ML050060054

Design Change Package 80062466 Revision 1 Extended Power Uprate Piping Vibration Monitoring Installation Package, 10/19/2004

ML050060054
Person / Time
Site:	Hope Creek
Issue date:	10/19/2004
From:	Public Service Electric & Gas Co
To:	Office of Nuclear Reactor Regulation
References
TAC MC5111 80062466 Rev 1
Download: ML050060054 (156)

Text

4LocCY1IO CHANGE NO: REVISION NO.: I FORM 1 ENGINEERING CHANGE COVER SHEET CHANGE PACKAGE TYPE: El ADMINISTRATIVE E EQUIVALENT El TEMPORARY 0DDESIGN El NON-POWER BLOCK FIELD WORK REQUIRE .D? YES Z NO El TITLE: EPU Piping Vibration Monitoring Installation Package STATION/ UNIT: 0 Hope Creek El Salem I E Salem 2 El Salem 3 FI Salem Common El Salem/Hope Creek El Other PSEG Nuclear facility CLASSIFICATIONS:

Important-to-Safety: YES El NO El

[Salem) Q-Listed YES El NO E N/A

[Hope Creek] Q 0 Qs El Qsh E F E R E NIA O REVIEWERSIAPPROVERS: (Type names and dates below, see SAP Operations for Electronic Signature)

RESPONSIBLE ENGINEER REVIEWERICHECKER DESIGN VERIFIER Phil Stashak 8-23-04 J. Annett 10-5-04 R.Vadhar 10-14-04 INTERNAL PACKAGE EXTERNAL PACKAGE PSEG NUCLEAR FINAL APPROVAL APPROVAL ACCEPTANCE REVIEW (Internal packages only) (External packages only) (External packages only)

N/A J.Gorga (0350) J. Bisti (0354) 10-19-04 10-14-04 M.Khan (0352)10-15-04 SORC CHAIRMAN SORC MEETING NUMBER STATION APPROVAL STATION APPROVAL N/A NIA N/A N/A DEPARTMENTISPECIALTY INTERFACE I ALARA (0304) Implementation &Test Welding (0316) Pipe Stress (0300)

Ken Watson 9-20-04 (0308) J. Carey9-20-04 S. Raguseo 9-20-04 P. Stashak 9-24-04 Cable Mgmt (0302)) Electrical (0312) Electric Load Mgmt. OPS (0320))

Paul Finch 10-7-04 Govindh Modi 10-13-04 M. Quadir (0306) T. Macewen 9-2-04

~~-.......... 9-13-04 . ..... -*... . ..

Digital Systems (0310) EPU I&C Digital (0314) Station Planning Engineering Mechanical Paul Beckman 9-29-04 Jim Metro 9-16-04 (0322) Lane Corbett (0318) 9-24-04 WCMP 9-21-04 K.Mathur Page 1 of 68 NC. CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I Discipline / Specialty Interface (cont'd)

HC-NSSS System Engineering (0324)

M. Lazar 9-13-04 AFFECTED DOCUMENT PREPARERS/REVIEWERS DISCIPLINE PREPARER REVIEWER Civil/ Structural (S) Phil Stashak 9-29-04 Bob Mollica 9-29-04 Digital (K) N/A N/A Electrical (E) N/A N/A Instrument & Controls (I) N/A N/A Mechanical (M) N/A N/A Pipe Stressl Supports (H) Phil Stashak 9-29-04 Bob Mollica 9-29-04 Programmatic (P) N/A N/A Page 2 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: 1 FORM 2 ENGINEERING CHANGE TABLE OF CONTENTS Chance Packcage Section Page Number

SUMMARY

(Form 3) 5 DESIGN BASIS/DESIGN BASIS IMPACT (Form 4) 9 DETERMINATION OF EQUIVALENCY (Form 5) N/A AFFECTED DOCUMENTS LIST (ADL) (Form 6) 43 MATERIALS LIST (Form 7) 45 NC.NA-AP.ZZ-0059(Q) REVIEW 51 (Include completed forms from NC.NA-AS.ZZ-0059(Q) as applicable)

LIST ANY SUPPLEMENTAL RECORDS SUBMITTED FOR SCANNING:

Design Input Record (Design & Temporary Changes only)(7 Sheets) - SUP 01 Data Acquisition System (DAS) Description (3 Sheets) - SUP02 Endevco Hardware: Accels, Charge Converter, High Temp. Wire, Signal Conditioner (8 Sheets) SUPO3 Design Considerations Checklist (33 Sheets) - SUP04 Pictogram - Monitoring Locations- Drywell Elevation 77' (1 Sheet) SUP05 Pictogram - Monitoring Locations- Drywell Elevation 100' (1 Sheet) SUP06 Pictogram - Monitoring Locations- Drywell Elevation 112' (1 Sheet) SUP07 Pictogram - Monitoring Locations -Drywell Elevation 121' (1 Sheet) SUP08 Pictogram - Monitoring Locations - Turbine Bldg. Steam Tunnel El. 123' (1 Sheet) SUP09

.Cable- Cable-USA Data.Sheet..(4-Sheets) .... .. . .SUP10.-.

Insulation Data And Insulation Modification Sketches (12 Sheets) SUP1I Accel Direction Pictograms (31 Sheets) SUP12 Accelerometer Strain Gage Functional Locations (2 Sheets) SUP 13 Wiring Block Diagram (3 Sheets) SUP 14 Page 3 of 68 NC.CC-AP.ZZ-0080(cQ, Rev 8

CHANGE NO: 80062466 REVISION NO1.: 1 PMCR (2 Sheets) SUP 15 Penetration Seal Work Release (PSWRs 5326 & 5327) (2 Sheets) SUP 16 Connection & Label Signoff (2 Sheets) SUP 17 Accelerometer Mounting Block Diagram (1 Sheet) SUP 18 Strain Gage General Info (8 Sheets) SUP 19 Strain Gage Installation Instructions (9 Sheets) SUP 20 Page 4 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I FORM 3

SUMMARY

DCP Revision Steam Dryer failures have occurred at several plants due to implementation of Extended Power Uprate (EPU) and the associated increase in steamn flow. To help facilitate the determination of the loads on the steam dryer due to the acoustic wave (pressure pulsations) in the main steam lines, strain gages will be installed on each of the four main steam lines. The acoustic wave (pressure pulsation) is thought by the industry to be a major contributor to the steam dryer cracking that has occurred at EPU power levels in several plants. This DCP was revised to incorporate the addition of strain gages to the Main Steam piping in the Turbine Building. Supplemental Records 13,14,17,19, 20 and the Critical Software Package were revised/added to update/provide strain gage information.

Supplemental Record 18 was added to aid in the Implementation & Test Plan.

Supplemental Record 10 was revised for editorial purposes. Affected Document (AD) H03, and the DIR were also revised to incorporate the strain gage information. The ALARA specialty checklist was revised to provide additional installation "wrench hours". Supplemental Record 11 was revised to incorporate comments. This document was revised in its entirety.

I. Description of Change This Design Change Package (DCP) has been produced as a result of The PSEG Extended Power Uprate Project, in conjunction with General Electric (GE), Task Report T-0318, and ongoing EPU industry issues, defining systems requiring Flow Induced Vibration (FIV) monitoring due to the implementation of the Extended Power Uprate. Piping system monitoring will occur inside the drywell (room 4220), turbine building steam tunnel elevation 123' (room 1405/3491), and in feedwater water heater room 1504 at elevation 137'. The following piping systems will be monitored for FIV; Main Steam (drywell and turbine building), Main Steam Relief Valve Discharge Piping (UJ" & "P "valves discharge), RCIC Steam Supply (inside drywell),

Feedwater (drywell and turbine Building), Extraction Steam, Recirc '(and RHR connections inside drywell). Forty-eight accelerometers at nineteen locations will be monitored in the drywell. Twenty-four accelerometers at ten locations, and twenty strain gages at eight locations will be monitored in the turbine building. The drywell instrumentation will be connected through drywell electrical penetration I BW202, to a cabinet mounted near the "B" side drywell access hatch in the reactor building at elevation 102'. This hardware cabinet was previously installed in DCP 4EC-3186 for the purposes of Recirc vibration monitoring. A Data Acquisition System (DAS) will be fully or partially mounted in this cabinet with the remaining components sitting atop a cart. The DAS will be powered via a convenience outlet when drywell data is to be obtained. Based upon constructability walkdowns, a second DAS setup will sit atop a cart (in lieu of a hardware cabinet), in the turbine building room 4101, near the turbine building steam tunnel at elevation 123'. Cable inside the turbine building Page 5 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I steam tunnel will be routed to this DAS through an existing grouted wall penetration (N-1401-001).

The hardware, software, and dat`aicquisition systems installed in accordance with this DCP are stand-alone systems. Information obtained from the DASs is not input into any permanent plant hardware or software system. Therefore, there is no effect on the Main Steam, RCIC, Feedwater, Extraction Steam, Recirc or RHR System Design Functions from the monitoring of these piping systems.

II. Operational Condition/Mlode required for Implementation This plant must be in an outage in order to implement this DCP. The installation of the vibration monitoring devices and hardware on the piping systems does not compromise the integrity of the systems. However, access to the piping systems, turbine building wall penetration, and containment electrical penetration requires an outage.

III. Technical Specification Action Statements Affected During Implementation There is no effect on the Main Steam, RCIC, Feedwater, Extraction Steam, Recirc or RHR System Design Functions during implementation of this DCP.This modification does not require any changes to the Technical Specifications and complies with statements and requirements of the Technical Specifications.

IV. Implementation and Testing Acceptance Criteria Procedure HC.MD-AP.ZZ-0004(Q) 'General Guidelines For Temporary Power And Communication Cables Installation And Removal" provides a method of installing temporary cable and ensuring personnel and equipment safety. In addition, E-1408 "Wire and Cable Notes and Details provides guidance for installing cable both inside and outside the Drywell.

In accordance with Procedure HC.MD-AP.ZZ-0004(Q) the following guidelines will be adhered to:

• Cable is not to be run in cable trays.

cOne-inch separation is maintained between cable and class 1E conduit.

• No separation required between cable and non-class 1E conduit.

-Cables will be routed off the floor to prevent physical damage and create trip hazards.

eCables will not be routed where water accumulates.

Page 6 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: 1 eCable spans will be restrained to limit swinging during seismic events.

• Cable will be supported using structural steel, support steel, equipment supports, cable trays as long as separation criteria is met. The span of cable between supports should not exceed 10 feet.

• Engineering will conduct walkdowns to ensure supporting requirements and cable separation criteria are met.

In addition to the above, the following installation steps will be followed; In the vicinity of the accelerometer and remote charge converter on the piping, the cable will be banded to the insulation jacketing with stainless steel or aluminum strapping. The strapping material will be matched to the insulation jacketing material.

As a minimum, the cables will be labeled for identification near the remote charge converter, on both sides of the CTMT penetration (for drywell installation), and near the data acquisition systems.

Cables will be supported from structural steel, support steel, equipment supports, cable trays (Non-1 E)with cable straps made of stainless steel in the drywell and tefzel or stainless steel outside the drywell. Raychem may be use as a sleeve for the stainless steel tye-wraps. On the reactor building side of the installation there is non-1 E raceway between the containment penetration and the cabinet / cart installation. Cable will be supported off of this raceway. In the turbine building the cable will be banded to the pipe and then supported off of structural and building steel using unistrut, unistrut clamps, and tie wraps. Separation Criteria is not a requirement in the turbine building All Welding shall be in accordance with the Nuclear Business Unit Welding and Brazing Manual.

Expansion anchor bolts will be used to anchor support structures for cable in the Turbine Building Steam tunnel vestibule. The Cut Rebar & Core Drilling Program (NC.DE-TS.ZZ-4007(Q)) will be adhered to, ensuring that no Rebar is cut w/o engineering approval per the program.

All Endevco Remote Charge Converters, BNC connectors, and BNC Breakouts will be wrapped in Raychem (shrink tubing). Raychem will be used to encapsulate the Endevco Remote Charge Converters, BNC connectors, and BNC Breakouts to preclude the possibility of FME concerns Each accelerometer, before it is screwed into the mounting block will be tested using a handheld shaker. A 1g acceleration at a frequency of 159hz will be applied through the shaker to the accel. This acceleration and frequency will be confirmed at the Digital

.- AqusI Qjffp require tS) on. Once

.AcquisitionSystem (DAS).Different results at the DAS will require troubleshooting the accelerometer (and wiring) is proven to be functional, the accelerometer is torqued to the mounting block and the mounting block tapped (pinged) to ensure the accelerometer and wiring were not damaged when the accel was mounted to the block. Once all the accels on a particular mounting block are proven functional, the "high hat" can be installed over the mounting block and attached securely to the pipe insulation jacketing.

This process is repeated for all mounting blocks.

The strain gages will be spot welded to the Main Steam pipe in the turbine building using a Portable strain gage welding and soldering unit. They are installed per details provided Page 7 of 68 NVC. CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: 1 in Supplemental Record 19, the NBU Welding and Brazing Manual, and calibrated per Supplemental Record 20.

It is important to note that this DCP installs vibration monitoring equipment; instrumentation, cable, accelerometers, and digital acquisition systems to obtain vibration information on specific piping systems. This DCP does not include information pertaining to when the tests will be performed, nor does it provide testing acceptance criteria for the piping being monitored. This information is provided in the Test Plan.

V. Pictogram See Figures 1 thru 7.

III. Training The Data Acquisition System will be operated by trained contract personnel.

However, plant personnel can be trained to operate the system once it has been installed, tested and its performance, verified. Plant personnel were trained on a similar system in support of the recent Recirc/RHR Vibration Monitoring TMOD.

Page 8 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I FORM 4 DESIGN BASIS ANALYSISIDESIGN BASIS IMPACT DESIGN BASIS ANALYSIS & IMPACT:

In 1986 and 1987, in accordance with Regulatory Guide 1.68 (Initial Test Programs -For Water Cooled Nuclear Power Plants) and UFSAR section 14.2, Hope Creek performed a test and startup program. The test and startup program consisted of three phases: the Phase I Construction Verification Test Program, the Phase II Preoperational Test Program, and the Phase III Power Test Program. The Construction Verification Test Program commenced during and immediately following construction. The objective of this program was to verify proper installation of structures, components, and equipment in accordance with design specifications. The program included static and dynamic tests, calibration, initial energization, functional checks, hydrostatic tests, meggering of cables/equipment and flushing or cleaning of oil systems. The Preoperational Test Program (Phase II)began with component / system turnover and terminated with commencement of initial fuel load. It consisted of two parts: the initial system operating phase, and the system and integrated testing phase. During the initial system operating phase all activities including operational energization of systems, run-in of pumps, verification flushing and chemical cleaning of piping, and implementation of programs for preventive maintenance and system layup were performed. During System and Integrated Testing Phase preoperational test procedures on individual and integrated systems were performed, baseline data for inservice inspections were completed, and operating and surveillance procedures were finalized. The Power Test Program - Phase IlIl commenced with the start of nuclear fuel loading and terminated with the completion of power ascension testing. Formal tests, denoted as startup tests, were conducted during this program. These tests confirmed the design basis and demonstrated, that the plant would operate and respond to anticipated transients and postulated accidents as designed. Startup testing was sequenced to ensure that plant safety was not dependent upon the performance of untested structures, systems, or components.

This Design Change Package (DCP) has been produced as a result of The PSEG Extended Power Uprate Project, in conjunction with General Electric (GE), Task Report T-0318, ongoing industry issues, defining systems requiring Flow Induced Vibration (FIV) monitoring due to the implementation of the Extended Power Uprate. This DCP installs instrumentation that will monitor Main Steam (drywell and turbine building), Main Steam Relief Valve Discharge Piping (J &P valves discharge), RCIC Steam Supply (inside drywell), Feedwater (drywell and turbine Building), Extraction Steam, Recirc (and RHR connections inside drywell) piping systems, to verify that the flow induced vibratory levels of the selected piping systems are within acceptable limits for those operating conditions anticipated during service after implementation of the Extended Power Uprate.

Page 9 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I Drywell Monitoring (Room 4220)

The Main Steam, and Feedwater systems are to be monitored because of their significant increases in flow to achieve increases in thermal power. In addition to these systems, the small bore piping attached to the Recirculation (Recirc) suction elbows has experienced numerous vibration-related cracks, since plant startup. The vibration levels have been correlated to specific Recirc pump speeds and Operating Procedures have been revised to limit system operation at those pumps speeds. Work performed within several previous DCPs implemented for the small bore Recirc piping included the addition of tie-back supports to minimize differential pipe movement, and the addition of strain gages and accelerometers to monitor pipe motion. Although the increase in Recirc flow due to the Extended Power Uprate is considered negligible, the Recirc large bore, and connected RHR piping will be included in the FIV monitoring to ensure that small variations in system flow do not produce unacceptable levels of vibration. The RCIC Steam Supply (inside drywell) and MSRV "P" & "J"Discharge piping were chosen to be monitored, because they are branch piping connections of the Main Steam System.

Main Steam, Main Steam Relief Valve Discharge Piping (J & P valves discharge),

RCIC Steam Supply, Feedwater, Recirc and RHR connections will be instrumented with 48 accelerometers. Functional Locations (F-LOCS) were created for each accelerometer. See Supplemental Record 13. Insulation at the monitored large bore piping locations will be temporarily removed. Strapping, banded around the piping and prefabricated accelerometer mounting brackets will be installed at the large bore pipe monitoring locations. The accelerometers will be installed. Then, the insulation will be reinstalled. See Fig.1 and Supplemental Record 11. The weight of the accelerometers and mounting configurations are insignificant in comparison to the weight of the piping being monitored. Therefore, there is no impact on the dynamic response of the piping systems with the monitoring and mounting devices installed. New instrument cables will be routed from the pipe accelerometer locations to containment electrical penetration I BW202. Cable connections at drywell electrical penetration 1BW202 used for previous piping vibration monitoring (DCP 4EC-3186) and TMOD 04-006, will be replaced with the cable connections for this DCP. Cables connected to the Reactor building side of penetration I BW202 are routed to a hardware cabinet near the Containment 'B' side access hatch at elevation 102' (room 4322). This cabinet (10-C-295) was installed as an instrumentation cabinet for Recirc vibration piping monitoring per DCP 4EC-3186. All of the existing pcble will be replaced and connected to a DAS mounted in the cabinet.

Space permitting, the entire Data Acquisition System (DAS) consisting of signal conditioners, amplifiers and a desktop will be mounted in the cabinet. If space is not available inside the cabinet, a cart will be provided. See Fig. 2 for a cart mounted DAS.

The DAS will be powered by a local convenience outlet when drywell data is to be obtained. All carts to be used, will be restrained to meet the seismic 11/I requirement per DE-PS.ZZ-001 1(Q).

Page 10 of 68 NAC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: 1 Drywell Monitoring Information Bldg. I Platform System I Dwg. Line# - Node Pt. No. Of Elevation System Designator _ _ Pipe Material Accels Drywell / 87' Recirc'A' / FSK-P- BB-012-V(D)CA-28' 14 3 BB 169 Stainless Steel Recirc'B' / FSK-P- BB-011-V(D)CA-28" 13 3 BB 170 Stainless Steel Drywell /1 00' Main Steam A l FSK-P- AB-030 - V(D)LA- 81 2 AB 214 26" Carbon Steel Main Steam B / FSK-P- AB-031- V(D)LA-26" 534 2 AB 214 Carbon Steel Main Steam A 1-P- AB-061- GBC-1 0" 22J 2 (SRV 'J") / AB-08 Carbon Steel AB Main Steam B 1-P- AB-065-GBC-10" 40P 3 (SRVup.) /AB-09 Carbon Steel AB Drywell /112' Main Steam A 1-P- FC-003-DBA-4" 430 2 (RCIC) / FC FC-01 Carbon Steel Recirc 'A' (RHR) / 1-P- BB-116-CCA-12" 602 3 BB BC-02 Stainless Steel Recirc 'B' (RHR) / 1-P- BB-114-CCA-20" 506F 3 BB BC-02 Stainless Steel Drywell /121' Main Steam 'A' / AB FSK-P- AB-030 - V(D)LA- 14 2 214 26N Carbon Steel Main Steam 'B' / AB FSK-P- AB-031- V(D)LA-26" 490 2 214 Carbon Steel Main Steam 'B' / AB FSK-P- AB-031- V(D)LA-26" 460 3 214 Carbon Steel Recirc'A' / FSK-P- BB-013-V(D)CA-12" 323 3 BB 169 Stainless Steel Recirc'B' I FSK-P- BB-014-V(D)CA-12" 323 3 BB 170 Stainless Steel Feedwater / 1-P- AE-035- DLA-24" 50 3 AE AE-04 Carbon Steel Feedwater / 1-P- AE-035-DLA-12" 220 2 AE- AE-04-- -Carbon Steel . .

Feedwater / 1-P- AE-035-DLA-12" 280 2 AE AE-04 Carbon Steel Feedwater / 1-P- AE-035-DLA-12" 160 2 AE AE-04 Carbon Steel Feedwater / 1-P- AE-035-DLA-12" Z002 3 AE AE-04 Carbon Steel

. . Total 48 Table 1 Page 11 of 68 NC.CC-AP.Z-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I Turbine Building Monitoring Information Twenty-four accelerometers at ten locations will be monitored in the turbine building.

Main Steam, Feedwater, and Extraction Steam will be monitored at 9 locations in the turbine building steam tunnel rooms 1405 / 3491 Elevation 123'. One location in Feedwater Heater Room 1504 Elevation 123' will be monitored. Functional Locations (F-LOCS) were-created for each accelerometer. See Supplemental Record 13. Insulation at the monitored large bore piping locations will be temporarily removed. Strapping, banded around the piping, and a prefabricated accelerometer mounting bracket, will be installed at the large bore pipe monitoring locations. The accelerometers will be installed. Then, the insulation will be reinstalled. See Fig.1.

In addition, twenty strain gages with protective covers will be installed on all four Main Steam pipes. Two strain gages will be installed in the hoop direction at eight locations on the main steam lines, two locations on each main steam line. In addition, two strain gages will be installed in the longitudinal direction at two locations to measure the amount of bending on the pipe. The insulation at the specified locations will be temporarily removed, the strain gages spot-welded to the pipe, the protective cover slipped over the strain gage, and the insulation reinstalled.

The cable from both Elevation 123' and 137' will be routed to a cart mounted DAS located in the room adjoining the turbine building steam tunnel - room 1401. The cable from the feedwater heater room at elevation 137' can be routed through floor grating located near room 1504 to the DAS on elevation 123'. Cable inside the turbine building steam tunnel will be routed through an existing grouted wall penetration (N-1401-001) to the DAS located in the adjoining room (room 1401).

Page 12 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: 1 Turbine Bldg. Monitoring Information Bldg. 1Floor System / Dwg. Line# - Node No. Of Accels Elevation System Pipe Material Pt. I Strain Designator Gages Turbine / 123' Feedwater/ 1-P-AE-01 AE-013-DBD-24' 731 2 accels AE Carbon Steel Turbine / 137' Feedwater! 1-P-AE-01 AE-013-DBD-24" 817 2 accels AE Carbon Steel Turbine! 123' Main Steam A / 1-P-AB-01 AB-001-DBC-28" Z013 2 accels AB Carbon Steel Main Steam A/ 1-P-AB-01 AB-001-DBC-28" Z018 3 accels AB Carbon Steel Turbine /123' Main Steam B / 1-P-AB-01 AB-002-DBC-28" Z003 2 accels AB Carbon Steel

., Main Steam B / 1-P-AB-01 AB-002-DBC-28" Z008 3 accels AB Carbon Steel R0- 2 11R Turbine/ 123' Extraction Stm 1-P-AC-01 AF-051-GFD-14" 46 2 accels (FWHTR #6A) / Carbon Steel AC (Copper)

Extraction Stm 1-P-AC-01 AF-055-GFD-14" Z010 3 accels (FWHTR #6B) / Carbon AC Steel(Copper)

Extraction Stm 1-P-AC-01 AF-055-GFD-14" 230G 2 accels (FWHTR #6B) / Carbon Steel AC (Copper)

Extraction Stm 1-P-AC-01 AF-059-GFD-14" 471 3 accels (FWHTR #6C) / Carbon Steel AC (Copper)

Turbine / 123' Main Steam A / 1-P-AB-01 AB-001-DBC-28" 233/234 4 strain gages AB Carbon Steel A Main Steam A/ 1-P-AB-01 AB-001-DBC-28" 237/238 2 strain gages AB Carbon Steel Turbine / 123' Main Steam B / 1-P-AB-01 AB-002-DBC-28" 62/64 4 strain gages AB Carbon Steel Main Steam B / 1-P-AB-01 AB-002-DBC 67/68 2 strain gages AB Carbon Steel Turbine / 123' Main Steam C / 1-P-AB-01 AB-003-DBC-28" 582/584 2 strain gages AB Carbon Steel Main Steam C / 1-P-AB-01 AB-003-DBC-28" 587/588 2 strain gages

. AB.--...- . Carbon Steel- - -

Turbine / 123' Main Steam D/ 1-P-AB-01 AB-004-DBC-28" 402/404 2 strain gages AB Carbon Steel Main Steam D / 1-P-AB-01 AB-004-DBC-28" 407/408 2 strain gages AB Carbon Steel Total 44 Table 2 Page 13 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I ECCS Suppression Pool Strainer Blocktage The ECCS is designed to provide protection against postulated loss-of-coolant accidents (LOCAs) caused by ruptures in reactor coolant pressure boundary (RCPB) piping. The ECCS injection network consists of an HPCI system, a core spray system, Automatic Depressurization (ADS) and the Low Pressure Coolant Injection (LPCI) mode of the RHR system. The installation of any commodities within the drywell creates concerns that these commodities can be dislodged, transported to the suppression pool, and clog the.

suppression pool strainers. The clogging of the suppression pool strainers could hinder or disable the ability of the plant to respond to accidents requiring ECCS operation.

Engineering Evaluation H-1-BB-MEE-1168 revision 1 identifies insulation sources inside the drywell and determines the amount of insulation transported to the drywell due to applicable pipe breaks identified in UFSAR Section 3.6. Several High Energy Pipe Breaks were evaluated for insulation damage potential which included; Main Steam, Feedwater, Recirc Suction, Recirc/RHR Line, Recirc Suction riser. Three breaks were chosen for more detailed analysis; Recirc Suction, Feedwater, and Recirc Suction Riser. The following summarizes the results of this analysis provided in Table 8.3.10 of Engineering Evaluation H-1 -BB-MEE-1 168; Recirc suction pipebreak 365.7 ft3 FW Break 244.5 ft3 Recirc Suction Riser 404.5 ft3 This DCP will install approximately 6000 ft. of cable in the drywell. Using a cable OD of 1/4', and assuming that all of the cable is damaged and falls into the wetwell, a total volume of approximately 2 ft3 is added to the wetwell.

The results tabulated in table 8.3.10 reveal that locations and angles relative to the pipe breaks were used as parameters in determining impacted targets (pipe) and damaged insulation. Based upon these values we see that 78% of the insulation damaged below the grating at elevation 100' became wetwell debris, compared to 28% of the insulation damaged above elevation 100'. Most of the insulation damaged above elevation 100' was considered to be screened by the grating. Therefore it is extremely conservative to consider that all of the cable added to the drywell regardless of its location relative to the postulated pipe break locations is delivered to the wetwell. Even with this gross assumption, less -than.2-cubic.feet of.material becomes potential ECCS.strainer.

blockage debris. This is less than a .5%of the wetwell debris calculated for the Recirc Suction riser pipe break scenario. The calculated volume of wetwell debris attributed to the added cable is negligible. No further evaluation is required.

Page 14 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: 1 Electrical General The vibration monitoring equipment wilr be installed in the fall of 2004 (1R1 2) for baseline data acquisition. In the 2006 (1R13) outage the Extended Power Uprate (EPU) will be implemented, and the monitoring equipment will be used during power ascension. The equipment will most likely be removed during the following refueling outage (1R14). See Figures 6 & 7 for typical wiring configurations.

Cable Routing Procedure HC.MD-AP.ZZ-0004(Q) "General Guidelines For Temporary Power And Communication Cables Installation And Removal" provides a method of installing temporary cable and ensuring personnel and equipment safety.

In accordance with Procedure HC.MD-AP.ZZ-0004(Q) the following guidelines will be adhered to:

Cable is not to be run in cable trays.

One-inch separation is maintained between cable and class 1E conduit.

No separation required between cable and non-class IE conduit.

Cables will be routed off the floor to prevent physical damage and create trip hazards.

Cables will not be routed where water accumulates.

Cable spans will be restrained to limit swinging during seismic events.

Cable will be supported using structural steel, support steel, equipment supports, cable trays as long as separation criteria is met.

Alara concepts will be utilized in cable routing per walkdowns performed during last refueling outage and recent mini -outage with installation engineers and Installation personnel.

Engineering will conduct walkdowns to ensure supporting requirements and cable separation criteria is met.

In addition to the above, the following installation steps will be followed; Inthe vicinity of the accelerometer and remote charge converter on the piping, the cable will be banded to the insulation jacketing with stainless steel or aluminum strapping. The strapping material will be matched to the inuslation jacket material.

As a minimum, the cables will be labeled for identification in accordance with E-1412 "Electrical Numbering System" near the remote charge converter, near the CTMT penetration (for drywell installation), and near the data acquisition systems. When data Page 15 of 68 NC CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: 1 is to be obtained, the data acquisition systems (DASs) in the reactor and turbine buildings will be powered by 120 VAC convenience outlets. Data will normally be obtained over 2 minute intervals. When the DAS is not be used it will be unplugged.

Cables will be supported from structural steel, support steel, equipment supports, cable trays with cable straps made of stainless steel or tefzel. A review of primary containment raceway drawings reveals that there are no Class 1E raceways inside primary containment. Class 1E cable is routed in conduit in primary containment.

Therefore, attaching the accelerometer cable to cable tray supports is acceptable and does not violate separation criteria. On the reactor building side of the installation there is non-1 E raceway between the containment penetration and the cabinet / cart installation. Cable will be supported off of this raceway. In the turbine building the cable will be banded to the pipe and then supported off of structural and building steel using unistrut, unistrut clamps, and tie wraps. Separation Criteria is not a requirement in the turbine building.

The Endevco Remote Charge Converter, BNC connector, and BNC Breakout will all be wrapped in shrink tubing. Normally the Endevco Remote Charge Converter is wrapped in a teflon sleeve. The BNC breakout has teflon as an insulator in the connector and PVC is used in the insulation material for the pigtail wires which are 7 inches in length.

The BNC Breakout (Pomona Model # 4970-See Supplemental Record 10) does not meet IEEE 383 or UL910 requirements. However, this part has been used with great success at other nuclear facilities performing similar vibration analysis. Shrink tubing will be used to encapsulate the Endevco Remote Charge Converter, BNC connector, and BNC Breakout to preclude the possibility of FME concerns. In addition, all components installed in this DCP will most likely be removed in refueling outage 1R14.

The majority of cable used is IEEE-383 rated CableUSA 18AWG, 2 conductor with a drain wire rated for 3020F. This cable does not have a radiation rating but has been used successfully at several other nuclear facilities for similar applications.

The High Temperature Endevco Cable 3075M6, used between the Remote Charge Converter and the Accelerometers has a temperature rating in excess of 900 0F. This cable is constructed of a fiberglass jacket over a stainless outer sheath. Both ends of the cable are terminated with a glass-fired connector. Although flame tests have not been performed on this item, the lack of combustible items in the construction of this

..cable, along with its high -temperature-rating assures-compliance with the intent of the UL flame test requirements.

Page 16 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I Containment Penetration 1BW202 In determining the impact of this DCP on the containment penetration two concerns are applicable; type of cable and circuitry (class IE vs. non-class1E) and penetration short circuit analysis.

Type of Cable Containment penetration I BW202 is an l&C penetration with Non-class 1E cables connected to it. None of the accelerometer cables are part of a Class I E circuit.

Therefore we are in compliance with UFSAR section 8.1.14.5 that states non-class 1E circuits are not routed in penetrations containing class IE circuits.

Short Circuit Analysis An evaluation has been performed to ensure the integrity of the containment electrical penetration 1BW202. Calculation 7.13 was reviewed to determine the impact of connecting the wiring for the accelerometer and remote charge converters to Containment Electrical Penetration 1BW202. Calc 7.13 is titled "Penetration Assembly Protection". The piezoelectric accelerometer is a self-generating device that requires no external power source for operation. It is connected to the DAS system through a remote charge converter and uses a high impedance cable. There is an external 18 volt power supply to the remote charge converter which carries milliamps through high impedance cable. These high impedance circuits carry milliamp signals, only. This type of circuit has been addressed in calc 7.13 Section h pages 6 and 7. The section states "...the.

continuous ratings for these penetrations are considerably higher than the maximum short circuit current they may be expected to experience." Therefore, the milliamp circuits installed per this DCP cannot create a short circuit challenge to the penetration. No further evaluation of the penetration is required.

Vibration Monitoring Equipment Data Acquisition System The DAS is a PC Pentium 4 based high speed digital data acquisition system. The system will accept a minimum of 48 channels of analog signals. The input channels are low passed (anti-alias) filtered, then fed into the analog to digital converter (ADC) where each channel -is amplified-and digitized at a rate of 1024 samples per second.per.

channel which provides useable bandwith from 1 to 300 hz. The ADC is a single card installed in the computer. The filters and ADC card are manufactured by National Instruments. The digitized data from the ADC is recorded directly to the hard disk. Data is stored on the hard disk in a binary format to maximize data storage capacity. Each file is time and date stamped and provided with a unique, update file name. After storage to the hard disk, the vibration data can be written to a CD-RW drive. The desktop PC provided with the system will meet the following minimum requirements: Intel Pentium 4, CPU 3.0 GHz, 512 MB RAM, 80 GB hard Drive, 48X Internal CD Rom, internal Page 17 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I 16x10x40x CD-RW drive, 3.5" Floppy, mouse, keyboard, 17" SVGA Monitor with 1024 x 768 resolution. The operating system is Windows 2000 Professional. The VDAS software is based on National Instrument's Lab view graphical interface software that provides virtual instrument to acquire, real time process and store high-speed digital data.

All operations are mouse controlled. Any two channels of data may be selected and observed on the monitor in real time as time history or frequency spectrum with both root-mean-square and maximum and minimum values indicated. After two minutes of recording, the system stops recording. The file is identified by the file name, which includes a date and time stamp. Also, a description of the test is entered form the keyboard. Along with the data file is a text file with all the VDAS settings (gain, conversion factors, sample rate, number of channels). At the end of the test the operator transfers the data to the CD drive for permanent storage. Data analysis is performed after the test. The root mean square (rms) values for each acceleromdter channel for each test condition are extracted from the recorded data. The rms values are printed out in a spreadsheet along with the acceptance criteria and a ratio of the rms to the acceptance criteria. The spreadsheet is labeled with the test condition, time and date of the test.

Remote Char-ie Converter (RCC) (Endevco Model 2771B-1)

The two ounce stainless steel encased device transforms a high impedance charge output, such as a signal from a high temperature piezoelectric accelerometer, into a low impedance voltage proportional to the transducer' charge. The RCC is powered by the constant current source inside the signal conditioner. Allowable operating range for this unit is -400F to 2120 F . The unit can operate up to 95% relative humidity and can handle radiation fields up to 1 x 10 E6 rads integrated gamma. The HCGS Environmental Design Criteria D7.5 Table 1(Drywell) lists the maximum temperature of the drywell as 150 0F, the humidity is 90% and the radiation field is 2.3E7rads/40 years. The HCGS Environmental Design Criteria D7.5 Table 6 (turbine building steam tunnel rooms 1405/3491 lists the maximum temperature 1300F, the humidity is 90% and the radiation field is 3.5E6rads/40 years. The RCC is typically provided with a Teflon sleeve. For this application, since Teflon is restricted, the RCC will be encased with a Raychem Sleeve configuration in lieu of the Teflon sleeve. The remote charge converter is strapped to the bracket or pipe insulation within 12 feet of the accelerometer such that there is no

-relative displacement between the accelerometer and the charge-converter. The accelerometer operates in a charge mode and produces picocoulcombs (PcCbs) proportional to the acceleration. The RCC converts the PcCbs to volts. While in the charge mode the accelerometer lead cable is sensitive to relative motion (produces charge) and the cable capacitance is a factor in the noise calculation (longer cable between accel and RCC creates more capacitance and higher noise). The best practice is to keep the accelerometer lead short and tied down. Also the lead is a special type of coaxial cable (in this case Endevco High temperature cable assemblies Model #

Page 18 of 68 NCCC-AP.ZZ-0080(QJ, Rev 8

CHANGE NO: 80062466 REVISION NO.: I 3075M6) that minimizes capacitance and charge creation and is generally not long.

Between the RCC and the DAS, the cable is insensitive to noise and motion.

Signal Conditioner (Endevco Model 2793)

The signal conditioning device provides an I 8VDC, 4-1 OmA bias power to each charge converter and receives the Vibra"ation signal from the accelerometers, The unit provides DC Power to the RCC and performs no amplification, integration or filtering. The shield for the entire cable from charge converter to DAS will be grounded only at the DAS. The signal conditioners are installed in the cabinet or cart in the Reactor Building (room 4322) and Turbine Building room 1401.

Accelerometers (Endevco Model 7703A-100).

The accelerometers weigh 1 ounce and have a stainless steel case. The temperature measurement range is -670 F to 550 0F. The unit is hermetically sealed with the signal return isolated for the case. The unit can operate at 100% relative humidity and can handle radiation fields up to 1OEB rad integrated gamma flux. The unit response is directional along the axis of the mounting stud, so the mounting arrangement, and number of accelerometers, depends on the piping location needs. Piezoelectric accelerometers are light compact sensors that measure vibration using a mass mounted on a piezoelectric crystal. The output is proportional to acceleration input and is low so it requires a charge amplifier in the lead. Higher temperature applications require an additional charge amplifier. The accelerometers meet the environmental requirements, have prior success in BWR operating environments and are adequate to obtain the required information.

Page 19 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I Fire Protection The overall HCGS fire protection program is based on the evaluation of potential fire hazards throughout the plant and on the effects of postulated fires on the performance of safe shutdown functions. Consistent with other safety requirements, systems, structures, and components, including those required for safe shutdown are designed and located to minimize the probability and effect of fires. The Auxiliary Building, Reactor building, and Turbine building are separated from each other by 3-hour fire walls. Redundant safety related components are separated form each other and the rest of the plant by 3-hour fire barriers, and or separated by 20 feet. The following is a list of designated Fire areas per Fire Area drawings M-5004, M-5114, and M-5115 for rooms where cable and monitoring equipment is added per this DCP; drywell room 4220 (RB7), reactor building room 4322 (RB2), turbine building rooms 1401(TBI),

1405/3491(TB1), and 1504(TB1).

Although we are adding cable to the drywell and safety related equipment is prevalent throughout the drywell, no fire hazards analysis is performed for the drywell per Table 9A-1 " Fire Hazards Analysis". The drywell is inerted during operation, making a fire impossible. The main concern for fire inside the drywell occurs during refueling and maintenance operations. During refueling and maintenance operations in the drywell, portable fire extinguishers, in addition to the hose stations, are adjacent to the work area and readily available for use by plant personnel. Self-contained breathing apparatus is provided near the containment entrances for firefighting personnel. Therefore, no further analysis of the drywell for implementation of this DCP is required.

The DAS located in room 4322 (Reactor Building) consists of a metal cart, if required, (non combustibles) and combustibles which include; a desktop computer, and an assumed amount of paper, pencils, and nearby reference materials. An assumption is that the equipment will add approximately 50 pounds of combustible plastic to the room.

It is also assumed that paper, pencils, and reference materials will add an additional 25 pounds of combustible material to the room. This DCP will install DAS equipment in a reactor building cabinet installed for DCP 4EC-3186 and later abandoned. The cabinet was recently reused for DAS equipment in TMOD 04-006. A review of the DAS components shows that the weight assumptions for combustibles used for DCP 4EC-3186 were conservative. Therefore the weight of combustible commodities listed in Table 9A-1 " Fire Hazards Analysis" and stored in Room 4322 is still acceptable. No changes are-required to Table 9A-9 "Fire Hazards Analysis Tabulation"-for Fire Area RB2 page 1 of 27 or Room 4322 page 25 of 27. Therefore, no further fire hazards analysis of the reactor building room 4322 for implementation of this DCP is required.

Page 20 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I Cables will be added to Turbine Building Rooms 1401, 1405/3491 and 1504. A second DAS sitting atop a cart will be stored in room 1401. Per Fire Area Drawings M-5115, these rooms are designated as Fire Area TB1. No safety related equipment exists in any of these rooms. These rooms are not listed in Table 9A-4 "Fire Areas and Associated Room Numbers" and Table 9A-1 "Fire Hazards Analysis Summary".

Therefore, no Fire Hazards Analysis is required for installation of the cable and/or monitoring equipment in these rooms.

Penetration Seal The cables for the accelerometers in the Turbine Building Steam Tunnel (room 1405) will be routed through penetration seal N-1401-001 to a DAS mounted on a cart in adjacent room 1401. Penetration Seal N-1401-001 is listed as a 3-hour fire seal. The grouted seal will be partially removed, conduit inserted, and cable routed through the conduit. The seal will be regrouted and the conduit sealed with foam in accordance with Penetration Seal Work Release Nos. 5326 & 5327(see Supplemental Record No. 16).

Therefore, restoring the penetration seal to its 3-hour fire rating.

Insulation The Main Steam, RCIC (inside drywell), Feedwater, Recirculation (attached RHR) and Extraction Steam piping will be instrumented with a total of 72 accelerometers at 29 locations. Insulation at the monitored bore piping locations will be temporarily removed.

Strapping, banded around the piping and prefabricated accelerometer mounting brackets will be installed at the large bore pipe monitoring locations. The accelerometer(s) will be installed. Then, the insulation will be reinstalled. Supplemental Record 11 depicts the manner in which the insulation will be reconfigured for each size pipe OD, insulation thickness, and insulation jacket material. The insulation and jacket materials will be reconfigured with "high-hat" designs that will allow for the space occupied by the mounting blocks and accelerometers, and at the same time restore the insulation and jacketing to their original insulating performance. Therefore, environmental room temperatures where the accelerometers are mounted on the piping are not affected.

In addition, twenty strain gages with protective covers will be installed on all four Main Steam pipes. Two strain gages will be installed in the hoop direction at eight locations on the main steam lines, two locations on each main steam line. In addition, two strain gages will be installed in the longitudinal direction at two locations to measure the amount of bending on the pipe. The strain gages are approximately 1" long and .35" in width. The strain gage covers are approximately 1/8" in height. The insulation at the specified locations will be temporarily removed, the strain gages spot-welded to the pipe, the protective cover slipped over the strain gage, and the insulation reinstalled.

Since the insulation where the strain gages are to be installed is rigid insulation (Main Steam Piping, Turbine Building, 3 1/2" thick) the insulation in the region of the strain Page 21 of 68 NC.CC-AP.ZZ-0080(Q, Rev 8

CHANGE NO: 80062466 REVISION NO.: I gages will be required to be notched. A maximum of Yz" in height over an area of 12" in length and 10" in width will be notched to allow for installation of the strain gages and covers. The volume of insulation to be removed at each of the 8 locations (approximately 60 cubic inches over an area of 12 inches in length) is negligible, compared to the exisitng 4156 cubic inches of insulation per foot of pipe. Since the performance of the insulation is directly related to the amount of insulation on the pipe, the 1.5% reduction in volume of insulation for 1 foot of pipe at 8 locations will have no impact on environmental room temperatures where the strain gages are installed. For all practical purposes, there is no reduction in performance of the insulation where the strain gages are installed.

Page 22 of 68 NC.CC-AP.ZZ-0080(0. Rev 8

CHANGE NO: 80062466 REVISION NO.: I Pipe Stress A modal analysis was performed on the as-modeled piping system to determine natural frequencies and mode shapes. The sensor (accelerometers) locations were determined based on a review of the mode shapes. The accelerometer locations correspond to node points with high-calculated modal displacements. Other factors used to determine accelerometer locations were; installation accessibility including ALARA concerns, minimizing the impact to insulation, and redundancy of accelerometers.

The static loads such as weight and thermal expansion were not considered since these loads do not contribute to the steady-state vibration of the piping system. Additionally, seismic and relief valve loads, inertia and anchor movements are not considered since these loads are transient dynamic loads and do not contribute to the steady state vibration loads. Each sensor will measure the acceleration in one direction. The directions were selected on the results of the modal analysis. The lower modes of a piping system typically govern the response. The directions were selected to coincide with locations of high response and the maximum modal displacement.

To reduce installation time, the accelerometers will be located as low as reasonably possible to minimize scaffolding. Additionally the accelerometers that measure different directions will be grouped at each location to minimize the mounting block locations. At least two accelerometers will be used to measure vibration in each direction on the main run of pipe.

The mounting block configuration, with accelerometers, high temperature wire, and remote charge converter are typically banded to the piping as shown in Fig. 1. The weight of the accelerometers, remote charge converters and mounting block for any monitored location is less than 3.5 lbs, total. This weight is insignificant to the lbs/ft of the pipe being monitored. The weights of the mounting hardware and monitoring devices will have no impact on the adjacent pipe supports. In addition, the weights of the mounting hardware and monitoring devices (including insulation "high hats" ) will have no impact on the dynamic effects of the piping they are monitoring. Therefore, the results obtained with the monitoring devices and hardware installed on the piping, are still valid for the piping when the monitoring devices and hardware are later removed.

Twenty strain gages will be installed on the Main Steam piping (two strain gages at six locations and four strain gages at two locations) in the Turbine Building. The strain gges'will 'be usedto rreasure the marriitude of the acoustic wave (pressure pulsation)'

thought by the industry to be a major contributor to the steam-dryer cracking that has occurred at EPU Power Levels in several plants. The strain gage and protective cover weigh a few ounces. There is no impact to pipe stresses or the dynamic response of the piping due to the addition of the strain gages and covers.

Page 23 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I The following table summarizes the PSEG stress calculations with monitored piping, and the corresponding vendor technical documents that document the monitoring locations.

PSEG Calculation I Revision Calculation Description Vendor Technical Document C-0141 / 10, C-0142 /10 Recirc Loop A + RHR, Recirc Loop B + 326528 RHR, C-0120 / 8 Feedwater Inside Drywell 326529 C-1921 / 11 Feedwater Outside Drywell 326530 C-1011 /7 Extraction Steam Piping To FWHTR# 6 326527 C-0010/8 Main Steam Outside Drywell 326531 C-0122/8 Main Steam Line 'A' Inside Drywell, 326532 Including SRVs A,J,R C-0121 /7 Main Steam Line 'B' Inside Drywell, 326533 Including SRVs B,K,F,P Table 3 Seismic l1/I This DCP installs vibration monitoring equipment in the Containment, Reactor and Turbine buildings. The vibration monitoring equipment consists of accelerometers inserted in mounting brackets banded to the pipe. Each accelerometer requires a remote charge converter which will be banded to the outside of the insulation jacketing near the accelerometer. See Figurel. Each cable will be routed from an accelerometer / remote charge converter to its data acquisition systems using the guidelines found in Procedure HC.MD-AP.ZZ-0004(Q) "General Guidelines For Temporary Power And Communication Cables Installation And ReimivalI". Th&6e bIe wiill be banded to the pipe and then tied 'off to structural steel, support steel, equipment supports, cable trays (non-1 E) with cable straps made of stainless steel or tefzel, as long as separation criteria is met. The cabinet used in the reactor building (room 4322, fig.3) for mounting the DAS equipment was evaluated in DCP 4EC-3186 and again used in T-Mod 04-006 for mounting Recirc vibration monitoring equipment. The conclusions that the cabinet anchorages are adequate for our DAS equipment was confirmed by a review of the DCP 4EC-3186 evaluation. A review for weight added with 100% of our equipment stored in the cabinet was compared to assumptions Page 24 of 68 NC.CC-AP.ZZ-0080(QJ, Rev 8

CHANGE NO: 80062466 REVISION NO.: I made for the 4EC-3186 evaluation. The weights of our components are enveloped by the previous evaluation. If adequate space is not available inside the cabinet for all of the equipment, a cart will be used for additional storage. See Fig. 2 for a cart mounted DAS.

A second DAS setup will sit atop a cart (in lieu of a hardware cabinet), in the turbine building room 4101 (see fig. 4), near the turbine building steam tunnel at elevation 123'.

All carts to be used, will be restrained lAW NC.CC-AP.ZZ-0011(Q) to meet the seismic Il/I requirement per DE-PS.ZZ-001 (Q).

DAS Software Package The quality assurance for the project software is documented following the guidelines of PSEG Procedures "Software Quality Assurance" NC.NA-AP.ZZ-0064(Q) Rev.2, and PSEG Procedure "Software Life Cycle Planning & Implementation" NC.IN-AP.ZZ-1000 Rev. 0. In accordance with NC.NA-AP.ZZ-0064(Q) Rev.2 Attachment 1,the software is classified as Level B. Level B software is software that "Indirectly Effects Nuclear Safety." Level B is defined as "Those applications important to compliance with regulatory requirements, commitments or required by law, and whose failure to operate as expected may have an indirect impact on nuclear safety, individual safety or other requirements / laws.' The applicable Software Quality Assurance (SQA) Elements of NC.NA-AP.ZZ-0064(Q) Rev.2 Attachment 2 are discussed in Structural Integrity Calc HC-04Q-109-001. The following SQA Elements are applicable; Configuration Of Custom Software, Testing Of Software, Error Notifications Following Delivery, Documentation, Training, and Records. In accordance with the requirements of NC.IN-AP.ZZ-1000(Q) Rev.0 "Software Life Cycle Planning & Implementation", Software Requirements Specification (SRS) and System Design Description (SDD) are addressed in Structural Integrity Calculations HC-04Q-1 09-002 and HC-04Q-1 09-003.

Structural Integrity Calculations HC-04Q-109-001('Project-Specific QA Plan For Software Testing"), HC-04Q-109-002 ("Project-Specific Software Requirements Specification And Software Requirements Review") and HC-04Q-109-003 ("Project-Specific Software Design Description") are located in the PSEG Document Management System as Critical Software Package H-1-ZZ-SCS-0253 (ADS01). The Critical Software Package is divided into several volumes (sections) as listed below; Volume I - Software Index Form Volume 2 - Software Requirements Specification Volume 3 - Software Design Description Volume 4 - QA Plan for software testing Volume 5 - System Backup Volume 6 - System Manuals Volume 7 -Test Implementation and Configuration Files Volume 8 - Harware Components CE Certificates Page 25 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: 1 The following is a summary from the volumes of the Critical Software Package; Volume 2 - Software Requirements Specification The software shall run on Windows XP Professional operating system. The software shall include the following features:

• Accommodate two separate sets of transducer signals

• Read-in acquisition parameters from setup files

• Read-in transducer sensitivities and charge converter gains from setup

• Read-in allowable vibration levels from setup files

• Display simultaneously signals from any two channels either in time history or frequency spectrum format in engineering units

• Calculate and display in real time maximum, minimum and RMS values for two displayed channels

• Acquire simultaneously signals from up to 64 transducers in engineering units

• Acquisition duration shall be controlled by the operator

• Calculate the ratio of the acquired vibration signal vs. the allowable

• Produce a results file

• Produce a setup documentation file Volume Software Design Description The software requirements specified in Reference 4 shall be designed as follows:

• An input screen shall be created to allow the operator to specify the location of the transducer set. Selections shall be Drywell and Turbine Building

• An input screen shall be created to display the acquisition parameters that are read-in from the ' Config General.txt' and '** Config Channels.txt' files, where "is either DW (Drywell) or TB (Turbine Building). The acquisition parameters are: sampling rate, channel address, channel input limits, number of channels, and high and low frequency bound defining the analysis band of interest

• An input screen shall be created to display the transducer sensitivities and charge converter gains that are read-in from the ' Config CF and Allowable.txt' file, where "**Sis either DW.(Drywell) or TB (Turbine Building).

• An input screen shall be created to display the allowable vibration levels that are read-in from the '** Config CF and Allowable.txt' file, where '**' is either DW (Drywell) or TB (Turbine Building).

• All configuration files shall be adequately controlled. They shall be setup during the system installation, tested, and controlled as a critical software document.

Only a trained operator or an otherwise authorized user shall be permitted to alter its content.

• An acquisition screen shall be created capable of simultaneously displaying Page 26 of 68 NC.CC-AP.ZZ-0080(Q). Rev 8

CHANGE NO: 80062466 REVISION NO.: I signals from any two channels. A toggle switch shall be included to allow the operator to choose between time history or frequency spectrum format. All data shall be shown in engineering units.

• The software shall automatically calculate the maximum, minimum and RMS values of the streaming data for the two displayed channels. Displays for the calculated values shall be included on the acquisition screen.

• The software shall be able to simultaneously acquire signals from up to 64 transducers. The data shall be recorded in engineering units and stored to the computer hard drive. The data file naming shall be automatic and the name shall be the year, date and time of the file creation (yyyymmddhhmmss). The data file extension shall be dta. The data file format shall be binary.

• Acquisition duration shall be controlled by the operator. Control dial for acquisition duration shall be included on the acquisition screen. Acquisition shall be initiated by the operator. Initiation button shall be included on the acquisition screen. Acquisition termination shall happen automatically.

• Upon termination of acquisition, the software shall automatically calculate an RMS value for the specified frequency band for all recorded channels. Further, the software shall automatically calculate the ratio between the calculated RMS and the allowable vibration RMS.

• A results file shall automatically be created. The file shall contain tabulated listing of all recorded channels, their calculated RMS values, the allowable RMS value for each channel, the ratio between the calculated and allowable RMS, and an OK/Exceeds flag. The results file extension shall be res. The results file format shall be ASCII.

• A setup file shall automatically be created. The file shall contain tabulated listing of all the acquisition parameters, the transducer sensitivities and the charge converter gains, and the allowable vibration levels. The setup file extension shall be set. The setup file format shall be ASCII.

Volume QA Responsibilities SI responsibilities are:

1. Configuration of custom software

2. Testing of software

3. Error notifications following delivery

4. Documentation

5. Training

6. Records The above responsibilities are discussed in more detail, below. All other responsibilities, following delivery, are at the discretion of PSEG.

Configuration - SI will assemble a custom system for PSEG, per contract 4500226359 including Change Order 1.The system configuration is defined by the functional specifications of the system, provided in Appendix A.

Page 27 of 68 NC.CC-AP.ZZ-0080(QJ. Rev 8

CHANGE NO: 80062466 REVISION NO.: I Validation and Testing - The technical description, and test results for the delivered software will be provided in Si caic HC-04Q-301, to be included in the system documentation package. This document will also identify the project manager, the performer and the validation checker of the software. The validation and testing of the software will be done in accordance with Section 5.5 of Reference 2.

Error Notification - SI will provide error notification to PSEG for a period of years, from the date of delivery. An extension may be negotiated, if needed.

Additionally, Si will notify PSEG of future upgrades, as applicable. This will be done in accordance with Section 5.10 of Reference 2.

Training - SI will train PSEG personnel on the installation and operation of the system, per the terms of the contract. This will be done in accordance with the Section 5.6 of the Reference 2.

Documentation - The documentation provided will include Software Requirements Specification (SRS) and Software Requirements Review (SRR) as specified in Section 4.9 of Reference 2, Software Design Description (SDD) as specified in Section 4.10 of Reference 2, procedure to run the software and the validation test package.

Records -All Si records pertaining to this activity will be retained in the SI project records, per the SI QA Program. The records will be transmitted to PSEG upon request, or discarded after 2 years following the closure of this project, and upon notification to PSEG. This will be done in accordance with Section 6.1 of Reference 2.

Volume 5 -SVstem Backup Data is initially collected to a computers hard drive. This data is then copied onto a CDROM for backup and use on other computers. Only the data files need to be backed up as everything else can be recreated by reinstallation.

Volume 6 - Svstem Manuals Before the data can be acquired, the user must go through all of the set-up screens (Define General Parameters, Define Conversion Factors, Define Allowable Vibration Levels) review the set-up variables and reenter values that require to be changed.

Some of the General Parameters that are checked are; sampling rate, number of channels, and bandpass filter frequency. A review of the transducer sensitivities and Page 28 of 68 NC.CC-AP.ZZ-0080(Q0,Rev 8

CHANGE NO: 80062466 REVISION NO.: I charge converter gains is part of the "Define Conversion Factors" review. The files that are generated for each test are stamped with a file name and extension.

Volume 7-Test Plan

.A 15MHz functionlarbitrary waveform generator will be used to test the software. The specific one used is an Agilent model 33120A. This device was calibrated on 03/30/2004 and the calibration sheet is included in Appendix A. The Agilent 33120A is shown in Figure 1.

The VDAS HC software will be tested using the following steps:

Step 1:

Verify that two distinct sets of transducer signals can be accommodated. This includes the verification that configuration files are read in for acquisition parameters, transducer sensitivities, charge converter gains, and allowable vibration levels. Table 1 outlines the configuration files created for this verification. All the configuration files listed in Table 1 are included in Appendix A.

DW Config CF and allowable.txt This file defines parameters for 64 locations. Each location is assigned a value of 100 for sensitivity, 1 for gain, 1 for allowable, and g for units. These values should be correctly displayed in the "HC Setcon.vi" window after selecting "Drywell" in the "HC Location.vi" window. In addition, the allowable level should be correctly displayed in the "HC Setallow.vi" window.

DW Config general. txt This file defines parameters for 64 channels. This file gives a value of 1024 samples per second, 8 for number of modules, I for the low frequency cutoff, and 160 for the high frequency cutoff. These parameters apply to all channels. These values should be correctly displayed in the "HC Setgenrl.vi" window after selecting "Drywell" in the "HC Location.vi" window.

DW Config channels.txt This file defines the input limits for each of the 8 modules (There are eight channels per module). This file gives a value of 0.5 and -0.5 for the high and low input limits for all modules. These values should be correctly displayed in the "HC Setgenrl.vi" window after-selecting '¶Drywell".in-the "HC.Location.vi" window.

TB Config CF and allowable.txt This file defines parameters for 34 locations. Each location is assigned a value of 100 for sensitivity, 1for gain, I for allowable, and g for units. These values should be correctly displayed in the "HC Setcon.vi" window after selecting "Turbine Building" in the "HC Location.vi" window. In addition, the allowable level should be correctly displayed in the "HC Setallow.vi" window.

Page 29 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I TB Config general.txt This file defines parameters for 34 channels. This file gives a value of 1024 samples persecond, 3 for number of modules, 1 for the low frequency cutoff, and 160 for the high frequency cutoff. These parameters apply to all channels. These values should be correctly displayed in the "HC Setgenrl.vi" window after selecting "Turbine Building" in the "HO Location.vi" window.

TB Config channels.txt This file defines the input limits for each of the 3 modules (There are eight channels per module). This file gives a value of 0.5 and -0.5 for the high and low input limits for all modules. These values should be correctly displayed in the "HC Setgenrl.vi" window after selecting "Turbine Building" in the "HC Location.vi" window.

Step 2:

Verify that two distinct signals can be displayed in the "HO Test.vi" window. Also verify that these signals can be displayed in time history or frequency spectrum format in engineering units. In addition, verify that the maximum, minimum, and RMS values are displayed and correct. The RMS value is simply 0.707 times the amplitude for this test.

The maximum and minimums correspond to positive and negative values of the input amplitude. For the strain gage channels, verify that the steady state condition in the Wheatstone Bridge can be adjusted to near 0 gs value and verify that the shunt calibration test yields a difference of 175gs i 10% with and without shunt resistor attached.

Step 3:

The last verification involves actual data taken by the program. The results file should contain 64 channels of data for the Drywell and 34 channels of data for the turbine building. The duration of the data acquisition should be equivalent to that specified by the user in the "HC Test.vi" window. Also verify that the results file contains the ratio of the acquired vibration signal to the allowable. In addition to the results file, a setup documentation file should be produced that corresponds to the data taken.

Failure Analysis Procedure ND.DE-TS.ZZ-5503(Q) requires .a.failure analysis .to be performed on digital systems being installed. A component level failure analysis is not required, but a system level failure analysis is required. A typical failure analysis should contain:

• Identification of system level failures

• Potential causes of system failures

• Assessment of the significance of failures (likelihood/consequences)

• Identification of resolution Page 30 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: 1

1) Identification of system level failures For the purposes of this analysis, the system level failures can be categorized as a signal failure (e.g., accelerometers, remote charge converters, strain gages, cabling) or as a computer failure. Since similar systems to this one have been in service at Hope Creek and other facilities (i.e., this is somewhat of a mature system), it is assumed that system level failures are identifiable. That is, either a failure causes a complete loss of a signal or of the entire system, or itfails in such a way that a trained system operator can identify the difference between good signals and bad signals.

2) Potential causes Signal failures can be caused by such things as individual component failure (as stated earlier, these need not be evaluated in detail), inadvertent cabling cuts, radiation effects, electromagnetic interference, and grounding problems. Computer failures can be caused by hardware or software failures.

3) Failure significance Ifa channel or the entire system fails, most components can be replaced, because the data acquisition systems are located in low radiation areas, in locations easy to access. The following is a discussion on selection of monitoring locations and component failure for the Drywell (Ctmt) and Turbine Building.

Drywell Accelerometers The main steam and feedwater accelerometer locations and directions were determined by performing a modal analysis of each line and selecting locations that are accessible, minimized ALARA, and are expected to have a dynamic response.

For redundancy, accelerometers were located such that at least two different locations are measuring the same direction. For example, on the feedwater system, the Z-direction vibration is monitored with 3 accelerometers at three different locations. So ifthe signal from one of the Z-direction accelerometers is bad, the

.-. remaining two Z-direction accelerometers can be used to.determine the-response in the Z-direction. Inthe unlikely event that all the accelerometers for a particular direction fails (e.g., X-direction on main steam line B), the remaining accelerometers in the other two directions plus the vibration measurements from the other main steam lines, and the dynamic analysis results of the piping can be used to infer the structural adequacy of the piping system with failed accelerometers due to steady state vibration. The recirculation piping accelerometer locations were selected based on previous evaluations and vibration issues that have occurred on this system. Similar to the main steam and feedwater piping systems, there are at least Page 31 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I two accelerometers for each direction. In addition, both recirculation loops are monitored at similar locations to aid in comparisons between the two loops. In the event that the sensors at one location fail, there is sufficient redundancy in the other locations and directions to still have the capability to assess the vibration of the piping systems.

Table 1 of the DCP summarizes the drywell accelerometers by direction for the main steam, feedwater, and recirculation piping. The total number of accelerometers is 10 on the main steam line A, 8 on main steam line B, 12 on the feedwater piping, and 18 on the recirculation piping system. A review of Table I shows that for each pipe line, each direction is monitored using a minimum of 2 accelerometers. Thus, there is sufficient redundancy in the direction and number of accelerometers to accommodate failures and still maintain the ability to assess the structural adequacy of the piping system due to steady state vibration.

Turbine Building Accelerometers Similar to the drywell accelerometers, the locations and number of accelerometers in the turbine building were determined based on performing a modal analysis of the main steam, feedwater, and extraction steam piping system. The routing of the main steam, feedwater, and extraction steam piping inside the turbine building is simple (straight runs of pipe) as compared to the pipe routing inside the drywell that contains curved pipe and branch piping (SRV discharge lines). The accelerometer locations on the main steam, feedwater, and extraction steam piping are readily accessible and the cabling from the accelerometers to the VDAS does not require the electrical connections at the primary containment penetration that are needed for the drywell accelerometers. The cabling can be routed directly from the accelerometer/remote charge converter (RCC) to the VDAS all located inside the turbine building.

Table 2 of the DCP summarizes the turbine building accelerometers by direction for each of the monitored piping systems. The total number of accelerometers is 10 on the main steam piping, 4 on the feedwater piping, and 10 on the extraction steam piping. Due to the similar piping routing of the four main steam lines, only two of the four are monitored. Between the two monitored main steam lines, at least two accelerometers are used to monitor each direction. The feedwater line does not have the same amount of redundancy in the X and Z-directions; this is due to the low expected dynamic-response of the piping system in these-directions. The structural adequacy of the feedwater piping could still be determined if failures of either of these directions occurred due to the remaining accelerometers and the piping analysis results. The configuration of the extraction steam system is not symmetric so additional locations were selected to be able to capture the dynamic response of the piping system. Due to the number of accelerometers on the extraction steam system, there is sufficient redundancy in directions such that failure of accelerometer signals would not compromise the ability to assess the response of the piping due to steady state vibration.

Page 32 of 68 NC.CC-AAZZ-0080(QJ, Rev 8

CHANGE NO: 80062466 REVISION NO.: I Strain Gaqes Steam dryers failures have occurred at a couple of plants due to implementation of Extended Power Uprate (EPU) and the associated increase in steam flow. To help facilitate the determination of the loads on the steam dryer due to the acoustic wave (pressure pulsations) in the main steam lines, strain gages will be installed on each of the four main steam lines. The acoustic wave (pressure pulsation) is thought by the industry to be a major contributor to the steam dryer cracking that has occurred at EPU power levels in several plants.

Two strain gages will be installed inthe hoop direction at eight locations on the main steam lines, two locations on each main steam line. In addition, two strain gages will be installed in the longitudinal direction at two locations to measure the amount of bending on the pipe. Two strain gages are used to increase the resolution of the signal, which is expected to be small (-1 pw). Ifone of the two strain gages were to fail, the remaining strain gage can still be used to measure the strain and determine.

the pressure pulsation in the main steam line. Strain gages will be installed at two locations on each main steam line to determine the attenuation of the pressure pulsation in the main steam line. If both strain gages were to fail at one location, the remaining strain gages on the other main steam lines can be used to determine the magnitude of the pressure pulsation in the main steam lines. As a minimum, there should be at least one set of strain gages on one main steam line that do not fail to be able to assess the pressure pulsation.

If the computer system fails, power increases could be restricted until the failure is repaired. The likelihood of a computer failure could be low to high, based on how long this system stays in operation in the plant. The likelihood of computer failure will increase if the system is used for several years.

The worst-case failures would be the failure of multiple vibration signals in a location that cannot be accessed at power, resulting in a restriction of increasing power. If it is determined that the accelerometers, remote charge converters or strain gages are the cause of the failure, and it is impossible to replace these components due to limited access, the impact of the loss of this data at the location will be reviewed on a case-by case basis;---There is sufficient redundancy to allow-accelerometer failures and still be able to assess the structural adequacy of the piping systems due to steady state vibration. Similar to the accelerometer installation, there is sufficient redundancy in the number and locations of strain gages to allow numerous failures and still retain the capability to determine the frequency and magnitude of the pressure. pulsation in the main steam lines. Lastly, there is no individual sensor whose failure would prevent the ability to determine the acceptability of the vibration of the monitored piping systems. Multiple signal failures would be the worst-case failure for which it may be necessary to reduce power to replace failed components.

Page 33 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: 1

4) Resolution For computer failures, the second data acquisition system (i.e., there is one data acquisition system for the reactor building and one for the turbine building) could be used as a backup until repair or replacement of the failed system. Hardware for this type of system should be readily available for some years to come. The software is controlled by the design process, so that the applications and configurations necessary can be re-installed on the repaired system. This type of failure should have little consequence.

Signal failures at locations that are accessible can be readily repaired if spare. parts are available. Signal failures at inaccessible locations may be compensated by additional locations on the same piping, if available. Multiple signal failures in inaccessible locations will have to be evaluated by the Test Plan. There is a potential of unknown likelihood that multiple signal failures could stop pending power increases and require power to be reduced for component replacement or repair.

This kind of power restriction and potential power reduction would impact power level increases associated with the Extended Power Uprate.

Digital EMI / RFI Concerns The hardware, software, and data acquisition systems installed in accordance with this DCP are stand-alone systems. Information obtained from the DASs is not input into any permanent plant hardware or software system. However the impact of the DAS on surrounding plant systems due to potential Electromagnetic Interference is an issue requiring discussion.

One DAS system located in the Reactor Building is used for CTMT vibration monitoring, while another DAS located in the Turbine Building is used for Turbine Building monitoring. Each system is similar in configuration (similar hardware components) but customized for the number of monitored channels. Since the DASs do not supply information to any plant system ,are not safety related, and walkdowns revealed they are not in "line of sight" of safety related systems, testing to the CE mark is considered sufficient. DCP personnel have contacted hardware vendors to obtain the CE certificates to satisfy Electromagnetic Compatibility issues required by the plant. Certificates were supplied for the SCXI-1 000 4-slot chassis, SCXI-1001 12-slot chassis, SCXI-1141 8-channel elliptical filter module, SCXI-1 305 8-channel BNC accelerometer input block, SCXI-1121 4-channel strain gage signal conditioning module, SCXI-1321 4-channel strain gage input block (all made by National Instruments) and 2793 ISOTRON accelerometer signal conditioner (made by Endevco). The CE certificates are stored as permanent plant documentation in the Critical Software Package (CSP)H-1-ZZ-SCS-0253 Volume 8.

Page 34 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: 1 Upon the review of the hardware Certs, two items require clarification; The SCXI-1141 certificate listed ferrite bead connectors as a requirement between the SCXI-1141 filter module and the SCXI-1 305 input block "when using mass termination terminal blocks. The configuration used for our DASs has the SCXI-1305 plugging directly into the SCXI -1141 via coaxial cable. Therefore, ferrite beads are not required.

The Certs for the DAS components required the use of double-shielded cables vs.

single shielded cables between the DAS components. Discussions with the vendor stated that single shield cables were acceptable since they provide 93% shielding (compared to 97% for the double shielded cable), and the routings between DAS components was only 6ft and in the immediate area of the DAS..

Based upon the review of the hardware Certs, the information provided in the CSP, and plant walkdowns, the Digital Acquisition Systems used for vibration monitoring per this DCP will not impact existing plant systems due to Electromagnetic interference.

Potential Defective Equipment List No new material added per this DCP is on the Defective Equipment List (NC.DE-TS.ZZ-5424(Q)).

Page 35 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I 51`;1CE (C4X. TO EXIS]114 t:5i~ UMENT CABLE)

Ax r rlr.FJc In" IFJtUXFhIT CAPTULIEZJ

/ ~ PPPS lbA.LVAX:ZM tMABNN Stainless or Aluminum band to 55= OP or stainless steel band match jacket material depending on pipe mat'I Fig. I - Typical Accelerometer Mounting Detail Page 36 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: 1 Fig. 2 - Typical DAS Configuration With Cart Page 37 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: 1

'i U -j t51. <@j O9

> am A

-11,!>

va-r1 D5 Lf-ZJ 5Ii l

I l .=S t

. - - - , u E ExistingT Harw Cabinet Existing Hardware Cabinet Niew DAS Location Electrical Penetration

- -(1 BW202)

Reactor Building Elevation 102' Monitoring Equipment Pictogram Fig.3 (Markup of Dwg. A-0203)

Page 38 of 68 NC. CC-AP.ZZ-0080(QJ, Rev 8

CHANGE NO: 80062466 REVISION NO.: I Turbine Steam Tunnel (Room 1405 / 3491)

(22 Accelerometers Monitored At 9 Locations On Main Steam,Feedwater And Extraction Steam, 20 Strain Gages Monitored at 8 Locations On The Main Steam)

i. ,l I I' rJ; I  ; I' jjj 1X I' I ." i I5 r[-3 1:UA

. '.-s...,'LJ' 1 ~CF4ASSi X

,a wJ l _. SiJSO

- 1 rtL I i * -_ i

.i

.t IEEE-. I . . i, i atc Ist3 AX

=,A40 . w ' ' i i---0r. s i  ; i . - v L RES XI,_ U I I *MIMu TRAYI' RpU i:

• l C\#~ p ~ t Penetration N1401-001 DAS Location For Monitoring Main Steam, Feedwater, & Extraction Steam Piping Turbine Building Elevation 120'-132' Monitoring Equipment Pictogram

. Fig. 4 . ..

(Markup of Dwg. A-0204)

Page 39 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I Turbine Building Elevation 137' Monitoring Equipment Pictogram I jx UK r XW7U I1 ll1 iFEED1PLW i1 !sFEUtlU I " 4 2 Accelerometers at I Location For Monitoring Feedwater Fig. 5 (Markup of Dwg. A-0205)

Page 40 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I MAMONADRFAKOtT01T

- _ K-kVCIL'-VT'rWcAL IBL1 L1EU5 -j TYHCAL.

mcr W.Nas IaT

.Fig. 6 Typical Wiring Configuration (Turbine Building)

Page 41 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I I'ANMONA IRIIEAKOUT IJT

- A- RAYCHEMTITICAL lYTICAL NEW N02C0I BCADI.E BUTT SPLICE 1RAYLIEN Typ.

TYPICAL EXISTING N0.1 6SH.CALE VSTING BNOESH CAIILt

.Fig. 7 . . ..

Typical Wiring Configuration (Drywell / Reactor Building)

Page 42 of 68 NC.CC-AP.ZZ-0080(Q). Rev 8

CHANGE NO: 80062466 REVISION NO.: I FORM 6 AFFECTED DOCUMENT LIST (ADL)

A B C D E Package AD No. Affected Document Document SAP Order Rev of AD Number/Revision Sheet Operation Deletions Requiring Update Number Number I

H01 1-P-AE-01 / 21 1 270 H02 1-P-AE-04 / 11 1 270 H03 1-P-AB-01 /18 1 270 H04 1-P-AC-01 /1 8 1 270 H05 FSK-P-0169 /12 1 270 H06 FSK-P-0170/14 1 270 H07 FSK-P-0214 / 14 1 270 H08 Not Used 270 H09 1-P-BC-02 /21 1 270 HIO 1-P-FC-01 /19 1 270 Hl1 1-P-AB-08 / 12 1 270 H12 1-P-AB-09 / 13 1 270 Sol H-1-ZZ-SCS-0253 /0 1 270 S02 H-1-ZZ-SCS-0253 /0 2 270 S03 H-1-ZZ-SCS-0253 /0 3 270 S04 H-1-ZZ-SCS-0253 /0 4 270 If the affected document is a CAT 1.document [NOTE: .CAT I is not the-same as uUse Category I", per. .

NAP-1]:

• CAT 1 (Restart) document to be updated prior to Turn Over to Operations [see Definitions].

• • CAT 1 (Post-Restart) document to be placed on hold until updated prior to next use [see Definitions).

. For Equivalent CPs ONLY I If the affected document is to be updated after installation is complete, place an "I" in the Affected Document Number column at the right. Normally, this column is left blank because Equivalent CP ADs are issued with all acceptable equivalencies included since SAP tracks current configuration at installation.

Page 43 of 68 NC. CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I FORM 6 AFFECTED DOCUMENT LIST (ADL)

A B C D E Package AD No. Affected Document Document SAP Order Rev of AD */** Number/Revision Sheet Operation Additions/ Requiring Update Number Number Deletions RqiigUdt S05 H-1 -ZZ-SCS-0253 /0 5 270 S06 H-I-ZZ-SCS-0253 /O0 6 270 S07 H-l-ZZ-SCS-0253 /0 7 270 1 S08 H-1-ZZ-SCS-0253 / New 8 270 If the affected document is a CAT 1 document [NOTE: CAT:1 is not the same as "Use Category I", per NAP-1 ]:

• CAT 1 (Restart) document to be updated prior to Turn Over to Operations [see Definitions].

• • CAT 1 (Post-Restart) document to be placed on hold until updated prior to next use [see Definitions].

j. For Equivalent CPs ONLY If the affected document is to be updated after installation is complete, place an "I" in the Affected I

Document Number column at the right. Normally, this column is left blank because Equivalent CP ADs are issued with all acceptable equivalencies included since SAP tracks current configuration at installation.

Page 44 of 68 NC.CC-AP.ZZ-0080(Q), Rev 8

CHANGE NO: 80062466 REVISION NO.: I FORM 7 MATERIALS LIST CATEGORY: (EQUIPMENT, SERVICES, MATERIAL AND INSTALLATION SPARES) DISCIPLINE: CIVIL STRESS ITEM QUANTITY ITEM DESCRIPTION / SPECIFICATION PURCHASE MATERIAL USAGE COMMENTS NO. (Add Material Master number as necessary) CLASSIFICATION 72 Endevco Model 7703A-100 Piezoelectric Accelerometer 4 Material Master:1040157. Accelerometers: Prior to calibration, including Mounting Stud (2981-12/2981-3C/2981-1) temperature soak the accelerometers for 48 hours5.555556e-4 days <br />0.0133 hours <br />7.936508e-5 weeks <br />1.8264e-5 months <br /> at 550'F.

2 72 Endevco Model 2771 B-1 Remote charge convertor w/o teflon 4 Material Master: 1040204Remote charge Converters: Prior to sleeve, gain = 1.0,; calibration, temperature 0 soak the remote charge converters for

. 48 hours5.555556e-4 days <br />0.0133 hours <br />7.936508e-5 weeks <br />1.8264e-5 months <br /> at 180 F.

3 72 Endevco Model 3075M6-120 High Temperature Cable 4 Material Master: 1040205 Assemblies (10 ft) 4 30 Accelerometer mounting block with bolting hardware 4 Do Not Order (Supplied by Structural Integrity),Use for each

. ___ _ mnitorinc lnstion 5 40000 Ft. Cable-Cable USA Part #381802S8.1 1 MM=1040315 6 200 Connector-Breakout BNC Connector (Pomona #Model 4970) 4 MM=1040316, Use As Needed 7 2 PCB Company Model No. 394C06 Portable Ig Handheld Shaker 4 1043346 8 4 Wire-Twister Cutting Pliers (McMaster Part No. 5649A2) 4 1043315 9 3 BAND-IT Tool - Strap Cutter-(Catalog No. COO1) 4 1043316 lo 3 BAND-IT Tension Limiter (Catalog No. C065) -Used With 4 1043317 Part # COO I ll This Item Deleted From BOM 12 This Item Deleted From BOM NOTE: This form is not required if material information is input directly into the Component Screen (tab) of the subordinate NUCM installation order.

Page 45 of 68 ANCCC-AP.ZZ-OOO(Q), Rev. 8

CHANGE NO: 80062466 REVISION NO.: 1 FORM 7 MATERIALS LIST CATEGORY: Electrical / I & C (EQUIPMENT, SERVICES, MATERIAL AND INSTALLATION SPARES) DISCIPLINE: Civil / Stress ITEM QUANTITY ITEM DESCRIPTION / SPECIFICATION PURCHASE MATERIAL USAGE COMMENTS (Add Material Master number as necessary) CLASSIFICATION 13 1 3" Conduit Cut To Suit 10' Length 4 Y555698 14 3 3" Conduit Bushing IB-300 4 Y584682, 15 2 Foam Kit For Pen Seal 20 oz. 3 Y278002, 16 500 pieces Raychem Tubing-WCSF-500-38/13-12N OD .53-1.35 1 Y874458 17 500 pieces Raychem Tubing WCSF-I15-9-12N-N OD. .11-.31 1 Y321277, 18 500 pieces Raychem Tubing WCSF-300-12-N OD. .31-.81 1 Y874482, 19 500 pieces Butt - Splice T&E 2B 14 Range 16-14 2 Y585676, 20 4000 ft. STRAP -0.5 X 0.02 STAINLESS STEEL 4 Y971477 Use with mounting blocks on SS pipe & SS jacketing 21 500 buckles BUCKLE-BAND 'IT SS 1/2 4 Y412534 Use with SS pipe straps 22 1 lb. WIRE-SFTY LIK SS .020 4 Y979962 Use to link each accel and mounting block 23 1500 F. STRAP - 0.5 X 0.02 CARBON STEEL 4 1042026,Use with mounting blocks on carbon steel pipe 24 250 buckles BUCKLE-BANDIT CS 1/2 4 1042027,Use with carbon steel pipe straps NOTE: This form is not required if material information is input directly into the Component Screen (tab) of the subordinate NUCM installation order.

Page 46 of 68 NC.CC-AP.ZZ-0080(Q), Rev. 8

CHANGE NO: 80062466 REVISION NO.: I FORM 7 MATERIALS LIST CATEGORY: Electrical / I & C (EQUIPMENT, SERVICES, MATERIAL AND INSTALLATION SPARES) DISCIPLINE: Civil / Stress ITEM QUANTITY ITEM DESCRIPTION / SPECIFICATION PURCHASE MATERIAL USAGE COMMENTS NO. (Add Material Master number as necessary) CLASSIFICATION 25 500 pieces Tie-Cable, TYZ27M 3/16" To 3 '2" Dia., 13-3/8" Length 4 Y58704 1, For Use In Reactor & Turbine Bldg.

(Tefzel Straps) 26 500 pieces Tie-Cable, TYZ28M 1/8" To 4" Dia., 14 5/8" Length 4 Y587042, For Use In Reactor & Turbine Bldg.

(Tefzel Straps) ,

27 500 pieces Tie-Cable, TYS-14 4' Dia., 14-3/4" Length 4 Y587032, For Use In Drywell, (Stainless Steel Straps)

Insulation -To Be Determined 28 2 Structural Integrity Associates, Inc. Vibration Data Acquisition 4 Do Not Order - Supplied by Structural Integrity Associates System (VDAS) - See Attachment I for details Drywell Monitoring: Includes desktop computer, 4 signal conditioners, filter/amplifier- 54 channels Turbine Building: Includes desktop computer, 2 signal conditioners, filter/amplifier-24 channels Signal Conditioner(s) -Endevco Model 2793 ISOTRON Filter/ Amplifier Desktop Computer NOTE: This form is not required if material information is Input directly Into the Component Screen (tab) of the subordinate NUCM installation order.

Page 47 of 68 NC.CC-AP.ZZ-OO8OfQJ, Rev. 8

CHANGE NO: 80062466 REVISION NO.: I FORM 7 MATERIALS LIST CATEGORY: (EQUIPMENT, SERVICES, MATERIAL AND INSTALLATION SPARES) DISCIPLINE: CIVIL STRESS ITEM QUANTITY ITEM DESCRIPTION / SPECIFICATION PURCHASE MATERIAL USAGE COMMENTS NO. (Add Material Master number as necessary) 29 40' N-1000 UNISTRUT I Y876559 30 10' P-1001-C UNISTRbT 4 Y373725 31 10t N-3300 UNISTRU:T Y873451 32 10 N-330I UNISTRUT 1 Y876506 33 12 Screw- Hex Head Cap 12 x 13 x 15/16 1 Y874325 34 4 I Y876514 UNISTRUT N-102S HG. BRACKET 35 10 2 Y876562 UNISTRUT NUT P-40 10 36 12 HILTI 1/2X3 3/4" I Y876009 37 500 pieces BUTT SPLICE T&B 2B-18-16 OVERLAP TYPE 2 Y586942 3S50 CHANNEL CLAMP T&B TC5363X 4 MM=1042303 39 1 BAG Grout 4 X370007 NOTE: This form is not required if material information is input directly Into the Component Screen (tab) or the subordinate NUCMI installation order.

Page 48 of 68 NC.CC-AP.ZZ-OO8O(Q0, Rev. 8

CHANGE NO: 80062466 REVISION NO.: I FORM 7 MATERIALS LIST CATEGORY: (EQUIPMENT, SERVICES, MATERIAL AND INSTALLATION SPARES) DISCIPLINE: CIVIL STRESS ITEM QUANTITY ITEM DESCRIPTION / SPECIFICATION PURCHASE MATERIAL USAGE COMMENTS

. (Add Material Master number as necessary) CLASSIFICATION 40 500 Butt-Splice T&B2A-18 1 Y593046 41 3500 FT STRAP - 0.5" x 0.02" Aluminum 4 Y562001, Use on Aluminum Jacketing 42 600 BUCKLE-Aluminum For Y2" Straps 4 Y971485, Use with Aluminum Strapping Buckles 43 28 Weldable Strain Gage WI 2-wire shielded leads ,(Part # 4 1043382 HBWAK-12-063-6-10FG -F) Protective Cover & Practice Cover, Hitec Products, Inc.

44 4 Bottles Loctite 242 (50ml Bottle) 4 Y221779 45 100 #10 Flat Stainless Steel Washer 4 Y583290 46 1500 Ft. Band-It Band Strapping (Part# C303), Carbon Steel 4 MM=1 044183, Used To Mount Accel Mounting Block On Strapping (3/8" x .025") Carbon Steel Pipe 47 500 Band-It Buckle (Part# C353) (Use with Carbon steel 4 MM=1044184, Use with Carbon Steel Strapping To Mount Buckles Strapping 3/8" x .025") Accel Mounting Block To Carbon Steel Pipe 48 Not Used NOTE: This form is not required if material Information is input directly into the Component Screen (tab) of the subordinate NUCM installation order.

Page 49 of 68 NC.CC-AP.ZZ-00S0(Q), Rev. 8

CHANGE NO: 80062466 REVISION NO.: I FORM 7 MATERIALS LIST CATEGORY: (EQUIPMENT, SERVICES, MATERIAL AND INSTALLATION SPARES) DISCIPLINE: CIVIL STRESS ITEM QUANTITY ITEM DESCRIPTION / SPECIFICATION PURCHASE MATERIAL USAGE COMMENTS NO. (Add Material Master number as necessary) CLASSIFICATION 49 1 Vishay Model 700 Portable Strain Gage Welding & 4 MM= 1044177, Used To Spot Weld Strain Gages To Pipe Soldering Unit .

50 1000 Ft. Band-It Band Strapping (Part# C403), Stainless Steel 4 MM=1044185, Used To Mount Accel Mounting Block On Strapping (3/8" x .025") Stainless Steel Pipe 51 500 Band-It Buckle (Part# C453) (Use with Stainless Steel 4 MM=1044186, Use with Stainless Steel Strapping To Mount Buckles Strapping 3/8" x .b25") Accel Mounting Block To Stainless Steel Pipe 52 This Item Deleted From BOM 3This Item Deleted From BOM This Item Deleted From BOM 55 30 Shts Brady label Self-Laminating Polysester B-361, 4 MM= 1044527, (1.5" Wide x 1.0" High), 45 Labels Per Sheet, Write- On Area: 1.5" x 0 .375" Brady Part# 62344 ( Catalog # LAT-52-361-1)

NOTE: This form is not required if material information is input directly into the Component Screen (tab) of the subordinate NUCM installation order.

Page 50 of 68 NC.CC-AP.ZZ-0080(Q), Rev. 8

NC.NA-AS.ZZ-0059(Q)

FORM-1 REGULATORY CHANGE PROCESS DETERMINATION Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package Activity

Description:

This Design Change Package (DCP) has been produced as a result of The PSEG Extended Power Uprate Project, in conjunction with General Electric (GE), and Task Report T-0318, defining systems requiring Flow Induced Vibration (FIV) monitoring due to the implementation of the Extended Power Uprate.

Piping system monitoring will occur inside the drywell (room 4220), turbine building steam tunnel elevation 123' (room 1405/3491), and in feedwater water heater room 1504 at elevation 137'. The following piping systems will be monitored for Fly; Main Steam (drywell and turbine building), Main Steam Relief Valve Discharge Piping (J & P valves discharge),

RCIC Steam Supply (inside drywell), Feedwater (drywell and turbine Building), Extraction Steam, Recirc (and RHR connections inside drywell). Forty-eight accelerometers at nineteen locations will be monitored in the drywell. Twenty-four accelerometers at ten locations, and twenty strain gages at eight locations will be monitored in the turbine building. The drywell instrumentation will be connected through drywell electrical penetration I BW202, to a cabinet mounted near the "B" side drywell access hatch in the reactor building at elevation 102'. This hardware cabinet was previously installed in DCP 4EC-3186 for the purposes of Recirc vibration monitoring. A Data Acquisition System (DAS) will be fully or partially mounted in this cabinet with the remaining components sitting atop a cart. The DAS will be powered via a convenience outlet when drywell data is to be obtained. Based upon constructability walkdowns, a second DAS setup will sit atop a cart (in lieu of a hardware cabinet), in the turbine building room 4101, near the turbine building steam tunnel at elevation 123'. Cable inside the turbine building steam tunnel will be routed to this DAS through an existing grouted wall penetration (N-1401-001).

The hardware, software, and data acquisition systems installed in accordance with this DCP are stand-alone systems. Information obtained from the DASs is not input into any permanent plant hardware or software system. Therefore, there is no effect on the Main Steam, RCIC, Feedwater, Extraction Steam, Recirc or RHR System Design Functions from the monitoring of these piping systems.

It is important to note that this DCP installs vibration monitoring equipment; instrumentation, cable, accelerometers, and digital acquisition systems to obtain vibration information on specific piping systems. This DCP does not include information pertaining to when the tests will be performed, nor does it provide testing acceptance criteria for the piping being monitored. This information will be provided in the Test Plan.

Page 51 of 68 NC.NA-AS.ZZ.0059(Q), Rev.6

NC.NA-AS.ZZ-0059(Q)

FORM-1 REGULATORY CHANGE PROCESS DETERMINATION Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package Note that more than one process may apply. If unsure ofany answer, contact the cognizant departmentfor guidance.

Activities Affected No Yes Action

1. Does the proposed activity involve a change to the Technical 1 If Yes, contact Licensing; process in Specifications or the Operating License? accordance with NC.NA-AP.ZZ-0035(Q) l_ LCR No.:

2. Does the proposed activity involve a change to the Quality E I If Yes, contact Quality Assessment; process Assurance Plan? Examples: in accordance with ND.QN-AP.ZZ-0003(Q)

Changes to Chapter 17.2 of UFSAR

• Does the proposed activity involve a change to the Security Plan? 1 f If Yes, contact Security Department; process Examples: in accordance with NC.NA-AP.ZZ-0033(Q)

• Change program in NC.NA-AP.ZZ-0033(Q)

• Change indoor/outdoor security lighting

• Placement of component or structure (permanent or temporary) within 20 feet of perimeter fence

• Obstruct field of view from any manned post a Interfere with security monitoring device capability

• Change access to any protected or vital area

• Modify safeguards systems or equipment

4. Does the proposed activity involve a change to the Emergency 1 If Yes, contact Emergency Preparedness Plan? Examples:

a Change ODCMlaccident source term

• Change liquid or gaseous effluent release path

• Affect radiation monitoring instrumentation or EOP/AOP setpoints used in classifying accident severity

• Affect emergency response facilities or personnel, including control rm

• Affect communications, computers, information systems or Met tower

5. Does the proposed activity involve a change to the ISI Program O If Yes, contact Reliability Programs ISI/ST; Plan? Examples: process in accordance with

• Affect Nuclear Class 1, 2, or 3 Piping, Vessels, or Supports NC.NA-AP.ZZ-0027(Q)

(Guidance in NC.DE-AP.ZZ-0007(Q) Form-1)

6. Does the proposed activity involve a change to the IST Program O If Yes, contact Reliability Programs ISI/IST; Plan? Examples: process in"accordance with

. Affect the design or operating parameters of a Nuclear Class 1, NC.NA-AP.ZZ-0070(Q) 2, or 3 Pump or Valve (Guidance in NC.DE-AP.ZZ-0007(Q)

Form-15)

Page 52 of 68 NVC.NA -AS.ZZ-0059(Q), Rev. 6

NC.NA-AS.ZZ-0059(Q)

FORM-1 REGULATORY CHANGE PROCESS DETE RMINATION Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitorincg Installation Package Activities Affected No Yes Action

7. Does the proposed activity involve a change to the Fire Protection LZ fL If Yes, contact Design Engineering; process Program? Examples: in accordance with NC.DE-PS.ZZ-0001(Q)

• Change program in NC.DE-PS.ZZ-000 1(Q)

• Change combustible loading of safety related space

• Change or affect fire detection system

• Change or affect fire suppression system/component

• Change fire doors, dampers, penetration seal or barriers

• See NC.DE-AP.ZZ-0007, Forms 3, 4 and 14 for details

8. Does the proposed activity involve Maintenance which restores 3 Li If Yes, process in accordance with SSCs to their original design and configuration? Examples: NC.WM-AP.ZZ-0001(Q)

• CM or PM activity

• Implements an approved Design Change?

• Troubleshooting (which does not require 50.59 screen per SH.MD-AP.ZZ-0002)

Is the proposed activity a temporary change (T-Mod) which meets 1 O If Yes, contact Engineering; process in all ithefollowing conditionss? accordance with NC.DE-AP.ZZ-0030(Q)

• Directly supports maintenance and is NOT a compensatory measure to ensure SSC operability.

• Will be in effect at power operation less than 90 days.

• Plant will be restored to design configuration upon completion.

• SSCs will NOT be operated in a manner that could impact the function or operability of a safety related or Important-to-Safety system.

10. Does the proposed activity consist of changes to maintenance O1 If Yes, process in accordance with procedures which do NOT affect SSC design, performance, NC.NA-AP.ZZ-0001(Q) operation or control?

Note: Procedure information affecting SSC design, performance, operation or control, including Tech Spec required surveillance and inspection, require 50.59 screening. Examples include acceptance criteria for valve stroke times or other SSC function, torque values, and types of materials (e.g., gaskets, elastomers, lubricants, etc.)

11. Does the proposed activity involve a minor UFSAR change FL1 If Yes, process in accordance with (including documents incorporated by reference)? Examples: NC.NA-AP.ZZ-0035(Q)

.. Reformatting, simplification or-clarifications that do not.. . _ .

change the meaning or substance of information

. Removes obsolete or redundant information or excessive detail

. Corrects inconsistencies within the UFSAR

• Minor correction of drawings (such as mislabeled ID)

12. Does the proposed activity involve a change to an Administrative [ O If Yes, process in accordance with Procedure (NAP, SAP or DAP) governing the conduct of station NC.NA-AP.ZZ-0001(Q) and operations? Examples: NC.DM-AP.ZZ-000l (Q)

• Organization changes/position titles

• Work controll modification processes _

Page 53 of 68 NCNA-AS.ZZ-0059(Q), Rev.6

NC.NA-AS.ZZ-0059(Q)

FORM-1 REGULATORY CHANGE PROCESS DETERMINATION Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitorinq Installation Packacie Activities Affected No Yes Action

13. Does the proposed activity involve a change to a regulatory O If Yes, contact Licensing and process in commitment? accordance with NC.NA-AP.Z-0030(Q)

14. Does the activity impact other programs controlled by regulations, If Yes, process in accordance with operating license or Tech Spec? Examples: applicable procedures such as:

• Chemical Controls Program NC.NA-AP.ZZ-0038(Q)

• NJ "Right-to-know" regulations NC.LR-AP.ZZ-0037(Q)

• OSHA regulations

• NJPDES Permit conditions

• State and/or local building, electrical, plumbing, storm water management or "other" codes and standards

• 10CFR20 occupational exposure

15. Has the activity already received a I0CFR50.59 Screen or 3 [l Take credit for IOCFR50.59 Screen or Evaluation under another process? Examples: Evaluation already performed.

• Calculation

• Design Change Package or OWD change ID:

• Procedure for a Test or Experiment

• DR/Nonconformance

• Incorporation of previously approved IJFSAR change If any other program or regulation may be affected by the proposed activity, contact the department indicated for further review in accordance with the governing procedure. If responsible department determines program is not affected, attach written explanation.

If ALL of the answers on the previous pages are "No," then check A below:

A. [X ] None of the activity is controlled by any of the processes above, therefore a 10CFR50.59 review IS required. Complete a 10CFR50.59 screen.

If one or more of the answers on the previous pages are "Yes," then check either B or C below as appropriate and explain the regulatory processes which govern the change:

B. [ ] All aspects of the activity are controlled by one or more of the processes above, therefore a 10CFR50.59 review IS NOT required.

C. [ ] Only part of the activity is controlled by the processes above, therefore a IOCFR50.59 is required.

Page 54 of 68 NC.NA-AS.ZZ-0059(Q), Rev.6

NC.NA-AS.ZZ-0059(Q)

FORMi-I REGULATORY CHANGE PROCESS DETERMINATION Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package Explanation: Combustible loadings added per this DCP are enveloped by the combustible loadings added per previous DCP 4EC-3186, and later removed. Penetration Seal Work Release Nos. 5326

& 5327 are provided for the modification to penetration N-1401-001. The Penetration Seal will be restored to its original fire rating upon completion of the modification. None of the activity is controlled by any of the processes listed above and a IOCFR50.59 review is required.

Preparer: Philip M. Stashak 8-23-04 Printed Name Signature Date Reviewer: J. Annett 10-5-04 Printed Name Signature Date Page 55 of 68 NCNA-AS.ZZ-0059(Q), Rev.6

NC.NA-AS.ZZ-0059(Q)

FORM-2 IOCF'R50.59 SCREENING Revision 0 Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package Applicability:

Salem 1 Salem 3 (Gas Turbine) PSEG Common Salem 2 X Hope Creek Salem I & 2 Common Hope Creek & Salem Common

1. Brief Description of activity Change to: 0 Facility C Procedures 1J Methodology ETest/Experiment M Fission Barrier MWat is being changed and why This Design Change Package (DCP) has been produced as a result of The PSEG Extended Power Uprate Project, in conjunction with General Electric (GE), and Task Report T-0318, defining systems requiring Flow Induced Vibration (FlV) monitoring due to the implementation of the Extended Power Uprate.

Piping system monitoring will occur inside the drywell (room 4220), turbine building steam tunnel elevation 123' (room 1405/3491), and in feedwater water heater room 1504 at elevation 137'. The following piping systems will be monitored for FIV; Main Steam (drywell and turbine building), Main Steam Relief Valve Discharge Piping ( "J"&

up.. valves discharge), RCIC Steam Supply (inside drywell), Feedwater (drywell and turbine Building), Extraction Steam, Recirc (and RHR connections inside drywell). Forty-eight accelerometers at nineteen locations will be monitored in the drywell. Twenty-four accelerometers at ten locations, and twenty strain gages at eight locations will be monitored in the turbine building. The drywell instrumentation will be connected through drywell electrical penetration 1BW202, to a cabinet mounted near the uB" side drywell access hatch in the reactor building at elevation 102'. This hardware cabinet was previously installed in DCP 4EC-3186 for the purposes of Recirc vibration monitoring. A Data Acquisition System (DAS) will be fully or partially mounted in this cabinet with the remaining components sitting atop a cart. The DAS will be powered via a convenience outlet when drywell data is to be obtained. Based upon constructability walkdowns, a

-second-DAS setup will sit atop a cart-(in lieu of a hardware cabinet),-in the turbine- - -

building room 4101, near the turbine building steam tunnel at elevation 123'. Cable inside the turbine building steam tunnel will be routed to this DAS through an existing grouted wall penetration (N-1401-001).

The hardware, software, and data acquisition systems installed in accordance with this DCP are stand-alone systems. Information obtained from the DASs is not input into any permanent plant hardware or software system. Therefore, there is no effect on the Main Page 56 of 68 NC.NA-AS.ZZ-0059(Q), Rev.6

NC.NA-AS.ZZ-0059(Q)

FORM-2 10CFR50.59 SCREENING Revision 0 Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package Steam, RCIC, Feedwater, Extraction Steam, Recirc or RHR System Design Functions from the monitoring of these piping systems.

Design Functions The testing performed with the vibration monitoring equipment installed per this DCP ensures that plant safety is not dependent upon the performance of untested systems.

The function of the vibration monitoring equipment and DAS is to confirm that the plant systems will continue to perform their Design Functions after implementation of the Extended Power Uprate.

Effect on DesignFunctions The hardware, software, and DASs installed in accordance with this DCP are stand-alone systems. Information obtained from the DASs is not input into any permanent plant hardware or software system. Therefore, there is no effect on the Main Steam, RCIC, Feedwater, Extraction Steam, RHR or Recirc System Design Functions from the monitoring of these piping systems.

Page 57 of 68 NC.NA-AS.ZZ-0059(Q), Rev.6

NC.NA-AS.ZZ-0059(Q)

FORM-2 10CFR50.59 SCREENING Revision 0 Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package

2. Summarize regulatory change determination (Other applicable regulatory processes identified on Form-l)

Combustible loadings added per this DCP are enveloped by the combustible loadings added per previous DCP 4EC-31 86, and later removed. Penetration Seal Work Release Nos. 5326 & 5327 are provided for the modification to penetration N-1401-001. The Penetration Seal will be restored to its original fire rating upon completion of the modification. None of the activity is controlled by any of the processes listed above and a 1QCFR50.59 review is required. 'i

3. Does the proposed activity require a change to Technical Specifications or the Operating License? Yes D No 0 If YES, then a License Amendment is required prior to implementation of the activity.

LCR.Number: N/A

4. Does the proposal require a UFSAR change? Yes F No 0 UFSAR Change Notice No. N/A Describe UFSAR change: N/A

5. 50.59 Screeniniz Ouestions Answer ALL screening questions Yes No

a. Does the proposed activity involve a change to the facility that adversely affects a UFSAR described design function? [l 0

b. Does the proposed activity involve a change to procedures that adversely affects how UFSAR described SSC design functions are performed or controlled? 0

c. Does the proposed activity revise or replace evaluation methodology described in the UFSAR that either:

_._.is.used.in the safety analses or .....

establishes the design bases?

d. Does the proposed activity involve a test or experiment NOT described in the UFSAR? (SSC is utilized or controlled in a manner that is outside the reference E Z bounds of its design or inconsistent with analyses or descriptions in the UFSAR)

e. Does the proposed activity affect a design basis limit for a fission product barrier (fuel cladding, reactor coolant system boundary or containment? El ED Page 58 of 68 NC.NA-AS.ZZ-0059(Q), Rev.6

NC.NA-AS.ZZ-0059(Q)

FORM-2 IOCFR50.59 SCREENING Revision 0 Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package

6. If a 50.59 Evaluation is not required, provide justification for that determination:

The hardware, software, and DASs installed in accordance with this DCP are stand-alone systems. Information obtained from the Data Acquisition Systems is not input into any permanent plant hardware or software system. Therefore, there is no effect on the Main Steam, RCIC, Feedwater, Extraction Steam, RHR or Recirc System Design Functions from the monitoring of these piping systems. However, the impact of the installation of the vibration monitoring equipment in various locations.of the plant must be addressed. Based upon a detailed review of the UFSAR, the following items require discussion: ECCS Suppression Pool Strainer Blockage, Cable Routing and Separation, Containment Circuits and Short Circuit Analysis, Fire Protection (addition of combustibles), Penetration Seal Modification, Insulation Modification, Affect of mounting blocks and hardware on pipe stress evaluations, and Digital EMI/RFI concerns.

ECCS Suppression Pool Strainer Blockage The ECCS is designed to provide protection against postulated loss-of-coolant accidents (LOCAs) caused by ruptures in reactor coolant pressure boundary (RCPB) piping. The ECCS injection network consists of a HPCI system, a Core Spray system, Automatic Depressurization (ADS) and the Low Pressure Coolant Injection (LPCI) mode of the RHR system. The installation of any commodities within the drywell creates concerns that these commodities can be dislodged, transported to the suppression pool, and clog the suppression pool strainers. The clogging of the suppression pool strainers could hinder or disable the ability of the plant to respond to accidents requiring ECCS operation.

Engineering Evaluation H-lBB-MEE-1168 revision 1 identifies insulation sources inside the drywell and determines the amount of insulation transported to the drywell due to applicable pipe breaks identified in UFSAR Section 3.6. Several High Energy Pipe Breaks were evaluated for insulation damage potential which included; Main Steam, Feedwater, Recirc Suction, Recirc/RHR Line, Recirc Suction riser. Three breaks were chosen for more detailed analysis; Recirc Suction, Feedwater, and Recirc Suction Riser. This DCP will install approximately 6000 ft. of cable in the drywell. Using a cable OD..of.1/4", and assuming that all of the cable ..isdamaged and falls-into-the wetwell, a.

total volume of approximately 2 ft3 is added to the wetwell. The results tabulated in table 8.3.10 reveal that locations and angles relative to the pipe breaks were used as parameters in determining impacted targets (pipe) and damaged insulation. Based upon these values we see that 78% of the insulation damaged below the grating at elevation 100' became wetwell debris, compared to 28% of the insulation damaged above elevation 100'. Most of the insulation damaged above elevation 100' was considered to be screened by the grating. Therefore it is extremely conservative to consider that all of the cable added to the drywell regardless of its location relative to the postulated pipe break locations is delivered to the wetwell. Even with this gross assumption, less than 2 Page 59 of 68 NCNA-AS.ZZ-0059(Q). Rev.6

NC.NA-AS.ZZ-0059(Q)

FORM-2 10CMR50.59 SCREENING Revision 0 Document I.D.: 80062466 Revision: 1

Title:

EPU Vibration Monitoring Installation Package cubic feet of material becomes potential ECCS strainer blockage debris. This is less than 0.5% of the wetwell debris calculated for the Recirc Suction riser pipe break scenario. The calculated volume of wetwell debris attributed to the added cable is negligible. Therefore, the addition of cable to primary containment does not have the potential to adversely affect the design function of the ECCS System.

Cable Separation and Routing The guidelines of Procedure HC.MD-AP.ZZ-0004(Q) "General Guidelines For Tempbrary PoWbr And Communication Cables Installation And Removal" will be used as a guideline in order to install the temporary cable and ensure personnel and equipment safety. Cables will be supported using structural steel, support steel, equipment supports, and cable tray supports (as long as the cable tray is not 1E). Cable will not be run in cable trays. Cables will be routed off the floor to prevent physical damage and create trip hazards. Cable spans will be restrained to limit swinging during seismic events. A one-inch separation will be maintained between cable and class 1E conduit. In the vicinity of the accelerometer and remote charge converter on the piping, the cable will be banded to the insulation jacketing with stainless steel or carbon steel strapping. The strapping material will be matched to the pipe material. As a minimum, the cables will be labeled for identification near the remote charge converter, near the CTMT penetration (for drywell installation), and near the data acquisition systems. The Endevco Remote Charge Converter, BNC connector, and BNC Breakout will all be wrapped in shrink tubing. Normally the Endevco Remote Charge Converter is wrapped in a teflon sleeve. The BNC breakout has teflon as an insulator in the connector and PVC is used in the insulation material for the pigtail wires which are 7 inches in length.

The shrink tube will encapsulate these materials to preclude the possibility of FME concerns. The small amounts of teflon and PVC are of little concern. In addition, these commodities are not a permanent installation to the plant and will be removed in the future. Engineering will conduct walkdowns and perform a final signoff to ensure supporting requirements and cable separation criteria is met. Therefore, the addition of cable and monitoring equipment IAW this DCP does not adversely affect UFSAR Design Functions.

Containment Penetration Circuits and Short Circuit AnalVsis In determining the impact of this DCP on the containment penetration two concerns are applicable; type of cable and circuitry (class 1E vs. non-class 1E) and penetration short circuit analysis. Containment penetration 1BW202 is an I&C penetration with Non-class 1E cables connected to it. None of the accelerometer cables are part of a Class 1E circuit. Therefore, we are in compliance with UFSAR section 8.1.14.5 which states that non-class 1E circuits are not routed in penetrations containing class 1E circuits. A review was performed to ensure the integrity of the containment electrical penetration Page 60 of 68 NCNA-AS.ZZ-0059(Q), Rev.6

NC.NA-AS.ZZ-0059(Q)

FORAI-2 IOCFR50.59 SCREENING Revision 0 Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package 1BW202. Calculation-.7.13 was reviewed to determine the impact of connecting the ...

wiring for the accelerometer and remote charge converters to Containment Electrical Penetration I BW202. Calc 7.13 is titled "Penetration Assembly Protection". The piezoelectric accelerometer is a self-generating device that requires no external power source for operation. It is connected to the DAS system through a remote charge converter and uses a high impedance coaxial cable. These high impedance circuits carry milliamp signals, only. This type of circuit has been addressed in calc 7.13 Section h pages 6 and 7. The section states "...the continuous ratings for these penetrations are considerably higher than the maximum short circuit current they may be expected to experience." The milliamp circuits installed per this DCP cannot create a short circuit challenge to the penetration. Therefore, the penetration will continue to perform its UFSAR described Design Function.

Fire Protection (Addition Of Combustibles)

The overall HCGS fire protection program is based on the evaluation of potential fire hazards throughout the plant and on the effects of postulated fires on the performance of safe shutdown functions. Consistent with other safety requirements, systems, structures, and components, including those required for safe shutdown are designed and located to minimize the probability and effect of fires. The Auxiliary Building, Reactor Building, and Turbine building are separated from each other by 3-hour fire walls. Redundant safety related components are separated form each other and the rest of the plant by 3-hour fire barriers, and or separated by 20 feet. The following is a list of designated Fire areas per Fire Area drawings M-5004, M-5114, and M-5115 for rooms where cable and monitoring equipment is added per this DCP; drywell room 4220 (RB7), reactor building room 4322 (RB2), turbine building rooms 1401(TBl),

1405/3491(TBl), and 1504(TBI1).

Although we are adding cable to the drywell and safety related equipment is prevalent throughout the drywell, no fire hazards analysis is performed for the drywell per Table 9A-1 " Fire Hazards Analysis". The drywell is inerted during operation, making a fire impossible. The main concern for fire inside the drywell occurs during refueling and

--h~riterace~-operations~.Duririgrefueling-ard maintenance-operations in-the drywell,----

portable fire extinguishers, in addition to the hose stations, are adjacent to the work area and readily available for use by plant personnel. Self-contained breathing apparatus is provided near the containment entrances for firefighting personnel. Therefore, no further analysis of the drywell for implementation of this DCP is required.

The DAS located in room 4322 (Reactor Building) consists of a metal cart, if required, (non combustibles) and combustibles that include; a desktop computer, and an Page 61 of 68 NC.NA-AS.ZZ-0059(Q), Rev.6

NC.NA-AS.ZZ-0059(Q)

FORM-2 10CFR50.59 SCREENING Revision 0 Document I.D.: 80062466 Revision: 1

Title:

EPU Vibration Monitoring Installation Package assumed amount of paper, pencils, and nearby reference materials. All carts to be used, will be restrained to meet the seismic 11/I requirement per DE-PS.ZZ-0011(Q).

An assumption is that the equipment will add approximately 50 pounds of combustible plastic to the room. It is also assumed that paper, pencils, and reference materials will add an additional 25 pounds of combustible material to the room. This DCP will install DAS equipment in a reactor building cabinet installed for DCP 4EC-3186 and later abandoned. The cabinet was recently reused for DAS equipment in TMOD 04-006. A review of the DAS components shows that the weight assumptions for combustibles used for DCP 4EC-3186 were conservative. Therefore the weight of combustible commodities listed in Table 9A-1 " Fire Hazards Analysis" and stored in Room 4322 is still acceptable. No changes are required to Table 9A-9 "Fire Hazards Analysis Tabulation" for Fire Area RB2 page 1 of 27 or Room 4322 page 25 of 27. Therefore, no further fire hazards analysis of the reactor building room 4322 for implementation of this DCP is required.

Cables will be added to Turbine Building Rooms 1401, 1405/3491 and 1504. A second DAS sitting atop a cart will be stored in room 1401. Per Fire Area Drawings M-5115, these rooms are designated as Fire Area TB1. No safety related equipment exists in any of these rooms. These rooms are not listed in Table 9A-4 "Fire Areas and Associated Room Numbers" and Table 9A-1 "Fire Hazards Analysis Summary'.

Therefore, no Fire Hazards Analysis is required for installation of the cable and/or monitoring equipment in these rooms.

Therefore, per the Fire Protection review, the additions of combustibles lAW with this DCP does not adversely affect any UFSAR Design Functions.

Penetration Seal Modification The cables for the accelerometers in the Turbine Building Steam Tunnel (room 1405) will be routed through penetration seal N-1401-001 to a DAS mounted on a cart in adjacent room 1401. Penetration Seal N-1401-001 is listed as a 3-hour fire seal. The grouted seal will be partially removed, conduit inserted, and cable routed through the conduit: The seal will be~regrouted and the conduit sealed withifoam in accordance with-Penetration Seal Work Release Nos. 5326 & 5327. Therefore, restoring the penetration seal to its 3-hour fire rating and not adversely affecting any UFSAR Design Functions.

Page 62 of 68 NC.NA-AS.ZZ-0059(Q), Rev.6

NC.NA-AS.ZZ-0059(Q)

FORM-2 10CFR50.59 SCREENING Revision 0 Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package Insulation Modification, Affect Of Mounting Blocks And Hardware On Pipe Stress....

Evaluations.

The Main Steam, RCIC, Feedwater, Recirculation (attached RHR) and Extraction Steam piping will be instrumented with a total of 72 accelerometers at 29 locations.

Insulation at the monitored piping locations will be temporarily removed. Strapping, banded around the piping and prefabricated accelerometer mounting brackets will be installed at the large bore pipe monitoring locations. The accelerometer(s) will be installed. Then, the insulation will be reinstalled. The insulation will be reconfigured for each size pipe OD., insulation thickness, and insulation jacket material. The insulation and jacket materials will be reconfigured with 'high-hat" designs that will allow for the space occupied by the mounting blocks and accelerometers, and at the same time restore the insulation and jacketing to their original insulating performance. Therefore, the environmental room temperatures where the vibration monitoring hardware and devices are mounted on the piping are not affected.

In addition, twenty strain gages with protective covers will be installed on all four Main Steam pipes in the Turbine Building. Two strain gages will be installed in the hoop direction at eight locations on the main steam lines, two locations on each main steam line. In addition, two strain gages will be installed in the longitudinal direction at two locations to measure the amount of bending on the pipe. The insulation at the specified locations will be temporarily removed, the strain gages spot-welded to the pipe, the protective cover slipped over the strain gage, and the insulation reinstalled.

The weight of the accelerometers, remote charge converters and mounting block for any monitored location is less than 3.5 lbs, total. The weight of the strain gages is a few ounces. This weight is insignificant to the lbs/ft of the pipe being monitored. The weights of the mounting hardware and monitoring devices will have no impact on the adjacent pipe supports. In addition, the weights of the mounting hardware and monitoring devices will have no impact on the dynamic effects of the piping they are monitoring. Therefore, the results obtained with the monitoring devices and hardware installed on the piping,

-- are still valid for the-piping when thermonitoring devices and hardware are later removed. The Design Functions of the piping and insulation are not adversely affected by additions of vibration monitoring equipment weight to the piping and modification of the insulation. The existing piping analysis is still valid and the room temperatures are unaffected by the modified insulation since the insulation is restored to its original insulating performance. The modification of the insulation and addition of accel mounting brackets does not affect the Design Functions of the systems be monitored.

Page 63 of 68 NC.NA-AS.ZZ-0059(QO, Rev.6

NC.NA-AS.ZZ-0059(Q)

FORM-2 OCFR50.59 SCREENING Revision 0 Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package

,Digital EMI / RFI ConcernsThe hardware, software, and data acquisition systems installed in accordance with this DCP are stand-alone systems. Information obtained from the DASs is not input into any permanent plant hardware or software system. However the impact of the DAS on surrounding plant systems due to potential Electromagnetic Interference is an issue requiring discussion.

One DAS system located in the Reactor Building is used for CTMT vibration monitoring, while another DAS located in the Turbine Building is used for Turbine Building monitoring. Each system is.similar in.configuration (similar hardware components) but.

customized for the number of monitored channels. Since the DASs do not supply information to any plant system ,are not safety related, and walkdowns revealed they are not in "line of sight" of safety related systems, testing to the CE mark is considered sufficient. DCP personnel have contacted hardware vendors to obtain the CE certificates to satisfy Electromagnetic Compatibility issues required by the plant.

Certificates were supplied for the SCXI-1 000 4-slot chassis, SCXI-1001 12-slot chassis, SCXI-1 141 8-channel elliptical filter module, SCXI-1 305 8-channel BNC accelerometer input block, SCXI-1121 4-channel strain gage signal conditioning module, SCXI-1321 4-channel strain gage input block (all made by National Instruments) and 2793 ISOTRON accelerometer signal conditioner (made by Endevco). The CE certificates are stored as permanent plant documentation in the Critical Software Package (CSP)H-1-ZZ-SCS-0253 Volume 8.

Upon the review of the hardware Certs, two items require clarification; The SCXI-1 141 certificate listed ferrite bead connectors as a requirement between the SCXI-1141 filter module and the SCXI-1 305 input block "when using mass termination terminal blocks. The configuration used for our DASs has the SCXI-1 305 plugging directly into the SCXI -1141 via coaxial cable. Therefore, ferrite beads are not required.

The Certs for the DAS components required the use of double-shielded cables vs.

single shielded cables between the DAS components. Discussions with the vendor

.stated-that-single shield cableswere acsepiable since they elding (compared to 97% for the double shielded cable), and the routings between DAS components was only 6ft and in the immediate area of the DAS.

Based upon the review of the hardware Certs, the information provided in the CSP, and plant walkdowns, the Digital Acquisition Systems used for vibration monitoring per this DCP will not impact existing plant systems due to Electromagnetic interference.

Page 64 of 68 NC.NA-AS.ZZ-0059(Q), Rev.6

NC.NA-AS.ZZ-00959(Q)

FORM-2 10CFR50.59 SCREENING Revision 0 Document 1.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package This implementation of this activity does not adversely affect UFSAR described Design Functions. It does not involve changes to procedures, or methodology, and does not involve tests or experiments. This activity does not involve changes to design limits for fission product barriers. Therefore, a IOCFR50.59 Evaluation is not required.

Conclusions:

fS If all Screening questions in Section 5 are answered NO, then a 50.59 Evaluation is not required.

El If any Screening question is YES, then perform a 50.59 Evaluation (Form-3).

50.59 Evaluation No: N/A

7. List the documents reviewed containing relevant information, including section numbers (UFSAR, Tech Specs, and others):

3.6 Protection Against Dynamic Effects associated With The Postulated Rupture Of Piping 3.6.2.6 Determination Of Break Locations And Dynamic Effects Associated With The Postulated Rupture Of Recirculation System Piping (NSSS) 3.7 Seismic Design 3.7.2 Seismic System Analysis 3.7.3 Seismic Subsystem Analysis 3.9 Mechanical Systems And Components 3.9.2 Dynamic Testing And Analysis 3.9.2.1 Thermal Expansion, Piping Vibration, And Dynamic Effects In NSSS Piping 3.9.2.2 Preoperational And Startup Testing Of Non-NSSS Piping 3.11 Environmental Design Of Mechanical And Electrical Equipment 4.1.1 Reactor Vessel 4.1.2.3 Shroud Head And Steam Separator Assembly 4.1.2.4 Steam Dryer Assembly 4.3 Nuclear Design 4.3.2.1 Nuclear Design Description 4.4.5 Testing And Verification 5 Reactor Coolant System And Connected Systems 5.1.6 Reactor Pressure Vessel 5.1.7 Reactor Recirculation System 5.1.8 Main Steam Lines And Flow Restrictors 5.1.9 Reactor Core Isolation Cooling System 5.1.10 Residual Heat Removal System

,5.1.11 Reactor Water Cleanup System 5.1.12 Feedwater System Lines 5.2 Integrity Of Reactor Coolant Pressure Boundary Page 65 of 68 NC.NA4ASIZZ-0059(Q), Rev.6

NC.NA-AS.ZZ-0059(Q)

FORM-2 lOCR50.59 SCREENING Revision 0 Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package 5.2.1 Compliance With Codes.And&Code Cases 5.2.1.1 Compliance With 10 Cfr, Part 50, Section 50.55a 5.2.1.2 Applicable Code Cases 5.4.1 Reactor Recirculation Pumps 5.4.1.1 Safety Design Bases 5.4.6 Reactor Core Isolation Cooling System 5.4.6.1 Design Bases 5.4.6.2 System Design 5.4.6.4 Preoperational Testing 5.4.7 Residual Heat Removal System 5.4.7.1 Design Bases 5.4.7.2 System Design 5.4.7.4 Preoperational Testing 5.4.9 Main Steam Lines And Feedwater Lines 5.4.9.1 Safety Design Bases 5.4.13.4 Inspection And Testing 6.3 Emergency Core Cooling Systems 6.3.1 Design Bases And Summary Description 6.3.1.1 Design Bases 6.3.1.2 Summary Descriptions Of ECCS 6.3.2 System Design 6.3.3.7 ECCS Analyses For LOCA 6.3.3.8 LOCA Analysis Conclusions 6.3.4 Tests And Inspections 6.3.4.1 *ECCS Performance Tests 7 Instrumentation And Controls 7.1.1.2 Protection Systems 7.1.1.3 Engineered Safety Feature Systems (Controls) 7.1.1.4 Systems Required For Safe Shutdown 7.2 Reactor Protection (Trip) System (Rps) 7.2.1 Description 7.2.1.3 Design Bases 7.3 Engineered Safety Feature Systems 7.3.1 Description 7.3.1.1 System p 7.3.1.2 Design Bases 7.4 Systems Required For Safe Shutdown 7.4.1 Description 10 Steam And Power Conversion System 10.3 Main Steam Supply System 10.3.1 Design Bases 10.3.2 Description 10.4.7 Condensate And Feedwater 10.4.7.1 Design Bases Page 66 of 68 NC.NA-AS.ZZ-0059(Q), Rev.6

NC.NA-AS.ZZ-0059(Q)

FORM-2 10CFR50.59 SCREENING Revision 0 Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package

• 10:47;.2 System Description 10.4.7.3 Safety Evaluation 14 Initial Test Program 14.2 Construction Verification, Preoperational, And Power Test Program 14.2.1 Summary Of Test Program And Objectives 14.2.1.1 Construction Verification Test Program - Phase I 14.2.1.2 Preoperational Test Program - Phase Ii 14.2.1.3 Power Test Program - Phase Iii

.14.2.2 Organization.

14.2.3.5 Preoperational Test Procedures 14.2.3.6 Startup Test Procedures 14.2.4 Conduct Of Test And Startup Program 14.2.7 Conformance Of Test Programs With Regulatory Guides 14.2.8 Use Of Reactor Operating And Testing Experience In The Development Of Test Program 14.2.12.3 Startup Test Procedures 15.0 General 15.1 Decrease In Reactor Coolant Temperature 15.1.1 Loss of Feedwater Heating 15.2.8 Feedwater Line Break 15.2.9 Failure of RHR Shutdown Cooling 15.3 Decrease In Reactor Coolant System Flow Rate 15.3.1 Reactor Recirculation Pump Trip 15.3.1.1 Identification of Causes and Frequency Classification 15.3.4 Reactor Recirculation Pump Shaft Break 15.3.4.1 Identification of Causes and Frequency Classification 15.6 Decrease In Reactor Coolant Inventory 15.6.1 Inadvertent Safety/Relief Valve Opening 15.6.2 Instrument Line Pipe Break 15.6.2.1 Identification of Causes and Frequency Classification 15.6.4 Steam System Piping Break Outside Containment 15.6.4.1 Identification of Causes and Frequency Classification 15.6.5 Loss-of-Coolant Accident Resulting from the Spectrum of Postulated Piping Breaks Within the Reactor Coolant Pressure Boundary Inside Primary Applicable Tech Specs Reviewed; 3/4.3.3 ECCS System Actuation Instrumentation 3/4.3.4 Recirc Pump Trip Actuation Instrumentation 3/4.3.5 RCIC System Actuation Instrumentation 3/4.3.9 Feedwater I Main Turbine Trip Systems Actuation Instrumentation 3/4.4. Reactor Coolant System Page 67 of 68 NCNA-AS.ZZ-0059(Q), Rev.6

NC.NA-AS.ZZ-0059(Q)

FORM-2 1 OCFR50.59 SCREENING Revision 0 Document I.D.: 80062466 Revision: I

Title:

EPU Vibration Monitoring Installation Package 3/4.4.7 Main Steam Line IsolationValves 3/4.4.9 RHR 3/4.5 ECCS 3/4.6 Containment Systems 3/4.7.4 RCIC System 3/4.7.7 Main Turbine Bypass System 3/4.9.11 Residual Heat Removal And Coolant Circulation COMPLETION ANTD APPROVAL 8-23-04 Philip M. Stashak 12-10-04 PREPARER (SIGN) DATE NAME (PRINT) QUAL EXPIRES 10-5-04 J. Annett 2-24-05 REVIEWER (SIGN) DATE NAME (PRINT) QUAL EXPIRES 10-15-04 Dan McHugh 3-11-05 APPROVAL (SIGN) DATE NAME (PRINT) QUAL EXPIRES Page 68 of 68 NC.NA-AS.ZZ-0059(Q). Rev.6

Technical Basis for Acceptance Criteria for Hope Creek Vibration

• Technical guidance for the acceptance criteria base on ASME OM-S/G-1994, Standards and Guides for Operation and Maintenance of Nuclear Power Plants, Part 3, 1994 Edition, "Requirements for Preoperational and Initial Start-Up Vibration Testing of Nuclear Power Plant Piping Systems."

• The equation from OM Part 3 for the stress criteria is given below:

Salt = C2K2 MK2<SeI /a z

• Salt is determined per Section HI of the ASME Code, Paragraph NB-3600 for piping.

• The acceptance criteria for the accelerations to be measured is determined by multiplying the calculated acceleration at each sensor location in a unit load analysis by the ratio of the allowable steady state stress to the maximum calculated stress in the piping system.

Page I of 1 Bhavnani, Dilip S.

From: Bhavnani, Dilip S.

Sent: Wednesday, October 27, 2004 10:01 AM To: Carey, John D.

Subject:

FW: Draft Piping Vibration Acceptance Criteria Calculations FYI

---

Original Message ---

From: Karen Fujikawa [mallto:kfujikaw~stru~,tint.com]

Sent: Monday, August 02, 20 4A:341't4 To: Phil Stashak Cc: 'Bhavnanl,' p.

Subject:

D ftPiping Vibration Acceptance Criteria Calculations

Phil, Draft calculations fo e.virtion accptarce-cri eahave been uploaded to the ibackup website in the directory called %acceptancecriteria. The following calculations are located in the directory:

Si Calculation No. HC-04Q-308 Rev. A, "Inside Drywell Feedwater Loop A Piping Vibration Acceptance Criteria" Si Calculation No. HC-04Q-309 Rev. A, "Outside the Drywell Feedwater Piping Vibration Acceptance Criteria" SI Calculation No. HC-040-311I Rev. A, "Outside the Drywell Main Steam Piping Vibration Acceptance Criteria" SI Calculation No. HC-04Q-312 Rev. A, "Main Steam Line A Piping Vibration Acceptance Criteria" SI Calculation No. HC-04Q-313 Rev. A, "Main Steam Line B Piping Vibration Acceptaance Criteria" I have also included the website address below (the address Is the same one that we have been using). Let me know if you have any comments/questions.

This is an email sent from IMackup on behalf of the sender.It may contain links to the files/folders that the sender chose to share with you.

Here are the links:

1. Folder: HC-04Q Secure Link:. https://www.ibackup.com/cimanager/servlet/share?key=954511I5900543969ssss Regards, Karen cc: HC-04Q-1 06, -308, -309, -311, -312, -313 11/3/2004

FILE No.: HC-04Q-311

<A' STRUCTURAL CALCULATION INTEGRITY PACKAGE PROJECT No.: HC-04Q Associates, Inc.

PROJECT NAME: Hope Creek Extended Power Uprate Piping Vibration Monitoring CLIENT: PSEG Nuclear, LLC (Hope Creek)

CONTRACT NUMBER: 4500226359 Including C.O. #1 CALCULATION TITLE: Outside the Drywell Main Steam Piping Vibration Acceptance Criteria Project Mgr. Preparer(s) &

Document Affected Approval Checker(s)

Revision Pages Revision Description Signature & Signatures &

Date Date A 1-7 DRAFT Issue K. K. Fujikawa Carl R. Limpus Appendix A 7/29/2004 7/29/2004 Al-AS William F. Weitze In 7/29/2004 Computer Files Page 1 of 7 F2001Rl

Table of Contents

1.0 INTRODUCTION

..................................................................... 3 2.0 VIBRATION ACCEPTANCE CRITERIA THEORY .................................................................... 3 3.0 CALCULATION OF ACCEPTANCE CRITERIA ..................................................................... 4

4.0 REFERENCES

..................................................................... 7 APPENDIX A FILES .................................................................... Al List of Tables Table 1: Nodal Accelerations and Acceptance Criteria Due to 1g Spectrum Input ................................. 5 Table 2: Nodal Displacements and Acceptance Criteria Due to lg Spectrum Input ............................... 5 List of Figures Figure 1: Outside Drywell MS Piping PIPESTRESS model, including Accelerometer Locations ......... 6

1.0 INTRODUCTION

The purpose of this calculation is to develop vibration acceptance criteria for the accelerometers installed on the Hope Creek main steam piping located outside the drywell.

2.0 VIBRATION ACCEPTANCE CRITERIA THEORY The acceptance criterion is based on the guidance of ASME OM SIG Part 3 [1], which states that the calculated stress shall not exceed S.:/a. The equation from OM Part 3 for the stress criterion is given below:

Salt =C2K2MSe l/a

. z Where Sait = Alternating stress as defined in ASME Code (NB-3600)

C2 = Secondary stress index as defined in ASME Code K2 Local stress index as defined in ASME Code M = Maximum zero to peak dynamic moment loading due to vibration only Z Section modulus of the pipe Sa = 0.8SA, where SA is the alternating stress at 106 cycles from Figure I-9.1 of Section III of the ASME Code [2] for carbon steel a = Allowable stress reduction factor, 1.3 for carbon steel The piping within the scope of this analysis is A106 Grade B carbon steel [3]. For carbon steel pipe, SA = 12,500 psi, thus, the maximum allowed stress due to steady state vibration is 0.8*12,500 psi /1.3

= 7692 psi.

The acceptance criteria for the accelerations to be measured are determined by multiplying the calculated acceleration at each sensor location in a unit load analysis by the ratio of the allowable steady state stress to the maximum calculated stress in the piping system. This may be expressed by multiplying the accelerations for each direction by a factor, and the factor is defined as:

F = 7692 psi / <max

- where-F-is the factor and-affc-is-the maximum-stress obtained -fromthe dynamic analysis..

It should be noted that exceedance of the allowable acceleration or displacement in one direction at a location does not necessarily indicate exceedance of the OM-3 criteria, as the stresses at a location are a function of the SRSS combination of the accelerations in three orthogonal directions. In addition, review of the frequency content of the collected data may allow for refinement of the shape of the input response spectra. The acceptance criteria are conservative, and if met, will eliminate the need for further review to justify the acceptability of the measured accelerations.

t Revision Al File No. HC-04Q-311 Page 3 of 5

3.0 CALCULATION OF ACCEPTANCE CRITERIA A PIPESTRESS [4] model was developed in Reference [3] and is shown in Figure 1. A flat I g spectrum was applied (0.lg below 5 Hz) in each of the three orthogonal directions. Static. loads such as weight and thermal expansion are not considered since these loads do not contribute to the vibration loading of the piping system. Additionally, seismic (inertia and anchor movements) and turbine stop valve loads are not considered since these loads are transient dynamic loads and do not contribute to the steady-state cyclic loading of the system.

Due to extended power uprate, the flow in the main steam lines will increase, which can potentially cause the vibration of the piping to increase due to flow induced vibration. Since the forcing function can occur over a range of frequencies, a broad band amplified response spectra (ARS) of lg from 5 to 100 Hz, applied in each direction, and was used to analyze the main steam piping system. To account for modes below 5 Hz, 0.lg is input for 0.35 to 5 Hz. The acceleration is lower in this range because a 1g input would yield unrealistically high displacements. This dynamic analysis provides the response of the piping system to a broad band ARS that corresponds to white noise input. As the vibration is flow induced, the vibration loading was applied only to the sections of piping normally containing flow. The displacements, accelerations and stresses due to the broad band ARS in each of the three orthogonal directions were calculated at each node in the piping system. The total response was obtained by combining the results from each of the three directions by square-root-sum-of-the-squares.

The calculated maximum stress in the model due to a Ig input in each direction is 38,457 psi at Node 140. Acceptance criteria are calculated for the 4 accelerometer locations. They are nodes Z013, Z018, Z003, and Z008. The locations of the accelerometers are shown in Figure

1. Reference [3] provides details of the accelerometer locations. The acceleration acceptance criterion calculation for Node Z013 is shown below. The acceleration values for each node are shown in Table I and the displacement values are shown in Table 2.

A.= 7692 /38457

• 1.062 g = 0.212 g Ay= 7692/38457

• 1.220 g = 0.244 g A. = direction not monitored a Revision A l File No. IC-04Q-311 Page 4 of 5

Table 1: Nodal Accelerations and Acceptance Criteria Due to Ig Spectrum Input Acceleration (g) Acceptance Criteria (g)

Node (X) (Y) (Z) (X) (Y) (Z)

Z013 1.062 1.220 1.067 - 0.212 0.244 -

Z018 0.996 0.817 1.183 0.199 0.163 0.237 Z003 1.126 1.121 1.086 - 0.225 0.224 - I ZOOB 1.082 1.239 1.638 0.216 0.248 0.328 Table 2: Nodal Displacements and Acceptance Criteria Due to ig Spectrum Input Displacement (in) Acceptance Criteria (in)

Node (X) (Y) (Z) (X) (Y) (Z)

Z013 0.033 0.040 0.042 0.007 0.008 -

Z018 0.067 0.018 0.151 0.013 0.004 0.030 Z003 0.028 0.030 0.042 0.006 0.006 --

Z008 0.087 0.051 0.182 0.017 0.010 0.036

-!--!I-,- - File No. HC-04Q-311

ark__ 3._ _AM 20C1 (WIND w 91f rigure Ar STAkmDmmfl VrEw I ICALX '/114 ~ETT 01:1 O Figure 1: Outside DrYnvell MS Piping PIPEDSTRESS model, including Accelerometer Locations Revision A File No. HC-04Q-311 Page 6 of 6

4.0 REFERENCES

1. ASME OM-S/G-1994, Standards and Guides for Operation and Maintenance of Nuclear Power Plants, Part 3, 1994 Edition, "Requirements for Preoperational and Initial Start-Up Vibration Testing of Nuclear Power Plant Piping Systems."

2. ASME Boiler and Pressure Vessel Code,Section III Appendices, 1989 Edition.

3. Structural Integrity Associates Calculation, Revision 0, "Outside the Drywell Main Steam Piping Vibration Monitoring Locations," SI File No. HC-04Q-305.

4. PIPESTRESS, Version 3.5.0 +67. DST Computer Services, S.A.

Revision I A I I I File No. HC-04Q-311 Page 7 of 7

APPENDIX A FILES File Name Size Date & Time Description Location Cl OR8A-ACrl.fre 22.9 KB (23,520 bytes) 8:32 08 PIPESTRESS input file A2 to A8 COR8A-ACLprc 354 B (363,4July29, 2004, PIPESTRESS output file - In computer file 8:35:49 AM accelerations CIORBA-AC rI.prf 350 KB (359.370 bytes) July 29,204, PRESTRESS output file - stresses In computer file Revision A A l I File No. HC-04Q-311 Page Al of A8

IDEN JB-1 *JOB NO. (1 to 9999)

CD=i *0=ANSI/ASME B31.1

• 1-ASME Class 1

• 2-ASME Class 2

• 3=ASME Class 3

• 4=ANSI/ASME B31.3

• 5-SNCT (French petrochemical)

• 6=KTA (German Class 1)

• 7-RCC-M (French Class 1)

• B=RCC-M (French Class 2)

• 9=KTA (German Class 2)

• N=ASME Code Case N-155 (composite)

GR--Y *Direction of gravity VA-0 *0=Calculation 2-Verification 3-Design (HANGIT)

IU-l *Input units 0-SIU 1-USA 2-USA2 OU- *Output units 0=SIU 1-USA CH-S *Delimiter character replaces ?

ABET *FREE errors - terminate execution PL-$PROB-MONITOR LOCATIONS PROJ-HC-04Q.

EN-$USER-CRL/SIS TITL EL-8 *Modelling option

• 0 - concentrated mass for static analysis

• concentrated mass for dynamic analysis

• no rotational inertia

• 3 - uniform mass for static analysis

• concentrated mass for dynamic analysis

• no rotational inertia

• 7 - concentrated mass for static analysis

• concentrated mass for dynamic analysis

• calculate rotational inertia

• 8 - uniform mass for static analysis

• concentrated mass for dynamic analysis

• calculate rotational inertia GL-l *Print forces/moments 0-Global 1-Local 2-G and L SU-0 *Type 1 support summary 0-No 1-Yes CV-10 *Code version (see Manual)

HS-l *Report 20 highest stress ratios for each load case MD-1 *Hot modulus J6-1 *Skip minor WARNING messages TI-$MAIN STEAM OUTSIDE DRYWELL $

FREQ RF-1 RP-8 FR-100 MP-20 MX-100 TI-$MODAL$

• • • THERMAL EXPANSION LOAD CASES

• LCAS CA-1 TY-0 TI-$Normal Operation$

• • • WEIGHT LOAD CASES

• LCAS CA-101 TY-3 TI-$OPERATING WEIGHTS

• • • SEISMIC CASES

• RCAS CA-201 EV-l TY-1 SU-l FX-1 FY-0 FZ-0 TI-$X VIBRATIONS RCAS CA=202 EV-l TY-l SU-1 FX-0 FY-l FZ-0 TI-$Y VIBRATIONS RCAS CA-203 EV-1 TY-1 SU-1 FX-0 FY-0 FZ-1 TI-$Z VIBRATIONS

• • • • LOAD COMBINATION CASES

• CCAS RF-1 CA-401 SS-1 ME-2 EQ=3 CI-201 C2-202 C3-203 FL-1 TI-$VIBRATION STRESS+$

CCAS RF-1 CA-402 SS-1 ME-0 EQ-3 Cl-401 Fl--l TI-$VIBRATION STRESS-S

. _**** LQAD-SETS

• ___ _ _ ___ __

LSET RF-1 PR-1 MO-1 LSET RF-1 FL-1 FC-0 PR-1 MO-401 TI-$+VIB$

LSET RF-1 FL-1 FC-0 PR-1 MO0402 TI-$-VIES SPEC FS-EVENT1 EV-1 ME-3 TI-SVIBRATION SPECTRUMS LV-1 DI-X 0.35/0.1 5.0/0.1 5.1/1.0 100.0/1.0 DI-Y 0.35/0.1 5.0/0.1 5.1/1.0 100.0/1.0 DI-Z 0.35/0.1 5.0/0.1 5.1/1.0 100.0/1.0 Revision A File No. HC-04Q-311 Page A2 of A8

• • MATERIAL PROPERTIES ***********************

• ASTM A-106 Grade B MATH CD-106 EX-0 TY-1 *C-Si MATD TE-70 EH=29.5 EX-0 SM-20.0 SY-35.0 MATD TE-100 EH-29.3 EX-0.21 SM-20.0 SY-35.0 MATD TE-200 EH-28.8 EX-0.95 SM-20.0 SY-31.9 MATD TE-300 EH-28.3 EX-1.77 SM-20.0 SY-31 MATD TE-400 EH-27.7 EX-2.67 SM-20.0 SY-30 MATD TE-500 EH-27.3 EX-3.64 SM-18.9 SY-28.3 MATD TE-600 EH-26.7 EX-4.63 SM=17.3 SY-25.9

• • • • • • • • • • • • • • • GEOMETRY ******************************

• • • • • • • • • • • • • • • • • MAIN STEAM~ LINE B *~**************~****

MATL CD-106 DESN TE-70 PR-0 OPER TE-70 PR-0 CA-1 OPER TE-70 PR-0 CA-101 CROS OD-26.0 WT-1.158 MA-342.2 IN-3.

• Location of Flued Head B COOR PT-FHB AX-11.000 AY-107.000 AZ--49.208 *GLOBAL ORIGIN ANCH PT-FHB KX-7.616E4 KY-2.666E4 KZ-2.885E4 MX-2.29E6 MY-2.82E6 MZ-3.96E7 CROS OD-26.0 WT-1.158 MA-342.2 IN-3.5 TANG PT-10 DX-0 DY-0 DZ--3.8333 CROS OD-26 WT-2 .316 MA-0.001 KL-1 VALV PT-IVB DZ--3'7" OD-26 WT-2.316 PL-1 PB-IVBM MA-0.12559 VALV PT-15 DZ--1'8" OD-26 WT-2.316 PL-2 PB-15M MA-0.05841 JUNC PT-IVB VALV PT-SBI DX-0.291 DY-1. 459 DZ-1.4299 OD-26 WT-2.316 PL-3 AL-$V033$

VALV PT-SB2 DX-0.063 DY--0.316 DZ-.3095 OD-26 WT-2.316 PL-3 MA-9.52 JUNC PT-SB1 VALV PT-SB3 DX-0.32 DY-1. 605 DZ-1.573 OD-26 WT-2.316 PL-3 VALV PT-OPE3 DX-0.538 DY-2.699 DZ-2.645 MA-2.78 PL-3 JUNC PT-15 CROS OD-26.0 WT-1.125 MA-333.9 IN-3.5 TANG PT-16 DX-0 DY-0 DZ--0.833 *DTI-1-P-AB-638 TANG PT-17 DX-0 DY-0 DZ--0.5 *DRAIN LINE EXTENTIONS TANG PT-20 DX-0 DY-0 DZ--2.0833 *DTI-AB-021-H05 RSTN PT-20 DX-1.0 SD-15000 AL-$AB-021-H05X$

RSTN PT-20 DY-i SD-2.765E3 AL-$AB-021-H05Y$

TANG PT-25 DX-0 DY-0 DZ--4.5

• TANG PT-26 DX-0 DY0 DZ--3.250 *BEND BEGIN-BRAD PT-27 RA-3.25 *BOTTOM BEND

• TANG PT-28 *DX-0 DY-3.25 DZ-0 *TOP BEND TANG PT-30 DX-0 DY-4.292 DZ-0 *DTI-AB-021-H03 RSTN PT-30 DX-l SD-14469 AL-$AB-021-H03$

TANG PT-35 DX-0 DY-4.70833 DZ-0 *DTI-1-P-KP-204 TANG PT-40 DX-0 DY-5.750 DZ-0 *DTI-AB-021-H04 RSTN PT-40 DX-1 SD-14469 AL-SAB-021-H04$

TANG PT-45 DX-0 DY-4.791 DZ-0

• TANG PT-46 DX-0 DY-3.25 DZ-0 *BEGIN OF BEND BRAD PT-46A RA-3.25 *TOP BEND

• TANG PT-46B DX-0 DY-0 DZ--3.25 *TOP OF BEND A

Page A3 of A8

TANG PT-47 DX-0 r)Y-C DZ--4.5 *DTIPP-1-AB-658 TANG PT-50 DX-' I)Y-C DZ--1.500 VALV PT-VB DZ--2.625 IPL-1 IA-12.374 OD526 V WT-2.:25 AL-SVC04S VALV PT-BOP DY-7.6667 IPL-3 iA-1.85 OD=26 WT-2.:25 JUNC PT-VB VALV PT-55 DZ--2.625 IPL-2 OD-26 IWT- 2. 25 CROS OD-26.0 WT-0.938 I4A=28 6.1

• TANG PT-56 DX-0 DY-C DZ--1.000

• TANG PT-57 DX-O DY-C DZ--1.000 CRED PT-57 DX-0C DY-0 DZ--2 .000 CROS OD-28.0 WT-1.0 I4A-32 5.7 IN-3.5 TANG PT-60 DX-O IDY-0 DZ--O. 781 *LOCATION OF HANGER H17 RSTN PT-60 DX-1 AL-$AB-002-HI7$

TANG PT-61 DX-0 IDY-C DZ--0.4688 *LOCATION OF HANGER H16 TANG PT-62 DX-O IDY-0 DZ--0. 5833 *LOCATION OF HANGER H15 TANG PT-64 DX-0 IDY-0 DZ--41.875 *LOCATION OF HANGER H14 RSTN PT-64 IDY-1 AL-$AB-002-HI4 $

TANG PT-66 DX-0 IDY-0 DZ--9.6875 *LOCATION OF HANGER H13 RSTN PT-66 DX-1 AL-$AB-002-H13$

TANG PT-67 DX-0 DY-0 DZ--22.063 *LOCATION OF HANGER H12 RSTN PT-67 DX-1 AL-$AB-002-H12$

TANG PT-68 DX-0 DY-0 DZ--6.4583 *LOCATION OF HANGER H11 RSTN PT-68 DY-1 AL-$AB-002-Hll$

TANG PT-72 DX-0 DY-0 DZ--37.542 *LOCATION OF HANGER H09 RSTN PT-72 DY-1 AL-$AB-002-HO9$

TANG PT-721 DX-0 DY-0 .DZ--0.6094 *LOCATION OF HANGER H10 TANG PT-73 DX-0 DY-0 DZ--5.724 TANG PT-74 DX-0 DY-0 DZ--12.458 *LOCATION OF HANGER H08 TANG PT-75 DX-0 DY-0 DZ--5.75

• TANG PT-76 DX-0 DY-C 3 DZ--3.500 *BEGIN BEND BRAD PT-78 RA-3.500 *BEND FROM Z TO X

• TANG PT-79 DX--3.5 DY-C DZ-0 *END BEND TANG PT-80 DX--4.0C33 DY-0 DZ-O *LOCATION OF HANGER H07 RSTN PT-80 DY-1 AL-$AB-002-HC7$

TANG PT-89 DX--41.958 DY-0 DZ-0 *LOCATION OF HANGER H06 TANG PT-90 DX--1.750 DY-0 DZ-C *LOCATION OF HANGER H05 RSTN PT-90 DY-1 AL-SAB-O02-HO5$

TANG PT-95 DX--35.833 DY-0 DZ-0 *LOCATION OF HANGER H04 RSTN PT-95 DY-1 AL-$AB-002-H04 $

TANG PT-100 DX--8.1667 DY-0 DZ-0

• TANG PT-101 DX--3.5 DY--0 DZ-0 *BEGIN BEND BRAD PT-101A RA-3.500 *BEND FROM X TO Z

• TANG PT-101B DX-0 DY-( DZ--3.5 *TOP OF BEND TANG PT-102 DX-0 DY-0 DZ--4.5 *LOCATION OF HANGER H03 TANG PT-105 DX-0 DY-0 DZ--2.7083 TANG PT-110 DX-0 DY-0 DZ--5.3333 *LOCATION OF HANGER H02 RSTN PT-110 DY-1 AL-SAB-002-H02$

TANG PT-lll DX-0 DY-0 DZ--7.6667 *LOCATION OF HANGER H01 TANG PT-112 DX-0 DY-0 DZ--4.3333 *DTI-P-1-AB-605 TANG PT-12A DX-0 DY-0 DZ--4.500 *DTI-P-1-AB-646 TANG PT-113 DX-O DY-C DZ--0.250 *DTI-TE-1004B TANG PT-114 DX-0 DY-0 DZ--0.750 *DTI-P-1-AB-649 TANG PT-115 DX-0 DY-C DZ--6. CCC *Line off maini;DTI-28X12WDLET CROS OD-12.75 WT'-.687 MA-105.7 IN-3.0 BRAN PT-11S DXC0 DY--1.1667 DZ-0 TE-6 INDI AT-118 C2-2.159 IK2-2.0 TANG PT-120 DX-0 DY--1.3333 DZ-0 LUMP PT-120 MA-0.082 JUNC PT-115 *MAIN LINE TO MSV-4 CROS OD-28.0 WT-1.0 MA-325.7 IN-3.5 TANG PT-125 DX-0 DY-0 DZ--1.500 INDI AT-125 C2-1.513 E2-2.0

• Connection to MSV-4 CROS CD=80 0D-80 WT-12 MA-4700.00 KL-1 l Revision l A I I

. L.Filel No. HC-04Q-311 Page A4 of AS

TANG PT-SV4 DX-0 DY-0 DZ-4. 000 *DTI-CV-MS-4 CROS CD-80 MA-0 RL-1 BRAN PT-126 DX-3.625 DY-0 DZ-0 TE-2 RSTN PT-126 DY-1 AL-$CV-MS-4$

JUNC PT-SV4 CROS CD-80 MA-4700 EL-1 BRAN PT-SVB DX--3.25 DY-0 DZ-0 TE-2 TANG PT-SV3 DX--3.25 JUNC PT-SV4 BRAN PT-CV3 DX-O DY--8.6458 DZ--7.0833 TE-2 VSUP PT-CV3 DY-1 SP-0 .001 FO=53.5 TANG PT-140 DX-0 DY--4.0 INDI AT-140 C2-1.533 K2-2.0 CROS OD-28 WT-1.4 MA'435.0 IN-3.5

• LINE AC-009-VBT-28 TANG PT-146 DX-0 DY--6.052 DZ-0 *DTI-AC-009-HOI TANG PT-144 DX-0 DY--0.3854 DZ-0 *DTI-AC-009-H02 TANG PT-150 DX-0 DY--3.9167 DZ-0

• TANG PT-151 DX-0 DY--3.5 DZ-0 *BEGIN OF BEND BRAD PT-152 RA-3.5 *BEND

• BRAD PT=152A DX-0 DY-0 DZ--3.5 *END OF BEND TANG PT-153 DX-0 DY-0 DZ--8.0 *DTI-AC-009-H03 TANG PT-155 DX-0 DY-O DZ--29.417 AL-$AC-009-HO4$

TANG PT-160 DX-0 DY-0 DZ--4.5 BRAD PT-160B RA-3.5 TANG PT-165 DX--6.2083 DY-17.375 DZ-0 BRAD PT-166 PA-14 TANG PT-167 DX-0 DY-10 DZ-0 *DTI-AC-009-HOS RSTN PT-167 DZ-1 AL-$AC-009-H05$

TANG PT-NZ9 DX-0 DY-8.0 DZ-0 INDI AT-NZ9 C2-1.533 R2-2.0 CROS OD-96 W1T-15 MA-0.001 KL-1 TANG PT-MB2 DX-12.5833 DY-5.25 DZ-2.0 AL-STURBINE$

ANCH PT-MB2 CROS OD-10.75 WT-.718 MA-92 IN-3.0 JUNC PT-17 BRAN PT-18 DX-0 DY--1.0833 DZ-0 TE'6 INDI AT-18 C2-1.594 K2-2.0 TANG PT-i9 DX-0 DY--1.1667 DZ-0 LUMP PT-l9 MA-.071 MAIN STEAM LINE A

• CROS OD-26.0 WT-1.158 MA-342.2 IN-3.5

• Location of Flued Head COOR PT-FHA AX-3.958 AY-107.000 AZ--49.208 *GLOBAL ORIGIN 3.958 ANCH PT-FHA KX-5.89E4 KY-1.55E4 KZ-2.04E4 MX-2.01E6 MY-1.65E6 MZ-1.87E7 TANG PT-180 DX-0 DY-0 DZ--3.8333

• CROS OD-26 WT-2.316 MA-0.001 KL-1 VALV PT-IVA PL-1 DZ--3'7" OD-26 WT-2.316 PB-IVAM HA-.12559 VALV PT-185 DZ--1'8" PL-2 MA-0.05841 JUNC PT-IVA-2.36 PB-185 VALV PT-SA1 DX--0.291 DY-1.459 DZ-1.4299 OD-26 WT-2.316 PL-3 AL-$V033$

VALV PT-SA2 DX--0.063 DY--0.316 DZ-.3095 OD-26 WT-2.316 PL-3 MA-9.52 JUNC PT-SA1 VALV PT-SA3 DX--O.32 DY-1.605 DZ-1.573 OD-26 WT-2.316 PL-3 VALV PT-OPA DX--0.538 DY-2.699 DZ-2.645 MA-2.78 PL-3 JUNC PT-185 *VALVE V032 Revision I A I I I File No. HC-04Q-311 Page A5 of AS

CROS o D-2 6.0 WT'1.125 MA-333.9 IN-3.5 TANG PT-18A DX-0 DY-0 DZ--0.833 *DTI-P-1PAB-637 TANG PT-187 DDX-0 DY-0 DZ--0.5 *DRAIN LINE EXTENTIONS JUNC PT-187 CROS 0DD=10.75 WT-.718 MA-92 IN-3.0 *10 IN LINE BRAN PT-188 DIX-0 DY--1.0833 DZ-0 TE-6 INDI AT-188 C:2-1.594 K2-2.0 TANG PT-189 DDX-0 DY--1.1667 DZ-0 LUMP PT-189 MMA-. 071 JUNC PT-187 *BACK TO THE MAIN LINE CROS C)D-26.0 WT-1. 125 MA-333.9 IN-3.5 TANG PT-190 r)X-0 DY-0 DZ--2.0833 *ETI-AB-020-H05Y RSTN PT-190 D)X-1 SD-15000 AL- $AB-020-H{05X$

RSTN PT-190 DY-1 SD-2765 AL-$AB-020-HO5YS TANG PT-195 DX-0 DY-0 DZ--4.5

• TANG PT-196 DX-0 DY-0 DZ--3.250 *BEND BEGIN BRAD PT-197 RA-3.25 *BOTTOM BEND

• TANG PT-198 DX-O DY-3.25 DZ-( *TOP BEND TANG PT-200 DX'O DY-4.292 DZ-0 *DTI-AB-020-H03 RSTN PT-200 DX-1 SD-14469 AL-$AB-020-HO3$

TANG PT205 DX-0 DY-4.70833 DZ-0 *DTI-1-P-KP-204 TANG PT210 DX-0 DY-5.750 DZ-0 *DTI-AB-020-H04 RSTN PT-210 DX-1 SD-14469 AL-$AB-020-H04$

TANG PT-215 DX-0 DY-4.791 DZ-0

• TANG PT-216 DX-0 DY-3.25 DZ-( *BEGIN OF BEND BRAD PT-216A RA-3.25 *TOP BEND

• TANG PT-216B DX-0 DY-0 DZ--3.25 *TOP OF BEND TANG PT-217 DX-0 DY-0 DZ--4.5 *DTI-P-1-AB-657 TANG PT-220 DX-0 DY-0 DZ--1.500 VALV PT-VA IDZ--2.625 PL-1 MA-6.187 OD-26 91T-2.25 PB-VAM VALV PT-AOP IDX--.5348 DY-7.648 PL-3 DD-26 WT-2.25 MA-1.85 JUNC PT-VA VALV PT-224 DZ--2. 625 PL-2 0D-26 WT-2.25 PB-224M MA-6.187 CROS OD-26.0 WT-0.938 FA-286.1 CRED PT-227 DX-0 DY-0 DZ--2.000 CROS CD28 OD-28.0 WT-1.0 MA-325.7 IN-3.5 TANG PT-230 DX-0 DY-0 DZ--0.8333 *ETI-AB-001-H17 RSTN PT-230 DX-1 AL-$AB-001-H18$

TANG PT-231 DX-0 DY-0 DZ--0.4166 *DTI'P1-AB-620 TANG PT-23A DX-0 DY-0 DZ--0.5 *DTI-1-P-AB-06 TANG PT-233 DX-0 DY-0 DZ--0.7708 *DTI-AB-001-H16 VSUP PT-233 DY-1 SP-2.35 FO-23.228 AL-$AB-001-H16$

TANG PT-234 DX-0 DY-0 DZ--41.146 *DTI-AB-001-H15 RSTN PT-234 DY-1 AL-$AB-D01-H15$

TANG PT-236 DX-0 DY-0 DZ--12.73 *DTI-AB-001-H14 RSTN PT-236 DX-1 AL-$AB-001-H14$

TANG PT-237 DX-0 DY-0 DZ--21.396 *DTI-AB-001-H13 RSTN PT-237 DX-1 AL-$AB-001-H13$

TANG PT-238 DX-0 DY-0 DZ--5.75 *DTI-AB-001-H12 RSTN PT-238 DY-1 AL-SAB-001-H1l2$

TANG PT-240 DX-0 DY-0 DZ--33.0 TANG PT-242 DX-0 DY-0 DZ--2.75 *DTI'AB-001-Hll

--RSTN-PT-242 DY-1;0- AL-$AB-001-Hll$-

TANG PT-243 DX-0 DY-0 DZ--1.833 *DTI-AB-001-H1O TANG PT-244 DX-0 DY-0 DZ--11.125 *DTI-AB-001-HO9 TANG PT-245 DX-0 DY-0 DZ--5.75

• TANG PT-246 DX-0 DY-0 DZ--3.500 *BEGIN BEND BRAD PT-247 RA-3.500 *BEND FROM Z TO X

• TANG PT-248 DX--3.5 DY-0 DZ-D *END BEND TANG PT-250 DX--5.667 DY-O DZ-0 *DTI-AB-001-H08 RSTN PT-250 DY-i AL-SAB-001-H08$

TANG PT-260 DX--34.833 DY-0 DZ-0 *DTI-AB-001-H07 RSTN PT-260 DY-1 AL-$AB-001-H07$

TANG PT-262 DX--15.750 DY-0 DZ-0 *DTI-AB-001-H06 Revision A . 1 File No. RC-04Q-311 Page A6 of A8

TANG PT-265 I )X-G20.250 DY-0 DZ-O *DTI-AB-001-H05 RSTN PT-265 DY-1 AL-SAB-O0l-HO5$

TANG PT-270 I)X-14.750 DY-0 DZ-O

• TANG PT-270A DX--3.5 DY-0 DZ-0 *BEGIN BEND BRAD PT-270B RA-3.500 *BEND FROM X TO Z

• TANG PT-270C DX-0 DY-0 DZ--33.5 *TOP OF BEND TANG PT-27A DX-0 DY-0 DZ--4. 1667 *DTI-AB-001-H03 TANG PT-271 DX-O DY-0 DZ--l. C TANG PT-272 DX-0 DY-0 DZ--1. C *DTI-AB-001-H04 RSTN PT-272 DY-1 AL-SAB-001-HC4$

TANG PT-275 DX-0 DY-0 DZ--4. 9583 TANG PT-278 DX-0 DY-0 DZ--3. 8333 *DTI-AB-001-H02 TANG PT-280 DX-0 DY-0 DZ--4. 500 *DTI-AB-001-H0I RSTN PT-280 DY-1 AL-$AB-0Ol-HOI$

TANG PT-281 DX-0 DY-0 DZ--1 .4.948 *DTI-P-1-AB-606 TANG PT-282 DX-0 DY-0 DZ--00.553 *DTI-P-1-AB-64 5 TANG PT-283 DX-0 DY-0 DZ--00.25 *DTI-TE-1004A TANG PT-284 DX-0 DY-0 DZ--0).75 *DTI-P-1-AB-649 TANG PT-285 DX-0 DY-0 DZ--(6.0 *DTI.28X12WDLET CROS OD-12.75 WT-.687 MA-IC05.7 IN-3.0 BRAN PT-288 DX-0 DY--1.1667 DZ-0 ITE-6 *12" BRANCH LINE INDI AT-288 C2-2.159 K2-2.0 TANG PT-290 DX-0 DY--1.3333 DZ-0 LUMP PT-290 MNA-0. 082 JUNC PT-285 *MAIN LINE TO MSV-3 CROS OD-28.0 WT-I.0 MA-325.7 IN-3.5 TANG PT-295 DX-0 DY-0 DZ--l.5833 INDI AT-295 C2-1.513 E2-2.0

• From earlier in ME101 file CROS OD-80 WT-12 MA-4700.00 KL-1 JUNC PT-SV3 TANG PT-EQM DX--3.25 VSUP PT-EQN DY-1 SP-0.001 FO-140 KL-i TANG PT-SV2 DX--3.25 AL-SPERTYAPPLIED$

TANG PT-SVA DX--3.25 AL-$CV-000-HC2$

SNUB PT-SVA DZ-1 SP-1970 TANG PT-SVl DX--3.25 DZ--.0833 AL-$ATGESTOPANDC$

CROS CD-80 MA-0 KL-i TANG PT-127 DX--3.25 RSTN PT-127 DY-1 AL-$CV-MS-I$

SNUB PT-127 DX-l SP-2557 JUNC PT-SV3 CROS CD-80 MA-4700 BRAN PT-CV4 DY--8.6458 DZ--7.0833 TE-2 AL-$CV-MS-7$

VSUP PT-CV4 DY-1 SP-0.001 FO-53.5 AL-$CV-MS-7$

TANG PT-310 DY--4.0 AL-$SASTIFFMODEL$ *JOINT-TRP INDI AT-310 C2-1.513 K2-2.0 JDNC PT-SV2 TANG PT-CV2 DY--8.6458 DZ--7.0833 AL-$CV-MS-6$

VSUP PT-CV2 DY-1.0 SP-0,001 F0-53.5 AL-$CV-MS-6$

TANG PT-480 DY--4.0 AL-$RESULTEDFROM$

JUNC PT-SV1 TANG PT'CVI DY--8.6458 DZ--7.0000 AL-$CV-MS-5$

VSUP PT-CV1 DY-1.0 SP-0.001 FO-53.5 AL-$CV-MS-5S TANG PT-660 DY--4.0 AL-$PREVIOUSCALS$

JUNfC PT-SV3-BRAN PT-295 DZ-4.0 TE-2 *JOINT-TRP JUNC PT-SV2 BRAN PT-465 DZ-4.0 TE-2 *JOINT-TRP JUNC PT-SV1 BRAN PT-645 DZ-4.0 TE-2 *JOINT-TRP JUNC PT-310 CROS OD=2 8.0 VIT1.4 MA-435 IN-3.5 TANG PT-316 DX-0 DY--5.9375 DZ-0 *DTI-AC-008-HO1 TANG PT-314 DX-o DY--0.5 DZ-C *DTI-AC-008-HO2 TANG PT-320 DX-0 DY--3.9167 Dz-0 BRAD PT-321 RA-3.5 Revision I A I I File No. HC-04Q-311 Page A7 of A8

TANG PT-322 DX-0. 0741 DY-0 DZ--8.0 *DTI-AC-008-HO3 TANG PT-330 DX-0.2167 DY-0 DZ--23.5 *DTI-AC-008-H104 BRAD PT-331 RA-3.5 TANG PT-332 DX-0 DY-4.58333 DZ-0 *DTI-AC-008-H04 TANG PT-334 DX-0 DY-22.7813 DZ-0 *DTI-AC-008-H05 vSUP PT-334 DY-1 SP-7.094 FO-33.7 AL-$AC-008-HO5$

TANG PT-335 DX-0 DY-20.4583 BRAD PT-336 RA-2.333 TANG PT-NZ8 DX-0 DY-0 DZ--3.0 INDI AT-NZ8 C2-1.533 K2-2.0 CROS OD-96 VWT-15 MA-0.001 KL-1 TANG PT-MB2 DX-12.5833 DY--7.1979 DZ--5.4167 JUNC PT-MB2

• • • • • • • • • • • SYSTEM P;ESTRAINTS/ SUPPORTS **********~*******

• LINE B RESTRAINTS SNUB PT-60 DX-0 DY-1 DZ-0 SP-752.4 VSUP PT-62 DX-0 DY-1 DZ-0 SP-2.35 FO-23.503 * .1 -

SNUB PT-74 DX-0 DY-0 DZ-1 SP-3571 SNUB PT-102 DX-1 DY-0 DZ-O SP-1331.2 SNUB PT-lll DX-0 DY-0 DZ-1 SP-3082.7 SNUB PT-SVB DX-0 DY-a DZ-1 SP-1970 SNUB PT-146 DX--0.669 DZ-0.743 SP-1654 SNUB PT-144 DX--.707 DZ--. 707 SP-2134 SNUB PT-153 DX-0 DY-1 DZ-0 SP-956

• LINE A RESTRAINTS SNUB PT-230 DX-0 DY-1 DZ-0 SP-630.8 SNUB PT-244 DX-0 DY-0 DZ-1 SP-3094 SNUB PT-27A DX-1 DY-0 DZ-O SP-1418 SNUB PT-278 DX-O DY-C DZ-1 SP-3158 SNUB PT-316 DX--. 6691 DZ-0.743 SP-1654 SNUB PT-322 DX-O DY-1 DZ-O SP-956 ENDP Revision I A I I l File No. HC-04Q-311 Page A8 of A8

IN NN UU UU DDDDD 777777 BBBBBB INN NN UU UU DD DD 77 77 BB BB RNNN NN UU UU DD DD 77 BB BB IN NNNN UU UU DD DD 77 BBBBB IN NNNUU UU DD DD 77 BB BB IN NN UU UU DD DD 77 BB BB IN NNWUUUUUU DDDDD 77 BBBBBB USERID: NUD7B DOCUMENT NUMBER: 215 PRINTED ON 11/3/04 9:53:57 AM

1- FILED No.: IIC-04Q-308 iv STRUCTURAL CALCULATION INTEGRITY PACKAGE PROJECT No.: HC-04Q Associates, Inc.

PROJECT NAME: Hope Creek Extended Power Uprate Piping Vibration Monitoring CLIENT: PSEG Nuclear, LLC (Hope Creek)

CONTRACT NUMBER: 4500226359 Including C.O. #1 CALCULATION TITLE: Inside the Drywell Feedwater Loop A Piping Vibration Acceptance Criteria Project Mgr. Preparer(s) &

Document Affected .. s.p.nApproval Checker(s)

Revision Pages Revision Description Signature & Signatures &

Date Date A 1-7 DRAFT Issue K. K. Fujikawa Carl R. Limpus Appendix 7/28/2004 7/28/2004 Al-AS Paul Hirschberg In 7/28/2004 Computer Files Page 1 of 7 F2001R1

Table of Contents

1.0 INTRODUCTION

.................................................................... 3 2.0 VIBRATION ACCEPTANCE CRITERIA THEORY .................................................................... 3 3.0 CALCULATION OF ACCEPTANCE CRITERIA ..................................................................... 4

4.0 REFERENCES

................................................................................................................................7 APPENDIX A FILES ................................................................... Al List of Tables Table 1: Nodal Accelerations and Acceptance Criteria Due to I g Spectrum Input ................................. 5 Table 2: Nodal Displacements and Acceptance Criteria Due to I g Spectrum Input ............................... 5 List of Figures Figure 1: Inside Drywell FW Loop A PIPESTRESS model, including Accelerometer Locations ......... 6 Revision l* A l I I File No. HC-04Q-308 lPage 2 of 7

1.0 INTRODUCTION

The purpose of this calculation is to develop vibration acceptance criteria for the accelerometers installed on the Hope Creek Feedwater Loop A Piping inside the Drywell.

2.0 VIBRATION ACCEPTANCE CRITERIA THEORY The acceptance criterion is based on the guidance of ASME OM S/G Part 3 [1], which states that the calculated stress shall not exceed Se]/a. The equation from OM Part 3 for the stress criteria is given below:

Salt = C2K 2 M<Sel/a Where Sot Alternating stress as defined in ASME Code (NB-3600)

C2 = Secondary stress index as defined in ASME Code K2 Local stress index as defined in ASME Code M - Maximum zero to peak dynamic moment loading due to vibration only Z Section modulus of the pipe S = 0.8SA, where SA is the alternating stress at 106 cycles from Figure I-9.1 of Section III of the ASME Code [2] for carbon steel a = Allowable stress reduction factor, 1.3 for carbon steel The piping within the scope of this analysis is A106 Grade B carbon steel [3]. For carbon steel pipe, SA = 12,500 psi, thus, the maximum allowed stress due to steady state vibration is 0.8*12,500 psi /1.3

= 7692 psi.

The acceptance criteria for the accelerations to be measured is determined by multiplying the calculated acceleration at each sensor location in a unit load analysis by the ratio of the allowable steady state stress to the maximum calculated stress in the piping system. This may be expressed by multiplying the accelerations for each direction by a factor, and the factor is defined as:

F = 7692 psi / ax,

--where F-is the -factor and m,,-is the maximum -stress-obtained-from the dynamic analysis.---- -----

It should be noted that exceedance of the allowable acceleration or displacement in one direction at a location does not necessarily indicate exceedance of the OM-3 criteria, as the stresses at a location are a function of the SRSS combination of the accelerations in three orthogonal directions. In addition, review of the frequency content of the collected data may allow for refinement of the shape of the input response spectra. The acceptance criteria are conservative, and if met, will eliminate the need for further review to justify the acceptability of the measured accelerations.

Revision I A File No. HC-04Q-308 Page 3 of 7

3.0 CALCULATION OF ACCEPTANCE CRITERIA A PIPESTRESS [4] model was developed in Reference [3] and is shown in Figure 1. A flat lg spectrum was applied in each of the three orthogonal directions. Static loads such as weight and thermal expansion are not considered since these loads do not contribute to the cyclic loading of the piping system. Additionally, seismic (inertia and anchor movements) and turbine stop valve loads are not considered since these loads are transient dynamic loads and do not contribute to the steady-state cyclic loading of the system.

Due to extended power uprate, the flow in the feedwater lines will increase, which can potentially cause the vibration of the piping to increase due to flow induced vibration. Since the forcing function can occur over a range of frequencies, a broad band amplified response spectra (ARS) of I g, applied in each direction, was used to analyze the feedwater piping system. This dynamic analysis provides the response of the piping system to a broad band ARS that corresponds to white noise input. The displacements, accelerations and stresses due to the broad band ARS in each of the three orthogonal directions were calculated at each node in the piping system. The total response was obtained by combining the results from each of the three directions by square-root-sum-of-the-squares.

The calculated maximum stress in the model due to a flat 1g input in each direction is 15,493 psi at Node 95. Acceptance criteria are calculated for the 5 accelerometer locations. They are Nodes 220, 280, Z002, 160, and 50. The locations of the accelerometers are shown in Figure

1. Reference [3] provides details ofthe accelerometer locations. The acceptance criterion calculation for Node Z002 is shown below. The acceleration values for each node are shown in Table 1 and the displacement values are shown in Table 2.

Ax= 7692 / 15493

• 1.943 g = 0.965 g Ay = 7692/ 15493

• 1.872g = 0.929 g Az = 7692/ 15493

• 1.991 g = 0.988 g Revision A File No. HC-04Q-308 Page 4 of 7

Table 1: Nodal Accelerations and Acceptance Criteria Due to Ig Spectrum Input Acceleration (g) Acceptance Criteria (g) I Node (X) (Y) (Z) (X) (Y) (Z) 220 1.428 1.907 1.491 0.709 0.947 __

280 1.914 1.225 2.232 0.950 - 1.108 Z002 1.943 1.872 1.991 0.965 0.929 0.988 160 1.667 1.798 0.703 0.828 0.893 _ __

50 0.845 1.118 j 1.057 0.420 0.555 0.525 Table 2: Nodal Displacements and Acceptance Criteria Due to 1g Spectrum Input Displacement (in) Acceptance Criteria (in)

Node (X) (Y) (Z) (X) (Y) (Z) 220 0.150 0.123 0.195 0.074 0.061 280 0.082 0.045 0.186 0.041 l - 0.092 Z002 0.217 0.201 0.097 0.108 j 0.100 0.048 160 0.211 0.234 0.025 0.105 0.116 -

50 0.029 0.035 j 0.020 0.014 0.017 0.010 Revision I A I I File No. HC-04Q-308 Page 5 of 7

i

's.0 i4i -11bi TkIj$-VjTP"

'I

)

lIm Fitf  : STXD VlI trmflrh L 'nt,,vay

• ,-. 1I O31G/C4 08R42E

.Ss\HMn,;ha Qin\P.-O43\IDfW.M ,

Fig Ii Figure 1: Insidle Drywell FW Loop A PIPESTRE SS model, including Accelerometer Locations Revision I AI I I Il I File No. HC-04Q-308 Page 6 of 7

4.0 REFERENCES

1. ASME OM-S/G-1994, Standards and Guides for Operation and Maintenance of Nuclear Power Plants, Part 3, 1994 Edition, "Requirements for Preoperational and Initial Start-Up Vibration Testing of Nuclear Power Plant Piping Systems."

2. ASME Boiler and Pressure Vessel Code,Section III Appendices, 1984 Edition.

3. Structural Integrity Associates Calculation, Revision 0, "Inside the Drywell Feedwater Loop A Piping Vibration Monitoring Locations," SI File No. HC-04Q-302.

4. PIPESTRESS2000 Solver, Version 3.5.0.67, DST Computer Services S.A., QA-1670-301, May 15, 2002.

APPENDIX A FILES File Name Size Date & Time Description Location FWIDW-ACjrl.fre 8.82 KB (9,035 bytes) July 07,2004, 11:44:27 AM PIPESTRESS input file A2 to A5 Jul 07,2004, PRPESTRESS output file -

FWIDW-ACjrI.prc 192 KB (197,100 bytes) 5:48:44 PM combined directions for Incomputer file accelerations and displacements FWIDW-ACyrl.prf 201 KB (206,010 bytes) July 07,2004, PIPESTRESS output file - stresses In computer file Revision IA I I V File No. HC-04Q-308 Page Al of A5

• • • FEEDWATER LINE A INS DW FOR ACCEPTANCE CRITERIA

• IDEN JB-8 *JOB NO. (I to 9999)

CD=I *1ASME Class 1 GR--Y *Direction of gravity VA-0 *O-Calculation 2-Verification 3-Design (HANGIT)

IU-I *Input units -SIU 1-USA 2-USA2 OU-1 *Output units 0-SIU 1-USA CH-S *Delimiter character replaces ?

AB-T *FREE errors - terminate execution PL-$PROB-MONITOR LOCATIONS PROJ-HC-04Q$

EN-$USER-KRE/SI$

TITL BL-8 *Modelling option

• 8 - uniform mass for static analysis

• concentrated mass for dynamic analysis rotational inertia GL-0 *Print forces/moments 0-Global 1-Local 2-G and L SU-0 *Type 1 support summary 0-No 1-Yes CV-10 *Code version (see Manual)

HS-i *Report 20 highest stress ratios for each load case MD-I *Cold modulus J6-1 *Skip minor WARNING messages TI-$FEEDWATER INSIDE DRYWELL - LOOP A ACC CRITERIA $

FREQ RF-1 RP-8 FR-100 MP-33 MX-100 TI-SMODAL$

• • • THERMAL EXPANSION LOAD CASES

• LCAS CA-1 TY-0 TI-SNormal Operation$

• • • WEIGHT LOAD CASES

• LCAS CA-101 TY-3 TI-SOPERATING WEIGHTS

• • • SEISMIC CASES

• RCAS CA-201 EV-1 TY-1 SU-1 FX-I FY-0 FZ-0 TI-SX VIBRATIONS RCAS CA-202 EV-1 TY-I SU-I FX-0 FY-1 FZ-0 TI-SY VIBRATIONS RCAS CA-203 EV-1 TY-1 SU-1 FX-0 FY-0 FZ-1 TI-SZ VIBRATIONS

• • • • LOAD COMBINATION CASES

• CCAS RF-1 CA-401 SS-1 ME-2 EQ-3 C1-201 C2-202 C3-203 FL-1 TI-$VIBRATION STRESS+S CCAS FF-1 CA-402 SS-1 ME-0 EQ-3 Cl-401 Fl--1 TI-$VIBRATION STRESS-$

• • • • LOAD SETS

• LSET RF-i PR-I MO-1 LSET RF-1 FL-1 FC-0 PR-1 MO-401 TI-$+VIB$

LSET RF-1 FL-1 FC-0 PR-1 MO-402 TI-$-VIBS

• • • ** **** *t**********

SPEC FS-EVENT1 EV-1 ME-3 TI-$VIBRATION SPECTRUMS LV-1 DI-X 3.0/1.0 100.0/1.0 DI-y 3.0/1.0 100.0/1.0 DI-Z 3.0/1.0 100.0/1.0

• ASTM A-106 Grade B MATH CD=106 EX-0 TY-1 *C-Si MATD TE-70 EH-29.5 EX-0 SM-20.0 SY-35.0 MATD TE-100 EH-29.3 EX-0.21 SM-20.0 SY-35.0 MATD TE-200 E8-28.8 EX-0.95 SM-20.0 SY-31.9 MATD TE-300 EH-28.3 EX-1.77 SM-20.0 SY-31 MATD TE-400 EH-27.7 EX-2.67 SM-20.0 SY-30 MATD TE-500 EH-27;3 EX-3.64 SM;i8.9 SY-28.3 MATD TE-600 EH-26.7 EX-4.63 SM-17.3 SY-25.9 MATL CD-106 COOR PT-5 AX-0 AY-113.167 AZ-0 *GLOBAL ORIGIN DESN TE-70 PR-0 OPER CA-i TE-70 PR-0 OPER CA-101 TE-70 PR-0 CROS OD-42 WT-10.531 MA-3538.16 KL-1 SO-1.0 ST-1 ANCH PT-5 *KX-39920 KY=16150 KZ-10930 MX-2689E3 MY-2695E3 MZ-1932E4 TANG PT-8 DX-0 DY-0 DZ-.667 CROS OD=24.0 WT-1.531 MA-387.8 SO-1 ST-1 IN-3 Revision A File No. HC-04Q-308 Page A2 of A5

TANG PT-10 DX-0 DY-' DZ-14.791 TANG PT-12 DX-0 DY-0 DZ-.250 *DTI-AE-035-H01 TANG PT-15 DX-0 DY-0 DZ-.250 EN-1 *ETI-V003 VALV PT-20 DX-0 DY-0 DZ-2.458 MA-6.584 TH-2.0 VALV PT-25 DZ-2.458 EW-1 TH-2.0 TANG PT-30 DX-O DY-O DZ-.500 *DTI-1" TEST TANG PT-40 DX-C DY-0 DZ-2.583 BRAD PT-41 RA'2.0 TANG PT-43 DX-0 DY-2.750 DZ-0 *DTI-PR-186-34 TANG PT-45 DX-C DY-1.714 DZ-0 BRAD PT-46 RA-3.0 *APPROX SUPPORT LOCATION TANG PT-50 DX-2.998 DY-5.657 DZ--4.797 BRAD PT-50F RA-2.0 TANG PT-55 DX-2.508 DY-0 DZ-1.568 TANG PT-60 DX-0.884 DY-0 DZ-0.552 EWN1 VALV PT-65 DX-2.085 DY-0 DZ-1.302 PL-1 MA-'l.835 TR-2.0 JUNC PT-65 VALV PT-67 DX--1.810 DY-6.560 DZ-2.897 PL-3 MA-1.94 TH-2.0 JUNC PT-65 VALV PT-70 DX-2.085 DY-0 DZ-1.302 PL-2 EW-1 TH-2.0 TANG PT-80 DX-5.301 DY-0 DZ-3.312 BRAD PT-80F RA-15.0 TANG PT-82 DX-1.766 DY-0 DZ-4.854 TANG PT-85 DX-0.175 DY-0 DZ-0.481 TANG PT-88 DX-0.643 DY-0 DZ-1.767 TANG PT-90 DX-0.298 DY-0 DZ-0.817 TANG PT-95 DX-0.484 DY-0 DZ-1.331 TANG PT-100 DX-0.485 DY-0 DZ-1.331 TANG PT-103 DX-0.200 DY-0 DZ-0.549 TANG PT-105 DX-0.495 DY-0 DZ-1.360 BRAD PT-1iSF PA-3.0 TANG PT-108 DX-0 DY-0 DZ-1.625 TANG PT-109 DX-0 DY-0 DZ-1.771 TANG PT-110 DX-0 DY-0 DZ-1.458 EW-1

• • • POINT 115 WAS CENTER OF REDUCER CRED PT-120 DX-C DY-C DZ-1.667 AN-30 EW-1 CROS OD-20.0 WT-1.031 MA-226.7 SO-1 ST-1 IN-3.0 TANG PT-122 DX-0 DY-0 DZ-0.500 TANG PT-125 DXC0 DY-0 DZ-0.500 TANG PT-130 DX-0 DY-0 DZ-1.250 TANG PT-135 DX-0 DY-0 DZ-1.250 TANG PT-137 DX-0 DY-0 DZ-0.375 LUMP PT-137. MA-0.3443 TANG PT-138 DX-0 DY-C DZ-0.906 TANG PT-140 DX-0 DY-0 DZ-0.719 EW-1 CRED PT-150 DX-O DY-C DZ-1.667 AN-30 EW-1 CROS CD-4 OD-12.75 WT-0.687 MA-99.73 SO-1 ST-1 IN-3.0 TANG PT-155 DX-0 DY-C DZ-0.267 LUMP PT-155 NA-0.1882 TANG PT-160 DX-0 DY-0 DZ-4.400 BRAD PT-160F RA-5 TANG PT-161 DX--3.404 DY-2.881 DZ-0.601 TANG PT-162 DX--0.902 DY-0.766 DZ-0.159 LUMP PT-162 MA-0.1882 TANG PT-163 DX--0.611 DY-0.517 DZ-0.107

-TANS-PT-1l64-'-DX--0;-41B- DY-0;353-- DZ-0.-074------ --

TANG PT-165 DX--8.844 DY-7.487 DZ-1.560 TANG PT-170 DX--5.217 DY-4.416 DZ-O.919 BRAD PT-170F RA-5 TANG PT'171 DY-3.271 TANG PT-172 DY-0.458 TANG PT-175 DY-0.771 TANG PT-178 DY-3.083 TANG PT-iB0 DY-1.000 TANG PT-185 DY-1.250 TANG PT-190 DY-4.167 TANG PT-195 DY-3.083 Revision A File No. HC-04Q-308 Page A3 of A5

BRAD PT-195F RA-1.5 TANG PT=200 DX--1.901 DY-0 DZ--3.292 TA-1 ANCH PT-200 *NOZZLE N4C JUNC PT-95 BRAN PT-205 DY-1.302 TE-1 TANG PT=210 DY-1.281 BRAD PT-21OF RA-1.5 TANG PT-212 DX--0.991 DY-0.708 DZ-0.280 LUMP PT-212 MA-.0978 TANG PT-215 DX--6.939 DY-4.956 DZi1.962 TANG PT=220 DX--3.S5S DY-2.755 DZ-1.090 BRAD PT-220F RA-5 TANG PT-223 DX--1.813 DY-2.035 DZ--2.069 TANG PT-225 DX--0.387 DY-0.433 DZ--0.441 TANG PT-227 DX--0.651 DY-0.731 DZ--0.743 TANG PT-230 DX--3.575 DY-4.011 DZ--4.078 BRAD PT-230F RA-2 *REDUCED FROM 5 TO AVOID PIPESTRESS ERROR TANG PT-232 DY-2.479 LUMP PT-232 MA-.1882 TANG PT-235 DY-1.979 TANG PT-240 DY-2.292 TANG PT-245 DY-1.250 TANG PT-250 DY-1.083 TANG PT-257 DY-3.083 TANG PT-260 DY-3.083 BRAD PT-260F RA-1.5 TANG PT-265 DX--1.901 DY-0 DZ-3.293 TA-1 ANCH PT-265 *NOZZLE N4A JUNC PT-130 BRAN PT-270 DY-1.135 TE-1 TANG PT-275 DY-2.198 BRAD PT-275F RA-1.5 TANG PT-277 DX--1.534 DY-0.722 DZ--0.209 TANG PT-280 DX--9.486 DY-4.464 DZ--1.291 BRAD PT-280F PA-5 TANG PT-282 DY-3.208 LUMP PT-282 MA-.0978 TANG PT-283 DY-1.292 TANG PT-285 DY-3.500 LUMP PT-285 MA-.0978 TANG PT-287 DY-4.521 TANG PT-288 DY-1.167 TANG PT-295 DY-2.792 TANG PT-297 DY-5.417 TANG PT-310 DY-3.083 BRAD PT-310F RA-1.5

• TANG PT-312 DX--116" TANG PT-315 DX--3.802 TA-1 ANCH PT-315

• • • SUPPORTS***

VSUP PT-12 DY-1 SP-7.08 FO-16.51 AL-$AE-035-HOI$

RSTN PT-43 DX-1 SP-746 AL-SAE-035-H25$

RSTN PT-55 DY-1 SP=1031 AL-SAE-035-HU2VS RSTN PT-55 DX-0.5299 DZ--0.848 SP-3437 AL-$AE-035-H02H$

VSUP PT-85 DY-1 SP-1.33 FO-11.622 AL-$AE-035-H03S

-- SNUB-PT -----.- DY-1--SP-51-1 -AL-$AE-035-H04$

SNUB PT-103 DX--0.8416 DY-.4449 DZ-.3063 SP-1730 AL-SAE-035-H05$

SNUB PT-108 DX--0.3409 DY-0 DZ--0.9401 SP-1627 AL-$AE-035-H06S VSUP PT-122 DY-1 SP-1 FO-10.071 AL-$AE-035-H07$

VSUP PT-165 DY-1 SP-.001 FO-3.617 AL-$AE-035-H11$

RSTN PT-171 DX--0.9977 DY-0 DZ-0.0674 SP-3409 AL-$AE-035-H12$

RSTN PT-172 DX--0.5 DY-0 DZ--0.866 SP-1192 AL-SAE-035-H24$

VSUP PT-178 DY-1 SP-.001 FO-2.306 AL-$AE-035-H13$

SNUB PT-223 DX-0.6794 DY-0.4286 DZ--0.5955 SP-459.5 AL-$AE-035-H15$

VSUP PT-225 DY-1 SP.001 FO=2.843 AL-SAE-035-H16$

VSUP PT-250 DY-1 SP-.001 FO-2.822 AL'$AE-035-H19$

RSTN PT-287 DZ-1.0 SP-8474 AL-$AE-035-H26$

A l HC-04Q-308 Page A4 of AS HC-04Q-308 rage A4 of A5

VSUP PT-288 DY-1 SP-.001 FO-4.784 AL-SAE-035-H22$

ILE No. HC-04Q-309

' STRUCTURAL CALCULATION ..

INTEGRITY PACKAGE PROJECT No.: HC-04Q Associates, Inc.

PROJECT NAME: Hope Creek Extended Power Uprate Piping Vibration Monitoring CLIENT: PSEG Nuclear, LLC (Hope Creek)

CONTRACT NUMBER: 4500226359 Including C.O. #1 CALCULATION TITLE: Outside the Drywell Feedwater Piping Vibration Acceptance Criteria Project Mgr. Preparer(s) &

Document Affected Approval Checker(s)

Revision Pages Revision Description Signature & Signatures &

Date Date A 1-7 DRAFT Issue K. K. Fujikawa Carl R. Limpus Appendix A 7/28/2004 7/28/2004 Al-A9 Paul Hirschberg In7/28/2004 Computer Files Page 1 of 7 F2001Rl

Table of Contents

1.0 INTRODUCTION

........................................ 3 2.0. VIBRATION ACCEPTANCE CRITERIA THEORY .......................................... ,.;. 3 3.0 CALCULATION OF ACCEPTANCE CRITERIA ........................................ 4

4.0 REFERENCES

........................................ 7 APPENDIXA FILES ......................................... Al List of Tables Table 1: Nodal Accelerations and Acceptance Criteria Due to I g Spectrum Input ................................. 5 Table 2: Nodal Displacements and Acceptance Criteria Due to lg Spectrum Input ............................... 5 List of Figures Figure 1: Outside Drywell FW Piping PIPESTRESS model, including Accelerometer Locations ......... 6 Revision I A I I T File No. HC-04Q-309 Page 2 of 7

1.0 INTRODUCTION

The purpose of this calculation is to develop vibration acceptance criteria for the accelerometers installed on the Hope Creek feedwater piping located outside the drywell.

2.0 VIBRATION ACCEPTANCE CRITERIA THEORY The acceptance criterion is based on the guidance of ASME OM S/G Part 3 [1], which states that the calculated stress shall not exceed SI/a. The equation from OM Part 3 for the stress criteria is given below:

C2K Salt= 22 M Sel /a Where Salt = Alternating stress as defined in ASME Code (NB-3600)

C2 = Secondary stress index as defined in ASME Code K2 = Local stress index as defined in ASME Code M Maximum zero to peak dynamic moment loading due to vibration only Z Section modulus of the pipe St,= 0.8SA, where SA is the alternating stress at 106 cycles from Figure I-9.1 of Section III of the ASME Code [2] for carbon steel a = Allowable stress reduction factor, 1.3 for carbon steel The piping within the scope of this analysis is Al 06 Grade B carbon steel [3]. For carbon steel pipe, SA = 12,500 psi, thus, the maximum allowed stress due to steady state vibration is 0.8*12,500 psi /1.3

= 7692 psi.

The acceptance criteria for the accelerations to be measured is determined by multiplying the calculated acceleration at each sensor location in a unit load analysis by the ratio of the allowable steady state stress to the maximum calculated stress in the piping system. This may be expressed by multiplying the accelerations for each direction by a factor, and the factor is defined as:

F = 7692 psi / ,,max

-where F-is -the.factor-and.a5 m,, ,.is the.maximum stress obtained.fromrnhe dynamic-analysis.,____,,,

It should be noted that exceedance of the allowable acceleration or displacement in one direction at a location does not necessarily indicate exceedance of the OM-3 criteria, as the stresses at a location are a function of the SRSS combination of the accelerations in three orthogonal directions. In addition, review of the frequency content of the collected data may allow for refinement of the shape of the input response spectra. The acceptance criteria are conservative, and if met, will eliminate the need for further review to justify the acceptability of the measured accelerations.

A Revision Al File No. HC-04Q-309 Page 3 of 7

3.0 CALCULATION OF ACCEPTANCE CRITERIA A PIPESTRESS [4] model was developed in Reference [3] and is shown in Figure 1. A flat I g spectrum was applied in each of the three orthogonal directions. Static loads such as weight and thermal expansion are not considered since these loads do not contribute to the cyclic loading of the piping system. Additionally, seismic (inertia and anchor movements) and turbine stop valve' loads are not considered since these loads are transient dynamic loads and do not contribute to the steady-state cyclic loading of the system. Although most of the piping is Class 2, designed to ANSI B31.1, the piping analysis was run using ASME Class 1 methodology, as the OM-3 criteria uses the Class 1 secondary and peak stress indices C2 and K2.

Due to extended power uprate, the flow in the feedwater lines will increase, which can potentially cause the vibration of the piping to increase due to flow induced vibration. Since the forcing function can occur over a range of frequencies, a broad band amplified response spectra (ARS) of 1g, applied in each direction, were used to analyze the feedwater piping system. This dynamic analysis provides the response of the piping system to a broad band ARS that corresponds to white noise input. The displacements, accelerations and stresses due to the broad band ARS in each of the three orthogonal directions was calculated at each node in the piping system. The total response was obtained by combining the results from each of the three directions by square-root-sum-of-the-squares.

The calculated maximum stress in the model due to a flatlg input in each direction is 29,239 psi at Node 490F. This stress is calculated using the Class 1 C2 stress indice, however this location is in Class 2 piping. OM-3 specifies the use of "2i" instead of C2K2 in the stress allowable. For this location, which is a long radius elbow, 2i/C2 = 1.8/1.95 = 0.923, therefore the maximum stress can be reduced by this amount. Acceptance criteria are calculated for the 2 accelerometer locations. They are Nodes 731 and 817. The locations of the accelerometers are shown in Figure 1. Reference [3] provides details of the accelerometer locations. The acceleration acceptance criterion calculation for Node 731 is shown below. The acceleration values for each node are shown in Table 1 and the displacement values are shown in Table 2.

Ax= 7692/ (29239

• 0.923)

• 1.207 g = 0.344 g Ay = 7692/ (29239

• 0.923)

• 1.171 g = 0.334 g A, = direction not monitored

Table 1: Nodal Accelerations and Acceptance Criteria Duc to 1g Spectrum Input Acceleration (g) Acceptance Criteria (g)

_Node  ;,(X). I 8--IYMZ 'I WYx M M 731 1.207 l 1.171 l 0.978 0.344 l 0.334 l -

817 0.849 1 0.917 1 1.192 - @ 0.261 l 0.340 Table 2: Nodal Displacements and Acceptance Criteria Due to ig Spectrum Input I ..Node I )

Displacement (in)

( .*

i) ( n I Dis I

(X)

A c Criteria Acceptance C (Y) a (in)

(nI (Z)

I 731 1 0.071 1 0.061 1 0.040 0.020 1 0.017 1 -

817 10.036 10.044 11.499 - l 0.013 1 0.427 l l

V Revision I A I File No. HC-04Q-309 Page 5 of 7

7o Xe xM =at rims)v I".

24'fron~mTee DP. 731 B.Y Figure A: StnkDARD VIEW ... .. .: . _ .

.,,.s first I .- .........

t ratel03io4 B:\Kltb\l;^rressdrpar*\C~aQ)W~wxW 35t03:32.

Fu1:g Figure 1: Outside Drywsell FW Piping PIPESTRESS model, including Accelerometer Locations

4.0 R FE,RENCES

1. ASME OM-S/G-1994, Standards and Guides for Operation and Maintenance of Nuclear Power Plants, Part 3, 1994 Edition, "Requirements for Preoperational and Initial Start-Up Vibration Testing of Nuclear Power Plant Piping Systems." ..

2. ASME Boiler and Pressure Vessel Code,Section III Appendices, 1989 Edition.

3. Structural Integrity Associates Calculation, Revision 0, "Outside the Drywell Feedwater Loop A Piping Vibration Monitoring Locations," SI File No. HC-04Q-303.

4. PIPESTRESS2000 Solver, Version 3.5.0.67, DST Computer Services S.A., QA-1670-301, May 15, 2002.

Revision lA l l File No. HC-04Q-309 Page 7 of 7

APPENDIX A FILES File Name Size Date & Time Description Location FWODW-A rIC.fre 23.5 KB (24,156 bytes) July 07,2004, PIPESTRESS input file A2 to A9 5:47:57 PM July07,204. PIPESTRESS output file -

FWODW-ACr1l.prc 574 KB (587,790 bytes) 11:y4957 PM2 combined directions for In computer file accelerations and displacements FWODW-ACrl.prf 617 KB (631,935 bytes) July 07,20046 PIPESTRESS output file- stresses In computer file

___ ___ ___ 11:50:06 PM Revision IA I I l File No. IIC-04Q-309 Page Al of A9

• • • FEEDWATER OUTSODE DW FOR ACCEPTANCE CRITERIA (PH CHANGES)

• IDEN JB-3 *JOB NO. (I to 9999)

CD-i *1-ASME CLASS 1 GR=-Y *Direction of gravity VA-0 *0-Calculation 2-Verification 3-Design (HJ IANGIT)

IU-1 *Input units 0-SIU 1-USA 2-USA2 OU-1 *Output units 0-SIU 1-USA CHl-S *Delimiter character replaces ?

AB-T *FREE errors - terminate execution PL-$PROB-MONITOR LOCATIONS PROJ=HC-04QS EN-$USER-XRE/Sl$

TITL BL-B *Modelling option

• 8 - uniform mass for static analysis

• concentrated mass for dynamic analysis

• rotational inertia GL-l *Print forces/moments 0-Global 1-Local 2-G and L SU-O *Type 1 support summary 0-No 1-Yes CV'10 *Code version HS-1 *Report 20 highest stress ratios for each load case MD0-0 *Cold modulus J6-1 *Skip minor WARNING messages TI-$FW OUTSIDE DRYWELL FROM T/B ANC TO FL HD ANCS$

FREQ RF-1 RP-8 FR-100 MP-33 MX-100 TI-$MODAL$

• • • THERMAL EXPANSION LOAD CASES

• LCAS CA-1 TY-0 TI-$Normal Operation$

• • • WEIGHT LOAD CASES

• LCAS CA-101 TY-3 TI-$OPERATING WEIGHT$

• • • SEISMIC CASES

• RCAS CA-201 EV-1 TY-1 SU-1 FX-1 FY-0 FZ-0 TI-$X VIBRATIONS RCAS CA-202 EV-1 TY-1 SU-1 FX-O FY-1 FZ-O TI-SY VIBRATIONS RCAS CA-203 EV-1 TY-1 SU-1 FX-0 FY-0 FZ-1 TI-SZ VIBRATIONS

• • • • LOAD COMBINATION CASES

• CCAS RF-1 CA-401 SS-1 ME-2 EQ-3 Cl-201 C2-202 C3-203 FL-I TI-SVIBRATION STRESS+$

CCAS RF-I CA-402 SS-1 ME-0 EQ-3 Ci-401 Fl--l TI-$VIBRATION STRESS--$

• • • • LOAD SETS

• LSET RF-l PR-1 MO-I LSET RF-1 FL-1 FC-0 PR-i MO-401 TI-$+VIBS LSET PF-i FL-1 FC-0 PR-i MO-402 TI-$-VIB$

SPEC FS-EVENTI EV-1 ME-3 TI-SVIBRATION SPECTRUMS LV-1 DI-X 1.0/1.0 100.0/1.0 DI-Y 1.0/1.0 100.0/1.0 DI-Z 1.0/1.0 100.0/1.0

• ASTM A-106 Grade B MATH CD-106 EX-0 TY-I *C-Si MATD TE-70 EH-29.5 EX-0 SM-20.0 SY-35.0 MATD TE-100 EH-2 9.3 EX-0.21 SM-20 .0 SY-35.0 MATD TE-200 EH-28.8 EX-~0.95 SM-20.0 SY-31.9 MATD TE-300 EH-28.3 EX-1.77 SM-20.0 SY-31 MATD TE-400 EH-27.7 EX-2. 67 SM-20.0 SY-30 MATD TE-500 EH-27.3 EX-3.64 SM-18.9 SY-28.3 MATD-TE-600 ---- EH-26i-7----EX-4.-63-- SM-I-7.3--SY-25. - -- -- *---.***-

MATI, CD=106 DESN TE=70 PR-0 OPER TE-70 PR-O CA-i OPER TE-70 PR-0 CA-101 COOR PT-5 AX-0 AY-113.167 AZ-O *GLOBAL ORIGIN ANCH PT-5 HX=3.992e4 KY-1.615E4 KZ-1.093E4 MX-2.689E6 MY-2.695E6 MZ-1.93E7 KL-i AL-SPEN. P-2AS CROS CD-1 OD-42 WT-10.531 KL-l SO=1 ST-1 MA-3538.16 TANG PT-B DZ--.6667 CROS CD-2 OD-24 WT-1.531 SO-1 ST-i MA-387.8 IN-3.0 Revision A I I File No. HC-04Q-309' Page A2 of A9

TANG PT-10 DZ--.875 TANG PT-15 DZ--3.5 *ETI-BR-P-AE-201

• V002/F074B DLA-CHK, VALVE DWG:302(Q)398, ITEM 16.1 TANG PT-20 DZ--1.0 TA-I *ETI-AE-VO02 VALV PT-25 DZ--2.4583 TH-2. MA-11.824 PL-1 *ETI'AE-VO02 VALV PT-35 DZ--2.4583 TH-2. TA-1 PL-2 *ETI-AE-V002 CROS CD-3 OD=24 WT-1.531 SO-1 ST-1 MA-390.6 IN-2.5 TANG PT-40 DZ--2.5833 TANG PT-42 DZ--0.417 *DTI'BR-P-AE-247 TANG PT-45 DZ--0.792 TANG PT-50 DZ--4.5 BRAD PT-50F RA-3.0 TANG PT-55 DY-4.5 TANG PT-60 DY-5.8333 TANG PT-65 DY-1.75 TANG PT-70 DY-4.0 BRAD PT-70F RA-3.0

• • • VOD1/HV032B DBB-CHK,VALVE DWG: 302(Q)372(i), ITEM 7.5 TANG PT-75 DZ--6.3333 TA-1 *ETI'AE-V001 VALV PT-80 DZ--2.4583 TH-2. MA-9.284 PL-1 *ETI-AE-VO01 JUNC PT-80 VALV PT-85 DX-0 DY-4.773 DZ-4.773 TH-2. MA-1.84 PL-3 *ETI-AE-VO01 JUNC PT-80 VALV PT-90 DZ--2.4583 TH-2. TA-1 PL-2 *ETI-AE-V001 TANG PT-95 DZ--8.375

• CODE-B31S73 TANG PT-100 DZ--1.4167 *TEE-WTEE TANG PT-105 DZ--1.4167 TANG PT-107 DZ--1.6458 TANG PT-110 DZ--0.875 TANG PT-115 DZ--20.422 TANG PT-120 DZ--22.588 TANG PT-124 DZ--16.302 TANG PT-125 DZ--22.745 TANG PT-130 DZ--3.0885 TANG PT-140 DZ--5.0 TANG PT-145 DZ--10.167 *L BRAD PT-145F RA-3.0 TANG PT-148 DX--4.0 TANG PT-150 DX--1.75 TANG PT-155 DX--3.666 TANG PT-157 DX--2.917 TANG PT-160 DX--4.0 BRAD PT-16OF RA=3.0 TANG PT-165 DY-7.75 *DTIT-PEN TANG PT-i70 DY-4.00 BRAD PT-175 RA-3.0 TA-1 TANG PT-180 DX-3.9844 LUMP PT-180 MA-4.214

• • • THIS PORTION OF THE PIPING (DP'S 185 THRU 220) IS SUPPLIED BY GE TANG PT-185 DX-.9844 TA-1 *JOINT'TRP TANG PT-188 DX-1.7812 TANG PT-187 DX-1.792 TANG PT-189 DX-2.902 *SIF-1.O

-- TANG-PT-190 ---DX-4;556----

TANG PT-193 DX-1.7917 TANG PT-194 DX-1.8783 *SIF-1.0, TANG PT-195 DX-0.93 TA-1 *JOINT-TRP

• • • PER FE DWG,DOWNSTREAM PRES TAP LOCATES AT THE PIPE-TAPERED HUB JUNC (DP 195)

TANG PT-205 DX=1.3333 LUMP PT-205 MA-11.238 TANG PT-210 DX-1.3333 TA-1 *JOINT-TRP TANG PT-215 DX-.3983 *SIF-1.0 TANG PT-216 DX-1.336 *DTI-PEN TANG PT-217 DX-18.00 TANG PT-218 DX-1.75 l Revision A I File No. HC-04Q-309 Page A3 of A9

TANG PT=219 DX-1.5208 TANG PT-220 DX-8.0 TA-1 *JOINT-TRP, TANG PT-225 DX-.9583 LUMP PT-225 MA-4.214 TANG PT-230 DX-.9583 TA-1 *JOINT=TRP, TANG PT-231 DX-1.813 *SIF-1.0 TANG PT-233 DX-1.833 TANG PT-234 DX-2.333 TANG PT-235 DX-3.833 BRAD PT-240 RA-3.0 TANG PT-240 DY-3.0 EW-1 *JOINT-BTWELD, CRED PT-250 DY-2.0 AN-30 EW-1 *JOINT-BTWELD, CROS CD-4 OD-30 WT-1.512 SO-1 ST-1 MA-494.0 IN-3.0 TANG PT-255 DY-1.8333 *TEE-WTEE, TANG PT-260 DY-1.8333 TANG PT-262 DY-4.834 *DTI-PEN, TANG PT-265 DY-4.125 BRAD PT-265F RA-3.75 TANG PT-268 DX--4.25 *SIF-1.0 TANG PT-270 DX--1.417 TANG PT-272 DX--9.833 *SIF-1.0 TANG PT-273 DX--13.917 *SIF-1.0 TANG PT-275 DX--2.583 TA-1 *SIF-1.9 ANCH PT-275 KX-4780 KY-30800 KZ-21500 MX-7.767E5 MY-1.508E6 MZ-1.833E6 KL-1 AL-$AE-013-H25$

JUNC PT-100 CROS CD-5 OD-16 WT-1.218 SO-1 ST-1 MA-208.6 IN-2.5 BRAN PT-302 DY-3.333 TE-1

• TANG PT-305 DY-2.0 BRAD PT-305 RA-2.0 TANG PT-308 DZ--4.25 TANG PT-310 DZ--3.0 BRAD PT-31OF RA-2 TANG PT-315 DX--3.000 *DTI-BR-P-AE-245,SIF-1.0 TANG PT-320 DX--6.000 TANG PT-325 DX--1.0 TANG PT-327 DX--0.6667 TANG PT-330 DX--1.0 *TEE-WTEE TANG PT-335 DX--3.0 BRAD PT-340 RA-2.0 TANG PT-345 DZ-7.25 BRAD PT-350 RA-2.0 TANG PT-355 DY--3.333 *TEE-WTEE JUNC PT-355 JUNC PT-330 CROS CD-5 BRAN PT-365 DY--3.0 TE-1

• • • AE-V009/HV3626 DBD-GT, VALVE DWG: P353-38(i), ITEM 1.3 BRAD PT-375 RA-2.0 TA-1 VALV PT-380 DZ-3.375 TH-2. MA-6.8613 PL-1 *ETI-AE-VO09 JUNC PT-380 VALV PT-385 DY-4.813 TH-2. MA-0.615 PL-3 *ETI-AE-V009 JUNC PT-380 VALV PT-390 DZ-1.375 TH-2. PL-2 TA-1 *ETI-AE-VO09 TANG PT-395 DZ-2.0

-BRAD-PT-395-TANG PT-400 DX-2.9167 TANG PT-402 DX-0.6667 TANG PT-405 DX-2.417 BRAD PT-410 RA-2.0 TANG PT-412 DZ--2.000 TA-1 VALV PT-415 DZ--3.375 TH-2. MA-6.8613 PL-1 *ETI-AE-V067 JUNC PT-415 VALV PT-420 DY-4.813 TH-2. MA-0.615 PL-3 *ETI-AE-V067, JUNC PT-415 VALV PT-425 DZ--1.375 TH-2 PL-2 *ETI-AE-V067, CROS CD37 OD-16 WT-0.5 SO-1 ST-1 MA-82.77 IN-O t Revision IA File No. HC-04Q-309 Page A4 of A9

TANG PT-427 DZ--3.25 TANG PT-430 DZ--0.5 TANG PT-432 DZ--9.646 TANG PT-433 DZ--9.646 TANG PT-435 DZ--0.583 TANG PT-436 DZ--11.375 TANG PT-440 DZ--12.271 TANG PT-445 DZ--0.458 TANG PT-450 DZ'-21.333 TANG PT-455 DZ--0.417 TANG PT-460 DZ--0.521 TANG PT-465 DZ--23.25 BRAD PT-465F RA-2.0 TANG PT-475 DX--1.6667 DY--4.0833 DZ--4.411 BRAD PT-475F RA-2.0 TANG PT-480 DZ--3.1146 TANG PT-490 DZ--19.307 BEND PT-490F Z1--2.0 X2--2.0

• INDI AT-490F C2-5.27 ***BASED ON 2*SIF FROM CLASS 2 RULES TANG PT-492 DX-70.75 TANG PT-495 DX--1.0 TANG PT-500 DX--15.5 *DTI-BR-P-AE-242SIF-1.0 BRAD PT-505 RA-2.0 TANG PT-510 DX--2.75 DY'2.75 BRAD PT-51OF RA-2.0 TANG PT-515 DZ--5.000 TANG PT-517 DZ--0.9167 *DTI-BR-AE-241 TANG PT-520 DZ--.4166 TANG PT-525 DZ--4.583 BRAD PT-525F RA-2.0 TANG PT-530 DX-2.333 TANG PT-532 DX-9.583 TANG PT-535 DX-9.583 TANG PT-545 DX-7.5 BRAD PT-545F RA-2.0 TANG PT-550 DZ--4.0 TANG PT-553 DZ--0.5 TANG PT-555 DZ--17.5 TANG PT-560 DZ--3.75 TA-1 *SIF-l.9 ANCH PT-560 KZ-24498 KL-1 AL-$AE-054-H24$

• • • V005/HVF032A DBB-CHK, VALVE DWG: 302(Q)372(1), ITEM 7.5 JUNC PT-355 CROS CD-3 BRAN PT-360 DZ-1.4167 TE-1 TANG PT-610 DZ-8.375 *ETI-AE-V005 VALV PT-615 DZ-2.4583 TH-2.0 MA-9.284 PL-1 *ETI-AE-VO05

• CODE-SC374,CLASS-2, JUNC PT-615 VALV PT-625 DX-O DY-4.773 DZ-4.773 TH-2. MA-1.84 PL-3 *ETI-AE-VO05, JUNC PT-615 VALV PT-620 DZ-2.4583 TH-2. PL-2 *ETI-AE-V005 TANG PT-630 DZ-6.3333 BRAD PT-630F RA-3.0 TANG PT-635 DY--4.

TANG PT-640 DY--1.75 *SIF'1.222

-INDI-'AT=i6'40 -C2'-1';'222--2Z0 TANG PT-645 DY--2 TANG PT-650 DY--3.8333 TANG PT-655 DY--4.5 BRAD PT-655F RA'3.0 TANG PT-660 DZ-4.5 TANG PT-665 DZ-1.2083 *SIF-1.0

• • • V006/F074A DLA-CHK, VALVE DWG: 302(Q)398, ITEM 16.1 TANG PT-670 DZ-2.5833 TA-1 *ETI-AE-V006 VALV PT-675 DZ-2.4583 TH-2. MA'11.824 PL-1 *ETI-AE-VO06 VALV PT-685 DZ-2.4583 TH-2. PL-2 *ETI'AE-V006 CROS CD-2 File No. HC-04Q-309 P~age AS of A9 I Page A5 of A9 File No. HC-04Q-309

TANG PT-690 DZ-1.0 ETI-BR-P-AE-201 TANG PT-695 DZ-3.5 TANG PT-696 DZ-0.875 CROS OD-42 WT-10.531 MA-3538.16 KL-1 SO-1 ST-1 IN'0 TANG PT-698 DZ-.6667 TA-1 *DTIT-PEN. P-2B ANCH PT-698 KX-3.992E4 KY-1.615E4 KZ-1.093E4 KL-1 MX-2.689E6 MY-1.346E6 MZ-1.93E7 JUNC PT-355 CROS CD-3 TANG PT-705 DZ--1.4167 *CCODE-B31S73 TANG PT-725 DZ--1.250 TANG PT-730 DZ--1.375 TANG PT-731 DZ--20.042 TANG PT-735 DZ--23.063 TANG PT-736 DZ--14.937 TANG PT-740 DZ--24.938 TANG PT-742 DZ--2.0208 TANG PT-745 DZ--5.0416 TANG PT-750 DZ--4.25 BRAD PT-750F RA-3.0 TANG PT-758 DX--1.674 DZ--1.674 TANG PT-759 DX--1.4142 DZ--1.4142 TANG PT-760 DX--2.828 DZ--2.828 BRAD PT-760F RA-3.0 TANG PT-762 DY-7.750 *r)TI-PEN TANG PT-765 DY-1.500 TANG PT-768 DY-2.3333 TANG PT-770 *DY-7.0 BRAD PT-770F RA-3.0 TANG PT-773 DX-3.802 TANG PT-775 DX-3.5 TA-i *JOINT-TRP

• • • THIS PORTION OF THE PIPING (DP'S 780 THRU 820) IS SUPPLIED BY GE TANG PT-780 DX-.9583 LUMP PT-780 MA-4.214 TANG PT-785 DX-.9583 TA-1 *JOINT-TRP TANG PT-Z16 DX-2.9020 TANG PT-790 DX-3.5730 *SIF-1.0 TANG PT-793 DX-4.5896 TANG PT-794 DX-1.645

• PER FE DWG,DOWNSTREAM PRES TAP LOCATES AT THE PIPE-TAPERED HUB JUNCTURE (I.E. DP 795)

TANG PT-795 DX-1.67 TANG PT-796 DX-.93 TA-1 *JOINT-TRP TANG PT-805 DX-1.3333 LUMP PT-805 MA-11.238 TANG PT-810 DX-1.3333 TA-1 *JOINT'TRP TANG PT-815 DX-.3983 TANG PT-816 DX-1.336 *DTI-PEN TANG PT-817 DX-18.374 TANG PT-818 DX-1.604 TANG PT-819 DX-1.646 TANG PT-820 DX-8.021 TA-1 *JOINT-TRP TANG PT-825 DX-.9583 LUMP PT-825 MA-4.214 TANG PT-830 DX-.9583 TA-1 *JOINT-TRP Tama. .=v-. Ho DX-1.813)

PT-831 *. U ACS __

TANG PT-835 DX-4.511 TANG PT-840 DX-1.15152 TANG PT-842 DX-0.54:117 BRAN PT-255C DX-1.75 iTE'1 JUNC PT-255C JUNC PT-40 CROS CD-3 BRAN PT-Z01 DY--.0 TE-1 CROS OD-4.5 WT-0.437 SO-1 ST-1 MA-25.6 IN-2.5 TANG PT-ZOiF DY--1.0 TANG PT-855 DY--2.0 Revision IA File No. HC-04Q-309 Page A6 of A9

BRAD PT-855F RA-.500 TANG PT-860 DZ-2.5833 BRAD PT-86OF RA-.500 TANG PT-862 DX-1-.917

• S* V128 DBB-TCK, VALVE DWG: P302(0)309, ITEM 7.9 TANG PT-863 DX--0.3333 TA-1 *ETI-AE-V128 VALV PT-864 DX--1.1667 TH-2. MA-.1795 *ETI.AE-V128, TANG PT-865 DX--2.9167 TANG PT-867 DX--.6562 TANG PT-868 DX--.3438 *TEE-WTEE TANG PT=869 DX--.3438 TANG PT-873 DX--.9062 TA-1 *ETI-AE-V021 *JOINT-TRP

• • • V021/HVF039 DBB-CHK, VALVE DWG: P302(Q)371(i) ITEM 7.1 VALV PT=875 DX--.5833 TH-2. MA-0.2395 PL-1 *ETI-AE-V021 JUNC PT-875 VALV PT-880 DX-1.7678 DY-1.7678 TH-2. MA-0.21 PL-3 *ETI-AE-V021 JUNC PT875 VALV PT-885 DX--.5833 TH-2. PL-2 *ETI-AE-V021 THIS PORTION OF THE PIPING IS IN ISO: I-P-BG-01 CROS OD-4.5 WT-0.337 SO-1 ST-1 MA-14.98 TANG PT-890 DX--.5 TANG PT-Y31 DX--2.0 TANG PT-892 DX--2.4167 BRAD PT-892F RA-.500 TANG PT-894 DZ-0.750 TANG PT-895 DZ-4.073 TANG PT-896 DZ-.3438 *TEEWTEE JUNC PT-896 BRAN PT-897 DY-.3438 TE-1 *JOINT-TRP TANG PT-898 DY-.375 LUMP PT-898 MA-0.103 JUNC PT-896 BRAN PT-899 DY--.3438 TE-i EW-0 TANG PT-900 DY--.4895 TANG PT-901 DY--.5888 TA-1 *JOINT-TRP

• ADDWT-329 LBS INCL. 129 LBS FOR FLANGES AND 200 LBS FOR BRANCH PIPING.

TANG PT-902 DY--.4113 LUMP PT-902 MA-0.329 TANG PT-903 DY--.4113 TA-1 *JOINT-TRP TANG PT-906 DY-3.4221 BRAD PT-906F RA-.500 TANG PT-907 DX-.8333 TANG PT-908 DX-2.75 BRAD PT-908F RA-.500 TANG PT-910 DY--1.5 TA-1 *SIF-1.9 ANCH PT-910 KY-18254 KL_1 AL-$BG-008-H43$

JUNC PT-665 CROS CD-3 BRAN PT-ZO6 DY--1.0 CROS OD-4.5 WT-0.437 MA-19.0 SO-1 ST-1 TANG PT-ZO6F DY--1.0 TANG PT-930 DY--2.0 BRAD PT-930F RA-.500 TANG PT-935 DX-6.3333 TANG PT-940 DX-1

--BRAD-PT-94OF--RA-0.500

• • • V127 DBB-TCK, VALVE DWG: P302(Q)-309, ITEM 7.9 TANG PT-942 DZ-.75 TA-1 *ETI-AE-V127 VALV PT-944 DZ-1.1667 TH-2. MA-0.1795 TA-1 *ETI-AE-V127 TANG PT-950 DZ-.3228 BRAN PT-868C DZ-.3438 TE-1 JUNC PT-868C JUNC PT-60 CROS D024 WT-1.531 MA-367.39 SO-1 ST-1 BRAN PT-952 DZ-1.0 TE-1 CROS OD=6.625 WT-0.562 MA-44.8 IN-2.5 SO-1 ST-1 TANG PT-954 DZ-1.9583 Revision A File No. HC-04Q-309 Page A7 of A9

BRAD PT-954F RA-.750 TANG PT-956 DX--1.7917 THIS PORTION OF THE PIPING IS IN ISO: 1-P-BD-01 V005/HVF013 DBB-GT, VALVE DWG 302(Q)300, ITEM 5.1 TANG PT-958 DX--.4583 TA-1 *ETI'BD-V005 VALV PT-960 DX--.8333 TH-2. MA-.4957 PL-1 *ETI-BD-V005 JUNC PT-960 VALV PT-962 DY-3.25 TH-2. MA-0.280 PL-3 TA-1 *ETI-BD-V005 JUNC PT-960 VALV PT-964 DX--.8333 TH-2. PL-2 *ETI'BD-V005 TANG PT-966 DX--.5 TANG PT-968 DX--2.9167 BRAD PT-968F RA-.75 TANG PT-969 DZ-4.0 TANG PT-970 DZ-1.0 TANG PT-972 DZ-2.75 *DTI-BR-BD3DBD-1" TANG PT-974 DZ-1.25 BRAD PT-974F RA-.75 TANG PT-976 DY--6.5 TANG PT-978 DY--.5 TANG PT-979 DY--2.9167 *DTI-BR-P-AP-02,SIF-1.4 TANG PT-980 DY--10.083 BRAD PT-980F RA-.75 TANG PT-982 DX--3.75 BRAD PT-982F RA-0.75 TANG PT-984 DY--1.5 TA-1 *SIF'l.9 ANCH PT-984 KY-246365 AL-$ETI-BD-003-Hl5$

JUNC PT-640

• • • THIS PORTION OF THE PIPING IS IN ISO: i-P-BJ-01

• • V059/HV8278 DBB-GT, VALVE DWG: P302(Q)439, ITEM 5.19 CROS OD-8.625 WT-0.593 MA-61.7 IN-2.5 SO-1 ST-1 BRAN PT-A10 DZ-3.5 TA-1 *ETI-BJ-V059 VALV PT-A15 DZ-1.0833 TH-2. NA-.89386 PL-1 *ETIEBJ-V059 JUNC PT-A15 VALV PT-A20 DY-3.083 TH-2. MA-0.340 PL-3 *ETI-BJ-V059 JUNC PT-A15 VALV PT-A25 DZ-1.0833 TH-2. TA-1 PL-2 *ETI-BJ-VO59 CROS OD-8.625 WT-0.593 MA-57.0 IN-1.5 SO-1 ST-1

• INSDEN-0.010736,INSTHK-1.5 TANG PT-AA6 DZ-0.500 *DTI-BR-PI-BJ-661 TANG PT-A26 DZ-0.583 TANG PT-A30 DZ-1.2083 BRAD PT-A30F RA-1 TANG PT-A35 DX--3.625 TANG PT-A40 DX--1.291 BRAD PT-A4OF RA-1 TANG PT-A52 DY--6.875 TANG PT-A55 DY--6.875 BRAD PT-A55F RA-1 TANG PT-A60 DX--2.25 TA-1 *SIF-1.9 ANCH PT-A60 YKX-63996 KL-1 AL-SETI-BJ-003-H51$

• • • • SUPPORTS RSTN PT-45 DY-1 SD-7857 AL-$AE-034-HO9S RSTN PT-55 DX-1 SD-100806 AL-$AE-034-H10$

RSTN PT-65 DX-1 SD-6379 AL-$AE-034-Hll$

--- RSTN PT107,---

RSTN PT-110 DX-1 SD-2946 AL-$AE-013-K27$

RSTN PT-120 DY-1 SD-8457 AL-$AE-013-H28Y$

RSTN PT-120 DX-1 SD-3794 AL-$AE-013-H28X$

SNUB PT-125 DZ-1.0 SP-1762 AL-$AE-013-H29$

RSTN PT-130 DY-1 SD-8696 AL-$AE-013-H30Y$

RSTN PT-130 DX-1 SD-3050 AL-$AE-013-H30X$

RSTN PT-140 DY-1 SD-8696 AL-$AE-013-H31Y$

RSTN PT-140 DX-1 SD-3050 AL-$AE-013-H31X$

VSUP PT-150 DY-1 SP-4.32 FO=9.38 AL-$AE-013-H325 SNUB PT-155 DY-1 SP-1113 AL-$AE-013-H33$

VSUP PT-187 DY-1 SP-8 FO-18.866 AL-$AE-013-H34$

Revision IA I I Filc No. HC-04Q-309 Page A8 of A9

SNUB PT-190 DZ-l.0 SP-358 AL-$AE-013-H36$

RSTN PT-193 DY-1 SD-2145 AL-$AE-013-H37$

VSUP PT'217 DY-1 SP-4.7 FO-20.665 AL-$AE-013-H138$

SNUB PT-218 )Z-1 Si;P-502 AL-$AE-013-H39$

SNUB PT-219 DY-1 SP- 1657 AL'$AE-013-H40$

SNUB PT-233 DX-1.0 SP-*996 AL-T$AE-013-H41$

RSTN PT=270 DY-1 SP- .2527 AL-$AE-013-H43$

RSTN PT-320 DY-1 SP- -3409 AL-$AE-013-H45$

RSTN PT-400 DY-1 SD5'2069 AL-$AE-013-H47$

SNU8B PT-402 DZ-1.0 SP-648 AL-$AE-013-H48$

RSTN PT-427 DX--.707 DY-0.70 D7 SD-807 AL-$AE-054-HOI$

RSTN PT-430 DX-.707 DY-0.7(07 SD-1135 AL-$AE-054-H02$

RSTN PT-433 DX-0.754 DY-0. 65i6 SD-2634 AL-$AE-054-103$

RSTN PT-435 DX--0.754 DY-0.6556 SD-2634 AL-$AE-054-H04$

RSTN PT-440 DX--0.815 DY-0.5179 SD-3198 AL-$AE-054-H05$

RSTN PT-445 DX-0.815 DY-0.5179 SD-3198 AL-$AE-054-HO6$

RSTN PT-450 DX--0.838 DY-0.5445 SD-3049 ALS$AE-054-H07$

RSTN PT-455 DX-0.838 DY-0.54315 SD-3049 AL-$AE-054-H08$

RSTN PT-480 DY-1 SD-3188 AL-$AE-054-HO9Y$

RSTN PT-480 DX-1 SD-1226 AL'$AE-054-HO9X$

SNUB PT-492 DZ-l.0 sP-744 AL-$AE-054-H10$

RSTN PT-495 DY-1 SD-313 AL-$AE-054-Hll$

SNUB PT-515 SP-122 AL-$AE-054-H12$

RSTN PT-520 DY-1 SD-1940 AL-$AE-054-H13$

RSTN PT-535 DY-1 SD-1940 AL-$AE-054-H15$

RSTN PT-550 DX--O. 70 DY-0.714 SD-1168 AL-$AE-054-H16$

RSTN PT-553 DX-0. 845 DY-0.534 SD-1008 AL-$AE-054-H17$

RSTN PT-635 DX-1 SD-6379 AL-$AE-037-HO6$

RSTN PT-650 DX-1 SD-100806 AL-$AE-037-H05$

RSTN PT-660 DY-1 SD-7857 AL-$AE-037-H04$

RSTN PT-725 DY-1 SD-4615 AL-$AE-013-H49$

RSTN PT-730 DX-1 SD-2963 AL-$AE-013-1H50$

RSTN PT-735 DX-1.0 SD-968 AL-$AE-013-H51X$

RSTN PT-735 DY-1.0 SD-8460 AL-$AE-013-H51Y$

SNUB PT-740 DZ-1.0 SP-2987 AL-$AE-013-HS2$

RSTN PT-742 DX-1 SD-2227 AL-$AE-013-H53X$

RSTN PT-742 DY-1.0 SD-110DO AL-$AE-013-H53Y$

RSTN PT-7 45 DX-1.0 SD-1945 AL-$AE-013-H54$

SNUB PT-758 DY-1.0 SP-552 AL-$AE-013-H55$

SNUB PT-765 DX-0.7455 DY-0 DZ-0.6665 SP-1224 AL-$AE-013-H56$

SNUB PT-768 DX-0. 6896 DY-0 DZ--0.7242 SP-635 AL-SAE-013-H57$

VSUP PT-773 DY-1.0 SP-8 FO-21.224 AL-$AE-013-H158$

RSTN PT-793 DY-1.0 SD-1450 AL-$AE-013-H59$

VSUP PT-818 DY-1.0 SP-5.32 FO-19.552 AL-$AE-013-H62$

SNUB PT-819 DY-1.0 SP-1016 AL-$AE-013-H63$

SNUB PT-835 DX-1.0 SP-1391 AL-SAE-013-H645 SNUB PT-840 DZ-1.0 SP-595 AL-$AE-013-H65$

RSTN PT-862 DY-1 SD-214.5 AL-SAE-034-HO2$

RSTN PT-890 DY-1.0 SD-100.5 AL-SBG-143-HO1$

RSTN PT-900 DZ-1.0 SD-497 AL-$BG-143-HO3$

RSTN PT-907 DY-1.0 SD-2359 AL-$BG-008-H47$

SNUB PT-956 DZ-1.0 SP-195 AL-$AE-034-HO1$

RSTN PT-966 DY-1.0 SD'102.5 AL-$BD-003-H16$

RSTN PT-970 DY-1.0 SD-97 AL-$BD-003-H18$

SNUB PT-976 DX--.7071 DZ-.7071 SP-83 AL-$BD-003-H1i9$

---SNUB PT-978--- DX-.-707 SP-83-.-AL-$BD-003-H205 RSTN PT-A26 DX-1 SD-549 AL-$BJ-003-H49$

ENDP

FILE, No.: HC-04Q-312 a STRUCTURAL CALCULATION INTEGRITY PACKAGE PROJECT No.: HC-04Q Associates, Inc.

PROJECT NAME: Hope Creek Extended Power Uprate Piping Vibration Monitoring CLIENT: PSEG Nuclear, LLC (Hope Creek)

CONTRACT NUMBER: 4500226359 Including C.O. i/1 CALCULATION TITLE: Main Steam Line A Piping Vibration Acceptance Criteria Project Mgr. Preparer(s) &

Document Affected .. s.p.nApproval Checker(s)

Revision Pages Revision DescriptionSignature & Signatures &

Date Date A 1-9 DRAFT Issue K. K. Fujikawa Carl R. Limpus Appendix 7/28/2004 7/28/2004 Al-All Paul Hirschberg In 7/28/2004 Computer Files Page 1 of 9 F2001RI

Table of Contents

1.0 INTRODUCTION

.................. 3 2.0 VIBRATION ACCEPTANCE CRITERIA THEORY....................................................................3 3.0 CALCULATION OF ACCEPTANCE CRITERIA .4

4.0 REFERENCES

.9 APPENDIXA FILES.. Al List of Tables Table 1: Nodal Accelerations and Acceptance Criteria Due to 1g Spectrum Input .5 Table 2: Nodal Displacements and Acceptance Criteria Due to 1g Spectrum Input .5 List of Figures Figure 1: Main Steam Line A Piping PIPESTRESS model .6 Figure 2: Locations of Accelerometers on MSRV Line and 26 inch Main Line A, and RCIC Line .7 Figure 3: Locations of Accelerometers on RCIC Line .8 Revision I A I I File No. HC-04Q-312 Page 2 of 9

1.0 INTRODUCTION

The purpose of this calculation is to develop vibration acceptance criteria for the accelerometers installed on the Hope Creek main steam line A piping.

2.0 VIBRATION ACCEPTANCE CRITERIA THEORY The acceptance criterion is based on the guidance of ASME OM S/G Part 3 [1], which states that the calculated stress shall not exceed Sd/a. The equation from OM Part 3 for the stress criteria is given below:

Sl =C 2K2 M<Sll z

Where St= Alternating stress as defined in ASME Code (NB-3600)

C2 = Secondary stress index as defined in ASME Code K2 = Local stress index as defined in ASME Code M Maximum zero to peak dynamic moment loading due to vibration only Z = Section modulus of the pipe Sl = 0.8SA, where SA is the alternating stress at 106 cycles from Figure I-9.1 of Section III of the ASME Code [2] for carbon steel a = Allowable stress reduction factor, 1.3 for carbon steel The piping within the scope of this analysis is A106 Grade B carbon steel [3]. For carbon steel pipe, SA = 12,500 psi, thus, the maximum allowed stress due to steady state vibration is 0.8*12,500 psi /1.3

= 7,692 psi.

The acceptance criteria for the accelerations to be measured is determined by multiplying the calculated acceleration at each sensor location in a unit load analysis by the ratio of the allowable steady state stress to the maximum calculated stress in the piping system. This may be expressed by multiplying the accelerations for each direction by a factor, and the factor is defined as:

F=7692psi/ a.

-where F-is the factor-and .~aois-the -maximum-stress obtained.from .the-dynamic analysis._ __._.

It should be noted that exceedance of the allowable acceleration or displacement in one direction at a location does not necessarily indicate exceedance of the OM-3 criteria, as the stresses at a location are a function of the SRSS combination of the accelerations in three orthogonal directions. In addition, review of the frequency content of the collected data may allow for refinement of the shape of the input response spectra. The acceptance criteria are conservative, and if met, will eliminate the need for further review to justify the acceptability of the measured accelerations.

Revision l A File No. HC-04Q-312 Page 3 of 9

3.0 CALCULATION OF ACCEPTANCE CRITERIA A PIPESTRESS [4] model was developed in Reference [3] and is shown in Figure 1. A flat 1 g spectrum was applied in each of the three orthogonal directions. Static loads such as weight and thermal expansion are not considered since these loads do not contribute to the cyclic loading of the piping system. Additionally, seismic (inertia and anchor movements) and turbine stop valve loads are not considered since these loads are transient dynamic loads and do not contribute to the steady-state cyclic loading of the system.

Due to extended power uprate, the flow in the main steam lines will increase, which can potentially cause the vibration of the piping to increase due to flow induced vibration. Since the forcing function can occur over a range of frequencies, a broad band amplified response spectra (ARS) of 1g, applied in each direction, was used to analyze the main steam piping system. This dynamic analysis provides the response of the piping system to a broad band ARS that corresponds to white noise input. As the vibration is flow induced, the vibration loading was applied only to the sections of piping normally containing flow. The displacements, accelerations and stresses due to the broad band ARS in each of the three orthogonal directions were calculated at each node in the piping system. The total response was obtained by combining the results from each of the three directions by square-root-sum-of-the-squares.

The calculated maximum stress in the model due to a flat 1g input in each direction is 19,854 psi at Node 32A. This stress is calculated using the Class 1 C2 stress indice, however this location is in Class 2 piping. OM-3 specifies the use of "2i" instead of C2K2 in the stress allowable. For this location, which is a long radius elbow, 2i/C2 = 1.8/1.95 = 0.923, therefore the maximum stress can be reduced by this amount. Acceptance criteria are calculated for the 4 accelerometer locations. They are Nodes 14 (Main A), 81 (Main A), 22J (SRV J), and 430 (RCIC). The locations of the accelerometers are shown in Figures 2 and 3. Reference [3]

provides details of the selection of the accelerometer locations. The acceleration acceptance criterion calculation for Node 14 is shown below. The acceleration values for each node are shown in Table I and the displacement values are shown in Table 2.

Ax= 7692/ (19854

• 0.923)

• 1.392 g = 0.584 g Ay = direction not monitored Az = 7692/ (19854

• 0.923)

• 1.168 g = 0.490 g

Table 1: Nodal Accelerations and Acceptance Criteria Due to 1g Spectrum Input Acceleration (g) Acceptance Criteria (g)

Node X Y Z X Y Z 14 1.392 0.770 . -. 1.168 0.584 - 0.490 81 1.043 1.513 0.813 0.438 0.635 -

22J 1.235 0.040 0.710 , 0.518 -- 0.298 430 1.311 3.197 2.309 - 1.342 0.969 Table 2: Nodal Displacements and Acceptance Criteria Due to ig Spectrum Input Displacement (in) Acceptance Criteria (in)

Node X Y Z X Y Z 14 0.070 0.007 0.052 0.029 - 0.022 81 0.007 0.009 0.001 0.003 0.004 -

22J 0.032 0.000 0.031 - 0.013 - 0.013 430 0.023 0.109 0.082 - 0.046 0.034 Revision I A iI File No. HC-04Q-312 Page 5 of 9

DA" VIMs 5SAEDW\I4ADW4.cs_

Figure 1: Main Steam Line A Piping PIPESTRESS model

-tw -c .e -et1--l qd- TO Am 1.,

I - -. Is - - ll

,J. r,* ,@ __ C3111/64 13144,3b I;i.%ldin\C-Cis%2q$'%PJAgr.4-t'- 2j12144 1XAr$. Cle-§srAlr &.w , ll 0414 1 Vi Figure 2: LocaItions of Accelerometcrs on MSRV Line and 26 inch Main Line A, and RCIC Line Revision I A I I I I File No. HC-04Q-312 Page 7 of 9

MON.

-M. -- - - - -

FAw Figure 3: Locations of Accelerometers on RCIC Line

4.0 REFtERE,NCES

1. ASME OM-S/G-1994, Standards and Guides for Operation and Maintenance of Nuclear Power Plants, Part 3, 1994 Edition, "Requirements for Preoperational and Initial Start-Up Vibration Testing of Nuclear Power Plant Piping Systems." I ....

2. ASME Boiler and Pressure Vessel Code,Section III Appendices, 1989 Edition.

3. Structural Integrity Associates Calculation, Revision 0, "Main Steam Line A Piping Vibration Monitoring Locations," SI File No. HC-04Q-306.

4. PIPESTRESS2000 Solver, Version 3.5.0.67, DST Computer Services S.A., QA-1670-301, May 15, 2002.

Revision I A I I File No. HC-04Q-312 Page 9 of 9

APPENDIX A FILES File Name Size Date & Time Description Location MSAIDW4-ACrl.fre 31.2 KB (32,040 bytes) Jl74243 PM PIPESTRESS input file A2 to All July07, 2004. PIPESTRESS output file -

MSAIDW4-ACrl.prc 522 KB (534,600 bytes) 10:16:35 PMcombined directions for In computer file 3 P accelerations and displacements MSAIDW4-AC_rl.prf 554 KB (567,405 bytes) July 07,:2004 PIPESTRESS output file - stresses In computer file I 1 10~l:16:44 PM III Revision I A l I File No. HC-04Q-312 l Page Al of All

• • • MAIN STEAM LINE A MODEL FOR ACCEPTANCE CRITERIA (PH CHANGES)

• IDEN JB-I *JOB NO. (1 to 9999)

CD-1 *1-ASME CLASS 1 GR--Y *Direction of gravity VA-0 *O-Calculation IU-1 *Input units 1-USA OU-1 *Output units 1-USA CH-$ *Delimiter character replaces'?

AB-T *FREE errors - terminate execution PL-SPROB-MONITOR LOCATIONS PROJ-HC-04Q$

EN-$USER-CRL/SI$

TITL BL-8 *Modelling option

• 8 = uniform mass for static analysis

• concentrated mass for dynamic analysis

• calculate rotational inertia GL-0 *Print forces/moments O-Global 1-Local 2- G and L SU-0 *Type 1 support summary 0-No 1-Yes CV-10 *Code version (see Manual)

HS-1. *Report 20 highest stress ratios for each load case MD-1 *Hot modulus J6-1 *Skip minor WARNING messages TI-$MAIN STEAM LINE A INSIDE DRYWELL $

• • • • • • • • • • • • • • Frequency Load ************************

FREQ RF-1 RP-8 FR-100 MP-33 MX-100 TI-$MODALS

• • • • THERMAL EXPANSION LOAD CASES

• LCAS RF-0 CA-1 TY-0 TI-SNormal OperationS

• • • • WEIGHT LOAD CASES

• LCAS CA-101 RF-1 TY-3 TI-$OPERATING WEIGHT$

• • • • DYNAMIC CASES

• RCAS CA-201 EV-1 TY-1 SD-i FX-1 FY-0 FZ-0 TI-$X VIBRATION$

RCAS CA-202 EV-I TY-1 SU-1 FX-0 FY-1 FZ-0 TI-$Y VIBRATION$

RCAS CA-203 EV-1 TY-1 SU-1 FX-0 FY-0 FZ-1 TI-$Z VIBRATION$

• • • • LOAD COMBINATION CASES

• CCAS RF-1 CA-401 SS-1 ME-2 EQ-3 C1-201 C2-202 C3-203 FL-1 TI-$VIBRATI ION STRESS+$

CCAS RF-1 CA-402 SS-1 ME-0 EQ-3 Cl-401 Fl--l TI-$VIBRATION STRESS-$

• • • • LOAD SETS

• LSET RF-1 PR-I MD-i LSET RF-1 FL-1 FC-0 PR-1 MO-401 TI-$+VIB$

LSET RF-1 FL-1 FC-0 PR-1 MO-402 TI-$-VIB$

SPEC FS-EVENTI EV-1 ME-3 TI-$VIBRATION SPECTRUM$

LV-1 DI-X 0.35/1.0 100.0/1.0 DI-Y 0.35/1.0 100.0/1.0 DI-Z 0.35/1.0 100.0/1.0 LV-2 DI-X 0.35/0.0 100.0/0.0 DI-Y 0.35/0.0 100.0/0.0 DI-Z 0.35/0.0 100.0/0.0

• • _********* _MATERIAL PROPERTIES

• - Ine r...A. V. _ I_

-1 *%QLVAn -Avu "LOU= 0 MATH CD-106 EX-0 TY-1 *C-Si MATD TE-70 EH-29.5 EX-0 SM-20.0 SH-15.0 SY- 35.0 MATD TE-100 EH-29.3 EX-0.21 SM-20.0 SH-15.0 SY-, 35.0 MATD TE-200 EH-28.8 EX-0.95 SM-20.0 SH-15.0 SY= 31.9 MATD TE=300 EH-28.3 EX-1.77 SM-20.0 SH=15.0 SY- 31 MATD TE-400 EH-27.7 EX-2.67 SM-20.0 SH-15.0 SY- 30 MATD TE-500 EH-27.3 EX-3.64 SM-18.9 SH-15.0 SY- 28.3 MATD TE-600 EH-26.7 EX-4.63 SM-17.3 SH-15.0 SY- 25.9 GEOMETRY ** *** ***** **** ** * ******* ***** **

• • • • • • • • • • • • • • MAIN STEAM LINE A **********

• GROUP 1 Revision l A I I I File No. HC-04Q-312 Page A2 of All

MATL CD-106 DESN TE-70. PR-0 OPER TE-70 PR-0 CA-1 CROS OD=26.0 WT-1.158 MA-332.8

• MODEL STARTS AT THE RPV (POINT 5)

COOR PT-5 AX-12.3637 AY-170.125 AZ--4.0172 ANCH PT-5 TA-1 LV-1 *AT RPV CROS OD-26 WT-1.39 MA-390.0 TANG PT-10 DX-3.8438 DY-0 DZ--1.2489 *ME101 PT COMBINED INTO PT-10 BRAD PT-l1 RA-2.1667 CROS OD-26 WT-1.158 MA-332.8 TANG PT-i1C DX-0 DY--5.000 TANG PT-12 DX-0 DY--5.2083 *PR-163-12 ME101 PT COMBINED INTO PT-12 TANG PT-14 DX-0 DY--6.875 LUMP PT-14 MA-0.927 *MASS DESIGNATED IN ME101 CODE TANG PT-15 DX-0 DY--18.343 DZ-0 BRAD PT-15A RA-10.833 *POINT ADDED TO ACCOMODATE BEND TANG PT-SA2 DX-1.5052 DY--6.6979 DZ--O.9-775 TANG PT-SA1 DX-0.1124 DY--0.5 DZ--0.0- 730 TANG PT-25 DX-.8989 DY--4 DZ---.5837 *RRE MOD BRAD PT-25B RA-3.25 *POINT ADDED TO ACCOMODATE BEND TANG PT-SA4 DX--2.4027 DY-0 DZ- -3.6998 TANG PT-33 DX--0.185 DY-0 DZ- -0.2849 TANG PT-35 DX--0.1948 DY-0 DZ---0.2782 *PR-43 GAP 12 TANG PT-36 DX--0.4873 DY-0 DZ- -0.6959 TANG PT-SA3 DX--0.5461 DY-0 DZ- -0.6508 TANG PT-37 DX--0.2201 DY-0 DZ---0.2623 TANG PT-38 DX--0.2292 DY-0 DZ---0.2545 TANG PT-39 DX--0.2273 DY-0 DZ- -0.2524 TANG PT-40 DX--0.2359 DY-0 DZ- -0.2443 TANG PT-43 DX--1.0638 DY-0 DZ---1.1016 *PR-69 GAP 12 TANG PT-45 DX--1.2230 DY-0 DZ- -0.9216 TANG PT-48 DX--0.5596 DY-0 DZ- -0.4974 TANG PT-50 DX--0.5885 DY-0 DZ- -0.3047 *ADJTUSTED TO AVOID PIPESTRESS ERROR TANG PT-51 DX--0.4201 DY-0 DZ- -0.2175 TANG PT-52 DX--0.4335 DZ--0.2496 *PR-47 GAP 12 TANG-PT-55 DX--2.8166 DZ--1.6216 BRAD PT-55A RA-3.25 *RRE MOD TANG PT-55F DY--3.250

• SECTION OF ME101 CODE THAT MODELS '

CROS OD-26.0 WT-1.158 MA-601.5 TANG PT-56 DY--0.667 TANG PT-57 DY--0.166 TANG PT-58 DY--1.682 TANG PT-59 DX-0 DY--3.357 DZ-0 TANG PT-61 DX-O DY--1.920 DZ-0 TANG PT-62 DX-0 DY-2.0 DZ-D *TO AVOID PIPESTRESS ERROR

• BACK TO NORMAL CROSS-SECTION CROS OD-26.0 WT-1.158 MA-332.8 TANG PT-65 DX-0 DY--3.365 DZ-0 BRAD PT-66 RA-3.25 TANG PT-67 DX--3.25 DZ--3.25 BRAD PT-70 RA-3.25 TANG PT-72 DZ--2.9063 TANG PT-74 DX-0 DY-0 DZ--1.9479 TA-1

---LUMPP-PT-74MAi.-926---926 -------

VALV PT-76 DX-0 DY-0 DZ--2.625 TH-2 MA-3.982 *INCLUDES DIST WT VALV PT-78 DX-0 DY-0 DZ--0.9583 TH-2 PL-1 JUNC PT-78 VALV PT-80 DX-0 DY-4.1798 DZ-4.1798 PL-3 MA-4.597 *OPERATOR JUNC PT-78 VALV PT-81 DX-0 DY-a DZ--1.6667 TH-2 PL-2 MA-1.926 TA-1 TANG PT-85 DX-0 DY-0 DZ--15.208 TA-1 ANCH PT-85 LV-1

• • • • • • MSRV LINE J BRANCH OFF AT PT-35 **********

Revision I A I I File No. HC-04Q-312 Page A3 of Al I

• GROUP 2 JUNC PT-35 CROS OD-8.625 WT-0.906 MA-85.05 BRAN PT-100 DX-0 DY-1.333 DZ-0 TE-4 TANG PT-101 DX-0 DY-0.6667 DZ-0 LUMP PT-101 MA-0.136 CRED PT-102 DX-0 DY-0.5833 DZ-O AN-30 TF'A-1 CROS OD-6.625 WT-1.436 MA-10.175 RL-1 LUMP PT-102- *MA-0.137 VALV PT-104 DX-0 DY-1.2813 DZ-0 PL-1 MA-0. 688 JUIC PT=104 VALV PT-108 DX--0.9215 DY-0.5625 DZ-0.6453 PL-3 MA-0.421 JUNC PT-104 VALV PT-11O DX=0.7082 DY-0 DZ--0.4959 PL-2 MA-0.047 TA-1 CROS OD-10.75 WT-0.73 MA-0.001 KL-1 TANG PT-112 DX-0.3157 DY-0 DZ--0.2211 LUMP PT-112 MA-0.047 CROS OD-10.75 WT-0.365 MA-40.48 RL-1 TANG PT-115 DX-1.2202 DY-0 DZ--0.8544 BRAD PT-115A RA-1.25 TANG PT-118 DX-026225 DY--0.9106 DZ-0.8890 LUMP PT-118 MA-0.010 TANG PT-125 DX-1.4144 DY--2.0689 DZ-2.0199 BRAD PT-125A RA-1.25 TANG PT-130 DX-0 DY-0 DZ-4.5885 BRAD PT-130A RA-1.25 TANG PT-131 DX--0.3238 DY--1.5104 DZ-0 LUMP PT-131 MA-0.1765 TANG PT-132 DX--0.1586 DY--0.7396 DZ-0 BRAD PT-132A RA-4.1667

-TANG PT-13B DX-0 DY--0.4688 DZ-0 TANG PT-133 DX-0 DY--0.3333 DZ-0 LUMP PT-133 MA-0.1765 TANG PT-134 DX-0 DY--3.1823 DZ-0 LUMP PT-134 MA-0.412 TANG PT-135 DX-a DY--3.5313 DZ-0 LUMP PT-135 MA-0.2114 TANG PT-20J DX-0 DY--4.3698 DZ-0 TANG PT-22J DX-0 DY--0.7083 DZ-0 JUNC PT-22J BRAN PT-24J DX-0.6134 DY-a DZ-0.3542 TE-1 TANG PT-26J DX-0.7217 DY-a DZ-0.4167 BRAD PT-27J RA-0.833 TANG PT-28J DY-0.833 EW-1 CRED PT-32J DX-0 DY-0.583 DZ-0 AN-3 0 EN-1 *REDUCER IS 7 IN LONG CROS OD-6.625 WTr0.280 MA-18.97 TANG PT-34J DX-a DY-0.3229 DZ-0 LUMP PT-34J MA-0.183 TANG PT-36J DX-0 DY-1.6667 DZ-0 LUMP PT-36J MA-0.400 JUNC PT-22J CROS OD-10.75 WT-a.365 MA-40.48 TANG PT-2J DX-0 DY--0.7083 DZ-a TANG PT-4J DX-0 DY--0.7083 DZ-0

-JUNC PT-4J BRAN PT;6-J 'DX- 0.61-34__DY-= - - DZ-a.35 42- -

TANG PT-8J DX--0.7217 DY-0 DZ-0.4167 BRAD PT-9J RA-0.833 *ADDED F OR CONVERSION TO PIPESTRESS TANG PT-10J DY-0.833 EW-1 CRED PT-12J DX-0 DY-0.583 DZ-0 AN-3 0 EW-1 CROS OD=6.625 WT-0.280 MA-18.97 TANG PT-16J DX-0 DY-0.3229 DZ-0 LUMP PT=16J MA-0.183 TANG PT-18J DX-O DY-1.6667 DZ-0 LUMP PT-18J MA-a.4a0 JUNC PT-4J CROS OD-10.75 WT-0.365 MA-40.48 lRevision I A I File No. HC-04Q-312 Page A4 of Al l

TANG PT=38J DX-0 DY--0. 7083 TANG PT-136 DX-0 DY--7.2083 DZ-0 TANG PT-138 DX-0 DY--2.5833 DZ-0 BRAD PT-139 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-140 DX--3.3960 DY-O DZ-1.3549 BRAD PT-140A RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-141 DX--0. 6485 DY-O DZ--1.6254 TANG PT-142 DX--0.2162 DY-0 DZ--0.5418 LUMP PT-142 MA-0.1765 TANG PT-14B DX--U.1853 DY-' DZ--0.4644 LUMP PT-14B MA-0. 1765 TANG PT-143 DX--0.3339 DY-0 DZ--0.8369 LUMP PT-143 MA-0.038 TANG PT-145 DX--1. 0808 DY-O DZ--2.7089 BRAD PT-146 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-148 DX-2.7864 DY-0 DZ--1.1117 TANG PT-149 DX-1. 1804 DY-D DZ--0.4709 LUMP PT-149 MA-0.038 TANG PT-150 DX-1. 6254 DY-O DZ--0.6485 BRAD PT-151 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-155 DX-1.8142 DY-U DZ-4.5473 BRAD PT-156 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-158 DX-0 DY--1.5833 DZ-O LUMP PT-158 MA-0.1765 TANG PT-160 DX-0 DY--1. 04 69 DZ-0 BRAD PT-161 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-170 DX-1.8446 DY--i.5045 DZ--0.7641 CROS OD-10. 75 WT-0.594 MA-64.33 TANG PT-175 DX-0.3688 DY--0.3011 DZ--0.1528 TANG PT-176 DX-0.3457 DY--0.2823 DZ--0.1432 TANG PT-180 DX-8. 4894 DY--6.9322 DZ--3.5164 TANG PT-182 DX-4.8871 DY--2.3324 DZ--2.0243 TA-1 ANCH PT-182 LO-1 X-U0.001 KY-409.1 EZ-452.9 MX-8.3e-5 MY-8.3e-5 MZ-8.3e-5 LV-2 vUNC PT-182 TANG PT-185 DX-8.2782 DY--3.9488 DZ--3.4289 BRAD PT-185A RA-1.25 TANG PT-19D DX-0.7973 DY-U DZ-1.9247 TA-1 *COMBIlED 186 AND 190 ANCH PT-19D LO-1 KX-1211.8 KY-1045.3 KZ-2519.2 MX-62101 MY-44513 MZ-28607 LV-2

• • • • • • • • MSRV LINE R BRANCH OFF AT PT-40 OF MSLA ****

• GROUP 3 JUNC PT-40 CROS OD-8.625 WT-0.906 MA-85.05 BRAN PT-200 DX-U DY-1.33 DZ-0 TE-4 TANG PT-201 DX-0 DY-0.6667 DZ-O LUMP PT-201 MA-0.136 CRED PT-202 DX-0 DY-0.5833 DZ-0 AN-30 TA-i CROS OD-6.625 WT-1.436 MA-10.175 KL-1 LUMP PT-202 MA-0.137 VALV PT-204 DX-0 DY-1.2813 DZ-0 PL-1 MA-0.688 JUNC PT-204 VALV PT-208 DX--0.3101 DY-0.5625 DZ-1.0814 MA-0.421 PL-3 TlN

- -7na VALV PT-210 DX-0.2382 DY-U DZ--0.8311 PL-2 IMA-0.047 CROS OD-10.75 WT=0.73 MA-U0001 KLL-1 TANG PT-212 DX-0.1062 DY-0 DZ--0.3705 TA-1 LUMP PT-212 MA-0.047 CROS OD-10.75 WT-0.365 MA-40.48 KL-1 TANG PT-215 DX-0.3445 DZ--1.2016 EW-1 BRAD PT-216 RA-1.25 EW-1 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-218 DX-1.4524 DY--1.0384 DZ-U. 4165 LUMP PT-218 MA-0.010 TANG PT-220 DX-1.1113 DY--0.7945 DZ-O. 3187 BRAD PT-221 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS Revision A, File No. HC-04Q-312 Page A5 of Al l

TANG PT-225 DX-2.0360 DY-0 DZ'-0.7411 BRAD PT-226 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-230 DX-1.2131 DY-0 DZ--2.072 BRAD PT-231 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT'234 DX-O DY--3.4688 DZ-0 LUMP PT-234 MA=0. 1765 TANG PT-235 DX-0 DY--0.375 DZ-0 TANG PT-236 DX-0 DY--1.8281 DZ-0 LUMP PT-236 MA-0. 1765 TANG PT-23S DX-0 DY--1.6719 DZ-0 LUMP PT-23S MA-0.2114 TANG PT-237 DX-0 DY--1.5156 DZ-0 LUMP PT-237 RA-0. 518 TANG PT-238 DX-O DY--2.276 DZ-0 TANG PT-239 DX'0 DY--3.833 DZ-0 LUMP PT-239 MA-0. 1765 TANG PT-240 DX-0 DY--3.333 DZ-0 BRAD PT-241 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-242 DX--3.2624 DY-0 DZ-2.3056 LUMP PT-242 MA-0. 020 TANG PT-245 DX--2.3181 DY-0 DZ-1. 6383 BRAD PT-246 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-250 DX-0 DY--5. 9271 DZ-0 BRAD PT-251 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-2R DX--0.9522 DZ--0.8098 TANG PT-4R DX--0.5396 DY-O DZ--0.4589 JUNC PT-4R BRAN PT-6R DX--0.4589 DY-O DZ-0.5396 TE-1 EW-1 TANP DX--.8098 DZ-.9522 *KREMOD,WAS:TANG PT-8R DX---0.8098 DY-0 D2-0.9522 BRAD PT-9R RA-1.25 *ADDED FOR CONVEERSION TO PIPESTRESS TANG PT-12R DX-0 DY-1.25 DZ-0 EW-1 CRED PT-14R DX-0 DY-0.583 DZ-0 AN-30 EW-1 CROS OD-6.625 WT-0.28 MA-18.97 TANG PT-16R DX-0 DY-0.3125 DZ-0 LUMP PT-16R MA-0.183 TANG PT-18R DX-0 DY-1.667 DZ-0 LUMP PT-18R MA-0.400 JUNC PT-4R CROS OD-10.75 VWT-0.365 MA-40.48 TANG PT-20R DX--0.5396 DY-0 DZ--0.4589 TANG PT-22R DX--0.9522 DY-0 DZ--0.8098 LUMP PT-22R MA-0.1765 TANG PT-23R DX--1.1744 DY-0 DZ--0.9988 LUMP PT-23R MA-0.382 TANG PT-26R DX--1.1269 DY-0 DZ--0.9583 TANG PT-28R DX--0.5396 DY-0 DZ--0.4589 EW-i JUNC PT-28R BRAN PT-30R DX--0.6209 DY-0 DZ-0.7300 TE-1 EW-1 CRED PT-34R DX--0.3780 DY-0 DZ-0.4444 AN-30 EW-1 CROS OD-6.25 WT'0.562 MA-36.39 BEND PT-38R X1--0.3238 ZI-0.3809 Y2-0.500 TA-1 TANG PT=40R DX-0 DY-0.3229 DZ-0 LUMP PT-40R MA-0.183 TANG PT-42R DX-0 DY-1.6667 DZ-0 LUMP PT-42R MA-0.400

--JUNC-- -

PT-28R CROS OD-10.75 WT-0.365 MA-40.48 TANG PT-44R DX--0.5396 DY-0 DZ--0.4589 TANG PT-253 DX--0.4919 DY-O D2--0.4184 BRAD PT-253A RA-1.25 *ADDED FOR CONVIERSION TO PIPESTRESS TANG PT-254 DX-0.0899 DY-O DZ--1.0273 LUMP PT-254 MA-0.1765 TANG PT-255 DX-0.1548 DY-0 DZ--1.7693 BRAD PT-256 RA-1.25 EW-1 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-258 DX-0 DY--4.1875 DZ-0 LUMP PT-258 MA-0.1765 V

TANG PT-260 DX-0 DY--0.75 D2-0 Revision I A l l File No. HC-04Q-312 Page A6 of Al l

LUMP PT-260 MA-0.1639 TANG PT-275 DX-0 DY--2.5781 DZ-0 BRAD PT-276 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-280 DX-0.1910 DY-0.3750 DZ--0.4611 CROS OD-10 75 WT-0.594 MA-64.33 TANG PT=284 DX-0.15277 DY--0.3011 DZ--0.3688 TANG PT-285 DX-0.1432 DY--0.2823 DZ--0.3457 TANG PT-287 DX-3.5164 DY--6.9322 DZ--8.4894 TANG PT-288 DX-2.0243 DY--2.3324 DZ--4.8871 TA-1 ANCH PT-288 LO=1 KX-0.001 KY-409.1 KZ-452.9 MX-8.3e-5 MY-8.3e-5 MZ-8.3e-5 LV=2 JUNC PT-288 TANG PT-289 DX-3.4289 DY--3.9488 DZ--8.2782 BRAD PT-289A RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS CROS OD-10.75 WT-1.125 KA-115.25 *COMBINED PTS 290, 291 TANG PT-291 DX-1.9247 DY-0 DZ-0.7973 TA-1 ANCH PT-291 LO-1 KX-1211.8 KY-1045.3 KZ-2519.2 MX-62101 MY-44513 MZ-28607 LV-2 MSRV LINE A BRANCH OFF AT PT-45 OF MSLA *

• • • • • *******t**********************************************

• GROUP 4 JUNC PT-45 CROS OD-8.625 WT-0.906 MA-85.05 BRAN PT-300 DX-0 DY-1.333 DZ-0 TE-4 TANG PT-302 DX-0 DY-0.6667 DZ-0 EW-1 LUMP PT-302 MA-0.136 CRED PT-303 DX-0 DY-0.5833 DZ-0 AN-30 TA-1 CROS OD-6.625 WT-1.436 MA-10.175 KL-1 LUMP PT-303 MA-0.137 VALV PT-304 DY-1.2813 PL-1 MA-0.688 JUNC PT-304 VALV PT-308 DX--0.1371 DY-0.5625 DZ-1.1166 PL-3 MA-0.421 JUNC PT-304 VALV PT-310 DX-0.1054 DZ--0.8582 PL-2 MA-0.047 TA-1 TANG PT-312 DX-0.0470 DY-0 DZ--0.3825 LUMP PT-312 MA-0.047 CROS OD-10.75 WT-0.365 MA-40.48 TANG PT-313 DX-0.1028 DY-0 DZ--0.8375 LUMP PT-313 MA-0.0381 TANG PT-315 DX-0.1358 DY-0 DZ--1.1063 LUMP PT-315 MA-0.382 TANG PT-316 DX-0.0800 DY-0 DZ--0.6514 LUMP PT-316 MA-0.010 TANG PT-317 DX-0.1587 DY-0 DZ--1.2924 BRAD PT-318 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-320 DX-4.7031 DY-0 DZ-0 BRAD PT-321 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-322 DX-0 DY--1.5 DZ-0 TANG PT-323 DX-0 DY--4.1563 DZ-O TANG PT-324 DX-0 DY--3.6094 DZ-0 LUMP PT-324 MA-0.412 TANG PT-330 DX-0 DY--2.7135 DZ-0 BRAD PT-331 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-2A DX--1.0851 DY-0 DZ-0.6206 TANG-PT-4A---DX--0.6149-- DY-O-- DZ-0.3517- -

TANG PT-20A DX--0.6149 DY-0 DZ-0.3517 TANG PT-22A DX--0.6149 DY-0 DZ-0.3517 TANG PT-38A DX--0.6149 DY-0 DZ-0.3517 TANG PT-332 DX--0.434 DY-0 DZ-0.2483 LUMP PT-332 MA-0.025 TANG PT-333 DX--1.7452 DY-0 DZ-0.9981 LUMP PT-333 MA-0.1765 TANG PT-335 DX--1.1574 DY-0 DZ-0.6620 BRAD PT=335A RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-336 DX-0 DY--1.8125 DZ-0 LUMP PT-336 MA-0.1765 Revision l A I I I File No. HC-04Q-312 Page A7 of All

TANG PT-338 DX-0 DY--4.0521 DZ-0 LUMP PT-338 MA-0.389 TANG PT-340 DX-C DY--4.3542 DZ-0 BRAD PT-341 RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-342 DX-0 DY--3.1816 DZ--3.1816 TANG PT-345 DX=a DY--1.9851 DZ--1.9851 BRAD PT-345A RA-1.25 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-346 DX-o DY--1.5521 DZ-0 LUMP PT-346 MA-0.1765 TANG PT-348 DX-0 DY--0.8073 DZ-O LUMP PT-348 MA-0.382 TANG PT-350 DX-0 DY--1.3906 DZ-0 LUMP PT-350 MA-0.1765 TANG PT-365 DX-0 DY--2.4948 DZ-0 EW-1 BRAD PT-366 RA-1.25 EW=1 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-370 DX-0.1910 DY--0.375 DZ--0.4611 CROS OD-10. 75 WT-0.594 MA-64.33 TANG PT-384 DX-0.1528 DY--0.3011 DZ--0.3688 TANG PT-385 DX-0.1432 DY--0.2823 DZ--0.3457 TANG PT-390 DX-3.5164 DY--6.9322 DZ--8.4894 TANG PT-392 'DX-2.0243 DY--2.3324 DZ--4.8871 TA-i ANCH PT-392 LO-1 KX-0.001 KY-409.1 KZ-452.9 MX-8.3e-5 MY-8.3e -5 MZ-8.3e-5 LV-2 JUNC PT-392 TANG PT-394 DX-3.4289 DY--3.9488 DZ--8.2782 BRAD PT-394A RA-1.25 TANG PT-395 DX--1.1548 DZ--0.4784 CROS OD-10.75 WT-1.125 MA-115.25 TANG PT-396 DX--0.7699 DY-0 DZ--0.3189 TA-1 ANCH PT-396 LO-1 KX-1211.8 KY-1045.3 KZ-2519.2 MX-62101 MY-44513 MZ-28607 LV-2 JUNC PT-22A CROS OD-10.75 WT-0.365 MA-40.48 BRAN PT-24A DX-0.3517 DY-0 DZ-0.6149 TE-1 EW-1 CRED PT-26A DX-0.1448 DY-0 DZ-0.2532 AN-30 EW-1 CROS OD-6.625 WT-0.280 MA-18.97 TANG PT-28A DX-0.1448 DY-0 D2-0.2532 BEND PT-32A X1-0.2482 Z1-0.4340 Y2-.5 INDI AT-32A C2-1.9 P2-2.0 TANG PT-34A DX-0 DY-0.3229 D2-0 LUMP PT-34A MA-0.183 TANG PT-36A DX-0 DY-1.6667 DZ-0 LUMP PT-36A MA-0.400 JUNC PT-4A BRAN PT-6A DX-0.3517 DY-0 DZ-0.6149 TE-i CRED PT-1OA DX-0.2896 DY-a DZ-0.5064 AN-30 EW-'1 CROS OD-6.625 WT-0.280 MA-18.97 BEND PT-14A XI-0.2482 Z1-0.4340 Y2-0.5 TA-1 TANG PT-16A DX-0 DY-0.3229 DZ-0 LUMP PT-16A MA-0.183 TANG PT-18A DX-0 DY-1.6667 DZ-0 LUMP PT-18A MA-0.400

• • • • • I**************** ********* **************************

• • • • • RCIC LINE A BRANCH OFF AT PT-SO OF MSLA *****

--*GRO>UP-5 JUNC PT-50 CROS OD=4.50 WT-0.337 MA-21.48 BRAN PT-402 DX-O DY--1.25 DZ-0 TE-4 TANG PT-405 DX-0 DY--0.2083 DZ-0

• TANP DY--0.2083 *KRE MOD, ORIGINAL IS:TANG PT-405 DY--0.2083 DZ-0 BRAD PT-406 RA-0.5 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-410 DX--0.75 DY--0.750 DZ-0 BRAD PT-411 RA-0.5 TANG PT-412 DX-0 DY--0.7604 DZ-0 TANG PT-413 DX-0 DY--1.9167 DZ-0 BRAD PT-414 RA-0.5 *ADDED FOR CONVERSION TO PIPESTRESS Revision A I File No. HC-04Q-312 Page A8 of All

TANG PT'415 DX-1.2829 DY'0 DZ-0.3437 TANG PT-416 DX-1.9369 DY-0 DZ-0.5190 LUMP PT=416 MA-0.007 TANG PT-418 DX-0.8251 DY-O DZ-0.2211 LUMP PT-418 MA-0.007 TANG PT-419 DX-1.3483 DY-0 DZ-0.3613 CROS OD-4.50 WT-0.337 MA-29.1 I KL-1 TANG PT-420 DX-0.3220 DY-0 DZ-0.0863 TANG PT-421 DX-0.1459 DY-O. DZ0.0391 TANG PT-423 DX-0.2767 DY-0 DZO0.0741 TANG PT-424 DX-0.9458 DY-0 DZ-0.2534 TANG PT-426 DX-0.322 DY-O DZ-0.0863 CROS OD-4.50 WT-0.337 MA-21.48 TANG PT-427 DX-0.5635 DY-0 DZ-0.1510 CROS OD-4.5 WT-0.337 MA-21.48 TANG PT-428 DX-1.2074 DY-O DZ-0.3235 BRAD PT-428A RA-0.5 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-429 DX-0.3451 DY-O DZ--1.2879 TANG PT-430 DX-0.4314 DY-O DZ--1.6099 BRAD PT-430A RA-0.5 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-431 DX--1.2074 DY-0 DZ--0.3235 TANG PT-432 DX--2.6563 DY-0 DZ--0.7118 LUMP PT-432 MA-0.007 TANG PT-434 DX--1.0313 DY-0 DZ--0.2763 LUMP PT-434 MA-0.007 TANG PT-436 DX--0.3371 DY-O DZ--0.0903 LUMP PT-436 MA-0.007 TANG PT-438 DX--1.8866 DY-O DZ--0.5055 TANG PT-440 DX--1.2477 DY-0 DZ--0.3343 BRAD PT-440A RA-0.5 *ADDED FOR CONVERSION TO PIPESTRESS TANG PT-441 DX-O DY--0.9792 DZ-O TANG PT-442 DX-O DY--0.7396 DZ-0 LUMP PT-442 MA-0.007 TANG PT-445 DX-O DY--2.6875 DZ-0 BRAD PT-446 RA-1.666 *5D ADDED FOR CONVERSIOEI TO PIPESTRESS TANG PT-450 DX-1.125 DY--1.9479 DZ-0 BRAD PT-451 RA-1.666 *5D ADDED FOR CONVERSIOtN TO PIPESTRESS TANG PT-452 DX-0 DY--4.375 DZO0 TANG PT-455 DX-0 DY--1.4167 DZ-0 BRAD PT-455A RA-0.5 *L ADDED FOR CONVERSION ro PIPESTRESS TANG PT-456 DX-0.75 DY-0 DZ-0 LUMP PT-456 MA-0.007 TANG PT-457 DX-1.0 DY-0 DZ-0 LUMP PT-457 MA-0.007 TANG PT-460 DX-7.5365 DY-0 DZ-0 TANG PT-462 DX-0.5 DY-0 DZ-0 TA-1 LUMP PT-462 MA-0.0575 CROS OD-4.5 WT-0.337 MA-6.5 KL-1 VALV PT-465 MA-0.119 DX-0.5833 DY-0 DZ-0 PL-1 JUNC PT-465 VALV PT-468 MA-0.240 DX-O DY-2.2375 DZ-0 PL-3 JUNC PT-465 VALV PT-470 MA-0.0615 DX-0.5833 DY-0 DZ-0 PL-2 TA-1 CROS OD=4.5 WT-0.337 MA-21.48 TANG PT-472 DX=0.8333 DY-0 DZ-0

--TANG- PT'474--- DX-0. 75 --Y'0 DZ-0 TANG PT-475 DX-0.75 DY-0 DZ-0 CROS OD-4.5 WT-0.5 MA-27.86 TANG PT-478 DX-10.792 DY-0 DZ-O TANG PT-480 DX-4.0 DY-0 DZ-0 TA-1 ANCH PT-480 LV-1

• *

• SYSTEM RESTRAINTS/ SUPPORTS *

• MSL-A RESTRAINTS VSUP PT-10 DX-0.6725 DY-0.7071 DZ'-0.2185 SP-0.001 KL=1 VSUP PT-12 DX--0.309 DY'0.0 DZ--0.9511 SP-0.001 KL-1 Revision I A I 1 I File No. HC-04Q-312 Page A9 of All

VSUP PT-12 DX-0.9511 DY=0.0 DZ--0.309 SP-0.001 RL-1 SNUB PT-SA2 DX-0.5446 DY-0 DZ-0.8387 SP-800 LV-1 RSTN PT-SA2 DX-0.5446 DY-0 DZ-0.8387 LV-1 SNUB PT-SA1 DX-0.9030 DY-0.2271 DZ--0.3648 SP-800 LV-1 RSTN PT-SA1 DX-0.9030 DY-0.2271 DZ--0.3648 LV-1 VSUP PT-25 DX--0.259 DY-0.0 DZ--0.966 SP-0.OOl RL-1 VSUP PT-25 DX-0.933 DY-0.259 DZ--0.25 SP-0.001 RL-1 SNUB PT-SA4 DX-0.7793 DY-0.3694 DZ--0.5061 SP-800 LV-1 RSTN PT-SA4 DX-0.7793 DY-0.3694 DZ--0.5061 LV-1.,

VSUP PT-35 DX-0.8387 DY-0.0 DZ--0.5446 SP-0.001 RL-1 VSUP PT-35 DX'0.0 DY-1.0 DZ-0.0 SP-0.001 RL-1 SNUB PT-SA3 DX--0.5428 DY-0.7057 DZ-0.4554 SP-800 LV-1 RSTN PT-SA3 DX--0.5428 DY-0.7057 DZ-0.4554 LV-1 VSUP PT-43 DX-0.669 DY-0.0 DZ--0.743 SP-0.001 KL-1 VSUP PT-43 DX-0.0 DY-1.0 DZ-0.0 SP-0.001 VSUP PT-52 DX-0.0 DY-1.0 DZ-0.0 SP-0.001 RSTN PT-56 DX-l.O DY-0.0 DZ-0.0 SD-8125 LV'1 RSTN PT-57 DX-0.0523 DY-0.0 DZ-0.9986 SD-1263.6 LV-1 VSUP PT-61 DX-0.0 DY-1.0 DZ-0.0 SP-0.001 RSTN PT-61 DX-1.0 DY-0.0 DZ-0.0 SD-8114 LV'1 VSUP PT-65 DX-0.0 DY-l.O DZ-0.0 SP-0.0D0 RSTN PT-72 DX-1.0 DY-0.0 DZ-0.0 SD-4264 LV-1 RSTN PT-72 DX-0.0 DY-1.0 DZ-0.0 SD-11601 LV-1

• J-BRANCH RESTRAINTS

• SNUB PT-131 DX--0.0610 DY-0 DZ--0.9981 SP-1060.7 SNUB REDUCTION RSTN PT-131 DX--0.0610 DY-0 DZ--0.9981 LV-2 *SNUB REDUCTION

• SNUB PT-133 DX--0.9665 DY-0 DZ-0.2569 SP-1005.6 SNUB REDUCTION RSTN PT-133 DX--0.9665 DY-0 DZ-0.2569 LV-2 *SNUB REDUCTION

• SNUB PT-134 DX-0 DY-1 DZ-O SP-492 SNUB REDUCTION RSTN PT-134 DX-0 DY-1 DZ-0 LV-2 *SNUB REDUCTION VSUP PT-135 DX-0.0 DY-1.0 DZ-0.0 SP-1.8 FO-4.031 LV-2

• SNUB PT-343 DX-0.6799 DY-0 DZ-0.7333 SP-1060.7 SNUB REDUCTION RSTN PT-34J DX-0.6799 DY-0 DZ-0.7333 LV-2 *SNUB REDUCTION

• SNUB PT-34J DX--0.4258 DY-0 DZ-0.9048 SP-1060.7 SNUB REDUCTION

• SNUB PT-16J DX-0.7718 DY-0 DZ-0.6359 SP-1060.7 SNUB REDUCTION RSTN PT-16J DX-0.7718 DY-O DZ-0.6359 LV-2 *SNUB REDUCTION

• SNUB PT-142 DX-0 DY-I DZ-o SP-1060.7 SNUB REDUCTION RSTN PT-142 DX-0 DY-1 DZ-0 LV-2 *SNUB REDUCTION SNUB PT-14B DX-0.9288 DY-0 DZ--0.3706 SP-1060.7 LV-2 VSUP PT-143 DX-0.0 DY-1.0 DZ-0.0 SP-0.168 FO-0.458 LV-2 RSTN PT-148 DX--0.3706 DY-0.0 DZ--0.9288 LV-2 VSUP PT-149 DX-0.0 DY-1.0 DZ-0.0 SP-0.300 FO-0.702 LV-2

• SNUB PT-158 DX-0.9063 DY-0 DZ-0.4226 SP-1060.7 SNUB REDUCTION

• • R-BRANCH RESTRAINTS

• SNUB PT-234 DX-0.8988 DY-0 DZ-0.4384 SP-1005.6 SNUB REDUCTION

• SNUB PT-236 DX-0.6428 DY-a DZ--0.7660 SP-1060.7 SNUB REDUCTION RSTN PT-236 DX-0.6428 DY-0 DZ--0.7660 LV-2 *SNUB REDUCTION VSUP PT-23S DX-0.0 DY-1.0 DZ-0.0 SP-0.448 FO-1.009 LV-2

• SNUB PT-237 DX-0.0 DY-1 DZ-0 SP-2121.4 SNUB REDUCTION RSTN PT-237 DX-0.0 DY-I DZ-0 LV-2 *SNUB REDUCTION

• SNUB PT-239 DX--0.9659 DY-0 DZ--0.2588 SP-870.2 SNUB REDUCTION RSTN PT-239 DX--0.9659 DY-O DZ--0.2588 LV-2 *SNUB REDUCTION VSUP PT-242 DX-0.0 DY-1.0 bZ-0.0 SP-1.2 FO-2.964 LV-2

• SNUB PT-16R DX-0.6280 DY-O DZ--0.7782 SP-1060.7 SNUB REDUCTION RSTN PT-16R DX-0.6280 DY-0 DZ--0.7782 LV-2 *SNUB REDUCTION SNUBPT-16R DX-0-.7880--DY-0-- DZ-0.6157---SP-1060.-7--SNUB REDUCTION-------------------

• SNUB PT-22R DX-0 DY-1 DZ-0 SP-1060.7 SNUB REDUCTION RSTN PT-22R DX-D DY-1 DZ-0 LV-2 *SNUB REDUCTION

• SNUB PT-23R DX--0.7618 DY-0 DZ--0.6479 SP-2121.4 SNUB REDUCTION RSTN PT-23R DX--0.7618 DY-0 DZ--0.6479 LV-2 *SNUB REDUCTION

• SNUB PT-40R DX--0.9488 DY-0 DZ-0.3158 SP-216.6 SNUB REDUCTION

• SNUB PT-40R DX--0.8046 DY-0 DZ--0.5938 SP-216.6 SNUB REDUCTION RSTN PT-40R DX--0.8046 DY-0 DZ--0.5938 LV-2 *SNUB REDUCTION

• SNUB PT-254 DX-0 DY-1 DZ-0 SP-1060.7 SNUB REDUCTION RSTN PT-254 DX-0 DY-i DZ-D LV-2 *SNUB REDUCTION

• SNUB PT-258 DX--0.7071 DY-0 DZ--0.7071 SP-1005.6 SNUB REDUCTION RSTN PT-258 DX--0.7071 DY-0 DZ--0.7071 LV-2 *SNUB REDUCTION

VSUP PT-260 DX-0.0 DY-1.0 DZ-0.0 SP-1.04 FO=2.507 LV-2

• A-BRANCH RESTRAINTS VSUP PT-313 DX-0.0 DY-1.0 DZ-0.0 SP-0.225 FO-2.346 LV-2 SNUB PT-315 DX--0.9925 DY-0 DZ--0.1219 SP-1060.7 LV-2 RSTN PT-315 DX--0.9925 DY-0 DZ--0.1219 LV-2

• SNUB PT-324 DX=0 DY-1 DZ-0 SP-492 SNUB REDUCTION RSTN PT-324 DX-0 DY-1 DZ-0 LV-2

• SNUB PT-16A DX-0.8660 DY-0 DZ--0.5 SP-1060.7 SNUB REDUCTION

• SNUB PT-16A DX-0.6428 DY-0 DZ-0.7660 SP-956 SNUB REDUCTION RSTN PT-16A DX-0.6428 DY-0 DZ-0.7660 LV-2 *SNUB REDUCTION

• SNUB PT-34A DX-0.6428 DY-0 DZ-0.7660 SP-956 SNUB REDUCTION RSTN PT-34A DX-0.6428 DY-0 DZ-0.7660 LV-2 *SNUB REDUCTION SNUB PT-34A DX--0.7071 DY-0.0861 DZ-0.7071 SP-911.1 SNUB REDUCTION VSUP PT-332 DX-0.0 DY-1.0 DZ-0.0 SP-1.6 FO-3.372 LV-2

• SNUB PT-333 DX--0.4611 DY-0.1435 DZ--0.8757 SP-1060.7 SNUB REDUCTION RSTN PT-333 DX--0.4611 DY-0.1435 DZ--0.8757 LV-2 *SNUB REDUCTION

• SNUB PT-336 DX-0.9848 DY-a0 DZ--0.1736 SP-1005.6 SNUB REDUCTION RSTN PT-336 DX-0.9848 DY-0 DZ--0.1736 LV-2 *SNUB REDUCTION

• SNUB PT-338 DX-0 DY-1 DZ-0 SP-2121.4 SNUB REDUCTION RSTN PT-338 DX-0 DY-1 DZ-0 LV-2 *SNUB REDUCTION VSUP PT-342 DX-0.0 DY-1.0 DZ-0.0 SP-0.680 FO-1.740 LV-2 .

• SNUB PT-346 DX--0.3353 DY-0 DZ-0.9421 SP-1060.7 SNUB REDUCTION

• SNUB PT-348 DX-0 DY-1 DZ-0 SP-2011.2 SNUB REDUCTION

• SNUB PT-350 DX--0.9945 DY-0 DZ-0.1045 SP-956 SNUB REDUCTION RSTN PT-350 DX--0.9945 DY-0 DZ-0.1045 LV-2 *SNUB REDUCTION

• RCIC BRANCH VSUP PT-412 DX--0.866 DY-0.0 DZ--0.5 SP-0.001 KL-1 VSUP PT-412 DX-0.5 DY-0.0 DZ--0.866 SP-0.001 KL-1 VSUP PT-415 DX-0.259 DY-0.0 DZ--0.966 SP-0.001 KL-1 VSUP PT-415 DX-0.0 DY-1.0 DZ-0.0 SP-0.001 SNUB PT-416 DX--0.2588 DY-O DZ-0.9659 SP-37 LV-1 VSUP PT-418 DX-0.0 DY-1.0 DZ-0.0 SP-0.126 FO-0.310 VSUP PT-427 DX-0.259 DY-0.0 DZ--0.966 SP-0.001 EL-1 VSUP PT-427 DX-0.0 DY-1.0 DZ-0.0 SP-0.001 VSUP PT-429 DX-0.966 DY-0.0 DZ-0.259 SP-0.001 KL-1 VSUP PT-429 DX-0.0 DY-1.0 DZ-0.0 SP-0.001 VSUP PT-431 DX-0.259 DY-0.0 DZ--0.966 SP-0.001 KL-1 VSUP PT-431 DX-0.0 DY-1.0 DZ-0.0 SP-0.001 VSUP PT-432 DX-0.0 DY-1.0 DZ-0.0 SP-0.126 FO-0.260 SNUB PT-434 DX--0.2588 DY-0 DZ-0.9659 SP-40 LV-1 RSTN PT-434 DX--0.2588 DY-0 DZ-0.9659 LV-1 SNUB PT-436 DX-0 DY-1 DZ-0 SP-84 LV-1 RSTN PT-436 DX-0 DY-i DZ-0 LV-1 VSUP PT-438 DX-0.259 DY-0.0 DZ--0.966 SP-0.001 KL-1 VSUP PT-438 DX-0.0 DY-1.0 DZ-0.0 SP-0.001 VSUP PT-441 DX--0.866 DY-0.0 DZ--0.5 SP-0.001 KL-1 VSUP PT-441 DX--0.259 DY-0.0 DZ--0.966 SP-0.001 EL-1 VSUP PT-441 DX--0.5 DY-0.0 DZ-0.866 SP-0.001 KL-1 SNUB PT-442 DX--0.9033 DY-0 DZ--0.4289 SP-83 LV-1 RSTN PT-442 DX--0.9033 DY-0 DZ--0.4289 LV-1 VSUP PT-452 DX-1.0 DY-0.0 DZ-0.0 SP-0.001 KL-1 RSTN PT-456 DX-0.0 DY-1.0 DZ0-.0 SD-769 LV-1 RSTN PT-456 DX'0.0 DY-0.0 DZ-1.0 SD-2222 LV-1 RSTN PT-457 DX-0.0 DY-1.0 DZ-0.0 SD-625 LV-l VSUP PT-457 DX-0.0 DY-0.0 DZ-1.0 SP-0.001 KL-1

-RsTN -PT-4714 -DX-0;:0 - -DY1-.0;-- -- DZ-0-;0- -- SD-152--- LV RSTN PT-474 DX-0.0 DY-0.0 DZ-1.0 SD-50 LV-1 ENDP

> Revision A File No. HC-04Q-312 Page All of All

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.TN NNUU Ut) DD DD 77 BB BB NN NN UUEUUU DDDDD 77 BBBBBB USERID: NUD7B DOCUMENT NUMBER: 24 PRINTED ON 11/3/04 9:58:24 AM

L FILE No.: HC-04Q-313 4 STRUCTURAL CALCULATION INTEGRITY PACKAGE PROJE CT No.: HC-04Q Associates, Inc.

PROJECT NAME: Hope Creek Extended Power Uprate Piping Vibration Monitoring CLIENT: PSEG Nuclear, LLC (Hope Creek)

CONTRACT NUMBER: 4500226359 Including C.O. #1 CALCULATION TITLE: Main Steam Line B Piping Vibration Acceptance Criteria Project Mgr. Preparer(s) &

Document Affected .. s.p.nApproval Checker(s)

Revision Pages Revision Description Signature & Signatures &

Date Date A 1-8 DRAFT Issue K. K. Fujikawa Carl R Limpus Appendix 7/28/2004 7/28/2004 A1-A13 Paul Hirschberg In 7/28/2004 Computer Files Page 1 of 8 F2001RI

Table of Contents

1.0 INTRODUCTION

............................................................ 3 2.0 VIBRATION ACCEPTANCE CRITERIA THEORY ............................................................ 3 3.0 CALCULATION OF ACCEPTANCE CRITERIA ............................................................ 4

4.0 REFERENCES

............................................................ 8 APPENDIX A FILES ............................................................. Al List of Tables Table 1: Nodal Accelerations and Acceptance Criteria Due to 1g Spectrum Input ................................. 5 Table 2: Nodal Displacements and Acceptance Criteria Due to ig Spectrum Input ............................... 5 List of Figures Figure 1: Main Steam Line B Piping PIPESTRESS model ............................................................ 6 Figure 2: Locations of Accelerometers on 26 inch Main Line B and MS 10" P Branch ......................... 7 I - ________________ - -

Revision I A File No. HC-04Q-313 Page 2 of 8

1.0 INTRODUCTION

The purpose of this calculation is to develop vibration acceptance criteria for the accelerometers installed on the Hope Creek main steam line B piping.

2.0 VIBRATION ACCEPTANCE CRITERIA THEORY The acceptance criterion is based on the guidance of ASME OM S/G Part 3 [1], which states that the calculated stress shall not exceed Sel/ac. The equation from OM Part 3 for the stress criteria is given below:

Salt=C2K2M<Sel/a Where alt Alternating stress as defined in ASME Code (NB-3600)

C2 Secondary stress index as defined in ASME Code K2 Local stress index as defined in ASME Code M Maximum zero to peak dynamic moment loading due to vibration only Z = Section modulus of the pipe Sel 0.8SA, where SA is the alternating stress at 106 cycles from Figure I-9.1 of Section III of the ASME Code [2] for carbon steel

= Allowable stress reduction factor, 1.3 for carbon steel The piping within the scope of this analysis is A106 Grade B carbon steel [3]. For carbon steel pipe, SA = 12,500 psi, thus, the maximum allowed stress due to steady state vibration is 0.8*12,500 psi /1.3

= 7,692 psi.

The acceptance criteria for the accelerations to be measured is determined by multiplying the calculated acceleration at each sensor location in a unit load analysis by the ratio of the allowable steady state stress to the maximum calculated stress in the piping system. This may be expressed by multiplying the accelerations for each direction by a factor, and the factor is defined as:

F = 7692 psi / Oa.

-where.F-isthe factor-and sm.,: is the maximum.stress obtained from the dynamic analy.sis. ___

It should be noted that exceedance of the allowable acceleration or displacement in one direction at a location does not necessarily indicate exceedance of the OM-3 criteria, as the stresses at a location are a function of the SRSS combination of the accelerations in three orthogonal directions. In addition, review of the frequency content of the collected data may allow for refinement of the shape of the input response spectra. The acceptance criteria are conservative, and if met, will eliminate the need for further review to justify the acceptability of the measured accelerations.

lRevision A l 1-313 Page 3 of 8

-313 Page 3 of 8

3.0 CALCULATION OF ACCEPTANCE CRITERIA A PIPESTRESS [4] model was developed in Reference [3] and is shown in Figure 1. A flat 1 g spectrum (0.1 g below 5 Hz) was applied in each of the three orthogonal directions. Static loads such as weight and thermal expansion are not considered since these loads do not contribute to the cyclic loading of the piping system. Additionally, seismic (inertia and anchor movements) and turbine stop valve loads are not considered since these loads are transient dynamic loads and do not contribute to the steady-state cyclic loading of the system.

Due to extended power uprate, the flow in the main steam lines will increase, which can potentially cause the vibration of the piping to increase due to flow induced vibration. Since the forcing function can occur over a range of frequencies, a broad band amplified response spectra (ARS) of I g, applied in each direction, was used to analyze the main steam piping system. This dynamic analysis provides the response of the piping system to a broad band ARS that corresponds to white noise input. As the vibration is flow induced, the vibration loading was applied only to the sections of piping normally containing flow. The displacements, accelerations and stresses due to the broad band ARS in each of the three orthogonal directions were calculated at each node in the piping system. The total response was obtained by combining the results from each of the three directions by square-root-sum-of-the-squares.

The calculated maximum stress in the model due to a flat Ig input in each direction is 24,417 psi at Node 26P. Acceptance criteria are calculated for the 4 accelerometer locations. They are Nodes 490 (Main B), 460 (Main B), 534 (Main B), and 40P (SRV P branch). The locations of the accelerometers are shown in Figures 2 and 3. Reference [3] provides details of the selection of the accelerometer locations. The acceleration acceptance criterion calculation for Node 490 is shown below. The acceleration values for each node are shown in Table I and the displacement values are shown in Table 2.

Ax= direction not monitored Ay = 7692 / 24417

• 0.940 g = 0.296 g A, = 7692 / 24417

• 0.742 g = 0.234 g Revision A l File No. HC-04Q-313 Page 4 of 8

Table 1: Nodal Accelerations and Acceptance Criteria Due to 1g Spectrum Input Acceleration (g) Acceptance Criteria (g)

Node - X Y Z X Y -.. Z 490 0.780 0.940 0.742 _ 0.296 0.234 460 1.504 0.841 1.215 0.474 0.265 0.383 534 1.026 1.088 0.690 J 0.323 0.343 -

40P 3.217 0.384 2.008 1 1.013 0.121 0.633 Table 2: Nodal Displacements and Acceptance Criteria Due to ig Spectrum Input Displacement (in) Acceptance Criteria (in)

Node X Y Z X Y Z 490 0.017 0.029 0.035 - 0.009 0.011 460 0.079 0.009 0.082 0.025 0.003 0.026 534 0.019 0.063 0.010 0.006 0.020 -

40P 0.174 0.011 0.073 0.055 0.003 0.023

-- -.- .1 Revision l A l l File No. HC-04Q-313 Page 5 of 8

ts-n so h r aptl tutu -

1

---

-. A[.- ---- wF1i51 riqiure A: Srillmo VIEW WS;t~R. . .rL L~ .. l I __________-I SiPJARI

X\ary7anI~tcnE)

-C4O IHSL-B)%\Pip.e8tr*3x fl.s\N5*lWDW2.r.l r03/04/0

&CAI0 )?31

.1t" f IISD913 1 Figure 1: Main Steam Line B Piping PIPESTRESS model Revision l A I I I i I File No. HC-04Q-313 Page 6 of 8

in- 5~s.04 Alion IvFhe,, I ,5.4 Aws ,Ot ICS I "I lDP<O X341 MS.BD.6 II EL 1 5-,-

xAyl 'b1/

/1sX em *.* ! Ip.49O Ill

-1 trt 1 I.. - .,-,rrX s::!.lri^no Oir.\ll^-O4giZOI^\to 4: IM.(.43111104 -9,47CSi B044'Jnqr.i (LC\iC-0q,\3O1A5.H4ITm.fr. 001,t04 CT.32,-

Figure 2: Locations of Accelerometers on 26 inch Main Line B and MS 10" P Branch Revision l! A I I I I I Page 7 of 8]

File No. HC-04Q-313

4.0 REFE,RENCES

1. ASME OM-S/G-1994, Standards and Guides for Operation and Maintenance of Nuclear Power Plants, Part 3, 1994 Edition, "Requirements for Preoperational and Initial Start-Up Vibration Testing of Nuclear Power Plant Piping Systems."

2. ASME Boiler and Pressure Vessel Code,Section III Appendices, 1989 Edition.

3. Structural Integrity Associates Calculation, Revision 0, "Main Steam Line B Piping Vibration Monitoring Locations," SI File No. HC-04Q-3 07.

4. PIPESTRESS2000 Solver, Version 3.5.0.67, DST Computer Services S.A., QA-1 670-301, May 15, 2002.

APPENDIX A FILES File Name Size Date & Time Description Location MSBIDW-AC-rl.fre 31.6 KB (32,407 bytes) July 26, 2004, PIPESTRESS input file A2 to A13 7:14:27 PM July262004, PIPESTRESS output file -

MSBBDW-AC rl.prc 552 KB (565,920bytes) 7l182 04, combined directions for In computer file

. 52 accelerations and displacements MSBH)W-ACuly.prf2623 KB (638,145 bytes) Jy26, 2004, PRIESTESS output file - stresses In computer file ISIWAr.r 2 B(3.4 byes 7:18:12 PM II

• • • MAIN STEAM LINE B MODEL FOR ACCEPTANCE CRITERIA (PH CHANGES) ***

IDEN JB-8 *JOB NO. (1 to 9999)

CD-1 *1-ASME Class 1 GR--Y *Direction of gravity VA-0 *0=Calculation 2-Verification 3-Design (HANGIT)

IU-1 *Input units 0-SIU 1-USA 2-USA2 OU-1 *Output units o-sru 1-USA CH-$ *Delimiter character replaces ?

AB-T *FREE errors - terminate execution PL-SPROB-MONITOR LOCATIONS PROJ-HC-04Q$

EN-$USER-CRL/SIS TITL BL-8 *Modelling option

• 8 - uniform mass for static analysis

• concentrated mass for dynamic analysis rotational inertia GL-0 *Print forces/moments 0-Global 1-Local 2-G and L SU-0 *Type 1 support summary 0-No 1-Yes CV--4 *Code version (see Manual)

HS-1 *Report 20 highest stress ratios for each load case MD-I ' *Hot modulus J6-1 *Skip minor WARNING messages TI-SMAIN STEAM LINE B INSIDE DRYWELL $

• • • • • • • • • • • • • • Frequency Load

• FREQ RF-1 RP-8 FR-100 MP-33 MX-100 TI-$MODALS

.**** THERMAL EXPANSION LOAD CASES

• LCAS RF-0 CA-1 TY-0 TI-SNormal Operation$

• • • • WEIGHT LOAD CASES

• LCAS CA-101 RF-1 TY-3 TI-$OPERATING WEIGHTS

• • • • DYNAMIC CASES

• RCAS CA-201 EV-1 TY-1 SU-1 FX-1 FY-0 FZ-0 TI-$X VIBRATION$

RCAS CA-202 EV-1 TY-1 SU-l FX-0 FY-1 FZ-0 TI-$Y VIBRATIONS RCAS CA-203 EV-1 TY-1 SU-1 FX-0 FY-0 FZ-1 TI-$Z VIBRATION$

• • • • LOAD COMBINATION CASES

• CCAS RF-1 CA-401 SS-1 ME-2 EQ-3 C1-201 C2-202 C3-203 FL-i TI-$VIBRATION STRESS+$

CCAS RF-1 CA-402 SS-1 ME-0 EQ-3 Ci-401 Fl--i TI-$VIBRATION STRESS-$

• • • • LOAD SETS

• LSET RF-i PR-1 MO-1 LSET RF-1 FL-1 FC-0 PR-1 MO-401 TI-$+VIB$

LSET RF-i FL-i FC-0 PR-i MO-402 TI-$-VIB$

SPEC FS-EVENT1 EV-1 ME-3 TI-$VIBRATION SPECTRUM$

LV-1 DI-X 0.35/0.1 5.0/0.1 5.1/1.0 100.0/1.0 DI-Y 0.35/0.1 5.0/0.1 5.1/1.0 100.0/1.0 DI-Z 0.35/0.1 5.0/0.1 5.1/1.0 100.0/1.0 LV-2 DI-X 0.35/0.0 100.0/0.0 DI-Y 0.35/0.0 100.0/0.0 DI-Z 0.35/0.0 100.0/0.0

• • • • • • • • • • • • MATERIAL PROPERTIES ***********************

• ASTM A-106 Grade B MATH CD-106 EX-0 TY-1 *C-Si MATD TE-70 EH-29.5 EX-0 SM-20.0 SY-35.0 MATD TE-100 EH-29.3 EX-0.21 SM-20.0 SY-35.0 MATD TE-200 EH=28.8 EX-0.95 SM-20.0 SY-31.9 MATD TE-300 EH-28.3 EX-1.77 SM-20.0 SY-31 MATD TE-400 ERN27.7 EX-2.67 SM=20.0 SYg30 MATD TE-500 EH-27.3 EX-3.64 SM-18.9 SY-28.3 MATD TE-600 EH=26.7 EX-4.63 SN-17.3 SY-25.9

• GROUP l NATL CD-106

• ' iRevision l~ A lFile No. HC-04Q-313 lPage, A2 of A13

DESN TE-70. PR-0 OPER TE-70 PR-0 CA-1 CROS CD-26 OD=26 VIT-1.158 MA=332.752 COOR PT-450 AX-12.3637 AY-170.1250 AZ-4.0172 ANCH PT-450 TA-1 LV-1 TANG PT-454 DX-1.7832 DZ-O .5794

• • • PR-72 ***

CROS CD-26 WT-1.39 MA-390

.TANG PT-455 DX-2.0607 DZ-O.6696 AL-$PR-72$

BRAD PT-456 RA-2.167 TANP DY--2.167

• • • PR-64 TANG PT-457 DY--8.0416 AL-$PR-64-GAP 12$

CROS CD-26 IT-1.158 MA-332.752 TANG PT-459 DY--5.250 LUMP PT-459 MA-0.927 TANG PT-460 DY--17.417 BRAD PT-46OF RA-10.8333 TANG PT-SB2 DX-4.8112 DY--8.3333 TANG PT-SB1 DX-.1924 DY--.3333

• • • PR-40 ***

TANG PT-463 DX-0.5292 DY--0.9166 AL-$PR-40-GAP 12$

TANG PT-465 DX-2.3726 DY--4.1250 BRAD PT-465B RA-3.25

• • • PR-44 ***

TANG PT-Z44 DZ--3.9739 AL-$PR-44-GAP 12$

TANG PT-SB7 DZ--1.000 TANG PT-468 DZ--1.1342 BRAD PT-469 RA-0.75 ***REDUCED TO AVOID ERROR MESSAGE TANG PT-4 70 DX--.0588 DZ--0.8404 TANG PT-472 DX--.0735 DZ--1.0508 BRAD PT-473 PA-1.0 ***REDUCED TO WOID ERROR MESSAGE TANG PT-SB4 DX--.1648 D2 --1.0404 *SB4 TANG PT-478 DX--.0823 DZ--.5199 TANG PT-480 DX--.1049 DZ--.5158 TANG PT-485 DX--.1660 DZ--.7567 TANG PT-488 DX--.8159 DZ--3.4395 BRAD PT-489 RA-3.0 ***REDUCED TO AVOID ERROR MESSAGE TANG PT-490 DX--1.7679 DZ--3.0614 TANG PT-493 DX--.7906 DZ--1.3694 BRAD PT-494 RA-1.0 ***REDUCED TO WOID ERROR MESSAGE TANG PT-495 DX--. 9626 DZ--1.2545 TANG PT-498 DX--.9626 DZ--1.2545 BRAD PT-499 RA-1.0 ***REDUCED TO AVOID ERROR MESSAGE TANG PT-500 DX--1.1181 DZ--1 .1181 TANG PT-501 DX--.9338 DZ--.9338 BRAD PT-502 RA-1.0 ***REDUCED TO WOID ERROR MESSAGE TANG PT-SB8 DX--1.0302 DZ--.8263 TANG PT-503 DX--.6873 DZ--.5513 BRAD PT-503B RA-1.0 ***REDUCED TO AVOID ERROR MESSAGE TANG PT-504 DX--.7257 DZ--.4997

• • • PR-48 TANG PT-505 DX--.8922 DZ--.6144 AL-SPR-48-GAP 12$

CROS CD-26 WT-1.39 MA-390 TANG PT-506 DX--1.7845 DZ--1.2288

-BRAD PT-506B--RA-2-:167 ----

TANG PT-510 DY--2.1667

• • • PR-52 ***

CROS CD-26 WT-1.158 MA-332.752 TANG PT-511 DY--.333 AL-$PR-52-GAP 2$

TANG PT-512 DY-1.5833 TANG PT-513 DY--2.85E3 TANG PT-514 DY--1.3083 CROS CD-26 MA-601.5 KL-1 TANG PT-515 DY--2.0492

• • • PR-56 ***

TANG PT-516 DY--1.9092 AL-$PR-56-GAP 2$

§lRevision A .1 File No. HC-04Q-313 Page A3 of A13

TANG PT-517 DY--1.6250 CROS CD-26 MA-332.752 TANG PT-518 DY--0.5

• • • BPR-60 ***

CROS CD-26 WT'1.39 MA-390 BEND PT-520 Yl--2.167 Z2--2.167 *521 CROS CD-26 WT-1.158 MA-332.752 TANG PT-522 DZ--.4115 TANG PT-524 DZ--.2448 TA-1 LUMP PT-524 NA-1.92575 CROS CD-26 WT-2.316 MA-24.5 KL-1 TANG PT-526 DZ--.5833 TANG PT-528 DZ'-2.0417 LUMP PT-528 MA-3.8515 TANG PT-530 DZ--.9583 JUNC PT-530 CROS CD-26 MA-0 RIGD PT-534 DX--2.6867 DY-3.2019 DZ-4.1798 LUMP PT-534 MA-4.597 JUNC PT-530 CROS CD-26 MA-24.756 KL-1 TANG PT-535 DZ--1.6667 TA-1 LUMP PT-535 MA-1.92575 CROS CD-26 WT-1.158 MA-332.752 KL-1 TANG PT-540 DZ--16.979 ANCH PT-540 LV-1

• • • LINE P

• GROUP 2 JUNC PT-470 CROS CD-8 OD-8.625 WT-0.906 MA-85.05 BRAN PT-550 DY-1.333 TE-4 TANG PT-551 DY-0.6667 *ADD-136, LUMP PT-551 MA-0.136 CROS CD-6 OD-6.625 WT-1.436 MA-10.175 KL-1 TANG PT-552 DY-0.5833 TA-1 *ADD-137, LUMP PT-552 MA-0.137 CROS CD-6 MA-6.75 KL-1 TANG PT-554 DY-1.2813 *ADD-679, LUMP PT-554 MA-0.679 *SNUB REDUCTION WT JUNC PT-554 CROS CD-6 MA-0 RIGD PT-558 DX--1.1223 DY-.5625 DZ-0.0785 *ADD-421,LBS/FT-0, LUMP PT-558 MA-0.421 JUNC PT-554 CROS CD-10 OD-10.75 IT-0.73 MA-0 KL-1 TANG PT-560 DX-0.8625 DZ--0.0603 LUMP PT-560 MA-0.047 *SNUB REDUCTION WT CROS CD-10 MA-0 KL-1 TANG PT-562 DX-0.3845 DZ--0.0269 *SIF-1.900,CLASS-2,ADD-47, LUMP PT-562 MA-0.047 INDI AT-562 C2-1.9 K2-2.0 CROS CD-10 MA-40.48 WT-0.365 TANG PT-563 DX-0.2805 DZ--0.0196 TANG PT-565 DX-0.8313 DZ--0.0581 *lJOINT-BTWELD BRAD PT=565B RA-1.25

.TANG-PT-570--DX-3.7553---DY--2--1250 DZ-lr4995--*-lJOINT-BTWELD-BRAD PT-570B RA-1.25 TANG PT-573 DY--1.25 TANG PT-571 DY--1.7344 LUMP PT-571 MA-0.543

• SNUB PT-571 DY-1.0 SP-2121.4 SNUB RED TANG PT-574 DY--2.125 TANG PT-74S DY--0.8333 *ADDi176.5,

• LUMP PT-74S MA-0.1765 **IF THERE IS NO SUPPORT, THERE IS NO CLAMP!

• SNUB PT74S DX-0.3894 DZ-0.9211 SP-1060.7 TANG PT-575 DY--1.5208 *JOINT-BTWELD BRAD PT-575B RA-1.25 I

Revision A File No. HC-04Q-313 Page A4 of A13

TANG PT-580 DX-. 9547 DY--.0208 DZ-1.4914 *JOINT-BTWELD BRAD PT-580B RA-1.25 TANG PT-583 DX--2.3150 DZ-10.5511 LUMP PT-583 MA-0.02 TANG PT-585 DX--.3215 DZ-1.4651 *JOINT-BTWELD BRAD PT-585B RA-1.25 TANG PT-587 DX--1.8670 DY--1.9114 DZ--0.4096 LUMP PT-587 MA-0.1765 TANG PT-590 DX-2.1044 DY--2.1545 DZ--0.4617 *JOINT-BTWELD BRAD PT-590B RA-1.25 TANG PT-2P DY--2.3490 *JOINT-BTWELD TANG PT-4P DY--.7083 *TEE-WTEE JUNC PT-4P BRAN PT-6P DX--.3542 DZ-.6134 TE-1 *JOINT-BTWELD BEND PT-10P Xl--.4167 Zl-.7217 Y2-0.8333 CRED PT-12P DY-.5834 AN-30 EW-1 *JOINT-RED CROS CD-6 WT-0.28 MA-18.97 INDI AT-12P C2-1.9 K2-2.0 TANG PT-16P DY-0.3229 LUMP PT-16P MA-0.142

• SNUB PT-16P DX--0.8561 DZ--0.5168 SP-956 CROS CD-6 MA-240 TANG PT-18P DY-1.6667 JUNC PT-4P CROS CDl10 WT-0.365 MA-40.48 TANG PT-20P DY--.7083 *JOINT-BTWELD TANG PT-24P DY--2.9167 *JOINT-BTWELD TANG PT-26P DY--.7083 *TEE-WTEE JUNC PT-26P BRAN PT-28P DX--.3542 DZ-.6134 TE-1

• JOINT-BTWELD, BEND PT-30P Xl--.4167 Zl-.7217 Y2-.8333 *JOINT-BTWELD, CRED PT-34P DY-.5834 AN-30 *JOINT-RED CROS CD-6 VIT-0.28 MA-18.97 INDI AT-34P C2-1.9 K2-2.0 TANG PT-38P DY-0.3229 LUMP PT-38P MA-0.142

• SNUB PT-38P DX--0.5205 DZ-0.8539 SP-1060.7 CROS CD-6 MA-240 TANG PT-40P DY-1.6667 JUNC PT-26P CROS CD-10 WT-0.365 MA-40.48 TANG PT-42P DY--.7083 KL-1 *JOINT-BTWELD TANG PT-594 DY--0.5 LUMP PT-594 MA-0.545

• SNUB PT-594 DY-1.0 SP-2121.4 TANG PT-22P DY--1.2917 LUMP PT-22P MA-0.1584

• SNUB PT-22P DX--0.8805 DZ--0.4741 SP-1060.7 TANG PT-44P DY--0.4167 TANG PT-595 DY--1.4479 LUMP PT-595 MA-0.090 TANG PT-596 DY--4.9792 *JOINT-BTWELD BRAD PT-596B RA-1.25 TANG PT-597 DX--1.7885 DZ-3.081 BRAD PT-597B RA-4.167

-LUMP -PT=597B -MA=01765 -

TANG PT-2S DX--1.0836 DZ-0.9992 TANG PT-600 DX--1.1193 DZ-1.0875 *JOINT-BTWELD BRAD PT-600B RA-1.25 TANG PT-602 DY--1.5052

• LUMP PT-602 MA-0.1584

• SNUB PT-602 DX--0.9511 DZ-0.3090 SP-870.2 SNUB RED TANG PT-605 DY--1.4948 *JOINT'BTWELD BRAD PT-605B RA-1.25 TANG PT-606 DX--7.6605 DZ-3.1731 LUMP PT-606 MA=0.1765 TANG PT-608 DX--0.9624 DZ-0.3986 9 Revision A File No. HC-04Q-313 Page AS of A13

• LUMP PT-608 MA-0.1765

• SNUB PT-608 DX-.3827 DZ-.9239 SP-1060.7 SNUB RED TANG PT-8S DX--0.7314 DZ-0.3030 LUMP PT-8S MA-0.020 TANG PT-615 DX--1.9632 DZ-0.0130 *JOINT-BTWELD BRAD PT-620B RA-0.8333 TANG PT-620 DX-.2579 DY--.5062 DZ-.6225 *JOINT=BTWELD CROS CD-10 WT-0.594 MA-64.33 TANG PT-622 DX-0.1528 DY--0.3011 DZ-0.3688 TANG PT-623 DX-0.1432 DY--0.2823 DZ-0.3457 TANG PT-624 DX-3.5164 DY--6.9322 DZ-8.4893 *1SIF-1.957 INDI AT-624 C2-1.957 K2'2.0 TANG PT-626 DX-1.8529 DY--2.134 DZ-4.4733 ANCH PT-626 LO-1 LV-2 RX-0.001 KY-409.1 KZ-452.9 MX-8.33E-5 MY-8.33E-5 MZ-8.33E-5 TANG PT-630 DX-3.6003 DY--4.1462 DZ-8.6920 *JOINT-BTWELD,SEG=2 BRAD PT=630B RA-1.25 TANG PT-631 DX--2.0787 DZ-0.8610 *1 SIF-1.365 INDI AT-6631 C2-1.365 K2-2.0 CROS CD-10 WT-1.125 MA-125.25 TANG PT-632 DX--0.7699 DZ-0.3189 *SIF'2.10, INDI AT-632 C2-2.1 R2-2.0 ANCH PT-632 LO-1 LV-2 KX-1212.8 RYY-1045.3 KZ-2519.2 MX-62101 MY-44513 MZ-28607 t LINE K

• GROUP 3 JUNC PT-4B0 CROS CD-8 OD-8.625 WT-0.906 MA-85.05 BRAN PT-650 DY-1.333 TE-4 TANG PT-651 DY-0.6667 LUMP PT-651 MA-0.136 CROS CD-6 OD-6.625 WT-1.436 MA-10.175 TANG PT-652 DY-0.5833 LUMP PT-652 MA-0.137 CROS CD-6 MA-6.75 TANG PT-654 DY-1.2813 LUMP PT-654 MA-0.679 JUNC PT-654 CROS CD-6 MA-0 YL-1 RIGD PT-658 DX--1.0669 DY-0.5625 DZ--.3570 LUMP PT-658 MA-0.421 CROS CD-10 OD-10.75 WT-0.73 MA-0 KL-1 JUNC PT-654 TANG PT-660 DX-0.8199 DZ-0.2743 LUMP PT-660 MA-0.047 TANG PT-662 DX-0.3655 DZ-0.1223 *SIF-1.900,CLASS-2 LUMP PT-662 MA-0.047 INDI AT-662 C2-1.9 K2-2.0 CROS CD-10 WT-0.365 MA-40.4B TANG PT-663 DX-.2568 DY--.007 DZ-.0859 TANG PT-665 DX-0.7606 DY--0.0143 DZ-0.2545 BRAD PT-665B RA-1.25 TANG PT-670 DX-.8939 DY--.0208 DZ-1.6953 BRAD PT-670B RA-1.25 TANG PT-675 DX-2.7668 DY--2.1058 DZ--.2965 BRAD-.PT-675B.RA-i.25 .

TANG PT-674 DY--1 TANG PT-677 DY--.2188 LUMP PT-677 MA-0.01 TANG PT=678 DY--5.792

• LUMP PT-678 MA-0.1765

• SNUB PT-678 DX--.9063 DZ--.4226 SP-1060.7 SNUB RED

• RAD 678 -0.9603 -0.4226 *I TANG PT-67S DY--0.625 TANG PT-680 DY--1.6146 BRAD PT-680B RA-1.25 TANG PT-676 DX-1.4574 DZ-1.2205 t Revision A File No. HC-04Q-313 Page A6 of A13

• LUMP PT-676 MA-0.1765

• SNUB PT-676 DY-1.0 SP911.1 SNUB RED

• RAD 676 1.0 *1 TANG PT-685 DX-0.8824 DZ-0.7390 BRAD PT-685B RA-1.25 TANG PT-682 DX-0.0045 DZ-0.7083 LUMP PT-682 MA-0.02 TANG PT-690 DX-0.0248 DZ-3.8716 BRAD PT-690B RA-0.8333 TANG PT-692 DY--1.1094

• LUMP PT-692 MA-0.1584

• SNUB PT-692 DX-1 SP-956 SNUBBER REDUCTION

• RAD 692 1 *I TANG PT-695 DY--0.7969 BRAD PT-695B RA-1.25 TANG PT-700 DX--1.6867 DY--3.2114 DZ-2.7328 BRAD PT-700B RA-1.25 TANG PT-703 DX--1.9614 DZ-3.1778 LUMP PT-703 MA-0.1765

• SNUB PT-703 DX--0.8223 DY--0.2615 DZ--0.5053 SP-956 TANG PT-705 DX--1.0094 DZ-1.6354 BRAD PT-705B RA-1.25 TANG PT-2K DY--1.25 TANG PT-4K DY--.7083 *TEE-WTEE JUNC PT-4K BRAN PT-6R DX--.5009 DZ-.5009 TE-1 *JOINT-BTWELD TANG PT-8K DX--.5892 DZ-.5892 *8K BRAD PT-10K RA-0.8333 *JOINT-BTWELD, TANP DY-.8333 *JOINT-BTWELD,10K CRED PT-12K DY-.5834 AN-30 *JOINT-RED, CROS CD-6 OD-6.625 WT-0.28 MA-18.97 INDI AT-12K C2-1.9 K2-2.0 TANG PT-16K DY-0.3229 LUMP PT-16K MA-0.142 **ASSUME THIS IS FOR ONE CLAMP

• SNUB PT-16K DX--0.0656 DZ--0.9978 SP-1060.7 SNUB RED

• SNUB PT-16K DX--0.8531 DZ--0.5218 SP-1060.7 CROS CD-6 MAt240 TANG PT-18K DY-1.6667 JUNC PT-4K CROS CD-10 OD-10.75 WT-0.365 MA-40.48 KL-1 TANG PT-20K DY--.7083 TANG PT-22K DY--0.4167 LUMP PT-22K MA-0.1233

• SNUB PT-22K DX--0.9614 DY-0.0587 DZ--0.2675 SP-1060.7 TANG PT-2KS DY--0.75 LUMP PT-2KS MA-0.272

• SNUB PT-2KS DY-1 SP-1912 TANG PT-24K DY--.5 *JOINT-BTWELD TANG PT-26K DY--.7083 *TEE-WTEE JUNC PT-26K BRAN PT-28K DX-0.207 DZ-0.6774 TE-1 *JOINT-BTWELD TANG PT-30K DX=0.2436 DZ-0.7969 *30K BRAD PT-32R RA-0.8333 *JOINT-BTWELD, TANP DY-.8333 *JOINT-BTWELD,32K CRED PT-34K DY-.5834 AN-30 *JOINT-RED, INDI AT-34K C2-1.9 K2-2.0 TANG PT-38K DY-0.3229 LUMP PT-38K MA-0.142 CROS CD-6 MA-240 TANG PT-40K DY-1.6667 JUNC PT-26K CROS CD-10 WT-0.365 MA-40.48 TANG PT-42K DY--1.9583 *JOINTBTWELD BRAD PT-710 RA-1.25 TANG PT-712 DX-0.1665 DZ--1.4278 LUMP PT-712 MA=0.02 3 Revision A File No. HC-04Q-313 Page A7 of A13

DZ-J.5747 TANG PT-715 DX-0.4168 DZ--3.5747 BRAD PT-715B RA-1.25 *BTWELD TANG PT-716 DY'-1. 6458 LUMP PT-716 MA=0.07

• SNUB PT-716 DY-1.0 SP-492 TANG PT-718 DY--0. 6875 LUMP PT-718 MA-0.1765 SNUB PT-718 DX-0.6852 DZ--0.7284 SP-1060.7 TANG PT-71S DY--.6958 TANG PT-720 DY--2.078 BRAD IPT-720B RA-1.25 TANG IPT-725 DX--2.3920 DY--1.8062 DZ-0.7872

• LUMP PT-725 MA-0.1765

• SNUB PT-725 DX--0.3126 DZ--0.950 S1P-1005.6 SNUB RED TANG IPT-721 DX--0.9166 DY--0.6921 DZ-0.3017 LUMP IPT-721 MA-0.450 TANG :PT-730 DX--2.5086 DY--1.8942 DZ-0.8256 BRAD :PT-735B RA-1.25 TANG :PT-735 DX-1.07 DY--0.87 DZ-0.44 *JOINT-BTWELD, CROS ICD-10 WT-0.594 MA-64.33 TANG PT-737 DX-0.3687 DY--0.3011 DZ-0.1527 TANG PT-738 DX-0.3457 DY--0.2823 DZ-0.1432 TANG PT-740 DX-8.4894 DY--6.9321 DZ-3.5164 *ISIF-1 .957,SEG=2, INDI ;AT-740 C2-1.957 K2-2.0 TANG PT-742 DX-4.4737 DY--2.134 DZ-1.8531 *1 ANCH PT-742 LO-1 LV-2 KX-0.001 RY-409.1 KZ-452.9 MX-8.33E-5 MY-8.33E-5 MZ-8.33E-5 TANG PT-745 DX-8.69200 DY--4.1472 DZ-3.6003 BRAD PT-746B RA-1.25 *1JOINT-BTWELD, TANG PT-746 DX-0.4784 DZ--1.1549 *1 SIF-1.365, INDI AT-746B C2-1.365 K2-2.0 CROS CD-10 WT-1.125 MA-115.25 TANG PT-747 DX-0.3189 DZ--0.7699 *SIF-2.1, INDI AT-747 C2-2.1 K2-2.0 ANCH PT-747 LO-l LV-2 KX-1211.8 rY-1045.3 KZ-251.9 MX-62101 MY-44512.8 MZ-28607

• • • LINE B

• GROUP 4 JUNC PT-490 CROS CD-8 WT-0.906 MA-85.05 BRAN PT-760 DY-1.333 TE-4 *CLASS-1, TANG PT-761 DY-0.6667 LUMP PT-761 MA-0.136 CROS CD-6 WT-1.436 MA-10.175 TANG PT-762 DY-0.5833 LUMP PT-762 MA-0.137 CROS CD-6 MA-6.75 TANG PT-764 DY-1.2813 LUMP PT-764 MA-0.679 JUNC PT-764 CROS CD-6 MA-D KL-1 RIGD PT-768 DY-0.5625 DZ--1.1250 LUMP PT-768 MA-0.421 JUNC PT-764 CROS CD=l0 WT-0.73 MA-0 KL-1 LUMP PT-770 MA-0.047 CROS CD-10 MA-0 KL=1 TANG PT-772 DZ-0.3854 *SIF-1.900,CLASS-2 LUMP PT-772 MA-0.047 INDI AT-772 C2-1.9 K2-2.0 CROS CD-10 WT-0.365 MA-40.48 TANG PT-773 DZ-5.1146 LUMP PT-773 MA-0.01 TANG PT.-775 DZ-1.6875 BRAD PT-775B RA-1.25 *JOINT-BTWELD TANG PT-776 DY--0.6602 DZ-0.9365 *1 Revision I A l I l File No. HC-04Q-313 Page A8 of A13

TANG PT-780 DY--1.4544 DZ--2.0635 BRAD PT-780B RA-1.25 *lJOINT-BTWELD, TANG PT-781 DY--1.0625 LUMP PT-781 MA-0.345 TANG PT-782 DY--1.6575 LUMP PT-782 MA-0.1765

• SNUB PT-782 DX--0.4035 D2)Z-0.9150 SP-1060 .7 TANG PT-783 DY--0.5

• LUMP PT-783 MA-0.1765

• SNUB PT-783 DX--0.9063 D:Z--0.4226 SP=1060.7 SNUBBER REDUCTION

• RAD 783 -0.9063 -0.4226 *1 TANG PT-785 DY--3.0521 BRAD PT-78SB RA-1.25 *BTWELD, TANG PT-790 DX--1.7494 DZ--- 1.7494 BRAD PT-790B RA-0.8333 *JOINT-BTWELD, TANG PT-792 DY--3.25 LUMP PT-792 MA-0.1758 TANG PT-794 DY--7.1042 LUMP PT-794 MA-0.1765

• SNUB PT-794 DX-0.9956 DZ--0.0935 SP-1060.7 TANG PT-795 DY--6.0 BRAD PT-795B RA-1.25 *JOINT-BTWELD, TANG PT-796 DX-1.8542 LUMP PT-796 MA-0.1765

• SNUB PT-796 DY--0.9724 DZ-0.2334 SP-1060.7 TANG PT-800 DX-3.2292 BRAD PT-800B PA-1.25 *JOINT-BTWELD, TANG PT-801 DZ-2.1667 LUMP PT-801 MA-0.1765

• SNUB PT-801 DX--0.9976 DY--0.0698 SP-956 TANG PT-802 DZ-1.09375 LUMP PT-802 MA-0.447

• SNUB PT-802 DZ-1 SP-2121.4 TANG PT-803 DZ-1.1146 LUMP PT-803 MA-0.1765

• SNUB PT-803 DY-1.0 SP-956 TANG PT-2B DZ-1.0938 *JOINT-BTWELD, TANG PT-4B rDz-0.7083 *TEE-WTEE, JUNC PT-4B CROS CD-6 OD-6.625 WT-0.28 MA-18.97 BRAN PT-6B DY-.6354 TE-1 *SIF-1.9, INDI AT-6B C2-1.9 K2-2.0 CROS CD-6 WT-0.5 MA-0 KL-1 TANG PT-BB DY-0.3229 LUMP PT-BB MA-0.041 CROS CD-6 MA-240 TANG PT-1OB DY-1.6667 JUNC PT-4B CROS CD-10 OD-10.75 WT-0.365 MA-40.48 TANG PT-12B DZ-.7083 *JOINT7BTWELD TANG PT-14B DZ-.7083 *TEE-WTEE, JUNC PT-14B CROS CD-6 OD-6.625 WT-0.28 MA-18.97 BRAN PT=16B DY-.6354 TE-1 *SIF-l.9, INDI AT-16B C2-1.9 K2-2.0

• CROS-CD6-6-WT-0.5- MA-0-L--

TANG PT-18B DY-0.3229 LUMP PT-IBB MA-0.041 CROS CD-6 MA-240 TANG PT-20B DY'1.6667 JUNC PT-14B CROS CD=10 OD=10.75 WT-0.365 MA-40.48 TANG PT-22B DZ-.7083 *JOINT'BTWELD TANG PT-805 DZ-1.375 LUMP PT'805 MA-0.02 TANG PT-804 DZ-1.625 BRAD PT-804B RA-1.25 *JOINT-BTWELD,

, Revision l A I I File No. HC-04Q-313 PIage A9 of A13

TANG PT-806 DY--3.3646 BRAD PT-806B RA-1.25 TANG PT-808 DX--1.9389 DY--2.1216 DZ-0.4964

• LUMP PT-808 MA-0.1765

• SNUB PT-808 DX-0.1750 DY--0.3947 DZ--0.90:10 SP-1005.6 SNUB REDUCTION TANG PT-810 DX--0.4016 DY--0.4395 DZ-0.1028 LUMP PT-810 MA-0.1765 TANG PT-814 DX--1.4819 DY'-1.6215 DZ-0.3794 BRAD PT-814B RA-1.25 TANG PT-812 DX-1.3642 DY--1.1127 DZ-0.5651 LUMP PT-812 MA-0.1765 TANG PT-820 DX-0.6033 DY--0.4921 DZ-0.2499 *JOINT'BTWELD CROS CD-10 WT-0.594 MA-64.33 TANG PT-822 DX-0.3688 DY--0.3011 DZ-0.1528

• RAD 822 .5560 .7986 .2303 *B

• RAD 822 -.3827 .9239 *B TANG PT-824 DX-0.3457 DY--0.2823 DZ-0.1432 *1 TANG PT-825 DX-8.4893 DY--6.9322 DZ-3.5164 *lSIF-1.957,SEG-2, INDI AT-825 C2-1.957 R2-2.0 TANG PT-826 DX-4.4737 DY--2.1340 DZ-1.8531 *1 ANCH PT-826 LO-1 LV-2 KX-0.001 KY-409.1 KZ-452.9 MX-8.33E-5 MY-8.33E-5 MZ-8.33E-5 TANG PT-828 DX-8.6920 DY--4.1472 DZ-3.6003 BRAD PT-829B RA-1.25 *lJOINT-BTWELD,SEG-2, TANG PT-829 DX--0.4784 DZ-1.15i49 *1 SIF-1.365 INDI AT-829B C2-1.365 R2-2.0 CROS CD-10 WT-1.125 MA-115.25 TANG PT-830 DX--0.3189 DZ-0.7699 *1SIF-2 .1 ANCH PT-830 LO-1 LV-2 KX-1211.8 KY-1045.3 KZ-2519.2 MX-62101 MY-44513.3 MZ-28607.4 JUNC PT-495 CROS CD-8 WT-0.906 MA-85.05 BRAN PT-832 DY-1.33 TE-4 *CLASS-1 TANG PT-835 DY-0.6667 CROS CD-6 WT-1.436 MA-10.175 TANG PT-839 DY-.5833 LUMP PT-839 MA-0.434

• • • LINE F

• GROUP 5 CROS CD-8 WT-0.906 MA-85.05 JUNC PT-500 BRAN PT-845 DY-1.33 TE-4 *CLASS-1 TANG PT-B46 DY-0.6667 LUMP PT-846 MA-0.136 CROS CD-6 WT-1.436 MA-10.175 TANG PT-847 DY-0.5833 LUMP PT-847 MA-0.137 CROS CD-6 MA-6.75 KL-1 TANG PT-848 DY-1.2813 LUMP PT-848 MA-0.679 KL-1 JUNC PT-848 CROS CD-6 MA-0 KL-1 RIGD PT-850 DX--0.7955 DY-0.5625 DZ-0.7955 LUMP PT-850 MA-0.421 JUNC PT-848

--CROS--CD-10-WT-0.73MA0R-TANG PT-851 DX-0.6114 DZ=-0.6114 LUMP PT-851 MA-0.047 TANG PT-852 DX-0.2725 DZ--0.2725 *SIF-1.900,CLASS=2 LUMP.PT-852 MA-0.047 INDI AT-852 C2-1.9 R2-2.0 CROS CD-10 WT-0.365 MA-40.48 TANG PT-854 DX-1.2301 DY--0.0187 DZ--1.2301 BRAD PT-854B RA-1.25 *IJOINT-BTWELD TANG PT=855 DX-2.6515 DY--0.0417 DZ-2.6515 BRAD PT-855B RA-1.25 *1JOINT=BTWELD TANG PT-85B DY--1.5 Revision A j File No. HC-04Q-313 Page A10 of A13

LUMP PT-85B MA'0.01 TANG PT-856 DY--0.4583 LUMP PT-856 t4A-0.020 *ESTIMATED WEIGHII FOR SPRING ONLY

• RAD 856 1.0 *l TANG PT-853 DY--3.75 TANG PT-857 DY--2.432 LUMP PT-857 MA-0.1584

• SNUB PT-857 DXG0.9892 DZ--0.1464 SP-1060.7 TANG PT=858 DY--0.4635

• LUMP PT-858 MA'0.1233

• SNUB PT-858 DX-0.0523 DZ-0.9986 SP-1060.7 *SNUB RED

• RAD 858 0.0523 0.9986 *I TANG PT-85A DY--0.7135 LUMP PT-85A MA-0.330

• RAD 85A 1.0 TANG PT-859 DY--1.8385 BRAD PT-859B RA-1.25 *JOINT-BTIrWELD TANG PT-860 DX-2.1710 DY--0.1146 IDZ-10. 5280 BRAD PT-860B RA-0.8333 *JOINT-BF3TWELD,SEG-2, TANG PT.1F DY--1.25 LUMP PT-1F MA-0.020 **SPRING CLAMP 0 NLY

• RAD 01F 1.0 TANG PT=2F DY--0.2604 *JOINT-BTWELD, TANG PT-4F DY--.7396 *TEE-WTEE, JUNC PT-4F BRAN PT-6F DZ-.7083 TE-1 *JOINT-BTWELD, BEND PT-10F ZI-0.833 Y2-0.833 *JOINT-BTWELD, CRED PT-12F DY-.5834 AN-30 *JOINT-RED, CROS CD-6 WT-0.28 MA-18.97 *SIF-1.9 INDI AT-12F C2-1.9 K2-2.0 TANG PT-16F DY-0.3229 LUMP PT-16F MA-0.142

• SNUB PT-16F DX--0.7826 DZ-0.6225 SP-956 SNUB RED

• SNVB PT-16F DX-0.6246 DZ-0.7810 SP-1060.7 CROS CD-6 MA-240 TANG PT-18F DY-1.6667 CROS CD-10 WT-0.365 MA-40.48 JUNC PT-4F TANG PT-20F DY--.7083 *JOINT-BTWELD TANG PT-22F DY--3.500 *JOINT-BTWELD, TANG PT-24F DY--.7083 *TEE-WTEE, JUNC PT-24F BRAN PT-26F DDZ-.7083 TE-1 *JOINT-BTWELD, BEND PT-30F Z1-0.833 Y2-0.833 *JOINT-BTWELD, CRED PT-32F DY-.5834 AN-30 *JOINT=RED, CROS CD-6 WT-0.28 MA-18.97 RL-1 INDI AT-32F C2-1.9 K2-2.0 TANG PT-36F DY-0.3229 LUMP PT-36F MA-0.142

• SNUB PT-36F DX--0.8174 DZ-0.5761 SP-956 SNUB REDUCTION

• SNUB PT-36F DX-0.6973 DZ-0.7168 SP-1060.7 CROS CD-6 MA-240 TANG PT-38F DY-1.6667 JUNC PT-24F CROS CD-10 WT.=0.365 ]MA-40.48 TANG PT-40F------- .7083 *JOIT=BTWELD TANG PT-863 DY--4.3855 LUMP PT-863 MA-0. 590

• SNUB PT-863 DY-1.0 SP-2121.4 TANG PT-865 DY--5.302 LUMP PT-865 MA-0.1233

• SNUB PT-865 DX--0.3706 DZ--0.9288 SP-1060.7 TANG PT-868 DY--1.5 BRAD PT-868B RA-1.25 *JOINT-BTWELD, TANG PT-869 DX--0.7826 DZ--1.5594

• LUMP PT-869 MA-0.1765

• SNUB PT-869 DX-0.8630 DY-0.2620 DZ--0.4330 SP-1005.6 *SNUBBER REDUCTION I

TANG PT-870 DX'-1.3059 DZ--2.6022 BRAD PT-870B RA-1.25 *JOINT.BTWELD TANG PT-885 DY--3.2917 BRAD PT'890 RA-1.25 *JOINT-BTWELD TANP DX-0.4612 DY-0.3750 DZ--0.1910 *liJOINT-BTWELD CROS CD-10 WT-0.594 MA-64.33 TANG PT-892 DX-0.3688 DY'-0.3011 DZ--0.1528 *1.LTH1-0.594,

• RAD 892 .5560 .7986 -.2303

• RAD 892 .3827 .9239 TANG PT=893 DX-0.3457 DY-0.2823 DZ--0.1432 *1 TANG PT-895 DX-8.4894 DY-6.9322 DZ--3.5164 *lSIF.-1.957, SEG-2, INDI AT-895 C2-1.957 K2-2.0 TANG PT-897 DX-4.4733 DY--2.1349 DZ--1.8529 ANCH PT-897 LO-1 LV-2 KX-0.001 XY-409.1 KZ-452.9 MX-8.3E-5 MY-8.3E-5 MZ-8.3E-5 TANG PT-900 DX-8.6920 DY--4.1462 DZ--3.6003 BRAD PT-902 RA-1.25 TANG PT-903 DX--0.4784 DZ--1.1549 *I,SIF..1.365 INDI AT-902 C2-1.365 K2-2.0 CROS CD-10 WT-1.125 MA-115.25 TANG PT-905 DX--0.3189 DZ--0.7699 *1SIF2.12 INDI AT-905 C2-2.1 K2-2.0 ANCH PT-905 LO-1 LV-2 KX-1211.8 KY-1045.3 KZ-2519.2 MX-62101 MY-44513 MZ-28607.4

• • • • SUPPORTS****

SNUB PT-SB2 DX--0.8580 DY-- 0.4565 DZ-0.2355 SP-800. LV-1 SNUB PT-SB1 DX--0.7194 DY --0.3152 DZ--0.6166 SP-800. LV-1 SNUB PT-SB7 DX--.3645 DY -.9312 SP-600. LV-1 SNUB PT-SB4 DX-.9877 DZ--.1564 SP-800. LV-1 SNUB PT-SBB D Y-1.0 SP-600. LV-1 RSTN PT-511 DX-1.0 SP-1894 LV-1 RSTN PT-512 DX-0.2385 DZ--0.9711 SP-1862 LV-1 RSTN PT-516 DX-1.0 SP-1767 LV-1 VSUP PT-571 DY-1.0 SP-0.600 FO-1.421 LV-2 VSUP PT-583 DY-1.0 SP-0.224 FO-0.532 LV-2 *E RSTN PT-587 DX--0.2143 DZ-0.9768 LV-2 *SNUBBER REDUCTION RSTN PT-16P DX--0.8561 DZ--0.5168 LV-2 *SNUBBER REDUCTION RSTN PT-38P DX--0.5205 DZ--0.8539 LV-2 *SNUBBER REDUCTION RSTN PT-594 DDY-1 .0 LV-2 *SNUBBER REDUCTION RSTN PT-22P DX--0.8805 DZ--0.4741 LV-2 *SNUBBER REDUCTION VSUP PT-595 DlY-1 .0 SP-1.360 FO-3.590 LV-2 *E RSTN PT-2S DX--0.6679 DDY-0.1891 DZ--0.7440 LV-2 *SNUBBER REDUCTION RSTN PT-606 DDY-1 LV-2 *SNUBBER REDUCTION VSUP PT-8S DDY-1.0 LV-2 SP-0.520 FO-1.395 *E VSUP PT-682 DIY-1.0 LV-2 SP-0.520 FO-1.460 *E RSTN PT-703 DX--0.8223 DY--0.261!5 DZ--0.5053 LV-2 *SNUBBER REDUCTION RSTN PT-16K DX--0.8531 DZ--0.5218 LV-2 *SNUBBER REDUCTION RSTN PT-22K DX--0.9614 DY-0. 0587 DZ--0.2675 LV-2 *SNUBBER REDUCTION RSTN PT-2KS DY-1 LV-2 *SUBBER REDUCTION RSTN PT-38K DX-0.3907 DZ--0.9205 LV-2 *SNUBBER REDUCTION RSTN PT-38K DX--0.7373 DZ--0.6756 LV-2 *SNUBBER REDUCTION VSUP PT-712 DY-1.0 LV-2 SP-1.600 FO=4.212 RSTN PT-716 DY-1 LV-2 *SNUBBER REDUCTION RSTN PT-718 DX-0.6852 DZ--0.7284 LV-2 *SNUBBER REDUCTION SNUB PT-721 DX-0.7718 DY-0.5828 DZ--0.2540 SP-2121.4 LV-2

-SNUB PPT-781 -DY-1.0-----------P 492--LV-2--------- - -- *--*-.

RSTN PT-782 DX'-0.4035 DZ-0.9150 LV-2 *SNUBBER REDUCTION VSUP PT-792 DY-1.0 LV-2 SP-1.360 FO-3.098 *E RSTN PT-794 DX'0.9956 DZ--0.0935 LV-2 *SNUBBER REDUCTION RSTN PT-796 DY-0.9724 DZ-0. 2334 LV-2 *SNUBBER REDUCTION RSTN PT-801 DX--0.9976 DY--0.0698 LV-2 *SNUBBER REDUCTION RSTN PT-802 DZ-1 LV-2 *SNUBBER REDUCTION RSTN PT-803 DY-1.0 LV-2 *SNUBBER REDUCTION VSUP PT-805 DY-1.0 LV-2 SP-1.200 FO-3.073 *E SNUB PT-810 DX--0.6860 DY-0.5345 DZ--0.4920 LV-2 SP-1060.7 SNUB PT=812 DX=0.7023 DY=0.7274 DZ--0.1798 SP-911.1 LV'2 VSUP PT-856 DY-1.0 SP-0.400 FO-1.682 LV-2 *E Revision I A I I File No. HC-04Q-313 Page A12 of A13

SNUJB PT-85A DY-1.O0 SP-492 LV-2 RSTN PT=857 DX-0.9892 DZ--0.1464 LV-2 *SNUBBER REDUCTION VSUP PTIlF DY-1.O0 SP-1.800 FO-3.962 LV-2 *E RSTN PT-16F DX-0.6246 DZ-0.7810 *SNUBBER REDUCTION LV-2 RSTN PT-36F DX-0.6973 DZ-0.7168 LV-2 *SNUBBER REDUCTION RSTN PT-863 DY-1.O0 LV-2 *SNUBBER REDUCTION RSTN PT=865 DX--0.3706 DZ--0.9288 LV-2 *SNUBBER REDUCTION ENDP