Text

Cycle 6 Startup Physics Test Rept.
	ML18139B520
Person / Time
Site:	Surry
Issue date:	09/30/1981
From:	Lozito E, Snow C; VIRGINIA POWER (VIRGINIA ELECTRIC & POWER CO.)
To:	;
Shared Package
ML18139B519	List: ML18139B518; ML18139B520;
References
	VEP-FRD-44, NUDOCS 8109150136
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{{#Wiki_filter:' *' . VEP-FRD-44. . ! *vepco SURRY UNIT 1, CYCLE i6 . . . . . ***-*-. '

STARTu*:p .PHYSlCS TES.T REPOR.T . 8109150136 810909 [ PDR AOOCK 05000280 '--p POR __ __j . . * *: F U E L I E S O U *I C E S D :E PA I T I E I T .. . . ' .* . ' *. . . , *.! . . . . . . . . c,** : ~**--* _.: .. ,.v I RC I Ill E LE C T 11 C Po* WE I C O I PI NY . I I

" SURRY UNIT 1, CYCLE 6 *STARTUP PHYSICS TEST REPORT BY vAY H. LEBERSTIEN VEP-FRD-4lJ 1 Reviewed By: ..

C. T. Snow, Nuclear Fuel Engineer Nuclear Fuel Operation Subsection Subsection Nuclear Fuel Operation Subsection Fuel Resources Department Virginia Electric and Power Co. Richmond, Va. September, 1981 / j : ** , '

" CLASSIFICATION/DISCLAIMER The data, techniques, information, and conclusions in this report have been prepared solely for use by the Virginia Electric and Power Company (the Company), and they may not be appropriate for use in situations otlier than those fo:r which they were specifically prepared. The Company therefore makes no claim or warranty whatsoever, express or irnplied,as to thei:r accuracy, usefulness, o:r applicability. In particular, THE COMPANY MAKES NO WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, NOR SHALL ANY WARRANTY BE DEEMED TO ARISE FROM COURSE OF DEALING OR USAGE OF TRADE, with respect to this report or any of the data, techniques, information, or conclusions in it. By making this report available, the Company does not authorize its use by others, and any such use is expressly forbidden except with the prior written ... approval of the Company. Any such written approval shall itself be deemed to inco:rpo:rate the disclaime:rs of liability and disclaimers of warranties provided he:rein. In no event shall the Company be liable, under any legal theo:ry ~hatsoever (whether cont:ract, tort, wa:rzanty, or .strict or absolute liability), f6r any property damage, mental or physical injury o:r death, loss of use of property, or other damage resulting from or arising out of the use, authorized or unauthorized, of this repo:rt or the dat~, techniques, information, or conclusions in it . i

, , ACKNOWLEDGEMENTS Powe:i: The author would like to acknowledge the coope:i:at~on of the Surry Station pe:i:sonnel in pe:i:forming the tests documented in this repo:i:t.

T. Snow, Also, the autho:i: would like to exp:i:ess his g:i:atitude to Mr. C. and D:i:. E. J. Lozito fo:i: their aid and guidance in p:i:epa:i:ing this :i:epo:i:t. ii I I ~I ' ... SECTION 2 3 4 5 6 7 8 APPENDIX TABLE OF CONTENTS TITLE PAGE NO. Classification/Disclaimer.................. i Acknowledgements ........... ,* . . . . . . . . . . . . . . ii List of Tables. . . . . . . . . . . . . . . . . . . . . . . . . . . . . iv List of Figures .......................

. . . . . v Preface. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . vi Introduction and Summary .................. . Control Rod Drop Time Measurements

........ . Reactor Coolant System Flow Measurement ... . *control Rod Bank Worth Measurements ....... . Boron Endpoint and Worth Measurements ..... . Temperature Coefficient Measurements ...... . Power Distribution Measurements ........... . I References ................................ . Startup Physics Test Results and 1 1 0 15 17 22 26 31 43 Evaluation Sheets................ . . . . . . . . . . A. 1 iii LIST OF TABLES TABLE TITLE PAGE HO. I. 1 . 1 Ch:ronology of Tests. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4 11 2. 1 Hot Rod D:rop Time Summa:ry.. .. . .. .... ... . .. . .. ... . .. 12 3. 1 Reacto:r Coolant System Flow Measu:rement Summary.... .16 4. 1 Cont:rol Rod Bank Worth Summa:ry... ...... ... . .. . . . . .. 19 5. 1 Bo:ron Endpoints Summary............................ 24 6. 1 Isothermal Temperature Coefficient Summary......... 28 7. 1 Incore Flux Map Summary............................ 33 7.2 Compa:rison of Measured Power Distribution Pa:ram-eters With Thei:r Technical Specifications Limits... 34 ... :iv FIGURE 1 . 1 1 . 2 1. 3 1. 4 1. 5 2. 1 2. 2 4. 1 4.2 5. 1 *.,; 6. 1 6.2 7. 1 7.2 7.3 7.4 7.5 7.6 7.7 7.8 LIST OF FIGURES TITLE PAGE NO. Co:re Loading Map. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Beginning of Cycle Fuel Assembly Bu:rnups.. .. . ........ .... 6 Inco:re Inst:rumentation Locations......................... 7 Bu:rnable Poison and Sou:rce Assembly Locations............ 8 Cont:rol Rod Locations ..................................

. . 9 Typical Rod D:rop T:race. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13 Rod D:rop Time -Hot Full Flow Conditions

............. ~... 14 Bank B Integ:ral Rod Wo:rth................................. 20 Bank B Diffe:rential Rod Wo:rth........ ........... ... .... .. . 21 Bo:ron Wo:rth Coefficient.................................. 25 Isothe:rmal Tempe:ratu:re Coefficient -HZP, ARO............ 29 Isothe:rmal Tempe:ratu:re Coefficient -HZP, B-Bank In...... 30 Assembly Powe:r Dist:ribution -HZP, ARO................... 35 Assembly Powe:r Dist:ribution -HZP, B-Bank In............. 36 Assemb~y Powe:r Dist:ribution -I/E Assembly Powe:r Dist:ribution -I/E Assembly Powe:r Dist:ribution -I/E Assembly Power Dist:ribution -I/E Assembly Powe:r Dist:ribution -I/E Assembly Powe:r Dist:ribution -HFP, V Cal. Cal. Cal. Cal. Cal. Eq. -Flux Map ........ -Flux Map ........ -Flux Map ........ -Flux Map ........ -Flux Map ........ Xenon ............. 37 38 39 40 41 42 '* '*' PREFACE The purpose of this report is to present the analysis and evaluation of the physics tests which were performed to verify that the Surry 1 , Cycle 6 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. analysis were used. Standard test techniques and methods of data The test data, results and evaluations, together with the detailed startup procedures, are on file at the Surry Power Station. The:refo:re, only a cursory discussion of these items is included in this report. The analyses presented includes a brief summary of each test, a comparision of the test results with design predictions, and an evaluation of the :results. Sheets The Surry 1, Cycle 6 Startup Physics Tests Results and Evaluation have been included as an appendix to provide additional info:rmat~on on the startup test :results. Each data sheet provides the following information:

1) test identification, 2) test conditions (design), criteria, 3) test conditions (actual), q) test results, 5) acceptance 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 p:cio:c to startup physics testing. The entries for the design values were based on the calculations performed by Vepco's Nuclear Fuel Engineering G:coup.1 During the tests, the data sheets were used as guidelines both to verify that the proper test conditions were met and vi to facilitate the preliminary comparison between measu~ed and predicted test results, thus enabling a quick identification of possible problems occuring during the tests .. The AppendiK to this report contains the final completed and approved version of the startup Physics Tests Results and Evaluation Sheets. vii Section 1 INTRODUCTION AND

SUMMARY

On September 14, 1980 Unit No. 1 of the Surry Power Station was shutdown for its fifth refueling. During this shutdown, 76 of the 157 fuel assemblies in the core were replaced with fresh fuel assemblies. The sixth cycle core consists of 8 batches of fuel: four once-burned

batches fr~m Cycle 5 of Unit 1 and Cycles 2 and 3 of Unit 2 (Batches 7A, 7B, S2/4A4, and S2/6B3), respectively, one twice-burned batch that is carried over from Cycles 4 and 5 (Batch 6C2), one thrice-burned batch that is carried over from Cycles 2, 3 and 4 (Batch 4C2), and two fresh batches (Batches 8A and 8B). The core loading pattern and the design parameters
for each batch are shown in Figure 1.1. Fuel assembly burnups are given in Figure 1.2. The incore instrumentation locations are identified in Figure 1.3. Figure 1.4 identifies the location and number of burnable poison rods and source assemblies for Cycle 6; and Figure i.5 identifies the location and number of control rods in the Cycle 6 core. On July 6,* 1981 at 1700, the sixth cycle core achieved initial criti9ality.

performed as tests follows: Following criticality, startup physics tests were outlined in Table 1.1. A summary of the results of these 1.*The drop time of each control rod was confirmed to be within the 1.8 second limit of the Surry Technical Speci:fications.z

2. The reactor coolant system flow rate was confirmed to be 1 greater than the minimum limit specified in the Final Safety Analysis Report 3* 3. Individual control rod bank worths for all control rod banks were measured using the rod swap technique~

and were found to be within 5.5% of the design predictions. The sum of the individual control rod bank worths was measured to be within 1.6% of the design prediction. These results are within the design tolerance of +/-15% for individual bank worths (+/-10% for the rod swap reference bank worth) and the design tolerance of +/-10% for the s~m of the individual control rod bank worths. 4. Criti~al boron concentrations for two control bank configurations were measured to be within 4 ppm of the design predictions. These results were within the design tolerances and also met the accident analysis acceptance criterion.

5. The boron worth coefficient was measured to be within 4.3% of the design prediction, which is within the design tolerance of +/-10% and met the accident analysis criterion.

6. Isothermal temperature coefficients for two control bank corifigurations were measured to be within 1.7 pcm/°F of design predictions.

These results are within the design tolerance of +/-3 pcm/°F and also met the accident analysis acceptance criterion.

7. Core power distributions at HZP indicated measured wise power values to be somewhat larger than the established 2

design tolerance. These higher-than-expected power values were accompanied by a quadrant power tilt ratio CQPTRl which at hot-zero-power, was measured to be approximately 2.8%, but decreased to 1. 1% at full power. Core power distributions for various at-power conditions were generally within 5% of the predicted power distributions. These deviations of power distribution at HZP had no adverse consequences since, for all maps, the hot channel factors were measured to be within the limits of the Technical Specifications. In summary, all startup physics test results were acceptable.

Detailed results, together with specific design tolerances and ,., acceptance criteria for each measurement, are presented in the appropriate sections of this report. 3

.. '* fl Table 1.1 SURRY 1 -BOL CYCLE 6 PHYSICS TESTS CHRONOLOGY OF TESTS Test Date Time Hot Rod Dz:op-Hot Full Flow 7/5/81 0400 Reactivity Computez: Checkout 7/6/81 2257 Boron Endpoint-ARO 7/7/81 0817 Tempez:ature Coefficient-ARO 7/7/81 1402 Flux Map-ARO 7/7/81 1630 Bank B Woz:th 7/7/81 2130 Boz:on Endpoint-B In 7/8/81 0320 Tempez:ature Coefficient-B In 7/8/81 0410 F.lux Map-B In 7/8/81 0735 Bank D Worth -Rod Swap 7/8/81 1025* Bank C Worth -Rod Swap 7/8/81 1104 Bank A Worth -Rod swap 7/8/81 1137 Bank SB Worth -Rod Swap 7/8/81 1241 Bank SA Worth -Rod Swap 7/8/81 1205 Flux Map -NI Calibz:ation 7/8/81 1853* Flux Map -NI Calibration 7/9/81 1525 Flux Map -NI Calibz:ation 7/13/81 2008 Flux Map -NI Calibration 7/14/81 0024 Flux Map -NI Calibration 7/14/81 1 121 Flux Map -HFP, Eq. Xenon 7/21/81 0949 RCS Flow Measurement 8/6/81 1345 4 Reference Power Procedure HSD PT-7 HZP PT28.11CB) HZP PT28.11CC) HZP PT28.11CD) HZP OP-57, PT28.2 HZP PT28.11CE) HZP PT28.11CC) HZP PT28.11CD) HZP OP-57, PT28.2 HZP PT28.11CF) HZP PT28.11CF) HZP PT28.11CF) HZP PT28.11CF) HZP PT28.11CF) 32% OP-57, PT28.2 47% OP-57, PT28.2 57% OP-57, PT28.2 65% OP-57, PT28.2 85% OP-57, PT28.2 100% OP-57, PT28.2 100% ETA-60002 R p N M L K FIGURE 1.1 SURRY UNIT 1 -CYCLE 6 CORE LOADING MAP J H G I 7A 88 7A F E I OA3 ) 1C6 I OA8 I 1 __ 1 __ 1 __ 1 ,-4-C-2-.,...1 _8_8_1 88 I *683 I 88 ,-e-s-~, C2-I D I D29 ) 5C4 I 3CO I Wl4 I OC2 I 3C5 I Dll ) __ 1 __ , __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ I 7A I 88 I 88 I 78 I 78 I 7B I 88 I 88 I 7A I I 1A6 I 1C4 I 4CO I 3A9 I 3A6 I SAl I scs I ocs I 1A7 I C __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ I 7A I 78 I 88 I 78 I 8A I 78 I 8A I 78 I 88 I 7B I 7A I I 2AO I 2A3 I 4C9 I 2A6 I 188 I 4A3 I OB8 I 3A2 I lCS I 4A8 I 1A3 I 8 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ , __ , __ 1 __ 1 __ 1 __ 1 __ I 4C2 I 8B I 88 I 78 I 8A I 7B I 8B I 78 I 8A I 78 I 88 I 88 I 4C2 I I D38 I OC9 I 5C6 I SAO I OBS I 4A6 I 2C9 I 4A7 I 082 I 5A3 I 4C3 I sco I D20 I , __ 1 __ 1 __ 1 __ , __ , __ , __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 ,~ loo 17B IM 17B ,~ In loo 17B IM 17B ,~ ,~ I I 4CS f OC4 I 5A9 f 180 I 2A8 f 1C7 f OA4 I 4C7 f 3A8 I 086 I SA4 f 2C3 f 3C4 f A __ , __ , __ , __ 1 __ 1 __ , __ 1 __ , __ 1 __ , __ 1 __ , __ , __ 1 __ ) 7A I 88 f 7B I 8A f 78 f 88 f 6C2 f 8A I 6C2 I 88 ) 78 I 8A f 7B I 88 I 7A f I lAO I 4C2 I 3AO I 1B4 I SAS I 4C6 I Jl5 I 064 I J09 I 5C2 I 5A6 I 166 I 4A9 I 2C5 I OA2 I * , __ , __ , __ , __ , __ , __ , __ 1 __ , __ 1 __ , __ 1 __ 1 __ 1 __ , __ 1 I 88 I *6B3 I 78 I 76 f 88 I 7A I 8A I *4A4 I 8A I 7A I 88 I 7B I 78 I *6B3 I SB I I 1C9 I Wl8 I 2A7 I 3A5 I 1C2 I 1A4 I 1B5 I S20 I 089 I !Al I 3C8 I 5A7 I 3A4 I W31 I 4Cl I 1 __ 1 __ 1 __ 1_*_1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 -I 7A I 88 I 7B I 8A I 78 I 88 I 6C2 I 8A I 6C2 I 88 I 78 I 8A I 78 I SB I 7A I I OAl I OC6 I 4A5 I 187 I SAS I lCl I J42 I 1B2 I J03 I OC7 I 2A9 I 1B9 I 6AO I 2Cl I OAS I , __ , __ 1 __ , __ 1 __ 1 __ , __ 1 __ , __ 1 __ 1 __ 1 __ 1 __ 1 __ , __ 1 100 ,~ 17B IM 17B ,~ In loo 17B IM 17B loo loo I I 2C6 I 3C7 I 2Al I 2BO I 4A2 I lCS I OA7 I 3C6 I 2A5 I 1Bl I 4A4 I 3Ci I 2C7 I , __ 1 __ , __ 1 __ 1 __ , __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 I 4C2 I 88 I 88 I 7B I 8A I 78 I 88 I 78 I 8A I 7B I 8B I 8B I 4C2 I I D24 I 4C4 I 2CO I 3A3 I 083 I 2A4 I 2C2 I 6A2 I OB1 I 3A7 I SCl I 1C3 I 037 I 1 __ 1 __ 1 __ 1 __ , __ 1 __ 1 __ 1 __ , __ , __ 1 __ 1 __ 1 __ 1 In 17B ,~ 17B IM 17B IM 17B ,~ IIB In I I 1A2 I 6A4 I 3C3 I 6Al I 183 I 6A3 I 087 I 2A2 I lCO I 5A2 I OA9 I , ___ 1 ___ 1 ___ 1 ___ 1 ___ 1 ___ 1 ___ 1 ___ 1 ___ 1 __ 1 ___ 1 ,--f--> BATCH In loo I~ IIB Im Im 100 loo In I I 1A5 f OC3 I 5C3 I 4Al I 3Al I 4AO I 4C8 I 3C9 I OA6 I 1 __ 1 __ 1 __ , __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 I 4C2 I 88 I 88 I *663 I 8B I 88 I 4C2 I I 030 I OCl I OC8 I Wl5 I 3C2 I 2C8 I D23 I 1 ___ , ___ 1 ___ 1 ___ 1 ___ 1_. __ 1 ___ 1 I 7A I 88 I 7A I I 1A9 I 2C4 I 1A8 I I 1--> ASSEMBLY ID 1 __ 1 __ , __ 1 . '---' FUEL ASSEMBLY DESIGN PARAMETERS BATCH 4C2 6C2 7A 7B SA 8B S2/4A4 Initial Enrichment (w/o U235) 3.33 2.90 2.90 3.39 3.22 3.40 2.61 Burnup at BOC-6 (MWD/M'l'U) 25,619 21,534 17,158 15,425 0 0 11,042 Assembly Type 15X15 15Xl5 lSXlS lSXlS 15X15 15X15 15X15 & Number Of Assemblies 8 4 20 44 20 56 1 Fuel Rods per Assembly 204 204 204 204 204 204 204

Transferred from Surry 2. 5 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 S2/6B3 3.20. 10,951 lSXlS 4 204 R p N M L FIGURE 1.2 SURRY UNIT l -CYCLE 6 BEGINNING OF CYCLE FUEL ASSEMBLY BURNUPS K J H G F OA3 1C6 I OA8 I 163121 o I 165381 E ____ ...,.... ____ 1 ___ 1 ____ 1 ____ 1 ________ __ I D29 I 5C4 I 3CO I Wl4 I OC2 I 3C5 I Dll I I 256701 o I o I 109151 o I o I 257011 D ____ 1_* ___ 1 ____ 1 ___ 1 ____ 1 ____ 1 ____ 1 ____ 1 ___ I 1A6 I 1C4 I 4CO I 3A9 I 3A6 I 5Al I 5C5 I ocs I 1A7 I I 174041 o I o I 151911 134921 1s2111 o I o I 174931 C ~1 ____ 1 ____ 1 ____ 1 ____ 1 ___ 1 ____ 1 ____ 1 ___ 1 ___ 1 __ _ I 2AO I 2A3 I 4C9 I 2A6 I 1B8 I 4A3 I OB8 I 3A2 I 1C8 I 4A8 I 1A3 I I 177031 104951 o. I 152981 o I 177521 o I 157291 o I 108441 174461 B-____ 1 ____ , ____ , ___ , ___ , ____ 1 ___ 1 ___ 1 ___ 1 ___ 1 ____ 1 ____ 1 __ __ I D38 I OC9 I 5C6 I SAO I OBS I 4A6 I 2C9 I 4A7 I OB2 I 5A3 I 4C3 I sco I 020 I I 256851 o I o I 134901 o I 173751 o I 173551 o I 134931 o I o I 256021 , ____ , ___ . _, ____ 1 ____ 1 ____ , ____ , ____ 1 ____ 1 ____ 1 ____ 1 ____ , ____ , ____ , I 4C5 I OC4 I 5A9 I 1BO I 2A8 I 1C7 I OA4 I 4C7 I 3A8 I OB6 I 5A4 I 2C3 I 3C4 I I o I o I 154101 o I 174321 o I 11aasl o I 173151 o I 155611 o I o I A ____ , ____ 1 ____ 1_. ___ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ *1 ____ 1 ____ 1 ____ 1 ____ 1 __ __ . I lAO I 4C2 I 3AO I 1B4 I SAS I 4C6 I JlS I OB4 I J09 I SC2 I 5A6 I 1B6 1. 4A9 I 2C5 I OA2 I . I 165041 o I 153261 o I 175441 o I 214041 o I 215531 o *I 173111 o I 152301 o I 166141 , 1 ___ 1 ____ 1 __ , ___ , ____ 1 ____ , ___ , ____ 1 ____ 1 ____ 1 ___ 1 ___ 1 ____ 1 ____ 1 ____ 1 I 1C9 I Wl8 I 2A7 I 3A5 I 1C2 I 1A4 I 1B5 I 520 I 089 I lAl I 3C8 I 5A7 I 3A4 I W31 I 4Cl I *~ I o I 1oaas1 136741 176151 o I 179161 o I 110431 o I 177911 o I 177801 138271 11oosl o I 1 ____ 1 ___ 1 ____ 1 ____ 1 ___ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ___ ._1 ____ 1 ____ 1 I OAl I OC6 I 4A5 I 1B7 I SAS I lCl I J42 I 1B2 I J03 I OC7 I 2A9 I 1B9 I 6AO I 2Cl I OAS I I 167221 o I 153801 o I 174881 o I 216541 o I 215281 o I 174781 o I 156251 o I 165421 1 ____ 1 ____ 1 ____ 1 ____ 1 ___ 1 ____ 1 ___ 1 ___ 1 ____ 1 ____ 1 ____ 1 _____ 1 ____ 1 __ . __ , ____ , I 2C6 I 3C7 I 2Al I 2BO I 4A2 I lCS I OA7 I 3C6 I 2A5 I 1Bl I 4A4 I 3Cl I 2C7 I I o I o I 154001 o I 178711 o I 175691 o I 177151 o I 1s11s1 o I o I 1 ___ 1 ___ 1 _____ 1 ___ 1 ___ 1 ___ 1 ___ 1 ___ 1 ____ , ____ 1 ____ , ___ 1 ____ , I D24 I 4C4 I 2CO I 3A3 I OB3 I 2A4 I 2C2 I 6A2 I 081 I 3A7 I 5Cl I 1C3 I D37 I I 255981 o I o I 142601 1 0 I 112s11 o I 173881 o I 136301 o I o I 256981 1 ____ 1 ____ 1 ___ 1 ____ 1 ___ 1 ____ 1 ___ 1 ___ 1 ___ 1 __ 1 ___ 1 ___ 1 ___ 1 I 1A2 I 6A4 I 3C3 I 6Al I 1B3 I 6A3 I 087 I 2A2 I lCO I SA2 I OA9 I I 174011 105931 o I 154791 o I 176011 o I 152911 o I 109661 173621 1 ___ , ___ 1 ___ 1 ___ 1 ___ 1 ____ 1 ____ 1 ___ 1 ____ , ____ 1 ___ 1 I lAS I OC3 I SC3 I 4Al I 3Al I 4AO I 4C8 I 3C9 I OA6 I I 112201 o I o I 157731 134981 151641 o I o I 173801 1 ____ 1 ___ 1 ___ 1 ____ 1 ____ 1 ___ 1 ___ 1 ____ 1 ____ 1 I D30 I OCl I OC8 I Wl5 I 3C2 I 2C8 I D23 I I 255731 o I o I 110001 o I o I 254271 1 ____ , ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 I 1A9 I 2C4 I 1A8 I I 166871 o I 166711 ,----!-->*ASSEMBLY IO I !--> ASSEMBLY BURNUP I ____ , ___ , ___ , , ___ I 6 l 2 3 4 5 6 7 8 9 10 11 12 14 15 II R p N M L FIGURE 1.3 SURRY UNIT l -CYCLE 6 INCORE INSTRUMENTATION LOCATIONS K J H G F I I I E 0 C B A I l11DITCI l __ ..,..... __ 1 __ 1 __ 1 __ 1 __ ..,..... __ I I I I I I I I TC I I TC I MD I I 2 __ 1 __ 1 __ 1 __ 1 __ 1 ___ 1 __ 1 __ 1 ___ IMO! I I 11101 I I IMDI I TC I I TC I MD I TC I I TC I I TC I 3 ___ 1 ___ 1 ___ 1~_1 __ 1 __ 1 ___ 1 __ 1 __ 1 __ 1 ___ I I I I I I I I I I I I I TC I I .MO I I I MO I I MD I TC I I I 4 ___ 1 ___ 1 __ 1 __ 1 __ 1 __ 1 __ 1 1 __ 1 ___ 1 ___ 1 __ I I I I I I I I . I I I MD I I ND I I I MO I I MD I TC I MD I TC I I TC I 110 I TC I I TC I 5 1 __ 1 ___ 1 __ 1 __ 1 __ 1 __ 1 __ 1_._1 ___ 1 __ 1 __ 1 __ 1 ___ 1 I I I I MD I I I I I I I I I I I I TC I I TC I I I MD I TC I MD I I I I I 6 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 ___ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ I 1* I I I I I I I I I -I I I I -I I TC I TC I MD I I I I MD I I
MD I I TC I HD I I HD I I 7 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ , __ 1 __ 1 __ , ___ 1 __ 1 __ 1 ___ 1 ___ 1 ___ 1 I I INDI IMDI I I I I I I IMDI I I I MD I TC I TC I I TC I TC I I TC I TC I MD I TC I I TC I HD I TC I 8 1 __ 1 __ 1 ___ 1 ___ 1 __ 1 __ 1 __ 1 __ 1 __ 1 ___ 1 ___ 1 __ 1 ___ 1 ___ 1 __ 1 . ., I I I I I I I I I I ND I I I I I I I I I I TC I MD I I I TC I MD I TC I I I I I MD I 9 1 ___ 1 __ 1 __ 1 ___ 1 __ 1 __ 1 __ 1 __ 1 ___ 1 ___ 1 __ 1 ___ 1 ___ 1 ___ 1 __ 1 I I MD I I I I MD I I I . I I I I MD I I I TC I I I I TC I I I I TC I MD I I TC I 10 1 __ 1 ___ 1 __ 1 ___ 1 __ 1 ___ 1 ___ 1 __ 1 ___ 1 __ 1 __ 1 __ 1 ___ 1 I I I I I I I MD I I MD I I I I I I I I TC I MD I TC I I TC I I TC I MD I I I I 11 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 ___ 1 __ 1 __ 1 __ 1 __ 1 ___ 1 __ 1 I I I I I MD I I I I I I HD I I MD I I TC I I TC I I I I TC I MD I TC I 12 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 ___ 1 __ 1 __ 1 __ 1 ___ 1 I I I I I MD I I MD I I I I I I I I TC I I TC I I I 13 1 ___ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 I MD I I I I I I I I TC I I I I MD I I TC I 14 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 'MO -MOVABLE DETECTOR I I I I TC -THERMOCOUPLE I MO I TC I TC I 15 1 __ 1 __ 1 __ 1 7
,.; .* R p N 11 FIGURE 1.4 SURRY UNIT 1 -CYCLE 6 BURNABLE POISON AND SOURCE ASSEMBLY LOCATIONS L K J H G F E I I I ss I I _________

1 ____ 1 ____ 1 ____ 1 ________ _ I PS I I I I I I 12 I I 12 I I I D ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 __ __ I I I I I I I I I I I I a I 16 I I ss I I 16 I a I I C ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 __ __ I I I I I I I I I I I

I I I I 16 I I 16 I I 16 I I 16 I I I B ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 __ __ I I I I I I I I I I I I I I I I 8 I 16 I I 16 I I 20 I I 16 I I 16 I a I I 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 I I I I I I I I I I . I I I I I I 16 I I 16 I I 16 I I 16 I I 16 I I 16 I I A ____ 1 ____ 1 ___ ._1 ____ . 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 __ __ I I I I I I I I I I I I I I I I I I 12 I I 16 I I 16 I I 12 I I 16 I I 16 I I 12 I I 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 I I I I I I I I I I I I .. I I I I I I I I I 20 I I 12 I I 12 I I 20 I I I I I 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1_. ___ 1 ____ 1 ____ 1 I I I I I I I I I I I I I I I I I I 12 I I 16 I I 16 I I 12 I I 16 I I 16 I I 12 I I 1 ___ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ___ 1 ____ 1 ____ 1 ____ 1 ____ 1 __ 1 ____ 1 ____ 1 ____ 1 I I I I I I I I I I I I I I I I 16 I I 16 I I 16 I I 16 I I 16 I I 16 I I 1 ____ 1 ____ 1 ____ 1 ____ 1 ___ 1 ____ 1 ____ 1 ____ 1 ____ 1 ___ 1 ____ 1 ____ 1 ____ 1 I I I I I I I I I I I I I I I I a I 16 I I 16 I I 20 I I 16 I I 16 . I a I I 1 ____ 1 ___ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ___ 1 ____ 1 ____ 1 ____ 1 I I I I I I I I I I I I I I I 16 I I 16 I I 16 I I 16
I I I 1 ___ 1 ____ 1 ____ 1 ___ 1 ____ 1 ___ 1 ____ 1 ____ 1 ___ 1 ____ 1 ___ 1 I I I I I I I I I I I I a I 16 I I ss I I 16 I a I I 1 ____ 1 ____ 1 ___ 1 ____ 1 ____ 1 ____ 1 ____ 1 ____ 1 ___ 1 992 FRESH BURNABLE POISON ROOS SS -SECONDARY SOURCE PS -PRIMARY SOURCE ATTACHED TO 12 BURNABLE POISON ROD CLUSTER I I I I I PS I I I I I I 12 I I 12 I I I 1 ____ 1 ____ 1 ____ 1 ___ 1 ____ 1 ____ 1 ____ 1 I I I I I I I I I ____ I ____ I ____ I 8 l 2 3 4 5 6 7 8 9 10 11 12 13 14 15

.. R 1' N M L FIGURE 1.5 SURRY UNIT l -CYCLE 6 CONTROL ROD LOCATICNS K J H G 180° I F E D C LOOP C I I I I LOOP B OUTLET I __ I_I __ I INLET ~I IAI IDI IAI 1/ _1_1_1_1_1_1_1_1_ N-41 I I I I SA I I SA I I I I N-43 _1_1_1_1_1_1_1_1_1_1_ I I c I I B I I I I B I I c I I B _1_1_1_1_1_1_1_1_1_1_1_1_ I I I sa I I SP I I SP I I SB I I I I 1_1_1_1_1_1_1_1_1_1_1_1_1_1 IAI IBI IDI ICI IDI IBI IAI A LOOP C __ I __ I __ I __ I_I __ I __ I_I __ I __ I __ I __ I __ I __ I__ LOOP B INLET I I I SA I I SP I I SB I I SB I I SP I I SA I I I OUTLET 9~ 1-l-D-l-l-l-lTl-l-l-. -l-c-l-l-l-l-D-l-l /[7o 0 . 1_1_1_1_1_1_1_1_1_1_1_1_1_1_1_1 I I I SA I I SP I I SB I I SB I I SP I I SA I I I 1_1_1_1_1_1_1_1_1_1_1_1_1_1_1_1 IAI IBI IDI ICI !DI IBI IAI 1_1_1_1_1_1_1_1_1_1_,_,_1_1 I I I I SB I I SP I I SP I I SB I I I I 1_1_1_1_1_1_1_1_1_1_1_1_1_1 I I c I I B I I I I B I I c I I 1_1_1_1_1_1_1_1_1_1_1_1 I I I I SA I I SA I I I I N-44 I_I_I_I_I_I_I_I_I_I N-42 I I A I I o I I A I I ,_1_1_,_,_1_1_1 Jr"' I I I I LOOP A I __ I_I __ I LOOP A ABSORBER MATERIAL OUTLET INLET AG-IN-CO 1 0 0 FUNCTION Ulfffffflllflfl CONTROL BANK D CONTROL BANK C CONTROL BANK B CONTROL BANK A SHUTDOWN BANK SB SHUTDO~'N BANK SA SP (SPARE ROD LOCATIONS) NUMBER OF CLUSTERS fllllllllllffllfllllllllllflllllllfl 8 8 8 8 8 8 8 9 1 2 3* 4 5 6 7 8 9 10 11 12 13 14 15 Section 2 CONTROL ROD DROP TIME MEASUREMENTS The drop time of each control rod was measured at cold and at hot RCS conditions in ordex to confirm satisfactory operation and to verify that the ~od drop times were less than the maximum allowed by the Technical Specifications. The hot control rod drop time measurements were run with the RCS at hot, full flow conditions C 597 °F, 2235 psig) and are described below. The rod qrop 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 g~ipper coil voltage, the LVDT (Linear Variable Differential Transformer) primary coil voltage and a 60Hz 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 A 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 10 tube, the velocity slows causing a voltage decrease in the LVDT coil. The LVDT voltage the11 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 summarized in Table 2.1. Technical Specification 3.12.C. 1 specifies a maximum rod drop time from loss of stationary gripper coil voltage to dashpot entry of 1.8 seconds with the RCS at hot, full flow conditions. results met this limit. ll All test Table 2.1 SURRY UNIT 1 -CYCLE 6 BOL PHYSICS TEST HOT ROD DROP TIME

SUMMARY

ROD DROP TIME TO DASHPOT ENTRY SLOWEST ROD FASTEST ROD C-9, 1.42 sec. M-12, 1.24 sec. "ROD DROP TIME TO BOTTOM OF DASHPOT SLOt.?EST ROD FASTEST ROD G-13, 2.16 sec. P-8, 1.76 sec. 12 AVERAGE TIME 1.29 sec. AVERAGE TIME 1.91 sec. ( Figure 2.1 SURRY UNIT 1 -CYCLE 6 BOL PHYSICS TEST TYPICAL ROD DROP TRACE R p N M L FIGURE 2.2 SURRY UNIT l -CYCLE 6 BOL PHYSICS TEST ROD DROP TIME -HOT FULL FLOW CONDITIONS K J H G F E I I I I I -__,,-_1 __ 1 __ 1 __ 1 _ __,,__ I 1. 30 I I 1. 25 I I 1. 28 I I I 1.93 I I 1.81 I I 1.91 I I D __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1_ I I I I l. 28 I I 1. 30 I I I I I I I I 2. 05 I I 1. 90 I I I I C __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ I I 1. 29 I I 1. 25 I I I I 1. 28 I I 1. 29 I I I I 1.82 I I 1. 77 I I I I 1.85 I I l.89 I I B __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ I I I I 1. 28 I I I I I I 1. 32 I I I I I I I I 1. 93 I I I I I I 1. 95 I I I I 1 __ 1 __ 1 __ 1_. _1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 I 1. 30 I I 1. 2s I I 1. 29 I I 1. 28 I I 1. 28 I I 1. 28 I I 1. 33 l I 1. 93 I I 1. 78 I I 1. 86 I I 1. 83 I I 1. 82 I I 1. 83 I I 1. 98 I A __ 1 __ 1_* __ 1 __ , __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ I I I 1. 28 I I I I 1. 30 I I 1. 28 I I I I 1. 28 I I I I I I 1. 95 I I I I 1. 98 I I 1. 95 I I I I 2 .13 I I I 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 I I 1.26 I I I I 1.28 I I I I 1.29 I I I I 1.28 I I I I 1.76 I I I I 1.80 I I I I 1.84 I I I I 1.82 I I. 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 I I I 1. 32 I I I I 1. 30 I I L 32 I I I I 1. 42 I I I I I I 2. os I

I I I 2. 02 I I 1. 90 I I I I 1. 95 I I I 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ *_1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 I 1.30 I I 1.27. I I 1.29 I I 1.25 I I 1.31 I I 1.26 I I 1.32 I I 1.98 I I 1.80 I I 1.82 I I 1.84 I I 1.87 I I 1.83 I I 1.97 I 1 __ , __ 1 __ 1 __ , __ 1 __ 1 __ , __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 I I I I l. 28 I I I I I I 1. 27 I I I I I I
I I 2. oo I I I I I I 2. 07 I I I I , __ 1 __ 1 __ 1 __ 1 __ , __ , __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 __ 1 I I 1. 24 I I 1. 28 I I I I 1. 28 I I 1. 35 I I I I 1.77 I I 1.85 I I I I 1.81. I I .1.87 I I 1 __ , __ 1 __ 1 __ 1 __ 1 __ 1 __ , __ 1 __ , __ 1 __ 1 I I I I l. 32 I I 1. 28 I I I I I I I I l. 92 I I 2 .16 I I I I 1 __ 1 __ 1 __ 1 __ , __ 1 __ 1 __ 1 __ 1 __ 1 I I 1. 32 I I 1. 2s I I 1. 35 I I I I 2
os I I l
79 I I 2
os I I I !--ROD DROP TIME TO 1 __ , __ 1_._1 __ 1 __ 1 __ 1 __ 1 I I DASHPOT ENTRYCSEC.

l I I I I I __ I--ROD DROP TIME TO I I I I BOTTOM OF DASHPOTCSEC.l 1 __ 1 __ 1 __ 1 14 l 2 3 4 s 6 7 8 9 10 11 12 13 14 15 "-Section 3 REACTOR COOLANT SYSTEM FLOW MEASUREMENT The reactor coolant flow rate is measured in order to verify that the minimum flow rate ~equirement is sa~isfied. The RCS flow rate is determined using the calorimetric measurement technique. Precision calorimetric data (i.e., feedwater temperature, feedwater flow, and steam pressure) are obtained in order to accurately determine the secondary-side heat rate._ The primary-side enthalpy rise is determined from the RCS pressure and. the temperature: ii:icrease associated with each RCS loop. The flow for each RCS loop is determined by establishing a primary-side to secondary-sid~ 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. ,I This data was analyzed .using the RXFLows computer code. 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. 15 _j I I I I I I Percent Power

10 0 ?. Table 3.1 SURRY 1 -CYCLE 6 BOL PHYSICS TEST REACTOR COOLANT SYSTEM FLOW MEASUREMENT

SUMMARY

Loop A Loop B I Loop C !Total Flow IFlow Cgpm)IFlow (gpm)IFlow C gpm) I (gpm) I I I I I I I I I 97,526 I 97,502 I 96,710 I 291,738 I I I I Minimum Flowl Limit* Cgpm)I I I 265,500 I I

FSAR Section 4.1.3; Letter from J. H. Ferguson CVepco) to H. R. Denton CNRC) dated April 28, 1981 (Se*rial No. 232); Letter from C. M. Stallings (Vepco) to E. G. Case CNRC) dated November 16, 1977 (Serial No. 516). lb Section 4 CONTROL ROD BANK WORTH MEASUREMENTS Control rod bank worth measurements were obtained for all control and shutdown banks using the rod swap technique.

The first step in the rod swap procedure was to dilute the most reactive control rod bank (hereafter referred to as the reference bank) into the core and measure its reactivity worth using conventional test techniques. The reactivity changes resulting from the reference bank movements. were recorded continuously by the reactivity computer 6 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 stabilized such that the reactor was critical with the reference bank near iull insertion. Initial statepoint data £or the rod swap maneuver were obtained by moving the reference bank to its fully inserted position and recording the co%e reactivity and moderator temperature. At this point, a rod swap maneuver was performed by withdrawing the reference hank while one of the other control rod banks Ci~e., a test bank) was inserted. The core was kept nominally critical throughout this rod swap and the maneuver was continued until the test bank was fully inserted and the reference bank was at the position at which the core was just critical. This measured critical position CMCP) of the reference bank with the test bank fully inserted is the major parameter of interest and was used to determine the integral reactivity worth of the test bank. Statepoint data (core reactivity, moderator temperature, 17 __ j and the differential worth of the reference bank) were recorded with the reference bank at the MCP. The rod swap maneuver was then performed in reverse order such that the reference bank once again was near full insertion and the test bank was once again fully withdrawn from the core. The rod swap process was then repeated for all of the other control rod banks (control and shutdown). 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 (+/-10% for the reference bank and +/-15% for the t~st banks). The sum of the individual rod bank worths was measured to be within 1.6% of the design prediction. This is well within the design tolerance of +/-10% for the sum of the individual control rod bank worths. The integral and differential reactivity worths of the reference bank * (Control Bank B) are shown in Figures 4.1 and 4.2, respectively. The design predictions and the measured data are plotted together in order to illustrate their agreement. In suMrnary, all measured rod worth values were satisfactory. 18 BANK B-Refe1:ence D C A SB SA Total Wo1:th Table 4.1 SURRY UNIT 1 -CYCLE 6 BOL PHYSICS TEST CONTROL ROD BANK WORTH

SUMMARY

MEASURED PREDICTED PERCENT DIFFERENCE WORTH WORTH (PCM) (PCM) (M-P)/P X 100 Bank 1440 1406 + 2 . 4 1234 1226 + 0.7 815 833 -2 . 2 551 546 + 0.9 1013 1005 + 0.8 1137 1078 + 5.5 6190 6094 + 1 . 6 19 '.L u Q_ :c o:::: 0 3:: :....J a: 0:::: 0 w 1-z 0 D "" N 0 D D N 0 0 lD .-D 0 c" .-D '-' co D* '--' "<t" D 0 SURRY UNIT BRNK. B B BRNK I ---,-,_ :.. ... " ""~' ',, I ' " 40 '\ l FJ GURE 4. i l -CYCLE 6 BOL PHYSICS INTEGRAL ROD WORTH WITH ALL OTHER ROOS OUT PREDJCTEO )I( MEASURED I I I I " ' :~ . l ' 'I ' " II'-1, I "' ' ,._ 1, .,. I " II " I .,,,, ' " ...... '" I i.,_ ' l>I ,, ...... " ' I -I ' , ..... .,. TEST ' "' I "' ! 80 12Cl 160 200 BANK POSITION (STEPS) 20 I --.*. -----' I I -' 226 " 0 0 ""d" N 0 0 0 0.... w 1-C!Jo '-.O '.:L' u~ 0.... _J a: -a l-0 z* woo 0::: w LL LLo -a D. ""d" 0 0 I -----------------------*---------------

FlG-URE 4.2 SURRY UNIT 1 -CYCLE 6 BOL PHYSICS TEST BANK B DIFFERENTIAL ROD WORTH I I I ,... .. ,. .. / "' .,, B BANK WITH ALL OTHER RODS OUT PREDICTED llE MEASURED I I ! I ' I I I ! -.ll! It, .. ; !It .. "' ill I .. I' It " .. ... I" r--"' llt " .. """" ... ,, 'f I "' I ,. ... "If l I Ii C r ntJ "' I ' I ii --" -\ / ..... ,... I I 40 80 120 BANK POSITION 21 I ! I I I i I ! ! ' I I -"'ill; ' ;lilj ;II ' ----~---I I 160 (STEPS) I I I I I I I I I I I It "

I, I -;..... I I I : i I ' I I I I ' ! I ,I I\ "" I \ 'l. I \ I I I 200 228 Section 5 BORON ENDPOINT AND WORTH MEASUREMENTS Boron Endpoint With the reactor critical at hot zero power, reactor coolant system boron concentrations were measured at selected rod bank configurations to enable a direct comparison of measured boron endpoints with design predictions.

For each measurement, the RCS conditions were stabilized 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 o£f-nominal core conditions, moderator temperature. i.e., for rod position and 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 values met the accident anal~sis acceptance criterion. results were satisfactory. Boron Worth Coefficient In summary, all The measured boron endpoint values provide stable statepoint data from which the boron worth coefficient was determined. A plot of the boron concentration as a function of integrated reactivity can be constructed by relating each endpoint concentration to the integrated 22 rod 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 -8.78 pcm/ppm. The measured boron worth coefficient is within 4.3% of the predicted value of -8.42 pcm/ppm and is well within the design tolerance of +/-10%. The measurement result also met the accident analysis acceptance criterion. satisfactory. 23 In summary, this result was Cont:rol Table 5.1 SURRY UHIT 1 -CYCLE 6 BOL PHYSICS TEST BORON ENDPOINTS

SUMMARY

Measured P:redicted Rod Endpoint Endpoint Configuration (ppm) (ppm) ARO 1484 1480 B Bank In 1320 1320 :t: I Difference I M-P I (ppm) I I I 4 I I 0 I :t:The predicted endpoint fo:r the B Bank in configuration has been adjusted for the difference between the measured and predi~ted 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. 24 2400 2000 r-.. 1600 "" "' 10 u r,,. v: (L "'I t( .,._., "" >--I-1200 1--i > 1--i I-u 0: w 0:::: 800 400 0 1280 1320 FIGURE 5 .1. SURRY UNIT 1 -CYCLE 6 BOL PHYSICS TEST BORON WORTH COEFFICIENT l!l ENDPOINT MEASUREMENTS = -8. 78 pcm/ppn .--I [".. "'""' "" "" " " "' " "~ "' I~ "" -""rs.. C---"' "--1360 1400 1440 1480 1520 1560 BORON CONCENTRATION (*PPMl 1---1600 Section 6 TEMPERATURE COEFFICIENT MEASUREMENTS The isothermal temperature coefficient measurements. were accomplished by controlling the RCS heat gains/losses with the steam dump valves to the condenser, and/or steam generator blowdown establishing a constant and uniform heatup/cooldown rate, and then monitoring the resulting reactivity changes on the reactivity computer. These measurements were performed at very low power levels in order to minimize 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 pressurizer, the pressurizer 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 t~mperature varied approximately 6°F. Reactivity was determined using the reactivity computer and was plotted against the RCS temperature on an x-y recorder. The temperature coefficient was then determined from the slope of the plotted lines. The x-y recorder plots of reactivity changes versus RCS temperature for 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 26 Appendix, all measured isothermal temperature coefficient values were within the design tolerance of +/-3 pcm/°F and met the accident analysis acceptance satisfactory. criterion.. In summary, 27 all measured results were Table 6.1 SURRY UNIT 1 -CYCLE 6 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COEFFICIENT

SUMMARY

I BANK !ISOTHERMAL TEMPERATURE COEFFICIENT! IPOSITIOH I (PCI1/°F) I I Csteps) ITEMPERATUREI BOROM I __________________ I I RANGE I CONCENTRATION I I COOL I I I DIFFER. I I B I D I C 0 Fl I (PPM) IHEATUPI DOWN IAVER. IPRED. I CI1-P) I I __ I __ I ______ I _______ I ___ I ___ I I I ____ I I I I I I I I I I I 1228 1202 I 543 -549 I 1463 1-2.17 1-2.rn 1-2.321-4.00I +1.68 I I I I I I I I I I I I o 1223 I 543 -549 I 1331 1-5.52 1-5.57 1-5.551-6.361 +0.81 I t __ l __ l ______ l _______ l ___ l ___ l I I ____ I 28 Figu:r:e 6. 1 SURRY UNIT 1 -CYCLE 6 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COEFFICIENT HZP, ARO TEMPERATURE (Op) 29 Figure 6.2 SURRY UNIT 1 -CYCLE 6 BOL PHYSICS TESTS ISOTHERMAL TEMPERATURE COEFFICIENT HZP, B-BANK IM TEMPEPmURE (°F). 10 Section 7 POWER DISTRIBUTION MEASUREMENTS The core power distributions were measured using the incore movable detector flux mapping system. This system consists of five fission detectors which traverse fuel assembly instrumentation thimbles in 50 core locations (see Figure 1.3). For each traverse, the detector output is continuously monitored on a strip chart recorder. The output is also scanned £or 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 program, INCORE7. INCORE couples the measured fluK map data with predetermined analytic power-to-flux ratios in order to determine the power distribution £or the whole core. A list of all the flux maps taken during the test program together with a list of the measured values of the important power distribution parameters is given in Table 7.1. The measured power distribution parameter values are compared with their Technical Specifications limits ' in Table 7.2. Flux Maps 1 and 2 were taken at zero power. These flux maps serve as the base case design checks. Figures 7.1 and 7.2 show the resulting radial power d~stributions associated with these flux maps. These maps indicated the presence of a slight quadrant power tilt (2.8%) and some assemblywise relative power values in excess of the design tolerance, but all measured hot channel £actor values were within the Technical Specifications limits. Flux Maps 3 through 8 were taken over a wide range of power levels and control rod configurations. These flux 31 maps were taken to check 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. The radial power distributions for these maps are given in Figures 7.3 through 7.8. These figures show that the measured relative assembly power values are generally within 5% of the predicted values, and that the quadrant power tilt ratio decreased significantly during power ascension. In conclusion, all power distribution measurement results were considered to be acceptable with respect to the design tolerances, the accident analysis acceptance criteria, and the Technical Specification limits. It is therefore anticipated that the core will continue to operate safely throughout Cycle 6. 32 l,..l l,..l TABLE 7.1 SURRY UNIT 1 -CYCLE6 BOL PHYSICS TESTS INCORE FLUX MAP

SUMMARY

I I I 1 2 I I I I I I I BURNI F-Q(T> HOT F-DHINJ HOT I CORE f(ZJ I 4 I I I I I I UP I IBANK CHANNEL FACTOR CHNL.FACTOR I MAX I 31 QPTR AXIAL I NO.I I MAP IMAPI DATE I MWD/IPWRI D I I IF<XYJI OFF I OF I I DESCRIPTION INO. I I MTU l<Y.JISTEPSI I I AXIAL I I AXIAL I I I SET ITHIMI I I I I I I IASSYIPINIPOINTI F-Q<TJIASSYIPINIF-DH(NJIPOINTI FIZll I MAX ILOCI 00 IBLESI I I_I 1 __ 1_1 __ 1_1_1 __ 1 I_I_I 1 __ , __ , __ 1 __ 1_1 __ 1_1 I I I I I I I I I I I I I I I IARO 11 7-7-81 01 01 201 J12I GHI 22 2.442 J12I GHI 1.584 22 ll.50111.48211.0261 SWI 21.411 40 I I I I I I I I I I I I I I IB AT 21/22 21 7-8-81 01 01 228 H09 HGI 21 2. 776 H091 HGI 1.796 21 ll.43Sll.780ll.028I SWI 21.511 40 I I I I I I I I I I I I I II/E CAL. 31 7-8-81 DI 321 160 Fll HG! 32 2.184 D071 HII 1.473 33 ll.43911.41411.0131 SWI -7.191 41 I I I I I I I I I I I I I II/E CAL. 41 7-9-81 101 471 180 L06 GHI 25 1*.930 J121 GHI 1.451 32 11.29411.37411.0111 swl -1.181 40 I I I I *I I I I I I I I I II/E CAL. SI 7-13-81 301 571 175 Fll HGI 33 1.986 D071 HII 1.451 34 ll.32711.39511.0lOI SWI -7.651 41 I I I I I I I I I I I I I II/E CAL. 61 7-14-81 351 651 200 L06 GHI 23 1.918 0071 HII 1.435 23 ll.28211.38911.0121 SWI 5.901 42 I I I I I I I I I I I I I II/E CAL. 71 7-14-81 401 851 204 Fll HGI 31 1.828 Jl2I GHI 1.421 33 l1.232ll.383ll.012I SWI -1.221 41 I I I I I I I I I I I I I IHFP, EQ.XENON 81 7-21-811 11011001 228 Fll HGI 34 1.810 Flll HGI 1.413 34 ll.22311.37711.0lOI SWI -2.471 42 NOTES: HOT SPOT LOCATIONS ARE SPECIFIED BY GIVING ASSEMBLY LOCATIONS (E.G. H-8 IS THE CENTER-OF-CORE ASSEMBLY!, FOLLOWED BY THE PIN LOCATION lDENOTED BY THE "Y" COORDINATE WITH THE FIFTEEN ROWS OF FUEL RODS LETTERED A THROUGH RAND THE "X" COORDINATE DESIGNATED IN A SIMILAR MANNER). IN THE "Z" DIRECTION THE CORE IS DIVIDED INTO 61 AXIAL POINTS STARTING FROM THE TOP OF THE CORE. 1. F-Q(Tl INCLUDES A TOTAL UNCERTAINTY OF 1.08. 2. F-DHINJ IHCLUDES A MEASUREMENT UNCERTAINTY OF 1.04. 3. F(XYI IS EVALUATED AT THE MIDPLAtlE OF THE CORE. 4. QPTR -QUADRANT POWER TILT RATIO. Table 7.2 SURRY UNIT 1 -CYCLE 6 BOL PHYSICS TESTS COMPARISION OF MEASURED POWER DISTRIBUTION PARAMETERS WITH THEIR TECHNICAL SPECIFICATION LIMITS I F-2(T) HOT I F-DH(N) HOT CHANNEL FACTOR 1 I CHANNEL FACTORZ MAP I HO. MEASI LIMITIMARGIHI MEASI LIMIT I 1'IARGIH I I (%) I I I 0!) I I I l I 3 2. 18 I 4.36 I 49.9 I 1. 471 1. 76 I 16. S 4 1. 9 o I 4.30 I 55.0 I 1.451 1. 71 I 15.2 5 1.991 3.82 I 48. 1 I 1. 45 I 1. 68 I 13.7 6 1.921 3.29 I 41. 6 I 1.441 1 . 6 6 I 13.3 7 1.831 2.56 I 28.5 I 1 . 42 I 1. 60 I 11. 2 8 1 . 81 I 2. 18 I 17.0 I 1 . 4 1 I 1. 55 I 9. 0 I I I I I 1 The technical specification limit for the heat £lux hot channel £actor, F-2CT) is a £unction of core height. The value £or F-2(T) listed above is the maximum value of F-2CT) in the core. The technical specification limit list~d above is evaluated at the plane of maximum F-2CT). The minimum margin values listed above are the minimum percent difference between the measured values of F-2CT) and the technical specifications limit for each map. All measured F-QCT) hot channel factors include 8% total uncertainty. 2 The measured values for the enthalpy rise hot channel £actor, F-dHCH) include 4% measurement uncertainty. 34 'l . R p H Figure 7.1 SURRY UNIT 1 -CYCLE 6 BOL PHYSICS TEST A.SSEMBLYWISE PG-JER DISTRIBUTION HZP, ARO " L K J H G D C II PIICD ICTtD

PREDICTED , 11E~SllllED , PCT DIFHREIIC!, 0,311 0.67 0.311 0,37 0.67 0.37 -0.1 -0.2 -1.11 11£ASVl'ED .PCT DIFPEREHC!, ......................

o.u 0,90 1.oz 1.n 1.oz o.9o o.36 o.36 0.111 1.00 1.01 o.n o.e6 o.34 *O.:S -:S.4, *1,7, *l,1 * *Z,9, *4,11 *lt,11 o.39

o."
1.1"
1.zz
1.zs
1.zz
1.1"
o." o.39
a. 39
o. 91
1. o9
1.111
1. 21
1.11
1. n . o. 90 o. 311 * , -0.11 , -2.11 , *4, 7 , .-3.lt * -J.5 , -3.9 * -4. 7 , *lt,5 ..... , ................................................................

o.39

a.ee 1.1s 1.26
1.z"
1.z"
1.z, 1.211 1.is
a.ea o.39
0,39*. o.~6
1.10
1.zo
1.19
1.n
1.20
1.z1
1.1s
o.e11
o.~o * -o.ti , -z.1. -4,l * -4.t * -4.o. -3,11. -3.4. 1.1 * -0.1 * -0.1. z.ti * ..............................................................................

0,311 , 0,9lt , 1,15 1,ZG 1.24, 1.Z:S, 1,16 , 1.Zl , l,Z4 1.ZII, 1,15 , O." 0,36, 0,39 , 0,91 , 1,lZ , 1.25

1.21 , 1.17 , 1,11 , 1,111 , 1.:Z
1,Z9 , 1,17 , 0,99 , 0,40 , 11,9, *3,1 , -z.z , *2,7, *l,9, *<>,4, *°'1,2 * -4,l , *l.5, 0,7, 1,7, 5,11, 9,7, ******************************************************************************************** , 0,90 , 1,14 1,Z6 1,24 1,19 , 1,17 l,OZ , 1.17 1.19 1.Zlt 1,26 1,1'1 0,90 , , 0,'16 , 1.ZZ , 1.ZII, 1.25 , 1.17, 1.IZ ; 0,911 , 1.U, J,U , 1.23 , l.Z7, 1.111, 0.96 , , 6,9 , 11., , 1,11 , 0.9 , *l.5 , -4.J , -1., , *3,11 , *3,5 , *0.11 , 0.11 , J,11 , 6.5 , ............................................................................................

A , 0,311 , l,OZ , 1,ZZ , 1,Z4 , 1.Z3 , 1,17 , 0.91 , 1.10 , 0.91 , 1,17 , 1,Z3 , l,Z4 , 1,ZZ , 1.0Z , 0,311 ,

0.11
1.olt
1,z9
1.21
1.z4
1.111
o.es
1.01
0.119
1.n
1.:0
1.n
1.23
1.0<1
o.39 * * *0,6
Z,11 , 5,9 , Z, 7 , O,G , 0,11 , -4,l , *2,9 , *Z,J , -J,O , *Z,2 , *0,11 , 0,11 , Z,6 , 2, 7 , ***********************************************************************************************************

0,67 , 1,03 , 1,25 1,24 1*.16 1.oz 1.10 0.911 , 1.10 1,02 , 1.111 l,Z°'I 1,Z5 , 1.0J , 0.67 ,

o.66
1.05
1.21. 1.z11
1.16 1.oz
1.10
0.,1. 1.011 o.99 1.1". 1.u. 1.25 1,05. 0.11 , *0,7, 1,Z, 1,1, 1,7, O,l, 0,6, *0,1, *1,9, *2,6, *Z,9, *t,J, *1,0, -0,6, 1,9. 6,1, ................................................

,;,,, ..................................................... . , 0,311 1,0£ l,ZZ , l,Z4 , l.Z3 1,17 , 0,91 1,10 , 0,91 1,17 1,ZJ l,Z4 1,ZZ 1,0Z , 0,311 o,37 1.02 1.n

1.zs
1.zs 1.111
o.n 1.12
o.eo 1.n 1.:0 1.zz 1.21 , 1.os
0,41 * -o., o *. ,. o.,. o.,. 1.:, o.9. 1., 1,5. -:,.1 -1.2 * -z.11 -1.5. -0.1 J,J. 10., ******************************************************************************************** , 0,90 , 1.14 , l,ZII , l,ZC'i, 1,19, 1,17, 1.oz , 1.17, 1.19, 1.Zil , l.Z6 , l,IC'i , 0,90 ,
o.91
1.16
1.26
1.z<i
1.111
1.19
1.01
1.16
1.111
1.zz
1.Zlt
1.u
o.119 *
1.1. 1.1. o.5. -o.,. -o.s. 1,5
1.s. -o.,. -z.1 * -1.3. -1,3. -1.1. -o.ti. ............................................................................................

0,36 , O." , 1,15 , 1,ZII , 1,29 , l,Zl , 1,16

l,ZJ , l,Z9 , 1,ZII , 1,15 , 0,9'o , 0,3" , 0.3& , 0,99 , 1,17 , 1,Z5 , 1.211 , 1.3Z , 1,19 , 1,25 , 1,Z'o , 1,ZII , 1,15 , 0.93 , 0,35 ,
5,6 ., 5,11 , *Z.O , *Z,5 , 3,5 , 7,0 , 2,6
1,5 , *O,Z , *0,2 , *O,J , *0,9 , *Z,O , .............................................................................. , O,J9
0,1111 , 1,15 , l,Z6 , 1,24 , 1,Z4 , 1,24 , l,ZII
1,15 , 0,1111 , 0,39 * , 0,43 , 0,93 , 1,12 , 1.34 , 1,36 , 1,211
1,Z._ , 1.26 , 1.is , 0.89 , 0,40 , , 9,5 , 4,11. *t,5 , 6,7 , 10,l , 3,7 * *O,J , O,J , 0,4
0,7, 0,11 , STAIIOARD DEVIATION
Z ,311 ................................................................ , 0,59 , 0,94 , 1,14 , l,ZZ , l,ZS , 1,ZZ , 1,14 , 0,94 , 0,39 *
o.43
o.91
1.:9
1.za
1.z~
1.zz
1.is
o.95
o.4o * * . 9,5 , *2,11
lZ,11 , ti.II * *1,0
0,4 , 0,9 , 0.7 , 0,11 * . . . . . . . .. . . . . . . .. . . . . . . . . . . . ... . . . . .. .. . . . .. . . . . . . , 0,36 , 0,90 , 1,0Z
l,OJ
l,OZ , 0,90 , O,Jfl , 0,37 , 0,91 , 1,01 , 1.04 , 1,04 , 0,9Z O,Jfl *
1.J , 1,J , *0,5 , 0,5
Z,7 , 1,0 , o.* . 0.311 , 0,67 , 0,311 , 0.311 , 0.611 , 0.39 , 1,1 , Z,0 ., J,S , AV[IIAG! ,PCT DlfFEREHC!,
Z,6 HAP NO: Sl-6-1 DATE: 7/ 7/81 POWER: ox COHTROL ROD .POSITIONS:

F-QCTJ = 2.442 QPTR: F-DHCN) = 1.584 NW 0.995 I NE 0.986 D BANK AT 201 STEPS ----------1---------- FCZl = 1.501 SW 1. 026 I SE 0.993 FCXYl = 1.482 BURNUP = 0 HWD/HTU A.O = 21.41( X) 35 g t r 1~ fi z'* 3 . {{ 5 6., (<: 71 a~ I /!' ' 10 f t 11 11 ** n 14i, ~c"! 15 j . p H Figure 7.2 SURRY.UNIT 1...; CYCLE 6 'BOL PHYSICS 'IEST ASSEMBLYWISE PCWER DISTRIBUTION HZP, B-BANK IN " l K J H G D C II PREDICTED

0.46 0.114
0,46 PPEDICTED
11EASURED
o.41
o.eo
o . .r,1 *
PCT D1FFEREIIC!. , *5.0 * *5,0 , *4.9
11CASURCD .PCT D1FF[IIEIIC!.

0.35 O.U 1.16

1.26
1.16 0.93
0.35 *
o.35
o.u
1.n. 1.:z. 1.12
o.e6
o.n. , 1.4 , o.o , -2.5 * -z.s , *3.5 , *4.11 , .... 6 , 0.34 0.110 0.99
1.Z6 1.40 1.:6 0.99 0.110 0.34
0.34
0.79
0.97
1.Z6
1.40. 1.23. 0,9ft
0.76
0.33 *
1.0 * -o.3 * -1.9 , o.o * -o.o * -1., . -4.9 * -4,,. ** -..1 . o.34. o.74 0.1111 o.6!1
1.16 1.n. 1.i. o.u 0.1111 o.74 o.34
0.35. 0.74
0.87
0.63
1.12
1.30
1.16
0.66
0.611
0.74
0.35. , 1.:s * *0.5 * *1.6 * -:s.:s , -:S.6 , -z ... , 0.1 , 1.1 , *0,1 * -0.4
1.6
o.:ss 0.110
0.1111 1.011
1.11 , 1.:so
1.:sz
1.,0
1.11 , 1.06 o.ae o.eo o.n *
0.35
0.79. 0.119
1.06
1.10
1.ZZ
1.26
1.ZZ
1.07. 1.07. 0.90
0,113
0.37 *
z.11. -o.9. o.4 * -o.3. -1.5. -5.7. -4.6. -5.e. -3,6
o.5
z.1 * "*". 6.s *
o.n. o.99. o.65 1.11 1.n
1,.r,z 1.n. 1.u
1.1z 1.11
o.65 o.n o.n *
o.95
1.oz
o.66
1.16
1.12
1.1s
1.z4. 1.1s
1.n. 1.09 . 0,66
1,0,
o.99 *
Z,4. z.11
z.1 * <1.1
o.:s, -4.6 * -3.4. -4,6 * -1.1 * -1.1. o.e. 1.11. 6.,.
A 0.46
1.16
1.26
1,16
1.10 , 1,42
1.22
1.52
1.ZZ
1.42
1.30
1.16
1,26
1,16
0.46
0.47 , 1.19 , 1.29
1.19
1.32
1.45
1,111
1.411
1.111
1.35
1.26
1.16
1.27
1.21
0,47
3,1
z.s. Z.4, z.z
2,0
Z.O. *3.3, *Z.7, *Z.9, *4.7, *3,3, *O.Z , 0.7. 4.5. 3.5. o.84
1.26
1 * .r,o
1.n
1.n
1.2,
1.sz
1.40
1.5z
1.29
1.12
1.n
1.40
1.26
o.e<t
i 0.87. 1.29 . 1.41. 1.35 . 1.Jl . 1.30
1.50 . 1.37. 1,46
1.:3 . 1.27. 1.30 . 1.37. 1,Z6
0.88. 3.1
Z.6 , z.z
1.6 * *O,:S
0.9 * *1.1 * *Z,1 , o<\.O , *4,0 * *3.6 , *1. 7 , *Z.Z , 0,3 , lt,2 , 0.46
1.16 , 1.26
1.16
1.30
1,42
1,ZZ , 1.52 , 1.22 , 1.4Z , 1,30 , 1,16 , 1,2' 1.16 , 0.46 , 2 J 0.47
1.Zl
1.lZ
1.%0
1.34
1.45
1.Z6
1.53
1.14
1.lZ
1.ZZ
1.lZ
1.23 , 1.17
0.49
9* J,l
4.6
5.3
3.,.
J,Z
1.9
3.9 *. 0.7 * *l.9 * *6.1 , *!I.II , *:S.S , *2.0
1.0 , 6,J ,
o.n. o.99. o.n 1.11
1.12
1.4Z
1.z9. 1.4z
1.12
1.11
o.65 o.99. o.n.
1.01
1.011
0.61
1.13
1.34 , 1.43
1.30
l.ll
1,211
1.09
0.66
0,98
0,93 *
8.,.
8,Z * -..z
1.8
1.8
o.e . 0.1 * -Z.9 * -1.1 * -1.0
1.11 * -1.0 * -o.o * :
ii:is *:
ii:aii *:
ii:ii; *:
i:a6 *:
i:ii *:
i:iii **:
i:ii':
i:iii *:
i:ii *:
i :;,6 *:*ii:;,;,*:*

ii:aii *:

ii:;s*:
0.11
o.a6
0.,2
1.0,
1.12
1.,2
1.n
1,z9
1.10
1.011
o.,o
a.so
o.34 * . 1,4. 11.3 *. -..4 * *0,5
0.0 * ~*? ;_ 0.9. *0.7 * -1.7
1.4
z.z , O.O. *l,O , .............................................................................................. , 0.34 , O. 711 , 0.88 , 0.65 , l,'16 , 1.33
1.16 , 0.65 , 0.811 , O. 74 , O.Vt , , 0,37, 0,70. 0.86. 0.611
1,19 .* l.JZ, 1.15, 0.65. 0.69, 0.76
0.3S. , 8.3
4.0 , *0.6
1.3 , 1.9 * *0.3 , *1.1 , *O.l
1.Z
Z.5 , Z,6 , * * *****:*ii:;;*:*

ii:aii *:*ii:;;::* i:i,::

i:;ii *:
i:26 *:*ii:;,*:*

,: ,ii*:*

ii:i4 *: * * * * * **

0.11
o.79
1.oz
1,z& : 1.1s
1.u
1.01
0.111
0.1s *
8.J * -o.s
z. 7 * -o.,:. -1.-. * -o.8
1.5
z.11
z., .* * ** ** * * -******** .; **********
- .-.-.;-*.-;*
- ,i ** *** -.; ........................... . , 0.35 , 0.9:S , 1,16 , 1.26 , 1,16 , 0.9J , 0.35 ,
0.1s
0.111
1.14
1.z*
1.16
o.94
0.1s ,
o.*
o.* . *-1.5 * -1.s * -o.o
1.0
1.6
STANDARD DEVIATION
2z.os1
o.46
o.e~
o.*, *
o.*6
o.o*
o.46 *
O,J
O.J , O.J , , AVERAGE , .PCT DIFFEIIEHCE,
z., HAP NO: Sl-6-2 DATE: 7/ 8/81 POWER: or. CONTROL ROD POSITIONS:

F-QCTJ = 2,776 QPTR: D BANK AT 228 STEPS F-DHCNJ = l.796 NW l.003 I NE 0.983 ----------1---------- B BANK AT 21/22 STEPS FCZJ = l.435 SW l.028 I SE 0.986 FCXYJ = l.780 BURNUP = 0 MWD/MTU A.O = 2l.S1Cr.J 36 10 . ' 11 1Z 1J 14 . 15 .. " * " .. Figure 7.:3 SURRY UNIT

1 ...;. CYCLE 6 "BOL PHYSICS TEST ASSEMBLYWISE PCWER"DISTRIBUTION I/E CALIBRATION
...;. FLUX MAP N n L K J* H G , r D PREDICTED
0.311
0.66
0.311
11EASUl!ED
0.15. 0.62. 0.15. C D PREDICTED
PCT DIFFEREIICE.
***" * *6.6 * ***"
11USUPED ,PCT DlfFEREIICE
0.311
0.92 1.01 0.97
1.01
0.92
0.311 *
o.37
0.1111
o.9S
o.n
0.11s. 0.1111. o.n * * -2.2 * *"*1. -s.J. -6.0. -s.J. *"*1 * -z.e. 0,62 . 0.97
1,16 , 1,22 , 1,24
1,22 , 1,16 , 0,97
0."2 *
0.41 , 0.96
1.16
1.17, 1.18. 1.17, 1.11 , 0,94
0.40 * * -1.9 * -0.9
O.J * -4.Z * "",J * *4,Z * -4,0 * *2,9 ** *2,9
0,42 0.91 , 1,16
1.26
1.24
1,24
1.24
1,26 , 1.u.
0,91 , o.u *
0,41
0,90. 1.16 , 1.a , 1.zo
1.ZO. 1,19, l.ZS
1.u. , 0.91
0.42 * * *2,Z * *1,3. *0,3, *1.0. *2.7. *J,Z * *"*1 * *0,6 * *O.J. *0.1
0,4 *
0,311 0.97 1.16
1.27
1,ZZ ** 1,U
1,16
l.:Z
1,ZZ
1.27
1.16
0.97
0.311 * , 0.38
0.94
1,16 , 1.25. 1.Zl , 1.zo
1.14. l.ZO , 1.Zl
1.27. 1.19. 0.9'1. 0.311. * *0,6 * *Z,". *O,J. *l.4. *0,7. *l.7, *1,4, *l,Z, *1,0 , *O.Z
2.4 , 2.1
1.J *
0.'12
1.16 , 1,26
1.22. 1.10 , 1.15. 1.0Z , 1.1!1, 1.10. 1.22
1.26
1.16 , 0.92 *
0,'11 , 1.15
1.:6 , 1,24
1.10
1.14
1.01
1.14
1.09
1.23
1.29
1.19
0.94 * * *0.7 * *0,7
O.Z
1,11 * *0,0 * *1.4 * *l.Z * -1.J * *l,6
0,6 , Z.l
Z.6
Z.J * " , 0.38
1.01
1.zz
1,24
1.22
1,15
0.92
1.12
0.92
1.15
1.22 , 1.24
1.22
1.01 , 0.311 , . , 0,38
1.00
1.Zl
1,24 . 1,24
l.111
0.91
1.11
0.'11 , 1.14
1,23
1.27
1.ZJ
1.03
0.39 * * -o.6 * -0.1. -0.1. o.6. z.1. z.1 * -1.1 * -1.2. -1.J. -1.2. o.6
z.,. 1.5. 2.s. z.1 * **a:"*** a*:;;*** i:z.;* *
i:24*:
i:i, *:
i:at: *i:ii *:
i:oo *:
i:ii * *
i:az *:
i:i, *:
i:z. *:
i:z~ *: * ;:,; *: * ;:,;,; *:
o.66
o.96
1.21
1.24
1.111
1..04
1.14
0,99 .* 1.11
1.01
1.16
1.zs
1.n
o.911
o.67 * * -o.a * -1.0 * -o.6
o.5
1.6
1.s
1.6 * -1." * -1.1 * -1.0
o.z
o.9 * -o.s
o.4
z.o * , 0,38
1,01 l.ZZ
1,2"1 , 1,22
1,15
0.92
1.lZ
0,92 , 1.15 , 1.22 , 1.24
1.22
1.01 0,311 ,
0.311
1.01
1.23
1,25 , 1.24
1.17 , 0,'11
1,14
0.91 , 1.14
l.Zl
1.24
1.22 , 1,02
0.39 * * *0,1 . O.S. 0.9, l,J, 1 .... 1,5. 1,4, 1,1. *0,9, *0.9. *O.J. O,Z. O.Z. l,l
1.7,
0.92
1.16
l,ZI,
1.22
l,10
1.15
l,OZ
1,15
1.10
l.ZZ
1.26
1.16
0.92 *
o.94
1.111
1.21
1.zz
1.11
1.11
1.0"
1.11
1.12
1.2:s
1.21
1.11
o.n *
z.4
2.<,
1.1
o.z
o."
1.9
1.a
1.6
1.0 *. 0.9
1.0
1.0
1.z *
o.Ja
0.97
1.16
1.21
1.22
1.zz
1.16
1.zz
1.zz
1.21
1.16
o.97
o.38 *
0.111
o.911
1.11
1.26
1.:z
1.zs
1.111
1.zs
1.zs
1.28
1.16
o.97
0.111 *
1.6
1.6
o.z * -1.2
o...
z.J
1.9
z.s
2.11
o.4 * -o.s * -0.1
0.11 *
o.4Z
o.91
1.16
1.26
1.z*
1.z"
1.2"
1.26
1.16
o.91
o.*2 *
0,42
0.91
1,1S
1,27
1.26
1.25
l.ZS
1,29
1.17
0.119
0.42 *
o.5 * -o.s * -1.1
1.z
z.2
0.1
1.1
z.z
0.1 * *Z,6
0.1 *
o.42
o.97
1.1,
1.u
1.z*
1.zz
1.16
0.,1
o.u *
o.42
o.95
1.n
1.22
1.21
1.21
1.111
o.97
o.*1 *
0,5 * *l,J
Z.7
O,l * -Z.l * *0.7. z.o
0.1 * -1.1 *
0.31
0,92
1,01
0.97
1.01
0,92
0.38 *
0,39
o.94 ** 1,01
0.96
0.99
0,'12
O.J9 *
J.O
Z.9
O.S * -1.J * *1,5
l,J
Z,4 * , AVER.AGE STAlllARD DEVIATION , 21,325
0.38 , D.66
0.38 * , 0,39. D,67. 0.37.
Z.4
D. 7 * -1.a * .PCT DIFFERENCE.
1., MAP NO: Sl-6-3 DATE: 7/ 8/81 POWER: 32?. CONTROL ROD' POSITIONS:

F-QCTl = 2.184 QPTR: D BANK AT 160 STEPS F-DHCN) = 1.473 NW 0.986 I NE 0.989 ----------1---------- FCZ) = 1.439 SW 1.013 I SE 1.012 FCXYl = 1.414 BURNUP = 0 MW0/11TU A.O = -7.19(?.l 37 J r Zf I "'* s ,: 7 . 1J . 15J I 'I .. i tl R p Figure 7.4 SURRY UNIT 1*~ CYCLE'6 BOL PHYSICS TEST "* PREDICTED 11EASUl!ED " ASSEMBLYWISE'PrnER*DISTRIBUTION I/E CALIBRATICN -FLUX MAP t: K J H G , [ -o "?" D" , PCT DIFFERENCE. 0.39 0.611 , 0.]9 0,311 0.66. 0.38 *].l *],3 , *l, 7 PREDICTED 11EA5l'R[D ,PCT DIFFEREIIC!, ...................... 0,37 0.91 l.OZ l,OJ l,OZ 0.91 0,37 o.39 o.e6 o,QII o.'111 1.ao 0.,1 o.]11 1.z -5.t ..... t .* ,.,5 . -t.z

o." . 1.z 0,41 o.95 1.1"
1.zz 1.u
1.zz 1.14 o.95
o.u o.<o: o.97 1.14. 1.15 1.111. 1.111 1.15 o.n. o.42 2,9 1.5 *O,Z *, *5,J *5,3 , *J.O o., 1,6 , 2,4 ................................................................

0,41 0.90, 1,15 1,25, l,ZJ. l,ZJ, l,ZJ, 1.Z5 1.15 0,90 0.41, o.4Z

o.9o
1.1s
1.z1
1.19
1.111
1.16
1.zz
1.15
o.90
o.tiz , 3,Z , 0,6 , *O,Z , *1,1 , *2,9 * *J,7 , *5,t , *Z,J , *O,l , 0,6 , Z,5 ..............................................................................

0.37, 0."5, 1,15, 1.26 , 1,ZZ , l,ZZ , 1,16 , 1.Z2 , 1.zz , 1,Z6 1,15 0.95 0,37, 0,311, 0,'13, 1.l<t , 1.Z<t, 1.21 , 1,20 , 1,14, 1.1'1, 1.111 , 1.24, 1.15 , 0,911 , 0,39 , 1,2 , *2.3 , *1,0 , *1,6 , *l,O , *l,J , *0,9 , *Z,3 , *1,2 , *Z,O , O,J , 2,6 , ,.,6 , ............................................................................................ 0,91 1.1 .. , 1,2!1 1.ZZ 1,16 , 1,16 , 1.oz 1,16 1,16 1.ZZ 1,25 1,14 0,91 , 0,9Z , 1,16 , 1.24, l,ZZ , l;l!I, 1.15, 1.0Z , 1.1", 1,11 , 1,21 , 1.25 , 1,17, 0,94 ,

1:z
1.2 * -o.z * -o.o * -0.11 * -o., * -o.,. * -1,5 * -1.11 * -1.5
o.,
2.1
1.1 * -I o.39 1.oz 1.zz 1.21 1.zz 1.16 0.9Z 1.1t o.9z 1.16 1.22
1.n 1.zz 1.az 0.19 ! ' 1i t-1 ;, i: ~* ti h 3 < "'.~ f 5~ 6 0.39 1.03 l.n 1.24 l,ZJ 1.17 0.92 l.lZ 0.92 1.14 1.Zl , 1,24 1.22 1,03 0.39 7 , 1.s o.5 0.11 o.6 1.0 1.0 -o., -0.1 -o., -1.1 -0.11
1.z o.6 1.z 1.s
0.611
1.n
1.z5
1.n
1.16
1.02
1.u
1.00
1.12
1.oz
1.16
1.n
1.25
1.01
0.611 * , 0,69 , l,DJ. 1.23. 1,24. 1,111. 1.04. 1.14, 1.00. 1.11
1.01
1.15
1.23
l.Zlt
1.04 , 0,71 * , 1.5. o.o * -1.1
0.1. 1.11. 1.11. 1.1. o.r. -o.*. -o.,. -0.1
0.1 * -0.11. 1.3. 3,'I. **********************************************************************************************************

o.39. 1.02. 1.zz. 1.23. 1.zz. 1.16. o.,z. 1.12. o.9z. 1.16. 1.zz. 1.21. 1.zz. 1.02. o.39. 0.39. 1.03. 1.zz

1.24
l,Z'I
1.111. 0,9ft. 1.12
0.9Z , 1.16
1.:1
1.23, l.Zl , 1.04
0.41 1,5 * *o.6
0.1
1.1
1.11
1.11
1.11
o.5 * -0.1 * -o.5 * -o.J * -o.3 * -o.z
z.z
5.1 , ********************************************************************************************
o.91
1.14
1.z5 1.zz 1.16
1.16
1.oz
1.16 1.u 1.zz 1.25 1.14
o.n *
o.93
1.16
1.26
1.21 1.16
1.11
1.n
1.11,
1.1,
1.zz
1.zs
1.15
o.n * , 1,7 , 1,7 , 0.11
O.Z
O.:S , o ... , 0.5
0.0 , *l,l * *0.6
O.l , 0.7
1.5 , ........................
.................................................................... .
o.37
o.9!1
1.15
1.26
1.zz
1.zz
1.16
1.zz
1.zz
1.26
1.l!J
o.9!1
o.37 *
0.39
0,911
1,16
1,24
1.22
l.Zlt
1.16
l,ZZ , 1.zo
1.25
1.15
0.97
0,311 , * :s.1 ; 3.1
1.1 * -1.6
0:1
1.s
0.1 .* o.s * -1.1 * -1.z
o.6
1.1
2.1 * .. . . . . . . *.-.................................................................................. . * ,r o.41
0.90
1.15
1.25 .* 1.n
1.n
1.21
1.25
1.15
o.9o
0 ... 1 * .* :o.43. 0.91
1.n .1.z&. 1.zs. 1.z:s. 1.z:s. 1.25. r.1s. o.90
0,4Z * }~* 4,5 , Z,1 * *1,6 , 0,9 , 1.11 , *0,1 * *O.Z
0.6
o.z
1,1 , l,Z , STAll!IARD DEVIAT10H

=l.3119 **************************************************************** , 0,,.1

0.9!1 , 1,1,.
l,t2
1.25 , l,ZZ , 1.1* , 0.95
0.41 , O,lt3
0.94
1,17 , l,Zl , l,Zl
l,Zl
1.16
0.97
0."2 , 4.5 * *1,6
Z,5 , *O ... , *Z, 7 , *0.11 , 1.11 , 1,6 , Z,O * ..................................................

o.l7

o.91
1.oz
1.01
1.02
o.91
0.11 *
o.40
o.96 , 1.o<o
1.oz
1.01
0.,2
o.311 *
5.11
5.7
z.o * -o.6 * -1.0
a.s
z.a
0,39
0.611 , 0,39 , o.u
0.10
0.311 *
5,5
z.11 * -1.1 *

SUMMARY

, AVERAGE ,

PCT DIFFEREHCE.
1,6 MAP NO: Sl-6-4 CONTROL ROD POSITIONS:

DATE: 7/ 9/81 F-QCT> = 1.930 F-DH!Nl = l.451 FCZl = l.294 POWER: 4TI. QPTR: D BANK AT 180 STEPS NW 0.994 I NE 0.994 ----------1---------- sw 1.011 I SE l.001 FCXYl = l. 374 BURNUP = 10 HWD/MTU A.O = -l.18Ci0 38 [i e( ,t 10, ! 11 'i lZ 13 H 15 ~. R p N Figure 7.5 SURRY UNIT *1 """ CYCLE 6 BOL PHYSICS TEST ASSEMBLYWISE'PCWER.'DISTRIBUTION I/E CALIBRATION -FLUX MAP " L I( J H G p t: II C II PPED!CTED , l'!!EDICTED , HEASURED .PCT DIFFEREIICE, 0.40 0.70 0.40 0,37 0.65 0,37 -7.11 -11.1 -7.11 HUS\/RED ,PCT DHFEREIIC!. ...................... 0.39 0,9] l.Ol 1.02 1,0l 0.91 0.39 O.J9 0,07 0.96 0.9S 0,96 0,117 0,35 0,7 -6,0 , -6.11 , -7.4, -6.11, *6,0 -z.o 0.43 0,96 1.14 , 1.ZZ 1.ZS 1,Z2 l,14 0.96 O.U 0,"3 0.97 1,15 , 1,14 1.17 1.14 1,07 0.94

0.4Z 0.6 0.5 0.4 *. -6.0 -6.0 *6.0 -6.0 -z.o -z.o ................................................................

0.4] 0,91 1.14 l.Z4 1,2: l.ZZ l.ZZ 1.Z4 1.14 0,91 0,4l o.43. o.91

1.14
1.n
1.111. 1.111. 1.14
1.a
1.u
o.n
0,41 0,6 , -0.4 , *0,0 * -0.11 , -Z,6 , -J,11 * *6,0 , -2.1 , -1.0 , -0.7 , 0.0 ..............................................................................

0,39 0.% 1.14 l.ZS l,ZO l.ZO 1,14 1.ZO l,ZO l,ZS l,lc; 0.96 0.31 0,39 0.91 1.14 1.23 1.ZO 1.20 1,13 1,20 1.19 1.23 1,16 0,97 0,39 -1.0 * -1.: . -0.1 * -1.1. -o.z . -o.c;. -o.s. 0.2 * -o.6 * -1.1

1.1
1.0
o.c; 0,93 1.14 1.Z4 1.20 1,12 1.15 1.03 1.15 1.lZ 1.:0 1.24 1,14 0,93 0,92 1.13 1.25 l.Z3 1.13 l,lc;
1.0Z 1,15 1.12 1.Zl 1.26 1,16 0,94 -1.0 -1,0 0.6 Z,9 0.9 -0.5 *0.6 0.0 O.Z 0.7 1.5 1.6 1.0 A ..........................................................................................................
0.40 , 1.01 , 1,Z2 , 1.22 , l.ZO , 1.15 , 0,93 , 1.13 , 0.93 , 1.15 , 1.ZO , 1.Z2 , l,ZZ 1.0l , 0,40 , 0.1;0
1.01
1.:0
1.:2
1.zs
1.19
o.Ql
1.11
o.9J
1.15
1.22
1.:5
1.22
1.04
0,40 * * -1.1 * -1.4 * -1.z
0.1. 3.6
1.1 * -o.6 * -o.4 * -0.1
o.o
1.1
1.1
o.6
0.11. o.o * ..........................................................................................................
0.70 , 1,0:! , 1,25 1.22 1,14 , 1.03 , 1.13 , 1.0:S 1.13 I.OJ , 1.14 l.ZZ 1,25 1,02 0.70 ' , 0.70 , 1.00 , 1.:2 , 1.:3 , 1,17, 1,05 , 1,17. 1.0:S, 1.13 , 1.02 , 1,15 , 1.:1. l.ZJ, 1.00 , 0.70 , , -1,3, -z.o , -Z.5, O.Z , 2.9, Z.4
3,l, -0.l , 0,2 , *0,2 , 1.J , 0.9, -1.Z , -2.1 , -0.l * ......................................................................................................... . 11 0,40 1,03 l.:z l.Z2 l.ZO 1,15 0,9J 1.13 0.9J 1.15 l.ZO 1,22 1.22 1.01 0,40 0.40 1.02 l.U 1.Z3 1.22 1.17 0.'14 1,16 0,?4 1,16 l.U l.Z2 1,20 l.OZ 0,41 * -1.1 -o.,s -0.1 o,9 1.J 1.9 o.9 z.1 0.11 1.1 o.9 -0.1 -1.0 -a.a 1.0 0.93 1,14 l.Z'* l.ZO 1.12 1.15 l,Ol 1.15 1.12 l.ZO 1.24 1,14 0,93 0.95 1.17 l,ZS 1.ZO 1,12 1,111 1,05 1,17 1.14 l.Zl 1.25 1.14 0,92
2,1 Z,l 1,0 0,3 0.4 2,6 . 2,6 Z,S 1,8 1,3 0.9 -0,1 -0.9 ********************************************************************************************

0.39 , 0.96 , 1,14

l.ZS , 1.20 1.20 , 1.14
1.:0 , 1.20 1.25 1,14 0.96 0,39
0.19
o,97
1.1s
1.:5
1.:1
1.n
1.11
1.:4
1.:1
1.z5
1.14
o.96
o.J9
0.1. 0.1.
0.2 * -o.4
o.6
z.4. Z,6
1.0
z.11. o.z * -0.1 * -0.1. -0.11 * . .. .. .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .. . . . . .. . . . .. . .. . .. . . . . . . . . . . . . . . . . . . . . . . . . 0,41 , 0,91
1.14 , l,Z4
1,22 , 1,22 , l.ZZ
l.Z4 , 1,14 , 0,91 0.4:S 0,U
0,91 , l,H , l,ZS
l,Z4 , l.ZJ , 1.2]
l,Z7
1,.15 , 0,91
0.4] , -0,11, -0.7, -0,5
1,1 , 1.6. O.Z , l,Z , Z,4 , 0.8. -1.0 , -0.:S. ................................................................

o.43. o.96

1.14
1.zz
1.25. 1.zz
1.14. o.%
o.41 o.42
o.96
1.11
1.zo
1.:0
1.:0
1.11
o.9s
0.42 .. -o.a * -o.s
2.2 * -1.1 * -1.11 * -1.1
2.s
1.4 * -o.a
STAIIDARD DEVIATION
=1, 777 . . . . . . . . .. . . .. . . . . . . ... . . . .. ... . . . . . . .... .. . ..... .. 0.19 0,93 1,03 1.02 1.01 0.91 0.39
o.39
o.M 1.02 o.99 1.01 o.n o.40
l,J
l,Z , -1.Z * -2,6 * -1,9 , 0.5
l.O , 0,40 o. 70 0,40 0.41
0,70 0,39
o. 7 -0.6 -z.z HAP NO! Sl-6-5 DATE: 7/13/81 CONTROL ROD POSITIONS:

F-QCTJ = 1.986 D BANK AT 175 STEPS F-DHCNl = 1.451 , AVERAGE , .PCT DIFFERElltE.

1,7 POWER: 57/. QPTR: NW 0.991 I NE 0.992 ----------!----------

FCZl = 1.327 SW 1.010 I SE 1. 007 FCXYJ = 1.395 BURNUP = 30 MWD/MTU A.O = -7 .65(Y.) 39 l { I ! e i r :sl r f 4 ! ,: i, sf ,, 11 t 6 t; ! ; 7/: ! r at

9¢ t t ~I l ll~ ll(
13., 14f 15" ,, \'

'1 f t !* R Figure 7.6 SURRY UNIT l *...:. CYCLE . 6 'EOL PHYSICS TEST ASSEMBLYWISE PO'JER'DISTRIBtJrION I/E CALIBRATION'""" FLUX MAP p N " L K J " ; , D C 8 ...................... PREDICTED

o.1o1
o.tJ
o.u
PIIEDICTED ,
11EASU1lED
0.3&
0.67
O.J9. , 11EASU1!ED , .PCT DlFFEl!EIICE.
-7.0 * -7.Z * -5.5 * ......................

0.39. 0.92 1.04 1.06 1.04. 0.92

O.J9 0.1a
o.e8
o.98
1.00
o.99
o.e,
o.:sa -1.0 * -4.1 * -s.6 * -6.o * -ti.s * -J.z * -2.8 ,PCT DlffUEIIC!
0.42
0.95 , 1.13 , 1.21 , 1.25 , 1.21 , 1.13
0,95 , 0."2 ,
0,42 , 0,95
1,14 , 1,16 , 1,ZO
1,17
1,10 , 0.9J
O.U , * -o.9 * -o.J
o.4 * -4.2 * -4.J * -l.8 * -1.2 * -2.6 * -2.2 * ............................................................................... , 0,42 0.90 , 1.ll , 1.23
1.21 , 1.22 , 1.21 , 1.23 , 1.ll
0.90 , 0.42 * , 0.42 , 0.90 , 1.13
1.22
1.18 , 1.18 , 1.16
1,22 , 1,lZ , 0.90 , 0.42 , * -1.0 -o.,
o.o * -o.6 * -Z.4 * -1.0 * -4.1 * -o.9 * -o., . -o.6
0.2 * . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ... ' .......................................................... . 0.1, o.95 1.n 1.zti 1.20 1.20 1.1* 1.20 1.20
1.2* 1.u o.95 o.n
0.38 0,94 , 1,13 1,24 1,20 1.19, 1,U, 1,19 1,19 1.24, 1,1", 0,96 , 0,39, * -0.1. -1,4
o.4 * -o.6 * -0.1 * -1.z * -0.1. -o.6. -o.,. -o.,. 1.0
1.4. 1.* * ............................................................................................
0,92
1.13
1.:J
1,20 , 1.16 , 1.15
1,0l
1.15 , 1.16
1,20
I.ZJ
1.ll , 0.92 * , 0.92 , 1.12, 1.24, l.2J. 1,16, 1.15. I.OS. 1.15, 1.15, 1.21, 1.25, 1.15, 0,93, * -0.1. -0.1. o.e. 2.5 , 0.1. -o.8. -o.J. -o.J. -1.0
o.*. 1.s. 1.8. 1.J. A I I e I I* e e * * * * * * * * * * * *
e ****I I I* e *I*******

I** a* I e e * *

e *
e e e *
e * * ** ee * * *
e ******I**

I* e I e e * *

e ** * * * * * * * * * * * ** e , 0.41 1.04 1.21 1.21 1.ZO 1.15 , 0.94 1.U
0.94
1.15 1.20 1.21 1.21 1.04
0.41 ; 1~ r fl t i:} ,* I I 3f ! .r I ' o.41
1.01 1.zo 1.22 1.:1 1,19
o.94 1.u
o.94
1.15 1.21 1.24 1.:z 1.04
o,41 7 -1.4 -1.0 -0.1 0.1 2.8 2.8. -o.z o.o
o.o * -o.s o.9 2.1 o.4 o.4 * -0.2 .. *
o: ;j *:
i: o& *:
i:zs * *
i:22 *:
i:i.i * *
i:oi *:
i:ii *:
i:oi *:
i:ii *:
i :oi * *
i:i; *:
i:zz * *
i:is * *
i:o, **
o: ;; ** , 0,71 , 1.05 , 1.Z4 , 1,Z2 , 1.16 , 1.05 , 1.16 , l.Ol , 1.ll , 1.0Z , 1.1, , 1.2]
1.24 , 1,04 , 0.7Z , er * -1.5. -1.4. -1.2. o.5. 2.2. 2~0. 2.1. o.J*, o.o. -o.4. o.8. o.8. -1.1. -z.1. -0.1. **I** I****** I**** I I I***** I I I* I** I** I** I* I* I***** I* I** I** I****** I****** I***** I I I I* I** I* I I* I I I I I*** I* I I* I* I I , 0,41 , 1.04
l.Zl , l.Zl , 1.20
1.15 , 0,94
1.ll , 0.94
1.15
1.20 , 1.21
1,21 , 1.04 , 0.41 ,
ct.41
1.04
1.22
1.22
1.22
1.19
o.95
1.16
o.94
1.16
1.20
1.20
1.20
1.01
o.41 * , *.. , -1 *** -0.J. O.Z
1.1
1.6
1.9, 1.5. 2.Z
0.2
0.5. O.l. -0.5. -0.9. -0.6 , 0.7 *
o.92
1.n. 1.2J. 1.zo
1.16
1.15. 1.n. 1.1s. 1.1,
1.:0
1.21. 1.u. o.92 * , 0.94
1.15 , 1.24 , 1.21 , 1,16 , 1.10
1.05 , 1,18 , 1.17
l,U , 1.23
1.U , 0.92 *
1.6 , 1.6
0.9
0.4
0.5
Z.2
2.z , 2.0
l.l , 0.8
0.2
0.1
0.1 * .. . . . . . . . .. . . . . . . . . . . . . . . . ... .. . . . . .. . . . . . .. . . . ... . . . . . .. . . . . . . .. . . . . . . . . . . . . ... . . . . . .. . . ... 0.39. 0.95. 1.11. 1,24. 1.20, 1.20. 1.14. 1.20. 1.20. 1.24, 1.11. 0.95, 0.39, *0.1,
0.,1
1.11o
1.21
1.21
1.zs
1.16
1.n
1.u
1.24
1.n
o.9s
o.n *
1.6
1.5
o.5 * -o.8
o.6
2.4
2.2
z.1
z.1 * -o.o * -0.1 * -0.2 * -o.o
e I I I e
I e I I* I** I I I* I* e. I e *I*** e *I* e e II I*** Ill I I I I e I I e I I I a e I II I I I* I* II** I II I I I I e , 0.4Z
0.90 , 1.1]
1.21 , 1.21 , 1.zz , 1.21 , l,Zl , 1.ll
0.90 , 0.4Z ,
o.41
0.,1
1.12
1.24
1.n
1.22
1.22
1.25
1.1,
o.89
o.*z *
1.5
o.6 * -o.,
1.z
2.0
o.5
1.0
1.a
o., * -o.9 * -o.z * . . . ... . . . . . . . .. .. . . . . . .. . . . ... . . . . .. . . . . . ... . . . . . .............

.. . . . . . ....... .. STANDARD

0.4Z
0,95
1.13 , 1.21
1.25
1.21
1.13 , 0.95
O.ltZ *
o.o
o.94
1.16
1.21
1.zz
1.20
1.1s
o.96
o.4Z *
1.s * -o.,
z.6 * -o.3 * -z.6 * -o.9
1.6*
o.e . -0.1 * . .. . ..... ... .. ...... ..... ..... ... .. . .... .. .. ... .. .... .. .. ....... .. 0.39 0.92 , 1.04 , 1.06
1.04 , 0.92 0.39
0,39 0.94 , l.Ol 1.05 1.03 D.9S
D,39
1.7 , 1.6 , -0.5 * -1.7 * -1.l
O.l
Z.O
0.<11 , o. 73 , 0.41 , DEVIATION
0,42
o. 73
0.41 * , AV[IIAGIE , ,PCT D1ff£REIIC!,
1., =l.330 MAP NO: Sl-6-6 CONTROL ROD POSITIONS:

D BANK AT 200 STEPS l.l

0.1 , -1., *

SUMMARY

DATE: 7/14/81 F-QCT) = 1.918 F-OHCN> = l.43S FCZ> = 1.282 FCXY> = 1.389 BIJRNUP = 35 MWO/MTU 40 POWER: 65?. QPTR: NW 0.991 I NE 0.992 ----------1---------- SW 1.012 I SE 1.oos A.O = 5.90(,-) 10, !* 11/i 11 1J H(f [i 15U I r

p H Figure 7.7 SURRY UNIT 1 ....; CYCLE 6 BOL PHYSICS TEST ASSEMBLYWISE'PCWER'DISTRIBurION I/E CALIBRATION*-

FLUX MAP " L I( J H G [ D C II PREDICTED ,

a.42
o.n. o.tiz
PREDICTED
, M£ASUR£0 ,
0.19
o.~a
o.40 * , -6,7, -6.11, -4.7,
HtASL'11£D , ,PCT DIHERCNCE.
0.1,
o.9:
1.04. 1.01. 1.a,
o.92
o.39.
o.n
o.87. o.95. 1.01
1.00
o.91
o.38. , 0.1 , -5.5 , *6,l. *6.J * -4,l * -1., . *1,6 * ,PCT DIFFERENCE.
0,'12
0,95 , l.U, 1.21 , 1.zs, 1.21
l,U. 0.95
o.-.z * , 0.42
0.95 , l,U
1.1'
1.111 , 1,16
1,11
0,9J , 0.42 ,
0,1 , O,Z , D,S * *5,5 * *5,5 ** -..o , *1,6 * *l,6 , ~1.6 * , 0.42 , 0,90 , 1,12 , l,ZZ , l,ZO , 1.21 , 1.ZD
l,ZZ
l,lZ , 0.90
O,U ,
0,42
0.90 , 1,12
l,Zl
1,17. 1.17. 1.14. 1,21
1,12 , O,H. 0.42 *
0.1 * -o.*. -0.1 * -0.1 ** z.s. -J.6 ** ,., * -o., * -0.1 * -o., . 0.1 * . o.n . o.n
1.12
1.24
1.20
1.zo
1.n
1.20
1.zo
1.z,
1.12
o.95
0,39 * , 0,39. 0,93 , l,lZ , 1,22 , 1.19. 1,19. l.lJ, 1.19, 1,19, l,U. l.lJ, 0,96, 0.39, , *0,7 , -z.z * *O,J , *l,3 * *0,4 * *0,6 * *0,6 * *0.7 * *0,1 * *0,7
D,'I
1,0
1,3 *
o.92
1,13
1.22
1.zo. 1.11. 1.u.. 1.n. 1.16
1.11. 1.20
1.zz
1.u
o.9Z *
o.n
1.12
1.zz
1.n
1.11. 1.15. 1.n. 1.15
1.u, . 1.20 , 1.21. 1.1, , o.93, , *0.7 , *0,7 , 0,0 , l,S
D,O , *0,6 , *0,5 , *O,'I * *0.9 , 0,1 , 0,9 , l,! , l,O , A , o.'IZ
1.a,
1.21
1.zo. 1.20
1.16
o.95. 1.1,. 0,95. 1.16. 1.2a. 1.20
1.21
1.04
o.42. , 0.41
1.03 , 1.za , l,Zl , 1,22 , 1,111 , 0,94 , 1.14 , 0.95 , 1,15 , 1.n , l,Z] , l,Zl , 1.04 , 0.41 , , *1,9 , *1,4 , *0,9 , O,S , Z,l , 2,1 , *0,5 , *0,2 , -O.l * -0.4
0,7 , 1,9 * *0,1
0.0 , *0.7 ,
o.n
1.01
1.25
1.21
1.n
1.0:s
1.14
1.H
1.14
1.n
1.n
1.21
1.zs
1.01
o.73 *
o.n. 1.05. 1.21. 1.zz. 1.u.
1.as
1.11. 1.0,*. 1.14. 1.01
1.1,. 1.zz
1.21
1.05
o.n * * -r.1 * -1.9 , -1.1
0.1
z.1
1.6
z.:s
0.1
o.z * -0.1
o.,
o.z * -1.s ** z.s * -o., . ..........................................................................................................
0.4Z
1.04
1.21
1.20
1.::0
1,16
0.95
1,1'
0.95
1.1'
1.20
1.zo
l,Zl
1,04*, O.ltZ ,
o.41
1.01
1.21
1.21
1.21
1.11 , o.9s
1.19
o.9s
1.11
1.n
1.20
1.20
1.n
o.tiz * , *1,9 , *0,8 * *0,3 , 0,6 , 0,S , 1,3
0.6 , '1.0
0,6 , 1,0 , 0,7 * *O.Z , *l,Z , *0,1 , 1,1 , ......................................................
................................................... .
o.9z
1.n
1.zz
1.:0
1.11
1.16
1.n
1.16
1.11
1.20
1.zz
1.n
a.9Z *
o.n
1.14
1.:1
1.20
1.11
1.21 , 1.os
1.19
1.18
1.:1
1.z1
1.u
o.n *
1.J
1.z
o.4 * -0.1 * -0.1 * ,.1 * -..1
z.1
1.J
o.e
o.e * -0.1 * -0.1 *
o.39
o.95
1.12
1.z4
1.zo
1.20
1.n
1.zo
1.zo
1.211
1.12
o.95
o.J9 * , 0,39, 0.96
1.12 .*1.z3, l.Zl. 1.z*. 1,18, 1,24. 1,ZZ , 1.Z4
1.12
0,95. o.J9, . o.e . 0.1
0.1 * -o.9
o.,
s.<1 * ,.,
3,J
z.1 * -o.z * -0.1
o.o * -o.J *
o.u
0,90
1.12
1.22
1.20
1.n
1.zo
1.zz
1.12
0,90
o.u *
a.o
0,90
1.11
1.z4
1.zs
1.zz
1.zz
1.z4
1.n
o.s9
o.u . , O,'I , *0,1 , *0.9
1.3 , Z,Z , 0,7 , 1.1 , 1.7 , O,* , *0,9
0.6
e e *******es es** s s s
s es s s s s s e *
e ***I**** I****************

I I I**** I* I********* P.** . o.u . o.95

1.n
1.21
1.zs
1.u
1.n
o.95
o."z * , o.u
0.9 ** 1.16 , 1.20 , 1.zo , 1,ZO , 1.15 , 0.16 , 0.4Z ,
0,'I * *0.9 , Z.I * *0.9 * -'1,0 , *1,Z
z.z , 0.9 , *O,'I ,
0.39 , 0,9Z , 1.04 , 1.07
1.04 , 0.9Z
I.H , , 0,40
O.~ , l,OJ
1.05
1.03
0.9'
O.toO * , Z,J , Z.3 , *0,5 , *Z.Z , *l,Z
Z,Z , z.z , !ITAIIOAIID
DEVIAT10M , s1.to86 , o.,z . 0.73
o.u , , 0.43
0.75
O.ioJ * , Z,Z , Z.1 , Z,Z , , AYEIIAGE *
PCT DJFFERENCIZ,
1.* MAP NO: Sl-6-7 DATE: 7/14/81 POWER: 85Z CONTROL ROD POSITIONS:

F-QC Tl = 1.828 QPTR: D BANK AT 204 STEPS F-DHCNl = 1.421 NW 0.988 I NE 0.988 ----------1---------- FCZ) = l.232 SW 1.012 I SE l.012 FCXYl = 1.383 BURNUP = 40 MWD/MTU A.O = -l.22CZl 41 l zl \ t JI 6' 7 10 11 R p Figure 7.8 SURRY UNIT 1 -CYCLE 6 BOL PHYSICS TEST ASSEMBLYWISE POWER DISTRIBUTION HFP, EQ. XENON C B PRED!CTEO 11EASUREO .PCT DIFFERENCE. 0.42 0.74 0.42 . 0.40. 0.70 . 0.40. . -5.7. -5.7. -4.5. PRC:OICTED MEASU;;!ED .PCT DIFFEREHCE. 0.39 0.91 l.04 l.09 1.04 0.91 0.39 . 0.39. 0.88. 0.99. 1.04. l.00 . 0.89. 0.38. 0.7. -3.9. -4.8. -4.8. -3.9. -2.7. -1.3. 0.42 0.94 1.12 1.20 l.25 1.20 1.12 0.94 0.42 . 0.43

0.94
l.ll . l.16 . 1.20 . 1.16 . l.09
0.?4 . 0.43 . 0.6 . 0.2 * -0.3. -3.9. -3.9. -3.4. -2.7. -0.5. 0.9 .
0.42 0.90 1.12
l.21. l.20 . l.21 1.20. 1.21 l.12
0.90 0.42
0.43. 0.89. l.ll. 1.21. l.18. l.18. l.15. 1.21 . 1.12. 0.90 . 0.43. 0.1 * -0.1 . -o.3 . -0.1 * -2.0 :* -2.6 . -3.9 . -o.3 . o.3
o.6 . 2.0 . 0.39 0.94 1.12 l.23 l.20 1.20 l.14 1.20 l.20 1.23 1.12 0.94. 0.39 . 0.39. 0.93. 1.11. 1.22. 1.20 . 1.19. 1.14. 1.19. l.18. l.23. l.12 . 0.96
0.40
0.5. -l.2. -0.2*. -0.7. -0.3. -0.6. 0.0 * -0.9. -l.4. -0.4. 0.6 . 2.5. 4.2. 0.91 1.12 1.21 l.20 l.~9 1.17 l.04 1.17 l.19 1.20 l.21 1.12 0.91
0.92 . 1.12. 1.22. 1.22. 1.19. 1.17 l.05. 1.17. 1.17. 1.20 . 1.22 . 1.13. 0.93. 0.5. 0.5. 0.5. 1.2
0.2 . 0.0 . 0.7. -0.l. -2.0 . -c.s . 0.6
l.3. 1.7. A 0.42 l.04 1.20 1.20 l.20 l.17 0.96 l.15 0.96 1.17 1.20 1.20 1.20 1.04 0.42 ~. 0.41. l.D3. 1.21. 1.21. 1.22. 1.19. 0.97 .. 1.16
0.97. 1.17. 1.20 . 1.21 . 1.19. l.03 . 0.42 * , * -1.8 * -Q.7
0.2
o.5 . 1.5 . l.5
o.a . 1.1 . 1.0 . -0.2 * -0.1 . o.8 * -o.9 . -i.o . -1.2 * ...........................................................................................................

0.74 1.09 1.25 1.21 l.14 1.04 1.15 1.05 1.15 l.04 1.14 1.21 1.25 1.09 0.74

0.73. l.OS. 1.23. 1.21 . 1.15. 1.06
l.!7. l.06 . l.lf. . 1.05. 1.14. l.20 . 1.22
1.07. 0.7~ . * -1.a. -1.1 * -1.1. o.5. 1.5. 1.6 . 1.4. 1.4, o.8. o., . o.6 . -o.6 *. -1.9. -1.5. o.6
0.42 1.04. l.20 1.20 1.20 1.17 0.96 1.15 0.96 l.17 1.20 1.20 1.20 l.04 0.42
0.41. l.03. 1.20. 1.21. 1.22
1.19. 0.98. 1.18. 0.96 . 1.17. 1.20 . 1.19. 1.19. 1.04. 0.44. * -1.8. -0.9. -0.5. 0.7. 1.8. 1.7. l.9. 2.3. 0.4. 0.3. 0.2. -1.0 . -1.4. 0.1 . 3.2.
0.91
1.12. 1.21
1.20 . 1.19. 1.17. 1.04. 1.17. 1.19. 1.20 . 1.21 . 1.12
0.91 .
0.92. 1.12. l.?.2. l.Zl. l.19. 1.20
1.06. 1.19. 1.20
1.21. 1.21
l.ll. 0.92. 0.4 . 0.4 . 0.3 . 0.3
0.3
2.3 . 2*.3 . l.6 . 1.0
0.4 . -0.l . -0.2
O.l . 0.39. 0.94 l.l2 l.23 l.ZO 1.20 l.14 1.20 1.20 l.23 1.12 0.94 0.39
0.40 . 0.96. 1.12. 1.22. 1.21 . l.23. 1.16
1.23. 1.23. 1.23. 1.12 . 0.95
0.39. 2.2. 2.2. 0.7. -1.3. 0.4. 2.7. 2.4. 2.3 . 2.0 . 0.2 . 0.4. 0.9. 0.9 *
0.42 0.90 1.12 1.21 1.20 1.21 1.20 1.21. 1.12 0.90 0.42 ** 0.44. 0.91
1.10
1.23. l.Z3. 1.21. l.ZO
l.Zi. 1.12
0.90
0.43. 4.0. 1.9. -1.3. l.3. 2.3. 0.4. O.l. 0.9 .* 0.4. 0.3. 2.5
STANOARO DEVIATION

=l.251

0.42. 0.94. 1.12 . 1.20
l.25. 1.20. 1.12
0.94. 0.42. . 0.44. 0.93. 1.15. 1.20. 1.21. l.!8. 1.12. O.S4. 0.43 *
4.o. -1.3. 3.1. -o.5. -3.2. -1.8. -0.1. -a.1. 1.1 * . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ~; ... *** ....* ; .. -. ; **..................

0.39 0.91 1.04 l.09 l.O~ 0.91 0.39

0.40 . 0.95. 1.05. l.08. l.03. 0.91. 0.39. 3.6. 3.6 . 0.6 . -l.l. -1.4. -0.6 * -o.o * ................................
................. . 0.42 . 0.44 3.6 0.74 0.42 0.75 0.42 l.7 * -l.3 *

SUMMARY

-------AVERAGE .PCT DIFFERENCE

= l.4 MAP NO: Sl-6-8 DATE: 7/21/81 POWER: 100?. QPTR: CONTROL ROD POSITIONS:

F-Q(T) = 1.810 D BANK AT 228 STEPS F-DHCNJ = l.413 NW 0.992 I NE 0.997 ----------1---------- F(Zl = 1.223 sw 1.010 I SE 1.001 FCXYJ = l.377 BURNUP = 170 MWO/MTU A.O = -2.47(?.l 42 6 9 t ' 10 11 r 12 l3 14

i 15 Se"c:tion 8 REFERENCES

1. S. A. Ahmed, T. W. Schleicher, "Surry Unit 1, Cycle 6, Design Report," N'.FE Technical Report No. 183, Vepco, May, 1981. 2. Surry Power Station Technical Specifications.

3. Surry Power Station Final Safety Analysis Report. 4. T. K. Ross, W. C. ~eek, "Control Rod Reactivity Worth Determination By The Rod Swap Technique," VEP-FRD-36A, December, 1980. 5. T. J. Kunsitis, "RXFLOW, A Computer Program to Calculate Reactor Flow and Thermal Output," NFO-CCR-8, Vepco, Decemb~r, 1979. 6. "Technical Manual for Westinghouse Solid State Reactivity Computer," Westinghouse Electric Corporation.

7. W. Leggett and L. Eisenhart, "The INCORE Code," WCAP-7149, December, 1967. 43 APPENDIX STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEETS

I JUL 3 1981 SURRY POWER STATIC~ UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I Re:fe:rence II Test Conditions I (Design) I I Test

Description:

Reactivity Compute:r Checkout P:roc Ho /Section: PT28.11/APP. B Sequence Step Ho= Bank-Positions (Steps) SDA: 228 CB: 228 SDB: 228 cc: 228 CA: 228 CD: X RCS Ternpe:ratu:re C°F): 547 Powe:r Level C?. F.P.): 0 Othe:c (specify): Below Huciea:r Heating *At the just c:rit. position ------'------------------

III Test Conditions (Actual) :IV . ~est Resul.ts V Acceptance Crite:ria V:I Comments Bank Positions (Steps) RCS Ternperatu::e C °F): S1S: 0 'F SDA: 228 CB: 228 SDE: 228 cc: 228 CA: 228 en: 1513 Powe:r Level C 7. F. P. ) : -o fo Othe:c (Speci:fy): Date/Time Test Per£o:rmed: Measu:red Parameter C Des-cz:iption) Heasu:red Va1ue Design Value (Actual Conditions) Design Value (Design Conditions) Re:ference FSAR/Tech Spec Re:fe:rence = Measured Reactivty using -corn? = Inferred React f:rom :react period 7.D = I C ~c.. -~-t ) / ~;t-X 1007. S 4.0?. 7.D =IC~~---~)/~ Ix 1007. S. 4.07. WCAP 7905, Rev. 1, Table 3. 6 Hot Applicable Mot Applicable Design Tolerance is met Acceptance Criteria is met /YES _NO .. 7YES __ HO Allowable Range = :!: S 'f pe,m A. l Evaluated By: Recommended £0:r App:roval B.y : NFO Enginee:r JUL 3 1931 SURRY POWER STATION UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATION SHEET I Re£e:r:ence II Test Conditions (Design) III Test Conditions (Actual) IV Test Resul.ts Test Desc:r:iption: C::c:itical Bo:r:on Concent::c:ation -ARO P::c:oc Ho /Section: PT28.11/APP. C Sequence Step No: 7 Bank Positions (Steps) SDJI.: 228 CB: 228 SDB: 228 cc: 228 CA: 22.8 CD: 228 Bank Positions (Steps) SDA: 228 CB: Z..28 SDB: 2.2..S cc: Z.2-8 CA: Z.2..8 CD: .;t2.8 Date/Time Test Pe:r::fo:r:med: 1-1:;1a1 I os 11 Meas Pa:r:amete:r:

I RCS Tempe::c:atu::c:e

(°F): 547 Powe~ Level. C?. F.P.): 0 Othe:r: Cspeci£y): Below Huclea:r: Heating RCS Tempe:r:atu:r:e (°F): S4S.Z °F Powe:r: Level. C:'. F.P.): 0% Othe:r: CSpeci:y): ' "" C Desc::c:iption) I C C5 )MO; C::c:i t Boz:on Cone -ARO ---------'------------------------- I1easu:.::ed Value Design Value '*( Actual Cond l Design-Value (Design Cond) Re:fe:r:ence-1 C CB ):P.D = I 1-8 __ +.-;;;;m.. Cs= 1480 ! 50 ppm VEP-FRD-HFE-183 V FSAR/Tech Spec Acceptance \Cz:ite:r:ia Ref~::c:ence FSAR Section 14.2.5 v:c -Comments Compl.eted Design Tole:r:ance is met Acceptance C::c:itez:ia is met 7°YES _HO :Z:YES _NO o< .C.& = -8.42 pcm/ppm :fo::c: p:r:elimima:ry anal.ysis o<: C --=--8.1B re-/pr~ f.w. +\...J """"-'~ys*,s B / Eval.uated By: J. 4 -1~ Recommended

fo:r: App:coval By A _;,f C_. 7 __ ,.....,..~,)

}ff~ Eng inee:r A.2 JUL 3 1981 SURRY POWER STATION UH!T 1 CYCLE 6 STARTUP PHYSICS -TEST RESULTS AND EVALUATION SHEET I Re:fe:tence II Test Conditions (Design) III Test Conditions C Ac t'!._al ) IV Test Results V Acceptance C:z:i te?:'ia VI Comments Test Desc:tiption: Isothezmal Tempe:tatu:te Coei:ficient-ARO P:toc No /Section: PT28.11/APP. D Sequence* Step Ho= Bank Positions (Steps) I I SDA: 228 SDB: 228 C". ,. . 228 I RCS Tempe?:ature C°F)L 547 Powe?: Level (% F.P.): 0 OtheI: Cspeci:fy): CB: 228 cc: 228 en= 228 I Below NucleaI: Heating Bank Positions SDA: :Z..Z SDB: :U..l?° CB: 2.2.%-cc: 22.3-(Steps) CA : "l.2.. 3'" CD: ~C'l.. I I I I I I RCS TemPeratuI:e C °F): t:."'4L/,1 °f Poue:r L~vel C?. F.P.): -oio Othe:r (Specify): Below Nuclea:t Heating Date/Time Test Pe:i::i:01:med: I 7/1/8! Meas Pa:i:::amete:i::: (Desci:iption) Measui:ed Value nesign Value (Actual Cond) Design Value (Design Cond) Re:fe:rence FSAR/Tech Spec Re:fezence /1../0 "'2.. I I ,4so )AAD Iso Temp Coe:£:£ -AP.O (~o )AAO = -1~32. pur,/0 r CC5 = 1r./f::.3 ) pp.-.--c.qso )AAo -= ~--4.00 +/-?,o r,vnj°f(ce, = 1'-lb3. >pf,.._ *< = -3.79 ! 3.0 pcm/°F (Cs = 1480 ppm) VEP-FRD-HFE 183

0.45 pcm/°F TS 3.1, VEP-FRD-HFE 183 ~p = -2. 05 pcm/°F Design Tole:i:::ance is met Acceptance Crite:i:::ia is met* /YES _NO LYES _NO
Uncer.tainty on aT "' 0.5 pcm/Op (

Reference:

memorandum from

MOD C.T. Snow to E. J. Lo~ito dated June 27, 1980) Completed By~-~.LJ~~~ . Test °tlgit)" A. 3 .Evaluated By, ti ft. ,CP,,Ad, << Recommended

-£or // /? * / App:roval ~Y ;---z?-?-/C........ ./ XFO Enginee:i:: T JUL 3 rsar SUP.RY POWER STATION UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATION SHEET I I Re:fe:t:ence I II Test Conditions I (Design) I I III I Test I Conditions I (Actual) I I I I I I :rv I I I I I Test I Results I I *I I I Test Desc:t:iption

H/D Flux Map -HZP, ARO P:r:oc No / Section: PT28. 2, OP-57 Sequence*

Step Ho: C\ Bank Positions (Steps) I RCS Ternperatu:r:e C°F):TRE~ !1 _________________ ! PotJe:t: I.evel o: F.P.): .... o SDA= 228 SDB: 228 CA: 228 CB 22s cc : 22s en: 22s I Othe:z:: (specify) I Must have~ 40 thimbles _________________ ,_. ---------------- Bank Positions (Steps) 1 -----------------' SDA: :Z2Z SDB: 223" CA: 22.B I CB : z:z.?: CC : ZZli CD: 20 I I ------------------' Date/Time Test :1-,; I RCS TempeI:a tux:e ( ° F) : 5'45" 0 F' Powe:r: Level (7. F.P.): ,.....0 Othe:r: (Specify): Pe:r::fo:z::rned: 7/7; // /030 I -----------------'---------------- MAX. REL I NUC ENTHALITOTAL HEATI 2UADRANT Meas Pa:r:amete:r:I ASSY PWR I P.ISE HOT I FLUX HOT !POWER TIL~ (Description) I DIFF I CHAN FACT ICHAN FACT RATIO I CM-P)/P I F-dHCH) I F-2CT) 2PTR ----------' ' '--------------- 112. (/'(.._ C f'l(.13=i.;z1I I ;;k /. 0257. Measu:r:ed Valuel/c.4~£-p

o411 /.584 I 2.430 --------'

A~

I '-------------Design Value f :io: for Pi .:o. *9 I .
l c Design Conds) I ~1s: for Pi< .9 I -!a..s1.ssc1+.2c1-P))

I r~cz:)~4.36

z: x~z) $ 1.02 I (Pi

Asay. Pvr.) I *-** J ---------------------I WCAP-7905 I I Re:fe:r:ence" I REV; 1 I NONE I HONE WCAP-7905 REV. 1 I ---------'

I '------------- I ! I I V I FSAR/Tech Spec! MONE I HA I HA MA Acceptance

'

I '------------- C:r:ite:z:ia ! I I R.e:£e1:ence I NONE I T.S. 3.12 I T.S. 3.121 T.S. 3.12 I I I I -------------------' I '------'------- VI Comments Completed Design ToleI:ance is met Acceptance CI:ite:z::ia is met K °""'SAT"" .-tcl<2.v-~-s no+~, ~s:+.:. .c,.,r'4. A.ce>r--b..bk. j"""' R"k~: L Sv,.<<1. f'o~ s+,d~\°" l'.).w'1cet\~ ~e,,y-t:; No: Sl-~l-1,s-. Evaluated By: Recommended £0:z:: Appi::oval By HFO Engineer A.4 JUL 3 7987 SURRY POWE?. STATION UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATION SHEET I Re:fe:r:ence II Test Conditions (Design) III Test Conditions (Actual) IV Test Results v. Acceptance C::cite::cia VJ: Comments Test

Description:

Cntl Bank B Worth Meas.-Rod swap Re:£ Bank Px:oc Ho /Section: PT28.11/APP. E Sequence Step No: \0 Bank Posi*tions (Steps) I RCS Tempe:r:atu:r:e C ° F) : 547 I Powe:c Level C 1. F.P.): 0 SDA: 228 .SDB: 228 CA: 228 I Othe:r: (specify): CB:t1oving cc: 228 en: 228 I Belot.1 Huc1.ea:c Heating I Bank Positions (Steps) I RCS Tempe:r:atuxe (OF): S45.Z "F I Powe:c Level ( 7. F.P.): 0% SDA: '-'-8 SDB: z:z.B CA: 'Z..'Z..S I Othe:r: (Speci:Ey): CB: l'1o"i"j cc: Z2.8 cn:z'Z.8 I Below Nuclear Heating I Date/Time Test Pe:r:fox:med: I 1-/7/8! /Zl30 Measured Parameter CDesc:r:iption) Measu::ced Value Design Value jActual Conditions) Design .Value (Design Conditions) R.e:fe::cence FSAR/Tech Spec Re:fe::cence I I ;Integral Wo:r:th o:f Cntl Bank B, All Othe::c Rods Out I P.$.F = ei IRE.F = e, /_4ot +/-:' 14 / f°Cl'Yt. 1406 +/- 141 pcm VEP-FRD-HFE-183 I£ Design Tolex:ance is exceeded, SHSOC shall evaluate impact 0£ test ::cesult on safety analysis. SHSOC may specify that additional testing be pe:cfo::cmed. VEP-FRD-36A Design ~ole:cance is met Acceptance C::citeria is met Completed By* Evaluated By: J S. !f ;;tdi~ C. :J. .c-t:-J A.5 Recommended £0::c App:coval By HFO EngineeJ: JUL 3 1931 SURRY POWER STAtIOH* UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET. I Re:fe:i::ence II Test Conditions I (Design> I Test

Description:

Critical Boron Concentration -B In P:r:oc Ho /Section: PT28.11/APP. C Sequence *Step Ho: \ \ Bank Positions (Steps) SDA: 228" SDB: 228 CB: .O cc: 228 CA: 228 CD: 228 Res-Tempe:i::ature C °F): 547 Power Level. C?. F .P.): 0 Othe:i:: Cspeci:fy): Below Hucl.ear Heating ------'------------------

III I Bank Positions (Steps) Test ! __________________ _ RCS Temperature C°F): 546.l"f" Powe:r:: Level. (?. F.P.): 0 % othe:i:: CSpeci:fy): Conditions (Actual.) IV Test Re13ults SDA: Z..2. 8 CB: o SDB: z.z .. g cc: u .. s CA: Z'Z-8 CD=Z.U':l Date/Time Test Perfo:i::med: t-(8/81 I 03-z.o Meas Paramete::c I (Desc:i::iption) I M CC5)s ; C:i::it Boron Cone -B Bank In ---------'------------------------- Maasu:r::ed Val.ue 1 I I I 3_2.., p f rm ---------'------------------------- Design Value* .(Actual Cond) ' I ca= / 31.. 0 I 2-t -~l°m ---------'------------------------- Design Value (Design Cond) 1 :!: C 10 I C B = 1 3 1 6 + C.~RE'I ---------'------------------------- Re:ference 1 VEP-FP.D-HFE-183*

'-------------------------. V Acceptance . C1:ite:r::ia 1 FSAR/Tech Spec I o<.c..5xCe,S15,115pcm

_________ I _________________________ _ Re:fe:r::ence I FSAR Section 14.2.5 ------__________ l _________ ~--------------- 7YES __ HO VI . Comments Design Tole::cance is met Acceptance C:r::iteria is met VYES _HO -8.42 pcm/ppm *:for p:r:elimimary analysis "' = C c6 )AAo -1480 ppm -8.TS t""lf'r"' .f-. f.-~-I ~lys;*s Completed By: Evaluated By: J.d. c..:J. Recommended £01: App:r::oval By HFO Enginee:t: A, 6 JUL 3 1981 SURRY POWER STATION UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATIOH SHEET I Re:fe:z:ence Test Desc:z:iption: Isothermal Temperatu:z:e Coe:f:ficient-B In P:z:oc Ho /Section: PT28.11/APP. D Sequence Step Ho: l 7: II Test Conditions I (Design) I Bank Positions (Steps) SDA: 228 CB: 0 SDB: 228 cc: 228 er..: 22s CD: 228 ______ I __________________ _ III I Bank Positions (Steps) Test '------------------------- Conditions I (Actual) I SDA: Z.."Z..8 CB: 0 SDB: 2.-'t.8 cc: Z..Z..8 CA: z.:z..8 CD: 2.'2.3 ------'-------------------- 1 Date/Time Test Pe:x:£0:z:med: RCS Temperature C°F): Powe:z: Level CY. F.P.): Othe::t C specify): Below Huclea::t Heating RCS Ternpe:z:atu:z:e C 0 f): Power Level (7. F.P.): Other C Specify): Below Huclea::t Heating 547 0 1 1!a/Bt / o4-Jo , __ ... z.:_ __________________

1 Meas Pa::tamete::t IV I CDesc:z:iption) c4So )i; Iso Temp Coe:fi -B Bank In '---------- 1 Test I Measu:z:ed Value Results I __________ _ V Acceptance Cl:ite:z:ia I I Design Value (Actual Cond) Design Value (Design Cond) Re:fe::tence FSAR/Tech Spec Re:fe:z:ence (~ )5 = ..:.*i. s~ i'~m/o'F-ca = 133/ >rt"'-cciqso )5 = -' 3fo 3 0 ( C B = l 33 [ ) ff""--. -. f'cf1{.c~ (~ )~ = -6.55 : 3.0 pcm/°F CC13 = 1316 ppr:i.) VEP-FR.D-NFE 183 TS 3.1. VEP-FRD-NFE 183 ------'----------

1 I Design Tole:z:ance is met : .,/YES _HO VJ: I Acceptance C:z:ite:z:ia is met ~YES _HO '---------------------------------------- 1

I Uncertainty on aT I
MOD Comments a 0.5 pcm/OF (

Reference:

memorandum from I C. T. Snow to E. J. Lozito dated June 27, 1980) ----------..----------------------------------- Completed By A. 7 . . Evaluated By: R.ecommended

fo:z: App?:oval By NFC Enginee:r:

-...-*,:. JUL 3 1931 ,, SURRY POWER STATION UNIT 1 .CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I Refe:r:ence II I* Test Desc:r:iption: HZP Bo:r:on Wo:r:th Coefficient P:roc Ho /Section: PT28.11/APP. E Sequence Step Ho: ff/A Bank Positions (Steps) Test RCS Tempe:r:atu:r:e (°F): 547 Powe:r: Level (?. F.P.): 0 Othez: (specify): Conditionsl '(Design) I III Test Conditions (Actual) IV V Acceptance Cz:ite::r:ia VI

Comments SDA: 228 SDB: 228 CB=noving cc: 228 CA: 228 CD: 228 Below Huclea:r:

Heating Bank Positions (Steps) RCS Tempe:r:atu:r:e C°F): S-46,/Dp-' Powe:r: Level (7. F.P.): 0% Othe:r: (Specify): SDA: 2.'Z. 8 SDB: 2:2 .. s CA: Z.z..8 CB: no.ti~ cc: z. Z.8 CD: 'Z. Z..B Date/Time Test Pe:r:fo:rmed: ~/8/BI I 03s-o Measu:r:ed Pa:r:amete:r: CDesc:r:iption) Measu::r:ed Value , Design Value {Actual Conditions) Design Value (Design Conditions) Re:fe:r:ence FSAR/Tech Spec Re:fe:r:ence ()( C.e,, Bo::r:on Wo::r:th Coe:f:ficient VEP-FRD-HFE 183 °'C5 x Ce, S 15,115 pcm FSAR Section 14.2.S Design Tole::r:ance is met Acceptance C:r:ite:ria is met Completed By: Evaluated By: c~ :J'. J~ Recommended fo:r: App:r:oval ~y: MFO Enginee:r: A. 8 JUL 3 i3B1 SURRY POWER STATIOij UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATIOH SHEET I Reference II Test Conditions (Design) Test

Description:

M/D Flux Map *~HZP, B-Bank In Proc No / Section: PT28. 2, OP-57 Sequence Step No: \ 3 Bank Posi~ions (Steps) I RCS Temperature C°F):TREF !1 ----------------------------------' Power Level (7. F.P.):-o SDA: 22S CB 0 SDB: 228 cc : 228 CA: 228 I Other {specify) CD: 228 I Must have*~ 40 thimbles ------------------------------------1--------------------- III Test Conditions (Actual) Bank Positions (Steps) I RCS Temperature ( ° F): .,47------------------------I P 01Je r Leve 1 C?. F

P * ) : -o SDA: l'Z 6 CB :u/z.~ SDB: -z.zs cc : Z.-Z.8 CA: 7.z.B CD: "l..Ze. I I ---------------------,--,-------'

Date/Time Test: ;r'~BJ I Other CSpeci:::y): 10 pl/,,..,,6L.£'"$ IV Test Rirsults Performed: 07:J.J I -------------------'------------------ MAX. REL I HUC EHTHALITOTAL HEAT QUADRANT Meas Parameter! ASSY PWR I RISE HOT I FLUX HOT POWER TILT (Description) I DIFF I CHAH FACT ICHAH FACT I CM-P)/P I F-dHCN) I F-2CT) ---------' 1..--------'------ I +sAj;,~di:>"11' I RATIO QPTR

1.oz 7rs, Measured Value 1., 6-4,;FoJt fl,;0.3'r I*] '1~ I z. 11~ ---------~--=-,,-----=-'

'-------------- .:10: for Pi

9 I I Design Value =cnesign Conds) Re:Eerence

.:15% for pi< .9 I HA 1* HA (Pi

Auy. Pvr.) I I ------WCAP-7905 I I REV. 1 I NOHE I HONE I !':: 1. 02 WCAP-7905 REV. 1 --------------------

' '------'------

V Acceptance C:z:iteria 1 I I FSAR/Tech Spec NOHE I NA I HA I HA -----------------1 I I _____ _ I I I Re:Eerence HONE I T.S. 3.12 I T.S. 3.121 T.S. 3.12 I I I ~-------------------- ______ I I I ______ _ VI **.comments Completed Design Tolerance is met Acceptance Criteria is met _ YES /xo vYES __ HO ,;,:: 0"S:,V\ -b lca.,,-~c..cz. t'\O+ I bv::*f ('".;a.su.1+ ,~ o...cf,,j,k_. ~-t~-:. . 1. 5,~*--vYl ~'u1.......r St~IC'Y'-~.o:*,iey,.. ~c:-r-t-No. S\-8\-t,s. A. 9 Evaluated Recommended Approval --*~ JUL SURRY POWER STATION UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATION SHEET I Reference Test Test

Description:

Cntl Bank D Worth Measurement-Rod Swap Proc Ho /Section: PT28.~1/APP. F Sequence Step No= \4 Bank Positions (Steps) Conditions! SDA: 228 SDB: 228 CA: 228 (Design) I CB=Moving cc: 228 CD:Moving RCS Temperature (0:): 547 Power Level C?. F.P.): 0 Other (specify): Below Nuclear Heating III Test Conditions (Actual) IV Test Results V Acceptance C:z::iteria VI Comments I I I Bank Positions (Steps) SDA: 2.'2. g SDB: 2.2 g CB =N\oviY\~ cc: e. 2.8 CA: 2.2.8 cn: Mw*~ Date/Time Test Performed: 7 /?/81 -/02S-RCS Terape::c:atu:i:e (0 f):£"+7."/ Power Level(% F.P.):0 Other CSpeci:::y): Below Nuclear Heating Meas Parameter (Description) I:;5 ;Int Wo:z::th o:f Cntl Bank D-P.od Swap Measured Value Design Value I~ . =. / 2. 31-fC-M (Adj. Meas. Crit. Re:: Bank Position*= /7S-.steps) IC Actual Cond) (Adj. Meas. Crit. Re:: Bank I:,S =/2.2~ +/- /S'rpcrnPosition = J 7.S-steps) I I I Design Value 1221 +/- 183 pcm (Critical Re! Bank ICDesign Cond) I~= D . P6sition = 185 steps) I I I I I Re:ference FSAR/Tech Spec Reference VEP-FRD-NFE-183, VEP-FRD-36A, HFO-TI-2.2A I:f Design Tolerance is exceeded, SKSOC shall evaluate impact o:f test result on safety analysis. SHSOC may specify that additional testing be performed. VEP-FRD-36A Design* Tolerance is met Acceptance Crite~ia is met ~YES _NO ...X.,YES _HO A.10 Evaluated By: Recommended

for Approval By 7K& c.:J~ NFO Engineer:

,;:-~-~f .

JUL 3 1981 SURRY POWER STATIOH UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I Re:ference II Test Conditions I (Design) I III Test Conditions (Actual) IV Test Results V Acceptance C:z:ite:x:ia VI: Comments Test

Description:

Cntl Bank C Worth Measurement-Rod Swap Proc No /Section: PT28.11/APP. F Sequence Step Ho: l6 Bank Positions (Steps) RCS Temperature C°F): 547 Power Level (2 F.P.): 0 Other (specify): SDA~ 228 SDB: 228 CA: 228 CB=Moving cc:Moving en: 228 Below Huclear Heating Bank Positions (Steps) RCS Temperatu:z:e C °F): S~7.S" Powe:x: Level C~ F.P.):O Othe:z: (Speci:fy): SDA: 2.2.8 SDB: 2.2.8 CA: 22.8 CB :/J\ovi~~ CC: Movi~~ CD: Z:28 Below Nuclear Heating Date/Time Test 7/a/s, /(0~ Meas Pa:z:ameter CDesc:z:iption) Measured Value Design Value (Actual Cond) Design Value (Design Cond) Re:fe:x:ence FSAR/Tech Spec Re:fe1:ence I I I I I I I I I I I I I I I I I I I I I I I Performed: I~ ; Int Wo:z:th o:f Cntl Bank C-Rod Swap I~ = g /5" pe,'tf\ (Adj. Meas. Crit. Ref Bank Position= /10 steps) (Adj. Meas. Crit. Ref Bank I~ = 833:t lcS-pe.'ft\ Position = //0 steps) I~= c.. 827: 124 pcm (Critical Re:f Bank Position= 130 steps) VEP-FRD-HFE-183, VEP-FRD-36A, HFO-TI-2.2A If Design Tolerance is exceeded, SHSOC shall evaluate impact o: test result on safety analysis. SHSOC may specify that additional testing he performed. VEP-FRD-36A Design Tolerance is met Acceptance Criteria is met ~YES _HO ~YES __ NO .Evaluated By: Recommended fox: App::i::oval. By c.~2~ XFO Enginee::c A.11 JUL 3 1981 SURRY POWER STATION UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I Re£e:z:ence II Test Conditions I (Design) I Test Desc:z:iption: Cntl. Bank A Wo:z:th Measu:z:ernent-Rod Swap Pz:oc Ho /Section:. PT28.11/APP. F Sequence *step }{o: I (p Bank Positions (Steps) SDA: 228 SDB: 228 CB=Moving cc: 228 CA=Moving en: 228 RCS Tempe:z:atu:z:e C 0 f): 547 Powe:z: Level C?. F.P.): 0 Othe:i: Cspeci:fy): BeJ.ow Nuclea:z: Heating ______ ! __________________

III I Bank Positions (Steps) RCS Tempe:z: atu:z:e C ° F): Sl/--7. 3 Powe:z: Level(~ F.P.):O othe:z: CSpeci:fy): Test ! ________________ ,___ Conditions! SDA:22~ SDB:22.8 CA:Mbvi°"-' CActuaJ.) CB:Mov1\I\~ cc: 2.2.8 CD: 228 Be1ow Nuclea:z: Heating IV Test -Results V Acceptance! Date/Time Test Pe:z::fo:z:med= 7/3/91 //37 Meas Pa::camete:r CDesc:z:iption) Measu:z::ed Valu'e Design Value (Actual Cond) Design Value (Design Cond) Re:fe:rence FSAR/Tech Spec I~ ;Int Wo:z:th o:f* CntJ. Bank A-Rod Swap (Adj. Meas. C:z:it. Ref Bank I~ = S-S"/ pc'('()

Position = 83 steps) RS (Adj. Meas. C:z:it. Ref Bank IA =S-1-,"!:.

/OO~fl)Position

g:; steps) I~S = 555 100 pcm CC:ritical Ref Bank Position

100 steps) VEP-FRD-HFE-183, VEP-FRD-36A, HFO-TI-2.2A I:f Design Tole:i:ance is exceeded, SNSOC shall evaluate impact of test ~esult on safety knalysis. SHSOC ~ay specify that additional testing be pe:z::o:i:med. C:rite:i:ia '----------

1 R.e:fe:z:ence VEP-FRD-36A

'----------

1 Design Tole:z:ance is met ~YES __ NO VI I Acceptance C:z:ite:i:ia is met ~YES __ NO Comments '------------------------------------------- 1 I ------'--------------------------------------- Completed B Evaluated By: Recommended £0:i: App:coval. By A. 12 .7K..~ c.:J.~ NFO Enginee:z:: JUL 3 1981 SURRY POWER STATION UNIT 1 CYCLE 6 STARTUP'PHYSICS TEST RESULTS AHD EVALUATIOH SHEET I Re:fe:z:ence II Test Test Desc:z:iption=Shutdown Bank B Wo:z:th Measurement-Rod Swap P:z:oc Ho /Section: PT28. 11/ APP. F Sequence *step Ho: \ Bank Positions (Steps) Conditions! SDA: 228 SDB:Moving CA: 228 (Design) I CB=Moving cc: 228 en: 22s* RCS Tempe:z:atu:z:e (°F): 547 Power Level (7. r.P.): 0 Othe:z: (specify):. Below Nuclea:z: Heating -----'-----------------

II:I I Bank Positions (Steps) RCS Tempe?:atu:z:e C ° F): S".l/-7.1-Powe:z: Level (7. F.P.): 0 Othe:z: (Specify): Test '-----~---..-~------- Conditions I SDA=2.2.~ SDBdVlovlY\"CA= 2.2.8 (Actual) i CB=.Mo\/1"j cc:2.28 cn:228 Below Huclea:z: Heating -----'----------------- 1 Date/Time Test Pe:z::fo:z:med: I 7/a/ 8/ /2 Lf-J '-----------------

1 Meas Pa:z:amete:z: I CDesc?:iption) I~ '---------

Int Wo: :rth o:f Shutdo.wn Bank B-Rod Swap IV I Test I Heasu:z:ed Val'l.te I~ =. /0/3 f>C..Yf> * (Adj. Meas. C:z:it. Ref Bank Position = /38 steps) Results '---------

1 Design Value IC.Actual Cond) Design Value (Design Cond) Re:fe:z:ence (Adj. Meas. exit. Ref Bank :I~ =/()()St/S-lpe'ff\Position = /38 ste:i:;s> (D/0 *IS2 :t .J-6< pcm ';'7 /<.f.?.. '1 Kie. 7/9/a, 7/~/81 CC::ritical Re:f Bank Position = J.,&6"' steps) ,s~ 11</l il1/i1 VEP-FRD-HFE-183, VEP-FRD-36A, HFO-TI-2.2A V FSAR/Tech Spec I£ Design Tole:z:ance is exceeded, SNSOC shall evaluate impact of test ~esult on safety analysis. SNSOC may specify that additional testing be pe:z:fo:z:med. Acceptance C:z:ite:z:ia VI Comments Completed Re£e:z:ence VEP-FRD-36A Design Tole:z:ance is. met Acceptance Ci:ite:z:ia is met .ll. 1 1 ~YES __ HO -2(.YES __ NO Evaluated By: Recommended £0:z: . Appi:oval. B,Y c.:J.~ NFC Enginee:r .. JUL 3 1987 SURRY POWER STATIOH UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATION SHEET I Re:fez:ence II Test

Conditions (Design) III Test Conditions (Actual) IV Test R~sults Test Descz:iption:Shutdown Bank A Woz::th Measuz::ement-Rod Swap Pz:oc H.o /Section:

PT28. 11 /APP. F Sequence Step Ho:

l B Bank Positions (Steps) SDA:Moving SDB: 228 CB:Moving cc: 228 CA: 228 CD: 2 28 Bank Position~ (Steps) SDA: MoiJIYi9 SDB: c.2.8 CB: /AO'li~~ CC: '2.28 CA: 2.~ CD: 2.2.8 Date/Time Test Pez::oz:med:

7/8/~1 le.OS-RCS Tempez:atuz:e C°F): 547 Power Level (7. F.P.): 0 Othez: (specify): Below Hucleaz: Heating RCS Tempez::atuz:e ( ° F): Powe:r Level C?. F.P.):0 Othez: (Specify): Below Nucleaz: Heating Meas Parametez: (Descz:iption> PS IsA ;Int Wo:z:th o:f Shutdown Bank A-Rod Swap l1easu:red Value Design Value (Actual Cond) Design Val.ue (Design Cond) Re:Ee:rence I~ =//37fC!.rf\. (Adj. Meas. C:z:it. Ref Bank Position = /5'1 steps) (Adj. Meas. Crit. Re:f Bank I~ = /078 :t 1,; p¢W\ Position = / S7 steps) ,,2. ~pcm iK.f. 7/'l/91 tCz::itical. Ref Bank Position= )...S-S"'"steps) ,~s-71<./c. 1/9/81 VEP-FRD-HFE-183p VEP-FRD-36A, NFO-TI-2.2A V FSAR/Tech Spec If Design Tolerance is exceeded, SHSOC shall evaluate impact of test*z::esult on safety analysis. SHSOC may specify that additional testing be peI::formed. Acceptance C:z:ite:z:ia Re:fe:rence VEP-FRD-36A Design Tolexance is met VI I Acceptance CI:iteI:ia is met ..2S:..YES _NO : ..XYES _NO Comments '--------------------------------------- 1 I ------'------------------------------------- A.14 Ev~luated By: Recommended £oI: ... AppI:oval By : C.,1.~ NFC EngineeI: " JUL 3 1981 SURRY POWER STATION UNIT 1 *CYCLE 6 STARTUP PH~SICS TEST RESULTS AHD EVALUATION SHEET I Re:fe:z:ence II Test Test Desc:z:iption: Total Rod Wo:z:th-Rod Swap P:z:oc Ko /Section: PT28.11/AP~. F Sequence Step Ko: lq

Bank Positions (Steps) ConditionslSDA:Moving SDB:Moving CA:Movingl (Design) I CB=Moving CC=Moving CD=Movingl RCS Tempe:z:atuie C°F): 547 Powe:z: Level C~ F.P.): 0 Othe:z: (specify):

Below Kuclea:z: Heating --------'-----------------'-----'-------------- III Test Conditions (Actual) Bank Positions (Steps) ( --------------- ...... -' SDA :/y\o..,in, SDB: /v'to'liV\~ CA: ,V\ovi.,., I RCS Tempe:z:atu:z:e C°F):5'f7.J Powe:c Level C?. F.P.): 0 Othe:c (Specify): Below Huclea% Heating CB: Mo"i""' CC: M O'liv"I-' CD: Mb\JiV\j I ------__________________ i J:V Test Results Date/Time Test Pe:c~o:z:med: I 7/7/a1 e.130 7!9/~I lc.~J I _____________ / __ *--------'----------------- 1 Heasu:z:ed Pa:camete:c I rTo~\;rnteg:cal Worth oz All Rod Banks-CDesc~iption) I Rod Swap ------------'---------------------- ' : :!.roib.1 = <o. I CJ O f~m ------------ Measu:ced.Value Design Value I -(Actual Conditions)

ITc,;c..J=

0.0 91-t DCf pe,vn Design Value I (Design Conditions) I I"G'h>J= 6098 ! 610 pcm ------------'---------------------- ' VEP-FRD~HFE-183, VEP-FRD-36A, NFO-TI-2.2.A R.e:fe:cence

'---------------------

V Acceptance C:cite:cia I I VJ: *, Comments I I I I Completed FSJl.lVTech Spec ! I I I I:f Design ~ole:cance is exceeded, SHSOC shall evall.fate impact o:f test :cesult on sa:fety analysis. SNSOC may specify that additional testing be pe%fo:cmed.

'----------------------

1 Re:fe%ence I VEP-FRD-36A

'------,-----------------

.2S...YES -'-HO Design Tolerance is met Acceptance C:z:ite%ia is met A.15 -A.YES _NO . Evaluated By: Recommended

fo% App:coval By c.f.~_ NFO Enrr~;. -..

"' JUL -3 1931 SUP.RY POWER STATION UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATION SHEET I Test Description M/D Flux Map -At Power, HI Calib. Re:ference Proc Ho/ Section: PT28.2, OP-57 Sequence Step Ho: 45 II Bank Positions (Steps) I Test I Conditions I SDA: 228 SDB: 228 CA: 228 I RCS Temperature (0 f):TR~F !1 Power Level C?. F.P.):-40 Other Cspeci::fy) (Design) I CB 228 cc : 228 en: :s: I. Must have~ 40 thimbles I I III I Bank Positions (Steps) I Test I I Conditions I SDA: 2'2.8 SDB: .z..z..B CA: iz.s I RCS Temper a ture C ° F) : 5"S"o cp Power Level (7. F.P.): 3Zio Other CSpeci:fy): (Actual) IV .Jl'est Results I I I I I I I I I I I I I CB : 2.2.8 cc : Z..z.8 en: l~O I I Date/Time Test: I 4-i Th -im b Jes Per:Eormed: t-/8/8! / 1ss-3 I I MAX. REL I HUC EHTHALITOTAL HEATI QUADRANT Meas Parameter! ASSY PWR I RISE HOT I FLUX HOT !POWER TILT (Description) I 7. DIFF I CHAN FACT ICHAH FACT I RATIO I CH-P)/P I F-dHCH) I F-2CT) I QPTR ---------------' '------' '------. 1-,% ~z.= o.,t1 I I Measured Value I .,, r I ;,423 I z. / 84-. I /. ()/33 ------------ i-'*~ ;,,.-~-I.: 0.6~ T I I _____ _ I~ Design Value I :1io::: for l'i .2. *9 I I I I (Design Conds) I :1t 5% to-r Fi< *9 I HA NA I S 1. 02 I -I (P *

Any. Pv?-,) I I --------------

1 WC AP -7905 I IWCAP-7905 Re:ference I REV . 1 I HONE HONE I REV. 1 ---------------------!

I I _____ _ I I I V Acceptance C:2:iteria FSAR/Tech Spec I NOHE I ~s1.s5C1+.2C1-P>> F~C:n~4.J6 z iccz> I HA _______________ I I I _____ __ I I I Re:ference I HONE I T. S. 3. 12 T. S

3
12 I T
S. 3. 12 I I I ----------------------'

I '-------VJ: Comments Completed B Design Tolerance is met Acceptance Criteria is met

Above Insertion Limits A. 16 VYES _xo ./ YES _:_xo Evaluated By: Recommended

fol: Approval.

F:Y MFO Enginee.i: -. <

, . .. ~~-------~

JUL . 3 1981 SURRY POWER STATION UNIT 1 *CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I *Re:ference II Test Conditions I .(Design) I Test

Description:

M/D Flux Map -At Power. NI Calib. Proc Ho/ Section: PT28.2, OP-57

Sequence Step Ho= 4G, Bank Positions (Steps) SDA: 228 SDB: 228 CA: 228 CB 228 CC : 228 CD: x RCS Temperature C°F):TREF

1 Power Level CX F.P.l=-50 Other Cspeci::i:y)

Must have~ 40 thimbles ------'-----------------

III I Bank Positions (Steps) Test ! ________________ _ RCS Tempe:z:ature( °F): TR.EF! I Powez: Level C 7. F. P. ) : ..,..47°7o Other CS~eci:fy): Conditions I (Actual) I SDA: 1.:2.& CB : 2.2% SDB: _1.1~ cc : ").:i.8 CA: '1.2.'?° cn:nCJ/,~o LI o Th ,* ..... b ks :IV Test Results Da.te/Time Test:* Pei:£01:med: 7/'i/%1 tlAX. REL Heas Pai:ametei:1 ASSY PWR (Description) I X DIFF I Ctl-P)/P ________ I ! . I +s:,"lo .f.r P~,q0.9(. I Measured Value l+s:i-, r-_ n :o.uu I

i/o~ rLI'~ ,, --------Design Value 1::io:forPi.2..

9 C Design Conds) I ::t 5::t fol' Pi< *9 --------I CPi. #Jay. Pvr.> 1 'WC AP -7905 Reference l REv.*1 ------_________ I ____ _ I V FSAR/Tech Specl NOHE Acceptance--------'------ C~iteria I I I Refe~ence I NONE I *1 HUC EHTHALITOT;tL HEAT RISE HOT I FLUX HOT CHAN FACT ICHAH FACT F-dHCH) I F-Q(T) I. YS'I f.9'3>0 NA .. HA NOHE NONE ~Hst.SS(l+.2(1-P)) F~Cz.>i;1 8 X J;(Z.) T.S. 3. 12 T.S. 3.12 QUADRANT POWER TILT RATIO QPTR 1.0lll/ s 1. 02 WCAP-7905 REV. 1 HA T.S. 3. 12 --------' '--------------------------- 1 I I Design Tolerance is met Acceptance C;ite~ia .is met _LYES _HO /YES __ NO VI: '---------------------------------------------- Comme~ts I I I

Above Insertion Limits ------'---~--:---~-----==-------------------:--------:-----

Eva1uate d By* ~Jl. ,C~~ Completed A.17

Recommended for --;-) // / !7 / Appx:oval By : .-..k_;(..t._v._/_...h,

... NFO Engiieex:

-----i -*"' "' !*

-'\ JUL 3 1sa1 SURRY POWER STATION UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AHD EVALUATIOH SHEET Test Descr:iption*: M/D F1uK Map -At Pouer:. KI Calib. 'I Re£er:ence Pr:oc Ho/ Section: PT28.2. OP-57 Sequence Step Ho= 47 II Test Conditions I (Design) I Bank Positions (Steps) SDA: 228 SDB: 228 CA: 228 CB : 22a cc : 22a en: % RCS Tempe~atu%e C°F)=T~EF t1 Poue:z: Level C?. r.P.):-60 Othe:z: (speci::::y) Must have~ 40 thiDbles -----'----------------

III I Bank Positions (Steps) Test 1-------------------- RCS Tern Per: a tu:z:e ( ° F) : ...., -56Z '"'!= Pouer: L~vel C~ F.P.):57%. Othe:z: CSpeci:y): Conditionsl SDA: zzS SDB: z.z.S CA: Z.'Z.S cc : *u .. s CD: , 1-s (Actual) I CB :z~g _____ r _______________ _ +I T/i,*ml,le~ I I I I 'IV I Test Results Date/Time Test: Per::for:med: 1 /1a/ 8/ j Z 00.f:> I MAX. REL I HUC EHTHALITOTAL H~ATI 2UADRAHT Meas Par:ameter:l ASSY PWR I RISE HOT I FLUX HOT !POWER TILT CDescr:iption) I 7. DIFF I CHAH FACT ICHAH FACT I RATIO I CM-P)/P I F-dHCH) . I F-2CT) I 2PTR ________ ! I I I _____ _

1-1-.+t fw. ':-r= o.1s-l I . I Measur:ed Value:-s.,i{....fy.fMf:

/,4S"/ : /. 'f8(,. : /.OO?~ * *Design Value 1::1o:forPi 2" 9 I I I *cnesign Conds)l~lS%forPi<. 9 I HA I HA I s*1.02 . (pi

Auy. ~.) I I I ---~--WCAP-7905 I I IWCAP-7905 P..e:fe:z:ence REV.1 I NOHE l HONE l REV.1 --------------------

_______ ! l I ______ _ I I I FSAR/Tech Spec HONE NA V Acceptance C:cite:cia I ;M:.l!sl.SS(l+.2(1-P)) I F~(z>s\18 x xcz> I ---------* I I I _____ _ I I I R.e:fe:rence HONE I T.S. 3.12 I T.S. 3.121 T.S. 3.12 I I I ------* I I I '------------I-Design To*le:rance is met --I Acceptance Cr:ite:z::ia is met ~YES HO VYES =HO VI '-------------------------------------------------------------- Comments I Above Inser:tion Limits I I ------'-----.---..,...---------------------------- Completed Byr: >< I /-, *.* ~. A.18

Evaluated By: Recommended

£01: App:z:oval By : J. ,.I. r,Zl(,_ C.,1~ NFO Engineer:

-.. I I i . -* I I

, JUL 3 1'81 I SQRRY POWER STATION UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I P.e:fe:z::ence II Test Conditions I (Design) I Test Desc::ciption

M/D Flux Map -At Powe:z::, NI Calib. P:z::oc }{o / Section: PT28. 2, OP-57 Sequence Step Ho: 4 B Bank Positions (Steps) SDA: 228 SDB: 228 CA: 228 CB 228 CC : 228 CD: x RCS Tempe:z::atu:z::e C°F)=T~Ef

1 Powe:z:: Level CX F.P.)=-70 .othe:z::

Cspeci:fy) Must have~ 40 thimbles -------'----------------- ___ ,_. ------------- III I Bank Positions (Steps) RCS Tempe:z::atu:z::e{ °F): ,,.,5(;::, GF Power Level C:'. F.P.): ~5'%

Othe:z:: C Speci:f.y)

Test '---------------------

Conditions I SDA: ZZ.8 CB : 2.2-8 SDB: Z.Z.8 CA: 2U3 cc= en= ~oo (Actual) I -----'------------------- ' Date/Time Test: I Pe::c:fo::cmed: , 1 I. / I ?!(418'/ . OeJZ.4-'-----------------------

1 I MAi. REL I HUC EHIHAL TOTAL HEATI QUADRANT IV l Meas Pa:z::amete::cl ASSY PWR I RISE HOT FLUX HOT !POWER TILT Test Resu1ts V (Desc::ciption) I X DIFF l CHAN FACT CHAH FACT I RATIO I CM-P)/P I F-dHCH) F-Q(T) I QPTP. -------------'

____________ , _____ __ 1-~ .f.... ~-z 1.00 I I Measu: :ced Value: .. '1,1.'f.~P.t.,o.,'fl

/.435° /.1/8 : /.0//r ------------

Design Value. ( :tlO::: for pi 2 *9 I (Design Conds) :!lS:t for Pi< *9 HA NA I S 1 02 Re:fe::cence .FSAR/Tech Spec (pi

Auy. Pvr.) I ------WCAP-7905 REV. 1 HONE IWCAP-7905 HOME I HONE I REV. 1 -------'---------'------

' I _N * --I T 2.18 I HA Acceptance I _________

*i11.s.1.55(1+.2(1-PD FQ(Z):.-l'-

x K(Z) . '-------'------ C::cite:cia I I Re:fe1:ence HONE T.S. 3.12 IT.S. 3.12 I T.S. 3. 12 I I -----------------------

' '--------v:r Comments Completed B Design Tole:cance is met Acceptance C:z::ite:cia is met = Above Inse::ction Limits ' . A.19 ./YES _NO ;_LYES __ HO Eva1uated By: Recommended

fo?: App:coval By c.:J~ NFO Engineer .1 JUL 3 7987 SURRY POWER STATIOH UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATIOH SHEET I Refe:cence II Test Conditions (Design) III Test Conditions (Actual) IV Test Results Test Desc:ciption

M/D Flux Map -At Powe:c, HI Calib. P:coc No / Section: P-TZ8. 2, OP-57 Sequence*

Step Ho: 4 C\ Bank Positions (Steps) SDA: 228 SDB :* 228 CA: 228 RCS Tempe:catu:ce C°F):TREF +/-1 Powe:z:: Level(~ F.P.)=-90 Othe:r (specify) CB 228 cc : 228 en: :s: Bank Positions (Steps) SDA: 2.2..% SDB:22~ CA: 2.2..8-CB : 2.2.S-cc : 2.2.~ CD: *u:J'-f Date/Time Test:/.;/ Pe:z:::fo:cmed: 7 14 'if , , ,_, MAX. REL Must have~ 40 thimbies RCS Tempe:ratu:ce C ° F) :T~ t I Powe:r Level (~ F. P.) =-is-% Othe:c CSpeci:fy): 4 I Th;,.,..bl e..s NUC EHTHALITOTAL HEATI QUADRANT Meas Pa:camete:c! ASSY PWR RISE HOT I FLUX HOT !POWER TILT CDesc:ciption) I 7. DIFF CHAH FACT !CHAN FACT I RATIO I (?1-P)/P F-dHOO I F-QCT) I 2PTR -----------'

' '------1c..s%~rP1t-~1,01 I J I1easu:ced Value I,~"",. P. ~0 ,,~ l.*1-fZ.I I l.~'2...%

I l,Ol7-___________ l,.,1r,oto<" ~-I "'O ______ f I _____ _

Design Value I ~io: £or Pi 2 *9 I* I (Design Conds) I :is: for Pi< *9 HA I NA I S 1. 02 --------'\'.Pi*

bay. ?wr.) ------' '------JWCAP-7905 I IWCAP-7905 Re:fe:z::ence I REV. 1 NOHE I HONE I REV. 1 -------------'------

' '------1 I I V FSAR/Tech Spec I HONE ~8~1.ssc1+.:ZC1-,>>

I r~CZ>s-\;1-8 x KCZ) I Acceptance---------'------- _________ I I ______ __ HA C:cite:cia I I I I I Re:£e:cence I NOHE T. S. 3. 12 I T. S. 3. 121 T. S. 3. 12 I I I I ______ I I I I _____ _ I I I Design Tole~ance is met Acceptance C:z::ite:cia is met : /YES _MO ./ YES __ HO VI I _________________________________________ __ Comments I I I :s: Above Inse:ction Limits ------'----,,--,.---,,....-----------------~--------- Completed A.20 Evaluated By: Recommended £0:c * . / / . ..-;--7 / App:toval ~Y : ,JU;/~/~/ NFO Eng*i.nee.r: -*' JUL 3 1981 SURRY POWER STATION UNIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I Re:Eerence II Test Conditions (Design) II! Test Conditions (Actual) IV -?est Resul.ts V Acceptance Criteria v:r::"

Comments Test Desc::ciption:

M/D Flux Map -HFP, ARO, Eq: Xe. Map P::coc No/ Section: PT28.2, OP-57 Sequence Step No: 5D Bank Positions (Steps) SDA: 228 SDB: 228 CA: 228. CB 228 CC: 228 CD: x RCS Tempe::cature C°F):TREf =1 PotJer Level C?. :r.P.): 100 Other (specify): Eq. Xe. Must have~ 40 thimbles Bank Positions (Steps) SDA: ~,;). 8 SDB: .l..). 0 CA: ~i,l. 9 CB : ;)._J-8 CC :~.). 8 CD: ~;J..8 RCS Temperature C ° F): T,..11¥' +/- l Power Level C?. F .P.): Joo t.' Other (Speci~y): ' '-/~ Th;ft'ble-s Date/Time Test: Performed: ?'/ ~1(8! 01'{1 I MAX. REI. I Meas Parameter! ASSY PWR I (Description) I 7. DIFF I I CM-P)/P I NUC EHTHALIT~TAL HEAT RISE HOT I FLUX HOT CHAN FACT !CHAN FACT F-dHCN) I F-2CT) --------' '------------ 2UADRANT POWER TILT RATIO 2PTR 1-C{. g Z f'oc-f:D-111 I Measured Value I :r--~ I J '-/ I 3 I. 'ii O f .O/ o _______ -_t*S.71.-t. .. :, "'0.~------

..... --Design Value I ,no: for Pi 2 *9 (Design Conds) I :is: £or Pi< *9 I (pi* Asay. Pvr.) --------1 WC AP -7905 Reference I REV. 1 NA HA HONE NOHE S 1. 02 WCA.P-7905 REV. 1 --------'------

' FSAR/Tech Spec! NONE I I Reference I HONE I I Design Tolerance is met Acceptance Criteria is met

Above Insertion Limits r'.6llsl.55(1+.2Cl-P))

r~cz,s?/8 s 1'(i) NA T.S. 3.12 T.S. 3.12 T.S. 3.12 Compl~ted BY, Evaluated By: A,21 Recommended

for Approval By : NFO Engineer --.

JUt s rsa 1 5u..r~ POWER STATIOH UHIT 1 CYCLE 6 STARTUP PHYSICS TEST RESULTS AND EVALUATION SHEET I. Refe:rence II Test Conditions I (Design) Test

Description:

RCS Flow Measurement P:roc Ho /Section: ST-52 / Sequence Step Ho: 5 / eTA-4,ooo.:z. Bank Positions (Steps) SDA: 228 CB: 228 SDB: 223 cc: 228 CA: 2 2 8 en: AR RCS Tempe:ratuz:e C°F)=T~ !1 Power Level(~ F.P.):95 +5/-0 Otli.e:z: (specify): III Test Conditions C A.ctual) Bank Positions (Steps) SDA: Z,.?..S SDB: 2.2.s CA: '2.2.8 RCS Ternperatu:re C ° F): 574°F /SIDC/ cp PotJe:z: Level C?. F. P.): /Oo%, Othe:r (Specify): IV Test Results V Acceptance Criteria CB: Z.l .. S cc: Z.2.8 en: A-9-Date/Time Test Pez:formed: B-G,-8 I 0946-/34-5 Meas Parametez: CDesc:z::iption) Measu:z::ed Value Design Value (Actual Cond) Design Value (Design Cond) Refez:ence FSAR/Tech Spec Re:fe:z::ence I I I I I I I I I I I I I 1 I I I I I *I FTam.~ , Total RCS Flou Rate r Tc:1rAL.. = ::z. q \ > 1 o B '\.~ ""' Hot Appl.icabl.e Hot Applicable Hot Applicable FTbTA.L / 1. 02 Cmeas unce::cty) 265,500 gpm !SAR Section 4.1.3; Letter from J. H. Ferguson(Vepco) to H. R. Denton(NRC) dated April 28, 1981 (Serial No. 232); Letter from C. M. Stallings(Vepco) to E.G. Case(NRC) I dated November 16, 1977 (Serial Na. 516) 1 ----------------

VI: Comme*nts 1 I Design Tolerance is met I Acceptance Criteria is met ;,YES _HO __ YES _HO '---------------------------------- ' I I Completed By: µl,,i,t_ ct Evaluated By: ti: zztt:.v' ______ , ____ ,..._...,... __ _,~------------------------ f'est Engine~ A.22 .,. ~~-------------------~~-, NOTICE -. THE ATTACHED FILES ARE OFFICIAL RECORDS OF THE DIVISION OF DOCUMENT CONTROL. THEY HAVE BEEN CHARGED TO YOU FOR A LIMITED TIME PERIOD AND MUST BE RETURNED TO THE RECORDS FACILITY BRANCH 016. PLEASE DO NOT SEND DOCUMENTS CHARGED OUT THROUGH THE MAIL. REMOVAL OF ANY PAGE(S) FROM DOCUMENT FOR REPRODUCTION MUST BE REFERRED TO FILE PERSONNEL. DEADLINE RETURN DATE p/P/ RECORDS FACILITY BRANCH}}

ML18139B520

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g:; steps) I~S = 555 100 pcm CC:ritical Ref Bank Position

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ML18139B520

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SUMMARY

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Reference:

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g:; steps) I~S = 555 100 pcm CC:ritical Ref Bank Position

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