ). _ v.e. r.

. -.44ie e[ r.

- r e..,_ J J A e

.e.r O _. A _,. 4 f

e s

s s

a i

I I

I Id Oasign Tola:caca is excaedad, SM CC 1

I shall avaluata i= pact oi :ast :asult on v

i TSA2/ Tach Spec ! sada:y cnclysis. SNSOC =cy specify tha:

Acceptancel l-additic..al tasting ha'pc:de==ad.

021: aria 1 1

I Refe:ence

! */I?-; A3 - 3 6 A I

I I Design !:larance is =at X IIS MO v!

.I Acceptanca C: ta:ia is cat X YIS NO Comments I l

I I

/'

/

~

V[

Complated 3y:,s I7aluated 3y:

.. Tas-In;1ana:

Eacomma.. dad i:

App::v:1 3 ;.

(I.

6 M.~ ^

E.'.7 1 n a s :

A.8

1-PT-94.0 Attachmsnt 6.9 Page 10 of 35 10-29-82

'NC R* 3 AMM A POWIZ STATION 'JN " 1 0*f0LI 4 S. A R.,J,

P.,, a-,. C S

.ea.

.J..a

,. X 3...l a...J a...

.(

S,. _.

g

.as..

.4.z.._4o.,..

.. u.

-.g

.3

..a.

2ada:ence !. Proc Mo /Section: 1 - P T ~ '- ' A T T. ~.i Gaquanca 5'ap Men ll c

94 7 II i

3ank Positions (Staps)

! RCS Tamparatura (87 ' 507

!ast i

I Foua: Laval (% T.?.3: O Conditionsi SOA: 220 SDS: 223 CA: 220 l C ha:'(specify):

(Design) l C3 Moving CC:Movin7CO: 203 1 3alou Muclear Me: tin 7 l

l II:

I 3ank Positions (Staps) l RCS !a=pe ::ura ('T): M/

Tast i

I ?cua: *atal (% T.?.): O Conditionsi S;A:

2."2. 8 Sp3: 22.8 OA:

~2.'2. F

! 0-ha:

Specidr):

(Actual)

C3 /Pfay;o 00 : /FWy : : 2.2.8 3a'.cu 5 cles: 'iactia; i

Data / Tim-Oast

.e:de:=ad I

' U f19 !82.

2.332.

l l Maas Pa cneta: I y

I (Dese:ip' ion)

! C

Int L'o: th od Cn:1 3:nk C-Fod Suay e

I 1

IV I

i (Adj. Maas. 0:it. 7.ad 3ank Test 1 Matsu:ad Valua i I' 8N PCM P o s i ti o n.= 1(a 3 :t.:a'p s ;

=

e Results i

i i Oasign */ clue I

(Adj. Meas. C : :. :. In f 3 a.k f(Actual Cond) i If = 7[s 4 f. IID ?:sitica = 1/oS s-ca p s ?

g g

I

s 755 E ! 13 pen (0:. i0:1 Iai Zin%

! Design Valua

=

l(3asign Cond) 1.

?:sition = '35 s aps!

I I

3.a _.= a _. a n c a i

.I

_ r..a.

v..e. _.,. a 1,. - s _ r.3... _.v. 5,

.t a

......a a

I I

I I Id Oscign Tolerance :. s ex:aaded. 03 SOC i

i shall avalusta :.ny c: ci ta:t :ssult en v

I TSAR / Tech Spec I snia:y analysis. SttS00 scy specify tha:

Acceptancal I additional ta::ing

'a'ps:fo==ad.

C:i ta r '. c I I

I Radaranca I */ ?-723-35A I

l Oasipn

la:nn:a is =a:

X ?IS M3 7-g accep..,

..a-_2 4.

.e.

_a Commants 1 1

l

/V/]

s/

Completed 37:

M#

Iveluated 3y:

e

-- w

!a s t-' In g : n,a a :

y Race:manded fo:

Ap :: :1 2y C~-

.:-" In;inta:

4 A.9

i l

l-PT-94.0 i

s

,.9 Page 11 of 33 10-29-82 1 C '.' " 'u ' 4

.M O T.."..H a'.'(."s a' a" '. n' ~. O N,,U '.( - ~.

~

. u "n ".'.

'^

,.., S S

3...,,. a-a.(3 e.l a...... 0 N -./. r -.

S., 3.. n. 3

.d.

a -

1 Tas-Dasc:iption: Cn:1 3ank A Wo:-h Measu: ament-Rod Susp Rade:anca l

?:oc No /Saction: 1 - ? T - 0 2 / A.'.', 3 Saquence Sta? No lL 94.7

.II I

3ank Positions (Steps)

,1

?.C C Ta=;a:::u=2 ('T): 547-Test I Foua: Laval (% T.?.): O Conditions!

S3A: 203 503: 223 C A :;o v i n g.l othas.(specidy):

(DesignJ l C3: Moving CC: 203 CO: 223 i 3alou Mucles: Heating i

I II l

3ank Positions (Stays) i ECS Tamperatu:a ('T): 5470 i

Test I Foue: Laval (% T.?.): 0 Conditions!

S3A: 22Y S D 3 : 11f C A : mcW^g ! Otha: C0pe:idy)*

. (Actual) l C3:mo'2g CC:'z17 CO

'2.~2.y I 3alou "uclat: Heating I

Cata/Ti=c Oast Pardo::ad:

i l

N zo/n_

00.2.+

l l Maas Pa:a:ete: I g5 1 (3 ascription) l I

Int Ho: th of Catl Sank A 4

I I

IV i

I (Adj. Maas. Crit. 2ed 3ank Test I Measu:sd value i I,As = J[/ 2

[(p1 Position = f 72. s ta p s )

p Results i

I

.I Design Va lue I

(Adj. Maas. C:it. Rad 3ank If a f,ZA/.f /80 /E#1 l(Actual Co-d) 1 1 J.t s ta p s )

Position

=

l l

1 I

1 3asign Vclua 1 0,Ss

=

327 100 pen (C:1tical 7.ad 3:nk l(Design Cend)

Position = 103 staps)

I 1

I I

I

,e2 e-n-ca 1 1r,-:,a,.u.-r

.,.,1, 1r.

r,D

.,oa, u.-

.s...

a s -

.s

.n I

I I Id Ca sign Tola:anca-1: exceedsd, GX Cc l shall avclusta i= pac cd test :esult on.

V l TSAR / Tach Spec l sadety analysis. SXSOC say specify that Acceptancel I additional testing ha.; ardor =ad.

Critaria l i

I 2edaranca i VI?-TAJ-3GA I

I I Oasign Tolerance is st x TI3 MO V:

I Acceptance C:ita: a is set X ?I3 Mc i

Cossents I i

l I

//

/

Compl. tad 3y:

/ ##

/C Ivaluated 3y.:

M.

!ast Int;nas: '

C

-1 2:co:: ended fo:

17?!0'.*01 37

(-

TO In7 naa

1

-A.10

1-PT-94.0

..9 1

Page 12 of 35 i

10-29-82 i

1

.4 0.R. 4 4'.N N '

..?..'.

~..' *. _ w.4 U.N _~ ~. 1 C Y "..*..~. 4 4

S~.A.*.~.U'

..u."..'._~~..~a

~.. ~.. ~. ~.

a"w~~..', a'.

' '/ 4'.' 's a' ~. _~ ~.'(

S.*. ~ ~_ ~.

w 1

1 I

l Tast ::a s e:17:io n : Shutdeun 3ank 3 Morth.'aac.

Rod Sua?

3 eda:anca I proc No /Section: 1 - ? ? - 0 1 / A.'.'. "

Sequence Stap Mot }3 94 7 1

3ank positions (Steps)

I RCS !asperatu:a ('?): 347

=. a s.

I 3 c..a _..a....'.

r. **..?.3 4...

a.

A Conditions!

.SCA: 208 SO3:MevingCA: 223 i Cther-(spacidy)-

(Design) 1 C3 Meving CC: 203 CD: 223 1 3alou Muclear Heating i

i l

3ank Posit. ns (Staps) 1 RCS Ta=peratt:a ( ' 7

54M 7 Tast l

I poua: Laval (:: 7.?.): O Conditions!

SOA: 2."2.t' SD3:c"'% CA: N I C ha: (Spacidy):

CAc ual) I C3: M Q CC: 7.?_t CO: ? 't r-

-1 3alou Nuclas: Maatin; D

I i

Ja:a/Ti=a !ast pa:Io::ad:

1 l

n/u/n..

0%

l l~Maas pa:c=sta: i y

I (3 ascription) l I IIUt 20 th'05 Uh"IdCME 33^k 3~300 32EF sa l-1 IV I

I (Ad). Meas. C:it. Iai 3ank Test i Maasu:ad Value ! If[ = \\O T3 fCM position = WD staps)

Results. I I

r

~

l Design Value

! - gg (Adf. Maas. Crit. Eai 3ank 1(Actual Cond) l I 3 % i M N position 33 MD sjap:)-

=

I I

" R4 1 Design'7alue i

=

933 :- 144 pcm (C:::i:al End 3ank g

i ICDasign cond) positica = 132 staps) 1 1

1 1

i Rafa:ence i VI?-p20-NTI-231, VIP-TID-351, NTC-?!-2.2a l

I I

I Id Decipn Tola:ance is ex:caded. SN::C C 1

I shall evalusta := pact of tas:

asult on V

l.TSAE/*ech Spec ! safety analysis. SMSCC say specify th t Acceptancel l additional tasting ha pa:d==ed.

C:itaria l I

Ref ers:.c a i VI?-720-3GA I

I Cas17n Ic12:.nce is me X IIS MO VI i Acceptanca C:ite:ia is st X ?IS NO Comments I 1

l I'

l d hobe.h Completad 3y:

4_

Ivalustad 3y:

a s t.== =.<aai 1-Eac*2:andad IO:

C5

. p p = o, - :.

m

T: In; na s:-

a' A.ll

o 1-PT-94.0

.".9 Page 13 of 35 10-29-82 uCp 2....

A.sI.i s.

J' p q * ?. =>.

e.

. _ = o.(

i.n. I _. m.

s

_.d..

.,.a.

wa

- e.r.. y w s a.

.T

.s S.=.=. 3.

.J.3

.3gyS Ca.

3.

c.,. S a ew y e., n...,., _ m.y S.,.

y m.

s

..s l

.a

.....:.........3...

s... a..

...a.-

e....,.

s ledarence !

P:oc Xc /Section:

1-?"

.'U '*.J.;

Sa uanca Step Mc: Q 94.7 i

3ank position: (Staps:

'l

?. 0 5 Tenparatu:a ('T): 34~

Test I

i r o ua r..,a v e s,.

....,...0 Conditions!

SDA:Movin-SD3: 200 CA* 203 i Othe:'C0pecidy!'

(Desi n) 1 C3: Moving CC: 223 CD: 223

! 3elow Nt:clas: Matting g

f

.. 3. a _. 2. a _.. _ __ 2_..-. M. /

I.,.

g-

3.., a,. 3os

_4.c

. r.e. _. a.,..,.

l 4

2415 I

! Poua: Laval CM T.?.)* O

$NW^gS33: 7.~7.T OA: 'L'I.Y I C;ha (Opecidy):

Conditions!

SOA:

.g.g

.~. ~,

.z.t t.

_a _,...s.__._4_.

,.. 1 _.,.

..=_z..,

... e s a. g a

i I

, a. a /. _s __._

.. _ _ - _,._ s_ :

.a-.

e

\\ \\ f*2. O h._

D%0 i Maas ?c:a=a:a: I g5 I (Dasc:iption)

I 2

Int ": th of Shutdown 3cn% A-?.od Suap' 34 I

I

.I l

[

s,.aj.

..a_..

c. :. a

.a s.

g Tast

! Matsu:ad *.*s'ua l Ch = \\ D % P C.M Fosition = 2.b l : t a t s lasu.:. :s i_

i l Design Valua

(

'Adj. Maas. C: :. Iad 3cnk 1D I\\ I 132- @"o sitic.

I(Actual ~Cend)

I :

=

oi:.:a;s)

=

1 l

1

. a. n. g - 1_1

[. g g 3

., y g.t....

g

_._2_4...*

.: s.a.

e.

g...

..$ p

..a l(Oasign C:nd)

Positi:n = 1 3 3 aps; I

I 1

g g a _.:. _.._.. _. a

[

.. -.s _ r 3., _ s. t - r.

. -.,.; r : _ r...,. _ s :,

e r. a. _.

.,..a.

.2

as ksnased from 2.14 to 2.2.o by Te ek.,1csg I

5gec:Cea+1m C ka y e A4. 4 *+, Ta wa y 1.1,19 y 3 l

r complated 37:

./h I

Ivaluated 37:

Test Enginas:

(

Rece== ended 50:

A p p r o *J a i 3 */

NIO EnginGA:

L 7

l A.14 wg--e T

y

-e-9 y

y--

->pt v

ymete e-ww--

e

--ese-e-

--w s----

- ~ ~ - -

e-

-N-----~-*-er-w

1-?T-94.0

..9 Page 17 of 35 10-29-82 M01TH AMMA POUI2 STA!!OM UNIT 1 CYCLI 4 s

S. a,.,.. eJ n

.s u.. v. e i e

.rS.

..a b,,. S A u.D.

/ r U a.. e n d. S s.t. r r.

.u w

s

..a I

I

!ast 0 ascription :M/D Flux Map-At ?cuar.NI Cal h ation Raderer.ce i

?:oc Mo / Section: 1-??-22.2 Saquenca Step Mo:

[

II i

3ank Positions (Staps) 1 RCS Ta=perature (

T) : T yss :1 1

Test i

I Foua: Laval (M T.?.):~50 Conditions!

SDA: MC SDS: 223

' ' ' - 223 1 Cther_(specify) x _

CDesign) 1 C3 : 223 CO : 223 CD:

I i

III I

3ank Positions ( S ta ps )

i ROS Tamparatura(*F): Tas:

Test i

I ?oua: Laval (% T.P.): 29.2 Conditions!

S3A:221 SD3:221 CA:227 i Other (Specify)r (Actual) 1 03 227 cc : z27 cs: s9 4 1

21 At bfes i

~~

Qu.Ao.<- c.v a.

u,c m g

,.m../

4

=

.,s..s.

s s.

i Ferdo::ed:

3h4/F3 19o9 i

l M.o C.

.n.==. l g *.*.*. r %{ *. u. p. u* l..A =e y

t. _?

. 1 g g s 3 3.,..(.

=t o

I7 i Maas Parameter! ASSY ~ ?'J2 i RISI HCT I TLUX HOT IFOUEZ !!LT I (0 ascription) 1 M DITT l CHAM TACT I C *i A X TACT l RA!!O I

I (M-?)/?

I T-dHCN) 1 T-2CT) 2??R l

i I

I I

I 151% for Pp.z:/181 2

2 I

2 Test i Measured 7 alua 447, f,/;.,,: an !

A I

NA l

NA 21sults l

l 1

I I

Oas:.gn Value-l :.:: car n a.5 i

! (Dasign Conds)I '13: f *' " * * ' l XA i

XA l

5

.02 in = aan. Pn)

I I

i 1

!NCAF-7905 I I

l"0A?-79C5 I

Zade:anca 1

2IV.1 1

NCXI I

NOMI I 2I7.1 I

I

.#.v.n=m w rs.!

., a l

I E "33 C*' 3*M)!r"uj,L ;,',',")$

e-V I FSAa/ Tach Spect MONI l

a MA Acceptancel I

I l

G P 2o.s I

crite:ia 1 i

i i

l i

A=3a-=---

l NCHI I TS 3.2.3 i T: 3.2.0 1 TS 3.2.4 I

I I

I

__l i

I I

I I Cesign To'.a :.nea is mat Y:S MO

! A::a;: anes c ita:.a is =et

/?S No VI I

Comments

(*

Mus hate at laast 38 thi=bles do: a dull-core flux =ap c:,

I at least 15 thimbles do: a qua:ta:-co:a flux =ap.

14 Above the inra: tion linits.

l 0

/7 /

/?

_i complated 3y:

M M/'

Ivalua:ad 3y a-.

- -. w. -

n y... - -

2aco==arded :::

171,is diUece ce n accep hble Ace A/r c.n=N App:e tal Oy C.

bs y tekena.t ss+ts %ehe;Iy

.ee a w ;)e ya,.3e og p a e, ja,, g,,

? 3 2.3. nae

c a.s 2 7kese paea e4ers ' arc. not vertfred us.ag o.

pa.rH f-core f/w, map o l3 tat,, e /

for N I cattlera+t e.

3 The hil powet" f*a lir :+ was i,,e<eas ef %s 2.I4 +o 2.20 I"y lecL=ical T ac;Cea+ims Cl a $ e No. 4 Y, Tawwary 27,1473.

r A.15

.n

~

1-PT-94.0 7.9 Page 18 of 35 10-29-82

/

NCRTH ANMA PCWI2 STATIOM UMIf 1 CYCLI 4 STA27U?

.HYSICS T550 IISULTS AND IVALUA!!CN SHIIT I

i Test 3escription M/3 Flux Map-A 70uar,MI CaLih:atic.

j Reference I

?:oc.Nc / Section:

1-?T-22.2 Sequence S ta p No:

II I

3 a n.'<

.' o s i t i c a s (Steps) i RCS Ta=;e:atu:e ( ' T ) : ~ 3 2.e 21 Test I ?cua: Lavel (% T.?.): -~2 Conditions!

SDA: 223 SO3: 223 CA: 223 I Otha: -( s pe cif y t *-

(Design) !

C3 : 228 CC 228 CD:

4.

l l

l III I

3ank Positicas (Staps) l RCS Ta=;e:aturaT)- ~3 rte r "est

'l

'l Foua: Laval (% T.P.): 2 4. 2.g Condit.v ons,1 SDA:222 SD3:22%

cA:22T i Other (Spacify):

(.'-tur1)

I C3 :221 CC :223 CD: I S'7 I

.g ; g,;wn) q A_ g i

r k2ata/~4-a

"=st:

I W "f

! Par:o: ec.:

'3/s4/33

/Sto l

i I

I

. r..

.s. - - l NUr... N. u.

. ;. a...

.u. - a.I yv a r a s.. s.

a

r. s Ty l

.as

.....u._._.]

aaal o. r u.

I 2._ S e.

.u. r.s. l

.e-.

.u. a..,- l.s < r.r _.e.

..-.e v.

l Caaa s

_,.4 p 4.o

) I a..-

I 2

.: C....t

.w l

3..

. O

,....,(

caw.

ao..

w n a.

l 1 (M-?)/P l

T-dHC5)

T-9(2)

I

???R I

f I

f i

.'V.7% See P.22 1.03!

p 1

1 1

'?s t

! Me as ura d 71Lue !g,y, g,,y a

p ;p i

A/A I

A/A l

Rasus:s i

I I

I Design valua i m...,,s s., !

I MA 1

5 1.02 i

i I ( O a s t;n Conds ) I m.n tar r: <.' i NA g

(?t - un. Ne> g y

l..

2

,90s-

,. -.a I

Rade:ance l'

EI7.1 i

N0nr i

MONI I ?.I 7. 1 1

I I

I i

l l

[

[344e=wcaM.-PSAsj?

V

'l TSA2/ Tach Spaei MCMI I zh33M :WM) 9:1 U..-..::' 3 x;

'" 3" 3 l'M5MM'D'T Accaptancei I

C:iteria l i

I i

i I

Reference I

XONI I TS 3.2.3 1 25 3.2.2 i TS 3. 2. *4 I

I I

l I

I I

i l

fIS MO l Oasi;n 00lerance is met I Accaptance C itaria is =at

/?IS

': 0 I

.u

'Co:: ants 12 Must nave it least 33 thisbles fo: a full-c::a flux : p.

Or I at lans: 15 thishlez do: a quarte:-co:e flux

=ap.

16 Above -ha insa::io-linits.

l 0

s/ f/

h-

' f /h/

Cu= plated 3y:

Ivalua:ad 37:

est In;taka:

. IkI5.d4ccexe h acceptakte si ce gr cal.*br +,w E8CO 28Cd85 53:

A 2?:ovai 2?.

C. A cam ba tper4e <A sa+tsc.et.rtly eve <.

wrge.

Gh.ge o f p o wa,- lev els.

MT3 I.;;.se:

These. havn msiers a* e. no+ ver.i!**c A ' vsin o. parHA-care 4'lu x map a b tainej 2

b e N r cal.*bes+ ion.

'3 o%crea te l 4'em-. 2.14 fu 2.2 o by Tect.mical SpeelCico+io s The ~ %Ilye sett fe II*w'+ w*s a

che ge No.48+, To.w a<y 2.7 i473.

j

l-PT-M.0.9

." age 19 of 35 10-29-82

(-

XCATH AMMA ?C"I2 STATTOM UMIT-1 CYC'I L:

.aYa Ca-a ? S =.=.ypcUL S A.gf 3 7.I A.,..?.

a.

.m.p.-.-.?..=

.?

S., y..J.y

.y.. c

.a A

.a--.

l Tast Desc ip'ction:

1-?!- M 2ih % % @y Saquenca Stap No:

tion : M/D Tlux Map - HT?, AIO, Iq. Xa Rade:ence I

?:oc Mo /

Sa a.t. I Il 1

3ank Positicas (Steps) l ACS Tamperatu:e (

T ) : T,,, : 1 Tast I

i ? c :. e : *avel (% T.P.):95:5 Conditions!

S3A: 223 SD3: 223 CA: 223 i O ther. ( s pa cii'/ 3 (Design) l C3 : 223 CC : 228 C3:

i Must have 2 23 thimbles III l

3ank Positions Test I

(Staps) i ACS Tampe r atu:e (

T ) : 1 g e t=

I ?cua: 'aval (% T.P.)

10o.0 Conditions!

SDA: LES SD3: 221i C A : 2.7 ?

t Other (Cpecify):

(Actual) l C3 321 C"

2.23 C3: ZZ1 I

ef.g.f-bimbles I

t.

I Cata/Ti=c Tast:

I I Fe:for=ed:

~$/24/33

12. 4 /

I I

i l

l M a, {. :....

l

.. J w,.

?..,(..I 4 _.., 1.,.,.

......I

....,3..s..

.os.

IV i Maas Paramete: 1 ASSY FUR l RISI HCT 1 T L 'J X HOT ! ?CUI A T!* !

l ( D e s c rip'tio n ) !

% DITT l CHAM TACT 1CHAN i CT I 2ATTO l

1 (M-?)/P l

T-d H C lf) l T-RCT)

I 2 ? !?.

I I

l l

l

)f..c% 6c Pg4 = o.T7]

I r

Test.

I Ma as u:ed v alu a !4.V.6 P,_,r =o.sd

1. 3 %

1 1.765" l

/.oo9 Results l

l I

Design valta i : _.., 31 s., I i

l ( asign conds ) I m: =r ri a.' i 1(A I

XA I

i 1.02 i

, (?1

Assy..hrr) l I

luCA?-7?05 I i

! **~ A? -7 ' 0 3 i

Ra#--ance

!- Irv.1 i

McMI I

NOMI I II7.1 I

I I

2

. = #4af t u.ssn o.:n-m i:v,,.fz-I I

I

'r

,..q 3;

a V

l TSA2/ Tach SpecI McMI l

su-unsm_g

-m Ac v.ptancel l

i l

i C:ita:ia i l

i I

I i

laie:ence Nox:

1 TS 3.2.3 1 75 3.2.2 1 TS 3.0.'4 i

I I

i e

I I

.i 1

! Oesign Tole:ance.is met YES

'C

! Acca;;anca Critarin i: =at

/?!~

\\;0

./ -

I Comments I

ASoJo tha insertion limits.

I

T3 e All p= a cr-Fe /.* ;+ was increased -t' rom 2.14 +o 2.2 o b y i

Tech @ l Tr e c.*ficWo.s Cb qc A/o. 44, Ta-,y 27, M13.

Completed 3y:

8/ #

Ivaluated 3y:

Tast In;:.nde:

Reccananded der

..;p:or:1 3y

[.

xt: I n z :.n s e :

A.17

._.

ML20073K138

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