ML18092A210

Cycle 2 Startup Test Rept

ML18092A210
Person / Time
Site:	Salem
Issue date:	05/15/1984
From:	Jackson J, Liden E Public Service Enterprise Group
To:	Murley T NRC OFFICE OF INSPECTION & ENFORCEMENT (IE REGION I)
References
NUDOCS 8406280321
Download: ML18092A210 (38)

Text

(

SALEM NUCLEAR GENERATING STATION 8406280321 840515

• PDR ADOCK 050003'11 P

PDR UNIT 2, CYCLE 2 STARTUP TEST REPORT

.e PUBLIC SERVICE ELECTRIC AND GAS COMPANY

~

SALEM NUCLEAR GENERATING STATION UNIT 2 CYCLE 2 STARTUP TEST REPORT

,e List of Tables and Figures Table 1 Sequential List of all Tests Table 2 Swap mode rodworth comparisons Table 3 Dilution mode rodworth comparisons Table 4 Summary of Flux Map Results Figure 1 Reactor Core Map Figure 2 Burnable Poison Loading Pattern_

Figure 3 Flux Map 2200 FDH and Tilts Figure 4 Flux Map 2201 FDH and Tilts Figure 5 Flux Map 2202 FDH and Tilts Figure 6 Flux Map 2203 FDH and Tilts Figure 7 Flux Map 2204 FDH and Tilts Figure 8 Flux Map 2205 FDH and Tilts Figure 9 Flux Map 2206 FDH and Tilts Figure 10 Flux Map 2207 FDH and Tilts Figure 11 Flux Map 2208 FDH and Tilts Figure 12 Flux Map 2209 FDH and Tilts Figure 13 Rod Bank Insertion Limits versus Thermal Power Appendix A Physics Test Program Descriptions and Acceptance Criteria/Physics Results Sheet

Introduction The fuel shuffle commenced February 20, 1983 and required the removal of 193 fuel assemblies from the core.

The core unloading was completed 5 days later on February 24, 1983.

During the shuffle reactor engineering personnel with the assistance of Q.A.

and fuel management group personnel conducted a fuel assembly inspection.

This inspection identified grid strap damage to fuel assembly N18.

It was determined that the damage occurred in the

.Control Rod Change-fixture.

The determination was made by inserting the "DUMMY" Fuel assembly in the suspected Control Rod Change fixture and noticing the damage to the "DUMMY"'s grids when it was withdrawn.

A piece of weld splatter was found in the Control Rod change fixture and removed.

Fuel Assembly Nl8 was unusable and a new core design was done in order to use a replacement.for Nl8 and its symmetric fuel assemblies.

A lower core plate inspection and loose parts retrieval was conducted.

One small piece of unidentifiable debris was removed from the core support plate.

Otherwise, the core appeared very clean.

The core reload was started on March 23, 1983 and was completed on March 27, 1983.

A total of seventy-two* (72) new assemblies were lo.:;tded.

The new assemblies are located in.the core as indicated on the Core Loading Map, Figure 1.. Four Secondary source clusters were loaded into locations H-3, H13, D6, and MlO.

Sixteen depleted burnable poison rod inserts for a total of 304 rods and sixteen fresh burnable poison rod inserts for a total of 240 burnable poison rods are located as shown in Figure

2.

Three different burnable poison cluster patterns with 12, 16, and 20 rods were used.

Page 1

The startup physics_ test program was conducted to ensure the reactor, as loaded, was performing in accordance with design expectations and safety limitations.

Hot zero power tests were performed on July 23, July 24, and July 25, 1983.

Power escalation testing was started July 30, 1983 but was not completed until March 14, 1984 due to stator water cooling leaks in the generator and their subsequent repair.

A special flux map with. banks."D" and "C" *in was taken during zero power physics testing.

The map number is MAP 2200.

This map resulted from the concerns of the PSE&G Nuclear Fuels Group (NFG) in regards to a potential violation of the F& H Technical ppe.cif ication for low power rodded operation at the beginning of the cycle.

The results from this Map verified NFG's concerns and a special set of administrative rod insertion limits (more conservative than those in the Technical Specifications) were given to Operations.

The limits are shown in Figure 13.

Appendix A provides a brief description of each test and a summary.of test results relative to acceptance cr_iteria.

Table 1 is a sequential listing of all tests that were conducted during the startup.

Page 2

TYPE.

Reactor Startup

1.

Zero Power Physics Testing

2.

3.

4.

5.

6.

Power Escalation Testing

7.

8.

9.

10.

11.

12.

13.

14.

15.

16.

17.

18.

TABLE 1 STARTUP TESTS Post refueling Initial Criticality Pull control banks with ICRR Plot Dilute to criticality Reactivity computer checkout ARO Boron Endpoint Test ARO Isothermal Temperature Coefficient Measurement Rod Swap Reactivity Measurement (Rodworth)

Bank "D" and "C" in Flux Map (#2200))

Flux Map Analysis and Results for NFG ARO Flux Map (#2201)-Flux Map Analysis

& Results Heat Balance and NIS Calibration Heat Balance and NIS Calibration Flux Map #2202 Flux Maps #2203, 2204 Excore Calibration Flux Map #2205 for Fxy Surveillance Heat Balance and NIS Calibration Flux Maps #2206, 2207 Flux Maps #2208, 2209 Excore Calibration Power Coefficient Measurement RCS Flow Measurement 26% RTP 47% RTP 47% RTP 47% RTP 47% RTP 75% RTP 75% RTP 100% RTP 100% RTP 100% RTP 100% RTP 100% RTP Page 3

R p

N 11 L

P06 Pl>298 1

P13 P46 P48 PD246 RUD 20P.66 P32 P01 H<48 L06 PDJDS 20P72 PD337

. R68 3

P15 H16 H4S P61 R136 PD221 R70 16P89 4

P72 P49 L3B P<4S N12 PD232 20PBO R79 16PB6 PD322 5

P31 1164 11S6 N04. 1154 PD282 R72 PD331 PD135 PD224 6

P38 N25 N3B N06 N24 PD2SS PD312 R147 PD2'40 PD233 7

8 P07 1111 N16 11<42 P70 PD268 R152 16P79 R62 16P92 PU N64 N09 N53 N40 PD133 PD307 R130 PD239 PD23B 9

P16

• 1106 1137 N30 1128 PD205 R121 PD336 SS6 PD225 18 P42 P64 LD9 P39 N22 PD324 20P7S R139 16P84 PD223 11 P19 110'4 H1B PS1 R66 PD204 R151 16PB1 12 P04 P02 1151 L02 PD304 20PB3 PD329 R77 13 P66 P6B P25 PD262 R73 20PB1 14 15 P34 PD296 REACTOR SALEM DATE*

K PJO PJS PD31'4 Pl>271 H60 N21 Ri19 PJ>270 H19 N'43 PD277 R76 N61 N27 Pl>261 P,D242 H'47 N37 PD20B PD236 NS6 H23 R104 PD230 1113 P60 PD214 12P31 N23 N59 R126 PD206 1102 P23 PD207 12P30 N35 1110 R106 PD273 HOB N07 PD318 PD237 N03 N44 PD228 PD219 1125 N14 PD294 R140 1143 N54 R153 PD267 P18 P05 PD254 PD285 CORE MAP UN::lT 2

3/2?/B:3 H

G F

PSJ PSS P03 PD216 Pl>210 PD2'47 H07 N62 HJO R117 PD245 R67 N36 NSO 1103 SS4 R64 Pl>2S3 H20 N26 NU R116 PD201 PD333 PS7 NS2 H46 16P90 PD235 PD213 N32 1101 N17 RSO PD203 R65 NS1 P62 111S PD244 12P29 PD2SO L34 N15 N02 R146 PD220 R71 N33 P37 1133 PD202 12P32 PD231 N57 1131 N46 R74 PD21B R69 P17 N60 1129 16P91 PD243 PD27B 1152 N29 N55 R125 PD241 PD212 N48 NSB 1141 SS3 R144 PD136 1117 N28 1134 R75 PD299 R109 PSS P41 P33 PD209 PD264 PD290 NORTH t FJiGURE 1 E

D c

A P67 PD281 P<40 P4<4 P29 2DP82 R129 PD338 L62 11<49 P52 P27 R1<41 PD286 20P67 PD279 P59 11S7 H22 PSO 16P85 R138 PD33S R63 N13 Pl4 L16 P63 P12 PD24B 16PS2* R113 20P74

~D138 11SS ND1 HOS 1150 PS6 PD30B SSS PD317 Ri14 PD334 N2D N45 N34 N42 P71 PD234 PD21S R103 PD276 PD226 POB 1109 N63 1153 P22 16P67 R124 16P7B RiOB PD2S7 N41 N49 N39 NOB P36 PD222 PD252 R1*35 PD211 PD284 1139 N31 1114 1112 P54 PD229 PD302 PD227 R111 P1>274 N10 P28 L19 P10 P09 PD272 16PB3 R134 20P61 PD297 P6S

' 1144 11'40 P20 16P88 R118 PD320 R78 L39 1121 P26 P69 R142 PD265 20P56 PD311 P24 P47 P'43 20P54 R101 PD275 P21 PD280 Page 4

R p

N M L 20*

20*

16 20*

16 REACTOR CORE MAP SALEM UNIT 2 DATE 3/27/83 K J ti

~

180° F

E I

20*

4S 16*

16 16 12 12 D.

C B

20*

16

• ' 20*

45 90° --

16*

16 16 16*

12 4S 20*

16.

16 20*

20*

nn -.Number of Burnable Poison Rods 45 - 4*secondary Source Rods 16 4S ln*

I o~

FIGURE 2 12 16

. 20*

16 20*

20*

• - Indicates Depleted Burnable Poison.Rods BURNABLE POISON LOADING PATTERN A

1 2

3 4

5 6

7 8 270° I

9 10 11 12 13 14 15 Page 5

Zero Power Test Results The zero power test schedule for Cycle 2 was essentially identical to that done for Unit 1 Cycle 5.

The rod exchange technique was used for measuring the bank rodworth rather than the traditional boron dilution method.

Comparisons of swap mode rodworth measurements and design values along with review criteria are shown in Table 2.~

Comparisons of dilution mode measurements and design values along with acceptance criteria are shown in Table 3.

A Boron end point measurement was conducted-with all rods out and was within the +/- 50 ppm acceptance criteria.

The measured value of 1261 ppm was 44 ppm lower than predicted.

An Isothermal temperature coefficient measurement was performed with all rods out.

The value obtained was very close*to the predicated value and well within tolerances.

Results of the*zero power flux map (#2201) are.shown in Table

4.

A tilt in the power distribution of 2.3% was discovered in the N.W ** quadrant and the resulting peaking factor Fxy e~ceeded the full power Technical Specification limits, but was below the zero power limits.

The observed tilt was within the range p:redi,cted by the Fuel Vendor (Westinghouse)

• MAP 2200 was t~ken to support NFG's contention that the quantity F6H may violate the Technical Specification for low power, rodded operation at BOC. The vendor's evaluation of this potential violation on the appropriate accident analysis showed that there would be no adverse effects.

NFG analyzed that the potential cause for the violation would be a radial, in-out flux tilt.

Page 6

The results of MAP 2200 (Figure 3) confirmed the existence of the radial tilt. Administrative limits on rod insertion were imposed to ensure that F6H would not be violated for low power rodded operation (See Figure 13).

Page 7

TABLE 2 ROD SWAP MODE ROD WORTH RESULTS ROD TEST.

MEASURED DESIGN TOLERANCE INTEGRAL VALUE BANK CONDITIONS WORTH (PCM)

PSE&G *(PCM)

(PCM)

Dil 878 841 84 D

+/-

c Swan 770 731

+ 110 B

Swap 660 626

+/- 94 A

Swan 251 210

+/- too SD Swap 299 294

+/- 100 SC Swap 292 290

+/- 100 SB Swap 787 759

+ 114 SA Swap 562 518

+/- 100 TOTAL BANKS Swap 4499 4269

+/- 427 REVIEW CRITERIA

1.

Individual control and shutdown bank worth 6% < 15% for banks ~ 600 pcm except for reference Bank 6% <10%

6% < 100 pcm for banks <600 pcm

2.

Total of all Control and.Shµtdown Banks 6% < 10%

where 6% = measured-design x 100%

design Page 8

TABLE 3 DILUTION MODE ROD WORTH RESULTS MEASURED VENDOR ROD TEST INTEGRAL DESIGN BANK CONDITIONS WORTH (PCM)

VALUE (Pr'Ml CONTROL ARO D

878 896 CONTROL c

CB D IN 728 884 CONTROL B

CB D, c IN 1076 1046 CONTROL A

CB D,C,BIN 184" 267 CONTROL

+SD SUM(TOTAL N/A 6374 6455 ACCEPTANCE CRITERIA 1.* IndiVidual control and shutdown bank worth 6% < 15% for banks ~ 600 pcm 6% < 100 pcm for banks <600 pcm

2.

Total of all control and Shutdown Banks b.% < 10%

where 6% = measured-design = 100%

design TOLERANCE

( P("M)

+/- 134

+/- 133*

+/- 157

+/- 100

+/- 646

• PSE&G Nuclear Fuels Group pr~dicted that the presenbe of a radial tilt might cause an individual bank-worth to deviate from the Westinghouse design predictions by more than the acceptance criterion of +/-

15%,

however, there is a negligible effect on total bank worth associated with shutdown margin.

Page 9

FIGURE 3 HEASURED AND PERCENT. DIFF, OF FDHN BALH INCORE HAP2200r2.S% PWk,BK CIDI0*1168PPHrOHWD/HTUrPT.43 I

2 3

R P

N, H

L K

J H

BF ED C

8

• 1.223. 1.368. 1.157, 6.4.

2.4.

• 1.322. 1,774, 1.129. 1.199, 1.060.

10.3.

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1,5,

• 1.310. 1,954, 1.247, 9,4,

• 1.740. 1.224.

8.4.

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-.a....

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• .3.

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-9.1, -10.1. -11.s. -11.0. -11.9. -10.9. -10,3, -10.0.

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-6.6.

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,5, 3,y, SALH INCORE HAP2200.2.sz PWk.BK Cll!t0.116BPPHrOHWD/HTUrPT.43 CALCULATED POWER TILTS CNDRHALIZED TO 1.000>

1.0234,1.0482 1.0359

.9913 1.0429

,9593

• 1.0376

.9300

.9006 *** 1.0697

.9147

• 1.os11

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.9829 POSITIVE -X-VS, NEGATIVE -X-TILT t.0470

.9530 1.0536

, HEAS,

, l!lF F,

Page 10

FIGURE.4 MEASURED AND PERCENT. DIFF. OF FDHN IALK INCORE KAP2201t2o5% PWRtBK Dl220t1360PPK*OKW~/KTUtPT.42.~1 R

P N

K

• oL * *.K

,J oH,,.a,, oF,, oE,,

D C

D A

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,799, 1

7.o.

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4,5, 3,3, 4,0, 4,5, 4,5, 2

3

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• • 27. 1.154, 1.252, 11.e.

11.7.

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~*51 317.

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• 4o3o 715.

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• 1e1. 1.041, 1.075, 09730 1.172. 1.271. 1.176.

-.2.

1.7.

2o2o 2.00....

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I 1740. 11166

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, HEAS,

, DIFF,

SALK INCORE KAP2201t2o5% PWR.BK D*220.1360PPKtOKWD/KTUtPTo42t41 CALCULATED POWER.TILTS <NORMALIZED TO 1.000)

• 1.0461olo0355 0 100007 *

.9854 1.0234 0 100104 1.0408 09697 19887 198::.2 o9664olo0075 0 19681 I

P08ITIYE -v-*ue. NEBATIYE ~Y-TILT.

1.0169 19831 PD8ITIUE -X-US, NEGATIVE -X-TILT 1.0043

,9957

.9981

.9870 19870 Page 11

f. :Ct.:4?.o °Fb1AJC:e MllP5 Poe 1A.Jr::oof/J1.V....

+

1

+ The burnup indicated in this table is the core average burnup.

In order to obtain the burnnup relative to the beginning of the cycle being zero burnup substract the core average burnup at the beginning of the cycle 9859.l from the burnup indicated in this column.*

1-3

i::i to -

t:-t ttj

.i::.

l"rj t:-t c:::

x:

~

i::i

~

GJ

(/]

c:::

t:-t 1-3 (fl (fl

~

i::i e

0 K!.

Power Escalation Testing Power was increased to approximately 20% RTP on July 29, 1983 and held there eight hours to heat soak the turbine.

July 30, 1983, on the way down from the turbine soak the reactor tripped on Hi-Hi Steam Generator level at 11% power.

The reactor was taken critical that same day and after reaching 20% power

• started a 3% RTP per hour ramp rate.

On July 31, 1983 the unit reached the 47% RTP testing plateau.

During July 31, 1983 three incore flux maps were conducted in order* to obtain data for an excore calibration (maps

1. 2202-2204)

• Peaking factors for the maps (except Fxy obtained at the 47% RTP level) were found to meet the full power limits and the quadrant power tilt had d:i..minished to approximately 1.0% in the NW quadrant.

Only one map violated the full power Fxy limits.

MAP2207. Another map was scheduled to be taken at 72% power per the Technical Specifications in order to verify that Fxy was within the full power limits.

Note that Fxy was within the 47%

Power limits.

The target Axial Flux Difference (Delta I) was determined to be 0.0% and this value was set into the instrumentation.

Preliminary data evaluation at the 47% RTP level was conducted and power escalation at 3%/hr was started on August 2, 1983.

Page 13

Power was stabilized at 72% RTP and a heat balance for NIS calibration and a flux map for Fxy surveillance was taken.

MAP2205 (Figure 8) result showed all peaking factors including Fxy were within the full power limits.

Power was stabilized at

~99%

RTP and four flux maps (#2206-2209) for an excore calibration were obtained between August 8 and August 11.

The peaking factors obtained with these maps were within the full power limits.

The quadrant power tilt was approximately 0.6% on these full power maps.

The unit tripped on August 11, 1983 before reaching equilibrium poise~ conditions due to high river tides carrying grass which clogged up the travelling screens and tripped the circulators.

The unit was taken critical again on August 16, 1983 and reached full power on August 17, 1983.

On August 19, 1983 the unit was shutdown due to a Hydrogen leak to the stator water cooling system.

The problem was repaired and the unit was taken critical on September 24, 1983 and reached full power on September 28, 1983.

On October 3, 1983 while taking tests, the unit reduced power due to feed pump suction pressure problems.

The unit was back at full power on October 4, 1983 but reduced power on October 6, 1983 due to a transmission line being out of service.

On October 7, 1983 the unit was shutdown due to a Hydrogen leak in the stator water cooling system.

The unit went critical agin on March 4, 1984 and reached full power on March 11, 1984.

The Power Coefficient measurement was done on Mar~h 14, 1984 and a value of ~11.33 PCM/% was obtained.

Page 14

This value was compared to the FSAR limiting curves and founa to be in the acceptable region.

The State Point Data collection and subsequent RCS flow calculation were completed on March 15, 1984 with a measured flow of 370054' gpm.

The measured value exceeds the minimum 100% RTP required flow in the Technical Specification of 361000 gpm.

Page 15

FIGURE 5 HEASURED AND PERCENT, DIFF, OF FDHN SALH INCORE HAP2202,48,332% PWR,BK Dl1B9*11B2PPH*18HWD/HTU,PT.45*44 1

2 3

4 5

• 6

• R P

N H

,,L,

,K

,J

,H,

,G * *,F,

,,E,

D C

B A

-.846. 1.249, 11.6.

18.1.

• 1.114, 12.2.

~*------....... ~

• 804. 1.112.

7,7, 4,1.

,970.

3.6.

.152.

.966. 1.010. 1.028. 1.019,

.996.

,794,

,5, 2.e.

1,9, 2.2.

2.1.

6.1.

6.1.

1.135.

,919, 1.053,

,977, 1,041,

,912. 1.150,

.eo4.

,5, 2.6.

_,...,.,_ _ _.,.. :.o..11..t_i..*!..-....:":.:.:*3:'..,

1.9,

.1,9, 11.8.

..~....

• 773.

.896. t1.134. 1.136. 1.126.

.869.

• 749-;-*-~16.

.184.

~-~

.804.

..2.s.

,994,

..3,7,

.. :7 *

• 6,1.. 2. 7,

.. 3,9,

.. 3,5, r:2,4.

r:2. 4.

r:2. 5.

11. 9.

l~I I

t I

I I

1*

1.010. 1.020. 1.129.

,931. 1.140, 1.003,

,993,

,771.\\

11.e.

1.os6.

)

.. 1.0.

..1.0.

..5,3,

..5,3,

.. 4,4,

.. 2.6.

..2.1.

..,9, 6_... 3_._~

1.064.

.. 2.e,

,993, 1.113. 1.168. 1.111.

,985. 1.064. 1.001.

..3.0 *

.969. 1.110.

.. 3,9,

-1.6.

.. 4,5,

.. 4,1 *

,990. 1.121.

..3,9,

.. 3,1,

.. 4.1,

.. 2.8.

,993, 1.1s2.

..4,5,

.. 5,0.

..2.e.

..1.0.

,959, 1.001.

-4.9.

-2.0.

.762. 1.120.

• . -.3.

-.s.

-+-'9 -*-** *

.872.

..1.6 *...

.877.

.. 1. 6.

,735,

-1,5,

,922,..

-1.s.

• 1.019, 7..

3.'1.

.890. :.843.

-.2.. -4.8.

1.047, *1.11s.

!,)**

.. 3,9, 1.142, 1.1oe.

,9e9, 1.114, 1,040, 1.111.

,977, 1.097, 1.131. 1.116. 1.013,

,973,

..3,e,

.. 4,5,

.. 4,0,

.. 3,9,

.. 3,5,

.. 4.1... 5,1,

.. 5,4,

.. 4,7,

.. 3,9,

.. 3,1... 1,5.

,999, B *

-,3, "963. 1.133.

~1.0. - -J.7.

,944, 1.1&1. 1.113. 1.035,

• 116. 1.026. 1.095, 1.142.

.928. 1.121.

.952. 1.011

• 1.5, 9 *

10.

11.

12 13

14.

15

• 981. 1,033, 1.127. 1.143, 1.101.

-,7,

~* -2,9,

-3,9,

-4161

,979, 1.153, 1.019. 1.112.

.. 5.1.

..5,6.

..5,5,

.. 4,1.

.982. 1.098. 1.120. 1.099, 1.034, 1.003 *

..4,7,

.. 5,4,

.. 5,7,

.. 5,4,

-1.1.

1,5,

.. \\'.

,949,

,902\\

.est.

,955,

.942. 1.130.

,9e1. 1.105.

,996. 1.160.

..3,2.

..4,3,

.960.

-4,7, 1.4.

1.1...... 3,9,

-6.5.

-6.5.

,794, 1.199, ~.

,945, 1.021.

..6.8.

-6.9.

-4.7.

-4.6.

,943, 1.103. 1.111. 1.139,

-1.0.

-s.3.

-J.9.

-2.J.

.988. 1.010.

-2.J.

,972.

-4.8.

.987.

-2.4.

.833.

..5,9,

,744, 1.204,

..2.6.

7.0.

,975, 4,2.

,79e, 6.9.

~,9,*.~6.6.

-~~....--.

.-:::-.*~-.

• t.075.

8.3.

. eo2.

11.s.

• 919.

.863,

,949, 10.1.

10.9i

-1.1.

1.179, 11.5,

.803.

11.6.

.956. 1.137.

-7.1.

-4160

,947, 1.153, 1.003,

.. 3.6,

.. 3,3,

.. 2.6.

1.120. 1.154, 1.139,

• 883 *

-.a.

.. 3,3,

-2,3,

-2.J.

1.015,

-.s.

.010

• 5,5,

.778 *

-.1.

,902.

7,9,

• ~*

(

.916

• 9,7, 1.1eo.

11.6.

,979, 1.049,

~

t.053.

.2.

.906. 1.216) 1.137, 1.2.

7,7, 14,4,

.838.

16.5.

i.1;:2\\)

0 13.1.

.854.

1s.s.

---

~.

,799, 6.8.

.982. 1.011. 1.033, 1~012.

2.6.

2.6.

2.0.

.950.

.eo5.

1.1.

SALH INCORE HAP2202*48,332% PWk,BK Dl189*1182PPH,18HWD/HTU*PT.45*44 CALCULATED POWER TILTS CNORHALIZED TO 1.000)

• 1.0111 ** 9961

• 1.0066 1.0104 *

.9895 1.0037 *

.9829

.9985

,9933 *

.9968

,9956

• 1.0045 1.0051

,9990.1.0122 POSITIVE.. y.. us, NEGATIVE.. y.. TILT

,9999 1.0001 POSITIVE.. X-US, NEGATIVE.. X.. TILT

.9970 1.0030

.9898 Page 16

FIGURE 6 REASURED AND PERCENT, DIFF, OF FDHN BALK INCDRE ffAP220Jo48,S66X PWRrBg D9180111D2PPffo21mHB/NTUrPT.45*44 R

P N

H

• .L *,.K,

• oJ * *

,*H,

,,e,,.F,

• .IE *

• D

.:.... C 8

It

.767,

.976. 1.01e, loOJl, 1.024. 1.003,

,799, 1

2.1.

J,5.

2.2.

2.0.

2.e.

6.J,

,,J, 2

6 *

,939, 1.160.

16.4.

16.4 *

• 157.

2.2.

,927, lo21B, 14,9, 15.1.

• 977. !

• 786.

16.9.

2.3, 0929. 1.063

• 3.4.

,912.

2.3.

• 983. l

• 054.

.2.

.1.

l.134.

-2.7.

0917~ 1.155, 1.061 *

,971,

-2.J.

-2.2.

1.193, 12.e.

.e12.

12.6.

0

• 1.121.

,949, 1.01e. 1.030,

,932, 1,149, 1.oos.

,994,

.764.'

13131 13,71-

-,5,

-,O, 111

-3,9,

-4101

-J,J,

-2141

-2,4o

-c81

,913. ~..<181.

,799, *~:

i.120. 1.178. 1.121.

,997, l.066. 1.000.

e.s.

4,7, 4,4, 1-2.0.

-2.2.

-2,4,

-3,7,

-3.0, -3.o. -2.s. -2.s.

-.9,

.9~o:

.896. ~~

',990,

.97s. 1.171,

.99o: i.121.

,994, 1.151,

,957, 1.003

• 4,2.

.1.

-4,4,

-J,o,

-3.2,

-3,4,

-J.B.

-3,0,

-4,4,

-5,1,

-s.o.

-1,7, 0.J.

• • 0

.890, 10063.

. 6.7.

6.8.

'167. 1.130,

~*-.. 1:

. e7e~.

-1.0. -1.0\\

0

,747,

-,4,

, 1.027, 1.os2; 1.11e. 1,141, 1.109,

.986. 1,173, 1.oJe. 1.16B*

,972, 1.091. 1.120. 1.119. 1.022

• 7 J,5,

• J..

-3,7,

• *i *

• 1.003, 8 *

-,3,

• 964. 1.132 *

-1.1.

-3.7.

!93J, 1.J60, 1.109, loOJO,

.763, 1,015, 1.090. 1,137,

-3.6.

-3,9,

-3,9,

-4,4, -s.6.

-5.e.

-s.s. -s.1.

• 918. 1.120 *

-s.2.

-4,7,

,939,; 1.031 *

-1.e

i,4, 9 *

11.

12 13 14 15

,955,

1. s.

7.o.

1.034.

1 4,..

1.2:"

1.124, 1.139, 1.1os.

,979, 1.153, 1.012. 1.160.

-s.o. -s.s. -s.e.

-4.9.

,979, 1.096. 1.117. 1.095, 1. 41. 1.016.

-4,9,

-s.~. -5,7,

-5,7,

-,B, 2,4,

-3,2,

-3.e.

,959.

-6.1.

-4.6.

09460 1o132o

,974, lo093,

,993, 1o160o

0962,

,974,

-6.1- -6.7.

-s,3,

-s.4.

-4.s.

-4,4,

-4.5.

-4.6..

,931 *.-

,943,

-6.3 5,4, 1.02s.

.946. 1,09e, 1.160. 1.121.

,9ee. 1.012.

,999,

.748 1.224.

-604.

-6.7o

-S.6.

-~.s. -J.1.

-2,5,

-2.0.

-2.0.

-2,2 B.~.

.991.

5,4.

.e12.

B.4,

• 1.079.

9,4, 10.0.

• 951 *

• 961. *1.129 *

,929. 1.143, 1.003. 1.020

• 1.130.

13,5,

• 796. 1. 170.

10.s.

10.6.

• 926.;

10.e.

,717,

-6.6.

,797, 1.oe9.: 1.2oe; 10.6.

9,3 6.7.

• eo1.

61.60

,943, 1.104. 1.120. 1.136.

.883 *

-5.4,

-s.4,

-4,4,

-2.s.

-,9, s.7,

,9oe. 1. 033,

.963. i465~':909:-*i.2i5.

• 956

• 1.4.

-.o.

.994. 1.014. 1.021 *

.3.

2.s.

,953, 1.0.

13.7.

SALH INCORE KAP2203r4B.566% PWRrBK D@1BOr1182PPffr21HWD/HTUrPT.45,44 CALCULATED POWE~ TILTS <NDRHALIZED TO 1.000)

• 100167.1.0000

• 1,0083 1.0113 *

.9931 lo005B,

.9862

,9999

,9940 ***,9999

.9913

• 1.0044

.9987

,9ees.1.0090

• POSITIVE -Y-VS, NEGATIVE -Y-TILT

1. 0022

• 9978 POSITIVE -X-US. NEGATIVE -X-TILT

,9997 1.0013 0

0 11.6.

,935, 16o0o

.9930

.852.

18.3.

, MEAS *

, DIFF,

Page 17

FIGURE 7

• at::AiluRED AND l"ERC£NT. DIFF, OF FDHN BAL" INCORE "AP2204,49,439z PWR*8K Dl180*11B2PP"*27"WD/"TU,PT.45*44 R

p H

• L *** K **

• J ** oH I

• e... F **

• E *

• D c

B A

,7se.

,911. 1.01,. 1.030. 1.024. 1.006.

.eo2.

1 1.0.

3,0, 1.*.

2.0.

J.o.

6.e.

6.9.

2 5 *..

6 *

,939, 1.160. 1.143, 16.~. 16.5.

1.1.

,923, 1.os1.

,979, 1.053,

,920. 1.160. 1.066.

.807.

12~..

• 825. 1.215, 14.6.

14.9.

1.120.

12.1...

,943, 13.0.

,979, 11.0.

,777, 1.2.

-2.9.

....... -.-*. a....,_. *-~.

.902. 1.141. 1.141, 1.132.

1.2. -2.2. -3,3, -2.9.

--a***...

.an;.

,753,

-1,9, -1.e.

.759, 1,004, 1.015. 1 *. 1H,.,... 32, 1,149, 1.006.

-1.9, -1.s.

-:~*4-....-.3, -,~~a.4, -:a.s. -2.2.

,996.

-2.J.

.0 7,1.

.a21. 1.1e1.

-1.a.

12.2.

.807.

12.1.

.771.

,993, 1.064.

-.J.

7,0.

7,0.

• e10.- 1.1e1.

,799, e.2.

4,1, *., 4.6.

• 986. 1. 064 *

-2.J. -2.1.

• 9e~. 1.119, 1.114, 1012Jo

-2.9,

~3.a. -3,5, -J.5.

09860 10065. 1.006 *

-2.7.

-2.1.

.771. 1.13::;,

,9,

,7,

,979,

,999,

• '853.

.989.

.973, 1.160.

.981. 1.104,

.986. 1.1se.

• 963. 1

• 008.

,6, -J,B,

-3,1, -3,4, -4,4, -4,7, -4,5, -4,2, -4,5,

-4,4,

-1,3,

.ee2.

-.s;

,999,

-.6.

.746.

-.4.

,93::;,

-,4,

• 1.021. 1.054, 1.122. 1.146. 1.114.

,993, 1.164. 1.021. 1.112.

,991. 1.099, 1.133, 1.122. 1.022.

.987.

7

,5,

-3,3,* -3,3,

-J,~, -4.6o

-4060

-4.6, -J,9, -4,9, -5,1,

-4,4,

-J,J,

-2,::;,

• 1.003.

e,

-.2.

• 964. 1.133,

-1.1.

-3.6.

,940, 1.165. 1.102. 1.01e *

-3.J. -J.s.- -4.5.

-5,5,

.763. 1.026. 1.097, 1.144,

-5,9, -4,9, -4.9.

-5,3,

,92::;. 1.i24.

-4.9.

-4.4.

• 958. 1. 028.

-1. 7,

10.

11.

12 13 14 -

15

,995, 1.034, 1.124. 1.141, 1.101.

-.6.

-1.3.

-3.2.

-3.7.

-4,5,

• 979, 1.153, 1.011. 1.169.

-s.o. -5,5, -5,5, -4.2.

.982. 1.102. 1.123.

1~102. 1.039, 1.013.

• 950.

1.1.

-4.6.

-4,9,

-5.2.

-5.o.

,902.

,949,

.956.

,943, 1.131,

.980. 1.102.

.992. 1.161.

,9, -4.2.

-6.4.

-6.4.

-6.7. -4.8. -4,7,. -3.6. -4,3, 0

0965.

-4.2.

,977,

-4,3,

,943,

-s.o.

-.e.

,943, 5,5, 2.2 *

,990, 5,4,

,795, 1.199.

• e14,

,944, 1.02s.

.946. 1.104, 1.166. 1.132,

,9e~. 1.013,

,990, 6.5.

-6.5. -6.3. -6.6.

-5.1.

-4,1.

-2.1.

~2.a. -2.0.

-1,9,

.750. 1.221.

.813.

• B.6

• 6.2.

-1.9.

a.a.

• 1.011.

,924.

.865.

,955,

• 936. 1.149, 1.000. 1.015.

,773,

.o.

.918. 1.134, e.3.

10.1.

12.0.

-6.3.

-6.3.

-4,5,

-3,9,

-3.6. -2.e.

10.0.

,797, 1.112.

10.1.

10.e.

,929.

.120.

.846. 1.101. 1.129. 1.137,

.883.

11.0. -6.2.

-5.1, -s.1.

-4,3, -2.5. -1.0.

• e10.

5,5,

,901. 1.101.

,797, 1.090. 1.209.

10.7.

9.4.

6.9.

.eo1.

6.8.

.909. 1.029.

1. 3.

-.2.2.

.960. 1.049.

-2.1.

-.~.

,956.

1.5.

,999, 1.001. 1.014.

-.6.

1.9.

.908. 1.216.

,952.

1.1.

7,5,

.806.

7,4, 7,9, 1.13::;,

14.0.

SALK INCORE KAP2204*49.439% PWR,BK Dl1B0,11B2PPK,27KWD/"TU,PT.45*44 CALCULATED POWER TILTS <NOR"ALIZED TO 1,000)

• 1.0103.1.0002

• 1.00:;2 1.0076 *

,9947 1.0049 *

,9993

.9988

.9929 1.0021

.9916

• 1.0061 1.0000

.9904.1.0095

• POSITIVE -Y-VS. llE8ATIVE -Y-TILT 1.0012

.9988 POSITIVE -X-VS, NEGATIVE -X-TILT 1.0004

.9996 11.6.

,939, 16.4.

.9960 14.0.

.856

• 19,9,

, KEAS,

, DIFF,

Page 18

FIGURE 8 "EASURED AND PERCENT. DIFF. OF FDHN SAL" INCORE "AP2205r72.093Z PYR.BK Dl214*1046PP"*47"WD/"TU.PT.45.44 1

2 3

4 R

P N

• .L * *.K

• c.J * *

• H,,,o,,,f,

,,E,,

D C

B A

,737,

,935,

,993, 1,000,

,991,

,957,

,763,

• sos. 1.112 *. 1.116.

12.7.

12.7.

-.1.

1.1.

.6.

.894. 1.0*35.

.962. 1.034, i.o.

-.9.

3,4,

,994, 1.141. 1.030.

1.0.

2.1.

4,3,

.763.

6.1.*

,779, 1.151.

,915, 9.0.

• 766.

-.o.

.886. 1.149, 1.162. 1.144.

.873.

,777,

-.1.

-1.6. -2.2. -1.9, -1.5.

1.4.

.e11. 1.12e.

,790

• 9,2.

9.0.

9,0.

• 1.058.

,997, 7,3, 1.1......

.151, 1.oa1. 1.031, 1.112.

s.2.

s.1.

-~o. -2.6.

,997, 1.177, 1.014, 1.033,

-2,5, -2.2. -1.6.

,5, 4,4,

.e22.

1.7 *.

6.8.

.eeo. 1.039, s.o.

5

• 6

• 7

• 8

• 9 *

10.

11.

12 13 14 15

,774, -1.152.

3,4,...

,792, 1.031, 1.067.

3.8.

1.2. -2.9.

,995, 1.151. 1.215. 1.154,

-2.9.

-1.1.

-1.4. -1.5.

,999, 1.oe5. 1.020.

-1.6.

-1.3.

.1.

.764. 1.113.

.1.

-.1.

0724.

-1.7,

,937, 1.s.

,977,

,955,

,991,

,977, 1.176. 1.007. 1.139. 1.006. 1,179,

-,5, -3.o. -3.1.

-3.2.

-3.1.

-2.4.

-2.0.

~2.6. -2.e.

,977, 1.013.

-3.2.

-,9.,

,973,

-1.0.

0872.

.90.7.

-1.1.

-1.7,

,990, 1.034, 1.132, 1.110. 1.136. 1.009. 1.202. 1.069. 1.199,

,999, 1.134, 1.164. 1.129, 1.oos.

,949, 1.6.

-.2. -2,5, -2,4.

-2.1~ -2.3,

-2.2.

-1,9, -2.5. -3,3,

-2.s.

-2,9.

-2.s.

-3,0,

-2.7.

,979,

,952. 1.149,

,997, 1.195, 1.136. 1.067.

-.9.

-1,3.

-2.9.

-2.2. -2,4.

-2.1. -2.4,

.830. 1.0~9. 1.123, 1.197,

-2.7.

-3.1. -3.2.

-3.1.

,997, 1.147,

,942.

,977,

-3.2.

-3.1. -2.4.

-1.2.

• 962. 1.021. 1.129. 1.170. 1.134, 1.003. 1.191, 1.057. 1.202. 1.00~.

-1.3. -1.s. -2.s. -2.4. -2.s. -2,9, -3.1,

-3.o.

-2.2. -2,7.

1.134, 1.157, 1.123. 1.01~ *

-2.s. -3.s.

-3,3,

-2.0.

• 928.

.6.

.ass.

,4,

,774, 1.173, 5,3,

• 1.043.

5,9,

,945,

.981.

.968. 1.160.

-4.2. -4.1. -4.1.

-4,4,

,999, 1.12s. 1.010. 1.1s3.

-J.2.

-3.0.

-2.1.

-2.6..

,980.

-2.9.

,993,.,949,

-2,9,

-3.9.

.912

• 3,4,

.so4.

,977, 1.051,

.969. 1.130, 1.200. 1.1s1. 1.001. 1.093, 1.014.

5~4. -4.1. -4.3.

-4,5,

-3,3, -2.7.

-1.7, -1.3.

-,5,

-.s.

,759, 1.177,

-.5.

• 092, 6.4.

,939, 1.006. 1.006. 1.160.

3,9,

-2.1~ -2,4,

-3.6.

.993. 1.171. 1.016. 1.040 *

-2.9.

-2,7. -1.4,

• a20

• 1.4...

,913. 1.009

• 8.9.

10.5,

• 766. 1.132,

• es2.

5.0.

.752.

-1,9, 0860. 1.111. 1,141, 1.141 *

-3.0.

-4,7,

-4.0.

-2.2.

.a00.

-.7.

.eo1.

4.6.

.896.

1.1~7.

6.7.

9.6.

.e22

• 1::;. o.

.767. 1.037, 1.149, 7,3, 5.o.

2.7.

0886. 1.012.

.946. 1.033,

• 1.

-2.1.

-2.6.

-.e.

,999, 1.177. 1.099,

,4, 5,3, 10.2 *

,904, 12.6.

.965.

-1.0.

,954, 3,4,

,777, s.6.

,775, 5,1.

,929.

.963.

.981.

,3,

-1.5 *.

-1.2.

,999, 1.1.

.929.

,4,

,777, 5,3,

, "EAS,

, DIFF,

SAL" INCORE "AP2205,72,093Z PWR,BK Dl214*1046PPHo47"W~/"TU,PT,4~,44 CALCULATED POWER TILTS <NORHALIZED ~O 1.000)

• 1.0097,1.0034

• 100066 1.ooss *

.9962 1.0013 *

.9890

,9977

.9956

.9942 *** 1.0021

,9926

• 1.0057 1.0001

,9909,1.0093

• POSITIVE -Y-US. NEGATIVE -Y-TILT 1.0009

,9991 POSITIVE -X-US, NEGATIVE -X-TILT 1.0010

.9990 Page 19

FIGURE 9 HEASURED AND PERCENT. DIFF. OF FDHN SALK INCORE HAP2206r95.931% PWRr*K Dl21Bo874PPKr213"WD/"TUrPTo45r47r44r4 R

P N

Lo K. * * *J. *

• H. *

• G. *

• F. *

• E.

• D

.C I

A 2

3 5

• 6 *

.736.

of25o 09740 of87o e976o

,933,

,744,

• o.

.2.

-.1.

-.2.

.1.

1.1.

1.1 *

,953, 1.026.

-1.6.

-1.2.

,744, 4.1.

,779, 1.076. 1.117.

1886. 1.027.

,995, 1.126. 1.009.

9.1.

9,1.

.1.

.3.

-1.1.

2.3,

• 764. 1.130.

,901.

7,2.

.768.

• 2.

• eee. 1.146. 1.160. 1.144,

.1eo.

,773,

.2.

-1.1. -2.3,

-1,9,

.e.

.861. 1.100 *

.756.

6.0

• 7.0.

• 1.043, 6000

,759, 1.143.

3,3, 2.7.

,922.

• 2.

.876.

-.s.

7.o.

2.4.

.889, 6.0.

• e40, 1.040, 1.040, 1,170. 1.003, 1.1eo. 1.021. 1.035,

.e28.

,971, 1.02e

• 1.9.

3,9, 4,4, 3o2o o9o o9o

-2080

-2141

-2101

-1101 151

.1,90. 1.038. 1.098. 1.011. 1.162. 1.224. 1.161. 1.003. 1.096. 1.034, 3.5.

1.6.

• 866. 1.013.

-1.e.

-1.0.

-.3.

-.e.

-.8.

-1.0. -1.2.

,999, 1.201. 1.022. 1.153. 1.019, 1.192,

-1.1.

-1.0.

~1.1. -1.0.

-1,4,

-1.e.

1.2.

.992. 1.023,

-1.7.

-.o *

,772, 1.121.

1.1.

.e.

.8eo *

-.2.

,977,

-.4 *

• 976, 1.030, 1,141, 1.1e1, 1.147, 1.020, 1.220. lo087. 1.223, 1.019, 1.154, 1,173, 1,137, 1.011, 07260

-1.1.

.9100

-1.10 o95:)o 1 *

• s.

-.4o

-lo7o

-1o5o

-1.7.

-1.3o

-.7. -1.4.

-1.20

-2.2.

-2.0.

-2o3o

-1.7

• 8 *

.971.

-1.5, 09480 lo153o lo010o lo206o lo149o 1o084o 0847, le077o 1o141o 1e2l0o 10003, 1o157o

-1.6.

-2.5,

-1,4,

-1.1.

-1.1.

-1.0.

-1.4. -1.6. -1.e.

-1,4,

~2.1. -2.2.

,943,

-2.1.

,954, 1.016. 1.129, 1.192, 1.149, 1.017. 1.211. 1.071, 1.217, 1.01e. 1.1s1. 1.172, 1.134, 1.014.

9 *

-1.e.

-1,9.

-2,7,

-1,5.

-1.6.

-1.6.

-1.6.

-1.9.

-1.2. -1,5.

-1.4,

-2,3.

~2.3. -1.9.

.916.

10.*

-.4.

08750

.8450 1.0000 09870 1.112. 1.0110 1o13Bo lo014o 1.194,

-o6i

-4o2o

-2~3. -2,3,

-2.60

-2020

-2020

-1080

-106.

.9930 lo006o

-1.6.

-1.7.

11.

12 13 14 o75Bo 1.1490.

3.3.

3.3.

• lo019o 3.5o

.790.

3o4o

• 8710 3080 07460 1o103o 4o5o 19980 1.069.

.9850 1.140. 1o214o 1o160o lo011. 1.1060 1.0270

-2.3.

-2,9,

-3.o. '-2.1.

-1,7,

-1.0.

-.4.

.s.

.6.

08210 09970

.9960 lo166o 1o005o lo179o 1o026o 1o053o

,9,

-3,3,

-3,4,

-3.2.

-2.1. -2.1.

-.5.

2.2.

18790 4.6.

07350

-4olo 18470 1.113. 1o145o 1.1440

-4o5o

-4o5o

-3.6.

-1.eo 08830

-,4,

.196.

3o.Bo 0834

• 2060 07460 1.02so 1.147,

• 8740 1.007.

-1.2.

-3.lo

.9400 lo026.

-3.0,

-1.20 08860 lol55. 1.055, 4,5, 4o0o 2oBo

• 2.

7.o

• 0

.e5eo

-2o7o

,997, 1 o9o

.169. lo15Bo

,7, 4,1.

9,10

.192

• 9,5, 9,3, oeoo.

12o1o

,973.

-1.3.

09600

-1o2o 09370 1.9

• 07640 4olo 15

.756.

2o7o

.9140

-1.0.

.9540

-2021

.9710

-1,9.

,979,

,4, 09240

.2.

.762.

3o5o o "EAS,

• DIFF o SALK INCDRE KAP2206r95.931X PWR,8K D@21B*B74PPH,213KWD/"TUrPTo45*47r44r4 CALCULATED POWER TILTS CNOR"ALIZED TO loOOOl 0 1.0074o1o0001

• 1.0037 1.0054 *

.9978 1.0035.*

• 9956

,9993 1.0001

• 9931

• 0

• 1.0046

.9905

• 1.0062

.9979

.98790110079 0 POSITIVE -Y-VS, NEGATIVE -Y-TILT 1.0016

,9994 POSITIVE -X-VS, NEGATIVE -X-TILT 100020 09980 Page 20

FIGURE 10 MEASURED AND PERCENT, DIFF, OF FDHN KAP2207 r.98, 438% PWR' BK D*22B, B74PPK r 222KWD/11TU' PT, 44

• 46 1

2 3

4 5

• 6

• 7

• R P

N H

L

• . 730.

-.2.

.776. 1.071. 1.109.

e.9.

e.9.

-.2.

K

.J H

0 FED C

• 918.

.1.

,965.

-.4.

.978.

.967 *

-.:s.

-.1.

.eeo. 1.021.

,949, 1.022.

-**O,

-1,3,

-1,7,

-1,2,

.926.

1.0....

,739, 1.0.

.&BJ, 1.123, 1.009, 1.1 *

,741.

4.1.

B

• 760. 1.127.

6,9, 6,B,

,902.

7, 1.

.ee4, 1.147, 1.164. 1.146 ** ee2.

-.2.

-1.6.

-2.2.

-1.6.

-.3.

,775, 1.1.

.864. 1.099, 2.6.

4.1.

.752.

5.6.

• 1.039, 5,7,

,754, 1.13e.

3,3/

2.7.

.eee.

5,7,

• e5o. 1.044, 1,041, 1.1eo. 1.020. 1.190, 1.026. 1.041

• 3,2.

.9.

,9,

-2.4,

-2.0.

-1.6.

-.6.

,7,

.837.

1.7.

,799, 1.042, 1,099, 1.012. 1.169. 1.2J6~ 1.170, 1.ooe. 1.100. 1.037, 3.3.

1.6.

-.2.

-.4.

-.s.

-.4.

-.4.

-.7.

-.2.

1.2.

,921.

,7,

,973,

.865. 1.014, 1.000. 1.201. 1.024, 1.15e, 1.026. 1.199,

-,3. -1.s.

-1.0.

-1.0.

-1.1.

-1.0.

-.7.

-.a. -1.2.

,999. 1.025.

-1.2.

.1.

.870. f,022

• 3,5, 4,1,

.770. 1.117.

1.0.

.e.

.eeo.

-.1.

• 87~.

-.2.

,970. 1.025, 1.140. 1.1eJ. 1.149, 1.021. 1.225, 1,094, 1.2J2. 1.026. 1.160. 1.1eo. 1.140, 1.010.

,4.

.961.

-.a.

-.4 *.

-.9.

-.9.

-2.0.

-1.e.

-2.0.

B,

-2,0.

,940. 1.1sJ. 1.019, 1.210. 1.151, 1.090,

-2.0.

-2.s.

-1.s.

-1,9,

-1.1.

-.9.

.e5e. 1.oe4, 1.145, 1.217, 1.016. 1.161.

-1.6.

-1.5,

-1.6.

-1.3.

-2.1.

-2.1.

9 *

,944, 1.007. 1.125. 1.102. 1.147. r.01e.

-2.J.

-2.2.

-J.1.

-1.e.

-2.0.

-1.7,.

1.210.

-1.3.

1.078, 1.21e. 1.010. 1,153, 1,176, 1.135, 1.012.

-1.s.

-1.3.

-1.6.

-1.5,

-2,4,

-2.2.

-1.e.

--~-* -.906 *

• 867.

10.

-.9.

1-1.1.

,940. 1.003.

-4,7,

-2.1.

.989. 1.186. 1.012. 1,139, 1.013. 1.194,

-2.1.

-2.4.

-2.2.

-2.4.

-2.1.

-1.6.

,994, 1.007,

,957,

-1.6.

-1.7.

-2.7.

,994, 2.0.

11.

12 13 14

,749, 1.137.

2,7, 2,7,

• 1.010.

2.9.

,793, 1.004. 1.075.

2.1.

-2.1*.

-2.s.

.989. 1.144, 1.220. 1.161. 1.014, 1.109. 1.031,

-2.6.

-2.6.

-1.7.

-1.2.

-.2.

.6.

.6.

.867

• 3,1.

~eJo. 1.ooe. 1.004, 1.172, 1.010. 1.1&4. 1.030, 1.05e,

.e. -2.6.

-2.7,

-J.o. -2.2.

-2.1.

-.2.

2.J.

,944, 2.5,

.76&. 1.155.

.7.

4.3.

..904. 1.060.

7.6.

7,9,

,741. 1.097,

• e76,

,739,

.e5o. 1.119, 1.152. 1.145, 4,1.

-J.6.

-J.9.

-4.o.

-J.2. -1.e.

.ee1.

-.s.

• 796.

3,9,

.890. 1.136 *

• 5,e,

.7.7.

,793, 11.3, 4.1.

4,0.

,742. 1.017. 1.134, 4,2.

3,5, 2.0.

.869. 1.004,

-1.2.

-2.9.

• 938. 1

• 021 *

-2.e.

-1,4,

.&79. 1.152, 1.057,

-.1.

3,7, 7.s.

,779, 9,3, A

,724,

-.9.

.907.

-.9.

.952.

-1,4,

.969.

-1.1.

.956.

-1.0.

.93'3; 2.0.

.761*

4,3, HEAS 15

,747,

,908.

,949,

,965.

2.0.

-1.1.

-2.1.

-1.9,

.969..,917,

.o.

-.1.

,759, 3,7,

, DIFF

• KAP2207*9B,438% PWR,BK Dt22Br874PPK*222HWD/KTU,PT.44*46 CALCULATED POWER TILTS <NORMALIZED TO 1,000>

• 1.0071.1.0022

• 1.0046 1.0049 *

,9996 1.0026 *

,9969

.9965 1.0007

,9903 *** 1.0045

.9894

• 1.0062

.9982

,9995,1,0079

• POSITIVE -Y-VS, NEGATIVE -V-TILT 1.0022

,9979 POSITIVE -X-VS, NEGATIVE -X-TILT 1.0029

.9971 Page 21

FIGURE 11 HEASURED AND PERCENT, DIFF. OF FDHN SALH INCORE HAP220Br98.9Z PWRrBK Dl22Br861~PHr287HWD/HTUrPT.44r46 2

3

4.

5

• 6

• 7

• R P

N

• .L * *.K * *.J *,.H,,.a., eF * *.E *

• D C

I

.732.

.917,

.966.

.979.

.972.

.931.

,743, t

6 *

.ae5. 1.

5. 1.009 *

• 1.

• 5 *

,774. 1.068* 1.112....

• eeo. 1.021.

• 947. 1.023.

.743 *

.903.

7.1

• 769.

.2.

,997, 1~148, lol65o 10147~

• 2.

-1.4. -2.1. -1.6.

.882 *

-.4 *

• e6s *.**1. u~i.

1 2.7. *.

4.4.'

,755, 6.o.

t'

• 1.040.

.e91.

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.e39.

---

~6.o.

5,9, 3.o.

.2.

.2.

-2.s.

-2.1. * -1.1.

-.e.

.6.

1.6.

. ~

...-{.

,754, 1,140,

.791. 1.043. 1.097, 10009. 1.169. t.236. 1.168, 1.006. 1,099, 1.038.

3,3.

• 919.

• s.

3.6.

1.6.

-.6 *. -*J*

-.s.

-.s.

-.6. -1.0.

-.4.

1.1.

,975,

.867. 1.014 *

-.2. -1.6.

-1.1.

• 998. 1.199. t.024. t.156. 1.024. 1.196.

-1,3: -1.3.

-1.1.

~.9. -1.1. -1.s.

,997, 1.023 *

-.1 *

,973. 1.024

• 3.e.

4,4.

.111. 1.115.

• 9.

• 7,

• 878.

.872.

-,4,'

.971. 1.026. 1.141. 1.194, 1.149. 1.021. 1.225, 1.093, 1.230. 1.024. 1.159. 1.177. 1.136. 1.006.

• 6.

-.5

• A

.121 *

-1.2.

..903 *

-1.2.

,949,

• 964.

,942, 1.1s2. 1.01er 1.210. 1.150, 1,099,

,959, 1.os4, 1,144, 1.2t6. 1.014. 1.158.

,93a,

.964.

e *

-1.6. -1.e.

-2.e.

-1,9. -1,9,

-1.2. -1.0. -1.6. -1.5, -1.e.

-1.~. -2,4.

-2,3,

-2.2.

-1,5,

,941. 1.009, 1.12s. 1.112. 1.14e. 1.011. 1.211. 1.01e. 1.220. 1.01e. 1.153, 1.116. 1.135. 1.ooe.

,950, 9 *

-1.e,

-2.0.

-3,1. -1.s. -1.9, 4>1,1.

-1.4, -1.e.

-1.3. -1.1.

-1.s. -2.4.

-2.2.

-2.1. -1.s.

,901.

.e6e.

.142, 1.004.

,990. 1.116. 1.015. 1.142. 1.01e. 1.194.

.995, 1.ooe.

.&60.

.e92,

,931,

10.

-,7,

-1.0.

-4.s.

-2.-0.

-2.0.

-2.4.

-2.0.

-2.1.

-1.7. --1.7.

-1.6.

-1.7 *. ~2.4.

1.e~

1.e.

11.

12 ol: ' H 14 us

• 7so. 1.130, 2._e.

2.e.

• 1.011.

3.1.............

,742. 1.099.

.'878.

,739.

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4,3. -3.8.

-4.2.

-4.4.

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-1.9..

• 11&2.

-.4...

,79~

• 3.7.

,743,.1.019. 1.138.

.869. 1.003.

.937. 1.022.

.884. 1.1~3.

• 749.

• 907.

,949.

• 966.

2.5.

-1.0. -1.9. -1.1.

,973,

.6....

.s.

3.8.\\ 7.2.

.921.

• s.

.759.

3.8

• SALH INCORE "AP220Br98,9% PWRrlK.. 228r861PPHr287"YD/HTUrPT.44r46 CALCULATED POWER T!LTS <NOR"ALIZED TO 1,000>

• 1.006s.1.0026

• t.0048

.9991 1.0031 *

,9955

'".'.*~*-

"tr*

4.'*

.9901 i.0060

• 9914

~91a1.1.ooe1 *

... j

POSITIVE 1.0020

'..f;

., ~

!'~; ~--*

-y.;.-*"s,"'.llEHTlllE -Y-1'1LT

.9980 P.OSITIUE -X- *"6, ftEBATIUE *X- :ULT

• .;;;f

1. 0026

• • 974

'~.

1.0046

.99,72

.99114

.778.

9.J.

,794, 11.6.

• HEAS *

• DIFF,

Page 22

FIGURE 12 HEASURED AND PERCENT, DIFF. OF FDHN SALH INCORE HAP2209*9B.401% PWR*BK Dl228*B60PPH,292KWD/KTU*PT,44*46 R

P N

H

,.L,

,K,,,J,,,H,,,O,,,f,

,,E,,

D C

B A

3 4

5

• 6

• 7 *

,734,

• 4.

• ?76. 1.012. 1.11s.

t.o.

9,0.

.4.

.918.

.966.

,977,

.968.

,927.

.740.

~2*

-.2.

-.s.

• .10 1.2.

1.2

• 0

.882. 1.022.

,,47, 1.023.

.3.

-1.1.

-1.1.

-1.1.

.883. 1.123. 1.00?.

,743, 4,3,.

• ~.

.760. 1.127.

6.e.

6.e.

,902.

?.1.

,770,

,4,

,999, 1.149, 1.166. 1.149,

,4,

-1,3.

-2.0. -1.s.

,993,

,775,

-.3.

1.1.

• 863. 1.100.

2.4.

4,3,

.756

• 6.2.

• *1. 038.

5,7,

,754, 1.138.

J,4.

,920.

. * ?.

,999, 5.6..

,949, 1.043, 1.039, 1.1e2. 1.020. 1.199, 1.022. 1.040, 2.9,

,7,

,7,

-2.2.

-2.0.

-1.6.

-1.0.

,4,

.?90. 1.043. 1.099. 1.012. 1.111. 1.237, 1.169. 1.003. 1.094, 1.036.

3,4, 1.s.

-.3,

-.s.

-.4.

-,4,

-.s. -1,3,

-,9,

,9,

,973, 1.025

• 3,7, 4,:::;,

,772. 1.110.

1.1.

,9.

• 867. 1.015, 1.000. 1,199, 1.022. 1.154, 1.024, 1.195,

,995, 1.024 *.* ee1.

-.1 *

-.1.

.967. 1.025. 1.142, 1.1s5. 1.150, 1.020. 1.224, 1.092, 1.234, 1.02e. 1.162. 1.179, 1.139, 1.009.

,3,

-.4.

-1.6.

-1.6.

-1.e.' -1,4,

-1.0.

-.6.

-.2.

-,7,

-.e.

-2.1.

~1.e. -2.0.

,960.

8 *

-1.9.

,942, 1.156, 1,021, 1.212, 1.149, 1.087,

-1.e.

-2.5.

-1.6,

-1.e.

-1.3,

-1.3.

.&56. 1.oes. 1.146. 1.219, 1.016. 1.160.

-1.9,

-1,4.

-1.6.

-1.2.

-2.2.

-2.1.

.941.

-1.9.

,723,

-.e.

.906.

-.e.

,951,

-1.4.

.968.

-1.1.

,944, 1.009, 1.129. 1.1es. 1.150, 1.019, 1.219. 1.011. 1.221. 1.019, 1.154, 1.116. 1.135, 1.011.

,955, 9 *

-2.1.

-2.0.

-2.1.

-1.6.

-1,7,

-1.6.

-1,4.

-2.0.

-1.2.

-1.s.

-1,4,

-2.J.

-2.2.

-1.1.

-1.0.

10.

11.

12 13 14 15

,905.

-.9.

,866.

-1.1.

,745, 1.131.

2.1.

2.1.

• 1.009.

2.s.

,945, 1.oos.

-4.2.

-1.9.

,991. 1.101. 1.014. 1.140. 1.015. 1.192.

-1.9.

-2.3,

-2.0.

-2.J. -2.0.

-1.e.

,994, 1.00?.

-1.1. -1.e.

• 100. 1.001. 1.015, 2.1.

-1,9,

-2,5,

,999, 1.144, 1.221. 1.162. 1.010. 1.109. 1.032 *

-2.1.

-2.6.

-1.7,

-1.1.

-.6.

~s.

,5,

• 871.

3,5,

• 833. 1.007, 1.002. 1.1?1. 1.011. 1.102 *

-2.2.

1.026. 1.050,

,9,

-2.e.

-.6.

• e:se.

-2.? *

.896

• 2.2.

• 769. 1.159,

,7,

-4.7 *

• 904. 1. 060

• 1.s.

e.o.

,743, 1.101.

4,4, 4,4,

.eeo.

,737, 4,4,

-3,9,

,947, 1.113, 1.146. 1.141,

-4.4.

-4,5,

-3.7.

-2.1.

,979,

-.7.

,794, 3.6.

.ees. 1.133,

,791.

5,4, 7~4 *. 11.1.

,744, 1.021. 1.141.

4,5, 3,9, 2.e.

• 751.

2.e.

• 869. 1.002.

-1.1.

-3.1.

,900..

.946 *

,935, 1.019,

-3.o. -t.4.

.964.

,969.

.2.

.878. 1.147, 1.040 *

-.1.

3,3, 6.7.

,755, 3,3,

,775, e.e.

.764.

4,7,

, DIFF,

SALH INCORE KAP2209,9B.401% PWR,BK D@228,860PPH*292HWD/HTU,PT.44,46 CALCULATED POWER TILTS <NORMALIZED TO 1.000)

• 1.0079,1.0015

• 1.0047 1.0054 *

,9993 1.0029 *

• 9971

.9971 1.0010

.9912

• 1.0049

.9899

• 1.0054

.9972

,9885.1.0059

• POSITIVE -V-VS. NEGATIVE -V-TILT 1.0024

.9976 POSITIVE -X-VS. NEGATIVE -X-TILT 1.0023

,9977 Page 23

e e

FIGURE 13 ROD BANK INSERTION LIMITS. VS. THERMAL POWER NFG 83-187 7/25/83 SALEj(l UNIT :2.

Rop BANK. INSfRTtDtJ t1Mt'T5

.... I I

~ :. :

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~:;;:~--~~*.~:~~1'..~~j~~~~~~~;~~~~~~~~i.~: ~@~~;J~~~:~.~~~:~:'.:*~,:.:t~~j

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Page 24

APPENDIX A STARTUP TEST PROGRAM DESCRIPTION.

SALEM UNIT 2 CYCLE 2 The startup program is written such that deviations between measurement and design beyond established tolerances could call for a review of test data, a repeat of the measurement or a review of the safety analysis.

Operation is always within FSAR and Technical Specification limits.

A-1

STARTUP TEST PROGRAM DESCRIPTION SALEM UNIT 2 CYCLE 2 Test:

Initial Criticality Initial Conditions:

Mode 3, Tav~ = 547°F, CB = 2000 ppm Shutdown Banks*Withdrawn Control Banks Inserted Test

Description:

Pull control banks to D at 160 steps.

Dilute to criticality.

Checkout reactivity computer.

Acceptance Criteria:

Design:

Reactivity computer readings are within 4% of doubling time measurements.

FSAR/T.S.:

Reactor must achieve criticality with the control banks above the zero power insertion limits.

A-2

STARTUP TEST PROGRAM DESCRIPTION SALEM UNIT 2 CYCLE 2 Test:

Flux Mapping Initial Conditions:

HZP, ARO Test

Description:

Operate Flux Mapping System in accordance with Part 13 of the Reactor Engineering Manual "Incore Flux Mapping System Operation" Acceptance Criteria:

Design:

Assembly Power Design +/- 10% for assembly Power greater than 0.9 Design +/- 15% for assembly Power less than 0.9 FSAR/T.S.:

Not applicable below 5% power.

A-3

STARTUP TEST PROGRAM DESCRIPTION SALEM UNIT 2 CYCLE 2 Rod Worth Measurements Initial Conditions:

HZP The rod exchange method is used to measure all control bank worths.

Based on the results of these measurements 6 additional measurements using the boron dilution method may be necessary.

Test

Description:

Determine the worth of the reference rod bank by using the boron dilution method.

Exchange this reference bank with another bank while keeping the reactor critical and consta~t RCS boron concentration.

Using the heights of the rod banks with respect to the reference bank, infer the equivalent boron dilution rod worths using analytical techniques and compare results to acceptance criteria.

Acceptance Criteria:

Design:

Design value +/- 10%.on total banks worth Design value +/- 15% on any individual bank greater than or equal to 600 pcm Design value +/- 100 pcm on any individual bank less than 600 pcm FSAR/T. S.:

Worth of all rods less most reactive stuck rod must b~ 1.6% Delta K/K.

A-4

STARTUP TEST PROGRAM DESCRIPTION SALEM UNIT 2 CYCLE 2 Test:

Boron Endpoint Initial Conditions:

HZP Endpoint is run for the ARO configuration.

Test

Description:

Adjust RCS boron to near the just critical endpoint configuration.

Move rods to endpoint while measuring additional worth on the reactivity computer.

Acceptance Criteria:

Design:

Design * +/- 50 ppm FSAR/T.S.:

Design +/- 100 ppm

• Design values on attached Table.

A-5 l

STARTUP TEST PROGRAM DESCRIPTION SALEM UNIT 2 CYCLE 2 Test:

lsothermal Temperature Coefficient Initial Conditions:

HZP The coefficient is measured at the ARO rod configuration.

Test

Description:

Starting with Tave = 547°F, cooldown the primary system approx. 5°F.

Heat the primary system back up to 547°F.

The X-Y Recorder will plot reactivity vs. Tave.

Acceptance Criteria:

Design:

FSAR/T.S.:

ARO:

-2.8 +/- 3 pcm/°F

-3.1 x 10-4 delta K/K is less than or equal to MTC* less than or equal to 0

• MTC = ITC -

doppler A-6

STARTUP TEST PROGRAM DESCRIPTION SALEM, UNIT 2 CYCLE 2 Test:

Power Coefficient Initial Conditions:

Reactor power is not changing.

The Xenon concentration is within 3% of its equilibrium value.

This test is run at 100% Power.

Test

Description:

Take a heat balance.

Change turbine power between 2%

and 4% with the control rods in manual.

The Tave and Delta T recorders will monitor changes ~n these parameters as a function of time.

Acceptance Criteria:

Design:

Design value* +/- 30%

FSAR/T. S.:

Must fall between upper and lower curve assumed in FSAR accident analysis.

• See attached curve (Figure A-1)

A-7

i::i I co PARAMETER TEST MEASURED CONDITIONS Isothermal Critical Temperature HZP Coefficient ARO Critical,HZP C/B D Inserted Critical Crit.i.cal Boron HZP, ARO

~oncentratiori Critl.cal,HZP C/B D inserted Critical, HZP C/B C inserted Critical, HZP

'C/B B inserted Critical,, HZP C/B A inserted Power Coefficient 47% RTP 95t RTP

~eactivity Critical Computer HZP,controlling Check on C/B D

/

Reviewed By

( --).//)...

L/-

(

Re~~r ~ngineel/'

Salem 2, Cycle ~*

Rx. ENG MAN PART 200 SALEM ", -iCLE -

ACCEPTANCE CRITERIA SHEET 1 PHYSICS RESULTS MEASURED REQUIRED VALUE VALUE ox10-4 AND

-lf,J pc~/(}p

-J.lxl0-4 k/k/°F

-2.8 +/-3 PCM/°F Ox10-4 AND

/l//"9

-3.lxl0-4 k/k/°F

-6.1 +/-3 PCM/°F

/ 3t, t/

1408 +/-SOoom (Cal. from ARO

/;).{,/

Boron)

I

)!,._

./

1310ppm N *. A.

N.A.

N.A.

Figure 1

/1///1

t: 30%

Limits of Fiqure 2 d*f'ple~

Figure 1

-- //, 331C r-e

+/- 30%

Limits of

-J~

.. /g 0

Figure 2 (Double Time Reactivity +/- 4%

l'; 8'

~/.D:t: /106

$0.0 s.,o.o +/- l100 7/,2(

""~ 0 :t:

~.S:t

>>~I'~ A REQUIREMENT REFERENCE COMMENTS TaS.3.1.1.3 tnTC vA./.,,'

Ref. 2.3

= - z. ti"%

T.S. 3.1.1.3 Ref. 2.3 Ref. 2.3

'l'I fl"" lo~

• PART 15 oft "'-""'

aJjo;\\'l'r,/ t~,.

Ref. 2.2

_ "' i/ Pt',., 81;.r N.A.

N.A.

N.A..

Ref. 2.3 Ref. 2.4 Ref. 2.. 3 Ref.,2. 4 Ref. 2o3 Refueling Test Sequence

~

I

\\.0 uclear nthalpy ot Channel z

Bat Flux ot Channel actor TEST ONDITIONS Critical,HZP ARO Map 2:JO I 47%

Map ~;10'3 95%

Map~.). lo Crit ca,HZP, ARO ~ a O I tU-P Map.P.r rJo *l'Jlr}

Map d-~o~

95%

Map ';).~Jfl i

Salem 2 9 Cycle...:!_.

SALEM 2, "'.tCLE ~*

ACCEPTANCE CRITERIA SHEET 3 FLUX MAP RESULTS MEASURED VALUE

-+JI, 7 MAX

-r I'(,'? (MAX)

(Attached Cor.e Map)

Rx. ENG MAN PART 200 -

REQUIRED REQUIREMENT VALUE REFERENCE

+/-10% for F A pwr~.9

+/-15% for F/A pwr ~. 9 Ref. 2.3 (for measures Thimbles p.., ': 0. "t-10 "

~1. = o. 'i1" 6

R1=F.fH/l.49[1.0+0.3(1.0-P T.S. 3.2.

R2=lt1/£1-RBP(BU)]

Fig 3.2-3 RI ~ 0. j"'Cjl-.1 lL i. -: * -o * " ' s-~

2.32 K z p

i. ~ '13'1

.O-P T.S. 3.2.

_Fig. 3.2-3 T.S.

(INFO)

T.S.

T.S. 3.2.2 Retuelinq Test Sequence

PARAMETER TEST l-!EASURED CONDITIONS Cri.tical, HZP,

'xyC ARO Map J.~ o I Computed Radial 47t Peaking Map -:Zieo3 Factor 95%

Map J.~ Io Salem 2, Cycle..!t_.

SALEM 2, CYCLE ~*

ACCEPTANCE CRITERIA*

SHEET 3 (contd)

FLUX MAP RESULTS MEASURED VALUE TOP /.~~~o BOT l1 S' fl. f.£:..

TOP

/,&fill

• BOT L.t. 61!'.!:S-TOP. ( >.J./.S-BOT /,.f..J..18' Rx. ENG MAN PART 200 REQUIRED REQUIREMENT VALUE REFERENCE RTP L

r-

'F T.S. 3.2.2 1:Clo 2'!Ke (INFO) 1.64 2.13 1.60 L, ~~62 T.S. 3.2.2 1.64

{. 1:2.it'.

1.60

/, 'O'ffi T.S. 3.2.2 1.64

/. {, 'IY' Refueling Test Sequence

l'ICORE A-1 PCM PER PERCENT POWER 0

I I -

N I.... *

.----...----.,.-.--...----.----...-~-T----r---""T'"--.....,r-"..,.~

M I.........

11 a*

I

!~

1=

Is

=

1=

s:E --*= '

I

• l p

I...... -

!l,;

II

• I !.....

=-~

• ~

~..

0 -4 N

Doppler POW9' Coefficient Ueed in

• Accident Analysis

• Updated FSAR Figure 15. 1*5 Salem 2, ~ycle a--

• Refueling Test Sequence A-11