ML20126K896
| ML20126K896 | |
| Person / Time | |
|---|---|
| Site: | North Anna  |
| Issue date: | 05/31/1981 |
| From: | Kapuschinsky D, Lozito E, Rotella T VIRGINIA POWER (VIRGINIA ELECTRIC & POWER CO.) |
| To: | |
| Shared Package | |
| ML20126K894 | List: |
| References | |
| VEP-FRD-43, NUDOCS 8105220382 | |
| Download: ML20126K896 (79) | |
Text
{{#Wiki_filter:_ _ _ - _ _ _ _ _ _ _ _ _ _ _ _ _ _ l l O ' - VEP-FRD-43 MORTH AHMA UNIT 1, CYCLE 3 STARTUP PHYSICS TEST REPORT BY I l T. S. Rotella D. M. Kapuschinsky Reviewed By: Approved By: b, - , Rf C. T. Snou, Nuclear Fuel Engineer E. J Lolito, irector Nuclear Fuel Operation Subsection NL ear Fuel - eration Subsection Nuclear Fuel Operation Subsection Fuel Resources Department Virginia Electric and Power Co. Richmond, Va. I May, 1981 l 8 /053637a.
i i { CLASSITICATION/ DISCLAIMER The- 'd a t a , techniques, information, and conclusions in this report have ! baan prepared solely for use by the Virginia Electric and power Company * (the. Company), and they may not be appropriate for use in situations other'than those for which they were specifically prepared. The Company, , therefore, makes no claim or uarranty whatsoever, express or implied,as
- to their. accuracy, usefulness, or applicability. In particular, THE L
COMP ANY; MAKES NO WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURp0SE, 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 doe's not authorire its use by others, and any' such use' is. expressly forbidden except with the prior written I approval of the company. Any such written 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 I 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 dcta, techniques, informa' tion, or. conclusions in it.
. _,_,,_...__,,._.,..,_-,.._._._.._.,__a.-_._,,__._.._._..__.-..-_ _ . . _ . . - . _
ii ACKNOWLEDGEMENTS The authors would like to acknowledge the cooperation of the North Anna power Station personnel in performing the tests documented in this report. Special thanks are due to Messrs. J. p. Smith, A. K. White, and G. L. Amodeo. The authors would like to express gratitude to Mr. C. T. Snow, and Dr. E. J. Lo ito for their aid and guidance in preparing this report. l l l l l t l l l l
" ~ -- w M w #*,4-,
iii TABLE OT. CONTENTS
-SECTION TITLE PAGE NO.
Classification / Disclaimer.................. -i Acknowledgements........................... ii List of Tables............................. iv List'of Figures............................ V Preface.................................... vi i 1 Introduction and Summary................... 1 1 2 Control Rod Drop Time Measurements......... 10 t.
'3 Reactor Coolant System Flow Measurement.... 15 r
4 Control Rod Bank Worth Measurements........ 17 l e 5 Boron Endpoint and Worth Measurements...... 22 6 Temperature Coefficient Measurements....... 26 l' 7 Power Distribution Measurements............ 31 l l 8 References................................. 46 APPENDIX Startup Physics. Test Results and
. Evaluation Sheets.......................... 47 O
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a iv J l LIST ~OF-TABLES l TABLE TITLE PAGE No. 1.1 Chronology of Tests................................ 4 i L2.1 Hot Rod Drop Time Summary.......................... 12 i 3.1-j Reactor Coolant Syst'em Flou Measurement Summary.... 16 4.1 Control Rod Bank Worth Summa'ry..................... 19 5.1 Boron Endpoints Summary............................ 24 i 6.1 Isothermal Temperature Coefficient Summary......... 28 1 1 [ . 7 .1 Incore Flux Map Summary............................ 33
.7.2 Comparison of Measured pouer Distribution param-leters With Their Technical Specifications Limits... 34 e
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k v i LIST OF FIGURES. FIGURE: TITLE PAGE NO 1,1 Core Loading Map......,................................... 5 l 1.2 Beginning of cycle Fuel Assembly Burnups.................. 6 ]
'1.3 Incore Instrumentation Locations.......................... 7 1.4 Burnable Poison and Source Assembly. Locations............. 8 Control Rod Locations..................................... 9 1.5 2.1 . Typical' Rod Drop Trace.................................... 13 2.2 Rod Drop Time - Hot Full Flow conditions.................. 14 4.1 Bank B Integral Rod Worth - HZP........................... 20 l, ,
4.2 ' Bank B Differential Rod Worth - HZP....................... 21 e
-5.1 Boron Worth coefficient................................... 25 6.1 ' Isothermal Temperature Coefficient - HZP, ARo............. 29 Isothermal Temperature Coefficient - HZP,'B-Bank In....... 30 6 '. 2 7.1 Assembly Power. Distribution - HZP, AR0.................... 35 7.2 Assembly Power Distribution - HZP, D/2, C/130 Steps....... 36 Assembly Power Distribution - Prelim. I/E Cal.- Flux Map.. 37 7.3 Assembly Power Distribution - Prelim. I/E Cal.- Flux Map., 38 7.4 Assembly Power Distribution - APDMS - Flux Map............ 39 7.5 Assembly Power Distribution - APDMS - Flux Map......... .. 40 7.6 Assembly ~ Power Distribution - AFDMS -
Flux Map............ 41 7.7 Assembly Power Distribution - APDMS, I/E Cal - Flux Map... 42 17.8 Assembly Power Distribution - APDMS, I/E Cal - Flux Map... 43 7.9 7.10 Assembly Power Distribution - APDMS, I/E Cal - Flux Map... 44 Assembly Power Distribution - HFP, Eq. Xenon - Flux Map... 45 7.11 . l 1 I
l vi l PREFACE The purpose of this roport is to present the analysis and of the physics tests which were performed to verify that the i evaluation North Anna 1, Cycle 3 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 there items is included in this report. The analyses presented include a brief sumdary of each test, a comparision of the test results with design predictions, and an evaluation of the results. The North Anna 1. Cycle 3 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) acceptance criteria, and 6) comments concerning the test. 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 Vepco's Muclear Fuel Engineering Group'. During the tests, the data sheets were used as guidelines both to verify that the proper test
vii conditions were met and to facilitate the preliminary comparison between and predicted test results, thus enabling a quick measured of possible problems occuring during the tests. The identification Appendix to this report contains the final completed and approved version of the Startup physics Tests Results and Evaluation Sheets. i 4 I
i 1 i j Section 1' l 1 INTRODUCTION AND
SUMMARY
l On December 28, 1980, Unit No. 1 of the North Anna power Station 'l uns shut downLfor its second refueling. During'this shutdown, 64 of the
-157 fuel assemblies in the core were replaced with fresh fuel
- assemblies. The cycle three core consists of four batches of fuel: two once burned batches (1A3 and 3A2), one twice burned batch (4), and one fresh batch (5). The core loading pattern and the design parameters l
for each batch are shoun in Figure 1.1. Fuel assembly burnups are given in Figure- 1.2. The incore instrumentation locations are identified in i Figure 1.3. -Figure 1.4 identifies the location and number of burnable poison rods and source assemblies for Cycle 3; and Figure 1.5 identifies the location and number of control rods in the Cycle 3 core. t on- April 6, 1981, at 0140, the third cycle core achieved initial \ criticality. Following criticality, startup physics tests were l performed as outlined in Table 1.1. A summary of the results of these tests follous
- 1. The drop time of each control and shutdown zod was confirmed to be within the 2.2 second limit of the North Anna Technical Specifications 2,
- 2. The reactor coolant system flou rate was confirmed to be greater than the minimum limit specified in the Technical Specifications:.
- 3. Individual reactivity worths for all control and shutdown rod banks were measured using the rod swap technique 3 and were ev.n=,-=- --,---.-,n--+wu +w--,,-- wr -, ,, r w n w. c i v - ,-e w e m e w .-- -,,- #, e ,,,,-e....s--c-rmm.-m---,---,---~..,-w.
l 2 found to be within 12.31% of the design predictions with the exception of Shutdown Bank A which showed a percent difference of 19.54% from design predictions. Except for Shutdown Bank A, these results are within the design tolerance of 115% for individual bank worths ( 10% for the rod swap reference bank. worth). This deviation is discussed further in section 4. The sum of the individual control and shutdown lod bank worths was measured to be within 4.78% of the design prediction which is within the design tolerance of 210%.
- 4. Critical boron concentrations for two control bank configurations were measured to be within 26 ppm of the design. predictions. These results were within the design tolerances and also mot the accident analysis acceptance criterion.
- 5. The boron worth coefficient was measured to be within 4.7%
of the design predication, which is within the design tolerance of 210% and meets the accident analysis criterion.
- 6. Isothermal temperature coefficients for two control bank configurations were measured to be within 0.74 pcm/'T of design predictions. Thes e results are within the design tolerance of 13 pcm/or and also met the accident analysis acceptance criterion.
- 7. Core power distributiens for various HZp and at power conditions indicated reasured assemblyuise power values to be somewhat larger than the established design tolerance.
i' l-3 These higher-than-expected power values were accompanied by a quadrant power tilt ratio (2pTR), which at hot-sero-Power,.was measured to be approximately 4%. The SpTR decreased to 1.3% at full power. These deviations of power
. distribution had no adverse consequences since, for all flux maps, the hot channel factors were measured to be within the limits of the Technical Specifications. All measurement parameters met their respective accident analysis acceptance criteria.
In summary, all startup physics test results were acceptable. results, together with 'apecific design tolerances and Detailed acceptance criteria for each measurement, are presented in the appropriate sections of this report. b
4 Table 1.1 NORTH ANNA 1 - BOL C CLE 3 PHYSICS TESTS CHRONOLOGY OF TESTS l l 1 1 I Referencel l Test i Date l Time ! Power ! Procedurel I I I I I l I I i l l I i Hot Rod Drop-Hot Full Flow 104/05/811 1205 l HSD 11-PT-17.2 l l Reactivity Computer Checkout 104/07/811 0518 I HZP 11-PT-94(B)I l Boron Endpoint-ARO 104/07/811 1040 i HZP 11-PT-94(C)] l Temperature Coefficient-ARO l04/07/811 1113 l HZP 11-PT-94(D)l i Bank B Worth 104/07/811 1224 i HZP 11-PT-94(E)l l Boron Endpoint-B In 104/07/811 1840 i HZP 11-PT-9u(C)1 1 Temperature Coefficient-B In 104/07/811 2300 l HZP ll-PT-94(D)I l Bank D Worth - Rod Swap 104/08/811 0026 l HZP 11-PT-94(G)l l Bank C Worth - Rod Suap 104/08/811 0138 l HZP 11-PT-94(G)! l Bank A Worth - Rod Swap 104/08/811 0244 i HZP ll-PT-94(G)l l Bank SB Worth - Rod Swap 104/08/811 0334 l HZP 11-PT-94(G){ l Bank SA Worth - Rod Swap 104/08/811 0421 i HZP ll-PT-94(G)l 1 Flux' Map-ARO l04/08/811 2141 1 HZP 11-PT-21.1 l 1 Flux Map-Insertion Limits 104/09/811 0455 l HZP 11-PT-21.1 l l Flux Map 104/11/811 0407 l 26.5 11-PT-21.1 I l Flux Map - APDMS 104/14/811 1623 1 49.7 11-PT-21.1 l l 1 Flux Map - APDMS 104/14/811 2258 l 49.2 11-PT-21.1 1 I Flux Map - APDMS 104/15/811 0445 l 60.6 11-PT-21.1 1 1 Flux Map - APDMS, I/E Calibration 104/15/811 1024 l 74.2 11-PT-21.1 l l Flux Map - APDMS, I/E Calibration 104/15/811 1410 1 79.4 11-PT-21.1 i l Flux Map - APDMS, I/E Calibration 104/16/811 0227 l 84.8 il-PT-21.1 1 1 RCS Flou Measurement 104/27/811 1018 1 99.9 11-PT-27 I l Flux Map - HZP, Eq. Xenon 104/27/811 1402 1 100.0 11-PT-21.1 I i l i ! I I
\ - - - _ _ _ _ - - . _ - _ _ . _ _ _ . . _ - - ~ . - - _ _ - _ - _ _ . _ _ - - . - _ _ _ - . _ . _ _ _ _ - _ _ _ 2_-.__ -
5 FIGURE 1.1 NDRTH ANNA UNIT 1 - CYCLE 3 CDRE LDADING MAP R P N N L K J H G F E D C B A I 3A2 15 1 3A2 l l C33 l E59 I C46 l 1 1 I I I I 3At i5 15 14 15 i5 1 3A2 l l C11 1 E53 1 E21 l D51 l E41 l E51 1 C29 l ' I I I I l- 1 -I l i 3A2 15 l5 l4 1 3A2 14 l5 l5 1 3A2 l I C17 I E64 1 EIS I D32 i C05 l D08 l E06 I E56 i C45 l 3 I I I I I I I I I I l 3A2 14 15 14 15 14 15 14 l5 14 1 3A2 l l C08 I D44 1 E04 1 006 I E29 I D18 I E61 l D30 l E14 1 D35 l C19 l 4 1 1 1 I I I I I I I I I l 3A2 15 15 14 15 1 3A2 14 1 3A2 I5 14 l5 l5 1 3A2 l l C24 1 E40 l E13 l DOS i E19 i C13 1 D34 i C48 I E50 1 047 l E02 l E60 l C37 1 5 I I I I I I I I l l l 1 I l 1 3A2 14 14 1 3A2 15 14 15 15 I5 I5 14 15 14 l l E08 l E24 1 017 l E30 l C32 i D45 1 D03 1 D14 i C28 l E47 l D02 1 E16 l E57 1 6 I I I I I I I I I I I I I i 1 3A2 15 14 15 1 3A2 14 14 15 14 14 1 3A2 15 l4 15 l 3A2 l i C50 l E01 1 D39 l E54 i C27 1 022 l 007 I E45 l D37 1 D20 l C51 1 E39 l D40 I E07 i C26 i1 7 I I I I I I I I 1____l 1 1 I I I l5 14 1 3A2 l4 14 14 15 l 1A3 l5 l4 14 14 1 3A2 14 15 l l E33 1 041 1 C43 1 023 l D09 l 031 1 EIS l All l E35 l D27 1 015 l D49 i IC49 1I 042 1l E20 l1 8 i ! l I I I i i i I i I i 3A2 15 14 15 1 3A2 l4 l4 15 14 14 1 3A2 15 14 l5 l 3A2 l 1 C06 i E44 1 050 l E17 l C42 i D10 1 D29 l E10 l D21 l D48 i C12 l E52 l 046 I E27 l C04 i g i I I I I I I I I i i i l I I I l5 15 l4 15 1 3A2 l4 14 14 1 3A2 15 14 15 15 l l E09 l E63 1 013 1 E46 l C14 1 026 1 004 l D25 i C25 l E22 1 019 Il E31 lI E38 II lo i I I I I i l i I I I i 342 15 15 14 i5 l 3A2 14 1 3A2 l5 l4 l5 15 1 3A2 l I C38 l E32 1 E23 l D11 1 E26 i C44 1 028 l C10 l E49 I D33 l E58 I E36 l C20 1I 11 I I I I I I I I I I I I 1 I 3A2 14 l5 14 l5 14 l5 l4 l5 14 1 3A2 I I C36 1 D16 l E55 l D12 l E42 l D38 l E25 1 043 I Ell l D52 l C07 l 12 I I I I I I I I I I I I l'3A2 15 l5 14 1 3A2 14 l5 l5 l 3A2 l l C03 i E12 1 E03 l D01 i CO2 1 024 l E37 i EOS l C21 1 13 l t I l l I I I I I l 3A2 15 l5 14 l5 l 5, l 3A2 l l C23 i E34 1 E62 i D36 i E28 l E48 i C30 l 14 I I I I I 1 1 I I 3A2 15 l 3A2 l l l--> BATCH I C39 I E43 i C40 l 15 l l--> ASSEMBLY I.D I l l l 1 l Fl'EL ASSEMBLY DESTC'i PARMTTERS Batch 1A3 3A2 4 5 Initial Enrichment (w/o U235) 2.11 3.10 3.21 3.40 Burnup At BOC-3 (P.!D/KrU) 14,054 23,273 9,941 0.0 Msc:nbly Type 17x17 17x17 17x17 17x17 Number of Assemblies 1 40 52 64 Fuel Rods per Assembly 264 264 264 264
i - I e
' FIGURE 1.2 ! HDRTH AM4A UNIT 1 - CYCLE 3.
_ BEG 1HNING DF CYCLE FUEL ASSEMBLY BURNUPS l t_ R P H H L K' J H G F E D C B A - J l C33 l-E59 i C46 l
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FIGURE 1.5
..dkti. AtttA UNIT 1 - CYCLE 3
'.0:tTROL ROD LOCATIOtlS R P tl N L K J H G F E D C B A 180 1
LOOP C l l l l LOOP B 1 OUTLET _ _l l l I ItiLET H-41 1 N l l*l l l SA I
!" lI SA Il*lI SP lV l H-43 3
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\ l I i SA I I I I SB 1 i SB l I SP l l SA 1 l l / 7 90hl
-1 i
ID I I I I I l-I1C I I I l I l I lC i I I l I i I ID 1 I I/ 1 - 270' 8 1 I I I l __ _ I I l ._ _ I I I I I I I I I I I SA I I SP l t Ud l l SB l l l l SA i l l 9 I I I I I I I I I I I I I I I I IA i 13 l l D l lC l lD l lB l lA l 10 I I I I I I I I I I I I I I I I I I SB I I I I SP l l SB I I SP l l 11 1 I I I I I I I I I I I I I I i: l lB 1 1 I Ie i IC I l 12 I i 1__ _ I I I I I I I i l I I Sp i i SA 1 l SA I i 1 1 13
- H-44 I I I I I I I I I I H-42 4
I l A l lD l l A l l 14 1 l l l l l l 1
/
LOOP A I l I l I I I l
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LOOP A 15 OUTLET ( 0 IHLET j ABSOPBER MATERIAL i AG-Itt-CD FUt4CTION ttUi1SER 0: CLUSTERS COttTROL BAttK D 3 CO!1 TROL bat!K C 8 COttTROL BAttK B 8 COttTROL BAttK A 8 CCitTROL CAttK SB 8 COltTROL BAttK SA 8 SP iSPARE ROD LOCATIOttSI 8 m
l l: 10 Section 2 CONTROL ROD DROP TIME MEASUREMENTS The drop- time of each control rod was measured at hot RCS conditions in order to confirm satisfactory operation and to verify that the rod drop times were less'than the maximum allowed by the Technical Specifications. The control rod drop time measurements were run with the RCS at hot, full flow conditions ( 547 *F, 2235 psig) and are
' described below.
The rod drop time measurements were performed by first withdrawing a rod bank to its fully withdrawn position, and then removing 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 gripper coil voltage, the LVDT (Linear Variable Differential Transformer) primary coil voltage and a 60H= timing trace which are recorded via a visicorder. The rod drop time to the dashpot entry and to the bottom of the dashpot are determined from this data. Figure 2.1 provides an example of the data that is recorded during a rod drop time measurement. As shown in Figure 2.1, the initiation of the rod drop is indicated by -the decay of the stationary gripper coil voltage when the stationary
. coil fuse is removed. A voltage is then induced in the LVDT primary coil as the rod drops. The magnitude of this voltage is a function of
-the- rod velocity. When the rod enters the dashpot section of its guide i
11 tube, the velocity slous, causing a 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 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 RCS at hot, full flow conditions. All test results met this limit. r - - - - ~
12 Table 2.1 NORTH ANNA UNIT 1 - CYCLE 3 BOL PHYSICS TEST HOT ROD DROP TIME
SUMMARY
ROD DROP TIME TO DASHPOT ENTRY l SLOWEST ROD l FASTEST ROD l AVERAGE TIME I l I 1 l I I I I I B-6, 1.77 sec. ! C-9, 1.45 sec. I 1.58 sec. I I I I I I I I I ROD DROP TIME TO BOTTOM OF DASHPOT l SLOWEST ROD l FASTEST ROD l AVERAGE TIME I I i I I i l i l l B-6, 2.47 sec. I C-9, 2.10 sec. I 2.25 sec. I I I I I I i I I
- t. .
Figure 2.1 5 MORTH ANNA UNIT 1 - CYCLE 3 BOL PHYSICS TEST TYPJCAL ROD DROP TRACE
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FIGURE 2.2 NORTH At2tA UNIT 1 - CYCLE 3 BOL FHYSICS TEST RO3 DROP TIME - HOT FULL FLO14 CONDITIONS R P H H L K J H G F E D C B A 1 1 I I i 1 1 I 1 1 I I I I i 1.57 l l 1.4a I i 1.ss i l i 1 2.18 I I 2.12 I I 2.22 I I 2 I I I I I I I I i l l l 1.57 I l 1.53 l l l l l 1 I I 2.23 I I 2.18 I I I I 3 I I i 1 1 I I I I I I i 1.60 I i 1.55 I I I i 1.60 l l 1.sa 1 I i i 2.28 1 1 2.22 I I I I 2.27 I I 2.25 I i 4 I I I I I I I i l i l I I I I i 1.63 1 I I I I i 1.55 I I I I i 1 1 I 2.33 I I I I i 1 2.22 I I I I 5 I I I i 1 I I I I I I I I I
! 1.52 I i 1.ss I i 1.57 I i 1.57 1 1 1.62 I i 1.62 I i 1.77 I I 2.15 I I 2.32 i i 2.27 1 1 2.25 I I 2.30 l I 2.30 l I 2.47 I 6 1 1 1 I I I I I I l l I I I i l l 1.58 I I I i 1.52 I i 1.57 I i i i 1.60 I I I I I I 2.25 I I I I 2.17 I I 2.22 I I I I 2.27 I I l- 7 I I I I I I I I I I I I I I I I I i 1.58 l l l 1 1.58 I I I i 1.60 t i i 1 1.68 I I I I 2.28 1 I I I 2.25 1 I I I 2.26 I I I I 2.42 I I a I I I I i I i i I I i I I i I i i l l 1.ss I i I i 1.52 I i 1.55 1 1 I i 1.45 I l l 1 1 I 2.23 I i I i 2.17 I I 2.22 I I I I 2.10 1 I I 9 I I I I I I I I I I I I I I I I i 1.ss i i 1.ss i i 1.55 I i 1.58 I l 1.63 I i 1.s7 l 1 1.58 1 1 2.22 1 1 2.25 I I 2.22 I I 2.25 I I 2.32 I I 2.22 I I 2.25 l 10 I I I I I I I I I I i 1 1 I I I I I 1.63 I I I I I i 1.55 I I i I i i i I 2.33 I I I I l l 2.20 l I I i 11 1 I I I I i i ! -I I I I I I I i 1.55 I i 1.63 I I I I 1.55 l l 1.sa ! l I I 2.23 I I 2.33 I I I I 2.20 l I 2.27 I i 12 I I I I I I I I I I I I i I I i 1.57 I i 1.53 l l l l 1 1 I I 2.23 i i 2.20 I i l l 13 I I I i l i I l l l l 1 1.72 I i 1.58 I I 1.62 I I I I 2.38 I I 2.27 I I 2.27 1 1 14 I l--> ROD DROP TIME I l l l l l l l l l TO D ASHPOT ENTRYt SEC. ) l l l l l l--> ROD OROP TIME l l 1 l 15 TO BOTTOM OF DASHPOT (SEC. ) l l l l
15 Section 3 REACTOR = COOLANT SYSTEM FLOW MEASUREMENT The . reactor coolant flow rate is measured in order to verify.that the minimum flow rate requirement is satisfied. The RCS flow rate is determined using the enlorimetric measurement technique. precision calorimetric- data (i.e.,- ~feeduater temperature,.feeduater flow, steam
=f l o w ,- and steam pressure) are obtained in order to accurately determine L
s . the - secondary-side . heat rate. The primary-side enthalpy rise is determinedLfrom the RCS pressure and the temperature increase associated with each RCS loop. The. flow for each RCS loop is determined by establishing a primary-side to secondary-side heat balance. Steam generator blowdown heat loss, system heat losses, and the power produced by the reactor coolant pumps are taken into account in the heat balance. A reactor coolant flow measurement was performed at 100% power. This . f data was analy=ed using the RXFLOW4 computer c o d e", and manually adjusted oto incorporate steam flow data. A summary of the results for this test is given in-Table 3.1. As shown by this table, the results demonstrated
- that the RCS flow limit was met.
5 5 O 1 ,,w.- ...,e- , ,c*w. .,e--w.,,,,-e-.,-,, -w w e , ,4%.n,-,-ev,,.-e~ ,--,,,,.--4,,-mr-,v-,,--..,-..,, c=. -,r,,,,,, m e,-.v ir e=r. .---r
16 Table 3.1 > HORTH ANNA 1 - CYCLE 3 BOL PHYSICS TEST REACTOR COOLANT SYSTEM FLOW MEASUREMENT
SUMMARY
I Percent I Loop A l Loop B i Loop C l Total Flow l Minimum Floul l Power IFlow (gpm)lFlow (gpm)l Flow (gpm)l (gpm) l Limit * (gpm)l l I l i l l I I I I l I I I 99,385 102,053 1 101,347 1 302,785 278,400 l l 99.9% i l 1 I I i i i i I t North Anna Unit 1 Technical Specification 3.2.5
1 17 Section 4 COHTROL ROD BANK WORTH MEASUREMENTS Control rod bank worth measurements were obtained for all control shutdown banks using the rod suap technique. The first step in the and zod 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 s 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 obtained by moving the reference bank to its fully inserted were position and recording the core reactivity and moderator temperature. At point, a rod swap maneuver was performed by withdrawing the this 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 uns 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 zeference 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 temperature,
18 and the differential worth of the reference bank) were recorded with the geference . bank at the MCp. The rod swap maneuver was then performed in l reverse order such that the- reference bank once again was near full insertion and the -test bank uns once again fully withdrawn from the coze. The rod swap process was then repeated for all of the other control and shutdown rod banks. A summary of the results for these tests is given in Table 4.1. As shown by this table and the Startup physics Tests Results and Evaluation Sheets given in the Appendix, the individual measured bank worths for all of the control and shutdown banks were within the design tolerance (210% for the reference bank and '15% 1 for the test banks), except for Bank A. This deviation uns reviewed uith respect to the Shutdown o licensing bases. As a result of this review it was concluded 6-7 that
-the deviation did not exceed the bounds of the licensing bases nor did it represent an unreviewed safety issue. The sum of the individual rod bank- uorths was measured to be within 4.78% of the design prediction.
This is well within the design tolerance of 110% for the sum of the individual control rod bank uorths. The integral and differential reactivity worths of the reference Bank B) are shown in Figures 4.1 and 4.2, respectively. bank (Control The design' predictions and the measured data are plotted together in ozder to illustrate their agreement. In summary, all measured rod worth values were acceptable. t
^ ~ _. . . .. .
'19
-Table 4.1 MORTH ANNA UNIT l'- CYCLE 3.BOL PHYSICS TEST CONTROL ROD BANK WORTH
SUMMARY
1 MEASURED l PREDICTED l PERCENT DIFFEREHCE l i WORTH I l l WORTH I I BANK l (PCM) l (PCM) l (M-P)/P X 100 I l 1 1 I I i I
'l I l. I i 1419 i 1311 I +8.26 1 1,
- l B-Re:Ee r ence . B ank I I
l' I I
+4.83 iD .I 1089 1 1038 1 1 1 I 1 I i 850 -8,59 I IC 1- 777 I l I I I
l- 1 722 643 1 +12.31 I IA I 1 I i I I l 919 1005 -8.54 I I SB 1. 1 l I I I I
.I 1238 1036 i +19.54 i I.SA i 1 l
i l I i 6164 l 5883 1 +4.78 I i Total Worth I I I I I I I I I I I
'l m___m.____.____--.__-m_-_________._m__ - _ . - . _ _ - _ _ _ _ _ _ _ _ . _ _ _ _ _ . _ _ _ _ . . _ ___m . _ _ _ _ _ _ _ _ . _ .__.-_-____._m._- .m__.__ _ . _ _ _ _ _ _ _ _ _ _
20 FJGURE 4.1 NORTH RNNA UNIT 1 - CYCLE 3 BOL PHYSICS TEST ROD SWAP REFERENCE BANK BANK B INTEGRAL ROD NORTH - HZP PREDJCTED R MEASURED o o y N I i
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3 I i i i N iiITmL 4 , i I i ! i i ! i i i , i i e i i i i + %_ ", i i I i 7 b 0 40 80 120 160 200 228 BANK POSITION (STEPS) a
# d. i.. - .h 4A.s. 44- Ain 2m-a d 3et-L- - > - 4 d +'a 44t.A - k .-
21 FIGURE 4.2 NORTH RNNR UNIT 1 - CYCLE 3 BOL PHYSICS TEST ROD SWAP REFERENCE BANK BANK B DJFFERENTIAL ROD WORTH - HZP
-- PREDJCTED M MERSURED-O O'
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i 22 Section'5-BOROH ENDp0 INT AND WORTH MEASUREMENTS
-Boron Endpoint .
With the reactor critical at hot =ero power, reactor coolant system-boron concentrations were measured at selected rod bank configurations l 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 , adjustment 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 5.1. As shown 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 t values met the accident analysis acceptance criterion. In summary, all results were satisfactory. Boron Worth coefficient The measured boron endpoint values provide stable statepoint data from ~ uhich the boron worth coefficient was determined. A plot of the concentration as a function of integrated reactivity can be boron constructed by relating each endpoint concentration to the integrated
.- ._.. _ ...-. . . . .._ ~ . . . - , . _ . _ . . . . _ . . . . . . - . . . . _ . _ _ _ _ _ _ _ _ , - . . . - . _ _ . . ~ _ _ , . _ , _ . - - _
23 sod- worth- present in the core at 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 Figure 5.1. As indicated in this figure- and in' the Appendix, the. boron. worth coefficient of reactivity was measured to be -8,54 pcm/ ppm. The measured boron worth coefficient is within 4.7% of the predicted value of -8.16 pcm/ ppm and is-well within the design' tolerance'of 110%. The measurement result also met the accident analysis' acceptance criterion. In summary, this result was satisfactory.
I 24 ) Table 5.1
'MORTH ANNA' UNIT 1 - CYCLE 3 BOL PHYSICS TEST BORON ENDPOINTS
SUMMARY
l l Measured I predicted l Difference l Control Rod 1 Endpoint l Endpoint ! M-p 1 l I configuration I (ppm) l (ppm) 1 (ppm) i l I l I l i i l l I l R RO - 1 1466.7 1 1492 l 25.3 1 I
- I l 1 I l B ~ Bank In i 1300.7 1 1304 1 -3.3 1 I I I I l
s The 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. ( , 1 I E e
-wnw- .e-e-www-aemi,.-en-, -eveu--..mwma- -, - _ , , _ _ , _ _ _ _
,l1 O
0 6 5 1 0 2 5 T 1 S E T m p p
/
S m c 0 C p 8 I 4 4 1 S 5 Y 8 i H \ P T
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=
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\ 4I 4
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26 Section 6 TEMPERATURE COETTICIENT MEASUREMENTS The isothermal temperature coefficient measurements were accomplished by controlling the RCS heat gains / losses with the steam the condenser and/or steam generator blowdoun, dump valves to establishing a constant and uniform heatup/cooldoun rate, and then monitoring the resulting reactivity changes on the reactivity computer. These measurements were performed at very low power levels in order to minimire the effects of non-uniform nuclear heating, thus, the moderator and fuel were approximately at the same temperature (between 543 - 549 'F) during these measurements. To eliminate the boron reactivity effect of outflow' from the pressuri=er,'the pressurirer level was maintained constant or slightly increasing during these measurements. Isothermal temperature coefficient measurements were performed at various control rod configurations. For each rod configuration, reactivity measurements were taken during both RCS heatup and cooldown ramps during which the RCS temperature varied approximately 6*T. Reactivity was determined using the reactivity computer and was plotted against the RCS temperature on an x-y recorder. The isothermal temperature coefficient was then determined from the slope of the plotted lines. The x-y recorder p. lots of reactivity changes versus RCS temperature for each measurement are shown in Figures 6.1 and 6.2. The predicted and measured isothermal temperature coefficient values are compared in Table 6.1. As can be seen from this summary and from the Startup physics Test Results and Evaluation Sheets given in the
27 Appendix, all measured isothermal temperature coefficient values were within the design tolerance of 3 pcm/'F and met the accident analysis acceptance criterion. In summary, all measured results were satisfactory. I 1 1
28 Table 6.1 NORTH ANNA UNIT '1 - CYCLE 3 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COEFFICIENT
SUMMARY
l
! BANK l I lISOTHERMAL TEMPERATURE COEFFICIENTl IPOSITION l l I (PCM/'F) I i (steps) ITEMPERATUREl BORON l l l l RANGE lCONCENTRATIONI l COOL l l IDIFFER. 1 I B l D l ('F) i (PPM) lHEATUPI DOWN LAVER.lPRED.I (M-P) l I I I I I I I I _I I I I 1 1 I I I I I I l I 2281 2281542.9-548.51 1487 l -4.521 -4.201-4.361-3.991 -0.37 I I I I I i l l I I I I 91 2281543.1-546.21 1311 1 -7.301 -7.501-7.401-6.661 -0.74 I I I I l l l I I l _. I
( l
29 Tigure 6.1 NORTH AHMA UNIT 1 - CYCLE 3 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COETTICIENT HZF, ARO l l 1 1 t ..iii! i, ,,,,,i.ii ,4 i i , 4 6 , ii,,i ,,,,,,,,,,,, , ,
,' . OD h ' ? ? . t i ,! I i ' t t ' t I i I , i ! ! r i ! , , , ,
, ,i;,;i;,
i,
,j i i;,,
, j , , ,' , j, , i
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i ,,, a .i i . , j i i i , i i , i,,6 , i , , ,, , ,,,,, , x N , . i i i I I I I '; i i , ,
, , ; ,, , j
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N I J i , j t e , i , , , j iiii,
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, j TEMPERATURE (*F)
30 1 Figure 6.2 NORTH ANNA UNIT 1 - CYCLE 3 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COEFFICIENT HZP, E-BANK IN L 4 ft._...
.t 3. ., . ,.p j p g, 7 . _
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I 31 l Section 7 POWER' DISTRIBUTION MEASUREMENTS The' core power distributions were measured using the incore movable detector iflux mapping system. This system consists of five fission detectors which l 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 1
scanned for- 61 discrete axial points by the PRODAC p-250 process computer. Full core, three-dimensional power distributions are then determined- by- analyzing this data using the Westinghouse computer .l i program, INCORE8 ,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. 1 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 7.1. The measured power distribution parameter values are compared with their Technical Specifications limits in Table 7.2. Flux Maps 2 and 3 were taken at zero power (Map 1 was aborted due to low incore detector signals). These flux maps serve as base ~ case design checks. Figures 7.1 and 7.2 show the resulting radial power -distributions. associated with these flux maps. These maps indicat'ed the presence. of a significant quadrant power tilt (-4%) and some- assemblywise relative power values in excess of the design tolerances, but all measured hot channel factor values were within the f Technical Specifications limits. L
?
32 Flux maps 4 through 14 were taken over a wide range of power levels configurations. These flux maps were taken to check 7 and control- rod the at-power design predictions and to measure core power distributions at various operating conditions. These maps also provide incore/excore ! calibration data for the nuclear instrumentation system as well as base power distribution curveillance. The radial power data for axial
' distributions for these maps are given in Figures 7.3 through 7.11.
These figures show that the measured relative assembly power values are 8% of the predicted values. Some relative assembly generally within l power values were in excess of design tolerances, but all measured hot } These figures also shou that the 1 channel factor values were acceptable. value of the quadrant power tilt ratio decreased significantly during e power ascension. In conclusion, all power distribution measurement results were to be acceptable with respect to the accident analysis considered criteria and the Technical specifications limits. It is acceptance anticipated that the core will continue to operate safely l therefore throughout cycle 3. i e
TABLE 7.1 HORTH AtatA Ut4IT 1 - CYCLE 3 BOL PHYSICS TESTS It1 CORE FLUX HAP SUtt1ARY I i i i i i i 1 1 2 l l t i l i I I I I BURHI l l F-QtT) HOT I F-OH(Hs HOT l CORE F(Z) l i 4 l 1 1 1 l l l UP 1 lBAttK l CHAtRIEL FACTOR l Chill.F ACTOR l MAX l 31 QPTR I AXIAll t:0.1 i MAP IMAPI DATE I MMD/IPWRl D I l l IF(XYll i OFF 1 OF l l DESCRIPTIOt4 l t40.1 l MTU l(%)lSTEPSl l lAXIALI l l l lAXIAll l MAX i i l SET ITHIMI I i l I l I lASSYlPIHlFOINTI F-Q(TilASSYlPIlllF-DH(H)l POINT! F(Z)1 1 MAX lLOCl (X) 10LESI l _,_ I I __ l l l I l___l l l I l__ t i I l __ I I I 1 I I I I I 1 5 I I I I I i l i I I I I I I I lARO l 21 4- 8-811 01 41 220 l J14l JLI 21 1 2.520 l J14l JL1 1.678 1 21 11.44911.796l1.044l Sul 16.961 46 I I I I I I I I I I I I i 1 1 I I I I I I I ID AT 2.C AT 1301 31 4- 9-811 01 41 2 i L131 OKl 38 1 3.114 l L131 OK! 1.843 l 38 11.61911.96011.0291 SEl-26.501 45 I I I I I I I I I I l t i I . I I i l 1 I I 1 l FLUX HAP l 41 4-10-811 01 271 58 l L131 OKl 47 1 2.824 i L13l OKl 1.673 1 48 11.68711.84611.0131 SEl-34.561 45 I I I I I I i 1 1 I I I I I I l i I I I I I IFLUX HAP l 51 4-11-811 101 271 138 l J14l JLI 37 1 2.444 l K14l NOl 1.570 1 37 11.483tl.73111.015l Sul-18.601 45 l 61 1 I I I I I I I I I I I I I I I I I I IAPDMS FLUX MAP l 81 4-14-811 531 Sol 200 l K141 MOl 36 1 2.116 i K141 MOl 1.544 1 37 11.30711.63111.0181 SMl -6.801 45 l 1 1 I I i 1 I I I I I I I I I I I I I I I l APDMS F LUX MAP l 91 4-15-811 631 491 206 i K14l MOl 36 l 2.064 i K14l NOl 1.545 1 30 11.27811.62911.015l Sul -1.811 46 l 1 I I I I I I I I I I I I I I I I I I I 1 IAPDMS FLUX MAP l 101 4-15-811 671 611 205 l K14l MOl 36 l 2.040 l K14l MOl 1.528 1 30 11.27611.60611.0141 Sul -2.841 46 l 1 1 I I I I I i 1 1 1 1 1 I I I I I I I I lAPDMS. I/E CAL.l 111 4-15-811 731 741 190 l K141 Mill 36 l 2.124 l K14l Mtil 1.509 1 38 11.34311.59111.016l SWl-12.151 46 I I I I I I I I I I I I I I I I I I I I I I lAPDMS. I/E CAL.I 121 4-15-811 781 791 180 l K14l Mtil 38 l 2.200 i K14l Mill 1.505 1 39 11.39711.62911.015l Sul-18.958 46 I I I I I I I l l I l I I I i 1 1 I I I I I lAPDMS. I/E CAL.1 131 4-16-811 881 851 210 i K14l Mtil 28 l 1.983 l K14l Mill 1.493 l 28 11.275l1.57411.0131 Sul 2.881 46 I I I I I I I I I I I I I I I I I I l l 1 I lHFP., EQ.XEt!OH l 141 4-27-811 48711001 224 l K141 MHl 37 1 1.953 l K141 Mtti 1.474 1 38 11.264l1.55311.0131 Sul -7.881 42 l IOTES: HOT SPOT LOCATIONS ARE SPECIFIED BY GIVING ASSEMBLY LOCATIOtis (E.G. H-8 IS THE CEllTER-OF-CORE ASSEMBLY LOCATIO!4) FOLLOMED BY THE "Y" COORDIt! ATE WITH THE SEVENTEEH ROWS OF FUEL RODS LETTEPED A THROUGH Q At0 THE "X" COORDINATE DESIGilATED Ill A SIttILAR MAtalER ). - IN THE "Z" DIRECTIOta THE CORE IS DIVIDED ItiTO 61 AXIAL POIt4TS STARTIttG FROM THE TOP OF THE CORE.
- 1. F-Q(Tl It4CLUDES A TOTAL UNCERTAlHTY OF 1.05 X 1.03
- 2. F-DHtH) IllCLUDES A MEASUREMEllT UtlCERTAINTY OF 1.04
- 3. F(XY) MAX. IttCLUDES A TOTAL UttCERTAINTY OF 1.05 X 1.03.
- 4. OPTR - QUADRAtlT POWER TILT RATIO.
**P 1 WAS ADORTED CUE TO LOW DETECTOR SIGt1AL. b$
- 6. MAPS 6 ANS 7 MERE QUARTER CORE M/D FLUX MAPS.
. . - - - - - _ - - . - - - = . . . - - - - .
.. - ~ , _. . . - . . - - . . . - - . . . . - - . - . . -
34 Table 7.2 f NORTH ANNA UNIT 1 - CYCLE 3 BOL PHYSICS TESTS 1 l COMPARISION OF MEASURED POWER DISTRIBUTION PARAMETERS \ WITH THEIR TECHNICAL SPECIFICATIONS LIMITS l I i I i i i F-9(T) HOT I F-DH(N) HOT l F(XY) MAX 3 l 1 CHANNEL FACTOR 2 l 1 l CHAHHEL TACTOR 1 l l l l lMAPI l lHO.I MEASl LIMITlMARGINI MEASI LIMITIMARGIN! MEASlAXIALI LIMITIMARGINI l 1 l l (%) i i I (%) l lPOINTl I (%) I l l l l l l l l l 1 l l l 4 l 2.821 4.20 1+32.8 1 1.671 1.78 i +6.2 l 1.851 10 l 1.96 1 +5.8 1 1 5 1 2.44l 4.20 i+41.8 l 1.571 1.78 l+11.8 l 1.731 22 1 1.96 l+11.7 l 1 8 1 2.121 4.20 l+49.6 1 1.541 1.71 i +9.9 l 1.631 44 l 1.73 1 +5.6 I l 9 1 2.061 4.20 l+50.9 l 1.551 1.71 l +9.4 1 1.631 44 1 1.73 1 +5.8 l 110 1 2.041 3.47 1+41.2 1 1.531 1.67 l +8.4 1 1.611 44 1 1.69 l +5.2 l 111 1 2.121 2.83 (+25.0 l 1.511 1.63 1 +7.4 l 1.591 36 l 1.65 l +3.6 l l 112 1 2.201 2.65 l+16.8 1 1.511 1.61 l +6.2 1 1.631 10 1 1.78 1 +8.4 1 113 1 1.981 2.46 l+19.3 1 1.501 1.60 1 +6.3 l 1.571 44 1 1.62 l +3.1 1
+6.8 l 1.471 1.55 i +5.2 1 1.551 35 l 1,57 l +1.3 I 114 1 1.951 2.10 l I I I I I I I I I I I I I
l 1 The Technical Specifications limit for the heat flux hot channel factor, F-9(T) is a function of core height. The value for F-9(T) listed above is the maximum of F-9(T) in the core. The Technical Specifications limit listed above is evaluated at the plane of maximum F-9(T). The minimum margin values listed above are the minimum percent differences betueen the measured values of F-9(T) and the Technical Specifications limit for each map. All measured F-9(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 F(XY) MAX values include 5% measurement uncertainty and 3% engineering uncertainty.
35 Figure 7.1 NORTH ANNA UNIT 1 - CYCLE 3 BOL PHYSICS TEST ASSEMBLYWISE POWER DISTRIBUTION i HZP, ARO a P N ft L K J H G F 'k D C 6 A 1 PREDICTED . 0.36 . 0.71 . 0.36 . . PRt0!C750 .
. MEASURED . . 0.36 . 0.70 . 3.36 . . MEASURED . 1
. PCT DIFFERENCE. . -1.4 . -1.4 . -1.7 . .PC7 O!PFERENCE.
. 0.39 . 0.98 . 1.18 . 1.16 . 1.18 . 0.98 . 0.39 . 2
. 0.39 . 0.93 . 1.13 . 1.11 . 1.14 . 0.96 . 0.39 .
. 0.1 . -5. 3 . -4.1 . -4.1 . - 2. 9 . -2. 0 . -0. 3 .
. 0.38 . 1.11 . 1.23 . 1.23 . 1.03 . 1.13 . 1.23 . 1.11 . 0.3S . 3
. 0.37 . 1.08 . 1.17 . 1.15 . 0.97 . 1.16 . 1.1S . 1.06 . 0.39
. -1. 9 . -2.1 . -4. 9 . -6. 2 . -6. 3 . -5. 4 . -3. 9 . -1. 0 . 1.6
. 0.38 . 0.94 . 1.21 . 1.25 . 1.21 . 1.13 . 1.21 . 1.25 . 1.21 . 0.94 0.38 . 4
. 0.38 . 0.92 . 1.17 . 1.16 . 1.13 . 1.05 . 1.14 . 1.19 . 1.18 . 0.92 . 0.36 .
. 0.5 . -2.3 . -3.4 . -5. 7 . -6.6 . -6. 7 . -6.5 . -5. 0 . - 3.1 . -2.1 0.5 .
0.39 . 1.11 . 1.21 . 1.28 . 1.21 . 0.94 1.02 . 0.94 . 1.21 . 1.19 . 1.21 . 1.11 . 0.39 . 5
. 0.40 . 1.12 . 1.17 . 1.22 . 1.14 . 0.86 . 0.93 . 0.87 . 3.14 . 1.22 . 1.16 . 1.10 . 0.41 .
-5. 2 . -4. s . -4. 0 . 0.1 . 3.8 .
0.8 . 0. 6 . -3.3 . -4.7 . -5.4 . -6.5 . -8.6 . -7.4 .
.............................................e..............................................
. 0.98 . 1.23 . 1.25 . 1.21 . 0.94 . 1.02 . 1.15 . 1.02 . 0.94 . 1.21 . 1.25 . 1.23 . 0.98 . 6
. 1.01 . 1.26 . 1.24 . 1.15 . 0.68 . 0.94 . 1.06 . 0.94 . 0.88 . 1.15 . 1.20 . 1.21 . 1.00 .
. 2. 7 . 2.7 . -1.1 . -4. 7 . -5. 7 . -7. 6 . =7. 9 . -7. 8 . -5.6 . -4. 5 . -4.1 . -1.3 . 1.5 .
0.36 . 1.18 . 1.23 . 1.11 . 0.94 1.02 . 1.13 . 1.14 . 3.13 . *.02 . 0.94 . 1.21 . 1.23 . 1.16 . 0.36 .
. 8.38 . 1.23 . 1.29 . 1.20 . 0.90 . 0.97 . 1.04 . 1.05 . 1.05 . 0.96 . 0.89 . 1.19 . 1.21 . 1.17 , 0.36 . 7 4.6 . 4.6 . 4.6 . *1. 3 . -4. 4 . -4. 9 . 7. 6 . -7. 9 . 7.4 . -6. 5 . -5. 2 -2. 4 . -1.7 . -0.6 . -0.8 .
. 0.71 . 1.16 . 1.03 .'1.13 . 1.02 . 1.15 . 1.14 . 0,84 . 1.14 . 1.15 . 1.02 . 1.13 . 1.03 1.16 . 0.71 .
. 0.74 . 1.21 . 1.08 . 1.13 . 0.99 . 1.11 . 1.07 . 0.80 . 1.06 1.09 . 0.97 . 1.10 . 1.01 1.19 . 0.75 .
3.2 8 4.6 . 4.6 . 4.6 . -0.4 . -2. 9 . - 3. 6 . -5. 9 . -5.1 . -5.1 . -5.1 . -b . 0 . t . 2 .
-1. 6 , 5.3 .
. 0.36 . 1.18 . 1.23 . 1.21 . 0.94 1.02 . 1.13 . 1.14 . 1.13 . 1.02 . 0.94 - 1.21 . 1.23 . 1.16 . 4.36 . 9
, 0.37 . 1.20 . 1.25 . 1.20 . 0.92 . 1.00 . 1.12 . 1.13 . 1.08 . 0.98 . 0.90 . 1.21 . 1.24 . 1.23 . 0.39 1.6 . 1.8 . 1. 8 . -1. 2 -2. 5 . - 2. 0 . -0. 7 . -1. 3 . -4.1 . -4. 3 . -4. 0 . 0. 6 . 0.8 . 5.0 7.8 ,
. 0.96 . 1.23 . 1.25 . 1.21 . 0.94 . 1.02 . 1.15 . 1.02 . 0.94 . 1.21 . 1.23 . 1.23 . 0.98 1.05 .. 10 i . 1.00 . 1.25 . 1.25 . 1.20 . 0.93 . 1.03 . 1.15 . 1.02 . 0.93 . 1.20 . 1.24 . 1.25 7. 0 .
1.8 1.8 0.4 . -0.4 . -0.5 . 0.2 . -0. 3 . -0. 8 . -1.1 . -0. 9 . -0.4 1.4 . l f .
........................................................................................... I
. 0.39 . 1.11 . 1.21 . 1.28 . 1.21 . 0.94 . 1.01 . 0.94 . 1.21 . 1.28 . 1.21 1.23 .. 1.11 1.14 .. 0.41 0.39 .. 11
. 0.41 . 1.15 . 1.24 . 1.28 . 1.23 . 0.97 . 1.05 . 0.96 . 1.22 . 1.28 0.5 . 1.6 . t.9 . 4. 7 .
. 3.9 3.9 . 2.5 . -0.3 . 2.0 2.6 . 2.5 1.7 , 1.2
. 0.36 . 0. 94 . 1.21 . 1.25 . 1.21 . 1.13 . 1.21 . 1.25 . 1.21 . 0.94 0.38 . 12
. 0.40 . 0.97 . 1.21 . 1.29 . 1.30 . 1.21 . 1.29 . 1.29 . 1.26 . 0.97 . 0.40 .
. 6.0 . 3. 0 . -0. 3 . 3.5 . 7.1 . 7.1 . 6.1 . 3.6 , 3.5 . 3.1 . 5.7 .
. 0.38 . 1.11 . 1.23 . 1.23 . 1.03 . 1.23 . 1.23 . 1.11 . 0.38 . 13 0.42 . 1.27 . 1.36 . 1.35 . 1.14 . 1.36 . 1.35 . 1.29 . 0.40 .
. 10.3 . 14.6 . 10.9 9.9 . 10.7 . 11.0 . 10.0 8.3 . 5.7 .
. 0.39 . 0.98 . 1.18 . 1.16 , 1.16 . 0.96 . 0.39 .
. 4.45 1.15 . 1.36 . 1.32 . 1.31 . 1.08 . 0.43 . 14
. 14.7 . 16.7 . 15.8 . 14.3 . 11.1 . 10.2 . 6. 3 ,
. STANDARD . 0.36 . 0.71 . 0.36 . AVERAGE ,
OtVIATICH . 0.41. Q.82 . 0.41 . .PC7 DIFFERENCE. 15
. 18.8 . 15.5 . 12.1 . s 4.5
. 83.i11 MAP NO2 N1 2 DATE: 4/ 8/81 POWER 4%
CONTROL ROD POSITIONSt F.Q( T ) = 2.520 QPTRt D BANK AT 220 STEPS F-OH(N) s 1.678 N'.4 0.%7 l NE 0.960
......... 1..........
F(Z) s 1.449 D 1.Clu l SE 1.029 F(XY) s 1.796 i i BURNUP =. O MWD /MTU A.0 2 16.96(%)
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37 4 i Figure 7.3 NORTH ANNA UNIT 1 - CYCLE 3 BOL PHYSICS TEST I 1 I ASSEMBLWISE POWER DISTRIBUTION PRELIM I/E CAL FLUX MAP l 1 J M S F t p C 6 A W P N n L A
................ PptDIC7t0 .
PptDIC7tD . , 0.31 . 0.55 . 0.31 . . HEA3URED 1 MEASURED .
. 0.33 , 0.57 . 0.33 . . .
5.1 , 4.6 . 5.5 . . .PC7 01FFERENCE.
.PC7 01FFtWINCE. .
. 0.43 . 0.97 . 1.03 . 0.78 . 1.03 . 0.97 . 0.43 . t
. 0.45 . 0.99 1.06 . 0.79 . 1.07 . 1.03 . 0.46 .
. 5.1 . 1.4 , 2.3 . 1.4 . 3.9 . 5.7 . 6.6 . *
. 0.43 . 1.17 . 1.25 . 1.20 . 0.97 . 1.20 . 1.15 . 1.17 . 0.43 . 3 0.44 .1.to .1.25 .1 19 . 0.96 . 1.21 . 1.30 . 1.23 . 0.47 .
f . 2.2 1.9 . 0.1 . -0. 6 . -0.9 0.6 . 3.6 . 5.1 - 7.9 .
. 0.43 . 1.03 . 1.26 . 1.30 . 1.25 . 1.17 . 1.25 . 1.30 . 1.26 . 1.03 . 0.43 .
1.16 . 1.26 . 1 22 . 1.15 . 1.23 . 1.32 . 1,32 1 07 . 0.46 . 4
. 0.45 . 1.04
. 3.9 . 0. 6 . -0.1 . -1.6 . -1. 7 . -1. 6 . -0. 9 . 1.5 . 3.0 . 3.6 . 6.7 .
. 0.4 3 .1.17 . 1.to .1.32 . 1.19 . 0.99 . 1.09 . 0.99 . 1.19 . 1.32 . 1. 26 . 1.17 . 0.43 . 5
. 0.44 . 1.21 . 1.26 . 1.20 . 1.15 . 0.92 . 1.01 . 0.94 . 1.19 ,1,32 . 1.30 . 1.25 . 0.46 .
. 8.9 . t . 9 . -1. 7 . -3. 2 . - 3. 3 . -7. 0 . - 7. 3 . -5. 0 . -0. 2 . 0.3 . 1.3 . 6.2 . 11.0 .
.......................................................................................d.97.
0.97 . 1.25 . 1.30 . 1.19 . 0.74 . 1 04 . 1.23 . 1.04 0.74 . 1.19 1.30 . 1.25 . 4 1.00 . 1.29 . 1.30 . 1.14 0.70 . 0.95 . 3.12 . 0.95 . 0.71 . 1.19 . 1 32 1.30 . 1.05 .
-9. 3 . -9. 0 . -4. 0 . 0. 2 . 1.0 . 4. 2 . 7.5 .
1.1 . 3.1 . -0. 6 . -4. 3 . -5.1 . -6. 6 .
. 0.31 . 1.03 . 1.20 . 1.15 . 0.99 1.04 1.20 . 1.23 . 1.20 . 1.04 . 0.99 . 1.25 . 1.20 . 1.03 . 0.31 . 7
. 0.32 .1.06 .1.t* .1.21 . 0.93 . 0.94 . 1.07 , 1.10 . 1.09 . 0.96 . 0.95 . 1.26 . 1.23 . 1.06 2.7 .. 0.32 3.1 3.0 3.1 . 3.1 . -3. 2 . -4. 6 -7. 3 . -10. 6 . -10. 6 . -9. 3 . -7. 6 . -4. 3 . 1.0 2.0 .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1.17 . . . . .. 0.97
. . . . ... 0.76 . . . . .. .0.55
. 0.55 . 0.76 . 0.97 . 1.17 . 1.09 . 1.23 . 1.13 . 0.94 . 1.23 . 1.23 . 1.09 8
. 0.57 . 0.60 . 1.00 . 1.13 . 1.02 . 1.14 . 1.12 . 0.06 . 1.12 . 1.12 . 1.02 . 1.18
-6. 6 . -6. 5 . -9.1 . -9. 2 . -6. 5 . 1.1 .. 0.99 1.9 .. 0.82 5.2 .. 0.60 4.4 ..
2.6 . 2.5 , 3.1 . - 3. 2 . -6. 5 . - 7.1 .
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1.25 . . . . ... 1.20
. . . . ... 1.03 . . . . ... 0.31
! . 0.31 . 1,03 . 1.20 . 1.25 . 0.99 . 1.04 1.20 . 1.23 . 1.20 . 1.04 . 0.99 9 ! I - 0.32 .1.05 . 1.It .1.20 . 0.93 . 0.97 . 1.10 . 3.15 . 1.10 . 0.95 . 0.93 . 1.26
-6. 6 . -6.6 . -6. 6 . -6. 7 . -4. 2 . 1.5 .. 1.24 3.2 .. 1.11 7.9 .. 0.3511.0 ..
i . 1.9 1.6 . 1. 6 . -3. 7 . -6. 2 . -6. 2 . .
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. . . ... .0.74
. . . . . .3.19
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. . . . .. 1.25
. . . . ... 0.97 ........................
0.97 . 1.25 . 1.30 . 1.19 . 0.74 1.30 . 1.06 . 10
. 0.99 . 1.57 . 1.29 . 1.16 . 0.72 . 0.97 . 2.15 . 0.98 . 0.71 . 1.16 . 1.31.
. 1.6 . 1. 6 . -1. 3 . -3,6 . 2. 6 . -e .1 . -4.3 . -6.1 . -4. 4 . -2.6 . 0.4 4.0 . 10.6 .
. 0.43 . 1.17 . 1.26 . 1.32 . 1.19 . 0.99 . 1.09 . 0.99 . 1.19 . 1.32 . 1.26 . 1.17 . 0.43 . 11
. 0.44 1.21 . 1. 30 .1. 30 . 1.19 . 0.96 . 1.06 . 0.95 . 1.1d . 1. 31 . 1.2.4 31 .. 1.23 . 0.46 .
5.0 . 6.6 .
. 2.9 . 2.6 . 1. 4 . -1.4 . -0. 5 . -2. 9 . - 3. 2 . - 3. 9 . -1.1 . -0.4 . ....
. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 0. .. .4. 3. .. .
. 0. 4 3 . 1. 0 3 . 1. t o . 1.30 . 1. 25 . 1.17 . 1. 25 . 1. 30 . 1.16 . 1. 0 3 l . 0.45 . 1.04 1.26 . 1.30 . 1.25 . 1.17 . 1.26 . 1,32 . 1.30 . 1.06 . 0.46 . It I . 3.6 . 1. 3 . -1. 4 . -0. 5 . col . 0.1 . 1.1 . 1.4 . 1.3 . 3.2 . 6.6 .
. 0.43 . 1.17 . 1.25 . 1.20 . 0.97 . 1.20 . 1.25 . 1.17 . 0.43 13
. 0.47 , 1.33 . 1.34 1.34 1.92 . 1.26 . 1.34 . 1.25 . 0.46 .
6.7 . 3.1 . 4.7 . 6.6 . 7.0 . 6.3 . 6.6 . 6.4 . 13.0
. 0.43 . 0.97 . 1.03 . 0.76 . 1.03 . 0,97 . 0.43 14
. 0.46 . 1.11 . 1.14 . 0.64 . 1.10 . 1.04 0.4. 6.3
. 13.0 . 14.0 . 10.1 . 6.1 . 6.5 . 7.0 .
. 0.31 . 0.55 . 0.31 . . Avt# AGE .
. 57ANDARD .
15
. 0.36 . 0.61 . 0.34 .PC7 DIFFERENCE.
. Dtv1A71DH .
- 4.6
. =3.253 . . 14.1 . 10.5 . 7.4 . .
DATE1 4/10/81 PCWERI 27% MAP Not N1 4 F-Qt T ) = 2.824 QPTRt CONTROL RCD POSITIONSt D BANK AT 58 STEPS F-DH(N) = 1.673 NW 0.982 i NE 1.007
..........l..........
F(Z) = 1.687 SW 0.999 i SE 1.013 F(XY) = 1.846 BURNUP z 0 MWD /MTU A.0 34.56(%)
38 Figure 7.4 MORTH ANNA UNIT 1 - CYCLE 3 BOL PHYSICSJEST ASSEMBLWISE POWER DISTRIBUTION PPELIM I/E CAL FLUX MAP li ea H ri 6 n J H G F 6 0 G 8 A
. h0hbib I03$E05$'.05 . Sibibib
. MEASURED . 0.34 . 0.6 3 . 0.36 . . ME ASUR ED . 1 JC7 D1FFERENC2. . -0.4 . -1.1 . 3.6 . . PCT D1FFERENC2.
. 0.41 . 0.06 . 1.10 . 0.99 . 1.10 . 0.96 . 0.41 .
. 0.42 0.16 . 1.09 . 0.98 . 1.11 . 1.00 . 0.<.3 , 2
. 2.6 . -0. 3 . -0. 7 . -0. 9 . 1. 3 . 3.3 . 5.2 .
0.41 . 1.12 . 1.22 . 1.21 . 1.01 . 1.21 . 1.22 . 1.12 . 0.41 . .
. 0.41 . 1.13 . 1.21 . 1.18 . 0.99 . 1.20 . 1.23 . 1.15 . 0.44 3
( . 0.9 0.7 . 0.6 . 1.9 2.1 . 0.9 1.2 . 3.3 . 7.3 .
. 0.41 . 0.97 . 1.22 . 1.26 . 1.22 . 1.15 . 1.22 . 1.26 . 1.22 . 0.97 . 0.41 .
0.42 . 0.94 . 1.22 . 1.24 . 1.19 . 1.12 . 1.19 . 1.26 . 1.24 . 0.99 . 0.43 . 4
. 3.2 . 0.6 . -0.5 . -2. 2 . -2.8 . -2. 9 . 2. 3 . -0.6 . 1.4 . 2.3 . 4.8
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. 4.43 . 1.16 . 1.21 . 1.26 , 1.16 . 0.92 . 1.00 . 0.93 . 1.18 . 1.27 . 1.22 . 1.16 . 0.44 . 5
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. 0.96 . 1.22 . 1.26 . 1.20 . 0.87 . 1.06 . 1.21 . 1.06 . 0.87 . 1.20 . 1.26 . 1.22 . 0.96 ,
. 1.00 . 1.27 . 1.27 . 1.16 . 0.84 0.98 . l.12 . 0.98 . 0.83 . 1.18 . 1.25 . 1.24 . 1.01 . 6
. 4.1 , 4.1 . 0. 4 . - 3. 3 . -4. 4 . -7.1 . -7.5 . -7. 5 . -4. 7 , -1. 9 -1.1 . 1. 9 . 5.3 .
. 0.34 . 1.10 . 1.21 . 1.22 . 0.93 . 1.06 . 1.19 . 1.21 . 1.19 . 1.06 . 0.98 . 1.22 . 1.21 . 1.10 . 0.34 ,
l
. 0.36 . 1.14 . 1.26 . 1.20 . 0.93 . 1.00 . 1.09 . 1.11 . 1.10 . 0.98 . 0.94 1.20 . 1.21 . 1.11 . 0.36 . 7
( 4.2 . 4.'3 . 4. 3 . -1. 9 . - 5 . 2 . -5. 7 . -4. 0 . -8.1 - 7. 4 -6. 7 . -4. 7 . 1.4 0.1 . 1.6 . 3.0 .
. 0.64 . 0.99 . 1.01 . 1.15 . 1.07 . 1.21 . 1.21 . 0.92 . 1.21 . 1.21 . 1.07 . 1.15 . 1.01 . 0.99 . 0.64 .
. 0.67 . 1.03 . 1.05 . 1.14 . 1403 . 1.15 . 1.13 . 0.86 . 1.13 . 1.11 . 1.01 . 1.14 . 1.01 . 1.04 0.69 8 4.2 . 4.2 . 4. 3 . 1. 3 . -4. 2 . -4. 9 . -6. 5 . -6. 0 . -6. 6 . -6. 7 . -5. 9 . - 1. 3 . 0.1 . 5.2 . 8.4 .
. 8.34 . 1.10 . 1.21 . 1.22 . 0.98 . 1.06 . 1.19 . 1.21 . 1.19 . 1.06 . 0.98 . 1.22 . 1.21 . 1.10 . 0.34
. 0.35 . 1.12 . 1.23 . 1.20 . 0.95 . 1.01 . 1.13 . 1.15 . 1.12 . 0.99 . 0.93 . 1.21 . 1.22 . 1.17 . 0.38 9 2.2 . 2.2 . 2.1 . -1. 9 . - 3. 8 . -4. 4 . -5. 4 . -4.5 . -6.1 . -6. 4 . - 5. 7 . -1. 0 . 1.0 . 6.4 9.9 .
0.96 . 1.22 . 1.26 . 1.20 . 0.87 . 1.06 . 1.21 . 1.06 . 0.87 . 1.20 . 1.26 . 1.22 . 0.96 . i 0.98 . 1.24 . 1.26 . 1.18 . 0.85 . 1.00 . 1.16 . 1.01 . 0.84 1.16 . 1.25 . 1.23 . 1.05 . 10 :
. 2.1 . 2.1 . = 0. 4 . -1. 6 . -3.1 . *4. 9 . -4. 4 . -4.4 . - 3. 7 . 3. 0 . -1. 4 1.5 . 9.0 .
. 0.41 . 1.12 . 1.22 . 1.29 . 1.20 . 0.98 . 1.07 . 0.98 . 1.20 . 1.29 . 1.22 . 1.12 . 0.41 .
. 0.43 . 1.16 . 1.24 . 1.26 . 1.18 . 0.96 . 1.05 . 0.95 . 1.18 . 1.27 . 1.24 . 1.15 . 0.44 . 11
. 3.8 . 3.8 . 1. 7 . -2. 2 . -1. 5 . -2. 2 . -2. 3 . -2. 9 . -1. 2 . -1. 4 1. 3 . 3.3 . 5.8 .
. 0.41 . 0.97 . 1.22 . 1.26 . 1.22 . 1.15 . 1.22 . 1.26 . 1.22 . 0.97 . 0.41 .
. 0.43 . 0.91 . 1.20 . 1.27 . 1.25 . 1.18 . 1.24 . 1.27 . 1.23 . 1.00 . 0.43 . 12
. 5.5 . 1.7 . -2.2 . 0.5 . 2.2 . 2.1 . 1.6 . 0.7 . 0.6 . 3.1 . 6.8 .
. 0.41 . 1.12 . 1.22 . 1.21 . 1.01 . 1.21 . 1.22 s 1.12 . 0.41 .
. 0.44 1.23 . 1.30 . 1.27 . 1.08 . 1.29 . 1.30. 1.17 . 0.43 . 13
. 7.9 . 10.4 4.8 5.3 . 6.7 ' . 7.1 . 6.7 . 4.5 . 6.8 .
. 0.41 . 0.96 . 1.10 . 0.99 . 1.10 . 0.96 . 0.41 .
. 0.45 . 1.09 . 1.22 . 1.09 . 1.18 . 1.03 . 0.43 . 14
. 10.5 . 13.1 . 11.6 . 10.4 7.4 7. 0 . 4.5 .
STANDARD . 0.34 0.64 . 0.34 . . AVERAG2 .
. DEVIA71DN . . 0.40 . 0.72 . 0.38 . .PC7 DIFFIliENCE. 15
. s2.927 . . 15.4 . 12.4 . 9.4 , s 4.0 .
MAP N01 N1 5 DATE: 4/11/81 PCWEP: 27% CCHTROL RCD POSITIONS: F-Q(T) = 2.444 QPTP2 D BANK AT 138 STIPS F-DH(N) = 1.570 HW 0.984 l NE 0.989
..........l..........
F(2) = 1.483 SW 1.015 l EE 1.013 F(XY) = 1.731 BURNUP = 10 MWD /MTU A.0 3 -13.60(%)
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40 Figure 7.6 NORTH ANNA UNIT 1 - CYCLE 3 BOL PHYSICS TEST ASSEMBLYWISE POWER DISTRIBUTIOM f APDMS - FLUX MAP i 1 1 I R P N M L K J H 8 F E O C 8 A
. PREDIC7ED . . 0.36 . 0.64 . 0.36 . . PREDICTED .
MEASURED . . 0.39 . 0.74 . 0.39 . MEASURED . 1 l .
.PC7 01FFERENCE. 4.3 . 4.2 7.4 .PC7 01FFERENCE.
. 0.39 . 0.94 . 1.12 . 1.11 . 1 I t . 0. 94 . 0.39
. 0.41 . 0.93 . 1.15 . 1.13 . 1.17 . 1.00 . 0.48 8
. 4.2 . -0.4 2.5 . 2.4 4.9 . 6.4 . 7.8 .
0.39 1.06'. 1.16 . 1.21 . 1.03 . 1.21 . 1.16 . 1.06 0.39 , .
. 0.39 . 1.07 . 1.16 . 1.19 . 1.02 . 1.21 . 1.11 . 1.11 . 0.48 3
. 1.0 . 0. 7 . -1. 4 . -1. 5 . -1,6 . 0.0 . 2.3 . 4.4 . 4.2 .
. 0.39 . 0.93 . 1.18 . 1.24 . 1.11 . 1.15 . 1.31 . 1.24 . 1.16 . 0.93 . 0.39 .
. 0.40 . 0.93 . 1.17 . 1.20 . 1.18 . 1.12 . 1.19 . 1.81 . 1.19 . 0.95 . 0.41 . 4
. 3.5 . 0. 8 . -0. 9 . - 2. 9 -2. 5 . 2. 6 . -2.1 . *1. 9 1.1 . 1.2 . 5.7 ,
. 0.39 . 1.06 . 1.16 . 1.27 . 1.21 . 0.99 1.06 . 0.99 . 1.11 . 1.27 . 1.18 . 1.06 0.39
. 0.41 . 1.10 . 1.16 . 1.23 . 1.16 . 0.93 . 1.01 . 0.94 . 1.17 . 1.24 . 1.17 . 3.11 . 0.43 . 5
- 3. 0 . 3. 0 . -1. 8 . -3. 5 . - 3. 9 . -4. 5 . -6. 6 . - 5. 5 . -3.1 . -2. 2 . -0. 8 , 4.5 . 8.7 .
. 0.94 . 1.18 . 1.24 . 1.81 . 0.96 . 1.09 . 1.23 . 1.09 . 0.98 . 1.21 . 1.24 . 1,16 . 0.94 .
. 0.97 . 1.23 . 1.24 . 1.17 . 0.93 . 1.01 . 1.13 . 1.00 . 0.93 . 1.16 . 1.21 . 1.21 . 1.00 6
. 3. 6 . 3. 8 . -0.1 . 3. 6 . -4. 8 . 7. 5 . -7. 7 . -7. 9 . -5. 2 -2. 9 . - 2.1 . 2.4 . 6.8 .
. 0. 36 . 1.12 . 1.11 . 1.11 . 0.99 . 1.09 . 1.21 . 1.22 . 1.21 . 1.09 . 0.99 1.21 . 1.21 1.12 . 0.36 ,
. c.18 .1.17 . 1.26 . 1 19 . 0.94 . 1.03 . 1.11 . 1.12 . 1.12 . 1.01 . 0.93 . 1.16 . 1.11 . 1.15 . 0.38 . 7
. 4. 5 . 4.5 . 4.5 . -t . 0 . -5.5 . -G . 9 . -4.4 . -4. 3 . -0. 0 . - 7. 2 . -6. 0 . -3. 3 . 0.3 . 2.6 . 4.9
. 0.68 1.11 . 1.03 . 1.15 . 1.08 . 1.43 . 1.2 t . 0.93 . 1.22 . 1.23 . 1.08 . 1.15 . 1.03 . 1.11 . 0.66 .
. 0.71 . 1.15 . 1. ca . 1.13 . b. 02 . 1.16 . 1.13 . 0.87 . 1.13 . 1.14 1."00 . . 1.13 . 1.04 . 1.16 . 0.75 . 4
. 4.4 . 4.4 4. 5 -1. 7 . -4. 6 . -5. 4 . -6. 8 . -4. 5 , - 7.1 . -7.1 . -4. 6 . -t . 0 , 0.3 . 6.7 . 10.5 .
. 4. 36 . 1.12 1.11 . 1.21 . 0.99 1.09 1.21 . 1.22 . 1.21 . 1.09 . 0.99 . 1.11 . 1.21 . 1.12 . 0.36 .
. 0.37 . 1.14 1.43 . 1.14 . 0.95 . 1.04 . 1.14 . 1.15 . 1.13 . 1.01 0.93 . 1.19 . 1.22 , 1 20 . 0.40 . 9
. 1.9 1.9 1. 9 . = 2. 5 . -4. 4 . -5. 0 -6. 0 . -5. 5 . -6. 8 . - F . 0 . -6. 3 . -1. 4 . 1.1 . 7.5 . 11.5 .
. 0.94 1.18 . 1.24 1.21 . 0.98 . 1.09 1.23 . 1.09 0.96 . 1.21 . 1.24 . 1.18 . 0.94 .
. 0.95 . 1.20 . 1.22 . 1.18 . 0.94 . 1.04 . 1.17 . 1.04 . 0.94 1.17 . 1.21 . 1.20 . 1.03 . 10
. 1.9 . 1. 6 . -1.1 . 2. 6 . -3. 9 . -4. 7 . -4. 7 . -4. 6 . -4.1 . - 3.4 . 2.1 . 1.4 . 10.4 .
. 0.39 . 1.06 . 1.14 . 1.17 . 1.21 . 0.99 . 1.06 . 0.99 1.21 . 1.27 . 1.18 . 1.06 . 0.39
. 0.41 . 1.11 . 1.80 . 1.23 . 1.18 . 0.97 . 1.05 . 0.97 . 1.19 1.24 1.19 . 1.10 . 0.42 . 11 4.1 . 4.1 . 1. 7 . -2. 8 . -4. 3 . -1. 4 , -8.4 . -2.6 . -1. 8 . -4.1 . 1.0 , 3.5 . 6.6 .
. 0.39 . 0.93 . 1.14 . 1.34 . 1.31 . 1.15 . 1.21 . 1.24 . 1.18 . 0.93 . 0.39
. 0.41 . 0.95 . 1.15 . 1.23 . 1.23 . 1.17 . 1.22 . 1.24 . 1.14 . 0.96 , 0.42 . 12
. 6.3 . 1.9 . -2.6 . =0.4 1.6 . 1.6 . 1.0 . 0.1 . 0.0 . 3.3 , 7.5 .
. 8.39 . 1.06 . 1.18 . 1.21 . 1.03 . 1.21 . 1.18 . 1.06 . 0.39 .
. 0.42 . 1.19 . 1.86 . 1.15 . 1.09 . 1.26 . 1.26 . 1.10 . 4.42 , 13
. 8.9 . 11.5 . 6.7 . 3.9 5.8 6.4 , 6. 3 . 3.6 . 7.5 . -
l . 0.39 . 0.94 . 1.12 . 1.11 , 1.11 . 0.94 0.39 0.44 . 1.07 . 1.25 . 1.12 . 1.19 . 1.00 . 0.41 . 14
. 11.5 . 14.3 . 11.6 . 10.4 . 6.6 . 6.6 3.6 .
. STANDADD . 0.36 . 0.68 . 6.36 . AVERAGE .
. DEVIATION . . 0.42 . 0.77 . 0.39 . ..PC7 DIF8tRENCE. 15 83.111 . . 16.9 . 13.2 9.5 . s 4.5 MAP HO! N1 9 DATE: 4/15/81 POWER: 49%
CONTPOL POD POSITIONS: F-Q(T) = 2.064 QPTR; D BANK AT 206 STEPS F-DH(N) = 1.545 HW 0.982 l NE 0.994
..........i..........
F(Z)
- 1.278 SW 1.015 l SE 1.010 F(XY) = 1.629 BURNUP z 63 MWO/MTU A.0 t 1.81(%)
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..........g..........
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42 Figure 7.8 i \ NORTH ANNA UNIT 1; CYCLE 3 BOL PHYSICS TEST l j l ASSEMBLYWISE POWER DISTRIBUTION APDMS, I/E CALIBRATION - FLUX MAP 1 l N P N N 4 K J H G F 2 D C 8 A
.s............. . . . . . . . . . . . . . . . . . . . . . . ...............
j , PREDICTED . . O.37 . 0.70 . 0.37 , PREDICTED
. NEASURED . . 0.39 . 0.73 . 0.38 . NE ASUR ED . 1
.PC7 DIFFERtNCE. . 4-3 . 4.2 . 4. 0 . ..PC7 01FFERENCE.
. 0.40 . 0.94 . 1.12 . 1.10 . 1.12 . 0.94 0.40 .
. 0.42 . 0.93 . 1.13 . 1.11 . 1.14 . 0.98 . 0.42 . t 4.8 . -1. 0 . 0.6 . 0.6 2.2 . 3.5 . 4.6 .
. 0.40 . 1.07 . 1.17 . 1.20 . 1.04 . 1.20 . 1.17 . 1.07 . 0.40 .
. 0. 41 . 1. 0 9 . 1.16 . 1.17 . 1. 01 . 1.19 . 1.18 . 1. 0 9 . 0.4 L . 3 2.3 . 2. 0 . -0. 9 , -2. 5 . -2.6 . -1. 3 . 0.8 , 2.5 . 5.9 .
. 0.40 . 0. 94 1.17 . 1.23 . 1.20 , 1.15 . 1.20 . 1.23 . 1.17 . 0.94 . 0.40 .
. 0.41 . 0.94 . 1.17 , 1.20 . 1.17 . 1.11 . 1.17 . 1.21 . 1.18 . 0.95 . 0.42 . 4
. 3. 7 . 1.0 , 0. 2 . - 2.1 . - 3. 0 . - 3. 0 . -2. 9 . -1.6 , 0.6 , 1.6 . 4.6 0.40 . 1.07 . 1.17 . 1.26 . 1.20 . 1.00 . 1.08 . 1.00 . 1.20 , 1.26 . 1.17 . 1.07 . 0.40 .
0.42 . 1.10 , 1.16 . 1.23 . 1.17 . 0.94 . 1.01 . 0.95 . 1.17 . 1.24 . 1.16 . 1.11 . 0.44 . 5
. 2.6 . 2.8 -1. 0 . -2.4 . -2. 7 . -5.4 . -6. 0 . -4. 9 .. -2.2 . - 1. 6 . -0. 5 . 4.3 . 4.4 .
. 0.94 . 1.17 . 1.23 . 1.20 . 0.98 . 1.09 1.23 . 1.09 . 0.98 . 1.20 . 1.23 . 1.17 . 0.94 .
. 0.97 . 1.21 . 1.23 . 1.16 . 0.94 . 1.03 . 1.15 . 1.02 . 0.94 . 1.18 . 1.21 . 1.20 . 0.99 . o
. 3.2 . 3.2 , -0. 0 . 3. 2 . - 3. 9 -5.9 -4. 0 . -6.1 . 3. 8 . ,- 1. 8 . -1. 2 2.1 . 5. 3 ,
. 0.37 . 1.12 . 1 20 . 1.20 . 1.00 . 1.09 . 1.21 . 1.22 . 1.21 . 1.09 . 1.00 . 1.20 . 1.20 , 1.12 . 0.37
. 0.36 . 1.16 . 1.25 . 1.18 . 0.95 . 1.04 . 1.13 . 1.14 . 1.14 . 1.03 . 0.96 . 1.18 . 1.30 . 1.13 . 0.38 . 7 3.6 . 1.6 , 3.6 , -1. 5 . -4. 2 . -4.6 , -e . 8 . -6.6 . -4.0 . -5.8 -4. 0 . -1.6 , -0.3 . 0.9 . 2.2 .
\ . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. 0.70 . 1.10 , 1.04 . 1.15 . 1.04 . 1.23 . 1.22 . 0.44 . 1.22 . 1.23 . 1.08 . 1.15 . 1.04 1.10 . 0.70 ,
. 0.72 . 1.14 . 1.08 . 1.13 . 1.04.. 1.14 . 1.15 . 0.89 . 1.15 . 1.14 . 1.03 . 1.13 . 1.04 . 1.15 . 0.74 . 8 3.6 . 3.6 . 3.6 - 1.1 . - 3. 5 , -4. 0 - 5. 3 . -4. 8 . - 5. 3 . -5.4 . 4.9 -1. 5 . 0.3 . 3.4 , 6.4
. 0.37 1.12 . 1.20 . 1.20 . 1.00 . 1.09 . 1.81 . 1.22 . 1.21 . 1.09 . 1.00 . 1.20 . 1.20 . 1.12 0.37
- 0.38 . 1.15 . 1.24 . 1.19 . 0.96 . 1.05 . 1.16 . 1.17 . 1.15 , 1.03 . 0.95 . 1.19 . 1.21 . 1.18 . 0.40 .
. 9 l 2. 9 . 2.9 , 2. 8 . -1. 3 . - 3. 2 . - 3. 6 . -4.1 . - 3. 7 . - 5.1 , . e . 3 . 4. 8 , - 1. 3 . 0.9 , 5.3 . 6.3 .
) . . ....... . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. 0.94 . 1.17 . 1.2 3 . 1.2 0 . 0. 98 . 1. 09 . 1. 23 . 1. 09 0. 9e . 1. 20 . 1. 2 3 . 1.17 . 0. 94 .
. 0.97 . 1.21 . 1.23 . 1.18 . 0.95 . 1.04 . 1.10 . 1.05 . 0.94 . 1.17 . 1.21 . 1.19 . 1.02 . 10
. 2.8 . 2.8 . -0.8 . -1.8 . - 2. 6 . -4.4 . -4. 0 . -4. 0 . - 3. 2 -2. 7 1.7 . 1. 7 . 7. 7 .
...........................................................4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .
. 0.40 . 1.07 . 1.17 . 1.26 . 1.20 . 1.00 . 1.08 . 1.00 . 1.23 . 1.26 . 1.17 . 1.07 . 0.40
. 0.42 . 1.11 . 1.19 1.23 . 1.10 . 0.97 . 1.05 . 0.94 . 1.18 . 1.24 . 1.14 . 1.10 . 0.43 . 11
. 4.1 4.1 1. 9 . - 2. 2 . -1.4 . =2.2 , -2. 3 . - 3.2 . - 1. 4 . -1. 6 . 1.1 - 3,5 . 6.1
. 0.40 . 0.94 . 1.17 . 1.23 . 1.20 . 1.15 . 1.20 . 1.23 . 1.17 . 0.94 . 0.40 .
. 0.42 . 0.95 . 1.14 1.33 . 1.21 . 1.15 . 1.21 . 1.23 . 1.17 . 0.96 . 0.42 - 12 5.3 . 1. 7 . -2,2 . 0.1 . 0.4 . 0. 7 . 0.5 . 0.4 . 0.3 , 3. 0 , 6.9 .
. 0.40 . 1.07 . 1.17 . 1.20 . 1.04 . 1.20 . 1.17 . 1.07 . 0.40
! . 0.43 . 1.18 . 1.25 . 1.24 . 1.08 - 1.26 . 1 23 . 1.11 . 0.42 . 13 7.9 . 10.5 . 6.3 . 3. 3 . 4.4 5.0 . 3.1 . 3. 9 . 6.9 l .. ... ........................................... ... . .. l . 0.40 . 0.94 . 1.12 . 1.10 - 1.12 . 0.94 . 0.40 .
. 0.45 . 1.05 . 1.22 . 1.19 . 1.18 . 0.99 . 0.44 . 14 l
10.5 . 11.9 . 8. 9 . 7. 7 . 5.1 . 5.2 3.9 . STANDARD 0.37 . 0.70 , 0.37 . - AVERAGE . DIVIA73CN , . 0.42 . 0.77 . 0.39 .PC7 OIFFERENCE. 15
. 82.411 . 13.0 . 9.8 6.5 .
- 3.6 MAP HO: Hl.3-11 DATE: 4/15/81 POWER: 74%
CONTROL POD FOSITIDHS: F-Q(T1 = 2.124 QPTR: D BANK AT 190 STEPS F-DHtH) = 1.509 HW 0.989 1 NE 0.990 _.........l.._____.-- F(Z) = 1.343 SW 1.016 l SE 1.004 F(XY) = 1.591 BURNUP
- 73 MW3/MTU A.0 = -10.15t%)
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- 0 = -19
- 6f) % (
> Figure 7.10 44 NORTH ANNA UNIT 2 - CYCLE 5 BOL PHYSICS TEST ASSEMBLYWISE POWER DISTRIBUTION APDMS, I/E CALIBRATION - FLUX MAP i
l l I E P H M L K J M G F 2 0 C 6 4 1 ( . P8201CTED 0.38 . 0.71 . 0.38 . . PREDICTED I
. ME ASUR ED . . 0.40 . 0.75 . 0.39 . M2ASURF0 . 1
. PCT DIFF262NC2. 5.1 , 5.0 . 4.4 . . PCT CIFFEPENC2.
. 0.41 . 0.94 . 1.13 . 1.12 . 1.13 . 0.94 0.41 .
0.42 . 0.94 . 3.14 . 1.14 1.16 0.98 . 0.43 . 2
- 3. 9 . -0.6 1.2 , 1.0 . 2. 7 . 3. 7 , 4.6 ,
. 0.40 . 1.06 . 1.17 . 1.20 . 1.04 4 1.20 . 1.17 . 1.06 . 0.4 0 ,
0.40 . 1.06 . 1.16 . 1.18 . 1.02 . 1.19 . 1.16 . 1.09 . 0.42 . 3 l . 1.6 . 1. 3 -0. 9 . - 1. 9 . -2.0 , -0.9 . 1.1 2.6 , 5.9 .
. 0.40 . 0.93 . 1.16 . 1.22 . 1.20 , 1.14 . 1.20 . 1.22 . 1.16 . 0.93 . 0.40
. 0.41 . 0.94 1.16 1.20 . 1.17 . 1.11 . 1.17 , 1.20 . 1.17 , 0.95 . 0.42 .
- 2.9 . 0.5 . =0.2 -2.1 -2. 5 . -2. 6 . 2.4 -1.4 , 0.8 . 1.7 e.6 0.41 . 1.06* . 1.16 . 1.25 . 1.20 . 1.00 . 1.06 , 1.00 . 1.20 . 1.25 . 1.16 . 1.06 . 0.41 .
0.41 1.06 . 1.15 . 1.22 . 1.16 , 0.94 1.02 . 0.95 . 1.17 . 1.24 . 1.16 . 1.10 . 0.44 . 5
. 2.0 . 2. 0 . -1. 2 . -2. 2 . -2. 6 . - 5.4 . - 5. 5 . -4. 2 . -1. 8 . - 1. 2 -0.4 . 4.0 . 7. 6 .
. 0.94 1.17 . 1.22 . 1.20 . 0.99 A.09 1.23 . 1.09 . 0.99 1.20 . 1.22 . 1.17 . 0.94 .
. 0.97 . 1.20 . 1.22 . 1.16 . 0.95 . 1.03 . 1.16 , 1.03 . 0.95 . 1.18 , 1.21 . 1.19 . 0.99 6
, 2.6 . 2. 5 . -0.1 -2.7 , 3.6 -5.6 -5.6 . -5.5 . - 3.4 . -1.4 . - 1. 0 . 2.0 5. 0 .
............ ........................................... .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . \
0.38 . 1.13 . 1.20 . 1.20 . 1.00 . 1.09 . 1.21 . 1.21 . 1.21 . 1.09 . 1.00 . 1.20 . 1.20 , 1.13 . 0.36 . I
. 0.39 . 1.16
. . 1.24 . 1.16 . 0.96 . 1.04 - 1.14 . 1.14 . 1.15 . 1.04 0.96 . 1.16 . 1.20 , 1.14 0.39 7 l'
! 3.1 . 3.1 3.1 . -1. 5 . -4. 0 . ** . 4 . -6.4 . ~6. 3 , -5. 6 . -4.8 . -3.5 , -1.1 , 0.1 1. 3 . 2. 3 .
- t. 1
. 0.71 . 1.12 . 1.04 . 1.14 1.06 . 1.23 . 1.21 . 0.94 , 1.21 . 1.23 . 1.08 . 1.14 . 1.04 1.12 . 0.71
. 0.73 . 1.16 . 1.08 . 1.13 . 1.04 . 1.16 . 1.15 . 0.90 . 1.15 . 1.16 . 1.03 1.13 . 1.04 . 1.17 . 0.76 . e 3.1 . 3.2 . 3.1 -1. 4 . - 3. 6 . -4.1 . -5.1 . -4. 7 . -5.1 . -5. 2 . -4. 6 , -1. 0 . 0.1 4. 4 . 7. 0 ,
. 0.38 . 1.13 . 1.20 . 1.20 . 1.00 . 1.09 , 1.21 . 1.21 . 1.21 . 1.09 . 1.00 , 1.20 . 1.20 1.13 . 0.38 .
. 0.38 . 1.15 . 1.23 . 1.18 . 0.96 . 1.05 . 1.16 . 1.17 . 1.15 . 1.04 0.95 , 1.19 , 1.21 . 1.19 . 0.41 . 9
. 2.2 , 2.1 . 2. 0 . - 1. 7 . - 3. 3 . - 3. 6 -4. 0 - 3. 5 . -4. 6 . - 5. 0 . -4.5 . -0.9 . 0.9 . 5.6 6.6 .
. 0.94 . 1.17 . 1.22 . 1.20 . 0.99 1.09 . 1.23 , 1.09 . 0.99 . 1.20 . 1.22 . 1.17 . 0.44 .
. 0.96 . 1.19 . 1.21 . 1.17 . 0.96 . 1.05 . 1.18 , 1.05 . 0.96 . 1.17 . 1.20 . 1.16 . 1.02 . 10 2.0 . 2.0 -0.6 . -1.9 . - 2. 7 . -4.1 , = 1. 7 . - 3. 6 , 2.9 -2.5 -1.6 1.4 7. 9 .
. ......0.41 . 1.06 . 1.16 . 1.25 . 1.20 . 1.00 . 1.08 . 1.00 . 1.20 . 1.25 . 1.16 . 1.06 . 0.41 .
. 0.42 . 1.10 , 1.18 . 1.22 . 1.18 . 0.97 . 1.05 0.97 1.16 . 1.23 . 1.17 1.09 0.43 . 11
- 3. 4 , 3.4 . 1. 4 . -2. 2 . -1. 6 , ~2.2 . -2.3 -2.6 . - 1. 2 - -1.4 . 0.7 . 2.8 5.1 .
. 0.40 . 0.93 . 1.16 . 1. 2 2 , 1. 2f . 1.18
. 0.42 . 0.95 . 1.14 . 1.22 . 1.21 . 1.11 . 1,29 1.21 ., 1.22 1.23 .. 1.161.17 .. 0.93 0.95 ., 0.40 0.42 , 12 4.8 , 1.4 . -2.2 , =0.3 . 0.4 . 0.7 0.4 . 0.5 . 0.4 . 2.3 . 5. 5 *.
0 . 4 0 . 1. 0 6 . 1.17 . 1. 2C 1.0' 1.*3 . 1.17 . 1.06 . 0.40 , 0.43 . 1.16 . 1.23 . 1.24 13
. 7.1 9. 3 . 5.4 . 3.1 . 1.4.1 s ' . 1.4.to 9 .. 1.4.29 2 . . 3.6 1.10 , . 5.5
- 0. 4. 2 .
. 0.41 0.94 . 1.12 , 1.12 . 1.13 . 0.94 . 0.41
. 0.44 . 1.05 . 1.23 . 1.21 . 1.18 . 0.99 0.42 14 9.4 . 11.1 8.9 , 7.7 . 5.0 . 5.0 . 3.6 .
STANDARD 0.32 . 0.71 . 0.38 . . AVER 42 . Oty!ATICH 0.42 , 0.76 . 0.40 , . PCT O!FFERENCE. 15 m2.321 .. 12.8 . 9.6 6.4 a 3.4 MAP N01 N1-3-13 DATE 4/16/81 PC 4 F . 65% CONTROL RCD POSITIONS F-Q(T) = 1.983 QP' O D BANK AT 210 STEPS F-CH(H) = 1.498 PN 0.991 1 NE 0.990
....l_.._______
F(Z) = 1.275 SW 1.013 l SE 1.007 F(XY) z 1.574 BURNUP = 88 i%'3/MTU A.0 = 2.88(%)
45 i l Figure 7.11 QRTH ANNA UNIT 1 - CYCLE 3 BOL PHYSICS TEST ASSEMBLYWISE POWER DISTRIBUTION HFP, EQ. XENON - FLUX MAP R P N M L K J H S F 2 0 C B A j
. PRE 01CTED . . 6.38 . 0.72 . 0.3a . . PREDICTED .
. , MEASU2ED . . 0.40 . 0.75 . 0.39 . MEASURED 1
.FCT 01FFEAENCE. . 3.5 . 3.5 . 2.9 . .PC7 01FFERENCE..
0.41 . 0.94 . 1.12 . 1.13 . 1.12 . 0.94 . 0.41 .
. 0.41 . 0.93 . 1.13 . 1.14 1.14 . 0.96 . 0.43 . 2
. -1. 0 . 0.5 . 0.7 . 0.7 - 1.6 . 2.2 . 4.3 .
. 0.40 . 1.05 . 1.16 . 1.19 . 1.04 . 1.19 . 1.16 . 1.05 . 0.40 .
0.40 . 1.04 . 1.15 . 1.17 . 1.02 . 1.16 . 1.16 . 1.06 . 0.43 . 3
. -1. 0 . -1. 0 . -0. 6 . -1. 9 . -2. 0 -1.1 0.5 . 2.6 6.6 .
. 0.40 . 0.93 . 1.15 . 1.21 . 1.19 . 1.14 . 1.19 . 1.21 . 1.15 . 0.93 . 0.40
. 0.41 . 0.9) . 1.14 . 1.19 . 1.17 . 1.11 . 1.17 . 1.20 . 1.17 . 0.95 . 0.42 . 4
. 1. 5 . -0. 6 . -1.6 . -1. 4 . -2. 4 . -2.5 . -2. 3 . -1.1 1.1 2.1 3.6 .
. 0.41 . 1.05 . 1.15 . 1.24 . 1.20 . 1.00 . 1.04 . 1.00 . 1.20 . 1.24 . 1.15 . 1.05 . 0.41 .
. 0.42 . 1.07 . 1.14 . 1.22 . 1.17 . 0.95 . 1.03 . 0.97 . 1.18 . L.23 . 1.15 . 1.06 . 0.41 . 5
. 1.5 . 1.5 . -1.1 . -2. 0 . -2. 5 . -4. 9 . -5. 0 . -3. 7 . -1. 4 . 0.9 . -0.2 . 0.6 , 1.2 .
. 0. 94 . 1.16 , 1.21 . 1.20 . 1. 01 . 1.10 . 1.2 3 . 1.10 . 1. 01 . 1. 2 0 . 1.21 . 1.le . 0. 94
. 0.96 . 1.16 . 1.21 . 1.17 . 0.96 . 1.05 . 1.17 . 1.05 . 0.99 . 1.18 . 1.20 . 1.16 . 0.95 . 6
. 2.0 . 2. 0 . -0. 2 . - 2.4 . 3.1 . -4. 8 . -5. 0 . -4. 5 . -1. 6 . -1.1 -0.6 . -0.0 . 1.2 .
) . 0.38 . 1.12 . 1.19 . 1.59 . 1.00 . 1.10 , 1.22 . 1.22 . 1.22 . 1.10 . 1.00 . 1.19 . 1.19 . 1.12 . 0.38 .
. 0.39 . 1.15 . 1.22 . 1.17 . 0.96 . 1.06 . 1.15 . 1.15 . 1.16 . 1.06 . 0.97 . 1.18 . 1.19 . 1.13 . 0.39 7
. 2.6 . 2.6 . 2. 6 . -1. 8 . -4. 2 . -4.1 . 5. 3 . -5. 5 . -4. 7 . - 3. 5 . - 3. 0 . -1. 3 . -0. 4 . 0.5 . 1.2 ,
. 0.72 . 1.13 . 1.04 . 1.14 . 1.08 . 1.23 . 1.22 . 0.95 . 1.22 . 1.23 . 1.08 . 1.14 1.04 . 1.13 . 0.72 .
. 0.74 . 1.16 . 1.07 . 1.13 . 1.04 . 1.19 . 1.17 . 0.92 . 1.17 . 1.18 . 1.04 . 1.13 . 1.04 . 1.10. 0.77 . 8
. 2.6 . 2.6 . 2. 6 . -1. 4 . -3. 5 . -3. 6 . -4. 0 3.1 . -4.2 . -4 3 . -4.1 . -1.2 . -0.4 . 3.9 . 6.4 .
. 0.38 . 1.12 . 1.19 . 1.19 . 1.00 . 1.10 , 1.22 . 1.22 . 1.22 . 1.10 . 1.00 . 1.19 . 1.19 . 1.12 . 0.36 .
. 0.39 . 1.14 . 1.21 . 1.17 . 0.97 . 1 07 .* 1.17 . 1.18 . 1.17 . 1.06 . 0.96 . 1.18 . 1.18 . 1.19 . 0.43 . 9
. 1. 3 . 1.3 . 1. 3 . - 1.0 . -3.1 -3.5 . 3. 9 . -3.0 . -4.1 . -4. 3 . -4.2 . -1. 3 1. 3 . 5.6 . 11.3 .
. 0.94 . 1.16 . 1.21 . 1.20 . 1.01 . 1.10 . 1.23 . 1.10 . 1.01 . 1.20 . 1.21 . 1.16 . 0.94
. 0.95 . 1.17 . 1.20 . 1.18 . 0.98 . 1.06 . 1.19 . 1.07 . 0.98 . 1.17 . 1.19 . 1.13 . 1.04 10
. 1.3 . 1.3 . -0.5 . -1.4 . -2.3 . -3.6 . 3. 3 . -3.1 . -2. 3 . -2. 2 . -1.4 . -2.1 . 11.3 .
. 0.41 . 1. 05 . 1. L5 . 1.24 . 1.20 . 1. 0 0 . 1. 06 . 1. 00 . 1. 2 0 . 1.24 . 1.15 . 1. 0 5 . 0.41 .
. 0. 4 3 . J . 0 9 . 1.16 . 1. 2 2 . 1.18 . 0. 98 . 1. 0 6 . 0. 96 . 1.19 . 1. 2 3 . 1.17 . 1. 08 . 0. 44 11
. 3. 9 . 3.9 . 1. 9 . -1. 9 . -1. 7 . - 2. 3 . . t .4 . -2. 4 . 0.8 . -1.2 1.2 . 2.3 . 6.5 .
. 0.40 . 0.93 . 1.15 . 1.21 . 1.19 . 1.14 . 1.19 . 1.21 . 1.15 . 0.93 . 0.40 .
. 0.43 . 0.95 . 1.13 . 1.20 . 1.20 . 1.14 . 1.20 . 1.21 . 1.16 . 0.96 . 0.43 . 12
. 6.5 . 2. 4 . -1. 9 . -0. 5 . 0.2 . 0.1 . 0.3 . 0.4 0.4 3.1 . 6.5 ,
. 0.40 . 1.05 . 1.16 . 1.19 . 1.04 . 1.19 . 1.16 , 1.05 . 0.40 .
0.44 . 1.16 .1.22 . 1.22 . 1.07 . 1.23 . 1.20 . 1.0a . 0.4 3 . 13
. 8.1 . 9.8 . 5.3 . 2. 0 . 3. 0 . 3.6 . 3.6 . 2.7 . 6.5 .
. 0.41 . 0.94 . 1.12 . 1.13 . 1.12 . 0.94 . 0.41
. 0.45 . 1.04 . 1.21 . 1.21 . 1.16 . 0.97 . 0.42 . 14
. 9.8 . 10.6 . 7.7 . 6.5 . 3.7 . 3.7 . 2.7 .
STANDARD . . 0.38 . 0.72 . 0.34 , . AVERACE ,
. Oly!AT10H . 0.43 . 0.78 . 0.40 . . PCT 01FFERENC2. 15
. s2. 16 3 . 11. 9 . 6.5 . 4.8 . s 2.9 l
l l MAP HO: N1-3-14 DATE: 4/07/81 N . .. . 3% CCNTROL RCD FOSITICHS- F-QtTI = 1.953 GFIE' D BANK AT 024 STEF3 F-CHIN) = 1.474 U'. . v d7 . tJE 0.903 ;
.........-;.......... 1 F(Z) = 1. M4 SN 1.013 l SE 1.C07 ]
1 FtXY)
- 1.553 1 i
BUPNUP
- 487 t'W3/MTU A.0 : -7. cst % )
l l
46 Section 8 REFERENCES 1, S. A. Ahmed, M. C. C h e o k , - T '. W. Schleicher, " North Anna Unit 1, Cycle'3, Design Report,"'HFE Technical Report'No. 161, Vepco, December, 1980.
- 2. North Anna Unit 1 Technical Specifications.
3.'T. M. Ross,2 W. C. Beck, " Control. Rod Reactivity Worth' Determination By The Rod Swap Technique," -VEp-TRD-36A,-December, 1980. 4 l. . T . J. Kunsitis, "RXFLOW, A Computer program to Calculate Reactor l Flou and Thermal Output," KFO-CCR-8, Vepco, December, 1979.
]
- 5. " Technical. Manual for Westinghouse Solid State Reactivity Computer,"
Westinghouse Electric Corporation.
- 6. Memorandum from R. M. Berryman to E. J. Lorito, " Evaluation of l North Anna 1 Cycle 3 Rod Swap Test Deviation," April 8, 1L31, 7.' Memorandum from R. M. Berryman to E. J. Lo=ito. " Evaluation of North Anna 1 Cycle 3 Rod Suap Test. Deviation," April 10, 1981.
- 8. W. Leggett and L. Eisenh' art, "The INCORE Code," WCAp-7149, December, 1967.
i It
47 r ' APPENDIX STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEETS 1 O
1 PT-94 1 .s: , ATTACEDENT 6.11 . j
- V .
I i Page 3 of 4I
- c. 02-11-81 f A.1 flerth ' A.ms l'over ' S ta tion Unit [ Cycle 3,, *
.i.
Startup thysics Tests Resulto and Evaluation Sheet e Test Descripcion: Reactivity Cor::puter Checkout s I' Procedurc 1:ur.t,cr/Section: 1-PT-94/ App. B equence step Sumber: g Heterence. to
- RCS Tet.porsture ('r): 547 -5
?.sak Positions (stepc)
II Fo'.ect Level (%F.P.): 0 ' Test S'.'B : 228 'CA: 228 other (specify): Conditions St/.: 228 CD: * .Below Nuclear Heating (Design) CB 728- CC: 228 RCCA: NA *At the just critical position ECS Temperature (*F): SV4/1.Y
- Bsak Fo:icions (steps) Power Level (::F.P.): 0 '7, III.
Tesc ,. CA: "r2 7 Other (specify): SDA: l'2.% SDB: 2l2.7 . Condicions (l.ctual) CB: O CC: %'1A CD: 2.'t.% . gg SM Q,h)
- RCCA: AJA Date/TimeTest.9l"Jf%) O S~d
.Perfcread:
Ao = Measured reactivity using the reactivity P.casured Fara:cter c computer (description) Ap r
= Inferred reactivity freta reacter period C ~- IV \ bQ& - hqL : 0 . O '1.5' l .
!!easured Valua 69e Desir,nValbe Nc. ~ t o,0 4 Tcsc . ~~
Kasults' (Actus1' Conditions) 69, -- , w a ,. Ao" - do" ~
< 0.04
Desir.n Value 00 O (Design Conditions) r
~ .; - -
WCAP-7905, Rev.1. Table 3.6 r J 7,c Reference -. E. .y ' TSAR / Tech Spec NA Acceptance Criteris NA _ Reference er W Lee teal % k uak/n
- vr Tke. re.lio.lalig a 6= roe-Nh co
; yo pc.4, Acuphe cibA. W M*. . ,
cc.xnce Evaluated By . . bufuL ab_ _ Completed Uy . _0 0 -
' ' Test !:ngineer 7 Recore.mnded 'For Approv.11 Ity ,, C. 1g M _
l' NFO 1:r.gi neer i g
/
., 's '
) . . ,
4 4-, 4.-,
*-' * * ' ' -. ,..e ee ...4,,,..,c. .,.
'p.,
at .
- l-PT-94 ATTACF_ MENT 6.11 Page 4 of 41 02-11-81 .
ilorth A. ins l'owcr ScacNu Uait 1 Cycle 1 Startup Physics Tests Results and Evalustien Sheet , , I Test Descripcion: Critical Boron Concentration - ARO - Procedure Nudor/Scetion: 1-FT-94/ App. C cquence scep xumber: 7 S ncierence. 40 f.sak Positions (ccce ) RCS Temper:t : (*F): '347 _$ II Powcr Level (:F.P.): 0 Tenc other (specify): SDA: 223 SDD: 228 CA:228 condiciu:us : Below Nuclear Heating (Design) CB: 228 CC: 228 CD:223
' ' RCCA: NA :i
!ank ros.itions (s: cps)~ RCS Temperature (*T): Th4.?*f III Power Level (%r.p.): o"7, !
Test - Other (specify): SDA: 't.O SDB:'J.2 7 CA: h % Conditions (Actual) CB :'1fl.S CD: 2/1I g g gg* Date/Ti=a Tes: s.// 3 /gl . fot/o rerformed: (C3) *M ; Critical Borou Concentratics - ARD Hessured Parscacer MO (description) t IV *
}!aasured V 1ca k Test DesiCn Value 3 l$ 60 [pm (Ac:us! Condi:icns)
.s-'
Results
= 1492 ~+ 50 pra C3 Design value ,
(Design Condi:1cas)
, Yepco NTT Technical Report *!o. 161. Deeceter 1980:
prsada f rom T.5. Race 11a to c.:. sm, deced 46 Referenco Jenuary :0. 1981. ( ao )xC3 < 24,000 pcm i V TSAR / Tech Spec 3C3 Accept:nce ' Criccria . FSAR section 1.5.2.4 ' Reference VI se, 3o = -8.16 pcm/ ppm for prel binary analysis Concents ,
"3
-%.N p/pf:m Usd be f.M wh5 5. Aetyt*-ce.c.Atenind; 3
o...w - a
,.M " Evalut.ted By br,M N.[
comp 1w:cd ty b
/ Tese encineer P
Recor: App wv.31 mended cr For C 1M _ llFO L:gi::ec.: ne e 9 4 e
~.m,ye...._
wf =Ey-' , ww evy w - -4 p- $- p,ignpym ogg%++am-%y-4.--ge ,.#w-mm-p -,.gre.--,.- y,e-q.=pmaeysggw.gy. gen-.y- --*y.eg-gg3---hw-.mymyy-p gi .--+mg---.g sw.p--g (
l.- 9 . * . I-PT-94 ATTACHMENT 6.11.
.a '
PAGE 6 of 4E
- 02-11-81 A.3 '
!! orth A.ma Po.cr Staciosi (fatt ,,,1. Cycre ,1 Startup thysics Testa Itasults and E*[aluation Theat
-I-Test
Description:
Isothermal Teenerature Coefficient - ARO Procedure Nuder /Section: 1.pT-94/ App,p Sc'luence Step Numsce: 3 ) Kcfcrence-Bank Post:fons (:cep )
- RCS Teeper:ture (*T): 547*'3 ~
II Yower :.evel ( F.P.): 0 Test' CA:228 other (cpecify): Conditions. SEA: 228 SDB: 228 C CD:228 Below Nuclear Heating (Desisa) C38 228 g8 Bank Po itions (stops) RCS Tc=pcts:ure (*F) tSTL.b$M.T III'
-- Power Lovel (%T.P.): 07o Tesc - CA 'Li% Other (specify): ,
SDA:11% SDS 11% ' Condicions (Ac:ual) - C3:11% CC:111 RCCA: AJA CD 1'L3 y SM M;,,) Date/ Time Tes y/g giJ3 Perfor=:d ISO Neasured Para.ccer ao
; Isothermal Temperature Coefficient-ARO (descripcion)
(Tf) ARO IV
~
!!casured value (" ) = --4 3(. pcm / F A *J O Tesc DesignValle (,3c.) ISO , _ 3,33 + 3,o '
j/#f" ((_g g yppm) Results (Actual Condi:1:n:) BT ARO * ! Design value (3o) ISO = -3.66 : 3.0 pcm/oF . (Design condistent.) ARO (D/228,1492 ppm, 547.0 F) Vepco 3M Technical Report ?to. 161. Decacher !?tti:
' ' ~ .' !!ctorandum f rom T.S . Rats 11a to c.T. Snow, dated Reference January 20, 1J61.
v rsAa/ Tech spec ($) iso < -2.00 pcm/ F (Doppler ($) - -2.00pcm/*F Acceptance Criteria-able 4. 3-2, Vepco UTE Technical Raper e vI Au.eptece c.c' tera me,t. . n tole.recA,* me,,i" . . cosa:its D
~~
Evaluated By _ >> b Completed By b, [ Test Engineer
- Recoramnded for
.h) f Appwval 1;y - _
HF0 Engineer 6 _ , ,,.,....._r,,... . . . - . . . , . , , . . . . . , , , . , , , , . , . _ . . _ . . . , , ._ , , , , , , . . . . .,,_,_.,.,.,,,-.....,r._?._,,... .~
*
- 1-PT-94
'
- ATIAC1DIENT 6.11
' Page 8 of 4k I 02-11-81
{A A.4
!! orth A.ina Power Station tlnit Cycle 1 Startup Fhysics Tests Kesults and' Evaluatien Sheet Control Sank. 3 llortn haasurement, All Otner i I Test Der:cription: Rods Out ~
l Ecference Proccdurc Nunter/Section: 1-PT-94/ APP.E Sequcnce Step Nuciace: 70 40 Bank Positions (etepc) RCS Tei.eperature (*F): 547 II
-5 Test Powcr I.evel (%F.1'.): 0 SOA: 228 SLD: 228 CA: 22g Other (cpecify):
Conditions. (Design) Cs Moving CC: 228 CD: 228 Below Nuclear Heating RCCA: NA Bank Positions (stops) RCS Temperature ('r): gtN.1*F III Power 1.cvel ( F.P.): 07, Test SDB: 1.tt CA:"1.17 Other (specify): Conditions , SDA: 1.lL% gCW gVgW y (Actus1) CC: n% CD:LL% C3:Mee3 l RCCA: MA ^] Dstc/Tiec Test Perforr.ed: hg qq 1:easured Pers=eter (description) 113 ggg Worth of Centrol Bank 3, All Other
?!casured Value I=
3 }Ql3,3 pc.m Test Results Design Value (Actual Conditien:) 73 . ggll i j] kg I = 1311 131pcm n on itions) S Vepco N7E Technical Report Mo.161, Dece=ber, Reference 19_8_0 If the Des:gn Toleranca is escoeded, the SNs0c : Pall evaluate the L=satt et th te s ro 1: on che utny m17see, td. susoc may spu u, trat . V FSAR/ Tech Spec add:tional sassing be perf ormed. Acceptsncc l Critcria VEP-TED--3 6 A Rcfcrencc VI .ke.LgYec.t C.r'sbik WUL Md. Coments -
.& g Evaluated By _
Completed cy [ Test Engineer Nh Reconemtided For C g. p %) Approval by HF0 nr.gine e r e
# D g
_ m , _ _ , _ _ .
-><o- ww- e. o.. e e
c . 1-PT-94 l I . . ATTACHMENT 6.11 Page 15 of 41 02-11-81 A.5 13 orth A. ins Pv.ce Sention Unit 1 Cyclo 3 - . l Startup Physics Tests rasults and Evaluatien Shoot I Test Deceription: Boron Worth Measure =egt 10 Kcterence Procedurc Nudcr/Succions i.p7 94/gpp, g cwence step uncer: Back Poe.1:icns (: tape) __ RCS Ter pr. ::ure (*7): 347+0
. 3 II Power f.evel ("T.P.) : O Test 220 CA: 228 other (specify):
Conditions SCA: 533: 228 CB Moving CC: 228 CD: 228 3elow Nuclear Heating (Dc 1gn) RCCA: NA i Bank Position: (scops) RCS Te=pera:ure (*F): 5W.1 *f III Power Level (*.F.P.): O lo Tes:. SDA: 2.~47, SDS:'L1Tr CA:'LN Cther (cpecify): , Conditions (Actual) C3:MoVmj '11 CD: 2."17 g g Date/Timo Tese af[dj ;2,qg. Perfor ed: iteasured P.tec=ecer ( lo, ) , Differential Boron Worth (descripcion) SC 3 IV ' ~"~ ' A 8)DM l J
!!aasured V:lue
, Test Design Value
( 12. ) - --%,1 L 0,%pqpp (Actual Condiciens) 3C3 Results ( J2,) = -8.16 1 0.82 pes / ppm
' Design Valu* 3C3 (Desica Con.ii: ions)
Vesco NTE Technical Report No . 161, D ec e=b er , H :-- Referenca yggg Bo < V TSAR / Tech Spec (Qg):cC3 "" 24,000 pcm Acceptance
' # FSAR Section 15.2.4 Reference VI Acc.e.pteet ciW 'cl L.Jeft mLi.
conraants _ Ne - bC.$ yc p Completed Ly . b F. valuated 3y i . u1I .,
! Tcat Engineer Nh Recer.euf ed Tor Appwval Dy b. . _
NFO r..gineer 1
i:
- 1-PT-94
- ATTACHXENT 6.11
- w. Page 5 of 41 02-11-81 A.6 North A.ms Power Statiois !! nit ,,1.,, Cycle 1 .
Startup Physics Tescs Results and E'inlustien Sheet
-I. Test Dcheription: Critical Boron Concentration - Bank 3 IN !
Referencu Procedure h*um!,cr/Section:1-PT-94/ APP.C 8"4"**** "C*P """I'*' H l l'
.. i
-II Bank Positions (scene) RCS Tur perr.curc ('T): 547 ~
' Test Power Level (~F.P.): 0 Conditionn SrAt 228 Sts: 228 CA: 228 other (upecify):
(Design) - cs: 0. CC: 228 CD:228 gCCA: NA Below Nuclear Heatins
~III Bank Positions (steps) RC3 Tc=persture (*F): Ml, 0% l f Test Power Level (:;?.P.):
l' SDB: 2,*2.% CA: "1.'2-t Other (specify): ' l~ Conditiscs . SDA:"L*1% .
;(Actua1) CB: *23 2. 1r ' CD: 2 *2.,) g gg l
Date/Tisa Test 4/*//%l l%40 I'
', Perferned:
Haasured Peraceter M *~
- (descripcion) (C3B TI # ### # #*
- IV Meassured Vr.lue C= GOO,7 ppS 3
r - l . '.
.c
[ .. . Tesc Results Desicn Valu'e (Actual Con:iitions) C"3 GON M.9 bbm 32 itiens) 3 3 ARO b
- Cg ib Vepco rT! Technical P.c;'of t : o. 161, Dece.ber 1?*0;
[ 7 Referenes ' D, ,","# k $gf* * * " I ' ** a ' 1 h !,, V FIAR/ Tech Spec (Ao BCa }
- b I
' E" I l- Acceptance i_ Criteria Reference TSAR Section 15.2.4
= -8.16 pc=/pp:: for preli$1 nary analysis e, e, . dsefC3
-%.54 vsg) &or 9*s\ oN f 56. bc'Lf Y o^% C N'N N] ^1*bb^*$
Completed 1:y Evaluated 3y .+ o . a .- i
/ Test Ingineer . 00 -
- Recom:emted Por Appcoval Dy C- -
NPO cnqincer e 4@ 6 t
l t
- l-PT-94
- ATTACIDDT 6. l'1 s Page 7 of 4E 02-11-81 A.7
!! orth Aana Pruer Otation Unit ,1_, Cycle ,3 __
Sta: tup thy =ics Tests Fesults and Evaluation Sheet I Test De::cription: Isothernal Temperature coefficient';'P :icm;> ct; Sank 3 In Kcierence Procedurc Narber/Section: 1-PT-94/ App . D 5*9"'nc: q -- Eank Positiens (etepe) RCS Tceper::ure (*T): 547 -5 +3 II Test Powcr Level (IF.P.): O Conditions SOA: 228 St3: 228 CA: 228 Other (spc:ify): (Design) CB' o CC: 228 CD: 228 Selow Nuclear Eeating P.CCA: NA
. Bank Poci: ices (steps) RCS Te=perature (*F):5931 iW #.
III. - Tca t '-
? owc: Lcyc1 (*:T . ?. ) : o */,
50A:116 SDS: 22.8 CA: 2.1B other (cpecify): Conditions (Actus1) C3: 'L1 CC: 21g CD: 22 8 13Etow NuC:,gM # EAT /AfG ROCA: pA Date/Tietc Test af/r[ei 23oc, Perfor ed: 1 150 Measured Paraneter ( 3o T ; Isother=al Te=perature Ceefficieny (description) BT 3 3ank 3 In l IV . pcrt
.!!aasured value
( 3e ) ISO 3
~ 7' 9o I
aI Design Value (," ) " -0 4 t3'O Test Results (Ac:usi Cor.di: ions) 3T B ((g. /3 Jt ppd
- i. ' resign V.:1ue ( % $5 - - 6.42 2 3.0 pc:/ ?
(Design condi: ions) BT 3 (3/0,C/220,D/228,1323 pp ., 547.c F) Vepco NT7. Technical Report No. 161. :ecester 191t;
. Memo r andus f r c:s * .S . Ro s al t a t o t.T. S now , dated Reference 2,,,,,7 :n, 1931,
[ ISO V TSAR / Tech Spec ) < -2.00 pe:a/# 7 (Deppler( ) --2.00pc=/ F) Acceptance cri:c ia ' FSAR Table 4.3-2, Vepco NFI Technical 2.apor: Reference No. 161. VI AccGPT*hMCg cRrTEA)h dfW W
"' DECic,fo ToLGA9CE" T167 ,
Completed ty 0AC,#~ r.va2ustedavTh # ei V<.n,#e@ w l [ Tes: Ingi: cur
- Recommen. led For Approval ' Jy C. .
NFO 1:'etree:
'4 .
+ 1-PT-94
- ATTACHMENT 6.11
- Page 9 of 41 02-11-81 A.8 florth A.ina l'over Statioit t' nit _1, Cycle _,
3_, Start.up thysics Tests Eccults and Evalastion Sheet . I Test neucription: Control Bank D Worth Measure =egt Stod Seap Referencu Procedurc Nudcr/Section: 1-pT-94/ App.c Sectuunce up surJacr: 74
.II Bank Positions (etcpc) 'RCS T ernr ure (*F): 54 Test .
Power Level (%F.P.): O Conditions SOA: 2.23 SUB: 228 CA: 228 Other (specify): (Des 1Gn) CB Moving CC - 228 CD: Moving Delow Nuclear Heac k P.CCA: NA
~IIL _ Bank Pocicions (stops) RCS Tc perature ('J'): $~M Y
' Tesc < v Power Level (%7.P.): o e/#
Conditions SDA: 2, M . SDE: & E 8 CA .2 E,8 Ocher (specify): (Actual) C3: Movm3 CC: 3.2,3 CD:)V.awmg , [ ,, .; RCCA: g 84.l6W MMlde Maash:3 Date/ Time Test f/F[Il [ Perferrid: po t.(e Measured Pc ct:ccer
.(descriptica) I DI Intettral U reh of Control Bank D - Red Swap IV 1:casured Value o c.ri&.f. Re.M. A.k.
(Posisene193ssps) f Q g y P e. m
\ D
. Test Desica.Value (C.NdcaQ, b8[CrtMCM Ruutta (Ac:uat C=uittons) In - fo3g r/fgp e, p,,;,;m = j,,3 ,, W ) i I = 1028 154 pc-(Critieni P.ef erence ::ent
-[
Desir.n Value' D (Design Condi: ions) Position = 157 steps)
't J - - c a ,. ,
vepco MTI Technical Report No. 161: vepco Rod set; m~ .'H %f . Topical Report .t?-71t. -36As Me=orandum f rom J. A. Ju p g,g,, ,, to c.T. soev, dat ed 's. comber 4.1980. ( - It in. p sa ret.eanse te .w..e.4. sne sxsce swa:1 eva:ance 2 . tmoset
# D'8 *^*17 *.. . n. smc 3.. n.eur o.s
.. V FSAR/ Tech Spec .44 tes '."1 .. sins " **. s een.4."**1' '. p * **' "7 7 Acceptance C:lteria Referenes E -W.D-36A , YI f f.C.tpbo.%,C,a C.T"[bfJ"t A. OdA4 MS D. Concen:s
.~
Dest Y Wcunc.n- k }.
~~
,{ $:,L Completed Ef O. Evaluated By d. . . kR_~.t.A
/ Test L gineer Recomem.ited For ~ 'y AppNyal tty / _
NTO rnqincer
l ..- .. I a ,
- 1-PT-94
- ATTACHXCIT 6.11 PAGE 10 of 4I 02-11-81 A.9
!! orth A.uyt l'o .ec t Sta tiest t! nit J Cycle a startup thysic: Tests Results and Peninstien thcet .,
I Test Deceriptioo: Control !1ank C Worth !!c:.isure::cgt **"*"C" CCP N"*" :
- Rod Nep 1:cierence Procedurc i;ur.!,cr/Section: 1-pT-94/ APP.C /:5"'
Eack Positions (:tr*p=) RCS Tc:gersture (*F): 547 II Fover Level (%T.P.):0 -5 Tect Other (specify): Condition: SOA: 223 SD3: 22 S CA: 223 (Design) C3: Moving CC. ing CD 228 Below Nuclear F. eating
* " Esnk Posicions (stc:ps) ECS Te=perature (*7): Sff 'F III .
Test Poseer Level (%T.P.): o% Cnditions SDA: 22 8 SDS: 2,Z8 CA: Z28 Other (specify): (Actn!) C3: Madri CC: Modetj CD: 22.8 , Bedow kuc]ew keabln Dutc/T.1::a Test Y/f/f/ / Perfor=:d: o /3g Measured Pere:ecer I C ; Integral Worth of Centrol 3ank C-nod Swap (description) 1' (Crikcal Re-ferenea Bank Measured Value I"C gcm 8os'1%n a
/03 efers)
- (Cr.hc l Reference Bark Test Design Vslue Resul:s (Actus1 Conditions) I C= 850 '+ / 28F fosMoo = /03 48,s)
.m.
Design Value I C=843t125cedCritical Reference Bank Positien =
~
(Design Conditions) 131 steps) Vepco N7E Technical Report No. 161; Vepcs And swap
*cpical Report VIP-F?>-36At W.ecorandum (f on J.R. Ju Refarcnce to c.T. Snow, dated ::. center 4,1980. _
- .t .h Castgu Taleranse is esteeded. the sNsec seali evataasa the tavac s t th test e m is en ,,,,.ac.sy t . ,,,,4, 173... 5. :::::: 3.y ,.etty :::.at V TT.AR/ Tech Spec ,,43,3,,,3 ,,,, ,, 3 Acceptance Criteria l -
Reference lVEP-FF.D-36Ae c'Ce bnc.e C.hbrict W cts rn e . Cone .ts on[y w_w hfh
~
T. valuated 3y t/ sl, fh81[A _ Cer.pleted cy
/ Test Incineer . - .
[
- ucem=cmted for yy Apptw.11 Ly / f( _ . , , , _ _ .
{ NFO tagincar
*
- e* .,, :
. .e.
A.10 llurth A.tna l'v.scr Statlen Unlt i Cyclu 1 .
' ' Startup Thysics Testr. Results snd Evaluation Sheet .
I Test D :.cription: Control Bank N Worth 1:easurement-Rod Sequence nep non;>cr: Suspf [, Procedure Nutr.!,cr/Section: 1-PT-94/ APP.C
. , ' Ecference . .
40 Esnh Positions (etcp )' RCS Tersper:ture (*T): 547 -5 II Power 1.cvel (%F.P.): 0 ( Tyst CA: 1!oving other (specify):
- 50/.: 228 Son: 228 f Canditions CC: 228 CD* 228 .
(Design) CB: Moving Belo,w Nuclear Heating RCCA: N/A RCS Tc=perature (*T): MP *F
~
Bank Positions (steps) Fover I.cyc1 (%T.P.): o3 III , Test CA:6.n other (specify): SDA: 228 SDB: EEB Conditions CC: rr.S CD: ,
C3: M.Ang (Actual) RCCA: .e/A Behu> dc]
9 / Date/ Time Test- NN/ .O~2.9/- . .~~. Perforced: . 1!easured Pere:eter I ; Integral Ucrth of Control Bank'A (description) IV - C G.'t cal Rderenie Bak y 1:capured value I= 77_2. ,, e j3 E'#/ 'S' b *' " 3 " ' .: 97 dp) Test - De it,n Ya'.m A" b 'em / Oo58/o',2 ' Results (Actus1 conditicas) - l . - % , 4 I = 645i97,pem' (Critical Reference Bank , Design ..sive 1 A . Position = 108 steps) (De'siCn conditionr) r
- Vepco ME Technical Report .No.161; Vepco Rod Swap Tepte' 1 Itaport VIMRA Nrch 18,1961; MA; Nasorandum f rom ff.L. C.*. 5.1:h to dated Saow, c.T. Sa:w. datedN morand o
' Reference Nrsh 20. 1981. !! the Design Tolerance is earceced the SN30C sh.all .wslu.te ot the impact .: the cut ruutt en u. ..tny an.irn . The sssoc or spuur TSAR / Tech Spec .u ltson.t se.stna b. perior=,d. , _ V Acceptance . Criteria . VEP-FRIF-36A Reference 'f "' ( ~' Y && neY ' Coon: ts osp . w_ J w/ /D /k Mkb8[ 1:valuateJ By Cocspletea ry ./ Test Engineer /
- l'.ccom scuded for 7 E /SAb .
V' , _ . emw.,1 or
- 1100 Ungineer
. a o . 1-PT-94 ATTACR!ENT 6.11
- Page 12 of 41 02-11-81
^* !! orth A.ina Power Station Unit Cycle ,3_ Startup Thysics, Tests Eacults and Evalustion Shoet I Test Deceription: Shutdown Bank B Unrth }:easurmacut - Rod Swnp - Referencu Procedure mvrter/Section: l-PT-94/ APP.C Sequunce Step hbcr: j7 II Bank Penitions (ctep:) RCS Ter per: cure (*7):547+5 - Tect Power 1.cvei (TT.P.): 0 SLA: 223 SM: Moving CA: 223 Other (specify): Conditions (ocsign) CB: Moving CC: 228 CD: 228 Below Nuclear Heating - P.CCA: J/A Bank Positions (steps) RCS Te=perature (*F): 5# #F III ,- Test Po*>cr Levci (*JF.P.) : o7 CA: 2.26 Other (specify): Conditions SDA: 22.6 SDB: PoV.] -, (Actual) CB: Mgg CC: 22_B CD: 22E3 Oe.le u) Yac.lca.y he 'rt Date/Tiric Test f/6/8/ Perfor:.:d C33i I - Heasured Para:cter I SU3 ; Integral Ucrth of Shutdewn Bank 3 ".od Svap (description) '~* 1V (g,;9g,g gg4ug,,_ $_g 1:2acured v:1ue , c pf f g p, gf;, , fj 9 g,g (Crifical Rehrwe % k. Re s c 1 o dicionJ) SDS" O lFl)'*" Os5 ion " //9.5bf 5) - -L. ~7 m Design value I CDE = 1022 153 pc:1 (Critical P.eference Bank (Design Conditions) Positi:n = 156 stees) . . -.. . a ; ' Vepco NTc Technicat Report No. 16L: '.*epco Rod Swap "^I * " " * * * * " I *#*** ,j" e . Re f erenc*' 'T'P to C.T *". Snow, dated Deember 4.1940. 4 ' I.t the Destsn tolerance is as edad, the $NSCC shall evaluate tne Lzpact
- f * * * * ** * *1t ** th' **'**7 ***17***- 'h* T850C **7 "**d7 **
V FSAR/ Tech Spec .4d1:1.3 1 : '..**t is t 3. p . te r3.d . Acceptance Criteria Reference VIP-FRD-36A VI dec.epbge e,n-fM A A s piu* *c re.te n t s I * ' Des y +o A 'G & ..- [ Test Incineer -
- Recommended For .y Approval ny / _
NTO Enginee r i . . a 4: .. 1-PT-94 ATTACHMENT 6.11 Page 13 of 41 02-11-'81 A.12 North A.ina Po*.sce n$tation Unit 1 Cyclo ,,3, Startup thysics Tests Results and Evalu.atica Shoot , I Test Deccription:3hutdom "ank A Worth Measurement-Rod Swap ' Refccericu Procedure Nunkr/Section:.1-PT-94/A?P. G Scecnce Step Kuuscr: jg> ' Bank Positions (ccepc)' ' RCS Tc: per: cure (*T): 547+0 ~/ , II -- -5 < Tece Fover Level (T.F.P.): O Coaditions stA: Moving 5 0: 228 CA: 228 other (specify): '(Desigu). CB: Moving CC: 228 CD: 228 Below Nuclear Heating ' .' . } ECCA: N/A i I Bank Focicions -(s:c;:s) RCS Tc=persture ('7): 944, */:' ,,J Power Level (IT.P.): og ,' III: .' Tcsc Conditions SDA: Movi% SDB2 2.Z8 ~ . CA: 226 Other (speci'y): ,e (Actua1) CB: ' CC: 7,LS CD: 2.2 $ , W Mevin[ECCA' A//A yj, Qj_ Q.,d . c/ pace / Time rese f/8/8/ /' Perfor==d: N2-/ t # "* * #" ^~ sc: t a SDAII [3("p f TV (Cr,'+rcal l<sterence Samk IMasured V:1ue ., I gg = '/ 2 38 pc.m , gyg.,, , f g fg , ( Gnhcal Kefcrence ca L. Re u s" ..c 1 C . iciens) I SDA - P 5 #" * /76 M4) / -?. 'j'f Design.Value (Critical Ref erence "ank te , 1 .I.UA=-1034 153 pc.m Position = 158 steps) , g "' (Design Conditions) Vepco NF% *echnical Report No. 161; Vepco Red Swap T"b , - ' " "I
- A I "" # *" # '" *A' "
f 5' -Refercnce to c".T. Snow, dated December 4, 1980. /,.> < 't ise oestaa toleranas is auseded, cae sasec or 11..1use ese 5.3 44: Y 'd V . TEAR / Tech Spec '#'"'****'"******#**7 addis tenai t ee tta g be pef f ermed. '"'1 7 ' * "# " **7 '* * #7 * * M Accepcance * **# D 0A Reference _ . Desi n folerarsce wo.S exceeclecf . c.ceft a.nce cro'lere'et w& S m eb . ~ , VI ' .e TLa.-+ ectr re.sul+ isfre a.cc7 Mk @ mea.s - c R. M . <y % +o s .J. Lo-Efo, 1.Ftwo l _ }. '
- Cem,tecca ey nf'sL,d ' r.vniuated ny < f J. /M//c~ -
) / T..e ensuaer ***" U M ' E - 7 f b _ m c.e..= 4,u r, pt .
- 2. NW h he bM.brmm E ',j , l._os's boriI ' 10,19 fI.
b% fo W "Shi'. e n. - OadicC(Ee n. ort- fdo. 8'l-244-( O Mw *y* 9 *4 ,-qwg g-+v h J ar- -g *ewin',g.idg gr g yy-- p y- g 9 w a,g-y++iy gg7-ww gi g r-rgw a A.13 llorth A.tna Ptr, ice Statlen tinit ,_I, Cycle 1 . Startup thysics *:'ests Pasultu and Evalu.2 tion Cheet " Test
Description:
Total Rod Vorth-Rod Susp ' F " I . Procedurc 2:uir!,cr/Section: 1-PT-94/ APP.C 'I"""* *
/9 F.efer ence --
Zach Positions (steps) RCS Tetsper:ture (*F): 547+0 5 II Tover Level (*r."F.P.): 0 . Tcot SDA: Moving SDD: Moving CA: Moving other (specify): Conditions CB: Moving CC: Moving CD: MovinE Below Nuc1 car Heating (Design) - RCCA: NA Bank Positions (steps) RCS Tc:nperature (*F): S M 'r III Power Level (%F.P.): o f-Test CA: otact (spccity): Conditions SDA:Niny SDS: Me.vi CC: M. q CD: Moe Mo*3 , (Actual) CB:Me,v;. choyYeaIin] Bele ' Datc/Tietc Test f/MW Perforr.cd: g26 g2j Measured Para =eter I gg Integral Uorth of All Banks-Rod Swap (description)
. IV MeacGred value I =
f /fef ,.,, o , Test Design Value "i Results .(Actual Conditions) I Total
=
$883 # 23[cm * '
Design Value = 5883 588 pe:3 (De' sign conditions) Total ~. let: Vepco Rod Swap Topical Report ss ,Vepco NFE Technical Kerort No. l
* . TEF-TRf> MA8 N:mrandum f rco M.L.. Smith to C.T. Sa rv, dated tiarch 28,1981; !!c-or ndu a f rom T.S. Kotella en c.7. Snow. datedN-ora ReferencQ Harch 20. 19511 l( the DE&gn Tolerance la cacreced, assure adequate sautdown margsn l cy sessuring the reactivsty worth of control banks O through A (and a so ISAR/TCCh Spec the remainder of the r.,d banas to the N-1 configurst'en.sf required) by the boren dtivateg# addition **ekat ue _ ,.
r
~~*** .
,Y succesolve ved le*ettien veist Acceptance i Criteria .
h P-FRD- M . ..
, Reference rict Ms me{ ,
Cont ts Cfm Cet a whn (,7 Evaluated Dy dM /S M /I . _ Completed by - [ Test Engineer ' 1:c.conciended For
. Apptw.11 1;y ) -
Nr0 1:ngineer
. O . .
g 8 .
- g. * * *
,-- - 4 ,1 ,
j , 1-PT-94 . l
,
- ATTACICtENT 6.11
.- Page 16 of 41 02-11-81 A.14
' I: orth Auns Tower Station ifnit _1, Cycle ,,1_ $c.irrup
- startup Physics Testa Ker.ults and Ev41uction Shcot I
Tese nescriptic.n: :un rt.ur. Par- ARO 2*9""*
- 8";'
n et.rnca} , Proerdure :tumcor/r~ction: 1-PT-21.1'. 2"'"I'" ' 8 43 l
' kank Positions (stepu) itCS Terriersture (8F) ' TYBf i 1 II Test Po.4'r 1.t vcl (T.F.P.) : N1 ca: 228 Oth*r (8 eecif 37 3 Conditlens . g3, -228 .sDs: 228 (ucst:.) cs: '228 CC: 223 cD: 228-RCCA: NA. .Must have 1 38 chimbles l
Bank Povisions (steps) RC5 Ter:peratur.' (OF): 5'L1"l.O F III- / Powe r I.. vel (*.;7.P.): wy'/o Teat - Och u (spczify); Cond!:l' ens' 3DA "12.? SDat t1% CA: 1'1.$ (Actual) C3 : t*2.j ' CC111% CD.'1"LQ _ . . RCca: /J A 4(, 'Tb,f} s - I Data /T1=a Test gfgl 1[q l Perfor ed r.AX. R 3. ,, ASSY. ?WF.. ff, TOT,tLHEAT QUA;;ra.;T
!!EASURYD PA tA r4TYP. F'g*g, 27JC:.7AR l
1
- (descripciun) f. ,
p g7, g- . . .,, } cua:c:= rreca re.C a uT:.. c:er
- e 1
L Ir .i any?P,yt.if g 3
- _ l. LM- ~2. 5'2 4 '
1.0937 l 1 . Wasured value eg,g Pa is'0** Tes't - Design Value -
'I 6 1.%41 6 4.09f. 6 1.02 ;
-._; 4 Results (Actual condit!nxt;- e
** .. ; 10:; for P g10.7
~ r.A f,1.02
([* r Q
; Desitu Valve ! 157. for P i<0.9 NA
;- 'f< '- .(Design Candictor.c' -(F Assy par) I
* ' ' 5;CA.M 9C3 ;
.,; . ! ^ ' gcyg.
WCAP-7905 NCNT
! Reference R2/ .1 get.1;f i ?.
X^ N *- - yA y' TSAR / Tech Spec NA .- Acceptance criteria TS 3.2.J Ts L2.2 TSL1' Koiecence gA i
*0i. sdn+.ime.u' neht,A md,b t +.M ruvIks rJo, bve.o.ccetdled. r SAw.e.:
v1
- c==~"" .rth Anw Powu bwid,a Rapt 2.
n pae ff p oo
/ .st wn..
""Z"rd.O' $ ' C 3,<dv4s Nr 0 r.w,p r. uter a 't
. v.
5 k I
1
. l A.15
. 1
. I llorth lauta Power Stat ion l' ult 1 Cycle 1 Star:np ,
startup rhynten Ter.tu nm:ultn and I;valu,ition she.it
'i Tcat Descriptions :t/p F1.cx ttw Control ganks At The Insertion Limits reference -Psocwdure I;uuber/Section: 1-PT-21.1 ?c#<iuNe#o st@0u5bN:stig A 8. *2.
11 tack Pocitjona (stepn) RCD Tenpernture ("r): T il Tect power Level (*P.P.): 3-5 Conditiona sDc: 228 orber (r.peef fy): SDA: 228 CA: 228 (1981c") Cai 228 Cc: AR - CD . AR FCCA: NA Must have > 38 thimbles III Bank Positlons (stt:rn) RCS Tew.icenture (OF)1 stn.o* F Test Power Level ('J P.P.): w t}*T, Con.tn ions SDn:11t CA 12.? Other (specify);
.(Actual) SDA11)
CB:11%' CC: l'lO CD: '2,. RCCA: Mk 45, TL,'dles Date/Ti.r.c Per forr.ed : Test 9 hl 095[ . .;
~ ItAX. REL.
ltEASURF.D PARM;LTER ASSY. WR. F Ig NUCtrAn F , TOTAL llEAT Qt;ADRA;iT I (description) % Diff. gg , , , p CliANACL FACToit FACTO:t RAT;0 (QPT!O l IV . t1 t Nensured Valuc ' tll.Nh*'l.ll
+}Lll7e* %)g 0Y ).%43 'S'i 14 1.01W dio7,'E., P;2.o.i Test Decitn Value
, licsults (Actual Conditions)
- b bs' M ~/.-1 %4% ~l- 4,100 6l07- ;
f 20% for Pg M.9 Deaf.n f Value i 15% for P g<0.9 NA . NA f.1.02 (Design Conditions) (P - Assy pur) '
. Reference WCAP-7905 N0!!E NONE L'CU-7905 RLV.1 + REV.1
- 1
=
TSA1:/ Tech Spec NA NA
.V NA NA Acceptance Criteria Referenco pA TS 3.2.3 TS 3.2.7 TS 3.2.4 h P.mu s.ts:,A 6Nn% hp rt tJt,. t dt.
i n toivec$.s a J M M ph w u
. Core en Dada i, i -wr,pv Muwt; .
Coa.pleted Ity
/
TcIntEnt,incer . Evalusted By _ Id t . [ Recorsarndod for p Approval liy C- #.WA.) ; HF0 f.ngineer
1-PT-94 ATTAC10EMT 6.11 l PAGE 18 of 41 ) ' l 02-11-81 A.16
' 1:ortti Annia ruwer .ct atten , Unit 1 Cyrf u L sentrup ,
- Cr.sttup Physics Tcut s te".uf ta and !!v.if usttou .% cec Test !)c*.t ription: :t/3 fl.!'". !'.t!'- A C ? :.jer , } I)aCa ."q 1
reference f Fruct dut e 1:au!mr/:;ce.tf un: 1_py,33,7 Sequersce Ottp " inlier:,jg 21 lack Ponitlant (et e; :) ttC:' *i. uprenture ("T) : T ef I l Tcat :'o cr 1.cvel. ( r.r.): s36 4 I CA: 228 0"I'* f (SPIf738 Cunatti""' (pesten) c.\ 228 SDs: 228 e,. C3:228 Ce: 228 "' AR M:.:s: have > 38 thi:tbics - AcCA: , NA III 3sak Position * (steps) 2CS Ter.g.cratur: (07): 554.O Y Test rower 1.evel (':r.I'.): w2,fo,5*7, Cond nion' SDB: *l.2.7 CA 'l.2,& cther (i.pecity): 3 DA: '2.'2.% (AC8"31} ca1M *0: Q CDsGS , RCCA: Q W R,*dk, Datc/ Time Test gfgg gqq Perfcreed: , 2:AX. Ri*.1.. HEA5tlRD PA.V.::LTDt A S.'i*f . 1"..'; . T[#3 , !C:C .rar. T , TOTA:.117.1T Qt:A:n/.. -
. (duerininn) ogf. , ,. .. ..!
. a. u.c im; r'.a x. a'. = t : . - - e_T.
l C:a::.:a. re.=: rAc :: .unoe:r:q
.. Iv n.M4 Ql.o't '2 ,4 'F{ l.0143 e ) . 5'70 P. car,ured Value 3y,4 b Py0.4t
.' tit >*To b 8 2.4 % ),)k
- Test I? ens;n value (Actual Con.if tirn:0 4
,gg g8 g, g dk / l,Q P sults
! 13" for P g:0.9 T,ccica Vclue ! 137. for P <0." 3:A !g f,,1.02 (Design Conditions (y . 333y pyr)
. ?.cfarence VCAP-7905 Nene None #~ Y 3.%Y..
RLY.1 TSAt/ Tech Spec !(A r"AM1.55:(12(1-Fb -
'.I'*"*"*'#^
"2 " ' :'"
.a V
reeeitantc
=0.-ur =], 'i : '
I l Criteria taerence s 2.2.3 Ts 3.2.2 Ts 3.:.'
>:A .
y,
- Das'y Ma<-a vsek 4;, bd kW ve 5 lis o<o qd-1 (<-
. . Cor*.-u t n Qdte.rw *. , ,
$e N$ 0% 00ts.4f &cbEcwC Mtc$tts 0:{mP'i' 00. 9 l ~ 2'((,,
- A ~ n .% , -.. e utv/e n m+4. . i Completed r.y 8 realu.ety,I y , a
) Ic s t T..et. int e t dh
- Reent su . .! -I r..s ,
Arri e.v.it ny _. . M u .. .r. i ni i r I d h 9 .C % bY> b% J s 4 Ace J, A hl ulud wLi<L /7L 'isn ~wk. din- %tM .waLib rak.eL b .&. m 6d ,e AL s- 4.4.z.G.t g"' ti, a,we.2. wu ydl.
1-PT-94 ATTACIL"CT 6. I1 Page 19 of !.L 02-11-81
^'
- north As.n.2 r.~er rear d.on uutt 1 _ Cyr!u .3__. sentrur
' startup Ptayates :wts !!csults and Ev1]ustion thcet
- sst ta,.. rt;.tsoni ::/p rmr. :ur. At P osic:, MI Calib. , i 2ata np 1
refer,nce l " Frucuanc 1:.md~r/r et:un: 1-?T-22.2 sequence scer :: aier:g 11 r:ok tor.itsan: (s i et..:) :::s ;,,i; v ra t ur e c>r) : Tref *1 fe.* C rewur 1.s: vel CY.P.) : , c, g cA: 22g Other (r.rve i f y) : Conditiom 37,3, 773 $3 2;g
'"""' C:8228 CU8 AR C: 223 ,, .,
}t:st have .>. 38 Thi=bles
- 3. k rositions (steps) Rr.5 :enperst ;re (OT): 54 2 (f" III 7est - :' owe r t..svel (!:*.P .): fo p,,
Canditico $7,,y 2 gg $c3: g2g cA: 2g$ Cthc; 6.pc:ify): (Actual) c3: cc: C3: 2m RC A: g , Y//y/g, 4 5 ~ O b.o Datc/:!=e Tesc r rcr!a ed: ,g g 3 _ , g o g, 1:AX. ra. r' :cT3:. ;re..:
. rzu a m r e : :x Am.ra.
r!.i. ::::::Au. un-J u.c. m.. a ,c..;,. -... (Je5::im=) ~ yf. Cacra re.ce: n ,; ..c.; c.u....,t n=: c::a (e.q y zy if.2 7."Sw {.; i.s} rn sur.s v :ue 14.1 OnJ t'oSor
- f. 5 % 2. l(C /. 0 /8t.
T /0 I /*r b C 7 !' s ts t 1e i t ied / T'/. A M 0.7 MA
+.
10: fcr ? 1'J.9 L 34 33 y,1.02 De ics Valve 2 157. !or Pg*0.7 * (DesJgn Conditions; g. 3 ry 3.r) g::::: L'C.'J'* 7 3 0 5 Ecference VCAP-7c05 NCH
. i'E ' .1 Riv.1 _.i 33, h. .:11-, j / :' a ":"" ' ' >
- w ..
r u* v rse. /.us . sg..e n m ~
'i :*.:n s::n r :e.s Acceptsnec x [1-73 Pit'* f .
Criterl.1 m.- . :s 3.:., :s 3.2.: :s 2.: a j co~..u e :. x9t-sUvetL.upeac.awc4a,n % % sbne agu% g.1ye.;9 ts,, s g-zy, h N w a d
- d a -f v I:17 -ete.m,.(s 4 T'Md Cy& ,
eo.v1e t . .: ., O fC.2Tl' >: ..a ... ..., c 1 4?' >d . /ML
/ ,.c r. ,.. /
- t. r ..e .. ?.-l r..e w an.. .. a .:, / AA 12 b F 9 L oc .,J j4, 7,g ,'] >g-'g Aen 4,2,2,7,c] ,,,
a
- w Lx % - a,w & f_c use &,
f';cu%rhJ~fc~ u , w -. a .
<e: p. ik F x1 "F Q q@,
^----~- -*--------------m___. _. ____ _ _
I-PT-94 ATTACF.XENT ' 6.11 Page 19 of 41 02-11-81 1 A.18 {
- North Apu:s T..wer Fratton %:It b Cyr!s b Starrtm ,
- Startup Playaics Tsuts itesults and Cva!ustion Sheet Test ne,.crtrunn: :!/a rr.m: :*.w At P ower. MI calib. , R ::sta ".sp 2
reference
- Pruct:dute !:undwr/L.r.:!wn: 1-?T-22,2 Sequence Step : ui.diert g 11 F4nk Por.ittan: (st et.n) ra:C . tire ra t u r e ("T) : Iref 1 1 Teac re er .evel (nr.1.): s50 cther-(neccuy):
C* *d l L 1"'"' snA 228 sca 228 CA: 228
' ' U"' cot AR C3! 228 CCs ECCA., 2 2 8 XusC have > 3B Thi=' ales NA III Sec.k Positjons (steps) ?.C5 Terpers:ure (oT): 67,2 *F Te1t Tower Level ("T.P.): A f,2 7, .'
condnico $0?.: 2167 CA: ?t$ Cther (a.pecifyJ: 333 7zB (Acttaal) C3 Iz6 CC: 2.Mt CDs ges-A,g, RCCAs
~ d
- g. ate / Time Test fattornedt 77.58 cop 1:AX. RIL. ,,
T'*.3, IrJCL".,V. ct:;.;;r/.. ;
. P.EAS'JRY.D PA3.'."CQt ASSY . 1" 'R. T,*), ;tT.* L : Ti?
(Jescription)
- D f. ."gg, , , . .
TAC 0t; it.A;10 (y!":.; C11:tJ:. . Y.*.CIC:t y gy /ffl.r P =+ s-n l.07
.'.cacured 'Value B,,f [a,-/)6* 3 CAL l* 5 $ <
A*D l* O TioY.lrrf'909 g g g f,op Test Desicn value q 7 P.rsults (Actual Canditteta.' 7e G
+ ICC for P g10.9
! 157. for P g<0.9 x4 3A ,1.02 De.cica Value *
(Design Conditions; (i. 3 sy pr) L g;;,g k'C.W- 7') 0 5 k' CAP-7?C5 NcNC
. Ecfsrer.ce MV.1 gCV.1 W 8 I d2 # **"*
7 4e*"9 h. ,; t 1.P -@ ') 1 *18
- yA y TSA!!/ Tech Spec NA AH
' **
- I' ' ' #I 8 ' *
- Acceptaner x (1-P *P 19*"If t
Cri:cria Ts 3.2,3 is J.2.2 TS J.2.% Esference g3 Con. ut:s
,,- g u ~+
- y w usa +s - p y y%un,. '.
I. h b M 9'i.Ik'tcm- M'd m :,,T k.SI~237. w.s _ Cameleted T.y Ev.atuate.1 siy _ .k 5 t [ Tc a t T igir.ce t a Rec.te . f.- I r.. r Ar,.. ... . i .:, 7M/ hy"d *lc O %y w.dc & T.J1".f"'"7 ;dem lidt (c,-
%y .
L e l ~ c2. aLTdad p44m 4.2.2.2.rQ alad Y- e-<v t & ry ws. ci,+4 c) <& pc#,- Idd 4 tk 22% ddc y 64 <* (Aict &. g e j;,,ig ,, uJ,
~
- e. .
1-PT-94 S ATTACEMDIT 6.11
., Page 20 of 4I 02-1t-81 A.19
' North Annas ruwer Station Unit 1 Cyr.!g 1 starrup ,
- Startup Physics Tuuts Results ant' 'valuacion sheet
- Tent uc,.ertetino:
- t/D rivr. tur. At Fever, NI Calib. , R' DaCa Map
- sequence sere mi.at>cri g reference Proceduse !!amimr/suessoas 1-PT-22.2 fank Ponttiens (seepti) nt:5 T.vyersture ("r): Tref + 1 II Test Power 1.svvl (~r.P.): s60 -
CA: 228 other .(specif y) : Conditio"d snA: 228 son: 228 o . (D"le") C3: 223 CC: 228 C38 AR ' RC A8 NA Must have > 38 thichies l I - Bank Positions (steps) RCS Tenperature (of): y p,g
- f' i
I31 rower t.aval (:r,p.): ^I.O.C. T Tes t . Other (specify): CA: Cundt:1ons 50A n ) sD3 ".1.2.) CD M (Actual) CC:11% C3:'2.2.3 RCCA:A)k N fa b.m 4b l Date/ Time Testtjfjg'h l 0946-Ferformed: .
~
- . uxx. R :.. ' .
r n,. tot.u. m i a us m D PAax c :a Asn. m. 19, wC:. rue. e:..au.:- (aes.ri,uon). gf. o m., m ,, Ts ,,.c m ,m _ _. Cax: u. re.cTC rACT:c. ame am3, I
. t. . - Iv n.cf4PgLu. , ~
- 1. 5~2.2, '1.04o 1.014I
- t'.cssmd Value 11.s To &yPjcNr. -
l Test Design Value .. -
+107
- E.r @2 0.9
- 4 %g MA, M i 1.02.
,b Itesults (Actual comittiensh 8 I y . .. .
t 10 fr .
- P g20.9 1 1.02
~
FA cH ^ Desicn Valve ! 13% for P g*O*9 NA
,<= ~c, (Design Canditier.s (g,L= Anzy pvr)
Y. 1.0' I*UI*~ IE VCA?-7905 _ tec fr- NCNE REY.1 ( ;. . ' Referenen gri.1 p NA . T y11,55sh*.2 T 1 2.1CxX(2)/F f;A y TsAlt/ Tech Spec Acceptance x(t-P*P(SV1) i Criteria TS J.2fJ Ts 3.2.2 Ts 3.2.4 soference yr fc @f Mw w rsck M hd ET 45d' 't" cL d, M _ s.Ls wn w ~n y,c m . m m .'J/e m y
. C.-. . t. , g NL WGLA< A v' bv, A s T QMegki 9 5 C..ri. a r., - OfLEF i:..:. . i :, L 1 6LLJZ -
f itet r.nginert $h
. Rcr..c . ?...! r..r -
- Apri..wil ny C. ' . _
p) nn e i.or . ...... r
- 12 b %y9 L cm 6 at~r h i p 4c A 4.2.z.z .4
- ~h f U- e- A y -s .L+a,J a u g fu sA a Tw% 4A. p 1.<dcri AL A q erep u.
CC " " ' dtNia. m(k .
1-PT-94 ATTACIDtENT 6.11
- Page 21 of 4t 02-11-81 A.20
' tiorth As.na Power station Unit 1 Cycle 1 Senreup ,
- Startup Phyntes Tuuts Resultu and Evaluacion Elicet Test De,.crt,,tran ::/a rtM HAP- At Pover, NI Calib. , 5 Dats Map /
truecause 1:.u.a,ur/suetiu.is 1-PT-22.2 sequence step :su ner: g i reference rJ:3 7.v;'erature ("Y) : T,sul6 Poc.iticus (s:cen) Tref ~+ 1 11 renc re-uc Luvvi (:v.r.): N70 l CA: 223 0*h*'*(P"*8IY)* C8"diti'"" sm: 228 SUS: 228 (D"len) C: 228 CC' 223 C AR - tCC.u NA Must have > 38 thimbles Bardc Positions (steps) ECS Ict.perature (07): St,*s
- F III Teat Tsucr leeci (27". P. ) : N. t*7 CA:11 Oc!scr (a,pecif y):
Conj 111cos s0A:'2.M SD3:1'lt (Actual) CC: 'L1% CD: RO C3:"1,*JJs
% D.
RCCA: AJ/\ e c5 Cate/ Time Test- lg ) lO M Performed:
- IIAX. R L. y 7 Qrg::A:-
.u.1'ASURED ? ARA *'LTif,'t A55Y. WR. .rg. TDDL l' EAT Y.3. !."JC:.r.AP.
' (Jescription) ~3 f.- y7gpy gg g_ gg ; g.,. ,.
Cw:.s re.C=. uC=n una men) ll.N. h"* 1.05 IV
'l 1.503 Ltd I.Old F.casured Value 3 3.g*[,$c fyg t C,tn .
Test Design valuu 4 Nk (JA 61.0"2.
- Itasults (Actual coniH r.icM 1fS7 Or D OA
. . ! 10I for P 2.0.9g 3157, for P g40.? xA }a < 1.02
,. -- peeten valu.
- (Design Conditions: (p ., A.isy pur) 1.'C.*J'-M 0 5 VCAP-7?OS HCN! };(.gg Y Reference A%Y.1 21,Y. 1
, 1s.w 1 _ , s, c , @ ." 4 :"->6 r;g.utm, o A.. ,,s.. 4 . - 29 Cricerla T3 3.2.J M 3.2 2 T3 3 '
- Avfusunc* NA y w n a. s , m -> ,, fm e w ._
Co ~nti f. .d4 6 h %b Od:ctb y 4o. 21-2s7. " m J,,J A 4 e,.,Js 4L,r.'R. ladAy&a;r LA C.. 1, d c., #RLd' ' r..i.. 4 c, o6
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1-PT-94 ATTACHMENT 6.I1
- Page 22 of 41 02-11-81
' north Anna r..wer sentton unts ,1__ Cyclu 3._. scarrur A.21 startup thyntes Tuuss nesults and Cvaluation sheet l
I , Test oc,.criptions :t/a rwn v.\r- At Power, MI Calib. , 5 Data >!ap Pcference Fruccdutu ::undeur/5a:ctf uus 1-PT-22.2 sequence seep :<ui.iiier: g i II tank ronitinus (stett) PJ::: *i.s , ratisce ("r) : Tref ~~+ 1 Tue ro=ur Luvv1 (:r.r.): %80 other (npeelfy): co nditioni,i snA: 228 SDS: 223 CA: 228 CD"1C") C3: 228 CC8 223 cui gg . EC ^8 NA Must have > 38 thir.bles _ III Ban's Fositions (steps) RCS Temperature (SF): N 3 #f Test rouer t : vel (:r.r.): ~ g,q C'aLEl'"' 2.? g 3:33 216 CA: LZ.8 Other (specify):
;st.A: CO3 Z Z.6 CU8 /80 d A* '"'( C33 'l28 RCCA* g Date/i'ime Test Ferformed: /HD - /55'f-N 't..
MEAsURY.D PAR 4*E*DL MTM / . r , T*JCIE\r. T , Tont, Ur.A; g A;mA.:T (Jescription) . g ,y . . .. , , b.7 cr.::.:1.:. ric:ct rActon uno(yet;q -
.n
.. TV //.S Iw(,*[5
/2.4'/[brP = 0.47. /.5 2, a M /. oi#
ressured Value
\ .T.u s tic % Fw f 10.9 Test Results Destcn valua (Actual conditions'. a 6 g g gg
., ! 10 for P 10.9 g Decicn Value !15%forPgo.9 xA ra 1 1!c2 (Desig: Cooditions) (r L= /si:y pur) ,
ec.u -nos mereceu. vCAP-nor xes: x::,.
, a:.v.1 xxv.1 TSA1:/ Tech Spec -NA I N" M $" **
r 3, ; .le xx(:) j ::3 V u c e, t . .,, , + meg Criteria Kufetence g3 :s 3.3.3 TS 3.2.2 Ts L2.4 cu-..u:
#4W% ,w- up a ca+ > ~n
- ( t\] A Arww. Pw STM m (bii:Elem No . El-257 C.,., i, u.a . , MCd~~ r.. . i u.. .... , J. >s'. M'a/4 -
/ 7,.c r e .,.c R.*r,.r*
s.,. . . . . . , m ,
. l.-l 1*. r 7K a Q y*g g
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b a~l- Je+L%kl &%. 4.z. .z.f A%,.J . U\- 41u y as c,Lu ,,.J zh a p Id w % 2d% & t h < f ' 64 & th.A +L. 5 " (;,,-i .s umb). A eqh M% ,3 /
~ n 1-PT-94 ATTACF2ENT 6.11
'. Page 23 of 4I 02-11-81 North Aons Power Station Udt ,1,,,, ,
Cyclu l Startup
- Startup Phynits Tuuts Resulta and Cvaluation shcut r Ten uc,.criptions :t/u errr. .sP- At Potter. NI Calib. , R* Data Map Feference Prucudute !!.mubur/kettuu: 1 p7 22,2 Cquenec Stre haber: O f.1ck Pocitions (stern) r.c3 T.ups.rnture ("r) : T;eg 4 1 -
II Tese Power t.uvel (27.P.) : 40 oct.c r. (neue s ty) : Cona nio"' ser: 228 sDs: 228 CA: 223 (! 'C" ) Cs: 223 CC8 228 C38 AR
"#C^*
NA Must have > 38 thi=bles l l 2.sak Positions (steps) RCS Temperature (OT): 574. 2. F
~ III
- Tes t g reuer Level (:y.p.): g,g 7*
Ctlict (upccify): Condnionc SDA 2.18 SC3: EZ8 CA: 228 U8t"31) C3 gg g CC: 7,gg CD: 2 to RCCA: g Date/ Time Test 4lt6!f/ Y Ferformeda ogly c3fo l'.AX. RCI.. j A$3Y. Pir.L. 7 , inTA[. [tgAT qr:/ggy,.;
. 12*.ASURYD PARN*ETEX Tfyg,!?JCLY.M:
) (description) : Oiff. ..:CllAL1'Y c 118C h0T FLL% bCY CILA:::U. PC' ~ 7:LT g p3 C'dtJ.~.*LI. YACC: yACOn n;10 (y?;;;
- g, .
ty /I.I%%F.= r.or 0 !* !. !* O ! Picasured Valuo /2. 8T h3'.e=s .42 l
+ */of, iw tl t o.9 I'st DestCn Value N d3 M M S L O2-Results (Actuni Coneit tiena n c
- f 10% for P g10.9
\. - ; 15% for P 50.* NA NA 1 1.02 De:1Cn value (p . g gy g ) (Design Conditions.1 5 posg ge;;g k' cal'- 7'30 $ Refereace LtAP-790$ rev.1 u.v. t "y rsav i.e.s : uc u ' r542 "a [1 2'2-'O r ' < :.1Ca(:>/r ** u
} Acceptance x (1 P2P (B'*If ~
l- Criteria T5 3.:.2 Ts 2.2a zwfuence u Ts 3.2.3 l A -W% ML I y
- 0#s n*,4 ktt 6.e c.,sg+ m y T P Co ~o t a LOn%
t.r M A h sh<h owmA,LJ e ad .A,C a-2s eJ_s 7. y g;_, m .u w el r. c [b, tv.i t u.a ...i :y J2 / h //x - Co.pteted r.y _ /' Test T.ngineer /
. Rcr..ew ...' 1 r..r arr, ... . i er 7R ..,o.........<
s V\ O Cf M CQ,. (t G. k & f'3 3p > aMwdLL % y , A w a a .. w a. i 2a 7. & -th. p %d g hLgg . c ro a _g
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e 1-PT-94
+
ATTACWINT 6.11 Page 24 of 41 02-11-81 A.23
- North Anna Power Station Unit b Cye.3u ,3,_,, scarrui,
- Startup Physics Tsuts Resulta and Evaluation Sheet l t ,
Test uencriccian :ua rwr. P.sr- HTP , AkO, Eq . Xe reference Proceduta t:wahurlsuets=2 1_p;_21,1 sequence sce? Nwalier: g l II fank Por.itlens (st epn) ncs * .v.s.esture ("T) : ref I1 Tec rower i.svet C:v.P.): 95 + 5 ~ i l conditicua 33,228 sca: 228 c.u 228 ottier. (::recify): Equilibrium :cenon (pesten) m 228 cc 228 CD2 AK gC::,u hast Have y,38 Thimbles NA III St.nk Positions (steps) RCS Temperature (OT): 67% *f
" Test - Towcr Level (21*.P.): too*7, Can.Irticas CAs ti? Other (2.pecify):
50A:119 sCO 217 (Actual)' C3:2lt.t CO: '1.7.5 CD: 12.9 ggfQ RecA:tJA Date/Tims Test d17bl l'lO3 Performed: PAC. RC..
- REA5'JRrD PARMS.T%R AsSY. M.'A. T , N*JC* L\R F , TOT.S.L *4AT W Qt%g,-l j
(description) ~*!. ,y ,, itA120 (y?T:: CWJ.*#d. FACTon FAC On _ y I' I Iy 31.'57/ for PQ l.04
.Maasured Valua. 0 I'9 N I' IN fl.N be E*5 71 43 2107s Fac P 20.s l.
Test Design Value _ 7* " g', g MA MA i 1.01 Resul:s (Actual Conditim s'4 III s
. + IC: for P 20.9 g Dc:1cn Yalve ! 137. f 0f I g40.9 ,A M NA 1 1.02
_._,_g..
'(Design Conditions; (P An y pvr) b- VCAP- N 5 Rafarence WCAP- m 3 l: arv.1 None None N.1 l -'
!~ . l y rsmarch sr.c n '
'54155"b2'*d r'q 1 2 ic=4:)/7 u Acceptance = [t-it.t r (ac1}
Cticctta TS 3.2 A Kofurcnce y3 T3 3.2. 3 75 3.2.2 n* * %: ~ +=Iom n*+ md, ht M+ tcwk is w'@dle tv Rduwe - ca-a r:' l. boa Am (kw Ssh thA% fk dpIJo, Td-32s he A n e A%w 4. .- C ,.gic ua ny MNFA cus .i a :,y k,3 d),M oo
/ :..t r s .r '
N.;. $ .s' ?, [ $ Y m J 9 e
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1-PT-94
- ATTACErr 6.11
' Page 25 of 4I 02-11-81 A.24 11 orth A.irn l'over Station Unit i Cyclu 3 Startup Physics Tests Pasu.lts a.nd Ivsluatien chect . I Test Des:cription: RCS Flow Measurement Kcterence Procedure Kurier/ Scc:lon:1_PT.27 Sevience Step Sum >ce: g ) I II Dank For.Leions (scepc) RCS T n per:ture (*F): TRef+,1 5, Test Powcr (specify): Level (%F.P.): 93+0 - - SDA: 228 503: 22S CA: 228 other conditions (Design) CB: 228 cc: 228 CD: AR RCCA: l l KCS Temocrature (*F): 57'/ *F j III ' - ' Bank reci:fons (stops) Power Level (*;F.P.): foo g ! Test l Condi:1ons SDA: 218 SDB: 2.2.8 CA: 726 Other (specify): j (Ac:ual) C3: 22.9 CC: 12.8 CD: 2.2.4-KCCA: Date/ Time Te:c f/2F/f/ Perfor=:d: fo f g _ fogg Measured 7:.ra:eter yTOTAL , Total RCS Flow Rate ' (descripcion) RCS IV FT E Heasured Value a 302.,7(4 fx, . Tes: Desica V Jun Not Applicable Kosults (Acta d Condi:icas) NoC Applicable Desigu Value.
" (Design Conditions)
NoC Applicable . Reference - . _ . . . . _
- n uncer a n y)1 , 0 ;pr V FSAR/ Tech Spec
.- Ac:cptance Cricerid Technical Specification 3. 2.5 .
Co m. :. VI Mef ance f Cr;teria HeI.
- i. c.
r 0 N 4 ,__ e e aw f du Geus: Recome.aunted Ter Approv.il Dy -CJ W NFO ;nginner .
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