ML20155G710

End-Of-Cycle 1 Surveillance Fuel Exam Rept

ML20155G710
Person / Time
Site:	Palo Verde
Issue date:	05/31/1988
From:	ABB COMBUSTION ENGINEERING NUCLEAR FUEL (FORMERLY
To:
Shared Package
ML17304A208	List: ML20155G710
References
CEN-375(V)-NP, NUDOCS 8806200074
Download: ML20155G710 (36)

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PALO VERDE NUCLEAR GENERATING STATION - UNIT 2 END-OF-CYCLE 1 SURVEILLANCE FUEL EXAMINATION REPORT CEN-375(V)-NP MAY, 1988 A REPORT TO ARIZONA NUCLEAR POWER PROJECT FROM COMBUSTION ENGINEERING, INC.

NUCLEAR POWER SYSTEMS WINDSOR, CONNECTICUT 8806200074 DR 880609 ADOCK 05000529 DCD

LEGAL NOTICE THIS REPORT WAS PREPARED AS AN ACCOUNT OF WORK PERFORMED BY COMBUSTION

. ENGINEERING, INC. NEITHER COMBUSTION ENGINEERING NOR ANY PERSON ACTING ON ITS BEHALF:

A. MAKES ANY WARRANTY OR REPRESENTATION, EXPRESS OR IMPLIED INCLUDING THE WARRANTIES OF FITNESS FOR A PARTICULAR PURPOSE OR MERCHANTABILITY, WITH RESPECT TO THE ACCURACY, COMPLETENESS, OR USEFULNESS OF THE INFORMATION CONTAINED IN THIS REFORT, OR THAT THE USE OF ANY INFORMATION, APPARATUS, METHOD, OR PROCESS DISCLOSED IN THIS REPORT MAY NOT INFRINGE PRIVATELY OWNED RIGHTS; OR B. ASSUMES ANY LIABILITIES WITH RESPECT TO THE USE OF, OR FOR DAMAGES RESULTING FROM THE USE OF, ANY INFORMATION, APPARATUS, METH00 OR PROCESS DISCLOSED IN THIS REPORT.

I l

l Table of Contents I

Section Title P3gg

1.0 INTRODUCTION

1-1 2.0 GUIDE TUBE WEAR EVALUATION 2-1 2.1 Evaluation af Guide Tube ' lear Data 2-1 2.2 Evaluation Results 2-4 3.0 FUEL ASSEMBLY DIMENSIONAL CHANGE EVALUATION 3-1 3.1 Pre-Shutdown Evaluation 3-1 3.2 Dimensional Change Data 3-2 3.3 Post-Shutdown Evaluation 3-2 ,

4.0

SUMMARY

AND CONCLUSIONS 4-1

5.0 REFERENCES

5-1 APPENDIX A Palo Verde 1 Cycle 1 Guide Tube Wear Eddy Current Test Data APPENDIX B Palo Verde 1 Cycle 1 Fuel Assembly Dimensional Change Data i

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List of Tables Table Title Page 1 PVNGS-2 Fuel Assemblies Selected for 1-2

.- Examinations Figure List of Figures Page 1 Cycle 1 Core locations of PVNGS-2 Fuel 2-2 Assemblies Inspected for Guide Tube Wear 2 ECT Voltage vs. Guide Tube Wear Volume 2-3 for PVNGS-2 3 Guide Tube Growth (PVNGS-1 20C-1) 33 4 Shoulder Gap Decrease (PVNGS-2 E0C-1) 3-4 5 Guide Tube Growth (PVNGS-2 EOC-1) 3-5 6 Fuel Rod Growth (PVNGS-2 E0C-1) 3-6 A-1 Guide Tube Identification Format A-1 B-1 Fuel Assembly and Fuel Rod Identification B-1

. Format ii

1.0 INTRODUCTION

This report documents fuel examinations conducted during the End-of-Cycle 1 refueling outage at Palo Verde Nuclear Generating Station -

Unit 2. The inspections were performed to fulfill examination require-

.- ments for E0C-1 that are specified by the PVNGS-2 operating license. The examinations conducted at E0C-1 include:

Eddy Current Testing of Assembly Guide Tubes for Wear Dimensional Measurements to Characterize Fuel Rod and Assembly Growth A total of 1/ assemblies were inspected. Table 1 lists the assemblies and identifies the specific examinations performed on each.

l 1-1 l

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Table 1 PVNGS-2 Fuel Assemblies Selected for Examinations Core Examinations Assygply Discharged Location Guide Tube Dimensiogy) CEA HfH EOC-1 Cycle-1 Wear Measures Type A057 yes R11 x

A062 yes H12 x 4 center fingers of a 12-finger CEA i A063 yes F4 x 4 center fingers of a 12-finger CEA

] A024 yes L3 x 4 finger part-length CEA A046 yes G15 x 4 finger part-length CEA A036 yes H8 x A059 yes N15 x B109 yes C8 x g B119 yes L7 x

4 B137 yes K2 x 4 center fingers of a 12-finger CEA B144 yes F3 x 4 outer fingers of two 12-finger CEAs P1B226(3) no 11 7 x x 4 outer fingers of two 12-finger CEAs B205 no B11 x C005 no J17 x x 4 finger CEA CO25 no C15 x x 4 finger CEA C112 n x ngers of a 12-finger CEA PIC114(3) no R4 _ _x 17 10 10 III Shoulder gap and guide tube length.

Assembly serial numbers are prefixed with "P2" unless otherwise specified.

Plxxx denotes fuel assemblies initially scheduled for PVNGS-1.

2.0 GUIDE TUBE WEAR EVALUATION This section describes the evaluation of the guide tube wear measurements

taken on ten PVNGS-2 fuel assemblies following Cycle 1. The selection of the measured fuel assemblies, establishment of a wear criterion, and extrapolation of the measured wear were all based on knowledge gained by C-E over nearly ten years of experience. Detailed information regarding this experience base is included in Section 2.0 of Reference 1. Also included in this reference are the evaluation results of the twenty PVNGS-1 fuel assemblies inspected after Cycle 1. Based on those favor-able results (a maximum projected wear volume of only 25% of the allow-able wear volume), the number of PVNGS-2 fuel assemblies inspected was reduced from twenty to ten.

Details on the ten fuel assemblies selected for examination following Cycle 1 are provided in Table 1, and their locations in the core are shown in Figure 1. It can be seen that all of the various CEA geometries are represented in the sample, and that in general the assemblies were located close to the reactor outlets. Each of the four outer guide tubes of the ten fuel assemblies were inspected with an eddy current testing (ECT) probe.

2.1 Evaluation of Guide Tube Wear Data The inspection of the ten PVNGS-2 fuel assemblies .u guide tube wear employed an improved ECT probe design compared to the ECT probe design l used for the PVNGS-1 inspections. The new probe design resulted in a

-' slightly different relationship between ECT voltage and guide tube wear volume. This relationship, shown in Figure 2, was again derived by using

-' the ECT probe to inspect calibration standards (actual Zircaloy guide I

tube stock with known geometries of mechanical flaws on the inner dia-meter).

l 2-1 l

l

Figure 1 Cycle 1 Core Locations of PVNGS-2 Fuel Assemblies Inspected for Guide Tube Wear

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1.EGEND:

S SPARE 4-FINGERED CEA Note: Reactor outlets are on the core centerline at the top and bottom of the diagram.

2-2

Figure 2 ECT VOLTAGE VS. GUIDE TUBE WEAR VOLUME FOR PVNGS-2 O 4 se e

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.. i i i r 0 1 2 3 4 ECT VOLTAGE 2-3

The ECT measurements are sumarized in Appendix A. The reported data include the serial number of the fuel assembly inspected, the ECT volt-age, location, and axial extent of any wear indication for each of the guide tubes within the fuel assembly. Figure A-1 shows the C-E conven- .

tion used when identifying individual guide tubes.

2.2 Evaluation Results The evaluation of guide tube wea/ is based on wear volumes. The _

analy _

tical technique, including the development of a volume loss of-as a limiting wear criterion, are discussed in Reference 1. The respits' of the PVNGS-1 inspection showed a maximum projected wear volume after threecyclesofoperationunderaCEAtobe[ ].Sincethis maximum projected value was well below the criterion of { ],itwas concluded that the guide tube wear data verified that PVNGS-1 fuel assemblies were acceptable for operation without guide tube modification (wear sleeves). Similarly, it could be concluded the PVNGS-2 fuel assemblies are acceptable without wear sleeves provided their wear data were bounded by the PVNGS-1 wear data.

A direct comparison of the ECT voltages from PVNGS-1 and PVNGS-2 is not appropriate because of the differences in the ECT probe designs and differences in the operating times of the two plants. The proper para-meters to compare are the maximum projected wear volumes for three cycles of operation. Asstatedabove,thisvalueis[ [forthePVNGS-1 data. Based on a conservatively large wear volume associated with the PVNGS-2 data and its extrapolation to three cycles, the PVNGS-2 value is less than half the PVNGS-1 value. Therefore, since the PVNGS-2 wear e extrapolation is less than the PVNGS-1 wear extrapolation, and since the PVNGS-1 wear evaluation confirmed that sleeves were not required, it is concluded that the PVNGS-2 fuel assemblies do not require wear sleeves.

2-4

3.0 FUEL ASSEMBLY DIMENSIONAL CHANGE EVALUATION

. This section describes the evaluation of the shoulder gap (distance between the top of the fuel rods and the bottom of the upper end fitting) y ., and guide tube length measurements taken at PVNGS-2 during the E0C-1 outage. A total of ten fuel assemblies wore inspected; three Batch A,

.. four Batch 8, and three Batch C. The specific fuel assemblies inspected are identified in Table 1. The shoulder gap of peripheral fuel rods on the fcur faces of the length of each fuel assembly were measured opti-cally using a periscope, while each of the four guide tubes was measured using the guide-tube length-measurement tool.

3.1 Pre-Shutdown Evaluation The shoulder gap evaluation for PVNGS-2 fuel parallels the method used for PVNGS-1, i.e., predictions of the remaining shoulder gap were based on the minimum available shoulder gap at the beginning of life (BOL), a conservatively high fuel rod growth prediction, and a conservatively low guide tube growth prediction. Both the PVNGS-1 and PVNGS-2 evaluations adjust the available shoulder gap at BOL to account for component dimen-sion21 tolerances, elastic compression of the guide tubes, and differen-tial thermal expansion between the fuel rods and the guide tubes. Both evaluations also employ a fuel rod growth rate that represents more i

growth than the 95/95 upper limit for the distribution of data from the batch whose high fluence rods had the highest observed growth rates of any fuel examined by C-E, (Arkansas Nuclear One Unit 2 Batch C). The difference in the Cycle 2 evaluations of the PVNGS-1 fuel and the PVNGS-2 fuel is the treatment of the guide tube growths.

j:

As discussed in Reference 1, the shoulder gap evaluation for the PVNGS-1

!.- fuel used a conservatively low guide tube growth prediction calculatod using the methods described in Reference 2. In order to accomodate the higher EOC-2 fluences at PVNGS-2, the PVNGS-2 3-1

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l evaluation uses the PVNGS-1 measurement data to reduce the excessive amount of conservatism in the guide tube growth predictions associated with the method i

of Reference 2. The minimum guide tube growth required to prevent shoulder gap closure for the limiting fuel rod in PVNGS-2 Cycle 2.is calculated. The growth rate associated with this required growth and the PVNGS-1 data are  ;

shown in Figure 3. The margin between the actual data and the calculated p p- growth rate indicates that the guide tube growths' of the PVNGS-1 fuel assemblies, extrapolated to the appropriate fluence, will all be in excess of the minimum guide tube growth required at E0C-2 for the PVNGS-2 fuel.

Therefore, a: long as the PVNGS-2 guide tube growth data show similar margin, ,

the use of the minimum required guide tube growth can be concluded to be l conservative for the PVNGS-2 Cycle 2 shoulder gap evaluation, i

3.2 Dimensional Change Data l

The individual shoulder gap measurements are tabulated in Appendix B, Tables 8-1 through B-10. For each shoulder gap measured, the tabulation  :

also contains the initial shoulder gap (the nominal value from the design ,

drcwings) .the resulting shoulder gap change (initial gap - E0C-1 gap),

the inferred fuel rod growth (shoulder gap change pit.s guide tube  ;

i growth), fuel rod growth strain (fuel rod growth / active length), and the fuel rod's axial average fast fluence. Guide tube information (average j growth and average fluence) is included-at the bottom of each fuel r assembly's shoulder gap tabulation. The shoulder gap change data, guide tube growth data, and fuel rod growth data are plotted relative to the appropriate fast fluence in Figure 4, 5, and 6, respectively.

1 3.3 Post-Shutdown Evaluation Fuel rod growth data are shown in Figure 6 along with the design basis

-' taken from the ANO-2 Batch C data w The figure shows that the high fluence data are all below the design 1 3-2 ,

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e GUIDE TUBE GROWTH .

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1 basis and the trend of the data is for increased margin at higher fluences. Therefore, it is conservative to use the fuel rod growth model when predicting limiting shoulder gap changes.

1 -

Guide tube length change data for the PVNGS-2 fuel are shown in Figure 5, along with the minimum required guide tube growth rate discussed in

.- Section 4.1 The figure shows similar margin for the PVNGS-2 measurements as Figure 3 shows for the PVNGS-1 measurements. Therefore, the use of the minimum rquired guide tube growth can be concluded to be conservative for the PVNGS-2 Cycle 2 shoulder gap evaluation.

The fuel rod growth data and the guide tube growth data from PVNGS-1 and PVNGS-2 at EOC-1 have confirmed the conservations of the analytical modeling used in the shoulder gap evaluation of the PVNGS-2 Cycle 2 fuel.

Therefore, since the shoulder gap evaluation verified that the limiting fuel rod in Cycle 2 had sufficient shoulder gap and since the analytical modeling used in the evaluation has been shown to be conservative, it is concluded that the fuel in PVNGS-2 Cycle 2 is acceptable with respect to shoulder gap.

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4.0

SUMMARY

AND CONCLUSIONS l

Guide tube wear originating from the mechanical interaction between guide tubes and CEAs was first observed by C-E in 1978. Since that time, C-E

has established several surveillance programs to ensure significant ,

margin to the limiting wear criterion. A program of this type was

.- implemented for the System 80 design.

Ten fuel assemblies from PVNGS-2 were selected for guide tube wear examination following Cycle 1. The assemblies examined represent all combinations of CEA types and geometries. The selections were biased towards regions of the core which have higher than average coolant flow rates; areas expected to generate more severe wear. A total of 40 guide tubes were examined bringing the total C-E experience with System 80 guide tubes to 120 (80 from PVNGS-1).

The criterion used to evaluate the results was based on deterministically conservative assumptions of wear geometry, loading severity, and material properties. This criterion was the same as that used in the original decision to operate the System 80 fuel type without protective wear sleeves.

The evaluation of all wear measurements showed that the most limiting of the 120 measured guide tubes (total System 80) had acceptable wear. Its wear rate was less than that determined in the original flow tests of the System 80 design. Extrapolation of the wear to three cycles of operation demonstrated significant margin to the guide tube wear limit criterion.

l The effects of core shuffling and of fuel exposure to the reactor environ-

ment lead C-E to conclude that no case of guide tube wear will be as severe as predicted by the extrapolation.

1

• The inspection samples and the evaluation results frem PVNGS-1 and PVNGS-2 support the continued operation of all System 80 fuel assemblies

through the completion of their design life without guide tube modifica-

! tion (wear sleeves).

4-1 l

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Dimensional measurements of peripheral fuel rod shoulder gap and of guide tube lengths were performed on ten PVNGS-2 fuel assemblies following Cycle 1. Fuel rod growth data, determined from the measurements, indi-cate that the growth of high fluence fuel rods is less than the growth predicted by the model used to determine design limits for shoulder gap.

In addition, the trend of the data is for an increasing margin between

,. rod growth and the design basis at higher fluences. The measured guide tube growths are greater than the growths predicted by the growth rate associated with the minimum guide tube growth required at E0C-2.

Based on the fuel assembly dimensional measurements performed at P,VNGS-1 and PVNGS-2, the C-E models for predicting guide tube growth and fuel rod growth have been shown to be conservative. As a result, adequate margin for shoulder gap reduction exists in all fuel assemblies designated for operation in PVNGS-2 Cycle 2. In addition, it is concluded that the shoulder gap evaluttion technique is acceptable for determining the fluence capabilities of PVNGS fuel. Therefore, comparisons of fluence capabilities and peak fuel rod fluence can be made for subsequent cycles to verify the acceptability of the shoulder gap of the operating fuel.

9 6

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5.0 REFERENCES

(1) CE NPSD-4'28-P, "Palo Verde Nuclear Generating Station - Unit 1 End-of-Cycle 1 Fuel Examination Report", December, 1987.

(2) CE NPD-269-P, Rev. 1-P. "Extended Burnup Operation of Combustion

,- Engineering PWR Fuel", July, 1984.

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Appendix A

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Figure A-1 Guide Tube Identification Format SDIAL NUtfB R

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E00Y-CURRENT GUIDE TUBE WEAR DATA i

Assembly Number Guide Tube Number Voltage Axial Axial Location Extent of From Top Indication of Post (Inches)

(Inches)

~

2A024 1

, 2 3

4 23137 1 2

3 4

23144 1 2

3 4

2C005 1 2

3 4

.' 2C112 1 2

3

{ , _ -

N.D. - Nothing Detectable l

t A-2 l

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E00Y-CURRENT GUIDE TUBE WEAR DATA Assembly Number Guide Tube Number Voltage Axial Axial Location Extent of Trom Top Indication of Post (Inches)

(Inches) 13226 1 -

2 '

3 4

2A068 1 2

3 4

2A062 1 2

3 4

2A046 1 2

3 4

20025 1 2

3 4

, N.D. - Nothing Detectable i

A-3

t 4

Appendix 8 I

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0 1 .

Figure B 1 Fuel Assembly and Fuel Rod Identification Format

. aisi n upper end fitting assembly  %, ,

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O B-1

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I FUEL ASSEMBLY DIMENSIONAL MEASUREMENTS ASSDBLY SDIAL NO. P2A036 )

l FACE: h0ATM (0) FACE: iAST (90) 1 CYl EOC 1 6AP RO) 6RCtTH CY ! EOC ! 6AP A00 GRCWTH 80L SAP FLUENCE SM. SAP CECAGSEBRCWTH SilAIN BOL GAP FLUEN;t SH. 6AP DECREASE GROWTH STRAlh E00 (ta.) (E)0.821) (In.) (in.) (la.) (1) ECD (in.) (E)0.821) (In.) (in.) (In.) (1) sanantsumines sessinessasunsunnunesassionsenssa,a au ssnes sa nss issis e sa nssp en sa n sa ss es sa ss ansassess as se na 1 1.682 3.785 1 1.682 3.810 2 1.682 3.793 2 1.682 3.816 3 1.682 3.800 3 1.682 3.821 4 1.682 3.805 4 1.682 3.824 5 1.682 3.809 5 1.682 3.826 6 1,682 3.815 6 1.682 3.831 7 1.682 3.822 7 1.682 3.835 I 1.682 3.826 8 1.682 3.838 t 9 1.682 3.825 9 1.682 3.837 10 1.682 3.821 10 1.682 3.B31 11 1.682 3.813  !! 1.682 3.822 12 1.682 3.606 12 1.682 3.815 13 1.682 3.802 13 1.682 3.B09 14 1.682 3.796 14 1.682 3.803 15 1.682 3.789 15 1.682 3.794 16 1.682 3.780 16 1.682 3.785 FACE: SOUTH (180) FACE: WEST (270)

CY I EDC-1 SAP ROD BROWTH CY ! EDC-1 6AP R00 SRDWTH IOL SAP FLUENCE SH. 6AP DECREASE GRDWTH STRAIN 80L 647 FLUENCE SW. SAP DECREASE GRONTH STRAIN 200 lis.) (E)0.821) (1s.) (in.) lla.) (I) ROD (le.) (E)0.821) (la.) (In.) (ie.) (1) n sessma n n ie n .s u n se n se n .. n n ou n ne .. assen n.nusessissarissaan ... s...

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I 1.682 3.790 l I.682 3.780 2 1.682 3.799 2 1.682 3.739 3 1.642 3.'07 3 1.682 3.796 4 1.682 3.813 4 1.682 3.803 5 1.682 3.020 5 1.682 3.909 6 1.682 3.826 6 1.682 3.815 7 1.682 3.835 7 1.682 3.823 8 1.682 3.841 B 1.682 3.828 9 1.682 3.843 9 1.682 3.830 10 1.682 3.838 10 1.682 3.825 11 1.682 3.833  !! 1.682 3.819

!2 1.682 3.828 12 1.682 3.813 l 13 1.682 3.B25 13 1.682 3.809 14 1.682 3.822 14 1.682 3.304

. 15 1.682 3.816 15 1.682 3.797 16 1.682 3.810 -'

16 1.682 3.790

. 11 NOMihAL BOL SHOUL ER 6AP 1.682in. h0TE: ALL REPd TED FLUENCE hCMSERS ARE I 10 EE 21 N/CMie2 FI,UDCES CALCULATED TOR E)0.821 ARE ADJUSTED TO ACTUAL SURNUP OF 44B ETPD

2) AVEAAit SUICE Tuit siCain [ ]

3) AVDA6E GUIEE TUlf FLUDCE: 3.164 41 AV6. BOL RCD ACTIVE LEh6TH:  !!0in.

B-2

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FUEL ASSEMBLY DIMENSIONAL MEASUREMENTS ASSEMBLY SERIAL h0. P24057 FAtti NORTH (0) FACE: UST (90)

CY l EOC 1 SAP RCD BROWTH CY I EOC 1 SAP RCD BRCNTH BOL BAP RUENCE SH. SAP DECAUSE GROWTH STRAIN 90L 6AP RUEWCE SH. SAP DECREASE 6tCWTH STRAIX RCD (ts.) (E)0.821) (Ia.) (in.) lis.) (1) 20D (la.) (E)0.8211 lia.) (in.) lin.) II) unn u u n ....n ....n. n u.. n ...u nun un .n .. uns n.n... n mune.

I 1.682

• 3.729 1 1.682 3.762 2 1.682 3.733 2 1.682 3.764

,- 3 1.682 3.735 3 1.682 3.78 4 1.682 3.735 4 1.682 3.7M 5 1.682 3.734 5 1.682 3.78 6 1.682 3.732 6 1.682 3.769 7 1.682 3.731 7 1.682 3.U2 8 1.682 3.727 8 1.682 3.U4 9 1.682 3.718 9 1.682 3.U2 10 1.682 3.702 to 1.682 3.765 11 1.682 3.68$  !! 1.682 3.758 12 1.682 3.M7 12 1.682 3.751 13 1.682 3.649 1,3 1.682 3.747 14 1.682 3.631 14 1.682 3.742 15 1.682 3.611 15 ' l.682 3.735 16 1.682 3.589 16 1.682 3.729 ,

FACE: SOUTH (180) FACE: NEST (270)

CY I EDC 1 GAP R00 GRONTH CY l EDC-1 SAP R00 GROWTH BOL BAP FLI O CE SH. SAP DECREASE SRCWTH STRAIN NL GAP FLUENCE SH. SAP DECREASE GROWTH STRAIN RCD (In.) (E)0.821) (is.) (in.) lis.) (!! R00 (1s.) (E)0.821) (in.) (in.) (la.) (I) u ..n==== y n .= n n==. u una .,. . une. unn 1 1.682 3.620 1 1.682 3.589 2 1.682 3.646 2 1.682 3.590 3 1.682 3.670 3 1.682 3.593 4 1.682 3.690 4 1.682 3.595 5 1.682 3.709 5 1.682 3.597 6 1.682 3.729 6 1.682 3.603 '

7 1.682 3.747 7 1.682 3.610 8 1.682 3.762 8 1.682 3.617 9 1.682 3.UI 9 1.682 3.619 10 1.682 3.U5 10 1.682 3.618 11 1.682 3.U5  !! 1.682 3.616 12 1.682 3.D5 12 1.682 3.615

,. 13 1.682 3.U5 13 1.482 3.617 14 1.682 3.U3 14 1.682 3.619 15 1.682 3.769 15 1.682 3.619

,- 16 1.682 3.762 16 1.682 3.620 ,

il WOMINAL BOL SHOULS B GAP. 1.682 in. N3TE: ALL REPORTED FLUENCE NtRID S ARE I 10 EE 21 N/CM *2 RUDCES CALCL". ATE 3 F08 !)0.321 ARE ANUSTED TO ACTUAL BURWUP OF 449 grPD

2) AVEHE 9)lCE TU!E EtCWTW. [ ]

3) AVERT.it SultE Tult FLUDCE. 3.071 *

4) AVI. BOL RCD ACilVE LEW6TH. 150 in.

B-3

o..

FUEL ASSEMBLY DIMENSIONAL MEASUREMENTS A55EN8LY SERIAL NO. P24059  !

PCE: NORTH (0) FACE: EAST (901 CY t EOC 1 BAP ADO $RONTH CY l i

EOC-1 GAP R00 GROWTH  !

3(N. SAP FLUENCE SH. SAP MCAEASE BRONTH STRAIN 80L BAP FLUENCE SH. SAP MCAEASE 8RONTH Site!N ROD fla.) (E)0.821) ' lla.) (la.) tia.) (1) R0D lin.) (E)0.821) (ts.) (in.) lin.) (1) u s . = m m = = u n e. m = == = u u m = = = = = u nuunuunu aau u.a.====

1 1.682 3.409 1 1.642 .699 '

1.682 3.391 2 1.682 3.695 3 1.682 3.371 3 i.682 3.687 4 1.642 3.350 4 1.642 3.676 5 1.682 3.328 1.682 5 3.644 6 1.682 3.309 6 1.682 3.651 7 1.682 3.290 7 1.682 3.644 I 1.682 3.272 8 1.682 3.626 9 1.642 3.248 9 1.642 3.606 10 1.682 3.223 10 1.682 3.580

!! 1.682 3.196 11 1.682 3.552 12 1.682 3.171 12 1.682 3.524 13 1.682 3.149 13 1.682 3.496 14 1.682 3.127 14 1.682 3.464 15 1.682 3.104 1.682 15 3.439 16 1.682 3.004 16 1.682 3.409 FACE: SOUTH (100) FACE: ut$T (270)

CY I EOC1 GAP A00 IROUTN CY l EOC-1 IAP R00 EROUTH BOL BAP FLUENCE SH. SAP M CREASE IRouTW STRAIN 90L BAP FLUENCE SH. SAP M CREASE BROUTH STRAIN Rol lin.) (D0.821) (la.) tin.) (In.) (1) R00 (in.) (E)0.821) (la.) (in.) (la.) (1)

=== = m=== == u g .==u=-- -

I 1.682 3.647 1 1.682 3.004 2 1.682 3.652 1.682 2 3.143 '

3 1.682 3.659 3 1.682 3.200 4 1.682 3.666 4 1.682 3.253 5 1.682 3.672 5 1.682 3.305 6 1.682 3.681 1.682 6 3.356

• 7 1.682 3.691 1.682 7 3.404 8 1.642 3.700 I 1.682 3.450 9 1.682 3.704 9 1.682 3.489 10 1.682 3.706 10 1.642 3.521

!! 1.682 3.703  !! l.682 3.548 12 1.682 3.703 12 1.682

' .575 13 1.682 3.704 13 1.692 3.599 4 2 14 1.682 3.704 14 1.6B2 3.620

!! 1.682 3.702 15 1.682 3.636 16 1.682 3.699 16 1.682 3.647

= .

1) NOMINAL 30L SHOULDER 64Ps 1.682in. NOTE: ALL REPORTED FLUENCE NLP.S. 't I 10 EE 21 N/Cnes2

2) AVERAGE BulDE TUM SECUTH: [ ] FLUENCES CALC'JLATEL FCR E)0.h.

• CSTE: T3 f.CT'#.;. ETEF GF 446 EFF0 '

3) AvfAASE SUISE TUM FLUENCIs 2.899

4) AVS. SQL RDD ACT!VE LINETHs  !!0 in.

B4

( _ - - - - . - - _ _ - - - - - - - - --- -

FUEL ASSEMBLY O!MENSIONAL MEASUREMENTS ASSEMBLY SEA!AL NO. P28109 FACE: NORTH (0) FACE: EAST (90)

CY I EDC 1 SAP 200 EROWTH CTI EDC 1 Sp R00 GROWTH SCL 6# FLUENCE SH. $U XCR D SE BA0WTH STRAIN 80L S W FLUENCE SH. 6AP MCADSE6RONTH STRAIN RCD (la.) (D0.821) (ie.) (la.) (la.) (1) R00 (la.) (E)0.8211 (la.) (fa.) (fa.) (1) sn .. u m ..un ..m..w.unua u .m au u .u. u.a. nu u.. u = .,

I 2.382 3.594 1 2.382 3.540 2 2.382 3.623 2 2.382 3.!!t 3 2.382 3.732 3 2.342 3.659 4 2.382 3.764 4 2.382 3.682 5 2.382 3.784 5 2.382 3.695 6 2.382 3.803 6 2.382 3.707 7 2.382 3.827 7 2.382 3.724 8 2.382 3.848 8 2.382 3.740 9 2.382 3.856 9 2.382 3.744 10 2.382 3.853 10 2.382 3.737

!! 2.382 3.645  !! 2.382 3.726 12 2.382 3.843 12 2.382 3.720 13 2.382 3.840 13 2.382 3.716 14 2.382 3.825 14 2.382 3.700 15 2.382 3.730 15 2.382 3.607 16 2.382 3.716 16 2.382 3.594 FACE: SOUTH (150) FACE: EST (270)

CY ! EDC-1 6AP R00 GRDWTH CTI EDC-1 6AP R00 SROWTN 30L SAP FLUENCE SH. EU K CREASE GROWTH STRA!E 80L SAP FLUENCE SH. SAP DECREASE SADWTH STRAIN RQD (la.) (DO.821) (ie.) (la.) (ie.) (1) RCD (la.) (E)0.821) (la.) (fa.) (la.) (3)

• ~ ~

~

I 2.182 3.673 l 2.382 3.716 2 2.382 3.681 2 2.382 3.724 3 2.382 3.768 3 2.382 3.814 4 2.!82 3.774 4 2.382 3.824 5 2.382 3.7T3 5 2.!82 3.825 6 2.382 3.772 6 2.382 3.828 7 2.382 3.775 7 2.382 3.836 8 2.382 3.776 8 2.382 3.843 9 2.!B2 3.768 9 2.362 3.841 10 2.382 3.749 10, 2.382 3.828 11 2.382  !.727 11 2.382 3.814 12 2.382 3.710 12 2.322 3.805 13 2.382 3.692 13 2.382 3.797 14 2.342 3.6e7 14 2.382 3.782 1: 2.3E2 3.565 15 2.382 3.638 16 2.382 3.!40 16 2.382 3.673

1) NOMINAL POL SHOUL3ER 6AP. nCTE: Att REPCRTED FLLThCE NUM$ERS ARE I 10 EE 21 ulCMe*2

2) AVEAant Sult! TUN GROWTH.

(2.!82in.}

3) AVERA6E GUIDE TUM FLUEM;E. 3.!!5 TLUENCES CgA,TfD FC7 E)0.821 AILE ANUSTED TO ACTUAL IURM9 CF 448 EF

4) AV6. 80L RCD ACTIVE LfhETH. 150 in.

t-

I FUEL ASSEMBLY DIMENSIONAL MEASUREMENTS ASSEMBLY SD!AL WO. P28119 FACI: NCATH (0) FACE: EAST (101 '

CY ! ECC 1 SAP A00 GROWTH CY l EOC1 6AP ROD SA0WTH BOL SAP FLUDCE $H. SAP DECREASE GROWTH $ TRAIN BOL GAP FLUENCE SH. SAP DECREASE 6ROWTH STRAIN 200 (la.) (E)0.8211 lin.) (in.) tin.) (2) ROD (in.) (E)0.821) (in.) (in.) lin.) (I) -

ana n m nga u.au u a n .n..n.a ns. nw ... un nuunsa a . na gg.

2.382 3.721 1 2.382 3.716

.- 2 2.382 3.U5 2 2.382 3.731 3 2.382 3.834 3 2.382 3.830 4 2.382 3.853 4 2.382 3.847 5 2.382 3.841 5 2.382 3.855 6 2.382 3.848 6 2.382 3.844 7 2.382 .883 7 2.382 3.878 8 2.382 3.895 8 2.382 3.890 9 2.382 3.895 9 2.382 3.890 10 2.382 3.884 10 2.382 3.879

!! 2.382 3.844 11 2.382 3.845 12 2.382 3.842 12 2.382 3.858 13 2.382 3.rl4 13 2.382 3.851 14 2.382 3.835 14 2.382 3.B33 15 2.382 3.n8  !$ 2.382 3.35 16 2.382 3.722 16 2.382 3.721

- - ~ ~

FACE: SCt'TH (180) FAQ: WEST (270)

CY ! EDC 1 GAP ROD GROWTH CY l EDC 1 SAP ROI IRONTH BOL BAP FLUDCE SH. SAP XCREASE GRDWTH STRAIN BOL GAP FLUENCE SH. SAP DECREASE GROWTH STRAIN RCD (ie.) (E)0.8211 (is.) (in.) (i.e. ) (1) R00 (ie.) (E)0.821) (in.) (in.) (is.) (1) n = wi.aus. an== unn . w u == uunsanun=neuen===== == n a

~ ' ' '

1 2.382 3.71b  ! 2.382 3.722 2 2.382 3.nl '2 2.382 3.737 3 2.382 3.828 3 2.382 3.835 4 2.382 3.846 4 2.382 3.853 5 2.382 3.854 5 2.382 3.859 -

6 2.382 3.862 6 2.382 3.547 7 2.382 3.876 7 2.382 3.881 8 2.382 3.587 8 2.382 3.893 9 2.382 3.887 9 2.382 3.892 le 2.382 3.876 10 2.3 82 3.879 11 2.382 3.862 11 2.382 3.865

12 2.382 3.854 12 2.382 3.856 13 2.382 3.846 13 2.382 3.848 14 2.382 3.828 14 2.382 3.830

.' 15 2.382 3.30 15 2.382 3.nl 16 2.382 3.716 16 2.382 3.716 11 WCMl U L 3CL ! C ".3ER 3 V $ 3.!32in. h3its ALL REFC4 tid su;ihCE asmiEAS AAE I 10 EE 21 m/C.=u2

2) AVERA&E BUlt! TUBE iR WTh FLLDCES CALCULATED FCR E)0.821 ARE ANU$iED TO ACTUAL ILOUP CF 448 ETPD

3) AVEAAGE $UIDE TUBE FLUD;E. [3.072 ]

4) Avl. IDL ROD Active LEh6TH.  !!0 in.

B6

I FUEL ASSEMBLY DINENSIONAL MEASUREMENTS AS$1MILY SDIAL WO. 728205

~

FA;E G TH (0) FACE: [AST (901 CY l [0C1 $AP A00 SA0WTH CYl ECC1 SAP RQD GROWTH SQL 6AP FLUEKE SH. SAP M CREASE GADWTH STRAIN 81 BAP FLUENCE SH. SAP XCREASE GROWTH STAAlk RO) (in.: (E)0.821) (la.) (la.) (la.) (I: RCD lia.) (E)0.821) lin.) (in.) Ila.) (3) un suunnemansinnunna. senannn anunn une...un nm nnuesunune.nne ununa I 1.642 2.985 1 1.682 3.161 2 1.682 3.035 2 1.682 3.159

, 3 1.682 3.155 3 1.682 3.225 4 1.682 3.212 4 1.682 3.22 4 5 1.682 3.258 5 1.682 3.215 6 1.682 3.305 6 1.682 3.207 7 1.682 3.357 7 1.682 3.205 8 1.682 3.406 8 1.682 3.201 9 1.682 3.442 9 1.582 3.189 10 1.682 3.466 10 1.682 3.169 11 1.682 3.486  !! 1.682 3.146 12 1.682 3.511 12 1.682 3.130 13 1.682 3.534 13 1.682 3.!!4 14 1.682 3.544 14 1.682 3.091 15 1.642 3.478 15 1.682 3.005 16 1.682 3.444 16 1.e42 2.985

- =

FACE: SOUTH (180) FACE: WEST 1270)

CY ! 20C 1 6AP A00 GRCWTH CY ! EOC-1 SAP ADO 6A0WTH 30L BAP FLUECE SH. SAP MCREASE 640WTH STRAIN BOL SAP FLUENCE SH. SAP MCREASE GROWTH STRAIN 1:00 (la.) (D0.821) (la.) (ta.) (la.) II) ROD (la.) (D0.821) (la.) (in.) (fa.) (I) une..m un===.mme um . nom n une. unu m.

~ ' ~

.. unne. n nnn'

! 1.682 3.504  ! 1.682 3.484 2 1.682 3.496 2 1.682 3.483 3 1.682 3.566 3 1.682 3.561 4 1.682 3.559 1.682 4 3.566 5 1.682 3. 54 3 1.682 5 3.566 6 1.682 3.!25 6 1.682 3.568 7 1.682 3.514 7 1.682 3.578 8 1.682 3.101 8 1.682 3.!89 9 1.682 3.476 9 1.682 3.392 10 1.682 3.440 10 1.682 3.586 11 1.682 3.402 11  !.682 3.579 12 1.682 3.370 12 1.682 3.580

. 13 1.682 3.!39 13 1.682 3.585 r 14 1.682 3.299 1.682 14 3.582 i 15 1.482 3.193 15 1.682 3.504 16 1.682 3.161 16 1.682 3.504

~

l l  :) O !NAL 8;L SHOULI G GAP. 1.682in.

• N0ft: ALL REPORTED FLUEhCE WUMlERS ARE I 10 El 21 N/CMa*2

{

l

2) 4VER$5! S'J1 t it!! tRO)Tw (

3) AVERAGE BUIM TUBE F1,UENCt. 2.829

} FL',u: s ;;LCaATE; Fca 00,g21 ARE A;;g3TE; TO ACTLAL iidhuP GF 448 [FFD l

41 AV6. 80L R;D ACTIVE lek 6TH  !!Oin. .

B7

FUEL ASSEMBLY O!MENSIONAL MEASUREMENTS ASSEMILY SDIAL bO. P18226 FACE: NORTH (0) FACI: EAST (90)

CY l EOC 1 6AP R0D BA0WTH CY ! EOC 1 SAP RCD SA0WIR 80L 6AP FLUENCE SW. SAP MCROSE GROWTH STRAIN 80L 6AP FLLINCE SH. SAP MCRO SE GROWTH STRAIN R08 (la.) (D0.821) ' lin.) (la.) (in.) (1) ROD (is.) (E)0.821) (In.) (in.) (in.) (1) nm u ..uns ,g n an an aus. u . n u .u

.. n u n u s..,. ..n n ....u su u n .. ,a i 1.642 3.717 1 1.682 3.718 2 1.682 3.722 2 1.682 3.732 3 1.682 3.810 3 1.682 3.830 4 1.682 3.819 4 1.682 3.847 5 1.682 3.820 5 1 682 3.855 6 1.682 3.822 6 1.642 3.862 7 1.682 3.831 7 1.682 3.877 8 1.682 3.838 8 1.682 3.888 9 1.682 3.837 9 1.682 3.888 10 1.682 3.826 10 1.682 3.876 11 1.682 3.814  !! 1.682 3.862 12 1.6 82 3.809 12 1.682 3.854 13 1.682 3.804 13 1.682 3.842 14 1.682 3.773 14 1.682 3.82h 15 1.682 3.702 15 1.6E2 3.730 16 1.682 3.692 16 1.682 3.717 FACE

SOUTH (180) FACE: WEST (270)

CY I EOC 1 SAP A00 GRCWTH CY ! EDC-1 SAP R00 IROWTW 80L SAP FLUENCE SH. SAP MCAEASE SACNTH STRAIN 80L BAP FLUENCE SW. SAP MCREASE SkOWTW STRA!I RCD (1s.) (D0.821) (ln.) (in.) (la.) (1) R00 (la.) (E)0.821) (1s.) (ie.1 (ls.) (1) an=== n a== gne. a == m un nu . nn =. wus... ==

I 1.682 3.612 1 1.682 3.692 2 1.682 3.702 2 1.682 3.702 3 1.682 3.793 3 1.682 3.792 4 1.682 3.805 4 1.682 3.803 5 1.682 3.810 5 1.682 3.806 6  !.682 3.81: 6 1.682 3.811 .

7 1.682 3.827 7 1.682 3.822 8 1.682 3.838 8 1.682 3.832 9 1.682 3.640 9 1.682 3.832 10 1.682 3.832 10 1.682 3.822

!! 1.642 3.823  !! 1.682 3.811 12 1.682 3.821 12 1.682 3.806 13 1.682 3.820 13 1.682 3.803

~

14 1. (82 3.811 14 1.682 3.791 15 1.682 3.723 15 1.682 3.701 I 16 1.682 3.718 m , 16 1.682 3.692

1) h0MINAL 80L SHOL'L D 6AP. 1.482in, hDTE: ALL REPDATID FLLO CE WUm!ERS AAE I 10 EE 21 N/ cme *2

2) AVERASE SUIDE TUSE 6RCWTH.][ FLUENCES CALCULATED F0s no.g21 ARE A:2L'gTO T0 ttiv:L TM.7 CF 44! E7?2

!) AvEAA6E SUIDE TLM FLLINCI. 3.181

4) AV6. BOL ACD ACTIVE LIh6TH. 130 in.

B8 t

FUEL ASSEMBLY DIMENSIONAL MEASURENENTS AS$EMBLY S D!AL NO. P2000$

FACE: NORTM (0)

FACE: EAST (101 CY l EDC1 SAP RCD $ROWTH CT I ECC 1 Sp R00 6ROWTH IOL BAP FLUFF.CE , SH. !# DECREA32 6KCWTH STRAIN FSO lin.) (E)0.821) tin.) tin.) BOL 6# FLUENCE $N. SAP DECREASE GROWTH STRAIX tin.) (!) RCD lia.) (E)0.821) (in.) (la.) (ta.) (1) nesunununuunusanuns . unnuunne asun unuu ssun nuneuu u uu u nnus u nnu u u u u u n i 2.382 1.436  !

! 2.382 3.288 2 2.382 1.437 2 2.382 3.263 3 2.382 1.446

• 3 2.382 3.237 4 2.342 1. 445 8 2.382 3.176 5 2.382 1.445 'i

. 2.382 3.100 6 2.382 1.447 6 2.382 3.011 7 2.382 1.448 7 2.382 2.911 8 2.382 1.448 8 2.382 2.796 9 2.382 1.448 9 2.382 2.M6 10 2.382 1.448 10 2.382 2.524

!! 2.382 1.447 11 2.382 2.369 12 2.382 1.445 12 2.382 2.203 13 2.382 1.445 13 2.382 2.027 14 2.382 1.446 14 2.382 1. 841 15 2.342 1.437 15 2.382 1.637 16 2.382 1.436

- 16 2. 82 1.436 FACE: SOUTH (180)

TACE: WEST (270)

CY ! EDC-1 GAP A00 GROWTH CY! E00-1 SAP R00 GROWTH 80L SAP FLUENCE 94. Se DECRDSE BROWTH STRAIN BOL SW FLUENCE SH. $# DECREASE GRONTH STRAIN R00 (in.) (D0.8211 lin.) (la.) tia.) (1) R08 tia.) (D0.8211 lia.) tia.) tin.) (1)

~ ~

~

1 2.382 3.288 l '

2.382 1.436 2 2.382 3.298 2 2.382 1.637 3 2.382 3.328 3 2.342 1.841 4 2.382 3.335 4 2.382 2.027 5 2.382 3.340 5 2.382 2.203 6 2.382 3.346 '

6 2.!82 2.369 7 2.382 3.351 7 2.382 2.524 8 2.382 3.!!6 8 2.382 2.6M 9 2.382 3.!36 9 2.382 2.796 10 2.382 3.!!! 10 2. 82 2.911 11 2.382 3.346 11 2.382 3.011 12 2. 82 3.340 12 2.382 3.100 13 2.;82 3.3:5

' 13 2.382 3.176 14 2 ;82 3.328 14 2.382 3.237 15 L382 3.218 15 2.382 3.263

, 16 2.382 3.288 16 2.382

, , 3. 288

!) WCMINAL 60L $400L3D GAP = 2.;82ta.

N3TE: ALL REPCRTID FLUENCE WU=lERS ARE I 10 EE 21 R/Che2

2) AVERA6E 6UIDE TU8E GRCWTH [ ] MD I! lAL LIATD TCR D0.521 ALE ANUSTIL 10 Actual IURNUP OF 448 EFPD

3) AVERAGE GUIDE TulE FLUDCE 2.168

4) AY6. SDL RCD ACTIVE LEh6TH: 150 in.

B9

l FUEL ASSEMBLY DIMENSIONAL MEASUREMENTS AtliM8LY SER! Ai, NO. P20025 FACE: NORTH (0) FACE: EAST (90)

CY ! EOC 1 SAP R00 SRONTH CY ! EOC-1 BAP A00 GRONTH BOL SAP FLUENCE .SN. SAP MCREASE GRDWTH STRAIN 80L 6AP FLUENCE SW. SAP MCRE!.M GROWTH STRAIN R0D (in.) (E)0.821) lla.) (ta.1 (in.) (1) ROD lin.) (E)0.821) (in.) (in.) (la.) (!)

nu== =n..=.ma = annmun  ; ..unua nunan .= ann ======- __ mm 1 2.382 0.656 1 2.382 1.971 2 2.382 0.742 2 2.382 1.862 3 2.382 0.831 3 2.382 1.7M i' 2.382 4 0.913 4 2.382 1.45 5 2.382 0.994 5 2.382 1.570 6 2.382 1.075 6 2.382 1. 482 7 2.382 1.154 -

7 2.382 1.398 8 2.382 1.236 I 2.382 1.316 9 2.382 1.316 9 2.382 1.236 10 2.382 . 1.397 10 2.382 1.156

!! 2.382 1.481  !! 2.382 1.075 12 2.382 1.570 12 2.382 0.994 13 2.382 1.M4 13 2.382 0.913 14 2.382 1.7M 14 2.382 0.831 15 2.382 1.861 15 2.382 0.742 16 2.382 1.970 16 2.382 0.656 FACE: SOUTH (180) FACE: MEtt (270)

! C1 1 EOC 1 LAP R00 IRONTH CY ! EDC-1 SAP R00 IRONTH 80L BAP FLUENCE SH. SAP M CREASE GROUTH STRAIN BOL SAP FLUENCE SH SAP MCREASE GROWTH STRAIN R09 (in.) (E)0.821) lia.) (in.1 (la.) (1) 200 (la.) (E)0.821) (ln.) (ta.1 (in.) (1) -

" ' ~ '

1 2.382 3.280  ! 2.382 1.970 2 2.382 3.249 2 2.342 2.107 3 2.382 ,3.228 3 2.382 2.254 4 2.342 3.179 4 2.382 2.380 5 2.382 3.120 5 2.382 2.499 l 6 2.382 3.0!5 6 2.382 2.611 7 2.!82 2.984 7 2.342 2.717 5 2.382 2.905 3 2.382 2.114 9 2.382 2.817 9 2.382 2.903 10 2.382 2.719 10 2.342 2.982

!! 2.382 2.613  !! 2.382 3.052 12 2.382 2.500 12 2.382 3.!!9

. 13 2.382 2.381 13 2.382 3.177 14 2.382 2.255 14 2.382 3.228 15 2.382 2.108  !$ 2.382 3.249

, 16 2.382 1.971 16 2.382 3.230

!) %MlhAL DOL SHOULDER SAPS 2.!I2 in. h0TE: ALL REPORTED FLtEhCE EMIERS ARE I 10 EE 21 N/CMut

2) AVEtAGE SUIDE E !! IROCWs [

31 AVERAGE SUIDE TU M FLUEntEs 1.781

] FU.EA313 C1.LCuu. FED F3R E)0.621 Mit AmSTED TO ACTW.L SuRauP OF 44

4) AV6. 30L ROD ACTIVE LENSTH: 150 is. W = not measured B 10

9 FUEL ASSEMBLY DIMENSIONAL NEASUREMENTS ASSEMBLY SEBIAL 40. PIClle FACE: NORTH (0)

FACE: EAST (101 CY 1 EOC-1 SAP RCD 6ROWTH CY ! E0C 1 SAP R00 SROWTH BOL GAP FLUDCE SM. SAP DECREASE 6ROWTH $ TRAIN RCD tin.) (E)0.821) tia.) tin.) 80L SAP FLUENCE SH. SAP LECREASE GR3WTH $fRAIN lis.) (3) RCD tin.) (E)0.8211 tia.) (in.) tin.)

g ue===un numanm u.ausuun uuuuuun (3) .

1 2.382 3.698 manau uuuuuuu u. nun u.mu .u a 1 2.382 3.571 2 2.382 3.704 2 2.382 3.593 o- 3 2.382 3.795 3 2.382 3.686

'4 2.382 3.805 4 2.382 3.723 5 2.382 3.805 5 2.382 3.740 6 2.382 3.803 6 2.382 3.758 7 2.382 3.809 7 2.382 3.782 8 2.382 3.811 8 2.382 3.803 9 2.382 3.801 .

9 2.382 3.812 10 2.382 3.700 10 2.382 3.811

!! 2.382 3.757 11 2.382 3.805 12 2.382 3.739 12 2.382 3.8%

13 2.382 3.722 13 2.382 3.8%

14 2.382 3.695 14 2.382 3.796 15 2.382 3.:92 15 2.382 3.707 16 2.382 3.571 16 2.!82 3.698

~

. ~

FACE: SOUTH (180)

FACE: WEST 1270)

CY ! ECC-1 GAP R00 GROWTH CY l EOC 1 GAP ROD GROWTH 80L SAP FLUENCE SH. SAP DECREASE GROWTH STRAIN RCD tin.) (E)0.821) tin.) BOL 6AP TLUDCE $H. GAP DECREASE 8RDWTH $fRAIN tia.) lis.) (3) RCD tis.) (E)0.8211 tia.1 (in.)

u.. u . . lis.) (3)

=,un .uu uuus u.a un u. u uun .u. .us u una.

1 2.382 3.289 1 2.382 3.571 2 2.382 3.326 2 2.382 3.577 3 2.382 3.438 4

3 2.382 3.M0 2.382 3.479 4 2.382 3.45 5 2.382 3.510 5 2.382 3.657 6 2.382 3.541 6 2.382 3.647 7 2.382 3.576 7 2.382 3.641 8 2.382 3.609 8 2.382 3.633 9 2.382 3.630 9 2.382 3.611 10 2.382 3.639 10 2.382 3.578

!! 2.382 3.645  !! 2.!B2 3.!42 12 2.382 3.655 12 2.382 3.!!!

13 2.382 3.M4 13 2.382 3.480 14 2.382 3.M0 14 2.382 3.439 15 2.382 3.577 15

• 2.382 3.327

. 16 2.382 3.571 3.;19 16 2.382

1) h0!!!hAL 80L SHOMER SAP. 2.382in. NOTE: ALL REPORTD FLUD:t WU".!!R! AA! ! 10 (( 'l N/C?**2

2) A'itid.st SME Tuni 610 sin. C ] FLUDCES CALCULATED FOR D0.82147E ANU$iD to ACTUAL BURNUP O

3) AVERAit SUICE TUBE FLUDCE 3.072

4) AVS. 30L RCD ACTIVE LDiiNa l'0 in.

8-11