ML20028B108

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Forwards Response to SER Issue 8 Re Dynamic Qualification
ML20028B108
Person / Time
Site: Shoreham File:Long Island Lighting Company icon.png
Issue date: 11/23/1982
From: James Smith
LONG ISLAND LIGHTING CO.
To: Harold Denton
Office of Nuclear Reactor Regulation
References
SNRC-796, NUDOCS 8211290468
Download: ML20028B108 (139)


Text

{{#Wiki_filter:_ m LONG ISLAND LIGHTING COM PANY SHOREHAM NUCLEAR POWER STATION ~- P.O. BOX 618, NORTH COUNTRY ROAD e WADING RIVER, N.Y.11792 November 23, 1982 SNRC-796 Mr. Harold R. Denton, Director Office of Nuclear Reactor Regulation U.S. Nuclear Regulatory Commission Washington, D.C. 20555 Safety Evaluation Report Issue No. 8 Dynamic Qualification Shoreham Nuclear Power Station - Unit 1 Docket No. 50-322

Reference:

(1) Letter NRC (A. Schwencer) to LILCO (M. S. Pollock) dated 11/10/82

Dear Mr. Denton:

In response to the reference (1) letter, enclosed please find ten (10) copies of Long Island Lighting Company's response to the concerns generated by the Seismic Qualification Review Team as a result of their plant site audit held from August 31 - September 3, 19E2. This information is being submitted in order to facili-tate the NRC staff's review and closeout of this SER item. Each concern is addressed separately with the concern restated and the response following. Any responses which require additional docu-mentation have this listed as an attachment. In accordance with R. L. Tedesco's letter to LILCO, dated January 28, 1981, four copies of this submittal are being forwarded directly to Dr. Morris Reich at Brookhaven National Laboratory. As stated in the Reference 1 letter a response to the audit trip open items was anticipated to be made by LILCO within two weeks after receipt of Reference 1. In view of this timely response, LILCO requests that the NRC staff review the enclosed information in a manner so as to facilitate final resolution of this SER item. Very truly yours, () [ / D L. Smith j jo Manager, Special Projects WVB:mp (,. g Enclosure cc: J. Higgins All parties 8211290468 821123 Dr. M. Reich (4) PDR ADOCK 05000322 E PDR

GENERIC ITEMS 1. Qualification documentation needs to be improved in the following areas: a. A " road map" should be provided to define the qualification process for BOP equipment. b. Complete test reports should be included in BOP SQRT

package, c.

Single spectra included in:62r:?qad. age should be identifed as limiting (worst case) spectra.

RESPONSE

a. A summary report will be provided which will define the scope of the dynamic qualification program for BOP equipment. The report will describe the basis for including equipment in the program and the specific methodology applied for qualification of equipment. This report will be provided 30 days prior to fuel load.* b. The vendor supplies qualification documents which normally include complete test reports which are included in the SQRT packages. In a few cases vendors may not have supplied a complete test report as part of their qualification documentation, e.g., for specific items 480V Emergency Switchgear Bus 112 and 480V Motor Control Centers 1R24*MCC1120, in the NRC audit report. In these cases, complete test reports will be requested from the vendor. If the vendor holds them proprietary, LILCO will take action similar to specific items 3 and 4. This effort will be completed by June, 1983. c. The single spectra included in the SQRT packages will be identified as limiting (worst case) spectra by fuel load. 2. The latest confirmatory load spectra should be included in all SQRT packages by the end of March 1983.

RESPONSE

The latest confirmatory load spectra will be included in all SQRT packages for floor-mounted equipment by the end of March 1983. Clarification will be provided to the extent necessary to relate confirmatory load spectra to the qualification basis. All replacement equipment (not in-kind) will be qualified to the confirmatory load spectra. _.-._,_,,_v._-.- , ~ _, .-._,--,.._t

~ \\ Generic Items, Page 2 3. The latest confirmatory loads should be considered for the qualification of pipe mounted equipment, i.e., valves. Prior to fuel load l Phase I a. Provide verbal description of 30 piping subsystems already analyzed. b, Provide a list of pipe mounted equipment by Shoreham valve Mark Nos. in these subsystems, c. Demonstrate qualification to confirmatory load values for the valves listed. Prior to operation above 5% power Phase II a. Identify all associated pipe mounted equipment for approximately 70 additional piping subsystems. b. Assess existing margin of safety for accommodating the upper bound of any load increase that could result,from the confirmatory loads. c. Where adequate margins of safety are not evident, perform analysis to demonstrate equipment qualification utilizing confirmatory loads.

RESPONSE

LILCO has proposed the following program to evaluate the effect of the hydrodynamic LOCA loads discussed in NUREG 0808 on pipe mounted equipment: Phase I t In the Shoreham Design Assessment Report (DAR), Rev. 5, Appendix L, LILCO has stated that a representative cross-section of primary and secondary piping was evaluated to the NUREG 0808 Confirmatory Load Definition. This cross-section consisted of thirty (30) piping subsystems (twenty-five (25) of which are attached to the primary containment at locations of high amplitude response spectra). is a listing of all the pipe mounted equipment on these thirty (30) piping subsystems by Shoreham Mark Number. LILCO has agreed to provide the SQRT qualification level and calculated acceleration for each item based on the NUREG 0808 Confirmatory Load Definition. Should any equipment acceleration levels be found to be above the present qualification levels, computer reanalysis of these pieces of equipment will be performed again, utilizing the NUREG 0808 Confirmatory Load Definition but eliminating simplifying assumptions that have been employed. This approach has been described in SNRC-755, dated 8/20/82 from J. L. Smith to H. R. Denton, and agreed to by the NRC Mechanical Engineering Branch. This analysis will be completed prior to fuel load. m. n

_...~ Generic Items, Page 3 Phase 7.I In SNRC-755, referenced above, LILCO committed to perform a one-hundred (100) percent reevaluation to the final Mark II long term program load definition (NUREG 0808) of the piping attached to the primary containment at the three (3) additional locations of

concern, i.e.,

21 ft., 83 ft., and 106 ft. This reevaluation work is considered confirmatory and not required for fuel load and low power testing. During the SQRT audit from August 31 to September 3, 1982, LILCO also committed to the NRC SQRT evaluation team to identify all pipe mounted equipment on these additional piping systems (approximately 70 piping subsystems) and to evaluate that the existing margins of safety are sufficient to accommodate the upper bound of any load increase that could result from the confirmatory NUREG 0808 load definitions. For the set of equipment where adequate margins of safety are not evident, requalification will be performed utilizing the NUREG 0808 Confirmatory Load Definition. This approach is similar to the agreement reached with the NRC Mechanical Engineering Branch for these same additional piping systems. This analysis will be completed prior to exceeding five (5) percent power operation. 4. Commit to establish a maintenance and surveillance program to maintain equipment in qualification status throughout the plant life prior to fuel load.

Response

The Shoreham Nuclear Power Station has a surveillance and maintenance program which includes documented program plans, procedures, and results to ensure that the safety-related equipment identified in the dynamic qualification program is maintained in a state of readiness and operability so that it will perform its intended safety functions properly during and after the excitation imposed by the SSE or hydrodynamic loads associated with suppression pool discharges or a combination of the two. The Shoreham surveillance and maintenance program includes information supplied by equipment manufacturers and vendors regarding required equipment mainteaance actions and their frequency. The Shoreham dynamic qualification program has not imposed any additional surveillance and maintenance requirements on the equipment included in the program as a result of qualification. However, if any specific requirements were generated they would be incorporated into the existing surveillance and maintenance program. 5. Provide monthly status of equipment summary list and provide justification for the equipment which will be qualified after fuel load.

Response

The latest equipment summary lists including BOP and NSSS equipment is provided in Attachment 2. This list will be updated and provided on a monthly basis.

Generic Items, Page 4 Justification for interim operation for the equipment which will be qualified after fuel load will be provided before the end of December, 1982. 6. NSSS qualification documentation file should be located in Shoreham plant file system by June 1, 1983.

Response

At present, LILCO has on file at the Shoreham site NSSS Dynamic Qualification Summaries for the equipment qualified under the NSSS scope of supply. The summaries provide-.*he requirements, demonstrate equipment capability and provide a rationale for qualification certification along with the Qualification Summary of Equipment (SQRT) forms. However, in order to comply with this NRC concern, LILCO is generating the necessary purchase order agreement to obtain the backup qualification documentation. The detailed NSSS backup qualification documentation will be located in the SQRT documentation packages at the Shoreham site by June, 1983. 7. To satisfy requirements of IEEE 323-1974, provide a wri.tten statement that margin to cover uncertainty in manufacturing and test exist for equipment qualified by test.

Response

IEEE Standard 323-1974 states in section 6.3 that for vibration, a margin requirement should be included to account for variations in equipment and reasonable errors in defining satisfactory performance. This standard has been endorsed by the NRC in Regulatory Guide 1.89, " Qualification of Class 1E Equipment for Nuclear Power Plants", dated November 1974. The Shoreham FSAR in Appendix 3B states that Regulatory Guide 1.89 is not applicable to Shoreham since the Shoreham SER (dated February 20, 1970) preceded the implementation date given in Section D of Regulatory Guide 1.89. The FSAR Appendix section goes on to state that an attempt would be made to procure equipment to the standard referenced in RG 1.89. The Shoreham FSAR cites IEEE Standard 323-1971 as the applicable standard for equipment qualification for Shoreham. LILCO feels that conformance to IEEE 323-1971 in addition to the TRS enveloping the RRS and the inherent conservatism used in developing the RRS provides the adequate margin to cover uncertainty in manufacturing and errors for equipment qualified by test. 8. Cycling effects of hydrodynamic load should be addressed prior to fuel load, based on worst case consideration. a. For equipment qualified by analysis, cumulative fatigue usage factor should be demonstrated to be less than one. The SQRT may decide to review the adequacy of the analytical model used. b. For equipment qualified by testing, the number of equivalent SRV cycle should be adequately defined.

Generic Items, Page 5

Response

a. For BOP equipment qualified by analysis, a survey will be conducted to identify the most highly stressed equipment in several categories, i.e., pumps, valves, heat exchangers and tanks. Peak stress will be determined by applying a stress intensification factor applicable to the configuration. Cumulative fatigue usage factors will then be determined for each equipment category. Vibration fatigue cycle effects for NSSS equipment designed to ASME code requirements was reviewed at GE by NRC consultants from Battelle Pacific Northwest Laboratories on October 7, 1980. The consultants stated satisfaction with the GE approach which encompasses OBE, SRV, thermal and pressure cycles. Non-ASME code components qualified by analysis have not been required to address vibration cycle effects. An overall review of non-ASME code components showed that the effect of SRV cycling fatigue did not require further additional analysis. b. For equipment qualified by testing, the number of equivalent SRV cycles has been defined in the Design Assessment Report, Revision 5, pages 9-11 and 9-12. 9. Provide information of any field modification made to the already qualified and installed equipment prior to fuel load. Response is the current status of field modifications to safety related BOP equipment since September 2, 1982. As of November 12, 1982, GE records do not indicate any field changes being made to NSSS equipment since September 2, 1982 which would affect seismic qualification as documented in GE SQRT reports. A revised list of BOP and NSSS equipment will be provided prior to fuel load. 4.

EQUIPMENT SPECIFIC ITEMS 1. Unit Cooler - 1T46*UC-022 Package No. SH1-276-5 A static deflection analysis was provided for the fan only. A clearance of.051" was noted between the fan and housing. Provide upgraded calculations to also include the deflection of the housing.

RESPONSE

An analysis of the fan housing has demonstrated a maximum displacement of approximately 0.001 inches. The vendor qualification report provides a maximums static deflection of 0.00306 inches for the fan. A combined maximum displacement of 0.00406 inches for the fan and housing is well within the available clearance of 0.051 inches. is a copy of calculation 331-1-CZC which was prepared in response to this request. 2. Permanent Control Rod Storage Rack - 1F16*RAK-23 Package No. SH1-427-1 a. The qualification loads report was not available in the SQRT file. Need clarification b. Provide evidence of verification for the non-linear analysis code used. c. Loads were not properly defined (i.e., a time history was used, but there was no description of what it represented). Provide clarification.

RESPONSE

The qualification loads report is now available in the SQRT a. file at the site. b. Verification of the non-linear code (RACKOE) used by the vendor to calculate rack loads was conducted by showing that the ANSYS code yields similar results for a test problem. Documentation is provided in Appendix E of the Seismic Analysis Report (Attachment 5) and is now included in the SQRT file at the site. c. The racks were subjected to horizontal time histories associated with SSE, SRV and LOCa. It was found that SSE was the dominant source of rack loads appearing at the corners where they are attached to the floor embedments. Other loads were insignificant contributors. This is addressed in Appendix A, Section 125F21 of the vendor's loads report.

Equipment Specific Items, Page 2 3. .480 V Emergency Switchgear Bus 112 Package No. Sill-95-1 a. The qualification report should be completed so that it includes a table of contents and sequentially numbered pages. b. The test reports from test labs should be reviewed as part of the qualification documentation package.

RESPONSE

a. The pages have now been sequentially numbered and a table of contents included. It has been verified with the vendor i that the qualification report is complete as filed. i b. The vendor's test report had been reviewed in its entirety i prior to acceptance. It will be reviewed again for the l purpose of identifying the substance of the test conducted. For example, any test anomalies that may have occurred will i be documented and included in the SQRT package on file at the site. 4. 480 V Motor Control Centers - 1R24*MCC 1120 j Package No. Sill-115-1 a. Provide resolution to the concern regarding clearance problems between motor control centers McC1133 and MCC1125, and battery chargers BC-01 and BC-B1 respectively. b. The test reports from the test labs should be reviewed as part of the qualification package.

RESPONSE

a. Review has indicated that the clearance between Motor Control Centers 1125 and 1133 and the battery chargers is 4 not sufficiently large to assure that these cabinets will not impact during a dynamic event. Accordingly, these cabinets will be rigidly tied to the respective battery chargers and implementation will be complete prior to fuel i load. Tying the battery chargers to the MCCs increases the fundamental horizontal frequency of the MCC above the peak frequency of the Control Building spectra, thus reducing the scismic loading. Therefore, the seismic qualification of the MCCs is not affected. b. As in the case of 3(b) above, the entire vendor's test report will be reviewed again and anomalies and basis of disposition will be included in the SQRT package on file at the site, i

Equipment Specific Items, Page 3 5. Service Water Pumps - 1P41*P-003 Package No. SH1-51-1 Provide information regarding the analysis to determine the a. pump's lowest natural frequency with consideration of the fluid mass. b. The analysis indicates that fundamental mode natural frequency is less than the pump rotary speed of 30 cps. Provide assurance that no potential problem will arise if the frequencies of high modes are also within the pump

speed, Provide justification of decoupling x and y dynamic -

c. degree-of-freedom in the frequency calculations.

RESPONSE

a. The vendor qualification report indicated that the lowest natural frequency of the pump assembly is 22.286 Hz and included fluid mass effects at the pump bowl assembly. A review of the applicable seismic Amplified Response Spectra for this pump assembly indicates rigid range response applies above 10Hz in the horizontal direction and above 12 Hz in the vertical direction. It is concluded that the results of analysis of the pump assembly, including the effects of fluid mass, are representative and acceptably qualify the assembly for seismic response effects, b. The minimum pump assembly natural frequency (22.286 Hz) is about 14% above the pump rotary speed of 1170 RPM (19.5 Hz). Therefore, there are no natural frequencies of the pump assembly within the operating speed range and the assembly can, therefore, be considered rigid for operating purposes, as well as for seismic considerations as explained previously. Also, these pumps have been operated successfully, confirming that no resonances are excited. An independent multi-degree of freedom dynamic frequency c. analysis of the pump assembly for a coupled x and y dynamic model has confirmed the natural frequencies of the pump assembly provided by the vendor in his qualification report. Review of the independent analysis results also verifies the original choice of decoupling the x and y dynamic models of the pump assembly. 6. Main Steam Isolation Valve - 1B21*AOV-081 a. Provide justification that the rapid closure of the valve which is not accounted for in qualification has negligible effects on the operability of the MSIV. b. Assure proper surveillance to insure adequate columns lubrication.

Equipment Specific Items, Page 4

RESPONSE

a. Stress Report 22A6416, (Revision 0, pages 1-4, 7-8, 143-150) provided in Attachment 6 shows all the load combinations considered in the evaluation. The MSIV does not close any faster during the dynamic event as compared to the normal situation. The closure time is controlled by a self-adjusting hydraulic control valve. The effect of the dynamic response of the extended mass of the MSIV actuator was analyzed as part of the piping analysis. The calculated forces and moments were than compared to the allowable and documented in Stress Report 22A6416, Revision O. Further, to assure each MSIV can withstand rapid closure, each MSIV was tested as part of the production testing sequence. The stress in the MSIV seating area is not significantly affected by dynamic loadings. shows the stress variation at the valve ends. At the seating area, the stress is even lower due to heavier wall thickness. The MSIV is routinely stroke for checkout in order to assure the effects of closure have not overstressed the MSIV seating area. The effects of closure are determined by a leak test. The impact force for MSIV closure under faulted conditions, with steam helping to close this valve, is not any greater than for the routine checkouts stated above. This is so because the stem and disc motions are controlled by a set of flow control valves and a hydraulic damper. Any excess closing force due to dynamic loads is absorbed by the hydraulic damper. The stress at the disc has been analyzed and found to have a maximum stress of 14,550 psi vs. an allowable stress of 19,900 psi @ 575 F. Based on the above, so-called " rapid closure" of the valve has a negligible effect on operability. b. GE does not believe special lubrication of the columns, over and above that recommended in the vendor's maintenance manual is required. This position is based on the fact that this MSIV actuator always closed properly during the seismic test, even though it exhibited some hesitation on opening. Closure of the MSIV is the safety mode, and is aided by the springs designed into the actuator. Opening of the MSIV occurs against the spring force, and accounts for the different behavior in closing vs. opening. Stroking behavior of the MSIV is routinely checked to verify proper operation of the valve.

Equipment ^ Specific Items, Page 5 7. RCIC Turbine - lE51*TU-005 a. The turbine in the plant (GS-1) is not the same as the one in the~ test report (GS-2). Establish dynamic similarity. b. Since the qualification is dependent on some modifications, report to the NRC when implementation of the modifications is completed.

RESPONSE

a. provides the General Electric memo which establishes dynamic similarity between the tested and installed turbines.
b. provides three Field Disposition Instructions (FDIs) which outlines the modifications required on the Shoreham turbine.

These FDIs are scheduled for completion prior to fuel load and LILCO believes that these modifications will provide similarity between the tested and the in-plant turbine. Upon completion, the NRC will be notified. 8. Pressure Transmitter IC41*PT-002 a. Field mounting configuration is different than that in the test. Provide assurance that the resulting response spectrum at the equipment mounting location would envelope the required response spectrum at the mounting location in the field. b. Documentation that justifies the similarity of the untested models to the tested units should be included in the over-all qualification documentation package.

RESPONSE

a. provides additional test data which verifies dynamic adequacy of the differential pressure transmitter.

b. GE PPD numbers 145C3240, 163C1558, 163C1560, 163C1561, 163C1563 and 163C1564 all refer to Rosemount Model 1151 or 1152 differential pressure transmitters. An excerpt from the Rosemount test report 2758 (Attachment 10) states that models 1151 and 1152 are mechanically identical. Differ-ences are due to requirements of material traceability for pressure retaining parts for the 1152 model and the use of non-Teflon wire in the 1152 assembly. Neither of these differences would invalidate the applicability of the test results in the qualification test report to the untested model. Since the 1151 and 1152 models are identical in construction and dimension, LILCO concludes that the 1152 model test results are applicable to the 1151 model. This test report will be included in the SQRT package.

Equipment Specific Items, Page 6 9. 120 Volt Distribution Panel - 1R35*PNL-R2 Package No. SH1-124-1 Field mounting condition is different than that in the test. Frovide justification that the qualification is valid from the viewpoint of dynamic similarity.

RESPONSE

The distribution panel was bolted by its four support ears to a fixture mounted to the test table during qualification testing. The fixture consisted of two braced structural members with a full height support plate between them, simulating a typical plant wall. The. field mounting of the panel assembly is by bolting through the four support cars to a wall mounted unistrut frame. The natural frequency of the support frame is well above the rigid range of the applicable required response spectra. It is, therefore, concluded that the field installation acceptability simulates the tested condition and will not alter the conclusions of adequacy. By way of background, the original biaxial multifrequency qualification testing program resulted in test input levels that were generally 60% or more above the required level. The assembly was subsequently fragility tested to even higher levels, which assures the adequacy of these panel assemblies in a very conservative manner.

10. GENERAL The SORT disagreed with GE's use of single frequency / single axis testing method to qualify some shipped loose items.

The Applicant was requested to provide the description of the items for which this qualification method was used.

RESPONSE

A list of Shoreham equipment qualified by use of single frequency / single axis testing is attached. Those items which are in iba category of GE shipped loose items are noted as such. 1 provides a listing of BOP equipment qualified by this method. 2 provides a listing of NSSS equipment qualified by single frequency / single axis testing. The attachment provides the following: 1. C&I devices on Local Panels See Table 2 from DRF A00.992, Rev. 1, Local Panels 2. C&I devices on Control Room Panels See Table 2 from DRF A00-992, Rev., 1, Control Room Panels i

Equipment Specific Items, Page 7 3. C&I Ship Loose Devices See table entitled, "Shoreham' Ship Loose Devices Qualified by. Single Axis / Single Frequency Testing" Note that several of the Local Panel and Ship Loose devices are the same device model, as identi-fled by GE PPD Number. 4. Mechanical. Equipment B31-FO31 -Limitorque actuator on Recirc Discharge Valve E32-B001 MSIV LCS Heater P

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  • COPIES OF DOC 10 DISTRIBUTIDH

~ _. -... ~ ~ -. 0 ^ 1 SeegetteaM tRett 1 Rt LISr STOME & HE8 STER EMsINEERING CmtreeATION RUPt DAff II/94/02 i Jte P4 seer 11400 3-SORT RfACTOR DUILDING CATEGCitY I FLOOR-IWITED ECUIPMENT RtM TIIIE 14.15.54 4 LILCO DOCHti 50-323 ACTIVt 90P QUM.IFICATI0tt LEVEL (205 ITEttSt PAGE 7 1 l reset terIPteMT SPEC DIV. BLDS AVAIL QUAL OU.11. TYPt SAFE QUAR. q l 94seE2 DESCRIPTION HO. RESP VEte0R ELF.V ItlSP REPT HETH FREQ Hil80 SHiDN STATUS 1T442TE 999 ate-21 t# TIT CLR 404 CD ROSEHOUNT SC159 YES 2747 SAT 40+ F2 CS.HS N 1T44 eft tot stE-tt t# TIT CLR 404 CD WOSEtt0UNT SC149 YES 2747 SAT des Ft CS.HS N f q 1749 EFT 00SM IIEPA FILTER IttET 404 CD ROSEHol#ff SC113 YES 127514 SAT 40e Ft CS.HS H l { t r 1293st.T ett SIPPRESS? fit POOL LEVEL 404 CO ROSEltRNT SC8 YES 127514 SAT 40+ Ft CS.IIS H } I 1293ePT 993 BRYtIELL vitESSURE 404 CD ROSEttDUNT SC99 YES 196025 lei des Ft C3.HS N 1293erf 004 sure penL Pres 9 404 Ce postlicuMT 3Ces Yes toests Hsf ese Ft Cs.sts et 4 1Z93:TE lit WV9924CL DISCHARGE 1FT 404 CD ROSEll0UNT PL28 H5T F4 H 8 - S i it 4 .i{ i 129321t Ill RV99290t DIStitalPCE-1FT 994 CD ROSEtIOUNT PLES teT F4 H B 12935T1 Ilt RW992H6 DISCHARGE-1FT 404 CD ROSEHOUNT PLte teT F4 M S 1293:TE 113 WVe9tFMJ DISOtARGE-tFT 494 CD ROSENDt#ff plt 8 pet F4 M B 4 1293sTE 132 RvettACL DISCttARCf-tFT med CD ROSEttCUNT PL28 teT Ft H S 12932TE III RW99200E DISCHARGE-tFT 404 CD ROSEllotttT plt 8 H8T Ft H S . ? g 1293 aft 134 RV99 Elf 8 DISCHARCE-tFT 404 CD ROSEllOUPIT PL20 IST Ft M 5 l 12933TE 135 Rvt92FHJ DIScttARCE-tFT 404 CD ROSEHOUNT PL20 HDT FE N 8 IP4teLS 912 IFBCLCM TM-924 407 CD HAGifETROL Sclet YES 43235-1 teT 17 Ft HS H f IP4 fels 913 ROCLCN TM-924 407 CD HACHETRet. SC140 YES 43235-1 MBT 17 Ft HS M g litteLS tel Cope LEVEL 407 CD HACHETROL SC73 YES 43235-1 teT 17 F2 HS M IF14:.CAN-It MI DENSITT SPNT FUEL R 427 PD HACHTER SC137 YES LIL-T-151 DA 10 F29 H H IF14eRAN-23 PERM CII STOR WACHS 427 PD HACHTER SC137 YES LIL-T-151 DA It F M N IF14mCAM-te TEls' CR STOR RACHS 427 PD HACHTER SC137 YES LIL-T-151 DA le Ft M N 122VaTIS111R LCPI ATS 438 ED ASCD SC112 YES 19404 HDT 13 F CS.HS H 3 ) CS ECOLD SHUT 00188 P PIPE ItOUNTED $8TrSINGLE FREQUEllCY OUALIFICATItti IIILEST0tlES REVISION 4 -HOVEleER 1982 O sDUCT tt0UtlTED PC :PRittAttY CollT. 81 AXIAL TESTIttG A rREEVALUATI0tt totPLETE D3 sOYttAll!C AllALYSIS PL :PEDESTAt. SC =SEC0tiOARY COtIT. 8 eREQUEST FOR QUAL OR DID ISSUtD t#0fE: tRAIDER Ill F sELOOR lint #1TED QP = QUALIFIED BY / = LOCATED Ott CotIT. C rS/H REColttElcATI0tt 10 LILCO 'TTPE IITtG' COLUtti IS HS elt0T STAIOBY PIPIttG Af4ALYSIS litLL D eQUAt. DOC RECEIVED QUANTITY OF ITEllS. 12TalRA.TI-EREQUEllCY SA zSTATIC AtlALYSIS M etlEITHER CS OR HS E rHADDilADE It0DIFICATIOt1 REQ'O 81 AXIAL TESilitG 5AI G *7 E FREQUrtiCT Z PASSIVE ITEH F =0UAL 00C APVD A FILED ifST:1XA.TI-F R E00E t8CY SIllGLA AMI AL TESTING (Sa9T PAPER tl0T G z SQR T Pr.PE R Col'PL E T E SIllCLE AXIAL TESTIHG REQ'Of H ecoPIES OF DOC TO DISTRIBUTION )

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1794eA0V939C 18 CD74-02 172 SC 2.3 .8 BETTIS 122C-SR-H3 H H IT94sA0V9399 10 CD74-82 172 SC 1.8 .8 BETTIS 722C-SR-If3 H H 41 3CCleRv0214 1.5 502499 191 SC 1.5 1.3 F .1 1CCleRVe218 1.5 FM499 191 SC 1.5 1.3 F O' 1E11eRV151A 1 502499 191 SC 1.5 1.3 F 1ElleRV1518 1 502499 191 SC 1.5 1.3 F p O. IE11eRv151C 1 502494 191 SC 1.5 1.3 F It11 MRV 1510 1 902444 191 SC 1.8 1.5 F IE11 MRV 152A 4 502499 191 SC 1.3 1.0 F ~- QUALIFICATI0tl HILESi0flES Of01ES REVISI0tl 9 -HOVEltBER 1982 (0 = A rREEVALUATION CultPLETE

1. Ct. 2 AND 3 VALVES 4 OR = 2 Ill. ARE
5. PREstitT QUALIFICATION VALTD 8 spt00EST FOR CUAL OR 010 ISSUtD FLOOR-It0UllTED (ElliG-5 I FOR OPERA 10ft LOADS < OR = 3 C's

]. C 5S/11 PEcot'ItEllDA110tl 10 LTLCO

2. e r DC 11010R.

AI.L OillERS ARE AC llDRI20:lTAL Ale VERTItaltFAllL1EDI ) D 20UAL 00C RECTIVED

3. CL 1 VALVES < Oft s 1 Ill. ARE
4. IF OllLT Of tt LOAD IS GIVEll FCU E-IlfrollADF If00lFICATI0tl REQ'O FLOOR-ifoUtilID IElliG-51 Tile OPIRATOR. IT IS file ItaXilfUll F r0eJAL 00C APVU S FILED
9. 2/1 = 2 Ill. CLASS 1

( G :59pf Ptff R C0f tPL F IE .) H : COPIES OF DOC TO DISTillDITT10ll [n 8M ll

SIENttttAll VIT 1 39PM LIST STCHE & letBSTt1r ENG1tlEERItes CORPORATION RUM DATE 11/99/02 I i O ' JOB tu mER 11499 3-SORT WEACTUR BUILDIllG LATEGORY I PIFE HOUtITED EQUIPHENT RUN TIllt 14.17.19 A. j LILCO DOCHET 50-322 ACTIVE BOP QUALIFICATI0tf LEVEL (393 ITEtts) FACE t lI( es 5 1 ., i 1 2 3 9 CPER LOAO-8'S OPERATOR 4 00AL STATUS [ teneM PIPE qunt. SPEC LOC. i tuett SIZE REPT HO. It0R VER SUITLIER IID0tt tio. YONE OPER { l ^ l SttteRVIStB 9 502499 191 SC 9.9 2.3 F It11eRV1534 1 501499 191 SC 1.5 1.3 F e 4 It11eW1538 1 502499 191 SC 1.5 1.3 F { L lt11eW159 1 502499 191 SC 1.5 1.3 F D h; 1E11eW155 t 502499 191 SC 1.5 1.3 F i,. 6 I ItllentetA 1 502499 191 SC 1.5 1.3 F Q SI It11eRv1428 1 502449 191 SC 1.5 1.3 P [ It11eW143 .75 502419 191 SC 1.5 1.3 F i 1t31eWVI44 .75 502499 191 SC 1.5 1.3 F i 1EtteW99tA .75 502499 191 SC 1.5 1.3 F Q 4, l l 1EtteW 9928 .75 502499 191 SC 1.5 1.3 F i 1ttleWO934 1.5 502449 191 SC 1.5 1.3 F t Q 1EtteRV9938 1.5 502499 191 SC 1.5 1.3 F - l IttleltV9944 .75 502499 191 SC 1.5 1.3 F f Q W! IttleRV9948 .75 502499 191 SC 1.5 1.3 F It41eRV195 .75 502499 191 SC 1.5 1.3 F (' Il 1E41eRV194 1.5 502449 191 SC 1.5 1.3 F It91eRV197 1.25 50*499 191 SC 1.5 1.3 P 1E91eRV199 .75 502499 111 SC 1.5 1.3 F QUALIFICAT10tl II1LESi0 TIES f.0TES REVISIDH 9 -tf0 vel! DER 1902 ) A WEEVALUATIDH C0trLETE

1. CL E AND 3 VALVES < OR e E IH. ARE
5. PRESEffT 00ALIFICATION VALIO 8 apt 00EST FOR QUAL OR BIO ISSUED FLOOR-IIOUllTED (EllTG-5 1 FOR OPERATOR LOADS < OR = 3 C'S

( C zS/H REC 0tillEt:0ATI0tl TO LILCO E. m : OC 19010R. ALL OTitERS ARE AC It0RIZo! ITAL AtID VERTICALIFAULTEDI 0 CUAL DOC RECEIVED

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GD 8 390RE11MI' u T 1 N8PM LIST STOME & MEBSTE18 Et4GIAtLRING CORPORAT1tRt IttM DATE 11/09/92 3-503T REACTOR SUILEIt3 C*.TECORY I PII'E HoutffED EQUIPMENT RUM TIIIE 14.1T.19 9 @ lJos taAmtR 11409 LILCO DOCHET 50-322 ACTIVE SCP QUALIFICATI0H LEvtl (393 ITEttSi PAGE 3 { f 5 7 4 A ! I t 3 9 OPER LOAN-S'S OPERATOR 4 QUAL STATUS l tWeN PIP 5 SUAL SPEC LOC. l DeAeER SIZE REPT t10. 1:0R VER SurPLIER 1100tL HO. YCHE OPER s Nf O M 1E51eerv 195 .75 502499 191 SC .4 .2 1E51eRV 194 .75 502449 191 SC .4 .t M A O 1E51eliv 197 1.25 502499 191 SC .4 .2 M IEfteltV 199 .75 502499 191 SC .4 .2 M O t O' 1933sM993 .75 502499 191 SC 1.5 1.3 F e l O'\\ l"33eRV0954 75 502499 191 SC 1.5 1.3 F l O 1333eM9958 .75 502499 191 SC 1.5 1.3 F vJ '\\ m,j 1691setV9194 1 502H9 191 SC 1.5 1.3 F 1s41eRV919s 1 502444 191 SC 1.5 1.3 F .i f' 1691sRV029 1 502H4 191 SC 1.5 1.3 F +'i e 1891sRV025 1 502499 191 SC 1.5 1.3 F ,[ IP91eltV9294 1 502499 191 SC 1.5 1.3 F O-i i@ IP91eltV9298 1 502449 191 SC 1.5 1.3 F 1P91eRV1104 .75 502444 191 SC 1.5 1.3 F 1 O' Q IP91eRV1108 .75 502499 191 SC 1.5 1.3 F a 1P91eRV119 .75 502899 191 SC 1.5 1.3 F 9 i@ 2P91eRV1304 .75 502899 191 SC 1.5 1.3 F IP41eRV1309 .75 502899 191 SC 1.5 1.3 F D '. Q IP92eRVOTTA 1 502699 191 SC 1.5 1.3 F QUALIFICATI0tl flILEST0 tits tioitS REVISIDH 4 -tiovitBER 1982 h A rREEVALUATIOtl Cott'LETE

1. CL 2 AfD 3 VALVES < OR = 2 Ifl. ARE
5. PRESENT QUALIFICATION VALIO 8 rREQtitST FOR QUAL OR DIO 155U00 FLO0ft-tfoUtrit0 IIITTG-5 I F0ff OrtRATOR LOADS < OR r 3 ges

( C eS/H REC 0f f tttfDAT10tl 10 LILCO

t. e = DC 11010R. ALL OTilERS ARE AC 110RIlt'tirAL AtID VERTICALIFAULTEDI 1

0 rotfAL DOC Rf CEIVED

3. CL 1 VALVES < OR s 1 III. ARE
4. IF Ott.Y OllE LDAD 15 GIViti FOR ErtlARO14Arlt IlODIFICAT10ll REQ'O FLOOR-110Vilit0 tillfG-Si litt OPERATOR. IT IS Tile ltAxttRAl F QUAL 00C ArVD E FILED
4. 2/1 = 2 Ill. CLASS 1 s

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~ ~- I ' :.. ; ; ;,. -7. - -. ^ii O O o t i 3415FtHAM LMIT 1 WBPM LIST STtRIE 1 NESSTER ENGINEERIHs CORPORATICH Rt44 DATE 11/09/02 j JOB hut 9ER 3I499 3-3047 REACTOR BUILDING CATEGORT 1 PIPE HOUHito EWIPHENT RtM TIllt 14.17.19 O. l ' PAGE 9 LILCO DOCHET 50-3tt ACTIVE BOP QUALIFICATION LEVEL E393 ITEHSI l ', nl! = 5 v 1 2 3 4 OPER LOAO-C'S OPERATOIt 4 OUAL STATUS I i OtMIM PIPE GUftL SPEC LOC. teAetR S!!! REPT 10. HOR VER SUPPLIER H00tl IIG. ' Y0l4 OPER

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1. Ct 2 AfD 3 vot.vt3 < M = t Ill. APE
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(* C zS/H RECOttift0Af!0f t TO LILCO

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5. PRESttn QUALIFICATION VatinFOR O Q

QUAL IFICAT I0ll It1LES10 TIES-

1. CL 2 AfD 3 VALVES A OR e 2 IN. ARE ll0RIZOffTAL Aff0 VfDTICAltF AUt.TED)

FLOOR-tIOUtfitO (tilfG-S IALL OTiltRS ARE AC

4. IF Ola.Y OffE LOAD IS U1Vitt FOR A enttVALUATIOtt C0f tPLETE fUlf elllE OPERATOR. IT IS THE ttAXIl Q

8 tREQUEST FOR DUAL OR 810 ISSUtc

t. m u OC 110104.

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3. CL 1 VALVES < OR a 1 Ill. ARE FLWT-It0UltitD ittffG-5) 0 20UAL 00C RtttIVfD

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SEpttHNt letIT 1 98PM LIST STON" 19tt93ffR EHOINEERING CORPORATION RUM Daft 11/09/92 JossteetR 11499 3-SORT REACTOR DUILOING CAf tGORY 1 PIPE 910VHTto EQUIPMEMT 5t24 TIttE 14.17.19 A f 5, LILC3 00CMET 59-3tt ACTIVE BOP QUALIFICATION LEVEL t 393 ITEtt39 PAGE 7 t 5 3 om ' t 1 2 3 4 OPES LOAO-G'S OPERATOR 4 QUAL STATUS

I ttMIII PIPE GUAL SPEC LOC.

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i It3tettevetIS 1.5/1 253 SC 2.8 1.9 LIltITottGUE SitC-0*-5 5 F h It3tettovetlC 1.5/1 251 SC t.5 2.4 LIll! TORQUE SHC 'J4-5 s F IE3tillDwetI9 1.5/1 253 SC t.4 1.5 LIttITORQUE '8C-04-5 8 F ) 183tattOV9ttA 1.5/t 253 SC 2.3 1.5 LIllITORQUE Set-04-3 8 F It3tattDvett8 1.5/2 253 SC t.9 1.7 LIMITORQUE SIC-09-3 8 F It3tettOV9ttC 1.5/t 253 SC t.2 2.7 LIttITORQUE SIC-04-3 8 F IE32 HOW9tte 1.5/2 253 SC t.4 .4 LIll! TORQUE Sitt-04 3 0 F 1t32:190V023A 1.5/t 253 SC 1.5 1.3 LIllITORQUE SHC-09-3 8 F It3t HOV9239 1.5/t 253 SC 1.5 1.3 LIMITORQUE SIIC-04-5 8 F It3tattov023C 1.5/t 253 SC 1.5 1.3 LIllITORQUE StIC-09-3 8 .P QUALIF ICAT10tl llILE Stullt3 440TES REV1310tl 4 -fluVitetR 1902 i A sptEveLUATION CotrLETE

1. CL 2 AfD 3 VALVES < OR s 2 IM. ARE
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i 4 4 "*W "S """""""""""""""""4 4 W O E5 " E g g g,---a zg = = = = = = = = = = = = = = = = = =. - e a--< o g a. g eB:ow-gsg ee- - E E:sc_Ec"o E.5 n n.. C $$n 3 <= = s s g 2 ,8 yr3 s w w ..,,,,,,,,, w u c a 4* - O Er Q L M ,m "sss $ ~E x c o < :g n M S. 3' .. S.... R. R. . 2 e O8==,- r. =. =. =. =. =. =. =. =. =. =. =. = s :a :. :. v

as=es.sw g

ggg ggBggBB$.Bl ,v 5 0 B B B .. u o t. - o = 5 5 7 i 7 i

: i : :

1 =W = a 2 : : : : : : : : : : : : : : : = = ~ w w - - - - - - - - - - - - - - - -. m g H N M N N N H H N W H H M N H H H Ms l lI ?LL-k --- - f7 H U L( L L (, b y

JI

  • I st0RtMAft tatti 1 NOPM LIST STtRit & MEBSitW ENGINEEWING CORPORAT10M IMM DATE 11/94/02 l

) JOB HUteEn 11490 3-SORT REACTOR SUILDING CATEGOIIY 1 PIPE tim.RITED EQUIPtitMT RtM TIttE 14.17.19 A i I LILC3 DOCHti 59-322 ACTIVE BOP OUALIFICATIOff LEVEt, (393 ITEttSI 8' AGE 19 i ! ' i 5 7

  • e-A I

t 3 4 OPtW LDAD-S'S OrtWATOR 4 OUAL STATUS I HARM PTPE 90AL SPEC LOC. DEACER SIZE REPT 800. HOR VER SLFPLIER IIODEL HD. YOI(E OPER 4 It11rA0V941A .75 19.3.115 314 SC 1.5 1.3 COPES D-199-49 H H lt11eAOW9418 .15 19.3.115 318 SC 1.5 1.3 COPES D-100-40 M M A 1 It11rA0vterA .75 10.3.115 310 SC 1.5 1.3 COPES D-100-69 M M l 3 {!', It11rAOW94:9 .75 10.3.115 310 SC 1.5 1.3 COPES D-100-40 M M O l t{l 3 it31ePCV9934 le 10.3.115 318 SC 2.9 3.9 COPES D-100-149 M M It11ePCV9938 18 10.3.115 310 SC .9 .4 COPES D-100-140 M M O 9: ) j It11ePCWe974 4 18.3.115 310 SC 1.2 .9 COPES D-let-lee M M I lt11ePCV9019 4 19.3.115 310 SC .4 1.3 COPES D-109-100 M M l. 3 It:1eA0veet 1 19.3.115 318 SC 1.5 1.3 COPES D-199-40 M M It 1eAOW992 1 16.3.115 310 SC 1.5 1.3 COPES D-100-40 M M 'T ) 1E41oAOW993 1 10.1.115 318 SC 1.5 1.3 COPES D-100-40 M M It:1oLCV-991 1 19.3.115 310 SC 1.5 1.3 COPES D-199-49 M M q ', i 0 1t;1eLCV995 1 19.3.115 310 SC 1.5 1.3 COPES D-100-40 M tt l - i IESicA0V991 1 19.3.115 310 SC 1.5 1.3 COPES D-100-49 M M e ItsitA0 vest 1 19.3.115 310 SC 1.5 1.3 COPES O-300-49 M M It511A0V063 1 10.3.115 310 SC 1.5 1.3 COPES D-100-40 M M i I I It51sLCV991 1 10.3.115 318 SC 1.5 1.3 COPES D-100-40 M M I 5 4 IE51sLCV095 1 18.3.115 314 SC 1.5 1.3 COPES D-100-40 M M b 1 1P42ePCVOT1 4 19.3.115 318 SC 1.2 .5 COPES D-100-40 H H ( QUALIF ICATI0ll IllLES10f tE S tt0lES REVIS10ll 4 -tt0Vil1 DER 1902 h j8 A :PEEVALUATIDH COtrLETE

1. CL t N C 3 VALVES < OR = 2 IM. ARE
5. I'REstIIT GUALIFICATIDH VALIO 8 rREntfEST F0t? OUAL 09 BIO ISSUED FLOOR-ItourtTED ttttTG-5 i FOR OPERAfort LOA 05 < OR = 3 G'S C $/H REC 0ttttttOATIOtt 10 LILCD
t. m OC ICTO't.

Alt. OtttERS ARE AC lt04IZutifAL Atc VERTICAltFAULTEDI p-

3. Ct.1 VALVES < CR = 1 Ill. ARE
4. IF Ott.Y OllE LOAD IS G1vtH FOR D =00AL 00C RECEIVED E:ItAt'CitARE It0DIF ICAf!Dil REQ'O FLOOR.1100tif f D ( E tttG-S i Tilt UPEPATOR. IT IS Till 11AX111U!t

~~ F squat 00C ArvD & FILED

4. 2/1 s 2 Itt. CLA531 G s50RT PAPER C0t1PLLi[

p H CDPIES OF 00C 10 DIST3tIOUTION l 1

(,7. ',,... - O O ~, ^.: h NtM Daft 11/99/02 STUtit & MtBSitt tilGIMttWING CORPORATION A ? WISPEMfM WitT 1 99PM LIST Rut TIlit 14.17.19 REACTDet DUILDIllG CATEGORY I P1rt HOLJtitD E001Pttiff i i b JOB taasta 11400 3-SceT Pact 11 I,0P QUALIFICATION LEVtt (39311titsi l k LILCO DOCHET 50-3tt ACTIVE ! i ~ a 7 .a s j j, 1 e 3 4 Orta toAo-s'5 OrtnATOR 4 qual STATUS 3 t f haIRt PIPt SUAL SPEC LOC. ItketR Silt REPT 800. HUR VER SUPPt.IER HODEL I40. YOHE OrtR h O 1719eapv9914 4 19.3.151 318 SC 4.8 3.4 COPES D-100-100 F F D I I litgeacutelt 4 19.3.151 318 SC 2.9 3.7 CtVES D-100-100 F F O ', S i 11tteA099994 4 19.3.151 318 SC 1.9 1.2 COPES D-100-100 F F D 11tteAOv9999 4 19.3.191 334 SC 3.t 2.2 COPES O-100-100 F F I I }, 1194e40We794 4 19.3.145 318 PC t.5 1.5 COPES D-100-100 M N t 3 1794eA0ve70s 4 14.3.195 318 SC 2.3 1.3 COPES D-100-100 M M . k. y

, 1 4

1794eAOv979A 4 19.3.151 310 SC 3.7 1.4 COPES D-100-100 M M e 7-I IT44sA0V9799 4 19.3.151 318 SC t.4 1.9 CDPts D-100-100 M M O I, i IP9teTCV991M lt C074-St 423 SC 1.4 1.4 FISIIER 454-40 M M i i 1P9teTCV991X 19 CD74-82 423 SC 1.3 3.1 FISittR 454-40 M M IP9talCV001Y 12 CD74-St 423 SC 1.9 1.4 FISilER 454-40 M M 1P9teTCV991Z 19 C074-82 423 SC t.0 1.8 FISittW 454-40 M M 5 (9 992 SC 1.5 1.3 g 1190sPCV1414 .25 ? 5 IT94ePCV1938 .25 492 SC 1.5 1.3 8 h 492 SC 1.5 1.3 1190ePCV!93C .25 8 1190ePCV1930 .25 492 SC 1.5 1.3 'T 8 Gs 492 SC 1.5 1.3 1TieuPCV1994 .25 8 1T;8sPCV1998 .25 992 SC 1.5 1.3

  1. )

8 h 492 SC 1.5 1.3 1T*8erCV195A .25 Rtv!SI0tt 4 -Il0VttetR 1902 .T it0TES QUAL 1r tCAT10tl llILES10 tits p

1. CL 2 Ate 3 vat.VES < OR = 2 III. ARE
5. PRESttIT GUALIFICATION VALID TOR 0?tRA10ft LOADS < OP = 3 C'S A tRttVALUATIOff Cott't.f f t 8 REQUEST FOR C'JAL OR 810 ISSUED TLOOff-ifntAITFD t rific 5 I HG'11Z0tliAL Af D VIRTICAlt f AUlltDI C S/II ptC0tatttR?ATI0tl TO LILCO
t. o OC fl0f 0ft.

ALL OillCRS ADE AC

4. Ir OtILY Clit LOAD IS GIVEll F0ft

(

3. CL 1 VALVES C On : 1 Ill. ARE D 200AL DOC RfCEIVED Ilit CI'ERAIOrt. IT IS Illt IIAXIIfUff E-Itaf'06tApt ItnDIFICAllotl REQ'O FLO0ft-lfoUtttto (titiG-5 3 F =00AL 00C ArVD & IIttD
4. 2/1 = 2 Itt. CLASS 1 Q

C :59ftT PArtR Cots'8. tit ll : COPIES Or DOC TO DISTRIDUTI0tl

-~ O StM Daft 11/94/82 STtRIE & HEBSite ENGINEERIlft Cf1RPORATIOtt EsWPttutt 19117 1 WWW LIST Rt#t fillt 14.17.19 REACTOR BUILOI?IG CAf tG0ftY I PIPE IIOLMitO EQUIPittHT % JOB In ste tiett 3-SORT PACE 11 80P OUALIFICATIort LEVtl (39311tHS) I LILCO 00CHti 50 3tt ACTIVE A 7

  • 8 5

1 2 3 4 OPER LOAD-8'S OPtWATOR 4 QUAL STATUS ttARM PIPt tIUN. SPEC LOC. Maett SIZE REPT

  1. 0.

110R VER SUPPLIER IID0tt 80. YOHE OrtR 4 ' t 1 8 + 492 SC 1.5 1.3 1140ePCV14M .t5 8 492 SC 1.5 1.3 o 1740erCV14SC .25 8 i t i 492 SC 1.5 1.3 1144erCV14SD .25 l 8 1144ePCV1944 .25 492 SC 1.5 1.3 4 ! ; 8 492 SC 1.5 1.3 $t! 1T49ePCW1948 .25 8 if IZ93sPCVS194 .25 492 SC 1.5 1.3 O p '. 8 p 492 SC 1.5 1.3 i( 1293mPCveles .25

  • l

' ? e 8 It93eFCv011A .25 493 SC 1.5 1.3 5 8 t pin 493 SC 1.5 1.3 1293eFCV9118 .25 4 i H 1821mSOV3134 .75 letSt45443271 det SC 1.5 1.3 ft g !!!!aSOV1138 75 9e15245481271 400 SC 1.5 1.3 H 1121mSOV1144 .75 let5245463271 400 SC 1.5 1.3

  1. )

I H IIrleSUV1148 75 1515245481271 400 SC 1.5 1.3 H O ', g It11mSOW1444 75 15t5245483271 400 SC 1.5 1.3 H O It11mSOV1448 75 195245401271 409 SC 1.5 1.3 ff It11mSOV1474 .75 15t5245481271 400 SC 1.5 1.3 H It11mSOV1878 .75 095245481271 400 SC 1.5 1.3 H It11eSUV148 .75 IR5745481271 400 SC 1.5 1.3 9 H (* 1E11aSOV149 .75 IR5245481271 400 SC 1.5 1.3 REV1510tl 4 -t40VElmtR 1982 h ImitS ~ QUALIFICAil0tt IIILESI0ttES O

5. PRESENT UUALIFICATIDH VALID
1. Ct. E Ate 3 VALVES < OR = 2 Ilf. ARE Top cPtpateR LOADS < 09 = 3 C'S A mREFValtmTI0tt Collrttit f LOOR-t0UtfTED (titTG-5 I llopilotif AL etc vtRTICAt.t F AULTEDI Q

8 rpt0UtST TOR QUAL OR D1D ISSUTO C zS/H ptCOf sttil0AT10tl 10 L1LCO

2. e = OC f80 TOR.

ALL OTHERS ARE AC

4. Ir OtLY Otit LOAD IS GIVtti FOR G,
3. CL 1 VALVES < OR = 1 1H. Apt tilt OrtRATOR. IT IS litt itAXilfult D squAL 00C RECEIVED tellApollApt it001FICAT10t8 fttfl*D Ft00ft-f fautif f D t tifiG-5)

F =00AL 00C Al'vD & Filto

4. 2/1 = 2 Itl. CLASS 1 g

G 250ffi PArtR C015'ltit Q Il COPIts or DOC 10 DISTRICUf f0tf

. -... _ ~. '.... _ O m; ~ I i SNUptf W f l#f!T 1 perpt LIST STONE A MEBSite EHCINEEWIMG COPPORATION NUM DATE 11/94/92 -![ A JOB IRABER 11400 3-3047 Rf ACTOR SUIlo!!E CATEGoltY I PIPE It0LAITED EQUIPIIENT RUM TIlit 14.17.19 A I LILCO DOCHET 54-3tt ACTIVE 80P QUALIFICATION LEvil (393 If ttfSt PAGE 13 i b 5 7 S A t { 1 2 3 4 OPER LOAD-s's OPEWATOR 4 OUni, STATUS j ; IWNt FTPt EUAL SPEC LOC.

  • i itASER SIZE REPT HD.

HOR VER SUPPLIER H00tL HD. YOHE OPER oIi h H i ! 1746 StP'1tAA .75 15t5245403271 det SC 1.5 1.3 ! I 1749eStN1tJ8 .75 195245483271 400 SC 1.5 1.3 H I i O i ! R ITeteSOV'.#74 .75 995245881271 400 SC 1.5 1.3 H 1144eSOY1279 .75 195245481271 400 SC 1.5 1.3 H 1 O l E% 1T;8sSOV1284 .75 tm5245483271 409 SC 1.5 1.3 H I ; f; g! O ]I d 1140eS0W1208 .75 995245483271 400 SC 1.5 1.3 H P 1T*.SeSOV1294 .75 Mt5245483271 400 SC 1.5 1.3 H ,6 l 1149eS0W1298 75 095245481271 ott SC 1.5 1.3 H 4 1T!8eSOV139 .75 IR5245483271 400 SC 1.5 1.3 H f ITt8eSUV111 .75 695245483271 400 SC 1.5 1.3 H O I (* H IT40sSOWI34A .75 195245481271 400 SC 1.5 1.3 IT48eSOVt36s .75 Im5245463271 400 SC 1.5 1.3 H O P 1708e50W1374 .75 Im5245483271 400 SC 1.5 1.3 H 1TI8e50V1375 .75 IW5245483271 400 SC 1.5 1.3 H 9 P 18tlettove35A 29/1 20-1500Glet 88AO SC 9.8 t.4 LDtITORout Sem-1-49 H H 1821eHov0355 29/1 to-1500GLO9 88AO SC 7.5 3.5 LIttITOPQUE Sin-1 49 H H 1E11stt0V0314 20 E5834-1.2 88AD SC 7.4 1.1 LIIIITOROUE S15-0-40 H H 1E11stIOV63tB te E5834-1.2 00AD SC 4.8 .5 LItt! TORQUE Ste-0-40 H H 3 1ElletIOV031C 20 E5814-1.2 80A0 SC 5.3 .5 LIlf!TOROUE stb-0-40 N H QUALIFICAT!0f t itILESi0 tits II0f tS REVISIOrt 9 -It0VifIDER 1902 A rptEVALUATI0f t C0f f'LETE

1. CL t AfD 3 VALVES < OR s t IH. AR[
5. I'ntstriT CUALIFICATION VALIO 5 rREQUEST FfN QUAL OR DIO IS5UED FLOOR-tiOUttitD (EllTG-5 I FOR OPERATCR LOADS < OR = 3 G'S C r$/H REC 0tattlinATI0tl TO LILCO
t. e s DC lt0 TOR.

ALL OilIERS ARE AC liOR120tliAL AfD VtRTICALIFAULTrol G

3. CL 1 VALVES < OR 1 Itl. ARE
4. IF CriLY OtlE LOAD IS GIVEN FOR D =00AL 00C rtCEIVtD ErllAD0ilARE IMDIFICATI0tt REQ'O FLOOR-It0VilTED fillTG-SI Titt OPERATOW. IT IS TifE ItAXIIIUtl F =00AL 00C APVO & FILEO
4. 2/1 e t Ill. CLASS 1 e

(I? G eS9RT PtPER CottPLETE ["j H COPIES OF 00C TO DISTRIflUTION 1*

o ...-e e- ~ e r .e mM DATE 11/981K2 5 TONE & MteSTEW ENGItitERItO CORPORATIfRt O RtM TiffE 14.17.19 l SOUREMM1 tMIT 1 WePM L157 RfACTOR BUILDING CATEGORY I PIPE HOUltit0 EQUIPttEfff PACE 14 1 i JOS 84UlttR llett 3-SORT BOP QUALIFICATI0tl LtVtl (393 ITEttSt LILCO DUtWtf 50-3ft ACTIWC F A 7 4 f 5 ( 1 2 3 4 OPER LOAO-S'S OPEWATOR 4 QUAL $TAttJS [ ) tthSgt PIPE SUAL SPEC LOC. e taastW SIZE REPT id. It0R VER SUPPLIER 9100tt. NO. YONE OrtR j 86AD SC 5.9 .5 LillITORQUE 395-0-40 98 H b. k l It11stRNO319 29 E5434-1.2 It11st1DVt3th te (5634-1.2 88AO SC 4.1 1.4 LittITORQUE stb-0-40 N N O 4 It11mitDVt3tB 29 E5814-1.2 O8AO SC 4.4 7.2 LIMITOROUE S15-0-49 fl 18 h [ lt11eHDVt3tc te E5834-1.2 88A0 SC 4.1 5.0 LItt1 TORQUE S10-0 40 N N i t 1E11sitOV0329 29 E5834-1.2 SSAO SC 5.2 4.5 LIMITOROUE S12-0-40 M N rb hd It11sttDV9344 18 18-3004 8640 SC 1.9 1.0 LIMITORQUE stb-3-150 N N 4 !1 I. f It11attave34s le 1s-3904 88A0 SC 1.5 1.9 L11tITORQUE Ste-3-150 M M j 9 IE11mitDVg344 24 E5634-19 G8AS SC 3.2 2.9 LItt1 TORQUE St B-4-200 M N et i p GSAO SC 4.9 2.2 LIttITORQUE Ste-4-200 ff M i ItlleHOV9348 24 E5834-19 j! 1811elWV9374 24/1 24229005T97 88A0 SC 3.7 5.4 LIllITORQUE $8-4-200 N N O ittleIIDV9179 24/1 2422900G107 80A0 SC 4.3 5.1 LItt1 TORQUE SS-4-290 N N a l P It11sttDVS10A 19 E5834-20 SSAO SC 5.8 1.3 LIllITORQUE Ste-t-40 ft M 'l It11=HOW0388 19 E5834-19 GeAO SC 4.3 1.5 LIIIITORQUE Ste-t-40 M If D It11mitDV94tA 14 E5834-4 08AO SC 3.2 4.1 LIMITORQUE Ste-3-80 N H T It31sttOV0429 14 E5834 4 66AO SC 3.3 4.4 LIttITORQUE $16 3-00 N N ij f. lt11stIDV047 20/1 20900-CT04 88AD PC 4.9 3.3 LIMITORQUE $8-2-40 M H l. It11stt0V048 20/1 20900-GT04 86A0 SC 4.4 3.0 LittITORQUE $8 2-40 m M M i lttistIOV931A 14 E5634-7 88AD SC 3.4 2.5 LIMITORQUE Ste-000-5 N H Ittlel10V0118 14 E5814-7 88AD SC 3.5 .4 LIttITORQUE Sim 000-5 Il ft REVIS10tl 4 tiovtitDER 1902 tiotts QUALIF IC ATI0tl titles 10 tits (=

1. CL 2 NO 3 VALVES < OR s t Ill. ARE
5. PREStiff QUALIFICATION VALID FOR OPER ATOR LOADS < 02 e 3 C'S A mREEVALUAT10tl Cele't.ETE 8 mRtqutST FOR QUAL OR BIO ISSUED FLOOff.It0UffitD (tiffG-5 I ll0RIzotiT AL Also VtRTICAlt FAULitDI Q

C wS/H REColettilDATI0tt TO LILCO

2. m n OCff0f0R. ALL OTilfRS ARE AC
4. IF OttLY otit LOAD 15 Givtti FOR p

O QtlAL 00C RfCttVfD

3. CL 1 VALVES < (Vi = 1 Itt. ARE lilE OPERATOR. IT 15 illE ttAXIf fUtt FLOOR lfoUttitD fillTG-St E:ltADDilant 1100lF IC ATInti REQ'O F 30UAL 00C APVD L FILED
4. 2/1 e 2 Iff. CLASS 1 g

G zSORT PAPER C0fE'Ltit g II COP 1tS OF 00C 10 OISTRIBUTIOff

.s.e.--..... .g..-..... .,_....................-~~g.=-..-..---. C ( e e e c ( c e e e c ~ o E He* ^. = = z z z = z = = z .==z = b

z =

Gn g*M a w .mW G>R M "gCm mOC W MW B = z

z = = = = =.

===w = = x ~ N"I" Us h

  • stEE 2"

E.E*~ = -mm >McMw a g kN MO h M M M M M M k s _g o. e M. e. a > e o e o M m e. - - - - - d i i a aii*i"~**aeaaa Ws'ws a Biii**iiiiiiiiii*i** bed 52 = = -e e e e e e e e e e e e e e e e e e s ~ Egu=eDg a a a a a a a a a a a a a a a a a a a : a 5 a s E wac w W 2006: E kw=M- -5 I sE EEEEEEEiE.1EEiENQ% i a e Es-a sasasaEaasssasssa s. -e-


w

--e-M M M M w M M M M w M w M M w M w g ow z = = =

= = = = = = = = = = = =

e M M M M M M M M M M M M M M M M M M M w l g g w-CM s J J J J J J J J J J J J J J J J J J J m g" e-: E E i= M g N 4 RMW M. M. M. M. M. F. M. S. W M. S. M. M. S. M M&J g - g "g. wg> g w W w W W M M M M M N M M M M & W W M s.a M. Ma M s. . ~.. B5 s M. M.

e. ~. ~.. ~.

e. .. ~. M. vo o-M=J.- M . - - M ,. M M J =P M Oh W = wwCRwm Rwd k Q-4 u O g>hU NO.ved l 1 >wg0~=M5e>E-w mc - NEW 4 Mg og WWW EWWWWWWWW WWW W WWW

  • E:dB.

"S J E+U> WMI C

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5 ee.een

  • g MeE s, n., g,.,,.,.,.,.,.,.,.,.,.,.,.

S a;, E k 5 so g "S 5 g a.......~~..--...==- es E .a

: : : : = =====

g

  • 7 i i*7 5
    • S

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  • i i i i i 8"
  • EBe-ww5 g*

WE :

  • RRRR RRRRRRRRRRRR E

g 0 5dO56eg3 eW-une-- s Be 0 988 5 9 E C~-oc2QCM o ~ s -- M S S e 9 9 M &M M M m M M M M m a a - a a a.. e e e 5 E*5v uED p>vowoc h e sewonoke N hw=<JhskU m M.S .s ccec = w 3 km E M m m e e m e m e > e. m a m m e w wws'mDCO sam 6Comu .e .e d gM-e m m m m M M M M M M e e e e e. a=== ma g g g g g g g g g g g g g g y B B ..ue"-== gEg E E 5 D, D, D D E E E D D 6 5 5 I B, 2 , I =., =, ;, 5, + og e ,,, 3 2 2 2 s 2 3 3 =. =.

.==. =- = = = =

..= = = = = ti n. = w - -. ws N N n m m m M N N N N M N H H H M M M i n-p n n n. n n n n p n g g e

..... -. -.... - ~. - ~. -. 1 ( ( ( e c e e e c e e e o e e (b) s, e .=. z = z = m z z z = = x z e z z z z z .g _g 1 e g s,e - ..""B E-w 2"I": 342 E w

  • W 5 : z = z e z z = z z z z z e z z z = =

W"tE: WE B "BiEW 2: hyMU" i w -me ema-- $!E S: 5..* m wase. Em m. m. m.

m. m m. - e.

_a .. n - - -.. d 4 3 i eaaa** i a"i WB'wB iii SEWEE " "

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$ *e ie e a s e a a e a e e a e e a s s s ~

-

EgeOg a a a a a a a a a a a a a a a a a a a E U "l l S EBBwe 2 a w-=-- Q = b gB-B B B B B B B B B B B B BB B B B B B 5 w* O M

    • E B = - = x = = E = = = x = = = = = x = =

inw w-M M a M M M M M M m M M M M M M M M M M w f Q WH d d d d J J J J J J J J d & 4 J d J J 4 m o me O" EEN - E '}i M m

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" 9 ", e E. ya. H H N N N M N H H M N H N F G y M m. -z md ,,....., -... N,. - - -. u M o e o e e v-. On ,e e e e o e e e e

  • _'5 M = s'

P P

M ed N go y e e o e .e M N N M P* M M O-O N M N M M wm 6Qwe W 3 .O-g t- - 5 wC zuM Qu 40

  • gWw U b s* U.

m -w-= $gI O2,- e S_: W a. v > 8. N -g .g WWXMNN WXEWWWXXXXXWM "S N$.~B" wI e sE o-5_ dd.d"t -"g nS'

t. >.

gE >. >. R. g4 j y E O Ee E CS 5 - e e N. ed - R e" ~ ~. -~ ~~-

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    • 2

~5.5".*Gc i i i NWt *i* i i i ii i 3E BE R R RR R R RR R R R RRR R R R RR s B ee:-e es .-av. .Dgw_we s e = e ,s_~~cL.u,,_,t3 M

s. >..

_2 e . M. =.- -J,wCCGEM C. N .=.J-- .M _.e = m. B. o< E.. m..s N aa N. mR_ d 5 I,, I I I I,. i. I, I,. -..5 5,5 m uan a u m M _- s B <=u=;-== E,, 5, t -[5 'e 5 2 e 2., s 5 O. E. E. %. 3 E O. N. O. O. O E E E E 7 E E E "o w w w w = = = w - H H H H H H H n n - n n H H H H H H u j 3 f-rse w

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I. ~~ O SMONTHf 1 St LIST STCHC & HESSTER ENGINEi CORPOR". TION ItuH DATE 11/04/92 JOS HLS. 494 3-SORT GEllETAL EttCT;IC COTE EQUIPittHT RUtt TIl3 14.14.C3 4, O LILCD St !!t ACTIVE HSSS OUALIFICATIO*t LEVELt151 ITElfSI PAGE 1 HARN ESUIPMENT St SLDO AVAIL QUAL QUAL TYPE SAFETY quel p . { t%stitR DESCRIPTICH NO. VttfSOR ELEV IHSP REPT HETH FRttl HTNG FUIC STATUS gj ?Dtle6-9 3 CERetMBEMB CMAPSER 921000t St SC000 YES DNF-A00T94-11 SA 49e P HS.CS S

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  • DESCRIPT!cM NO.

Vtte0R ELEV ItfSP REPT HETH FRtt flits FUllC STATUS ) g ) j k 3C11eAONG1 MCU DIAplWAWt VALVE C11F010 lett SCOTS YES SA P CSett$ B l IClasA0 Net MCU DIAPMRAEM VALVE C11F011 1994 SCPat YES SA P CS.MS S ) q j i 3C11eLS M9 LEVEL 3061708 C11M013 MAOMETROL SCOTe YES SHIP LOOSE S4T 396 F2 F . s IC11eLS 999 LEVEL SMITOt C11N013 MAGMETROL SCOTS YES DV159C9341 SAT 39* F4 M D l ( ) q t IC91 TM-903 SLC STORAGE TAtet C41Aest LANCO SC113 YES RA54t/C41-Et SA $9 F M S i i IC91: Tit-130 SLC ACOAtuLATORS C91A003 NYDRA COM SC997 YES DRF C41-tt SA M/A Pt M S ) g y ld ? IC91eP.Ott STUSY LI4 PtRP&HTR C91C991 tRtION PUH SC113 YES VPF-5517-t t 59T 40+ Ft M S IC41sEV 919 tilPLOSIVE Val.Vt C91F9M CollAX SC112 TES VPF3394-34 2 S8T 350 Pt M S l ) q i t;. 3C91sTS8914 TD5' SMITOl C91H003 NEED INST SC112 SHIP LOOSE SAT 400 F D/E j i

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IC91ePT Set PRESSURE TRAMSittTTER C41 NOM ROSttIDIRtf SC112 YES DV143C1543 SAT S F M D ) ,3 ii ICClePI Det PRESStAtt DWICATOR C91R993 ROBT SHAM SC11E YES DV143C1184 SAT 33e F M D ,(( ICS1sTIP-SM TIP VALVE eutDE Y C51J0M St SCOT 3 YES DRF-A00992-M SAT 400 F4 M D ) IC41sFT 991 DIFF PRESS 30fft C41M001 IPOSEMUtRtf SC000 YES DV143C1948 SAT Se F M D IC41ePT 904 PRESS TRANS C41H004 SAILEY SC979 YES DV141C1184 SAT 33e P M D ). q 3C41eCE 014 Core TRAttSetITTtt C41tt000 SALLSOAUS SC030 YES DV143C1599 SAT 3 P M D t ) q l 3C41sPtt.-RSP RtiWTE Set? DM Pvt. C41P001 St SC043 YES SAI-Ot90A80PA-B lef 14 F M D { 3CT1sPS 993 PetSSURE SetITCM CTitt003 BARMSOALE Cs931 YES DV149C5359 SAT 33+ F4 M D 9l It31tt-934 RMR NEAT titCHANGERS E118001 PERFtX CP SC004 YES DRF E11-1 DA 14 ft MS.CS 8 ) It11eP-014 NHR Ptss's almTORS E11C002 SJ/GE SC006 YES DRF E11-11 D4 le F4 HS.CS S } C5 eCONTWG. BLOS P PIPE H0tRITED SBTzSINGLE FREQUENCY QUALIFICATION ff!LESTONES REVISION 4 -NovtteER 1992 S _ CS rCOLO SHUT 00000 PC :PRIttARY CONT. BIAXIAL TESTING A rREEVALUATION C0tFLETE 03 rCYt4Aff!C ANALYSIS PL :PE0ESTAL SC MSEC 0fl0ARY CollT. B mREQUEST FOR REQUAL OR BIO ISSUED HOIEt IIUt DER lit F sFLOOR 810UHTED QP sQUALIFIED BY / eLOCATED Ott Cotti. C *S/H REC 0fttErl0ATION TOLILCO ' TYPE HTNG' C0ttAIN IS h ) MS SHOT STAfIDBY PIP 3tG AtlALYSIS HALL D = QUAL DOC RECEIVED QUAttTITY OF ITEttS. 13T:IfUL T I-FREQUEt4CY RH tRA018ASTE T altA1H STit. TIR88EL E silARDitARE tt0DIFICATION REQ'O BIKKIAL TESTIfG SA

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. _., aa..;, - ~ ~ q i 31EFE98WS IMIT 1 St LTSV STtME & 9EBSTER ENGINEERING CORPORLTItNt RL#t DATE 11/94/02 JOB Hulate 31400 3-SORT SLNERAL ELECTRIC CATEG0ftY I EQUIPittNT WUN TIIIE 14.14.43 i LILCO DOCMtf 50-3tt ACTIVE HSSS QUALIFICATI0H LEVEtt151 ITEttSI-Pact 4 f HARM . Emf! MENT st OLDO AVAIL OUAL QUAL TYPE SartTY OUAL ?' f Muiste DESC#IPTION HO. VENDOR ELEV IttSP REPT HETH FWtg HTHG FutIC,STA;US q 4 I ! ItStePT 035 OASE PWESS TWAMS E3tMOSS ROSttIOUNT SC043 YES DV143C1544 SAT 5e F M D l It3tePT 034 ABS PWESS TRANS E3tN054 ROSttIOUNT SC043 YES DV143C1558 SAT 59 F M D i 4 i - f RE3tePDT935 DIFF PRESS TRANS E32tt059 ROStHOUNT SC043 YES DV143C1541 SAT 50 F M D it:1eP-914 9FCI PtAF4800SYtW E41C991 PACIFIC P SC008 YES VPF-tT40-100-1 DA 23 F M D i q 1E*15tU-998 IFCI TUROINE E41C992 TEsntY SC000 YES teT F M D 1841eLSO934 LEVEL SMITCH E41N002 HACMETWOL YARD YES Dv159C4294 SAT 1 F M O 4 1tC1sLS8930 LEVEL SMITCM E41H003 IIACHETROL YARD YES DV159C4294 SAT 1 F M D .\\ It43aFE 803 FLOM ORIFICE V41H007 VICM set 3 SC021 YES SAI-DJC3 SA 40e P M F/Z g g fh 1E%2sLSO91 LEVEL SHITCH E41tIO14 MACHEYWOL SC014 YES DV159C4341 SAT 4 F M D EttleLSett Ltvtt SMITCM E41H015 MAGilETROL Stet? YES DV159C4294 SAT 1 F2 M D 1t4127t953 fttFEWATURE Ettlefff E41H024 PTCO SCO34 YES DV195C3224 SAT 40+ F2 M D l t 1E'Isit054 TETFt#ATURE EttHttff E41N028 PTCO SC025 YES DV195C3224 SAT 400 Ft M D ,) 1E;1:Tt955 TilFEWATURE ELEMENT E41N029 PYCO SC017 YES DV195C3224 SAT 406 Ft M D It417.Tt954 TEIFERATUtt EttHENT E41NO30 PYCO SC043 YES DV195C3224 SAT 400 F2 M D It41:TI191 Tier IIBICATOR E41R002 Mtt0 SC000 YES DV195C3103 SAT 109 P M D s i It51mP-915 pCIC PUllP ESIC001 DINGHAM SC000 YES ORF E51C00112 SA 24 F MS 5 It51sTU-905 - WCIC TURDINE E51C002 TERRY SC000 YES VPF3422-79(13-2 SA/IST 15 F HS D f It51tFE 003 FLOH ORIFICE E51H001 VICM SIMS SC018 YES SAI.D K 1 SA 4ee P MS F/Z l 1E51eLSO91 LEVEL SMITCM E51N010 MAGNETROL SC006 YES DV159C4341 SAT 4 F M B l CD atollTROL DLDD P PIPE HOUNTED SDTzSINGLE FREQUEHCY QUALIFICATICH HILESTONES REVISION 4 -HOVEtIDER 1992 ! _CS COLD SifUT 00699 PC :PRIllARY CottT. BIAXIAL TESTIllG A zREEVALUATION C0lIPLETE DA sOTIIAtlIC AtlALYSIS PL : PEDESTAL SC sSEC0ff0ARY C0tif. O rREquEST FOR RE0tlAL DR DID ISSUED HOTE: BluttntR Its F nFLOOR lt0UtifEO QP r00ALIFIED BY / rLOCATED OH C0rif. C zS/H REC 005ffil0ATION TOLILCO ' TYPE ffTNG' COLUt94 IS HS sitof Siellot)Y PIPIltG ArtALYSIS HALL D =00AL DOC RECEIVE 0 QUAllTITY OF 1tE113. ICTalIULT I.F RE QUEt8CY RH *RA0llASTE T =1lotti STit. YtNelEL E ellADDilARE tt001FIrATI0tl REQ'O BIAMIAL TEST!tlG SA STATIC AffALYSIS N stIEITIIER CS OR 113 F 300AL DOC APVO A FILED flSirlfJt.T I-f REQUfl4CY SAirStrict.E FREQUf flCY Z ePASSIVE ITElf G =SQRT PAPER CottrLETE SillGLE AXI AL TESTING SiliGLE AXIAL TESTING (SORT PArtR IIOT 51 = COPIES OF DOC 10 DISTRIBUTION l REQ'DI l ~- 0 s \\

i D D : -- - - m. ) l RtM Daft 11/94/82 STONE & MEesTE2 ENGINEE2ING CORPOR'.TIcti WUtt TIltt 14.14.43 O [ WigRenAM tmIY 1 St LIST GENERAL ELECTRIC CATEGORY 1 EQUIPItENT JOS PAmetR 11499 3-SORT PAGE S HSSS QUALIFICATION LEVElf151 ITElfst i ) LILC3 DotMtf SS-Stf ACTIVE MAmt

  • EWFIPHttff St SLOG AVAIL QUAL WUAL TYPE SAFETT GUAL g

I Mulett DESCRIPTISH 880. VDSOR ELEW INSP REPT METH FRtg Hite FtAIC, STATUS 1EStsit958 TBFtWATURE ELEttDff E31N911 PYC0 SCO25 YES DV195C3224 SAT 49e Ft M S ) [ 18515T1953 Yttet#Aftatt EtttENT E51H9tt PYC0 SCOET YES DV195C3224 SAT 40, Ft M S q 3 ltS1 sit 999 TttFERATURE EtttENT ES1H9E3 PTCO SC043 YES DW145C3224 SAT 49e Ft M S 1 ItS1:TitSS TD FERATURE tttttENT E51tettS PTCO SC044 YES DV195C3tte SAT 49e F4 H D q 1 g ltS1:Tt994 fttetRA1Upt ELEHENT E51tf924 PTCO SC044 YES DV195C3224 SAT 49, F9 M S 19512T1141 THERtIDtETTR E519995 ROBT SMAM SC999 DV195C3193 SAT 199 P M S q I i 1F11270-995 FUEL PetP ttACMItEE F11E991 St SCIT4 YES DRF F999999t-3 DA WA Ft M S \\ '. d IF11sTO-908 Stft PURPost SRAPPLE F11E011 St SC174 YES DRF139F11E011L SA WA F3 M S q 1F13sSL-991 DItYERtSEP SLING F13E994 CAL PAC SC174 YES DEIF F13-9 SA WA F M S J S } 3F13sTS-914 IIEAS STROMESACM F13E999 LAMCO SC174 TES DRF F13-11 SA WA F N O 9 IF*Cr.TO-Ott CONT It0D GRAPPLE F14E992 SE SC174 YES DRF139F14E99tM SA WA F M S 1F15eCNN-999 REFUEL PLTF ASST F15E993 STERM NOS SC174 YES DRFF999999tt DA WA F M S g } IF14eRAM-19 STRS RACMfCREDEF F3 F14E994 St SC13T YES DRF FI4-9993 DA 13 F3 M S DA Ft M B 1F14e#AM-99 FUEL RACMt1H VtSSL) F14E994 VOTAM SC174 I IF14:RAN-11 NEM FUEL STRS RACMS F14E997 GE SC151 YtS DRF F99-99992 04 WA FIT M S 1FIdeCSH-91 DEF F STRO CotfTAIM F14t999 GE SC151 YES 139F14E999N1 DA 1 FS M S 3 1F141 RAM-StS POISON CURTAIN F14E015 Dir SC151 YES DitF F14-99999-1 DA 1 F14 N 8 1533eFE 913 OIIIFICE FLANGE G33H911 VICH SIMS SC SHIP LOOSE SA 496 P F/Z IS33 ATE 971 fttFERATURE ELEHDff G33N914 PYCO SC134 YES DV195C3tt4 SAT 49e F4 M D

  • )

h CS aCOfffROL SLDS P ePIPE HOUNTED S8TsSINGLE FREQUENCY 00ALIFICATION HILESTCtlES REVISION 4 -HOVEt18ER 1982 PC PRIttARY C0ffT. 81 AXIAL TFSTItG A sREEVALUATI0tt cot 1PLETE _ CS 3 COLD SttUT DOMI SC SEC0f 0ARY C0tif. B 3 REQUEST FOR REQUAL OR BID ISSUED tiO1Et tU10ER IN DA EDYt4AttlC AllALYSIS PL PEDESTAL C zS/H RECollittfCAT10ft TOL.ILCO ' TYPE HitC' COLUlpt IS h F tFLCOR 110U41E0 GP =00AliFIED BY / mLOCATED Oil COttT. 00AtiTITY OF ITEttS. D zQUAL DOC RECEIVfD h itS tlinT ST At1DDY PIPItG AflAt.YSIS llALL l 137:11 ULT I-f R E QUttlCY WH mRA0llASTE T rifatti STM. 7tAffEL E =llARDilARE 110DIFICAT10N REQ'O l' 01 AMIPL 1ESittG SA eSTAt!C AtlALYSIS N rifEllHER CS OR llS F tQ9AL DOC APVO 1 FILED l ItSizittA.11 FRt09f tlCY SAf rSillCLE FREqutfiCY Z PASSIVE 27 Eft G e5f;nf PAPER Col 1PIETE

  • )

SillGLE AXI AL. TESTING Slfl0LE AXIAL TEST!!C 60013 T P Ar E R HOT 11 : COPIES Or DOC 10 OISTRIDUTIDH e, REQ'0 8 I ~

L,...,.,-- . ~. O O O b. m SeptMAM 1ptIT 1 St LIST STOHE & HESSTER ENGIllEERIHs CORPORATION stM OATE 11/04/CE j JOB tAseER 13499 3-SORT GEttERAL ELECTRIC CATEGORY I tou1P1tEt4T RUN TItfE 14.14.43 O LILCO DOCMtf 30-3tt ACTIVE 18333 OUALIFICATInN LEVEll151 ITEHS PAGE 4 fleRN "FWIPMDef Of t%DG AVAIL tRfAL QUAL TYPE SArffY OUAl. IAAZER DESCRIPTIWf NO. VEteOlt ELEV INSP RLPI HETM FRES HTt4G Fullt. STATUS ,g l 1833sFE 011 W IFICE FLANGE S13tt033 VICM SIMS SC SHIP LOOSE SA 49. P F/Z [ 1833:Ft91t W IFICE FLANGE S3399049 TH SIttS SC

  • SHIP LOOSE SA 49e P

F/Z g 1833eFTelt 81FF PRESS TRANS S33tt041 ROSEHOUNT SC100 YES DV14SC3240 SAT Se F M 0 ? 1933sTtettt Ttte'fRATURt EltilDff $33H042 PYC0 PC97 YES SHIP LOOSE SAT 10 F M 0 4 1M11epte.-491 REActCORE COOL 88 M11P401 SE C8043 TES SAI-0290A80PA-8 teT 14 F HS.CS S 1M11ertt.-492 RHCU & RECIRC BM M11P40t St C8043 YES SAI-0290480PA-B H8T 14 F HS.CS S t q, i 1N11ePIL-493 REACTOR CONTROL 8 H11 Pet 3 St C8043 YES SAI-9290A80PA-8 teT 14 F MS.CS S g. 3 . gt i 1N11sPIL-408 PtEl RANGE HEUT CA H11P400 St C8043 TES teT F M 8 g g.; 1M11ertL-499 TRIP SYS A RPS V8 M11P499 St C8043 YE:8 SAI-0290480PA-8 teT 22 F HS.CS S h 1111ePtt.-411 TRIP SYS 8 RPS V8 M11P411 St C8943 TES SAI-0290480PA-8 teT tt ? HS.CS S IM11eptL-412 FM & RECIRC IttSTR M11P412 St C8043 YES SAI-9299480PA-8 teT 19 F M S 1 11mPtt-413 PROCESS INSTR CAS M11P413 SE C8C43 YES SAI-0290A80PA-8 teT 14 F HS.CS S 1211ertL-414 ftSS TtlP LM DET V8 .H11P414 St C8043 YES SAI-0290A00PA-8 H8T 22 F M S f IM11ePtL-417 DIV 1 WHR RELAY V8 M11P41T SE C8044 YES SAI-029QA80PA-8 teT 19 F MS.CS S q 3M11ertL-414 WHR RELAY V8 M11P410 St C8044 YES SAI-0290A80PA-8 teT 19 F fts.CS S IM11ePtt-429 MPCI RELAY VERT 00 H11P420 SE C8044 YES SAI-0290Ae0PA-8 teT 14 F M S 3 1M11ertL-421 IC RELAY VERT 80 H11P421 St C8044 YES SAI-0290A00PA-8 teT 14 F HS.CS S 1H11ePtt.-4tt It90 ISO V RELAY V8 H11P422 St C8094 YES SAI 0290A60PA-8 teT 21 F CS S ) 1H11ePtL-423 OUT80 ISO V REL V8 H11P423 GE C8044 YES SAI-0290A80PA-8 teT 21 F CS S

  • )

I C8 aCCITROL BLDS P : PIPE HOUNTED SBTzSINGLE FREr.UENCY QUAL!rICATI0tt HILESTONES REVISION 4 -HOVUBER 1992 _CS ECOLO Situi 006et PC ePRIlfARY CONT. BIAXIAL TESTIllG A rREEVALUATIDH Col!PLETE 03 s3YttAtt!C ANALYSIS PL PEDESTAL SC e5EC0tIDARY C0flT. 8 rREQUEST FOR REQUAL 04 BIO ISSUE 0 NOTE fluttDER IN F sFLOOR 1100tifEO QP sQUALITIED BY / LOCATED OH CutlT. C eS/H RECatstEllDATIDH TOLILCO ' TYPE HitlG' COLUtH IS h HS til0T STAT 10DY PIPIflG AllALYSIS HALL 0 mCUAL DOC RECEIVED QUAtlTITY OF ITEttS. I:7. Tat tULTI-F REQUEtICY RH mRADilASTE T ellAtti STil. TUIRIEL E tilARDilARE IIUDITICATION REQ'O BIAXIAL TESTillo SA z5TATIC ANALYSIS tl stittletER CS Oft HS F = QUAL 00C Al'VD & FILEO ttSTst1ULTI-FREQUrtiCY 5ATrSillGLE FREQUENCY Z rPA551VE ITEll G s50RT PAPER CutirLETE I SINGLE AXIAL TESTING SIflGLE AXIAL TESTING ISQRT PAPER tt0T H 2 COPIES Or DOC 10 DISTRIDUTIDH REQ'03 ~

O SIDEIGNI l#tti 1 W LTST STr W & NESSTER ENGINEERIMO CopPotAT!tRt Rtst DATE 11/94/02 JOB ftsetR 11499 3-90RT GENERAL ELECTRIC CATEGORT I EQUIrllEffT RUN T!llt 14.14.93 e i q LILC3 00CHET 50-ftt ACTIVE HSSS QUALIFICATI0H LEVELt151 ITEttSI FACE 7 2 feest

  • ESLf!PtWtti St SLDS AVAIL QUAL QUAL TYPE SArtTY EUAL I i Impett DESCRTPTION te.

Vtte0R ELEV INSP REPT HETH FfttQ IITNG Futic STATUS g 19811erte.-484 DIV 1 CW SP Rtl VB M11Pete St C8094 YES SAI-029f!A00PA-8 teT 14 F CS S 1 ltoppe.-4t? SIV E CCR SP Rtt VS M11P427 St C8044 YES SAI-0290A40PA-8 teT 14 F CS S g 1211sPtt.-4tt At#TS BLtRetti REL VB M11Pete St C9994 YES SAI-9290480PA-B MBT 14 F CS S Ett31ePet.-431 At#TS OfPRESS M11P431 St C8094 YES SAI-0290A80PA-8 teT 14 F CS S g IM11erte.-43S DIV 1 RAS MtRtIT M M11P435 St C9043 YES SAI-0290480PA-B HDT 21 F M S i IM11epte.-434 OIV t RAS MDMITOR M11P434 St C9043 YES SAI.0290A80PA-B teT 21 F M S jf IR11ePft.-454 MSIL LISPMCASE M11P454 St C9043 YES SAI-8290A80PA-B teT 19 F M S { IM11erte.-455 MIST. LISHCAGE M11P455 St C8043 YES SAI-0290480PA-8 teT 21 F M S N q 1Mileptt.-01 CORE SPRAY RM CM A M21P991 St SC000 Yt3 SAI-0290A80PA leT 11 F CS S IMtlerte.-92 RHEU SYSTEM IttST M21P902 St SC151 YES SAI-9290480PA leT S F M S q { 18ttleret.-04 RX VES L & P RACM Mt1P404 St SC079 YES SAI-0290489PA teT S P ltS.CS S IMilePft.-95 RX VES L & P RACM M21P005 St SC079 YES SAI-0290480PA teT S F MS.CS S I ) 9 19ttlertt.-04 RECIRC PtRP A RAC .Mt1P004 St SC090 YES SAI-0290480P4 teT 11 F M S 1Milepft.-99 JET Putr A H21Pett GE SC079 TES SAI-0290A80PA lef 11 F M S IMiterte.-19 JET Pt#F IttST RM HEIP010 St SC079 YES SAI-0290A80PA leT 11 F M S IMtlePte.14 MPCI INST RACM H21P014 St SC000 YES SAI-0290A80PA lef 8 P M S g 1H21tPtt.-15 MAIM STM FLOM RM A H21P015 CE SC099 YES SAI-029QA00PA leT S F M S 1HttoPtt.-14 CS/MPCI LM Off I H21P014 St SC008 YES SAI.0290A80PA teT 11 F M C IHtlePtt.-17 NCIC IttST RACM H21P017 St SC000 YES SAI-029QA80PA leT S F HS S CD EColliROL OLDS P PIPE HOUNTED $8TzSINGLE FREQUENCY QUALIFICATION MILEST0ttES REVISION 4 -IRNEteER 1982 _CS eCOLD Sit 0T 00let PC :PRittARY C0tif. BitXIAL TEST!!G A rREEVALUATIcts Cot PLETE DA :DYllAtt!C AffALYSIS PL : PEDESTAL SC s5EC0tOAttY CotIT. 3 stEQUEST FOR PEQUAt. OR BIO ISSUED flofEt I Ut: DER Its F FLOOR IIOUlliED QP s0VALIFIED Bf / rLOCATED OH Cotti. C 25/H REC 0ttittf0AT10tl TOLILCO ' TYPE flittG' COLUtitt IS HS *1107 STAtt08f PIPIllG AttALYSIS IIALL D rQUAL DOC RECEIVED QUAttTITY OF ITEllS. IETalf9LTI-rREQUENCY RH rRADilASIE T ellaitt STH. TUlt'EL E *ilADDHARE 110DIFICATI0tt REQ'O DIU.IAL TEST 1ttG SA

  • STATIC ANALYSIS H site 11HER CS Ott 113 F rQUAL DOC APv0 A FILED ltST ul1VLT I-F Rt quEllCY SAirsifict.E FREcutitCY Z : PASSIVE 11 Ell G e57tt PAPER CottrLEIE SillGLE AXIAL 1ESf!HG 5!!IGLE AXIAI. TESTING ESQ'IT PAPER tenf H =COPIE3 Or DOC 10 DISTRIBUTION REQ'DI

e O O e Sq0NEMAM UNIT 1 St LIST STONE & MESSTElt EtCINEE1 TING CORPORATION ptM DATE 11/04/82 JOS teJteER 11409 3-50RT SENERAL ELECTRIC CATEGDRY I EQUIPIIENT WUN T11tE 14.14.43 n LILC3 00CHET 50-3tt ACTIVE 18535 QUALIFICATI0H LEVElt151 ITEttSt PAGE a l ttARM ' tGUIPtWMT St OLOS AVAII. QUAL. IRMt. TYPE SAFETY 4Unt, ItVISEll SESCRIPTION 140. VEtDell ELEV INSP REPT ttETH FRES ttitC FUNC. STATUS g 1MtleML-18 Wem 3MST WACM CM Mt1P010 St SC004 TES SAI-Ot90A80PA 95T S F ttS.CS S 1sttleptt-19 C098 SPWAY WM CM Mt1P019 St SC000 YES SAI-Ot90A80PA teT 11 F CS S 4 f3 3 1Htlertt-t1 NHW IMST WACM CM Mt1Pett St SC004 YES SAI-0290480PA lef 8 P HS.CS S 19ttlertL-It

  1. tCIWC Pt4F S WAC Mt1P0ft St

$0040 YES SAI-029QA00PA teT. 8 F M S 4 l} 3 Stetterte.-29 MAIM STM FLOM WM H21 Pets St SC040 YES SAI-0290A80PA 997 11 F M S t 1MilePIL-to WV LV & PRES ItM Mt1P024 St SC079 YES SAI-0290A80PA teT 11 F ttS.CS S lI 1settertL-30 SNM/IRM PRENF WM H21P030 St SC079 YES ORP A00-794-14 feT 4 F M S g ot 1stflertL-31 SetVIRM PRENF WM H21P031 St SC079 YES DRF A00-794-14 NBT 4 F M S { !3 10ttlertL-32 SetVIRM PREAfr WH Mt1P032 St SC079 YES DRF AOO-794-14 lef 4 F M S f 1sttlertL-33 SetVIWtt PRENF WM Mt1P033 St SC079 YES DRF A00-794-14 HDT 4 F M S q 1Hilert0,-34 HPCI LEAM Off WM H21P034 St SC008 YES SAI-0290A60PA teT 25 P M S i 1HttePtL-35 CS/plCIC LM DET I H21P035 St SC040 YES SAI-0290A80PA pet 11 F M S 3 IlltlertL-34 HPCI LEAN DET WH Mt1P034 St SC000 YES SAI.0290A80PA lef 11 F M S l r 1Itt ePtt-37 IICIC LEAN DET WM H21P037 SE SCOCS YES SAI-Ot9QA00PA teT IS F M S .) I 1HttePtt-30

  1. CIC LEAN DET ItM Mt1P010 St SC040 TES SAI-0290A8cPA teT 11 F

M S ( Itttisett-41 ING STEAM FLOH IN H21PO41 St SC040 YES SAI-029QA80PA pet 11 F M S q 1HttePtL-T3 ftSIV LEAMACE IIH Mt1P073 GE SC043 YES SAI-0290A80PA H8T 11 F M S 1HtlePtL-74 MSIV LEAMAGE WH Mt1P074 St SC043 YES SAI-0290A80PA 957 S F M S g CS ECONTROL BLOS P ePIPE HCtRtTED S8TsSINGLE FREQUttsCY QUALIFICATI0H HILEStottES WEVISIDH 4 -NOVEleEW 1982 _CS = COLD SitUT 0000t PC :PRIllART C0tif. SIAXIAL TESTIt1G A =REEVALUATIDH CotrLETE DA EDTilAllIC ANALYSIS PL PEDESTAL SC eSEcoff0 ART CoffT. 8 rREQUEST FOR REQUAL DR BID ISSUED NOTEt tiUl10ER IM F sFLOOR tt0UltiED QP zQUALIFIED BY /

  • LOCATED Ott C0tif.

C =S/H REC 0tttEll0ATI0tt TOLILCO ' TYPE HTilG' COLUtM IS j HS sit 0T STAlf00Y PIPittG AffALYSIS HALL 0 rGUAL 00C PECEIVED QUAf4TITY OF ITEHS. 11ST ltVLTI-Fpt0VEllCY pH PA0 HASTE T ellAlte STH. ftJiriEL E ritopot: ape It001FICATION REQ'O BIAXIAL TESitt10 SA = STATIC AtlALYSIS M allEITIttR CS OR HS F squAL DOC APVD 4 FILEO h itSTalIUL T I-F R E QUEllCY SAf rSIttGLE FREQUEllCT Z PASSIVE ITEtt G eSQRT PAPER C0irLETE h SIllGLE ARIAL TESTIffG SIllGl.E AXIAL TESTIIIO (SQRT PAPER f40T H aCOPIES OT 00C 10 OISTRIBUTION I REQ'D5 Y 4 P

1 c CS OF 07 01 62 f SHeptMart ItJCLtedt POMtt STATION SHORCMAM CAft00RT I EQUIFittNT CHAtIG! RECORO CURRttff DATE 11 13 82 Sfotit AtID ktnSTER tt#GIttttRIteG CCRPORATION l t EFFECT OM [ 90Ct#tttff 8 DATE OF ISSUt EQUIP. EFFECTED NATURE OF CttAff5E SEI5? TIC QUAL. F."tt15 99 00-02 1Htlertt. 040 ADDITIONAL RELATS TO DE ADCED TO CAT.1 ItASS CF ADOCO PAtttL REL ATS tit 0LIGIOtt HOMt r F49926J 99-09 82 1011ertt. 021 ATTACittttfliS TO SHIO / RAD. It0HITOR. STS. ItASS CF ATTACIGttttTS { tt[CLIGIOLE-t:OttE i i P.3930ft 99-27-02 1tttleRM 40.41 CLEARAtlCE PRCO. FOR 02 DOTTLE RACMS tt00!FICATIO!I IttCCCPORAf t0 4 It110 CALC'JLAT3CfI.ttotit t F4 tetS 09 30 82 1Z97pPit.ERI.4 ADDITIOHAL SUPPORT FOR tt00ULE CASES TO A00C0 ftASS OF LUISTRUT l'- CCitr0Rf1 HITit TEST tt0UtfTIllG CotCIT10ftS. FPAt!E I41LL STIFFr!I PArttL { }, I CAT. 1 PAfttL .itClit C F.3939L 10 05-62 ItttleRM 40.41 SUPPORT OF 'HARAtlITE I' FIRE BARRIER SitALL PLATES ADDCD TO FRAHE .t#0 IttPACT TO QUALIFICATI0tt h

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D > 's (D et F.194818 10-07-02 1RZ9eHCC.1119 ATTACH!ttflT OF 1* DIAffETER CCtCUIT MASS OF SODED C0tIDUlf .h'( :, ifECLIGIDLE. f40!st oo F.43145 10 26-82 174TeUC.174.8 NOZZLE SUPPORT FOR UNIT COOLER APPROVE 0 Of CALCULATION N et 19 3 F.3945tt 11 09-82 1011erf t..tl.tt la DIAttETER C0tIDUIT ATTACitttttF TO FLEX C0tIDUIT USED Ctl B tt

i CAT. I PAtlELS ALL COttitCT10ttS-t40!IE

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  • I F-294004 IN PROGRESS 1P50ePS-1134 It4STW. STAtiD ATTACitt0 TO STRUCT1JRAL PLATFORtt ePS-1130

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Attiachment 4 'Sp2cific Item No. 1 STONE & WEBSTER ENG'NEERING CORPORATION $ ~/// - A 7 5 -. CALCULATION

SUMMARY

c,,,,,,, y,, or'/. //6co. c 2 - 33 /. / - C E:C C i ..meu l' O A CATEGORT / CODE CL ASS CLIEwt / PROJ ECT Lit ce / :nos Citm chit,- / / l SUSJECT / TITLE / 6GfL.WC fice/ cP }/op:,'4G /d Unit Co*l.4ft T /T'/4.x uc cat 4, B; oh. A, 8 fo rt. 'Qf:1~ sitsoir~ Ah 2 R*' A / ^! G C, Ertr<. B, / C9JECTIVE OF C A L CI, L Aflo ts ~io~v~{ o/:TC c n'vC oF Tr/i: Cie.r-v s. A ricoV 1: -rs cAc c s A.A rc yw'c bEPLCC r tod of T*H C L),vir-Censlaos. Ibu:iaQ b u l r *.:;" C i :.s.i c A cc.C LC An'o a/:. CALCULATION M ETH O D /A SSU M P flC N S /~i em ST,4ssbit,e b EA'C;WCirc-.vS *TTCT2* o ie - L f/ w s c A u v u.e rto a : t A /_' C usso 70 BCn~ot.m:^!C TWrk>usik6 bCFede-rtant, 2. Csesc4* T;ts4' Ho v:isvr HAs A V Ct-n't.+ 1. o ot./ E ov rotrto.v!, 0^f:.y THC s b CrLCc.rton f/ec,~ f.A rcrEm scism;e, sccgg,gg,+7;o,vc o c centrisex.ct, SOURCES OF D ATA / EQUATIONS t. 6vfrs i-o AaGC Sas~c A'9*': kk" ' * * ' ' " " ' ~ ' " * " " /,l71 fM / 0F /-C/%os7 97L-36 39 L d-goy->*)~)7/ sr-b. t'. S +- W b 6, +/o. / /fo 00. o 2. - /0. G si - </1. /3 3, _/ cca sute: of M+7C'.~A L.: ~TTau osucaku ms Gca.g 1972./ Patt it s/ ) j j

  • . J '1 2.

p Conclusions (g( tt.Cru s rx of 7~H-f cat.c.u w og spow 7W4~ p ;~; % cryees c f 4 o f so'I;s.t. ry/ d" Ho ss * *'at 6 f.s l I l REVIEwE R (S) COM M E NTS PREPARER DATE st. if o'!c ci. w ic,he j,r REVIE wt R /CM ECR ER D ATE f/ 5'lY l Q fl.. //A dd oe th0EPENDENT aEvitWER DATE AlL' # /? C@,* d t.0 [* A w%MN f M.

. ~ _ STONE P CEBSTER ENGINEECING CORPORATION CALCULATION SHEET A WO GS CALCULATION IDENT!rlCATION NUMBER o J.O. O R W.O. N O. OlVISION D GROUP CALCUL ATION NO. OPTIONAL TASK CODE PAGE C 11 b Y.O 2 N MI5 ) .333 -/ C 2 C-a i 3 / J :)!.C C E.Y E,V r p r yp,E FA t/ H W.$ / */Q 8 u pl l.*?! Af d 3 E IS ?v' ' C E V Et " i a ? $ 22.!W _ a wsw Re y, j, z L to so 0 si u y "1 F L (,4 I er e or ru s _k h3 .1 n 'S C ii 0 l i Dt SC h 1 i/ M it, f s se j gf) ( g c d / /, / Yl 'C) to i t c. w L at as l *U' / N g 9 M N lN ~ Q S l' 24 I h_ \\.1 i as id" 27 i I I se D'i' L A C E V 5 8/T sue \\ 70 sEFLECTI.>r/ Cr ( N MONE :UPPO.2T. DISC. 33 ) 34 i H ous,C sS 36 Dr$P L9 d E u2NT 3, DUE TO.5.uA.=r !Evarrif se 3, 4o 44 42 43 44 45 46 - -. - ~ ~. -... -. -

'3 STONE G CEBSTER ENGINEERING CORPORATION CALCULATION SHEET s wa m CALCUL ATION IDENTIFICATION NUMBER J.O. O R W.O. NO. OlVISION 0 GROUP CALCUL ATION NO. OPTIONAL TASK CODE PAGE E ^ IIGO M 2 NMis) 33I-I C 2. c I 2 + 3 JDIS P:. 9CE M ENT 0= HMS!']G S is.oe e-9.94 P ~ ~ VI: v],< G < ?. 2E : I p N 425x I,2 x l. P5= SS o 'o R ' V \\ p;' L F '// 4 5 R E W - T 0 ;~ % vi E ~ P> l. l 4e, D c: ~5 P s y (: 9-j.5 5 :~ y :- jg '4 y% is g - HOR;avrac. d s ;1" t y' ACCELE2.W:Orl =CR 352 (RSP. I, Pn RT I, pg 6,2) to .Drset s ceme u r sus rc now:er M, a ~ S .I Y 0*lb5 ?i * = ,3., Pd M. w' < ( 13. 09 - f.u u) AC= A5 } ?' 22.1875 2 2, ig 75-n 30 A.: 2rrE t.= 277 Y ll. 099 A O. Ib 44 = II. 'I6 id 32 E = 2 9x 10 ' n r ; r= +n 2'- 0. iso 4 x - < n. 02 ?.= iv " 34 o uu hxbd d, x ( B. 09 - ?. u h< 9. L/ U y 5 n z z.ip%

  • Jt,yg*Z?t/O'x 22.1275 D

37 30 D t SPLpc2 MENT Bue ro POR c E Vf : 40 1 ,Q23

  1. ~, x 3. u u 2-1 42 s~.

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......... : ~ a. :....... a STONE & CEBSTER ENGINEERING CORPODATION

  • rJ.-

CALCULATION SHEET asco es CALCULATION IDENTIFICATION NUMBER J.O. O R W.O. NO. DIVISION & GROUP CALCUL ATION NO. l OPTIONAL TASK CODE PAGE If 600. 9 2 NM(y ) 33 l-( l CEC i & P6 ~ di e QA ~ 4 + W Hr= R.S [g - F9RM Fhc~~0 2-F% A Tliit/ 7 u.3 L%% R S ECT.' S//, hs = Ej h&P N 40 i. f0% THE SHEh DE Flee,9</ AS'umE Terra c>~'/CEN 2,2 53 Lpp 1// I ,3 ACTitJA AT THF J)lSThWCE S.H'l F ? St^ WE.Su?=?R' J= ~'5 ES HOUSING-ir G ~6HER12 HODULus OF ELN Tic /TJI: G = 3= 5 = lS f?I.? '..s. is 4xS$by$49 -5 c[3 * ~ 0* I f 19 = en /y,5xl.9' xI/36 23 Tb""L h t.s o L A C 5 MENT 0.C THE 4 9"'S144; es 4=[/+[+[=/,2x/v'g ~$ , / < ') # f a 8 v/O I s. Q = f x lO *' s. 30 Tas p u msgi.e c tan gnacs esrwerv wmssL ec 32 0.03)" R E.=, I # ( X P l; ll H CUS t.'I C. 34 35 34 3, 38 3. 40 4t 42 43 44 45 46 -~-.~.y-..-

w.- .>/* / Specific Item No. 2 ~~ APPENDIX E

13. 2. b>

_DESCRIPTICN AND VER!?ICATION OF THE NON-LINEAR IMPACT ANALYSIS E.1 OBJECTIVE AND OVERVIEW The purpose of this appendix is to describe and provide verificati for a special purpose computer program (called RACKOE*) on developed primarily to analyze fuel rack behavior resulting from seismic dis turb..s c es. The fuel is considered to rest in the rack at its center with a simple support (hinge) between the two. With the seismic disturbance, the clearances between the fuel and the box walls lead to impacts thus making the analysis a non-linear one. The space between the fuel and the rack wall is filled with water so that as the fuel and the box wall move relative to each other, hydrodynamic forces are set up due to the acceleration of the water These forces are exerted on the fuel and rack structure Methods described by Fritz (E1) and Dong (E2) are used to determine these hydrodynamic forces. Certain special features or options of RACKOE are discussed in attachments to this appendix. For example, calculation of the structural damping matrix is described in Attachment E-1. Friction with sliding behavior is another such option for fuel racks that are not tied-down to the ground (i.e. pool floor) or for fuel that is k allowed some translation within the confines of the box valls. formalism used allows RACKOE to treat multi-stick models witho The loss of generality. p The input preparation for the connection matrix, however, is more complicated for these models, so these multi-stick todels deserve special attention in the attachments The plastic olement option is also described separately. l The following sections describe the basic feature of RACKOE The input to the mcdel is an acceleration time history having i l points nt typical time intervals of 0.01 sec. The displacement and velocity n uRACKOE is an acronym for rack analys s considerin e non-linea- #4a4 *e element program developed for Wachter Associates g kinetics of eartncuakes, Prof. W. F. Stokey of Carnegie-Mellon University, Pittsburgh

- ~- -- .~.------:- 2. i of the ground are found by integrating the acceleration curve twice, however, these two quantities are not needed for the determination of i A verification of the basic the structural forces and displacements. p one-stick fuel model with fluid coupling and fuel to rack clearances with contact springs is given. This verification consists of a comparison between ANSYS (Ref. E3) and RACKOE results using identical models and input. b E.2 MODEL DESCRIPTION For the sake of discussion, the 8 mass model used for ANSYS verification is described as an example. This model is illustrated in Figure E-1. The numbered and circled masses Q typically represent the following: Parts Mass No. 1/7 rack mass, 1/7 fuel mass, base mass ~ 1 2/7 rack mass 2-4 5-7 2/7 fuel mass rotary inertia of the fuel 8 Some fluid or entrained water mass may be included in these masses, but here they are considered to be included in the hydrodynamic mass The terms in this fluid mass matrix will be outlined assuming I matrix. the above masses are " dry" masses. The numbered and lettered squares in Fig. E-1 refer to flexible elements. The CTAC formulation is used to find the stiffness matrix for the ~ numbered elements. ~ L. Flexibility Representation r-Bending and shear flexibility of the rack l-3 Bending and shear flexibility of the fuel 4-6 Local flexibility of the rack and fuel a-f elements where they meet. No forces are exerted on these ". springs" until the relative displacements of the masses ' exceeds the clearance distances. 7-9 Local support flexibilities E.3 THEORY The governing equations will be written explicitly for a two mass system and then extended to a general multi-mass system in matrix form: .m <e.e.mm, w - etw a w ww * *< " M W eE** ^ HW '** -m.- w- -. - 3,, e ,,-..-e. -*a e--- aee-m

.-... -..-..:.--..-. ~ - - -- ~ ~ '3. "Z -C i -C 5 "l*1 "~ Nil *l-k12*2 + F,1 + Fyyy+F12*2 + Fyy yy y y2 2 (E-1) x m *2 =-k21*l-k22*2 + Fs2 + I21*1 + F22*2 + F <21*1<22 2 (. E-2) 2 w2 1 1 where y = mass i m y = displacement of mass i x -kg3= the force exerted by the structure on mass i due to a unit displacement of mass j g3= hydrodynamic force exerted on mass i due to a F unit acceleration of mass j, described e.g. in Fritz (loc. cit. ). (F usually negative, others gg positive.) Fyy= fluid force extened on mass i due to a und acceleration of the wall. 1 -C;.3= damping force exerted by the structure on mass i due to a unit velocity of mass j. F,1= force exerted on mass i by the gap spring l 2 = ground displacement l In matrix form equations (E-1) and (E-2) are "l~I -F -kyy-k12 [*1\\ ksi F,1 -C -C ~ ll 12 yy l2 1 t.. = q K+J ?+ 4 (E-2) + 22

  • 2

-k -k

  • 2

. s2 [F,2 F -C21 -C22

  • 2

~ -F21 "2-F I 21 22 em -.7

.,l...... - - - ~. - - 4. Solving for the accelerations yields: X m -F -F K K E y yy 12 yy 12 l s1 wl 11 12 1 [ h+ . 5+ [(E-4) ~ = ( ,*21 22, X)j fs2] F -F w2 , 21 22, 2h 2) 21 "2-F E C C 22 j For a multi-mass system, the matrix form of this equation can be written as: I fX =(M-F)1((-K)fX - (C $C (E-5) F, + + F, 2 j s i f ) represents a column matrix with N entries, N being the where } number of masses, and ( ) represents an N x N square (and in these cases) [ symmetric matrix. Inthefluidcouplingmatrix(-Fg3), there are two effects considered; (1) fluid coupling between the fuel and the rack walls, and (2) coupling between the rack walls and the pool walls. In general, the fluid coupling matrix may be full; however, it is reasonable to assume that only the pairs (2,5), (3,6), and (4,7), in the example given, will have non-zero off-diagonal entries. Following the guidelines laid down by Fritz (Ref. El) and assuming that the pool walls move with the pool floor, the terms in the fluid mass matrix will be as follows: 1/7(M + Mont ) -F = yy H 22 = 2/7f M f Mf + M[) -F + H + F F

F 22

33 44 (E-6) Mf ) F25 = 2/7 + F25 = FS2 = F36 = F63 = F47 = F74 ) SS = 2/7 F

  1. 55 =

F66 = F77 m e =% =a go e. s eus F g.*e to P 9 '*4N"#-b

. ~.. _..... _ - - m. _m.._-_-_..__.._ 5.- where rw is the total rack to wall hydrodynamic mass ~ M is the total rack to fuel hydrodynamic mass H is the water mass displaced by the fuel is the water mass contained within the rack in the absence 4 of the fuel (includes water or poison box water) Mont is the mass of the water entrained within the (inside boundaries of the) rack and the (outside boundaries of the) fuel (=d-Mf). The remaining fluid effects in F, are ( F,1 = 1/7 +

  1. w2 = Fw3 = F,4 = 2Fwl (E-7)

Fw5 " w6 = F,7 = C M[ is the mass of water displaced by (the outside boundaries of) where the rack. Since the racks contain flow holes for coolant, no hydrodynamic mass effects are considered for mass 8. Expressions for M= are 9iven in Appendix C for horizontal and vertical H f j fluid flow. For MH, Dong (Ref. E2) recommends the "added mass" approach, Mf = C,Mf, where C, is of order unity for uncanned fuel assemblies. For the example considered, C, was chosen to be 2.75. For typical LWR fuel with pitch to diameter ratios - 1.3, a lower bound on C,of 1.5 would be a reasonable estimate. With the close proximity of the box walls, the assumed value is probably more reasonable. For channeled fuel assemblies, C,would be quite high. In the limit C,

  • oo, the rack and fuel will move together and the analysis can be shown to degenerate into a linear one.

E.4 METHOD OF SOLUTION In the program RT.CKOE, equation (E-5) is solved in the following manner: i I ~ ...-...nn.... - - ~ ~. ~ ~ ~ _

1 6. Using displacements and velocities from the n* time step, i (Determination of the C matrix 1. Ex and Ci are determined. is discussed in Attachment E-1.) The spring forces F, are calculated for each clearance by first finding the difference between the deflections of the 2. If the difference is less than this masses involved. Otherwise a non-zero K( Ax) clearance, the force is zero. is calculated for F

  • s These three structural forces are added together and

~* premultiplied by the inverted mass-fluid matrix IM - F] 3. The constant vector [M - F]~ {F,) is multiplied by the 4. input (or interpolated) ground acceleration and added,to the previous result. The absolute accelerations k are now known for each mass mi. n Although written in terms of the absolute displacements and 5. only require velocities, the terms Kx and CA (and also Fs)and velocities (y = i - z) relative displacements (y = x - z) The relative accelerations are found by subtracting the ground acceleration I Z Yn"Xn n ~ The relative velocities are then updated n+1"Y + IY ) ( At) n n L and these are used to find the relative displacements I + I n+1) ( At) n+1*Y Y n I The calculational time step At is chosen small enough that ~ x and its derivatives change very little over the interval. to At/2 (for example); Accuracy can be checked by changing At ' d typically, a calculational time step 0.1 times the input groun acceleration time interval is sufficient for one-stick models. i Thus, with ground accelerations specified every 0.01 sec, a calculational time step of 0.001 see is usually sufficient. for multi-stick 91 However, smaller time steps are often necessa: e.-- ,,m mt.e - .--ms.,w em ,y s w &-^ *^*~.?- ,- ~ -..,

~ ^ - -... - ~ -.... -... .... -. ~ 7.- models. It sho'uld be noted that using the updated velocity to find the displacement (instead of the velocity from the previcus time interval) improves the numerical stability. 6. Steps 1 through 5 are now repeated using the velocities, displacements, and ground accelerations for the n+1* time step. E.5 VERIFICATION Figure E-1 shows the model used for checking RACKOE against the more general structural analysis program ANSYS (Ref. E3). To verify the essential feature of RACKOE everything except structural damping in eq. (E-5), ANSYS was run only until and slightly after a fuel contact occurred. As input, both programs used the input ground acceleration shown in Fig. E-2. For completeness, the absolute ground displacement is shown. In addition to the input ground acceleration, the following summarizes the relavent input data: My= 12,714 lbs. M2= M = M = 3,689 h s. 3 4 M5" "6 "7 and 2 2 29,866,000 lb *m g,3gc3 represents the m1 M = 8 rotary inertia of the fuel.) There were six gaps (3 to the left of the fuel, 3 to the right of the fuel), each with 0.3 inch initial clearance. Each gap spring is assumed to have a stiffness K, = + + +.+ =Kg = 2.31 x 10 lb/in. ~ (For the problem modeled, this stiffness would be representative 1y hight a good check on numerical stability probably results by assuming a stiff value here since a short duration fuel impact would be implied.) The non-zero fluid effect matrix terms were as follows: -Fyy = 12,879 lbs. I " 38,121 lbs. = -F -r22 = -F33 44 = -F5 5 = -F66 = -F77 = 4,804 h s. F25 = F52 = F36 = F = 6,560 lbs. 63" 47" 74 *~ , e ,y g, q e,- ...e. nee e- -'-memp, e p is m e gayie4%' , _, = -_---.,-_g. -g-,._7 ._g

-w. ~..... I g, and for the wall coupling terms, 17,392 lbs. F,y = Fw2 = F,3 = F,4 = 34,784 lbs. The support springs were specified by 6 K8= K = 5.0 x 10 W in i 9 for the vertical ones, spaced 30 and ?O i.9ches, respectively, from the center of the rack. For the horizontal spring 0 2.041 x 10 lb/in. K = 7 The flexible elements 1 thru 6 are " beams" with shear and bending degrees of freedom, specified by E (Young's modulus), I (section inertia), G (shear modulus), A, (shear area), and J. (length). For each element, the values E = 27.76 x 10' psi, G = E/2.6, and A = 48.3 inches were assumed. Rack elements 1 thru 3 were taken to have A, = 176.6 in' and I = 117,351 in'. For fuel elements 4 thru 6, A, = 278.6 in* and I = 2 7 in +. (Realistically, E = 13 x 10' psi should be assumed for aircaloy, but EI as chosen corresponds to a fuel bundle natural frequency estimate of 3 cps.) Additionally, a shear factor (of 1.0) I is specified for all elements. u r Input ground accelerations were given every 0.01 sec and the RACKOE L calculational time step was 0.001 sec. The equivalent ANSYS time step used was

0. 0025 sec. (NITTER = 4).

Apart from this difference, input preparation was essentially identical. Figures E-3 thru E-6 illustrate the significant results of the comparison runs. Fig. E-3 shows the fuel (top and middle) displacements relative to ground. Since the ground displacement is initially positive, the displacements are negative. The top of the fuel contacts at 0.44 see and remains in contact for approximately 0.01 sec. As top contact occurs, the middle fuel mass slows down. As shown in Fig. E-4, the top of the rack moves very little until the e.. ..m.,-.w..-- - - + - +

. :.. a. _.- \\ 9. e 1 l impact occurs. The peak displacement predicted by ANSYS is slightly less than that predicted by RACKOE. This discrepancy is probably explained by RACKOE'S finer time step. The horizontal shear force at the bottom of the rack (proportional to the displacsiment) is shown in Fig. E-5. Note the small positive pulse at contact followed by a larger negative pulae due to fuel rebound. Again RACKOE picked-up the extreme not resolved by the longer time-step used in ANSYS. Finally, Fig. E-6 details the vertical support forces (or base moment). Again a contact-rebound effect is evident. Based on the RACKOE results, the peak horizontal force occurs 0.015 see before the peak vertical force. Considering the detailed agreement between ANSYS and RACKOE in this ~ comparison run, the basic one stick fuel impact model is considered verified. Various options of RACKOE are discussed and justified in attachments to this appendix. ~ 9 Der k e m ( e a m -.- =

  • m e'e-e a s.._

-. -. ~. - - - -.... -... 10. / / i k. v4 Li Mu ew 13M M '/ (3 b (ro) N3) e a ? g g 9 e-h@ (5) ~ / / I O O El 4 / L / m f G D A I A L e a v-J // /r rr r/ -r r l =6 Fig. E-1 RACKOE Model used for ANSYS Comparison l j 9 an =p.m g...ww . w -; es e

  • s-e e-+=

= =y 3,.ww,...,,mayw

,,_...._._1---.=-"*^-- eh...g'eM', e 11. P Q W D O --.-- C.. _ :- ~~--- - i " ;~ii'- F J - - - _-_ :;, ; _ c;. =. _ _ -~ ~ - ..,...y.e w..12 p czet.LeWW. 9%D C2p u .,,.. _... = * - * = - - - - - -. -. = - - * * * * ' " ",. ..s Q ..e. e-7- _ _g -- ..,_g_ g g;. .44;_ -E g. O h _-f----~ H~ :- - - _-.. F ; _ _. :#, - -: s..___-.-. - w -- - - --.: g - * --S.__,_, n -f - __w -e ~ r p y __p M

  • f.--

C ~ fg..M.w-**- e4 [ g. f.f3 s. a -o- --- g - Ez' m 'N _ --}-- } e b -g -s 1 o u r. -\\- -n -A "M u e-- 1 e-1 1 a W -g- .1 p E \\,

    • '4 s

ei.e ~~ - \\ P-x- E 1 ~ h-A~ g u 4 ^ ^ ~ _ Q x. m w_- x m __ g r- - _gr O O, ^-

e m

_ ~ _ y 1 m Cf. m 'O h M- -A_-m C., L. xw- - o { _ w_.. _ y g \\ -s g m ~.N ..M._- A '__---=- m,. C ( o N s ,,4 O P W Was 9 N ." = - g .*---o--'* - ' ' " * * 'e ^ .,C h-.=__- p ..se_- N L O2, _ _- - - r

------*._._..gs._

.ms;

s...u. s,. s. -

~.,.- T- -- _. -_.4__---,---_---,.-.....---- b I 1 I e. mme e.WM* * - *

..._ _...-......- -... ~.. e / 12. f \\ _n .-.:... i. _ n.. s 2-j.n.:.:=. =. f ut %ene.4 m 3 t [. 4.. 7:..=... .2.7:1 .;J.9 Fuel f*m ea h ' g 1~*1 " ~ I- - ?_:. :.4. t. * : a 7 "'S S ~~~-N!*"-l?' d@:C ~_ f.* - k- ~ [ IN-55 J- , _ ;, yy.p--- ._.._.....g.. y ~.g..-

. _ : a._. :[...

. ~; ? - * - 4 -- - - ; :.:=.... n.,=. 4::.g pg4 na3 g.,: t. *... : : u - ::-::-)l, \\ Q -* = ;. .:- :r = ~: \\ .u.-- (- ~2~~b*~h~~ ' se ~_~ bhPug1 C) N:E'M f kh!.W W n .= f:-:

.bi=4_[

_~'i

h::=~&.
5_- Q

' Q:.35f.t:;- i- ~ _ =. W4 ww/ e 9%:?.t _" _g = ! _=;.. i=.=.=l A -n; A..:= 81 i-a 'c0 i J=-h==~=f-7= =#/ M2isfi'

:- c..

s 3- ~~- .A -emen u=xce+=y-a m:a =w =: 1-::(r q

==- + ..=.;--.1 d ^ -i... . _;. : _. ; i ~~ [.:** -.,.*. 2 "-*.. ~ =.: ; 17.- --J.-'=- -~. :* L: : ) T.! 1 . :.T ! '. --*. .. 1== ". 3. = J.~.L.:

'
=,=..

3

=.: - a...-.:-. :: =:. = - -.: :. :-T I.t
C.. ;% :.

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=.u

=. _.-.===a=.=------_------: - / =:. J. =.--- - - -- - - - =.=. -- -c -a- . = _ _ _ _ _- - - =---

---o
= :-

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5 =

EEiU ,i _= 2 _.f _

== a_._ _.. _-- 1 =_E:.- _ _ _, = = =., _ = _ _ _. _.. - _ _ _.. r = :w . = ~ ~. ~-.-_=.=_= _. _ _ --- --._.-_._..._.=_..-.:=.:....._.c.._.=.__.=.=_ ..J... = ...a

j. =.. -

.=.a..:-.-L=-....

====: = = : - =.n = = 6 5.. =- - _-- -..-..-_.._.-=:- --=.--- -. _. _ _.=.-._._=.._.=_.-=-.==.----_.-.,_._-.__/:.f...v.i.--- = = _ -...

...j

=--c L=:;g ~ _.. ___. _l--V.. _.. _a====---=.=--= ~~_._-.2.---=:=__=_:=====.-,=.: =_ : e ...t r. p -OdC

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-===----

=:u _ s.;, _ _=._=._-_..==._-_--==_-=..-^l/==_--.:,.._____, =.m

-----_=--

- - -. = = = -. q=. Q,- _-. - -i_-- - = _ _ :-- :=--- / f -- - = - - - - - - - - - =

==c -- 2 L _._--t#==._-.---- ..:=.c---- _ : --=:- - --- _=- r : :q.--- - = _ 2._._._. _--- = . _ _ _ _ _ _ - - _.. _ _ -. = _ _.. _.. _ _ _ _ _ - . - _. =. _ _ --_._ _. _ _ _ --- ____ __ _.=. _..e

=.,_..__.

=.:.e -=--m-;-------=- .:._:__.:-=.----_ ____.:.= =: w ._=.=.~_;_==-::=---------1

= m -- - - - - - - - _ _ =. = = = - -.

..._.-_.=__-r==::=- t_ _ _ __ /. r = - -.=- ;-- =

==a -- ; - -. _. = =

== m ?. ".-"".",.Se ---__=_--.!.=*--d.......=:.-.--- - N. r.:._. ;_ = ~.J...=- 3 4 C =. ..J".-' = -"* r- - - = = = f: < =::.: := = : _..== =.===-=:==.===_.=_.=.-- 3 .=====:=__ -= = _.

.=----. =. - - - -
-== -

=.- ? =.. _:= : _==_

= =:= :

==.==_._._-=-_.=____:===._==:-- =---.=:.._.

= =..: __ : - -.=~.---:=---.--__.--.=

f T=5=_=21-~-^= f^_.g.=.

=- _=C==Q

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.=2*.*--L="-~_.:-'~ --*----.;=.- --.-v._._....._=.-=-:.-:.,.. - - = = - = - Fig. E-3 Comparison of Fuel Motions Predicted by ANSYS and RACKOE. The initial fuel to box wall gap = 0.2 inch. O - e e-e -e ew=g=--*w.g**.

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_ seconds --- -.._G -.:... = : =:r v-a ..=_._._;;:.=.... Fig. E-4 Displaccinent of the Top of the Fucl Rack as Predicted by ANSYS and RACKOE. l t .w..- .._e -.em. ._e w ...y..ygi.

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. t... ,a.- - _.i_.,_. 6. r.. Fig. E-6 Ccur.parison of ANSYS and RACKCE for Vertical Support Forces and Base Moments e

e . ~. 16. E.6 REFERENCES El. Fritz, R. J., "The Effects of Liquids on the Dynamic Motions of Immersed Solids," ASME Trans., Journal of Engineering for Industry, February 1972, p. 167. E2. Dong, R. G., " Effective Mass and Damping of Submerged Structures," UCRL-52342, L.L.L., April 1978. E3. ANSYS Runs and Restarts a. AQEUQSR - main run containing time history accelerations and model input data. Output includes l. UX11, UYll " corner of rack" displacements 2. UX6 " middle of fuel" displacement 3. UX7 " top of fuel" displacement 4. UX4 " top of rack" displacement ' ~ 5. UX12 " ground" displacement b. AQEVC4R - element forces on bottom elements of fuel and rack ~ c. AQERLEF - element stiffness matricles d. AQE3N43 e 1. UX1 thru 4 " rack" displacements 2. UY1 and 14 bottom of rack and fuel (no relative vert. motion) These runs were made possible by P. H. Titus of Stone and Webster 8" Engineering Corporation, Boston (noted 1/7/80 and 1/9/80). Wachter N Associates acknowledges Stone and Webster's disclaimer stated in their March 24, 1980 letter (LIL-R-231 - transmitting AQEUQSR and AQEVC4R) and L restated in their August 3,1981 letter (LIL-R-269 - transmitting microfiche for all ANSYS runs and post-process runs listed above). e, Sus I ei. hee t

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w'e GEN ER AL h E!ECTRIC 22As416 so. ~3. 2 NUCLEAR ENEf4GTUlVIS10N nev. 0 STRESS REPORT If!TEP. FACE Atl3 EQUIPME!!T LOADS MAlfiSTEA!! Pl.*!!i3 VOLUME 6 SHOREHNi *;L*; LEAR PONE _R PLAti! L.I, 12. M79 one PREPARED SY: , 44, A5'hi.4LEKAR, P.6. I A! ICE BY: / f.T tiiEHyP.E. VE'liFIED BY: /?44 H stERZOG () f 70)(n6:95C.i. Acting Manager APPRCMD SY: o.c ^ Piping Stress Analysis 80lLI1G ~4ATER REACTOR SYSTEM.S E!;Gl:lEERI:iG DUAR!:JE!;T MECHAfi! CAL EQUIP:'E IT DESIG!! SECTI'0:1 PIPIT;3 CESIG:4 SUSSECTIO:1 l ..? (

......=~ ~- s-.~u-~~s GENERAL @2'il E.LE CT R I C 221,s416 see. 3 NUCt. EAR ENERGY DIVislON u v. 0 TABLE OF CONTENTS Subject Sheet. Nurber_ 1. Introduction 5 2. Sumary 5 3. Descriptien of the System 5 4. Coordinates. ETement, and flode Diagram 6 5 Structural and Pressure Vessel Interface 6 6. Safety Relief Valve (SRV) Equipment Interface 6,

7. ~ Main 5 teen Isolation Valve Eculpment 'nterface 6

8. HPCI !solatiert Valve Equipment Interface 6 9. Suspension and Structural Attacheents 6

10. Pipe Branch Connection In'erface 7

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11. Terminology for Load Designation 7
12. References 8

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G E N E R A L h. E LE CTRIC 27A5416 sa ao. 4 NtlCLEAR ENERGY DIV1slON nev. 0 APDittDICES Sheet !!urber_ A. " Element and Node Diagrams 9 4 Reactor Pressure Vessel Interface 18 C. Safe:ty Relief Valve (SRV) Eqaip.ent !.iterface 36 D. Main Stem Isulation Valve Equiptent Interface 142 E. P.PCI Isolation Valve'Equipmer.t Interf ace 211 F. Suspensicn and Structural Attachments 218 G. Pige Branch Connectie interface 734 4 e e 4 s e e 6 9 e \\= 5 s

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10. P!,PO BFANCH CONNECT! 1 INTEliFACE (APPENDIX G) 50.1 Therm 11 expansion deflections at drain lines and for elbcx taas are givan in this avendix. No tynanic inforr:stion is provided for drains and elbow taps, as it is assu' red the piping is sufficiently supported at the.e points to limit the dyrramic loads applied at the branch cennections.
11. TERMINOLOGY F0F. LOAD DES! GNAT 10N 11.1 The folicwim) designation is used in all appendices to describe the types of loads.

Annulus Pressurizatio'n Loads (inertia Ef'fect)' AP = g Annulus Pressurizatio'n Loads (Anchor DNplac'eceit Loads) AP = O CHUG; Chugging Load (!nertia Effect) = Chugging Load (Anchor Displacemer.t Loads) CHUG = D COND; Condensation Oscillation (Inertia Effect) = COND Condensation Oscillation (Anchor Displacercnt loads) -= D Operating Basis Earthquake (Inertia Effect) OBE = g Operating Basis Earthquake (Anchor Displacectnt loads) OBE = D P Operating Pressure = O P Design Pmssure = D P Peak Pressure = p Safety Relief Valve Opening Loads (Acoustic Wave) RV1 = RV2 D' = Safety Relief Valve Basecat Acceleratic.) Loads (Inertia Effect) g afety ReMef Vahe Basemat Acceleration Lo'.ds (Anchor Diviacement RV2 = D Loads) D RV2 g Safety Relief Valve Basemat Acceleration Duc to,%tornatic Capressort- = zation System *(ADS) Vaive (Inertia Effect) ADS RV2 Safety 8telief Valve. Basemat Acceleration Due to Automatic Cepressuri- = g zation System (ADS) (Anchor Displacerent Loads) D 4 \\. ,. - l

GEN E.9 AL h ELECTHIC 22A6416 sw.s.o. 8 NUC1.E AR ENERGY DIVtslON nev. 0 11,1 (Conti..aed) Safe Shutdown Earthquake (Inertia Effect) SSE = g SafeShutdownEarthquake(AnchorDisplacementLoadg) SSE = D Themal Expansion TE = Turbine Stop Valve Closure Loads TSVC = Vent Line Clearing Loads (Inertia Effect) VLC = g Vent Lir.e Clearing Loads (Anchor Displacement Loads) VLC = D W Dead Weight = 11.2 For piping analysis ar. orthogonal coordinate system is used. This system consists of primary and auxiliary subsystems as follows: a. The primary coordinate systen (global) identifies "X", "Y" and "Z" oi:ections 42 showr. on the stress analysis diagrams where: "X"' is horizontal, positive in the 0* direction ")"' is vertical (also called " elevation"). positive is up from the reactor pressure vessel invert. "Z" is horizontal, positive in the 90' direction Moments about above axes are positive in the directions shown. -[ b. The auxiliary :cerd:nate system (normalized) identifies "A", "B" and "C" directier.s at nozzles as sncen on the stress analysis diagrams. "A" is always ax'al along the direction of a pipe run. Where the nozzle is horizontal on inclines, the dircction of the "B" axis lies in the planc containing the "Y" axis such that the pejEction on the "Y" 8xi' is positive. Uhere the no:Zie is vertical, the directicr. of the "A" axis is p.rallel to the "Y" axis and the "B" axis is set parallel to the "Z" axis.

12. REFERENCES 12.1 See Volut.e 1. Section 5 for all referer.ces cited.

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$5' e t s t-TABLr Di PIPE MOUNTED EQUIPftCNT - MS!Y ll!GIIEST LOAD / STRESS Stir?ARY RAII0 G6VERNING('I') IbENTIFICATIONOF .m ~ ~ lC SEisVICE ITEf1 CALCULATED ALLOWABLE [ACTt!AL)GENERIC LOAD EQUIPf!ENT WITH LEVEL EVALUATED VALUES VALUE (ALLO'J/ C0f tB I!:ATION ll!G11EST VALUES m e m D Axial 6.111 psi 0.455 1 Inner MSIV Inlet P S 2= ror ti.s.0. 1 l r-- E 5 cen< ting I,ll2 psi 13.431 psi 0.033 1 Inner MSIV inlet P g 4..- = I for flin. E = r-Q "'". G Torsion 605 psi 0.0450 1 Inner Msly inlet N N for 71.5.D. J g, U Sm 0 Axial 6,510 psi 0.181f! 4' Inner f tSIV Outlet N "O T f o r f4. s. n. C E* 11 liending 2,'>4 5 ps i 35,816 psi 0.0822 7 Outer MSiv Outlet T 3 i C for it.S.D. O R lorsion 732 psi 0.0204 4 Inner MSiv Inlet 0 S for fl.S.D. N 'i D Axial G,454 lb 10,200 lb 0.53 1 Inner MSIV - M.S.B. E S Bending 307,101 in-lb 678.700 in-lb 0.45 1 Inner MSiv - M.S.B. f I B G Torsion 44,100 in-lb 678,700 in-lb 0.06 1 Inner MSIV - M.S.B. O k'. N N N I f 0 Axial 5,434 alb 10,200 lb 0.53 8 Inner MSiv - M.S.B. E fi T T I Il Hending 547,662 in-lb 678,700 in-lb 0.01 8 inner MSIV - M.S.B. o m .E W N' R Torsion 64,306 in-lb 678,700 in-lb 0.10 8 inner MSIV - H.S.B. T M [' S E g (1) Load Combinations of 1 through 9 are evaluated. Weight force is taken out of this combination. 5 4 s

~.- s. ..i... m G EN E R AL h E LE CTRIC. 22A6416 sa ao.144 NUCLEAR ENERGY DIVISION 0 NOTES ON TABLE D1 LOAD COMBitlATION AND ACCEPTANCE CRITERIA FOR NSSS PIPING AND PIPE HOUNTED EQUIPMENT NO. LOAD C08INAT10?!S ~ SERVICE LE /ELS i 1 Normal Operating and Operating Basis Earthquake Design Condition 7 2 Normal Operating, Operating Basis Earthquake, Operatieg Transients A and B 3 Normal Operating and Operating Transients and Operating Basis Earthqt,ake C 4 Normal Operatino and Small Break Less-of-Coolant Accident and Associated Operating Transients C 5 Normal Operating and Infrequent Operating Transient C 6 Normal Operating and Operating Transients and Safe Shutdown Earthquake D 7 Normal Operatine and large Break Loss-of-Coolant Acciden: and Safe Shutdown Earthquale D 8 f.'ormal Operating and Interrediate loss-of-Coolant ~ Accident and Associated Operating Transients and Safe Shutdown Earthquake D 9 Normal Operating and Large Break Loss-of-Coolant Accident D e .g . :.i f

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i I GEN ER ALh ELECTRIC 22A6416 sa. uo.146 NUCLEAR ENERGY DIVISIOT a nev. O y i TABLE D2 (Con.tinued) i SERVICE LEVEL NO. lDAD COMBINATI0?4 2.... ACCEPTANCE CRITERIA b T - 2/2 D 1 TE + W + ISE; + SSE ) + (TSVC)2 2.0 S D m N g + SSE )2 + (RV2El 2 TE + W + SSE p 3 1 7 /2 ALL 2If + RV2 ~ D r- {5SE;+SSE) + (CHUG 3 + CHUGD 3 TE + W + D 1/2 + (RV2 ADS + RV2 ^ $) g 0 4 TE + W + SSEg + SS D) +(C0!iDg + COND } D + (RV2 ADS + RV2 ^ ) 7 0 - 1/2 i S TE + W + SSEj + SSE ) + (VLCg + VLC )2 } D g 6 TE + W + SSEg + SSE ) + (CHUG. + CHUG } D D N + (RVI)2 7 TE + W + SSEg + SSED + (C0!!Dg + C0f:D I D + (RVI) ~ x 1/2 g + AP )g + (SSEg + SSE I 8 TE + W + AP D D e ) \\/ v

..:~'*-"-"-- ~ / GEN ER A L () E LECTRIC 22A6416 sw. wo. 147 NUCLEAT ENERGY DIVIs!OM y REY. 0 TABLE D2 (Corttinued) LOAD CRITERIA CRITERIA FOR PIPE.(S +Se rec.gn. ) MSIV CRITERIA pp;., M p 1.0.75S,(Torsion) LeakageLimitl Service level A A P P 2,g 2 C 1 7S S,(Bending) 0 7 P FA+PA 3 1 0.75 S, (h ial) P H 3'{I{,L[efs 2 1 2.05,(Torsion) Op ity M +N B C y 1 2.05,(Bending) P FA + P^ + 3 1 2.0S,(Axial) P O e 'e ~ s \\. I

G EN ERA L h.E EE CTRIC 22As416 soo. 248 NUCL EAR ENERGY DJVisl0*d stv. 0 TAB,LE D2 (Continued) ,-j NOTAh!ON. F Axial loading due to pipe reactions g H Torsion load about A exis g M Bending load about B axis B H Bending load about C axis ) Combined values for various C levels as shu,m in this table. t Z Section medulus of pipe P P Axial load due to pipe's internal pressure g A Pipe retal cross-sectione' area p j S Primary stresses pg3g S Secondary stresses SECOND 5, ASME Code value for carbon steel pipe at design temperature %h "C ~,. N. n' 8 ~, V M A g

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J 3 GENER ALOa ELECTRIC i 22A6416 sw. wo. 149 NUCLEAP. ENERGY DivisJON ~ sa y. O TABLE 03 MSIV. BONtitT FLANGE - LOAD CRITERIA f SERVICE ~ LEVEL NO. LOAD Cotsit:ATION ACCEPTANCE CRITERIA (OBE)g+(TSVC)g372 kg ~~' 8 1 g EE I gw 2 (OBE )2 (RV1)y1/2 5-i 0 g "U ge 1/2 wm 3 (OBE )2 + (RV2 ALL)2 a l.'c o fs I 1 .J N -1/2 a-d f. (CHUG;)2 + (RVI)2 5~- C 1 1/2 v (C0 tid)2+(RVI)f s> 2 g Ex m2 - 172 .s m 3 (CHUG)2+(R"2 ADS)2 E'N i g g 8 4 (C0fD )2 + (RV2 ADS)21/2 s .f g g J 7 g ~ s G 6 l t I I \\ \\ """'7--.-.. g _ w__ ;mm _5 mmed - - - " ' " ^ ~ ^ '

~ .4 ':f. :. l GEN ER A L h ELECIRIC 22As416 so. uo. 150 NLELEAR ENERGY DW1310N arv. 0 TABLE D3 (Continued) SERVICE LEVEL NO. LOAD COMBIfiAT10!1 ACCEPTAfiCE CRITERIA ~ 1/2 o '(SSE )2 + (TSVC)2 g, D 1 I eM ~ ~ - 1/2 EE 2 (SSE )2 + (RV2 ALL)2 g,, I I g3 1/2 =E 3 (SSE )2 + (CHUG )2 + (RV2 ADS)2 g$ g g 3 W5 ~ - 1/2 no (SSE )2 + (C0tlD )2 + (RV2; ADS)2 4 g g u.-. 3/2 Ym ~ (SSE )2 + (CHUG )2 + (RVI)b 8,3 5 y y

e 1/2 5

6 SSE )2 + (C0:i0 )2 + (RVI) g g _ 3,2 7 (SSE )2 + (VLC )2 8 ~~~ I I g ~ 1/2 R ~ S (AP)2+(SSE)2 e - 3 3 }. \\., t .j.. g.

i i,.,, TABLE 16-B FSAR MSIV INLET /0UTLET - 'U ' '; :';, i '..f.$.i e HIGHEST STP.ESS SLtWARY 3 SHORE EM - MAIN STEMI LINE B .1 I LOAD COMBINATIONS i L 1 Identification of Equir Governing ment with Highest Lond:' l 3 Highest I Allowable Load (1) Calculated Limits Ratio l Comb. No. .;I Item Evaluated Load ( ]. f Node 97 LEVEL A 6086 15375 .396 1 Node 103 il !j STRESS DUE LEVEL B 6120 41000 .150 2 l. a Node 103 j TO AXIAL 6172 41000 .15 4 LEVEL C Node 103 a LEVEL D 6198 41000 .15 8 J 1 il I l LEVEL A 1155 15375 .076 1 Node 97 t t F 5 Node 97 41000 .034 2 STRESS DUE LEVEL B 1396 Node 121 4 41000 .035 L TO BENDING 1417 M0 MENT LEVEL C Node 121 41000 .045 8 LEVEL D 1845 i k i a; n-g g ~ Ee 4 m 6 s

TABLE 16CFSARMIIVINLET/0UTLET N , lg, [ HIGliEST STRESS SIM1ARY ' 'l SHOREHAM - MAIN STEAM LINE C gj i s L Governing i Highest Allowable Load (1) Identification of Equip! Item Evaluated Calculated Limits Ratio Comb. No. ment with Highest Leadsi Load a, I LEVEL A 6036 15375 .393 1 Node 91 & 85 STRESS DUE LEVEL B 6172 41000 .15 2 Node 91 TO AXIAL a LEVEL C 6720 41000 .16 4 Node 91 i I LEVEL D 6864 41000 .17 8 Node 91 H [ N Node 107 LEVEL A 543 15375 .035 1 STRESS DUE LEVEL 8 911 41000 . 62 2 2 Node 107 TO BENDING F10 MENT LEVEL C 1339 41000 .033 4 Node 107 LEVEL 0 1542 41000 .038 8 Node 107 4 i e e l i b

i NUCLEliR POWER ' STEMS ENGINEERING DErRTMENT MEM3 G.I. Samstad R.W. Hardy Attachnent' 8 .' t[ R.L. Lebre DATE: August 27, 1982 ~ Specific Item No. 7 REQUIRED RESPONSE rnou: J.C. Kelso/E. Intrator DATE: FOR: ACT,10N O SUB>t CT: SHOREHAM RCIC TURBINE SEISMIC SIMILARITY DEcis10N O ANALYSIS INFORMATiord - Q PWA 2613XS Rev. OC requested, for the SQRT progran, a similarity analysis between ~ the Shoreham RCIC turbine and the turbines that were dynamically tested. This letter presents the results of this analysis. In order to prop'erly support the similarity claim, submitted drawings and other cesign information were extensively reviewed for identifying the differences between the Shorehan RCIC turbine and the turbines which were tested. Also, during several visits to the turbine vendor's facility, detailed " bills of material" and other proprietary manufacturing drawings were reviewed. The results of these reviews confirm that many areas of the turbir.es are identical in design. There are, however, specific differences between the turbines, sone totally insignificant, such as changes in the oil well cover plate design, while others receire engineering judgcent or analytical efforts to justify the claim for similarity. These latter areas are sner.ifically identified below, with justification offered for similarity claim or recommendations for corrective action. Base Plate Desien (Refer Turbine Outline Drawing 65818E Yersus Eb53E, a' lid the Proprietary Base Plate Drawing 65983C Versus 675170) The coupling end pedestal for the Shoreham P,CIC turbine consists of two square columns, whereas the tested turbines had a solid rectangular section for the coupling end pedestal. An analysis of the Shoreham type base plate by Science Applications Incorporated (Marvin Cohn, dated August 28,1980) confirmed its capability of with-standing the required dynamic loads. There are other differences in the respective base plate designs which do not affect dynamic capability, such as grout hole locations, oil filter orientation, and a minor change in the location of the anchor bolts. The SA1 analysis also concludes that the #8 taper pins used for coupling end align-ment are adequate, but marginal. The first qualification test program was conducted on a turbine using (8 taper pins, one of which failed after 31 tests and an accumulated test time of almost 15 minutes (refer VPF 3622-79(1)-2, Tab 2, response to N0D-7 for more infornition). The turbine used in the second test program used (9 taper pins and lock plates for the pedestal bolting. No problems were encountered, but it should be noted that total test time was only 6.5 minutes (refer VPF 3622-527-1 for more information).. ACTION: Consideration should be given to the modification to install #9 pins an'd pedestal bolt lock plates. FD1 114-88524 will be issued to define this installation. ~ cc: C.W. Dillmann, J.S. Mokri, M.P. Patel 88E DG 917 (RE V 7/79)

1 f Oht. 8-27-82 .Page 2 pwer Half Turbine Case The Shorcham lower half turbine case is essentially the same as those used on the test turbines. There have been minor changes in machining for improved productivity. These changes are judged to have no effect on dynamic characteristics, ifpper Half Turbine Case The GS1 RCIC turbine has lower half steam admission only. As such, the upper half turbine case does not have a high pressure steam ring (refer section drawing 77322E vs. 99019E). The casing is rigid, but with less mass, resulting in less dynamic loading on the support pedestals. j Turbine Shaft I The machining of the Shoreham turbine shaft outboard of the governor end bearing has l minor differences from that on the test turbines due to different overspeed trip designs (refer section drawing 77322E vs. 99019E). These differences do not affect the dynamic characteristics of the trbine shaft. Overspeed Trip Desion The Shoreham turbine uses a " disc type" mechanical overspeed trip design whereas the test turbines used a " pin type" design (refer drawing 65638B vs. 98501D). Externally, the trip assembly components are essentially the same, with minor differences in the stem length on the tappet-ball holder, the connecting rod length, and the bracket design for the limit switch attachment. The major difference is internal, i.e., the trip actuating device -- disc versus pin. As is evident from the referenced drawings, the trip devices are spring loaded, small mass components which are judged to be insensitive to external dynamic loads. l In the unlikely event that an overspeed transient occurred simultaneously with a l seismic (or other dynamic loading) phenomena, it is possible that the actual trip [ speed would be lower than design. However, this possibility would probably occur with both trip devices. ACTION: No action is deemed necessary. However, if the customer is concerned, th'e turbine shaft could be modified to accept i conversion to the " pin type" trip device. _ Governor Valve The governor valve on the Shoreham RCIC turbine is smaller than the valves used cn the test turbines. The valve internal design is also different (refer 3 j drawing 77336D vs.101180D). 1 The steam forces associated uth governor valve operation are judged to be sub- )l .stantially greater than the forces related to external dynamic loads, thereby rendering the external loads as insignificant. The operability of both valve j designs has been demonstrated by test and by actual operating experience. L l l ~ -.. _. _ _...

J-j'. .DJst. 8-27-82 \\* r f. s Page*3 1.- I Finally, with the smaller, but rigid valve body, the forces associated with external dynamic loads are inherently less at the valve / turbine inter. face. ~ Trip and Throttle (T&T) Valve The Shoreham RCIC turbine uses a 3" - 900f Schutte and Koerting T&T valve, with overal'1 dimensions (inlet centerline to top) of 40-1/4" and face to face (inlet to outlet) dimension of 15-1/2". The test turbines used a 4" - 900# Gimpel T&T valve, with comparable dimensions of 41-3/8" and 17-7/8", respectively (refer drawing 69-XE-41 vs. 89621E). s.a Review of the referenced drawings substantiates the claim for similarity between i the two valves. The only major (but judged to be inconsequential) difference is that the Shoreham valve uses a G.E. trip solenoid -- push to trip, whereas the test turbines use a Thrombetta trip solenoid -- pull to trip. The actual trip nechanism is essentially identical on both valves. One $rea which could not be verified in the record search was the stiffness of the spring used on the trip latch assembly on the S&r, valve. During the first cual test program, we found it necessary to increase spring stiffness to 25#/ inch in order to prevent trip latch separation during the resonance search tests (refer, to YPT 3622-79(1)-2. Tab 2, response to NOD-2 for detailed information). ACTION: Verify stiffness of the trip latch spring used on the S&K valve. If necessary, replace with a spring having a stiffness coefficient of 25#/ inch FDI 114-88524 will be issued to define this irispection activity. Turbine Electronic Controls The electronic and electrical / hydraulic controls used on the test turbines included: Power supply (dropping resistor) - W8270-281 Ramp generator / signal converter - W8271-083 and W 8271-590 EGM Control Box - W827i-236 Hydraulic Actuator - W8250-133 Hydraulic Servo - WW8250-190 Dur records indicate that the following comparable equipment was originally installed on the Shoreham RCIC turbine: Power supply (dropping resistor) - W8270-281 Ramp generator / signal converter - W 8271-083 EGM Control Box .WW8270-849 Hydraulic Actuator' - WAS250-133 Hydraulic Servo . W8250-190 The only difference between the controls of the Shoreham turbine and the tested turbines is the EGM Control Box. Purchase Order 205-YC852 has been issued to . replace the Shoreham EGM Control Box by Model 8271-236. In addition, this P.O. .also provides replacement of the RGSC by Models 9903-091 or 8271-590, both qualified. F01 1)3 88524 has been prepared to define the installation of the new components. ACTION: Already taken. \\\\

~..-.--. - - -- - - ~.a Dist' 8 27-82 Page 4 i Turbine Oil Piping The turbine oil piping is the most difficult area to define design similarity. Unfortunately, the RCIC turbine oil piping was installed via a flow diagram only, without the use of an arrangement drawing. As a result, each RCIC turbine has a more or less unique piping arrangement. However, each arrangement presumably has adequate support to satisfy the minimum criteria defined in the seismic analysis (refer VPF 2757-35-1). However, with the criteria for new load evaluation moving the frequency range of interest up to 60 Hz and beyond, additional piping review is recommended. ACTION: FDI 121-88524 has been ' issued to define the required piping review and the addition of piping supports. The above information completes the required response to PWA 2613KS, Revision OC, Task 6. Support information will be maintained in Design Record File #E51-88. $ $/y/ w/ .C. Kelso Reactor Assembly & Plant Equipment Qualification MC-750, X51819 l( V E. Intrat r Reactor Assembly & Plant [quipment Qualification HC-750, X51776 Gqn ,-%= = ,w=wew, we. _ _ e--===g w+ --= = -

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~" sEP 281982 r .._rr'-- -.J 0 I MEVistoN FIE LD DisPOslTION INSTRUCTIO R.W. HARDY 1 h ,,,,7 o, Shoreham j D g 'g g E D$ o 8S Pn NEc7 HPCI and RCIC Turbine Control Electronics N EcumwEwr m .-' "'"'D T DD" / E41-C002 and E51-C002 w o uo. KS-01-1042 DisCRWTioNOFTAsK Purpose of Instruction The project has cormitted to upgrading critical electrical / electronic components to the qualification standards of Class 1E equipment. It is therefore necessary to replace existing electronic control components on the HPCI and RCIC turbine with new equipment, equivalent to that qualified by test. This new equipment has internal design improvements which enhance overall operability; externally the new equipment will be a "one for one" replacement with the existing equipment, except for terminal designations. Required Documents HPCI Turbine Instruction Manual, at site RCIC Turbine Instruction Manual, at site Woodward Plant System Wiring Diagram 9976-717(VPF3622-25-2), included Material Required The new electronic control components include: Woodward Governor EGM Control Box for the HPCI Turbine, Model #9903-109 (Terry Corp. Piece #890004A04) Woodward Governor EGM Control Box for the RCIC Turbine. Model #8271-235 (Terry Corp. Piece #075850A03) Woodward Governor Ramp Generator / Signal Converter Model #9903-091 or 8271-590 (Terry Corp. Piece #890005A02 or 075925A02) This material has been requested via MR #YC852, with delivery direct to site. 6 APPHoVALS oATE APPROVALS DATE 7.as to riputut is sarriv acLaito [T)<cs 0 o IS / sartiv rumetee= es arrtetto E vts Q , o,,, ",, FIELo WORK O6oER No. ',0 *' *l ' ' ' D,,",'7 " E.W. Ziebe 1[N?c deT3 [ g g,

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-.-.~.-...... ~ J.' M6. i:'.. - 7 113-88524 Fo No. 1, REVIStoN 0 O DisPO Tion INsMUCTION SHEET 2 oF - Of5Cr.PfloN oF,ASK ~ Procedure _ Caution: Verify proper terminal identification on wiring prior to its removal. HPCI Turbine Control Component Upgrade l Reference the mounting panel drawing 95414C (Section 15-M-17 of the Turbine t Instruction Manual), remove the existing EG-M control box and the ramp generator / ) signal converter module from the turbine control panel. Note: The original equipment may be returned to Woodward Governor Co. for upgrading. Install the new, upgraded EGM control box (Model #9903-109) and ramp generator / i signal converter module (Model #9903-091 or 8271-590) onto the existing turbine l control panel. The equipment interfaces (new versus original) are identical, and no panel modifications are required. The external terminal designations on the new equipment are the same as those on 1 ECM Control Box Model f8270-811 and ramp generator / signal converter module Model 3

  1. 8271-083. Therefore, install interconnecting wiring in accordance with the Woodward Plant Wiring Diagram 9976-705, contained in Section 8 of the Turbine Instruction Manual.

1 1 RCIC Turbine Control Component Upgrade ] Reference mounting panel drawing 95517C (Section 14-M-13 of the Turbine Instruction Panual), remove the existing EG-M control box and the ramp generator / signal converter module from the turbine control panel. Note: 1) The original equipment supplied may have included an EGM Control Box Model #8271-236. If so, do not remove, as this is the required upgraded unit.

2) Removed equipment may be returned to Woodward Governor Co. for upgrading.

[ Install the new upgraded EGM control box (Model #8271-236) and ramp generator / signal converter (Model f 9903-091 or 8271-590) onto the existing turbine control panel. The equipment interfaces (new versus original) are identical, and no panel modifications are required. Install interco$ecting wiring in accordance with the Woodward Plant System Wiring Diagram 9976-717 (included with FDI). Note changes in terminal designation, compared with existing diagrams in Section 8 of the Turbine Instruction Manual. L i l d~ ~ -., ,o

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^ 9 ' 'I. ':. c.. -. 9.. ($K)3Eyl # M nts fj ;;, , t.' f pog ny, li3-88524 .J,u, L t.u ?_= ..; _ +_a REvistoN O FIE LD DisPOslTioN INSTRUCTION SHEET 3 or ogsen PTeoN oF TA5K ~ Quality Control Requirements ~ Site Quality Control personnel shall inspect final equipment installation, and shall verify " terminal to terminal" wiring in accordance with the applicable plant system wiring diagram. Equipment Calibration The new electronic. control modules shall be calibrated in accordance with the procedures contained in Section 8 of the Turbine Instruction Manual and Service Information Letter (SIL) #351. Schedule for Implementation This FDI should be implemented as soon as the replacement equipment is available on site, and definitely prior to plant / system startup testing.

1) This FDI defines installation of upgraded electronic control equipment, NOTE:

while maintaining the existing 4 to 20 mA signal input from the system flow controller. Due to a potential " ground loop" problem associated with the Bailly flow controller and the turbine control system, a separate FDI will be issued by C&IE, defining conversion from the existing 4 to 20 mA flow controller output signal to a 1 to 5 VDC signal. The impact on the installation of the new ramp generator / signal converter module will be to remove the external jumper across terminals 9 and 10, and to move the existing wire on terminal 6 to terminal 10. This effort must be coordinated with the implementation of the C&IE FDI.

2) The turbine specification (s) will be revised to identify the con-version from the existing 4 to 20 mA control signal to the new 1 to 5 VDC control signal, in accordance with ECA 800801-1, Revision 1.

Appropriate MR/PO revisions will then be issued, requesting required changes to the applicable vendor control system wiring diagrams.

3) Inplementation of this FDI shall result in superseding previously approved FDDR KS-01-1042.

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,y ;. - @. a OF 7 FIE LD DisPostTION INsTRUCTIO { gw HARDY SHEET __ DATE DF ISSUE 1 ISSUED Bf PD & AC UNIT Shorsham DATE$~0 N non cT - RCIC Turbine.1EEE Uccrede setud _ ESi~C002 YA W8/s//2 guy m [E5CruPTION OF TASK Purpose of Instruction Two qualification test programs have been conducted on the GS-2N RCIC tur assembly provided by Terry Corporation. with test results and report cation test in accordance with IEEE-344-1975, The second progran was retrievable from Vendor Print File (VPF) #3622-79(1)-2.a complete e test results and report retrievable from VPF #3622-527-1. The first program identified several areas where design changes were ' required in order to positively assure that the turbine assembly could withstand the con-The adequacy of these design changes was servctive seismic test requirenents. successfully demonstrated during the second test program. The purpose of this FDI is to specifically address each area of potential concern, The and define the necessary inspection and possible corrective action required. items identified in this FDI do not affect GE documents, and ECA/ECN's are not applicable. Required Documents RCIC Turbine Instruction Manual, at site Vendor Drawing 111904C, Lockplate Assembly, enclosed Paterial Requirements The material required for this instruction is specifically identified in the follow-The material can be obtained locally by site ing procedures for each task. personnel, purchased directly from Terry Corporation, or ordered through the General Electric Company. t.cs touwtm, is sne ti v atta,ao Pges O=c APPROVALS DATE APPROVALS DATE sat tTv r v=.cTio= is m'a t c1to hvts p ~~ ,C jg FIELO WORK ORDER NO. j, gy',',C,,* "g, roc YES % NO O b_@ g M W W e/nb= FDi TASK COMPLE TED D AT E DISTRsBUTION CODE fg ? g INTERNAL EXTERNAL *4****G -' ~ e4.gz .pg

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e* -, :v.. * : caw i% " - A l' nevnsson _ O rino oispos: TION INSTRUCTION SHtti 2 OF 1_ ogscwrios or TAsx Procedure Detailed information follows, defining each area of potential concern, the required inspection,.and the necessary corrective action, if applicable. There are no special tools or handling equipment required in implementing these instructions. If vendor assistance is desired, arrangenents for a service representative can be made through the Project Manager, or directly with: Terry Corporation P.O. Box 555 Windsor, CT 06095 Attn: Robert Theroux, Service Panager Tel. (203) 688-6211 Item 1 - RCIC Turbine - Trip and Throttle Valve Latch Spring (Refer Drawing 69-XE-41 in Section 14-M-10 in the Turbine Instruction Manual) During the first (seismic qualification) test program, the initial test activity resulted in inadvertent, unacceptable closure of the trip and throttle valve. The attached photograph identifies the partial separation of the latching lever assembly at the completion of one of the seismic tests. The original latching spring was replaced with one having a higher spring coefficient. The operability of the solenoid trip mechanism and the mechanical overspeed trip mechanism were verified aYter the installation of the stiffer latch spring, and proved to be acceptable. The seismic qualification test program was then successfully comleted. The second (environmental qualification) test program, including dynamic testing, was also successfully completed. Corrective Action Remove the latch spring from the trip and throttle valve assembly, and measure its spring constant, which should be 25 lb/ inch,110%. If the installed spring does i not satisfy this value, it must be replaced. The appropriate replacenent spring I is Terry piece number 105594A10, a 0.845 inch diameter spring with a free length l of 2.75 inches. The installed spring, resting against the " jam nut" on the valve body and the washer in th adjustment is necessary. e latch lever, will have the proper compression. No 32.5 pounds,f, The spring " load" in the valve latched position is i \\ I""* Si

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[ i A9 O ety,sson _a { FIE LD DisPOslTloN INSTRUCTION 3 SHEET or D1sCRIPTioN oF TASK Item 2 - RCIC Turbine - Coupling End Pedestal Assembly During the first (seismic qualification) test program, the entire turbine assembly. was subjected to a total of 33 tests with an accumulated test time of 905 seconds. Approximately one-third of the way through the test program, turbine structural bolting began to loosen. The test facility did not have adequate tools to properly retorque the turbine bolting. Finally, after 31 tests with an accumulated test time of 875 seconds, one of the alignrent dowel pins in the coupling end bearing pedestal failed, and the second pin had an offset distortion of approximately 1/16 inch. Both conditions were attributed to bending loads on the dowel pins due to loosened pedestal bolting. The design of subsequent turbines was modified to use #9 tapered dowel pins in Ifeu of the original #8 pins for alignment control, and to use a positive " lock tab" for the pedestal bolting. The second (environmental qualification) test program, utilizing these design improvements, was successfully completed. Corrective Action With reference to vendor drawing 111904C, attached, inspect the turbine assembly for installation of the #9 taper pins and use of the positive lock tabs on the coupling end bearing pedestal holddown bolts. If not in compliance, the follow-ing corrective action is required: Material: Flat washer, 2 each, Terry Piece f75778A07 Locking Plate, 2 each, Terry Piece #111903B

  • Threaded Taper Pin, 2 each Terry Piece #111284B Taper Pin Nut, 2 each, Terry Piece #75238A05 Note:

(a) To avoid possible disturbance of the turbine alignment, the following procedure is to be carried out on one side of the coupling end bearing pedestal at a tirre. (b) Should it be necessary to realign the turbine, this should be accomplished before fitting the new dowel pins. (Refer to Section 4 of the Turbine Instruction Manual for alignment definition.) (c) Numbers in ( ) are the item numbers identified on assembly drawing 111904C. t

  • Caution:' This is a special 17-4PH stainless steel pin -

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-.7... '.. '..v [* $DYIdIhm,. r.-fisM64 ,,,... - ~ - a 3 $~~ : ! REVtsloN O L f*N5. AN - J w FIE LD DisPoslTION INSTRUCTION sMEET OF DEsCRIPTsoN OF TAsst 1. Remove the existing tapered dowel pin (3). If this pin is smaller than #9, drill 1/2 inch diameter pilot hole and ream for fitting the required #9 pin. 2. Remove the pedestal holddown bolt (5). 3. Locate flat spacer washer (1) on the machined spot facing around the pedestal holddown bolt hole. The washer must sit flat with full face-to-face contact. Any rocking or interference must be eliminated. 4. Place locking plate (2) on top of the flat washer (1), and align holes for the dowel pin (3) and the holddown bolt (5). It may be necessary to enlarge the holes in the locking plate to assure no interference with the dowel pin or the holddown bolt. 5. With the holes in the locking plate aligned, install the #9 tapered dowel pin (3) fimly in position. Assure that the pin extracting nut (4) is threaded back sufficiently to allow the pin to seat fully into its hole. The shoulder of the installed tapered dowel pin should be approximately 1/16 inch below the edge of its reamed hole (referDwg. 111904C). 6. Apply Fel-Pro "Hi-Temp" C5-A lubricant (or equivalent) to the threads of the pedestal holddown bolt (5), install, and torque to 310 to 340 ft-lbs, such that one flat of the bolt head is aligned to facilitate lock plate bending (refer to Section A-A of Drawing 111904C and the attached photo for acceptable orientation). 7. Using a blunt-ended tool (brass or wood), bend the end of the locking plate (2) against the flat of the pedestal holddown bolt (5). The bending line should have a small radius, as opposed to a square edge which could result in cracking. Quality Control Requirements Standard site quality control procedures shall be used in implementing this FDI. Particular emphasis shall be used in assuring that adequate procedures are used in conducting the inspections defined above, and assuring proper completion of the defined correcf,ive actions. Schedule for Implementation This FDI should be completed prior to the startup test activity on the RCIC system. NOTE: FDI 12l defines the required additional supports for the lube oil piping. .e7

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,,,,^N.n.-;.~.. G . %: ' >bw-*d ^ ~ E ~ ~ "- -- - - - - - y i. f!ST 4'V 121-88524 ]' R i.f}.hM. [?N.? ~N.; 3.T3 S Eh i . i; *, M~iX a_- -"r- _ _ _ J 3 REVl5loN SEP 291982 FIE LD DISPOSITION INSTRUCTIONp/ 3 3 SHEET oF R.W. HARDY SHOREHAM" 3 oATE oF I,5$uE paoncT univ ISSUED BY PD & HC RCIC TURBINE DATE k U~ 'O # M EcNiiniooRip ooR E51-C002 w'L No-N/A OtsCMWisONoFTASK This FDI supercedes Rev. O. The purpose of this FDI is to improve the load carr.ying capability required for confirmatory loads of the lube oil piping assembly by adding supports to the existing pipe assembly. 1.0 Required Documents ~GE document 213A8273, Rev. 1. 2.0 Paterial Required / . The material required in this instruction is a 2x2x3/8 angle (A-36), Plate (A-36) and U bolts as identified in the attached sketches for each support. The material shall be obtained by site personnel. 3.0 Procedure 1.ocate and install lube cil pipe supports in accordance with the attached document. 4.0 Quality Control Requirements Standard site quality control procedures shall be used in implementing this FDI, including site QC verification of above work. a APPR OV A LS ;' oATE APPROVAL.5 cATE ve*s t.wis=tast is s.e n v a t La,a o D es O: MP PATEL c M 8 4/ /;./r;

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,, a. s;. ;,> '.~ a ~-- 6 E : - .OI ~ gy._ ;. T :w w.w :.. _ =.,:.. iar.. g fj --w- -lf 10 X,< a ', .l Specific Item No. 8 E S. E ORE HAM NUC _IA7 . t. 4 POWER STATION c 1 UNIT 1 L ~ q 1 + SEISMIC QUAllFICATION REEVALUATION 'l CLASS 1E EQUIPMENT i; ' DIFFERENTIAL PRESSURE TRANS;i!TTER ( C O M P O N ENT N A M E;5,163c1560,163c15ci, 145C3240,163Cin .Mi i PP D. NO.: menn. mcisu s ? ll MPL

REFERENCE:

C41-nc04

p I

GE DRF A00-992, VOLUME 3 i SUPPLEl1 Erit 1 I 2 THE SE!SMIC CUAtlMCATION REPORT (S) IDENT1AED MERE 1N HAVE DEEN EVALUATED , 1 4 AND REQUALIRED WHEAE NECESSARY TO SHOW THAT THE ABOVE. MENTIONED i 3 COMPONENT IS CAP ABLE OF MEETING THE NUCLEAR AEGULATORY COMMISSION i SEISMIC QUAORCATION REVIEW TEAM (SQRT) REQUIREMENTS. ) q l 1 N*C' Db PREPARED BY3 DATE e i I GENERAL ELECTRIC CO., CONTROL ROOM DESIGN ENGINEE: TING onciniz,7,on: l .1 i I j l REVIEWED BY: DATE N SQRT PROGRAM MANA *ER / I s

E l

b Mb APPROVED BY: DATL-QUALIFICATION ENGINEERING MGR. t I 9 t G E N E R A'l h) E L E CT R I C. j .] i ~ --a, . EE7 7'*7_*,'"***7_7,'N __ _ E*** [7 I -.l '.. ' - ' -<k. ~1'-1Y -- j t. 33353 3 .*--m '*...-ea g es.o.~+e.e m e ew w e *, w e% - a

. ~. - - -.... s QUALIFICATION

SUMMARY

1. Component Name: DIFFERENTIAL PRESSURE TRANSMITTER 2. MPL or EDL Item No.: C41-N004, (CE Identification Numberc; 163C1558, 163C1560, 163C1561,163C1563,163C1564 & 145C3240) 3. Qualification Documentation A. Qualification summary of equipment (SQRT form) including required response spectra. Attached B. Reference Documents Reference Document Revision or Number Identification Date Title / Subject 1.

  • GE DRF A00-1084-101 1981 Seismic Test of Rosemount 1151.

2. S&W J.O. No. 116.00.02 9/2/82 Required Accele-File No. 930., GEA-2815 rations for Stand Hounted Equipment, SNPS-1 3. GE DRF A00-794-10 1980 Seismic Test of Ceneric H22 Local Panels. C. Additional Supporting Documents 1. As - Built Reviews of Equipment 2. Shipping Group MPL References 4. Requirements This device is required to maintain its structual integrity and operate when subjected to the seismic and hydrodynamic loads as specified in reference 2 and shown on each Shipping Group MPL Reference Sheet. 5. Demonstrated capability Sin 2 e axis, single frequency vibration tests with a frequency 1 1. scan of 4 to 70 hertz and a 2g input were run in all three axes. Output voltage was monitored during each 30 minute test. Resonant dwells of 30 seconds each were held at the resonant frequencies. Thoughout each test the output was continuously monitored on a strip chart recorder. Output voltage showed no deviation. See A00-1084-101, K for a detailed description of the test. . h%. e .,._.gge.,wp.we~,.-- ....mp,my., ge - 9w w,,,.. --

i s 2. Another single axis, single frequency test sequence in three axes was performed from 1 to 30 hertz with a 3g input. The cycling I time was 30 minutes per axis, and 30 seconds of dwell at each l resonant frequency was performed. There were no electrical shifts observed or mechanical failures noted. See A00-1084-101, L for ~ test details. 3. A multi-axis, multi-frequency vibration test was conducted as shown e in reference 3. The test input 2PA was 7.0g's over a frequency range of 1 to 260 bz. Although the device was mounted on a local rack, the test indicates that the unit can operate satisfactorily during a multi-frequency, multi-axis seismic test. 6. Rationale for Qualification Since the maximum expected acceleration for this device at the Shoreham site is less than the tested capability of 2g's over the 70 hertz range, the device is qualified to SQRT criteria. The dual axis test noted in Reference 3 further supports the qualification for mult-axis affects. e 'b 1 e 1 A eynes, w .... w w ,e

...... _ _ - _. _ _ _..:._.- - a - _ w.._; 8 4 145C3240, 163C1558 163C1560, 0 Qualification Summary of Equipment 163C1561, 163C1563 163C1564 (GE PPD Number) s I. Plant Name: Shoreham Type: 1. Utility: Long Island Lighting Co. PWR 2. NSSS: GE

3. A/E: Stone & Webster BWR-4 Mk II II. Component Name Differential Pressure Transmitter 145C3240;1 1.

Scope: [X] NSSS [ ] BOP 163C1558;1 163C1560;3 163C1561;1 163C1563;1 2. Model Number: Rosemount 1151 Quantity: 163C1564;1 3. Vendor: Rosemount 4. If the component is a cabinet or panel, name and model No. of the devices included: N/A 5. Physical Description a. Appearance Electronics housing attached to pressure sensor. b. Dimensions 4.5" diameter x 9" high c. Weight Approx. 11 LB 6. Location: Building: See attached "As Built Review of Equipment", line III.1. Elevation: See attached "As Built Review of Equipment", line 111.1. 7. Field Mounting Conditions [ ] Bolt (No. , Size ) [ ] Weld (Length ) [x] See attached "As Built Review of Equipment", line III.3. 8. a. System in which located: See device list for system in which each device is located, b. Functional

Description:

Instruments perform 1E function in the system indicated on device lists c. Is the equipment required for [ ] Not Standby [ ] Cold Shutdown See device list for each system. [ ] Both [ ] Neither 9. Pertinent Reference Design Specifications: PPD # 145C3240, 163C1558 163C1560, 163C1561, 163C1563 163C15654. NOTE: 163C1558, 163C1560, 163C1561, 163C1563, and 163C1564 are qualified by similarity to the tested 145C3240.. 12/80 L.

.~ -. _.. ..a._...-..... e 145C3240, 163C1558, 163C1560, 163C1561, 163C1563 163C1564 (GE PPD Number) ~2-III. Is Equipment Available for Inspection in the Plant: [x] Yes [ ] No IV. Equipment Qualification Method: f [x] Test [ ] Analysis [ ] Combination of Test and Analysis Qualification Report *: CE DRF A00-1084-101,K (No., Title and Date) Seismic Test of Rosemount Model 1151, 9/11/72 Company that Prepared Report: Rosemount Company that Reviewed Report: GE V. Vibration Input: [ ] Seismic only 1. Loads considered: a.

b. [ ] Hydrodynamic only
c. [x] Combination of (a) and (b) 2.

Method of Combining RRS: [ ] Absolute Sum [x] SRSS [] (other, specify) 3. Required Response Spectra (attach the graphs): Attached 4. Damping Corresponding to RRS: OBE N/A SSE 4% 5. Required Acceleration in Each Direction: [ ] ZPA [x] Other At location (specify) OBE S/S = N/A F/B = N/A V= N/A SSE S/S = F/B = V= 6. Vere fatigue effects or other vibration loads considered? [ ] Yes [x] No If yes, describe loads considered and how they were treated in overall qualification program: N/A

  • NOTE: If more than one report complete items IV thru VII for each report.

12/80

    • See device list for individual component required accelerations. Required ac-celerations were provided by Stone and Webster. [

Reference:

Stone and Webster J.O. No. 11600.02, File No. 930, CEA-2815 dated 9/2/82. .-s g ev .,w = g.e, w -e-6m-s.m==w.--e..y.gmw,.q-. - w-e

m.. \\ 145C3240, 163C1558, 163C1560, 163C1561, 163C1563 163C1564 (GE PPD Number). yI. If Qualification by Test, then Complete *: [ } random 3. [X) Single Frequency [ ] Multi-Frequency [ } sine beat [X) resonance search 2. [X) Single Axis [ ] Multi-Axis 3. No. of Qualification Tests: OBE _ N/A _ SSE _ N/A _ Other (specify) Resonance search (2g, 4-70 bz) and malfunction limit test (3g, 1-30 Hz). Device was subjected to 5 OBE's and 1 SSE while mounted on a GE local rack. See A00-794-10. 4. Frequency Range: 4-70 Hz 5. Natural Frequencies in Each Direction (Side / Side Front /Back, Vertical): S/S = 62 Hz T/B = _7_ _ (minor),50,68, Hz V = 70 Hz 6. Method of Determining Natural Frequencies [x] Lab Test [ } In-Situ Test [ } Analysis 7. TRS enveloping RRS using Multi-Frequency Test 2 g. accel is greater than the ZPA of the RRS [x} No[ ] Yes (Attach TRS & RRS graphs) S. Input g-level Test: OBE S/S = _N/A F/B = _N/A V = _N/A SSE S/S = _N/A F/B = _N/A V= N/A OTHER(specify) S/S = 2 a 's F/B = 2 e's V = 2 z's Also an input of 3 g's @ 1-30 Hz was applied during a subsequent see GE DRF A00-1084-101 for 2g and 3g tests. test 9. Laboratory Mounting: i 1. [ } Bolt (No. . Size ) [ ] Weld (Length )[] Transmitter was mounted to a pipe which was clamped to the table ( resonance Functional operability verified: Transmitter was mounted on a local rack fo test) 10 [x] Yes [ ] No [ ] Not Applicable 11. Test Results including modifications made: Test results were _s a t i s f a cto ry. 12. Other test performed (such as aging or fragility test, including results): _N/A L

  • Note:

If qualification by a combination of test and analysis also complet Iten VII. e _,,.y.. e.e a

~~._-..u-_- l .4 145C3240, 163C1558, 163C1560,' 1 163C1561 163C1563 163C1564 (CE PPD Number) . 5/A VII. If Qualification by Analysis, then complete: 1. Method of Analysis: s [ ] Static Analysis [ ] Equivalent Static Analysis [ ] Dynam'ic Analysis: [ ] Time-History [ ] Response Spectrum 2. Natural Frequencies in Each Direction (Side / Side, Front /Back, Vertical): S/S = F/B = V= 3. Model Type: [ ] 3D [ ] 2D [ ] ID [ ] Finite Element [ ] Beam [ ] Closed Form Solution 4. [ ] Computer Codes: Frequency Ronge and No. of modes considered: { [ ] Hand Calculations 5. Method of Combining Dynamic Responses: [ ] Absolute Sum [ ] SRSS [ ] Other: (specify) 6. Damping: OBE SSE Basis for the damping used: 7. Support considerations in the model: 8. Critical Structural Elements: Governing Load or Reponse Seismic Total Stress A. Identification Location Combination Stress Stress Allowable Maximum Allowable Deflection B. Max. Critical to Assure. Functional Opera-Deflection Location bility k i 12/80 S .m. ..,..w, pw e. - %. ~~+e**

  • w==e-

.mr

r A t + t SEISMIC OUALIFICATION REEVALUATION OF NUCLE.1R' SAFETY RELATED EQUIPMENT 1 SH GP MPL

REFERENCE:

C41-5110 TITLE: STDBY LIO CON LCL INSTR PL 028X153TFC001 i REQUIRED FOR: ( ) HOT STANDBY, ( ) COLD SHUTDOWN, ( )BOTil, (X)NEITHER REV 1 l 's-IIESC RIPT ION

E:SFISMIC CAPABil.ITY/ :

MAXIMUM EXPECTED

NATURAL FREQ. :

l EQUIPMENT NAME

IDENTIFICATION :C: MALFUNCTION l.IMIT
ACCEL.ERATION AT LOC.:

(Hz) I I 6 s MPL NUMPER

: F-B
S-S V

F-D : S-S : V

MTG.

INSTR; i l. 1 i

1EMPEAATURE SWITCH
157C4629P901
P:

l

U.11 !!993
: S.A.
S.A.
S.A.

( INDICATOR, PRES 50RE

163C1184P017
P:

l'

.41 R903
: 15.0 : 15.0 : 15.0 : 1.0
1.0
1.0 6

100+ : .I

T P At4SM I T TER, ~ GAGE PRESS
163C1563P917203 :P: ---- : ---- : ---- :

l _1>:C41' t:094

: 03.0 : 03.0 : 03.0 : 1.0
1.0
1.0 6

50 t j i

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... z..- a - - .. : _. :. ~. . :... - n. G *. L - M' g s. ~ AS-3CII.T RE*!!!"J OF ECUI?MCTI' Plz : Mr=e: Sh:::hn= tree: Zi.?. 4.'C: II 1. Utility: ' :* C0 '2. NSSS: E 3. A/E: Stone and Webster II. Ecui:=e:: Iden:1fics: ten (to be completed before field inspection) Scope: BCP. 1. Name: ?rcssure

  • 2nstitter 2.

Vendor (manufacturer if different) and model nucher: Reusenount. Mede; 1151 3. S&W Mark number: ICf. *?T002 4. Drawing nu=ber: 7.62-133J (Vendor or S&W file) 5. Location given by S&W records: S&W Dwg. ( Building sc Elevation 112 f t Source 11600.02-FK-1H 4 III. Installation Reviev (to be completed during field inspection) 1. Actual location: 31dg SC Elev 112 f t Col. No. 9 2. If not installed: Reason: N/A Present location 3. Mounting: N) Floor [ ] Pipe * [ ] Other (See Section VI. Supplenental Re= arks) (Describc) . - - - -.- -- De scribe-the weldin g. 4 r holcin g.. for: --- - -----.- - --- - - - -- - - - - - -.. Drawing (4) 1/4 in, dia bolts (SH1-3'43, Sketch K-25;-2) Field (4) 1/4 in. dia bolts If different, gise E&DCR No. and date N/A (attach copy)

  • to valve bonnet for operators 4.

Equipment matches the drawing [X). If not, describe differences N/A l e a. .*-*=e*.--*em--****-****e**.****""*b

  • ' * * ' " * " * ~

m -r,.,,-,., p w

.a-a 2 =a.,__.--....... . ~. x _w e /. s.

  • C Cil::0 %

D 5. 3ase.;rnfigurati:n ^ Wedge Anchers(O 1/2 in. 0.0. ezch baseplate E= bed =ents Supple =en:ary Steel Descrip:1cn: e IV. Namer 12:e Ec de - (:: be cr=,,leted during field inspection) 1. l.ocati:n en equip =en: Too 2. Type IX ).Me:a1 plate bended or riveted to equip =en ( ) If not, describe 3. Na=eplate contains the following inforr.ation: [X ] Equipnent Name Pressure Trans=itter [X ) S&W Mark Nu=ber 1C41*PT002 / [X ) Na=e of Vendor (=anufacturer if different) Rose = cunt ( [ X ) Vendor Model No. 1151 V. _P_hotocraehic Record Take photoBraphs of the =ounting. If the equip =ent is =ounted on a support structure such as a duct or instru=ent stand, take photographs of :he support structure and the equipment together. On the back of all prints, s:a=p with your "noted" sta p (approxi-mate date photo was taken) and shew the equipment = ark au=ber. VI. _Sucole= ental Remarks - - - - - - -- - - - -(A s-Bu i-i t -Lo ad s ).. -.Ye s-X. -- Ko. - - - - - - - - - - - -- - - -- - - - -- -- - - - - - Instru=ent =ounted on double les floor stand. (SH1-343) Reviewers Sta=p: NIO NAS 2 O bb2 C.03 Initials Distributi.on: Original to the As-Buil: Record Copy to the Seis=ic File Photos in the Equipment Albu= (pasted) Central File Package (at site) ~ 'C4E~ .".Y.. ~ - '. eE

  • R9  ?

. e 0 in k C *. Spacific Item No. 8 t A I p-me t i yd..na,vmcd ~ l Twx: sto-57s si 3. TELEX 39 0123 I

  • i SEISMIC QUALIFICATION TEST FOR 1151/1152 PF.ESStlFI TRANSMITTER WITH STAINLESS STEEL ELECTRCHIC HOUSING s,-

RMT F4 port 2758 i I Israil Isra11 . 2,W~..~ ~....

y?'. ,~ s-Vf l SEI.SHIC QUALIFICATION TEST FOR 1 151/1152 PRESSURE TRANSMITTER WITH STAINLESS STEEL ELECTRmIC HOUSING RHT Report 2758 SC0k AND SUM $. RY 1. This report covers a seismic test en a Rosencunt Pressure Transmitter model 1151/115 with stainless steel (SST) electronic hcusing. The test was perferned at E viren Laboratories, 9725 Girard Avenue South, Minneapolis, m 55431. Two configurat ons were tested, namely solid rount and with panel neunt mot.nting bracket (RMT Nh. 01151-0035-0004). The data obtaired shows minimal effec the given seishic vibratien input en the transnitter perfomances. A fragility limit of 3 9 was established for the bracket asse bly and in excess of 4 g's for solid rount. 2. TESTkNG 2.1 Gene' al r The seis,ic qualifications of Resercunt mocel 1151/1152* is intended to demcnstrate thy e:;u.pnent's ability to perfctm its function and within its specified accuracy during and after the time it is subjected tc the forces resulting fren a prespecified s{isni: spectrun. The transnitter is subjected to the seismic tests while simulatijg tne operating conditicns as proof testing and to detemine the transmitter (w{th SST housing) capabilities during such test, p ___ 'Nodel 1151 is; mechanically identical to nadel 1152. Model 1152 has the re- } d quiments of $aterial traceability o'f pressure retaining parts and the use of f non Teflon wird in its assembly. ._. m . a - _ __=. ~ m

a. - ~ _ _ _. = Attaclunant 11 Sp cific Ittm No. 10 SHORElIAM EQUIPMENT QUALIFIED BY SINGLE FREQUENCY / SINGLE AXIS TEST Spec Equipment No. Spec Equipment No. Item Description Items Item Description Item 39-1 4.16 kV Metal-Clad 3 310-2 Mtr Operated Cntrl 20 Switchgear Valves (Act'uator) 54-1 Fire Dampers 38 310-3 Mtr Operated Cntrl 12 Valves (Actuator) 89-1 Aux Skid & Accessor. 24 318-1 A0V - (Solenoid) 2 89-2 Gen & Exctr Control 3 318-2 A0V (Solenoid) 2 Panel 318-3 A0V (Solenoid) 2 89-4 Engine Control Panel 3 (Limit Switch) 2 89-5 Diesel Engine 3 318-4 A0V (Solenoid) 2 (Limit Switch) 2 89-6 Starting Air Rec'ver 12 318-5 A0V (Solenoid) 17 89-7 Starting Air 6 (Limit Switch) 17 Compressor 318-6 A0V (Solenoid) 6 105-1 Cont. Rm. AC Filter 2 (Limit Switch) 6 Trains (El Comp Only) 318-7 A0V (Solenoid) 4 105-2 RBSVS Filter Trains 2 (Limit Switch) 4 (Elec Comp Only) 319-3 Cntrl Pal (Pal Only) 9 111-1 A0V (Limit Switch) 6 (Solenoid) 6 348-1 Press - Temp Switch 4 111-3 A0V (Solenoid) 4 348-2 Press - Temp Switch 15 (Limit Switch) 4 406-1 Resist. Temp. Detector 18 I 118A-1 125 V Static Battery 3 14 Chargers 423-1 Chilled & Service Wtr l A0V (Solenoid) 7 120-1 B.O.P. Main Control 1 (Limit Switch) 7 Board (Elec Comp Only) 423-2 Temp control Valve 124-2 Dist Panel Board 12 (Solenoid) 2 (Limit Switch) 2 134-1 Reactor Cont. 10 Elec. Penetration 423-3 Temp Control Valve (Solenoid) 2 172-1 A0V (Limit Switch) 8 (Limit Switch) 2 (Solenoid) 8 GRP-1 Limitorque Oprtors 165 310-1 Mtr Operated Control 4 Valves (Actuator) CRP-2 Limitorque Oprtors 54 CRP-3 Limitorque Oprtors 4 GRP-4 Limitorque Oprtors 12 B3-11600.02-MS95

_ _ _ 2 i - s 1

  • g Specific Item No. 10

',----t-t ygw. ;. a.= = c..mx .7.r - ~ - - - r ; : n-7 u ' v ' :- " S2 :D ? M - = l * ~2 -.m c._ - g j p SHOREHAM SORT DRF# A00-992 ..j 1 [ t i Rev. 1 l 1 S HOREHAM NUCLEAR s/5/81 } i POWER STATION 'I t r UNIT 1 - i 1. u .I ti f i E. BEISMIC OUAl.lFICATION REEVALUATION j Ii CLASS IE EQUIPMENT f Efl .1 % J il LOCAL PANELS i 1 h SAI f 029-QA-80-PA Rev.2 [ h 2 0 .~{ l k0/ l :2 } Prepared by: E S. RAMADAS A ./ - i [ Date: April 3,1981 j f l j i 1, Orgon!20 tion: SCIENCE APPLICATIONS, INC. l s: I 5 Polo Alto Scuore, Suite 200 ) 4 5 J Polo Alto, Collfornio 94304 ,{ I l t ti 1 1 ,3 j f f , i f-4 i it } i l l { t y-1 ( 3 5 l 2 8 l- ) \\ J I i t GENERAL h, ELECTRIC =- . _. _ m _,.. __ r s ;. r, 'F**"*'. OU'37'TFf E "4,71* *-**," ".7 ?? 'l-g g ;. q. -- y a,*ag.g* Uy W R 7 r

n. w._-._ ~~ = s I, Table 2 a ,a e SHOREHtM NUCLEAR PO'a*ER STATION I.- N555 CLASS 1E LOCAL PANEL DEVICES WITH SItiGLE AXIS t / MAXIMUM EXPECTED ACCELERAT10'4 AT MOUNTING. LOCATION. f IEEE 344-71 CAPABILITY MAX. EXPECTED ACC. AT ANY LOCATION O'l MP1 # GE PPD DWG# (MAX.ACCN ON TESTED PANELS) SHOREHAM PA'iEL5 f-b s-s y f-b s_s v i ! 15.0.!. 15.0 ' 1.41 3.0 5.4 145C3008 15.0 Ol$'d!![ej ' 2 ^ i s 8 6.8 1,41 821.h06.N09.%021;t31.ND19-

22;t21.sca.m:5.tst.a:1.

145C3009 11.0 11.0 11.0 3.0 e

  • g in.sae.hn7 s

5 t41.h010.t51.h0E.NDB.N019 145C3011 .15.0 15.0 15.0 3.0 ! 6.8 e e 1.41 i I j I 145C3046 13 13 8 10 3.0 l5.4 I 1.41 C71.N02.111 ND10.hCil; ,'1;gpo21:E51.hos, a C71*"0" 15BC7055 5 10 '{ 10 3.0 4.5 1.41 i 821.NO37 159C4383 10 l 10 l 10 3.0 s 5.4 l 1.41 s 1 i i !. 4.5 !. 1.41 I 10.0 3.0 821.kD24,H026.h031.t;042 159C4384 10.0 10.0 i s' .s 621.ko25 159C4445 15.0 l 5.0 l 10 3.0 I 4.5 1.41 ~ I 121.no? 159C4606 29.0 l 29.0 j 29.0 3.0 l 5.4 1.41 e e t21. Rot,t 1.RG1,R33IRC5; 163C1184 15.0 15.0 a 15.0 3.0 l 5.4 1.41 e e E21. rot;t11.R02,RD3-8 e I!!.201.C N ~ i i i (11 8022,t51.ho31 163C1185 15.0 l 15.0 8 15.0 3.0 l 4.5 j 1.41 s I E E 402E ;t21.h:1;[41 309.wo13. 1QC1185 10 10 l 10 3.0 5.4 1.41 C32.h05.402:!11.ti:26 3 e i 131E.*:19.tti-sN s:s i 821 Nc55 163C1292 5.5 l 5.5 3.7 3.0 4.5 1.41 I I I 6 e h339.%585;t31.wole,t<1 164C5359 15.0 e 15.0 : 15.0 3.0 5.4 8 1.41 B21.h32,mc20,sc21,gc23, i ha).s:77 l L i 1 i i ? i A s e 9 e e e e. a 1-1F 1

.--.i , s' "... 1ABLE - 2 Shoreham Nuclear Power Station toistrol Room Panels Class 1E Devices Qualified With Single Axis Malfunction Limits at Least 1.5 Times Expected Acceleration at Mounting Location. u / l Maximum Expected Acen 1EEE-344-1971 ~ MPL GE PPD Dwg # Tested Malfunction Limits Sho ha s f-b s-s y f-b s-s y 5 8 8 l Li'"***$~,[.[41A-5. 272A8270 25 25 25 3.0 2.0 l 1.0 c 5218 5. E31A-5. 8 i 141A 5 272AB272 25 25 l 25 1.0 l 1.2 1.3 I I I i a l 2.0 l 1.6 ts1A-5 272AB274 . 10 10 l*10 2.5 tu A s. tria.s.141 A-5. a 1.0 { 1.2 l 1.3 f. 10 l 10 E*'I 272A8275 10 e s 2.0 { 2.0 (41A-s 272A9052 25 l 25 ~l 25 2.5 The malfunction limits shown are for a chatter detector timing of 10 milisecs. "The max malfunction limit in f-b is the acen this device was subjected to on tested panc) RPS Division B1 & B2' Logic Vertical Board, Lasalle H13-P611. e = 9 e q. 'X Y ,,7-- -M.-

1 M

s.v. -. = _ =.-:.n~n ,,~ ~n. =. SHOREH41 SQRT DRF# A00-992 f[i me l[ d Rev. 1 f, SHOREHAM NUCLEAR 8' 5 i s POWER STATION 4 UNIT 1 1 i e SA) -029-QA-80-PA-B REV 2 h y } SEISMIC QU LIFICATION REEVALUATIO 'I p i i CLASS IE EQUIPMENT t r. -} f f k I 'I Control Roorn Panels r. it e i l ) @/ E. 5. RA".ADAS b l Prepared by: ? 5 W f I. h. April 3. 19a1 t Date: _ ? 3 p I SCIEEE APPLIEATIONS. INC. 1 i Organization. r . UNION BANK BLDG., SUITE 900 [- r n s; 99 ALMADEN BtVD. e I ! i' m. m e<. y m,, r E i 'i [. ( g ? ? 1 ? ,s 6ENER AL $ ELECTRIC J I' _, _.. m tw_ _.. _..-_ _ _,__~ em. O eugg e m em.m _ + Ww - ,w y-_ -A-

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  • s

.. s _1ABLE - 2_ , *,~ i Shoreham Nuclear Power Station Control Room Panels Class 1E Devices Qualified With Single Axis Malfunction Limits at / / Least 1.5 Times Expected Acceleration at Mounting Location. Maximum Expected Accn IEEE-344-1971 at any locaticn on - MPL GE PPD Dwg # Tested Malfunction Limits Shoreham Panels. f-b s-s v f-b s-5 v I i s21t E s21w.r. C71A K e ti1A.K. [21A.E. [218.K. 13683137 8.4 e 11 l 7.5 5 6.5 0.8^ E414.r. [51A-E g ? s 8 I (211 5.921C.s.521A.5 3 e s ] e21H.5.t51A.s 145C3040 20 20 e 20 2.7 8.8 e 5.0 l tila. 145C3041 25 l 25 l*25 2.0 l 1.0 O.5 i e [41.is03 E51.x603 145C3027 15 15 10 1.6 l 1.0 1.0 l 5211.F. 521C.K. B21h K. l 011.r. EllA.K. [51A.x 145C3035 ~25 8 25 25 5 6.5 0.8 l DIA.K 145C3209 12 12 l 12 5 1.2 I 0.8 i UIA-5 159C4282 10 10 I 10 3 3.2 3.2 k E32.h!!D. hif1. h655 h656 nsss.nssi 159C4660 13 l 13 l 13 1.6 1.0 l 1.0 I i 163C1285 8.5 3.0 2.2

  • 0.6 s21 s.z 9.0 !.

8.0 e i s a a [32 8651. Rt52. R65. atie 164C5288 8 l 18 l 7 3.0 1 2.0 1.0 I i i (32.nsai 164C5630 8 8 8 1.6 l 1.0 1.0 f n I I 111A 5. (I1A 5 [41A.5 25 ; 25 2.5 8.8 5.0 234A9327 25 l l '#I*'5' U IA-5 234A9329 25 l 25 l 25 3.0 l 2.0 l 1.6 I l i l. s2in.s 234A9337 25 l 25 ; 25 3.0 2.0 2.0 trix.5 e 2 262A6023 25 i 25 s 25 1.2 i 1.0 1.3 i e ts1A.s 262A6824 25 25 25 1.0 l 1.2 l 1.3 I t I T tila.s 272A8268 25 25 l 25 1.0 1.2 I. 1.3 %%=,,, m., _,__y

m _.. o. '.s SHOREHAM SHIP LOOSE DEVICES QUALIFIE0 BY SINGLE AXIS / SINGLE FREQUENCY TESTING p REMARMS c.EIStitC C APADII.ITY / 11ALFUtlCT10tl Lit 11T (GE REFERENCES) i itAlfE i I DEllT IFIC AT r ott F-B S-S V m 95.0 05.0 05.0 A00-1684-91 l t TEMPER ATI. IRE El EMET lT I 145C32 4 03.0 03.0 03.0 A001084101W - DIFF PRESS TRAt!SMITTER 145C 3249 \\ \\ 1 ??.0 29.0 ?.9. 0 .A001084-141 i 159C4606 03.0 03.0 02.0 e's 101084-150 l t PPESSUPE StilTCH I!!DIC ATOR, PPESSURE 15.H 15.0 l 's. II - II.;- 11, TD17 g Ft.0tl METER 16 3C1107 163C1134 PPESS ItllitCATIllG tS.O 15.0 1 S. li lic.t - 12, T r: 7 t Stl! TCH, t 0.14 10.0 10. t:' f.Il010P 4 - 16?. j t.'3C1185 TP AllStil T TEP, PRESSifGE TR AtlSit! T T ER e DIFF PRESS 93.0 03.0 03'.0 A001084101W ? i S 3C 1164 A001084101W I TP Atistil T T EP, CAGE PRESS 0 3. tl 03.0 03.11 1 3C 154 s:1 15.0 15.0 15.0 A001004-215 163C157 3 St!! T C H. PPESSUPE ~ 164C5359 03.0 03.0 03.0 A001084101W 03.0 03.0 03.0 A001084101W TRAtlSitITTER, ABS PRESS 163C1558 TRAflSHITTER, DIFF PRESS 03.0 03.0 03.0 A001084101W 163C1561 TRANSMITTER, GAGE PRESS 163C1564 e SHEET tilitIDER 1 ! n '.T c.llrt T 5 y}}