ML20134J999

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Fuel Assembly Insp Program
ML20134J999
Person / Time
Site: Sequoyah  Tennessee Valley Authority icon.png
Issue date: 09/23/1996
From: Colburn D, Desiree Davis, Halligan J
WESTINGHOUSE ELECTRIC COMPANY, DIV OF CBS CORP.
To:
Shared Package
ML17062B149 List:
References
PPE-96-226, NUDOCS 9611180180
Download: ML20134J999 (9)


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Westinghouse 9%pdetary class 3 l

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Sequoyah Fuel Assembly inspection Program Contributors:

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D. J. Colburn D. D. Davis J. R. Halligan i

September 23,1996 i

l The inspection work was conducted at Sequoyah by an NSD crew. Jim Kisak, PPE contract engineer, supervised the crew. Various PPE engineers were responsible for the reduction and verification of individual portions of the inspection program. Their signatures on this document l

' attest that (1) they have independently verified the sections assigned to them; and (2) they concur with the results documented hereis.. A listing of the individual data reduction and verification assignments is given below:

Insoection Program Sectico Originating Engineer Verifying Engineer 1.0 Background & Objectives D. Colburn J. Halligan 2.0 Full Length RCCA Drag Tests D. Davis D. Colburn 3.0 Guide Thimble Ph!g Gage Exams J. Halligan D. Colburn 4.0 Summary D. Colburn D. Davis Signatures On File D. J. Colburn D. D. Davis Product Performance Engineering Product Performance Engineering J. R. Halligan l

Product Performance Engineering l

l 9611100180 961016 PDR TOPRP E B

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W:stinghoun Proprietary Clan 3 1.0 Background and Objectives A RCCA insertion anomaly was experienced at Wolf Creek and South Texas Unit 1. During SCRAMS, several RCCAs failed to fully insert. Both plants conducted drop tests after the

.anomalv. and additional RCCAs did not.fullv insert.. A subsecuent insoection orocram

  • >b>c The following tests were conducted during the inspection program:

(1) RCCA Drag Tests; (2) Guide Thimble Plug Gage Exams (Single Tube Probe Tests);

(3) Fuel Assembly Length Measurements; and (4) Fuel Rod-to-Nozzle Gap Measurements.

Fuel assembly length measurements and fuel rod to-nozzle gap measurements were used to determine if the growth of the fuel assemblies and fuel rods was within the anticipated j

range. Items 3 and 4 will be reported in a separate report when the on-site data is available. Re-measurement is necessary because the adjusted assembly growth values l

measured during the first campaign are abnormally low.

2.0 Full Length RCCA Drag Tests Fuel assemblies fabricated for seven (7) different contracts were drag tested in the spent fuel pool. The specific fuel features for each contract are shown below. Fourteen of the twenty-one fuel assemblies that were tested were fabricated with Vantage 5H fuel features.

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Westkughous2 Proprietary Class 3 The drag test results are tabulated in Table 2.1. The Sequoyah dashpot and guide thimble.,3,e

. data _ are shown in Figure 2.1 with data from other plants. The lines in the figure represent _

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Table 2.1: Sequoyah Drag Test Data a,b,e I

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Figure 2.1: Dashpot and Upper Guide Thimble Drag Data F".

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W:stinghous2 Proprietary Class 3 3.0 Single Tube Probe Single tube probing was conducted on three fuel assemblies at Sequoyah Unit 2. The assemblies were selected based on burnup and drag measurements, and are included in

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_the_ table balow._The.nbiectivamf_the_tastwas_toMatarmina_the_extantandjacationaf_.___

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Single Tube Probe Test Results a,b,c J

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wastinghous, proprietary class 3 4.0 Summary a,b,e l

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Appendix A 4

l Sequoyah Fuel Assembly Drag Data 1

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Figure A.1: Dashpot Drag and Fast Fluence Data 5

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Figure A.2: Upper Guide Thimble Drag and Fast Fluence Data i

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