Text

Balance-of-Plant Sys Piping Thermal Expansion Monitoring Program
	ML20203F183
Person / Time
Site:	Grand Gulf
Issue date:	06/16/1986
From:	Davant G, Megan Wright; MISSISSIPPI POWER & LIGHT CO.
To:	;
Shared Package
ML20203F123	List: AECM-86-0216, Forwards Listed Summary Startup Test Repts Not Submitted W/ Summary Startup Test Rept 12 on 860228,including 1C88-ST01, Special Test-Visual Steady-State Vibration Monitoring Program; ML20203F141; ML20203F161; ML20203F183;
References
	1C88-ST05, 1C88-ST5, NUDOCS 8607300120
	Download: ML20203F183 (185)
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{{#Wiki_filter:- ( GRAND GULF NUCLEAR STATION UNIT 1 STARTUP TEST REPORT Test Number: I C88-STOS Test Condition: Heatup through TC-6 Prngram Test

Title:

BOP System Pining Thermai pypo,,an, uggaz Criteria ( ) Satisfied ( x) Level 1 Not Satisfied ( ) Level 2 Not Satisfied BfI S/T b Report Prepared By: D% Date: 8 1"!.L !;.;; L;; Ji;; -/GE @D&A Engineer 4 f24 [86 Results Reviewed By: N-MA) Date: H M ar Test Group Leader n L !L?. 2 ( __

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c MP& startui Supervisor Date: 73 8 GE" Lead ST16A Engine or Date: Results Accepted By: "\\ l/W V(/' 95RC e 0 0607300120 060723 6 ADOCK 0500 PDR l P l

B0P Piping Thermal Expansion IC88-ST05 Page 1 1.0 PURPOSE The purposes of this test were to monitor the thermal expansion of selected plant piping systems throughout the range of power operation; to verify that the piping systems were clear of obstructions which could prevent free thermal movement; and to t ensure that spring hangers and snubbers were functioning properly. These objectives were satisfied by the performance of detailed system walkdowns and the collection of displacement data for comparison to specific criteris. 2.0 ACCEPTANCE CRITERIA 2.1 At no time during the entire thermal cycle (i.e., cold to hot) shall there be any evidence of thermal blocking in the piping systems unless it is intended by design. If pipe blocking occurs, the test should be put on hold pending Nuclear Plant Engineering (MP&L) approval to continue testing. 2.2 ' Spring hanger movement shall remain within the hot and cold l set points, and snubbers shall not become fully extended or retracted. If the spring or snubber limits were exceeded, the I test should be put on hold pending Nuclear Plant Engineering (NP&L) approval to continue testing. 2.3 The measured thermal movements shall be within the specified expected or acceptable limits. The expected thermal boundary limits are based on 10.25 inch or 125 percent of the analytical value, whichever is greater, at 550*F Reactor Pressure Vessel reference temperature, unless otherwise specified. If the measured thermal movements exceed the expected boundary limits, but are within the acceptable boundary limits, the testing may proceed but the data shall be evaluated. If the measured movements exceed the acceptable boundary limits, the test shall be put on hold pending Nuclear Plant Engineering (MP&L) approval to continue testing. 3.0 PLANT CONDITIONS 3.1 Non-Nuclear Heatup (NNH) Testing 3.1.1 First Partial Non-Nuclear Heatup Dates

Sept. 21 thru Sept. 25, 1982 Reactor Power

0 MWt (0%)

Reactor Temp. Range : 100'F through 350'F Reactor flooded above Steamlines, MSIV's closed, Main Steam line drains open to provide steam line warning flow path. 1

BOP Piping Thermal Expansion IC88-ST05 Page 2 3.1.2 Second Heatup Dates

Oct. 13 thru Oct. 23, 1982 Reactor Power

0 MWt (0%)

Reactor Temp. Range

100*F thru 514*F Reactor flooded above steamlines, MSIV's closed, Main Steam line drains open to provide steam line warming flow path.

3.2 NUCLEAR HEATUP (NH) TESTING 3.2.1 Reactor Heatup to Rated Temperature Dates

Sept. 26 thru Oct. 11, 1983 Reactor Power Range

0 thru $191 MWt (0% to $5%)

Reactor Press. Range

0 thru 952 psig Reactor Temp Range

100*F thru 535'F Reactor critical at less than 5% power, with turbine / generator off-line and turbine bypass valves closed.

3.2.2 SRV Actuations at 250 psig (1B21-F047D and F051D) Date

October 3, 1983 Reactor Power

$191 MWt ( i 5%)

Reactor Pressure

248 psig Reactor Temperature

~390*F SRV actuations in accordance with Startup Test 1-B21-SU-26-H 3.2.3 Bypass Valve Operation Date

October 30, 1983 Reactor Power

$191 MWt ( 15%)

Reactor Pressure

962 psig Reactor Temperature

535'F Turbine Bypass Valve Positions

A-5% B-1% C-0%

3.2.4 RCIC Operation Date

November 1, 1983 Reactor Power

$191 MWt ( 15%)

Reactor Pressure

942 psig l

Reactor Temperature

534*F RCIC Flow

800 gym l

l l

BOP Piping Thermal Expansion 1C88-ST05 Page 3 3.3 POWER ASCENSION TESTING 3.3.1 Turbine Warmup Date

October 17, 1984 Reactor Power

C'4 MWt (16.8%)

Reactor Pressure

951 psig Reactor Temperature

507'F Turbine Front Casing Temp. : 298*F 3.3.2 RER Steam Condensing Operation Loop A Loop B Date

Oct. 27, 1984 May 21, 1985 Reactor Power

732 MWt (19.1%) ~3373 MWt (88%)

Reactor Pressure : 951 psig ~1010 psig Reactor Temp.

507*F 522'F

~ 3.3.3 25% Main Steam System Flow Date

November 15, 1984 Reactor Power

950 MWt (24.8%)

Reactor Pressure

956 psig Reactor Temperature

506*F Main Steam Flow

3.6 M1b/hr Feedwater Flow

3.0 M1b/hr Feedwater Temperature

173'F 3.3.4 50% Main Steam System Flow Date

January 2, 1985 Reactor Power

2017 MWt (52.6%)

Reactor Pressure

970 psig Reactor Temperature

517'F Main Steam Flow

8.2 Mlb/hr Feedwater Flow

8.0 Mlb/hr Feedwater Temperature

362'F 3.3.5 SRV Actuations at Rated Pressure (IB21-F047D and F051D)

Date

January 3, 1935 l

Reactor Power

2041 MWt (53.2%)

Reactor Pressure

1000 psig Reactor Temperature

a-520'F SRV actuations in accordance with Startup Test 1-B21-SU-26-2 4

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BOP Piping Thermal Expansion IC88-ST05 Page 4 3.3.6 Main Steam Isolation Valve Leakage Control System Operation Date

January 5, 1985 Reactor Power

0 MWt (0%)

Reactor Pressure

$29 psig Reactor Temperature

--250*F MSIVLC Systems running in accordance with Startup Test 1-000-SU-77-2 3.3.7 75% Main Steam System Flow Date-

April 11, 1985 Reactor Power

2860 MWt (74.6%)

Reactor Pressure

992 psig Reactor Temperature

520*F Main Steam Flow

11.9 Mlb/hr Feedwater Flow

11.8 Mlb/br Feedwater Temperature

389'F 3.3.8 100% Main Steam System Flow Date

May 13, 1985 Reactor Power

3692 MWt (96.3%)

Reactor Pressure

1014 psig Reactor Temperature

525'F Main Steam Flow

16.0 Mlb/hr Feedwater Flow

15.6 M1b/hr Feedwater Temperature

410*F 3.3.9 RHR Shutdown Cooling Operation Loop A Loop B Date

May 18, 1985 May 18, 1985 Reactor Power 0 MWt (0%)

O MWt (0%) Reactor Pressure 147 psig 114 psig Reactor Temperature 349'F 329'F RHR loops in Shutdown Cooling in accordance with Startup Test 1-E12-SU-71-6 with Heat Exchangers partially bypassed Loop A Loop B Date

Oct. 13, 1985 Oct. 13, 1985 l

Reactor Power 0 MWt (0%) O MWt (0%) j Reactor Pressure O psig 0 psig i Reactor Temperature 125'F 146*F RHR loops in Shutdown Cooling in accordance with TSTI 1E12-85-003-0-5 with full RHR flow to Heat Exchangers and reduced SSW cooling flow to minimize cooldown.

BOP Piping Thermal Expansion IC88-ST05 Page 5 4.0 RESULTS I This test consisted of monitoring the thermal expansion of selected MSSS and BOP piping, throughout the Startup Test Program, from Mon-Nuclear Heatup through Full Power Testing. The results of the Non-Nuclear Heatup test phase were provided in an earlier interim test report, IC88-ST05, dated May 1983. Throughout the course of testing, data was collected using the GETARS Transient Recorder data acquisition system. Remote instrumentation consisted of FRA-MAR high tensioned Lanyard Potentiometer displacement transducers and precision 4-wire RTD's with Validyne BA-332 and PT-174 signal conditioning amplifiers, respectively. The lanyard pots were the same instruments used in the piping vibration test program, described in Test Report IC88-ST04. I Pipe displacement data was re:orded and trended during the first four plant heatups, in addition to over 200 separate data readings taken at rated reactor temperature during the test program. Table 4.1 summarizes the critical data collected at various plant operating conditions. For simplicity, data obtained at the intermediate reactor temperatures during the heatups are not provided here. Of the over 200 readings provided in Table 4.1, 51% experienced failures of the Expected Limits, while 24% of all data failed the Acceptable Limits. Additionally, 11% of the readings were judged to have been obtained at too low a system temperature to accurately ascertain acceptance. In addition to Table 4.1, the data is presented graphically in Appendix I with the criteria limits for ready visual comparison. In accordance with the requirements of the Bechtel Test Specification, 9645-M.275-0, criteria failures were referred to MP&L's Nuclear Plant Engineering (NPE) group for resolution. In several cases obstructions were concluded to exist and were actually located in the field. In other cases, engineering evaluations by NPE or Bechtel were performed to verify that no unacceptably high stress levels occurred. By the end of the program, all deficiencies had been satisfactorily resolved or accepted. i

BOP Piping Thsreal Exprn: sics IC88-ST05 PAGE 6 TABLE 4.1 NON-NSSS PIPING THERMAL EXPANSION DATA l l SENSOR l MEASURED DISPLACEMENTS (MILS) l ) l ID l Hax l Max l 25% l 50% l 75% l 100% l Bypass l Turbine l l l NNH NH l Steam Flow Steam Flow Steam Flow Steam Flow Valve OPS Warmup j l Reactor Power (%) 0 55 l 24.8 52.6 74.6 96.3 55 16.8 l l Reactor Temperature (*F)l 1514 1535 l 506 l 517 520 525 535 507 1 lFeedwater (Containment)l l l I lB21G02601DLY l +581 l +887 l +1013 l +731 l +665 l +610 l l l i l 2601TT l 397* l 227* l 174* l 333' l 374* l 377* l l l ] l 2602DLX l +258 l +269 l +280 l +275 l +260 l +250 l l l l 2602TT l 382* l 199* l 176* l 336' l 365* l 381* l l l l 2603DLX l +202 l -28 l -137 l -216 l -194 l -223 l l l l l 2604DLY l +416 l +1175 l +1348 l +770 l +642 l +641 l l l l l 2605DLX l -505 l +236 l +323 l +316 l +300 l +396 l l l 1 l 2606DLY l +465 l +488 l +560 l +418 l +402 l +357 l l l l l l l l l l l l l lFeedwater/ Condensate l l l l l l l l l lN19G00101DLZ l l l +86 l +63 l +244 l +204 l l l l 101TT l l l 95* l 113* l 112* l 126' l l l l 401DLX l l l +164 l +162 l +291 l +222 l l l l 401TT l l l 175* l 210' l 234' l 248* l l l l lN21G00101DLX l l l +80 l -136 l +58 l +24 l l l l 101T7 l l l 179* l 362* l 388* l 405* l l l i l l l l l l l l l l l l Main Steam (Non Con-l l l l l l l l l l l tainment) l l l l l l l l l j l1C88SAIT l l 535' l 535* l 536' l 537' l 539' l l 532' l l lN11G00101DLX l l -251 l Removed froml Service l 1 l 101TT l l 537* l 535* l 536' l 537' l 538' l l 535' l } l 102DLY l l -586 l -496 l -1305 l -603 l -556 l l -491 l l 102TT l l 536* l Removed froml Service l l l i e l l l 103DLY l l -394 l -376 l -471 l -386 l -415 l l -390 l l 103TT l l 534* l 534' l 535* l 536* l 536' l l 534' l l 104DLX l l -293 l -270 l -474 l -532 'l -178 l l -452 l l 105DLX l l -3548 l Removed fromlService l 1 I I I I l l l l l i I

BOP Piping Tharmal Exprnaics IC88-ST05 PAGE 7 TABLE 4.1 \\ NON-NSSS PIPING THERMAL EXPANSION DATA l SENSOR l MEASURED DISPLACEMENTS (MILS) l l ID l Max l Max l 25% l 50% l 75% l 100% l Bypass l Turbine l l l l NNH l NH l Steam Flow l Steam Flow l Steam Flow l Steam Flow Valve OPS l Warmup l l R2ector Power (%) l 0 l $5 l 24.8 l 52.6 l 74.6 l 96.3 55 l 16.8 l lResctor Temperature (*F)l 5514 l 5535 506 l 517 520 525 535 507 IMain Steam (continued) l l l lN11G00106DLY [ l -674 l -590 l -558 l -548 l -598 l l -593 l l 107DLY l l -602 l -437 l -573 l -496 l -490 l l -606 l 3 l 108DLY l l -287 l -239 l -299 l -284 l -229 l l -293 l l 109DLY l l -2407 l 4---Removed lfrom servicel l l 301DLZ l l +1028 l +1056 l +859 l +1039 l +905 l +1015 l+1194 l l l 301TT l l 535* l 535' l 536* l 537* l 537' l 534' l 535' l l 302DLY l l -620 l -612 l -870 l -643 l -595 l -695 l -576 l l 401DLZ l l +1051 l +1292 l +825 l +1228 l INOP l +1041 l+1388 l l 401TT l l 538* l 539* l 540' l 541* l 541' l 538' l 538' l l 402DLX l l -2534 l -2689 l -1174 l -2621 l-2244 l -2524 l-2694 l l 403DLZ l l +155 l -53 l +130 l +331 l +22 l +188 l +4 l lTurb. Front Casing Tempi l N/A l 251' l 302* l 328* l 347' l l 298* l I l l l l l l l l l l SENSOR l Max l Max l RCIC l HSIVLC l l l l l l ID l NNH l NH l OPERATION l OPERATION l l l l l l Racetor Power (%) l 0 l <5 l <5 l 0 l l l l l HRenctor Temperature (*F)l.s;514 l [535 l 2 534 ~250 l l l l l I RCIC l l l l l l l l lE51G004SA8DLY l +260 l +1028 l +1003 l l l l l l l l SA9DLX l +14 l +60 l -125 l l l l l l i l SA9DLZ' l -26 l +1426 l -2071 l l l l l l l l SA10TT l 137' l 530* l 530* l l l l l l j lE51G00401DLY l l +1 l +11 l l l l l l l 401TT l l 233' l 482* l l l l l l 1 l l l l l l l l 1 I lMSIV Leakage Control l l l l l l l l l lE32G10901DLX l l -4 l l +196 l l l l l l 10901TT l l 66* l l 208* l l l l l l l l l l l l l l l 1 l l l l l l l l I l ) l l l l l l l l l l 1 L

BOP Piping i Tharmal Exp:niica 1C88-ST05 PAGE 8 TABLE 4.1 NON-NSSS PIPING THERMAL EXPANSION DATA i l SENSOR l MEASURED DISPLACEMENTS (MIIS) i l ID l Max l Max l 25% l 50% l 75% l 100% l RHR Shut-lRHR Shut-I l NNH NH l Steam Flow Steam Flow l Steam Flow Steam Flow down Cool #1 Down Coo 1#3 l Reactor Power (%) 0 <5 l 24.8 52.6 l 74.6 96.3 0 0 i Reactor Temperature (*F) 5514 .s535 l 506 517 l 520 l 525 349/329 l 125/146 ECCS Systems l l l l lE21G00201TT l 103* l 105* l l l l l l l l 202DLL l+161 l +205 l l l l l l l lE22G00301TT l 103* l 102* l l l l l l l l 302DLY l+656 l +782 l l l l l l l I lE12G01501DLY l+770 l +931 l l l l l l l l 1501TT l 116' l 96* l l l l l l l l 1502DLX l +23 l +13 l l l l l l l l 1502TT l 100* l 88* l l l l l l l l 1504DLZ l+149 l +151 l l l l l l l l 1505DLY l+690 l +745 l l l l l l l l 1602DLY l+669 l +659 l l l l l l l l 1602TT l 99* l 88* l l l l l l l I i l l l l l l l l lRWCU/SLC l l l l l l l l l lB33G02401DLY l-667 l -704 l l l l l l l l 2401TT l 510' l 518* l l l l l l l lG33G01101DLZ l -67 l -36 l l l l l l l l 1101TT l 516' l 536* l l l l l l l lB21G16301DLL l +27 l -4 l l l l l l l l l 16301TT l 113' l 107* l l l l l l l l l l l l l l l l l lRHR Interties l l l l l l l l l lE12G02101DLZ l-469 l +15 l INOP l -51 l -116 l -149 l +2101 l -112 l l 2101TT l 436' l 450' l 429' l 431' l 424* l 411' l 307* l 100* l lB33G023RB6DLX l+736 l +761 l l l l l +357 l -14 l l lE12G012RB7TT l 152' l 271* l l l l l 349' l 146' l l ~ l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l l i J

-l BOP Piping Tharmal ExpIncica IC88-ST05 PAGE 9 TABLE 4.1 NON-NSSS PIPING THERMAL EXPANSION DATA l SENSOR l MEASURED DISPLACEMENTS (MILS) l l ID lRHR Shut-l RHR Shut-l RHR Steam l RHR Steam l l l l l l down Coo 1#3ldown Cool #3l Cond. A l Cond. B l l l l l l Reactor Power (%) 0 l 0 l l l l l l l l Reactor Temperature (*F) 349/329 125/154 l l RHR/RCIC l lE12G00901DLY l -2 l +85 l -21 l +6 l l l l l 2 l l 0901TT l 74* l 138* l 72* l 77* l l l l l l 0902DLY l +18 l +136 l -49 l -4 l l l l l l 1001DLZ l -214 l -161 l l l l l l l l 1001TT l 320' l 144' l l l l l l l l 1002DLY l +462 l +127 l -54 l +277 l l l l l l 1002TT l 308' l 143' l 75* l 272* l l l l l l 1005DLX l -289 l -58 l l l l l l l l 1005DLZ l -2883 l +3 l l l l l l l l 1201DLX l +174 l +46 l 44 l -30 l l l l l ) l 1201TT l 319* l 125' l 378* l 75* l l l l l l 1202DLY l +299 l +106 l + 4 7 ', l +11 l l l l l i 1202TT l 315' l, 119* l 73* l 74* l l l l l 4 l 1203DLY l +53 l +1 l l l l l l l l 1204DLZ l -254 l -138 l l l l l l l l 1301DLX l +122 l -26 l l l l l l l j l 1301TT l 280* l 99* l l l l l l l l 1302DLZ l -17 l -52 l l l l l l l l 1303DLY l +114 l -2 l l l l l l l l 1401DLX l -180 l -21 l l l l l l l l 1401TT l 66* l 123' l l l l l l l l 1402DLY l +92 l +29 l l l l l l l l 1403DLX l +324 l +1 l l l l l l l l 1404DLZ l +68 l +95 l l l l l l l l 1901DLY l +30 l -25 l l l l l l l l 1901TT l 100* l 91* l l l l l l l l l l l l l l l l l lE51G00101DLY l -11 l -92 l l l l l l l l 101TT l 119' l 122* l l l l l l l l 102DLZ l l l +1 l +17 l l l l l l 102TT l l l 81* l 105* l l l l l l l l 103DLY l l l -10 l -2 l l l l l l

BOP Piping Thermal Exp::naien IC88-ST05 PAGE 10 TABLE 4.1 NON-NSSS PIPI M THERMAL EXPANSION DATA l SENSOR l MEASURED DISPLACEMENTS (MILS) l l l ID l SRV @ l SRV @ l l l l l l l l l 250# Rated Press l l l l Raactor Power (%) l <5 53.2 l l l ' Reactor Temperature (*F)l ~ 390 ~520 l SRV Discharge l l lB21G02301DLA l -247 l -256 l l l l l l l l 2302DLL l -62 l -185 l l l l l l l l 2303DLL l -68 l -207 l l l l l l l l 2303TT l 231' l 308* l l l l l l l 4 l 2401DLA l +257 l +703 l l l l l l l l 2402DLL l +13 l +44 l l l l l l l l 2402TT l 234* l 348* l l l l l l l l 2403DLL l +221 l +731 l l l l l l l l l l l l l l l l l l l l t l l l l l l l l l l l l l l l l l l l l l l l l l l I I

BOP Piping Thermal Expansion IC88-ST05 Page 11 5.0 DISCUSSION 5.0.1 The remote instrumentation program had been organized to collect data with the plant in a variety of cold and hot conditions. Thermal displacements were calculated by the Startup group and compared to the criteria curves provided in Appendix I. Test failures were documented by a Test Exception, and referred to NPE's Piping Analysis Section. Their preliminary evaluations were provided back to the Startup group prior to the continuation of plant heatup or power ascension. In some cases additional piping walkdowns were required in order to locate potential obstructions. Where needed, formal analyses were performed at a later time, in conjunction with Bechtel Engineering to document the ultimate acceptability of the measured displacement. In this way a system of independent checks were enforced to ensure that proper engineering considerations were given to the documented failures. 5.0.2 To support the remote instrumentation measurement program, system walkdowns were periodically performed to identify actual and potential obstructions. During these walkdowns, interfereoces were identified by either direct observation or by finding evidence of crushed or deformed piping insulation. Additionally, areas of low clearance were identified as well. The actual or potential obstructions were dispositioned in a variety of ways. In a few instances, a plant design change was implemented, minor problem areas were either resolved by Maintenance Work Order (for trimming, cutting back, or otherwise modifying piping insulation or non-structural components) or by evalution indicating the acceptability of the obstruction. In conjunction with the visual observations, piping snubbers were checked to ensure that they were not fully extended or retracted and spring hangers were checked to ensure thay they were between their hot and cold settings. Actual spring and snubber readings were taken for numerous supports to baseline component and system operation, and to support the remote measurements. Due to radiological considerations, such of the piping was inaccessible during high power operation, thus the walkdowns were limited to some extent. For example, drywell piping was walked down with the reactor at rated temperature, but with the power level below 5%. The Turbine Building piping, such as Main Steam and Feedwater was easily accessible up to 25% power, but at high powers only limited portions cou'Id be accessed. This condition most affected the Feedwater System where the process temperature varies directly with power level, l consequently a rated temperature Feedwater System walkdown could not be fully performed. In lieu of a rated temperature walkdown, the sytem was checked after full i

BOP Piping Thermal Expansion IC88-ST05 Page 12 power operation following a reactor shutdown. This walkdown paid particular interest in identifying any areas where there may have been evidence of prior problems such as crushed or deformed insulation or obviously damaged components. 5.0.3 Throughout the course of testing certain factors continually contributed to the numerous criteria failures experienced. Provided below is a brief discussion of these factors and their impact on the test. a) Test criteria were found to be too conservative in relation to Code allowable stresses. The actual criteria were based on a specified tolerance band around the analytically predicted displacements. The bands were selected very conservatively for ease of criteria development. Displacements outside the more liberal " Acceptable Limit" band did not necessarily indicate equipment problems or high stress levels. Since over 98% of the " Acceptable Limit" failures were found to have adequate margins to the Code allowable stresses, a broader tolerance band would have been beneficial from a test performance / failure resolution point of view, thus expediting the test program. b) The analytical displacements from which the criteria limits were derived were based on analytically assumed line temperature distributions. During testing, it became evident that the actual line temperature gradients were higher than assumed (particularly on isolated lines) so numerous failures were experienced simply because portions of the piping were substantially cooler than assumed for the given system configuration. Analyses using actual line temperatures generally found substantial margins to Code allowable stresses. c) Inter-ties and connections between systems and major equipment provided variable boundary conditions which did not always correspond to those conditions assumed in the criteria development. An example of this situation was branch piping being independently subject to the thermal movement of the connected main line. This was particularly noticeable on RHR and RWCU system piping, both of which are heavily inter-tied to process piping such as Recirculation and Feedwater. Additionally, the temperature induced displacements of major equipment such as the RPV, turbine and heat exchangers provided variable boundary conditions which were not (and realistically could not be) thoroughly accounted for during the criteria development.

B0P Piping Thermal Expansion IC88-ST05 Page 13 d) True cold plant "zero displacement" conditions were difficult to obtain because the reactor was not always brought to an ambient condition (85*F) during shutdowns. On several occasions " ambient" data was obtained with the reactor at an elevated temperature, as high as 130*F. Consequently, the l cold-to-hot piping displacements often corresponded to varying degrees of pipe delta-T. Since the criteria assumed a relatively low ambient condition of 85'F, the criteria limits were based on higher than actual piping delta-T's, and it was often found that the piping moved less than expected. This situation, while leading to failures, was readily evaluated by NPE by simply pro-rating the criteria based upon the difference between the measured ambient temperature and the assumed 85*F ambient temperature. e) Sensor failures contributed to an increased work load. Sensors were found to fail due to a variety of mechanisms, such as dirt accumulation, water spray, and physical damage sustained during periods of heavy traffic. Despite periodic functional l checks and calibrations, sensors failed at inopportune times, and were not readily replaceable. Hard up-scale or down-scale failures were easily identifiable (readings > 3.7 inches). l Intermediate failures were not always immediately discernible. The sensor data was assumed to be accurate, unless proven to be faulty. Several i instances of criteria failures occurred which could not be substantiated by either data from other sensors or by physical measurements of nearby spring I and snubber supports. In these instances, the sensor was functionally tested at the first accessible time. If the device was found to be faulty, it was replaced and data recollected, if possible, at the next test condition. In instances where the sensor was found to be operable, increased emphasis was placed on visual observation. Additional system walkdowns were performed to identify any obstructions, and in certain cases, snubber functional testing was performed to identify the i existence of potentially locked snubbers. 5.0.4 The following report subsections describe the various phases of the Thermal Expansion testing. The actual test data is provided in Table 4.1 in tabular form, and in Appendix I in graphical form for comparison to the Expected and Acceptable criteria limits.~ As discussed earlier, off-rated temperature piping data taken during ) plant heatup to rated temperature is not provided. The l

BOP Piping Thermal Expansion 1C88-ST05 Page 14 i off-rated data was used for trending purposes, and though were compared to off-rated criteria during the program, only the final rated temperature data are given. This l trending data proved very useful in the early detection j of some system problems. The only significant thermal j expansion related problem occurred during Non-Nuclear Heatup (NNH) and was attributable to not having a reliable trending curve. Refer to Section 5.1.2 for details. 5.0.5 Appendices II and III contain the conclusions of the NPE calculation results for Nuclear Heatup (calculation MC-Q1111-830027) and Power Ascension (calculation MC-Q1111-85039), respectively. These are provided as background information for this report. The Piping Analysis section of NPE independently calculated the piping expansions using the test data provided by Startup, and were responsible for the evaluations of the acceptability of the measured displacements. 5.1 Non-Nuclear Heatup (NNH) Testing 5.1.1 First Partial Heatup (NNH #1) This test represented the second reactor heatup to rated conditions. The first heatup was performed in 1981 during the hot Recirculation Preoperational test. Pipe expansion was monitored at that time in conjunction with Special Test Procedure IC88-ST03, and is not discussed in this report. This second heatup was conducted in a similar fashion, with the reactor shutdown and the system heated by high speed recirculation pump operation. At the time of the test, the reactor was flooded, as were the Main Steam lines (with the MSIV's closed). The Main l Steam and RCIC Steam Supply lines were heated by opening a flow path through the steam line drains, and allowing hot, pressurized water to flow through I them. This was found to be necessary during the j previous plant heatup to prevent fully contracting or extending variable supports. If the steamlines l were kept cold, the upward vertical reactor vessel growth would " pull" the lines upward, without the l naturally occurring offsetting downward thermal expansion of the steam lines. During the test the following systems were remotely monitored at approximately 50*F increments of reactor temperature using the previously installed lanyard pots and RTD's:

BOP Piping Thermal Expansion IC88-ST05 Page 15 1 ' Residual Heat Removal (RHR) ' Reactor Core Isolation Cooling (RCIC)

Reactor Water Cleanup (RWCU)

'Feedwater (FW) - inside containment

Standby Liquid Control (SLC)
Low Pressure Core Spray (LPCS)

'High Pressure Core Spray (HPCS) ' Low Pressure Core Injection (LPCI) Subsystems of RHR ' Recirculation System (RR)

Main Steam (MS) - inside containment The Recirculation and Main Steam systems were specifically monitored in accordance with Startup Test Procedure 1-000-SU-17-H, as they are NSSS l

Vendor supplied piping. The thermal expansion data l was obtained from the installed lanyard potentiometers and RTD's at the following reactor temperatures: Reactor Temperature Date 166*F 9/21/82 189'F 9/22/82 258'F 9/22/82 293*F 9/23/82 322*F 9/23/82 346'F 9/25/82 On September 23, 1982, with the reactor at approximately 350*F, a complete drywell pipe expansion / vibration walkdown was conducted on the following systems: 'RHR 'RWCU 'LPCS

LPCI(RHR)
MS

'RCIC 'SLC 'HPCS ' Recirculation 'FW \\ l Additionally, the RWCU system was checked up to and including the non-regenerative and regenerative heat exchangers. The walk down identified numerous items, 6 of which required rework or increased attention. Most notable was the decreasing clearance between SRV IB21-F047A stainless steel air supply line and a structure I-beam. This clearance was to be visually checked every 15'F increase in temperature. However, the heatup was terminated prior to reaching rated reactor temperature due to an increasingly high drywell air temperature, resulting from inadequate temporary piping insulation and non-optimal performance of the drywell cooling systems. The reactor was cooled down and additional insulation was added on the hot piping systems, particularly in the vicinity of the RPV nozzles / shield penetrations. Also, additional work was performed on the drywell cooling system air flow balancing to force cooler air to the drywell hot spots.

t BOP Piping Thermal Expansion IC88-ST05 Page 16 5.1.2 Second Non-Nuclear Heatup (NNH #2) Following the drywell work, the reactor was cace again heated up in 50*F increments. The same systems as before were monitored using the installed remote instrumentation. Data was collected at these reactor temperatures: Reactor Temperature Date 197'F 10/13/82 244*F 10/13/82 320*F 10/13/82 i 348'F 10/13/82 402*F 10/14/82 451*F 10/14/82 498*F 10/16/82 512*F 10/22/82 514*F 10/23/82 At each temperature hold point, several hours of " soak" time were allotted for the piping systems to come to equilibrium before expansion data was taken from the remote sensors. Following the heatup this data was forwarded to NPE for evaluation. On October 14, 1982 with the reactor at approximately 350*F and again on October 20, 1982 with the reactor above 500*F complete drywell walkdowns were again performed on the following systems: 'RHR

RWCU
LPCI
LPCI(RHR)
MS
RCIC
SLC

'HPCS

Recirculation *FW Numerous obstructions, actual and potential, were identified and removed, particularly following the rated temperature walkdown. Most of these had to do with insulation butting against equipment or structures, and many low clearance (potential) obstructions were flagged. The most critical problem found was on the RWCU system, where snubber 1

j Q1G33G002R12 was found to be fully retracted. A design change was immediately implemented to resolve this problem. In addition to walkdowns, selected spring hanger and snubber movements were recorded with the reactor above 500*F. These readings were taken by the plant's Inservice Inspection (ISI) group over a several day period. The readings were compared to the expected readings based on design data in I

BOP Piping i Thermal Expansion IC88-ST05 Page 17 order to identify gross failures. Due to the limited time available for this effort, not all the desired measurements were obtained before the reactor was cooled down. The remaining hanger data was then 1 scheduled for Nuclear Heatup. It was during this phase of testing that the most serious criteria failures were uncovered. At the time of this test, the test criteria had been provided in the form of linear equations dependent on line temperatures. From these equations, criteria " envelopes" were constructed for trending purposes. While the test was in progress, an independent assessment of the criteria by Bechtel Engineering inoicated that a problem existed with the criteria equations, in that they were based on rated power operation (RPV at 535'F and Feedwater at 420*F), and were not applicable to the NNH lineup. The criteria equations were re-evaluated by Bechtel and were replaced with more specific criteria curves, for NNH use specifically. These curves arrived on site after the unit had achieved rated temperature, so the test data was backfitted into the plots. During their review of the lanyard pot data, NPE determined that three feedwater points fell significantly outside the Acceptable Criteria. Sensors IB21G02603DLX, 2604DLY and 2605DLX were determined to be subject to an unidentified obstruction which severely limited free movement. The analysis by Bechtel indicated that the magnitude of the stresses and loads on the feedwater nozzles were significantly high, although within the ASME Code ultimate stress levels. In response to this concern, NPE ordered UT examinations of the 6 welds l between the affected feedwater piping and RPV i safe-ends and the associated riser tee's. The UT examinations were performed after the unit had been cooled down and proved to be acceptable, but the source of the obstructions could not be located, even after numerous walkdowns following the reactor cooldown. During conversations with Maintenance Engineering, it was later determined that the unidentified obstructions had been temporary insulation packed between the i feedwater lines and the 6 RPV shield wall penetrations. l It was determined that vertical RPV growth pulled the feedwater lines hard against the dense insulation, on top of the lines, thereby preventing normal movement of the lines. The temporary insulation was verified to have been removed immediately after the NNH testing and was replaced with permanent insulation covers, the design of which would preclude a repetition of the problem. To ensure that this indeed was the cause

B0P Piping Thermal Expansion IC88-ST05 Page 18 of the problem, additional temporary sensors were installed in the drywell for future monitoring, and an increased monitoring interval was to be used on the effected sensors. 5.2 NUCLEAR HEATUP (NH) 5.2.1 Heatup to Rated Temperature Under the 5% power license, the reactor was brought critical and heated up to rated temperature and pressure in September - October 1983. During this testing the turbine generator was off-line and the turbine bypass valves were generally closed. Lanyard pot expansion data was collected at 50*F increments for the following systems, additional data was taken on the Feedwater piping inside the containment every 15*F. I og

RCIC

'RWCU 'FW

SLC

'LPCS

EPCS

'LPCI(RHR)

MS(to turbine and bypass valves)

Data was taken and plotted against the Expected and Acceptable Criteria limits at the following reactor temperatures: Reactor Temperature Date 205*F 9/26/83 243*F 9/26/83 1 304'F 9/27/83 341*F 9/27/83 404*F 10/2/83 449'F 10/3/83 499*F 10/8/83 535'F 10/11/83 As with the earlier heatups, NPE concurrence was obtained after their preliminary evaluations of the failed data points, prior to continuing the plant heatup. Their final acceptance of the data is documented in calculation MC-Q1111-830027. l l y.-_.. 7._ .-.-._y. .,___,_,,__y. ._,____._._,m_,,,,.y_,

BOP Piping Thermal Expansion IC88-ST05 Page 19 On September 27, 1983, with the reactor at 340*F an informal spot checking was conducted of the drywell and steam tunnel piping. Twenty seven (27) items were identified, the most noteable being the identification of RWCU drain piping below the A and B Recirculation Pumps being hard against the floor, including the insulation around valve G33-F102. Additional problems found were snubbers Q1B33G103R01 fully retracted, spring hanger E51G001H01 on the RCIC steam lines, bottomed out, and several instances of low to zero clearance between pipe insulation and whip restraints. Later, heatup walkdowns were conducted in the Turbine Building at 465* and 490 F reactor temperature. Several items were identified during each walk through. The unit achieved rated temperature and pressure on October 11, 1983. Between this date and November 1, extensive piping inspections were conducted in the drywell, Containment, Auxiliary Building and Turbine Building. The drywell problems were particularly few thanks to the previous problem resolutions. However, the Turbine Building steam lines were found to have numerous problems. This was not totally unexpected, as this heatup was the first time the complete Main Steam System had operated at temperature. The lanyard pot data had revealed the existence of a potentially locked Main Steam line snubber in the Turbine Building. NPE had evaluated the stress levels and found them to be acceptable. Snubber functional testing ultimately determined that NIN11G001R01, an INC mechanical snubber, was locked up. This component was replaced with an equivalent PSA type mechanical snubber, at the first oppor:une shutdown. The rated temperature walkdown ioentified 70 items which the Startup group flagged as requiring rework or NPE evaluation. I Major items found and later resolved were: i l

RCIC Steamline insulation hard against whip l

restraint, along with several other related l interferences.

Main Steam spring hangers in the drywell crushing protective box for SRV solenoids.

'HPCS test connection hard against unistrut.

Main Steam Lines in contact with grating.

During this test phase it became evident that the extensive walkdown efforts put forth during NNH testing significantly minimized the-time spent in the drywell while at power. Inspection and rework activities were reduced, thus attributing to significantly lower radiation dose rates received by plant personnel during NH testing. --w--n ,-,m----,w , -,, - ~,.,.. -, - - - - - - - - - -.

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B0P Piping Thermal Expension IC88-ST05 Page 20 5.2.2 SRV Actuation - Reactor at 250 Psig In conjunction with initial SRV testing, Startup Test 1-B21-SU-26-H, the thermal expansions of two representative SRV tailpipe lines were remotely monitored during the 10 to 20 second valve pops. Valves IB21-F047D and F051D (each tailpipe instrumented with 1 RTD and 3 lanyard pots) were opened and the expansion recorded on the high speed data acquisition system. The RTD's were found to quickly heat to approximately 230'F and the recordings of the piping movement show the sudden movement. However, due to procedural requirements, the valves were closed prior to the lines reaching equilibrium conditions. This contributed to several criteria failures, which NPE analyzed and found to i be acceptable. 5.2.3 Turbine Bypass Valve Operation Although the majority of the NH test phase was done with the bypass valves closed, some 5% power testing did require bypass capacity. Consequently, the piping between the bypass valves and the main condenser did experience brief high temperature operation. Lanyard potentiometer measurements taken I on the common line upstream of the valves did not reveal any problems. 5.2.4 RCIC Operation In conjunction with rated reactor pressure RCIC system testing, 1-E51-SU-14-H, thermal displacement data was taken on the RCIC steam supply line to the RCIC turbine with the system in operation. Visual inspections were also carried out on the entire RCIC steamline, from drywell to turbine, combined with hanger and snubber readings for comparison to design settings. No significant anamolies were found for this mode of system operation. 5.3 POWER ASCENSION 5.3.1 Turbine Warmup The initial turbine warsups were monitored over a three day period by checking the Main Steamline displacement sensor data. The final set of data was obtained with the turbine front casing temperature at a steady value of 298*F. This data was supplied directly to NPE for evaluation prior to continuing

BOP Piping Thermal Expansion IC88-ST05 Page 21 further turbine loading and power ascension. While not required by procedure, the steam piping was visually spot checked for potential obstructions near the turbine, this was possible due to the relatively low dose rates existing with the reactor below 25% power. No obstructions were found during this evolution. 5.3.2 RHR Steam Condensing On October 27, 1984, in conjunction with Startup Test 1-E12-SU-71-1, the RHR "A" subsystem was aligned in the Steam Condensing mode. Lanyard pot data'was collected and compared to the criteria. The steam condensing mode represents the greatest heat exchanger heat load, and thus temperatures, for the system. Numerous failures were observed however, most being traced to significantly lower l line temperatures downstream of the RHR heat exchangers. Final NPE resolution and acceptance of the data is documented in calculation MC-Q1111-85039. An optional RHR system piping walkdown could not be performed, nor could spring and snubber readings be taken due to the increasing radiation dose rates experienced near the various steam piping. The B RHR subsystem was tested in June, 1985, while the system controls were being optimized for operation. The results of the B Loop Steam Condensing test were quite similar to the A loop, l in that the heat exchangers cooled the process flow to temperaturet significantly lower than assumed for the criteria. Consequently the line temperature distributions, as well as the actual heat exchanger { shell temperature gradients created numerous apparent failures and data points being to low in temperature to reasonably apply the criteria. Once again, no walkdown could be performed due to radiological accessibility. 5.3.3 25% Main Steam System Flow i On November 15, 1984 with the turbine generator on-line remote sensor data from the Main Steam and l Feedwater lines was collected at approximately 25% l Main Steam Flow. The steam lines experience minor i temperature changes due to a slightly higher reactor I pressure and a hotter turbine front easing temperature, while the feedwater lines experience. heating due to the feedwater heaters being put into service. For comparison purposes, the 25% flow i . ~. _,

BOP Piping Thermal Expansion IC88-ST05 Page 22 condition, which approximates 25% power, resulted in a 180*F feedwater temperature, which is 70*F hotter than the temperatures experienced during Nuclear Heatup (without the heaters in service). Data was collected with no significant problems other than several sensors failing the criteria. NPE was able to evaluate each failure, and provide acceptance of the data. Their final acceptance is documented in calculation MC-Q1111-85039. On November 17, 1984 after the temperature on the feedwater lines had increased to approximately 300*F, the first high temperature walkdown of the Turbine Building Feedwater and Condensate piping was conducted. Except for the feedwater heaters, the bulk of the piping was accessible. High radiation in the vicinity of the various steam lines, limited access to the heaters. No significant problems, were discovered during this walkdown. 5.3.4 50% Main Steam System Flow Data was taken on January 2,1985 of the Main Steam, Feedwater and Condensate piping. The reactor was at 517'F, while the turbine front casing temperature was 302*F and the feedwater heater outlet temperature had increased to approximately 360*F. As with the 25% data, several sensors had failed the criteria limits, but acceptance of most of these l failures ws readily obtained from NPE due to the similarity between this data and the 25% data. The final NPE approval of all test results is given in calculation MC-Q1111-85039. } 5.3.5 SRV Actuation - Reactor at Rated Pressure In conjunction with Startup Test 1-B21-SU-26-2, i SRV's IB21-F047D and F051D were manually actuated at i rated pressure. This test was very similar to the 250 psig test performed during Nuclear Heatup, with l the exception of the higher resultant tailpipe temperatures of 300 to 348'F. As with the earlier 1 i test, the 10 to 20 second opening of the valves prevented true equilibrium conditions from being achieved. The criteria failures were reviewed and i accepted by NPE as satisfactory, these conclusions are formally documented in NPE calculation 4 MC-Q1111-85039. l -...__.,-v ..m.,_ ____-m_,, _. - - -

BOP Piping Thermal Expansion IC88-ST05 Page 23 5.3.6 Main Steam Isolation Valve Leakage Control System Operation The MSIV LC system was run in conjunction with Startup Test 1-000-SU-77-2 following a planned reactor shutdown. i 3 The reactor had been depressurized to near atmospheric pressure prior to system startup. The reactor temperature was below 250'F with the MSIV's 1 and the Main Steam Shutoff valves closed. The system was normally started up when the system i pressure interlocks cleared, and began to draw down the steamline pressures. The MSIVLC piping heated to approximately 208*F when the test data was obtained. This corresponds to near maximum system operating temperature. The data from the remote sensors was forwarded to NPE for evaluation. Their final acceptance is documented in calculation MC-Q1111-85039. 5.3.7 75% Main Steam System Flow On April 11, 1985 with the reactor at 74.6% of rated power, Main Steam, Feedwater and Condensate system j piping displacements were obtained and compared to J criteria. The following temperatures were measured: i Reactor - 520*F Turbine Front Casing - 328'F Feedwater - 388'F The test data was consistent with the lower power data in so far as the number of failed sensors, the degree: of failure ranged from slightly better to worse. The test data was, once again, provided to NVE. l Their preliminary approval was obtained prict to increasing power, and their final approval !.s documented in the MC-Q1111-85039 calculation. At this higher power condition, no visual inspections could be conducted, due to high area radiation doses. 5.3.8 100% Main Steam System Flow 1 The final check of the Main Steam, Feedwater and Condensate Systems thermal expansion was conducted on May 15, 1985. This test was run shortly after

BOP Piping Thermal Expension IC88-ST05 Page 24 the unit reached the rated power test condition (between 95 and 100% power). With the reactor at 96.3% power and 535*F recirculation suction l temperature, the turbine front casing was measured to be 347'F, while the Feedwater temperature at the outlet of the final high pressure heaters was 405'F, 15'F short of rated. Data from the 21 remote sensors on these systems were forwarded to NPE for evalution. Half of the points failed the " Expected" displacement limits, while one third failed the l " Allowable" limits. Additionally, sensor N11G0401DLZ was inoperable at the time of the test as proven following the next plant outage. NPE was abit to approve all test results (calculation MC-Q1111-85039) but lanyard pot N11G00403DLZ results indicated the existence of some obstruction. This sensor, located on the feedwater pump turbine steam i supply line had shown significantly low thermal i i movement throughout the program. Snubbers in the l vicinity of the sensor had been functionally tested previously, and were found to be operable. Since j this was the last opportunity to determine the source of the problem a final intense effort was put I forth to check for obstructions. Despite numerous walkdowns (with the reactor shutdown and again at low power) by Startup and NPE, no evidence of an obstruction was found. Despite this condition, NPE analysis was able to show that the actual stresses on the piping were acceptable, and no further action was taken. The final approval is provided in NPE calculation MC-Q1111-85039. In addition to the remote measurements, a full system walkdown on the Condensate and Feedwater was scheduled. In as much as radiologically possible, these systems were visually checked and selected spring hanger and snubber positions were recorded, with the feedwater system at 405'F. Except for the areas near the low pressure feedwater heaters, most of the Condensate System was inspected. However, only a very limited portion of the feedwater system piping was looked at. The piping near the process steam piping were in high dose rate areas and were rescheduled for inspection following a subsequent reactor shutdown. When the reactor was finally i shutdown following an inadvertent scram, the Feedwater and Main Steam systems were checked, with the plant in a cold condition. This inspection attempted to identify evidence of obstructions, such a 1

BOP Piping Thermal Expansion IC88-ST05 Page 25 l as crushed or deformed insulation, deformed pipe supports, etc. No problems were found during this effort, thus the walkdown was concluded on a satisfactory note. 5.3.9 RER Shutdown Cooling Operation i On May 18, 1985 with the reactor shutdown, at 349'F, 4 I the RER A System was aligned in a Shutdown Cooling Mode. Due to the high heat capacity of the heat exchangers it was impossible to fully align the system with full RHR flow to the heat exchangers without severely violating the maximum allowable Tech Spec cooldown rate of 100*F an hour. To solve this, the heat exchanger bypass line was cracked opened thus limiting the flow to the heat exchanger and minimizing the cooldown rate. The result of this valving was that the heat exchanger did not achieve the full design operating temperature, consequently the pipe displacements were significantly different than expected for the given system temperature. The B RHR loop was tested in a similar manner. The test results were forwarded to NPE, who requested that additional data be obtained. The low system temperature created negligble thermal growth on several segments of piping, so the test results were not conclusive. On July 29 and 30, 1985 a retest was performed with full flow RHR to the heat exchangers. This was possible because the reactor temperature was only at approximately 270*F, so the RPV cooldown rate was not as large as the earlier (higher temperature) test. Unfortunately, with the reduced inlet temperature, and high heat exchanger capacity, the discharge lines were very near ambient temperature and experienced little thermal growth. This data was also sent to NPE, and again they requested additional data at a higher outlet temperature. At this time, it was recognized that the heat exchanger capacities were so large, that normal system operation would not provide an opportunity to " heat" the discharge side of the heat exchangers. It was concluded that the only way to prevent on excessive l RPV cooldown was to decrease the Standby Service I Water (SSW) cooling flow to the tube side of the j heat exchangers. This would enable the RHR side from cooling down as much as it would under normal circumstances. i i

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BOP Piping Thermal Expansion IC88-ST05 Page 26 The third attempt was run on October 13, 1985 in conjunction with RHR System Technical Special Test Instruction 1-E12-85-003-0-S. This test aligned the system in the Shutdown Cooling Mode and then manually throttled down on the SSW flow to the RHR heat exchangers. Then, full RHR flow was valved to the heat exchangers by closing the heat exchanger bypass valve. During the test, these extra steps took longer than expected and by the time the system was ready for data collection, the reactor temperature had decreased to 146*F for the A loop l test, and 125'F for the B loop test. Once again, the system temperatures were barely high enough to properly check criteria. Ensuing discussions between NPE and Startup concluded that the higher discharge piping temperature operating state desired for the expansion monitoring were not practically achievable in the Shutdown Cooling mode, and high temperature operation would not be achievable during ) normal system operation. In response to this j conclusion, NPE indicated that the data collected to this time showed that the system displacements were 4 acceptable, including those portions the piping which never achieved design temperature. In lieu of i direct measurements, NPE personnel conducted an independent RHR system walkdown in an attempt to identify possible obstructions. Since only very minor interferences were observed, none of which 3 would impact the ability of the piping to freely expand, NPE accepted the RHR Shutdown Cooling data as having satisfied the test requirements. This subtest completed the BOP Piping Thermal Expansion Monitoring Program conducted as part of Special Test IC88-ST05. 6.0 PERTINENT DATA f 1. Appendix I - Displacement vs. Temperature Plots 2. Appendix II - NPE Calculation MC-Q1111-830027, Piping Thermal Expansion Evaluation During Nuclear Heatup 3. Appendix III - NPE Calculation MC-Q1111-85039, Piping Thermal Expansion Evaluation During Power Ascension Testing I l -, -.. ~ - - - - ~ -. - - ---- -

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Expected Limits Acceptable Limits -------- --4_ =- _,.__1_._

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l l N .-.O- _ _ _ _-4.m_ M -__. _-H".-_ g i_.i... 5._. .B m. 1 ._.u. m mm _M m _._ mg_ .-.u..e ..e .m.mm. u e_ .-__.i.._.___,._.nnin_ _ l' ._m...m.m ._4 ._m_ -_... _,s u W = i __m .-emen___ ..m m.- _... y..s._ _.m.% __ j _-_- _g . ~. - _.._e. _.,_t_.__. .=_.-g- -t e__ l.mmmm e.m m. __.. _. a -. _ _. _.. _ .g ~ .mu.. [.i. ipuu h 4-_- l m-.m._ __g_.._.__ q 1 .m. -..__E g -i-- g ..g-._m.... _.__ _ _.i - _ -., p _mmmm. e_. 7. _.. w .... _ -7, ____,3_ .s._._.. g-4__. . t __ . Gr _.._.__ _s g, _.~.A_*s__ '_-.__1... .._ _ w_-_ um.. _ -. - mm. - ( ..__.=== - _-.. _.. .. h am._.. ___.m.mm.. ._..m_. .mm-5 p.m_.,.. F.e_ sums. ..-_.a... --..__.mmmmm. .. m. .m +200 ...m.. .m.. ..m.. y.. g..... .mm._._m. l ...mm. ...-e ,_ __ _ _._., t. m _..... r.- _ww _._.f.___.. , _. a n - _ s..____ ._.._.,. _.. _._._t,.,.. w. y _ _._. _._.... g..f 2 _-.w _.__ _=:a e:........_.__..__,_ ___.__i.____._..,-x __u....__.. __..... s......... .... m. n_ t... _._..__:_... .__x=.._.. 0 _._t_.._..,._.__.._. _... s _ _ i._

s....

._.__i___..__..... ...._.._.._.._..i__.._ _.__i_____ \\ .. _.. _.._ _.. _..g. . _.... _..............s I ff C:t.1 17"T trl "r23 FED.*iW13TT1 IT1 tif t111tillifil T sittnisettletti t'ttti ;T1 17111g l -"U17U1!TD f]Trt. 0 100 200 300 400 500 550 s 1.P.Y.* Temp 'F i m r a I \\

BATA $1ETT.DJ Spee. 9E S-M.275.0 s f. BE-07. TIE 1Uut rwr.nunfitC APPeadia y 3,, n Sheet M of $9 Power Ascensies/Systee nesteps J Pre-ep Ise. No. M-1653 REv.2 ...... _,m, m g Lenyard We, B.36M GCE h1 . =. _ =S Stress Prob.Wo. ~.74

p. P..a o i.- =-.4.-J..-_

n00 _.......... m. i._e._a c ... n Mt_-n t.t:r i .._t...._=_=i..-... E Mvet, free computer output O . -*- e - Analytical Values

= =

= + 1000 EmPacted Limits

== E-Acceptable Limits -------- m n..._....._ _....I_,., ,_.....,..__-'-=1-..__.__... 4 4_.. WM ^ u ~ l ~ '""" i 4 em _ i- - j s.. r .e 't" _9 _-s.-.,_--~ ___..a,. q ._...g ._.9 _1 1 _,-.4_.-._,_ .... - _._i..-.. ] e.__ = ., _. _,._.. _ s~ "lE'E _. -..._m_,, _J' + g,9D . g w. a. __.._m__.,,,_j _ g,.. - _. _... _ g_ 4 r _. _ 3... _.._ _ ..-...3-,_z-U.....a.... ..p.. . _ _ 1._.- -_ S. .-W m.....'..%.. 3. 3. 3. _._i p. _.._.s

f...

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DATA SEEIT U. 5 Spec. 9645-N-275.0 Appendia O Rev.10 cecaa[ I/iA.Ift.

-'d - 8 3 GSLE oars oars onci avon N E}'MIU M Ur's NIIIeNIIl'I a 2 t[0$/

i m. ,.o, c, ' ' *1 ' ' 31 avs a cs 9lt E - 0 9 Aran vmnu mmunwa enns eno 1 QJ /d5 I I azio on sea my I a L

As l J TR Sb 2 A08 h I 'JP b) l HE" l

e ~ l l s ' O_ ever_esm aem.aa urnr n i 1 i i l i i i I.I ii I y Att &t.1 ft LM. VALut h l L s e ~ -EX?EC.TED SouMDAILY Liruft io -- - - -kEUTAME Sourd>MLT uMith / 1 I k' /T -[ } l l l e u f / o i L,1,. i i _s' / M ,s t .l f fr ~ 7 il l l l l l l ,,- / pr .-- '- j t '4 g/y y . _ _.l.1 +]% g . 2_4 V A 8 i l / l iE e i7 -M~ M-i (,'l is wg 1 l l l ,J"..- i _ _4, _,l __...._ l l 19 i I I ..E - sw 1 i zo 1 l 2: =

y_.9

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DATA SHrt? U.6 spec. 9M 5-N-275.0 rar-or." TurxMAL i,meirno appe=Hz e new. 10 t-W 7 of $O Sheet i i 1 Pre-op Iso. No. M 1653 REv.4 Lanyard No. 821GO2bO6 DIY Stress Prob.No. 75 geyel + ilmmu_LuH.U_u.W_ W N n d.d -2 tut:f ...-~ = e = Mvut. from computer output G = = Anal tical Values ,-4. :... - +1000 Expeeted Limits g-- Aces? table Limits -------- =- r=_2c - n.e .e -+- - e. _~ -1 g M, p..._ _4 M-Q .-.-ol--p-.-- ~ 4.--.. .mg t... f _f 2.". - i = . -. g g.

==- g6 6 _ t-=. = =. - "m ,-[ C%.._ -,._ m e.e _-4. _... _, - "J ---4 +600

i a-l

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e .i s..- e ..-.a.me ..I.

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4... :r= mn. n =: = n.... i =m m.., n ;-p in t m si m o n tai m in nius, nrn in inorii 0

100 200 300 400 500 550 R.F.Y.' Temp

F m

F BATA INEIT U.7 Sp.e. 9643.!!.273.0 PRE-OP. THERMAL MONITORINC APP.ndia g 3,, it e -.e 4... s is,.t N.. st..t X., M i Pre-ep Iso. No. M-1653 REV 2 Lany.rd No. E; I K46 G6 DW _=.g %g ,m..,4_.1 =5 = --- Stress Prob.No. 7si 3.p. H s; i: =- --s-4._ _ __ _ _ _-._ " _ __. M00 .. _.....f. _.. _._..

c. _.__ f---

1 '. _. _ __ _.. 3: =" P.w t. from comput.r output G i__

==

_ : :1 - -,:.::

... : J _ _ a Va u.s Espected Limits --= t2000 =r Acceptable Limits -------- M_... e __u 1600 4 l _,._ __ =_ =., l a +1200 m _mm._ _ _ __ : _. _ 4. _ _ __ _s_ _ __..~ ____._. _ __ v_ _ _., ._._.s.. __- __

1..__ _.

_._s_._._.. _.._.t. _ _ _ _ - =. _ _ _ _._ _.i._. _. _ a. 800- .v.i ' .__ _?s,_._.._, ...sc ...__a si L _, _._ ___ l .Jub _ _. .2 .l __ s. _.. _N__ ._.M..__...._.__ n. .v._.,___n_ 1 _m._... _.i. 00 _-T. _r.-_.__..__=., ._._..w_- i _ _ _. ~.. _..._.uc_....... ....i _.. _.. _... _ _ _ _ ~. _......... _ m__ ....,..g-_I__._ .a -. n m_. ___.i__...._r..... .. s. _.............. e. '"I'1*l* 4 f. f". *1'f' f* "l:"T".")1::"t *"D f i f"'a f f7M itJ 1111T 11 til f ff filt fit itj tll.riitttttegrg,*ttet f* fitrnl el?tttta i e 100 200 300 400 500 550 i R.9KioMC37emp *r

BATA S ETT U.7 spee. H45.x.275.0 t~ FRE-OP[ TERML NONTTORING APP **d18 U Rev. 11 Power Ascension / System Esatups Sheet N of 8 f Pre.., ts.. u.. M-lG9 5A PEV. I ,,,,,,,,e_,m_..,, Lanyard No. N 19GOGIO DLZ -- ~ Eanger Prob.Wo. 1 12 9 n.P. 38 ' - = - - _ :1_.m. _ ..._e t1200

3r m_u.n. u.s

==t=: ~ =. ut rte n t_mt ue e 2.__,=.. - -i: e c= -==.= m - _G e_ = -- ____...=_.:=_.:, :-.

= =

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m

= Analytical values J -- -.m,-.., _-.==9._. . a Expected Limits m-t.1000 _m,....-__

==: Acceptable Limite -------e -_. = ' --o m e. 6 @.$.6 SM M m WW -_6 m .- em m" g mm ~ e em-e ,.a. - -mm. g l -1 E N ._.m...

""~'

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===mm. 4... t6 f-=-=== m==m e W N em l-.n.mmm

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e..-4.....

e.... e. .e.e. m... 4 ..e.m. 6-e 66 O N e.m g M-.. .6 S..e.m.-...me....e.. 6 .ge.. au ..--e.e=..m.m...==.. e.me..e.-..m.e ee ...-......e..e a. e e-3 .. e. am. .e. e G...... ee ee am. e W. we. e .euw. - m. .-e e em. 5....- 4..= .me .....amm-..g g. g .e e _ _ _ a _e. mum._m _m_e e_mm_en. f.. __ _e. i.m_.. e_m. 9 _* 45.n.m .e.. e_ne. e e.m.... a ._m_. game i. 200 e. a ... _.i _. e.... ' t"1*L'ar:7.flTTU rIflMT'"11TIATU1117m fTTitu1711T11 1111f t t11111tInfil nittftenis.tflitt n mm1 fif f tflit 0 SO Id0 150 200 250 300 l N19GOOl0lTT "r-, *r m l l. -.

BATA S E TT U.7 Spec. 2 5-M.275.0 r ^ ,,,,,,, Tur* MAL NewtT9trwa A PP**M8 U mew.11 Power Asceaston/ System Easteps ' Sheet N ef_ d Pre-ep Iso. No. M-16s5b QEV 1 m,,,, -., m - e Lanyard No. Ati% o0401_DDC .=. -==$ --' ' Banger Prob.Wo. ~ 11cy 3.p,443 i: 52:. -- m.._- ..__. _ _ _ -=, c.:..:. a_.w w. I_cu_= =_. te-ttm n t._+rtiu:t -4._._ . ::= b _. _ =...._ : y 1200 -. A -_ n. ._._.L.., ' - = I=== - Si Mvat. from computer output O --i J-

=

== Espected Limits _._.....-.a na ca a us 1000 =: Acceptable Limits -------- u.

=:.==-

_-1 _._ -. _..s. m g.g _-[-, ,3 ..-e_. gg www -..-a u _ w. _ -.._.g _-y_' I- . _ _n = I~._.....i... -- - ( .. =.- j' i __-m. , j_ $.. _D.__ g _ _I.__,_., _ _ _. -f '_U._._.__... _._-..._A., p_ _..~. . -.._y.. g.J_ a3_me_ E=: _.. - _... _..... _....,...-.....ge g.g g g g, __m. ..... *.....m........_m.g.. g ...___.._._.-p..w._ _.._-.8. _..._ ..... _... ~. _.... _.S_-...,, __ w. -..s... ..l_.. g r. -.s -........ _. 4 _-._._

1...i

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BATA SWET Da7 Spes. H45-N-275.0 '~ Pu-ot.Jmrnstaomons APPadia. e se,.12 Power Ascension / System Bestupe Sheet.5. 9 f So V y 4 F2 00 OIDLX .: =' E Stress Prob.Wo., $9 3,y.40 . -.. d... _.. _ +. -. i - 1200 .2.:.c. u..m. i.ss a = n.:: : te te t,itee.t .= =. -.=.i:=_6 =. :

. =-=

I am.. i e =.c: t._ .a. r. E: Hvut. free computer output G i

3=1 - -?.:.===f : r

-E: Alialytical values ..._6 ~m.. : _ -_,.. ::. -j _.........a EnPested Limite - 1000 E_ Acceptable Limits -------- _ _"s.". e _

=

_.a s-e, _~_.==i. ~ ' " * - * * .~~ - _m 0 s.- . a., 1 --... i _. _ _- -.o. .-.. r _. -900 _,e- ..3.__. _ ~ --g--; g w-; .__2__._ 4 eum ,ac;

==-t__._...=_._.__i-: t 4 00 5 .. _. _ _._-.4_-_.. ...,. 7 s -.._.. ~ .a - w ._g_Ni____.__ eN

N mm _. -

M.. . M_ .W W i .-ee. m . -3 .___l..e. _..-f-.--. -...a W _- _A..-..- - -= n 7.

p-.

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. W.

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m. e. e. e _=.

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DATA METT V,6 spec. H45-N *.75.0 r pag.op[ TWIMAL )gingtIpg APyendia g Re% 10

- 5 Skeet $ et S O 1

I Pre-ep Iso. No. EI/?54. NNX ~ mann unmu o Laayard No. N alGocto1 DLY Jeress Prob.Ro. 1.g 3,y, 64 1-- 4-1200 mma-aum..uu un:m:++ -ti w m _ c--

==4-g . ~_ - -m Mwat. tres computer output 6

== Analytical Values .s = EE Espected Limits Acceptable Limits -------- .uma w wsw - --*i -i-0 --m. J a.e. --me m .-i. p._._- s .s -4 _-"y.m -m= g-W ,-.m- ..mm .= A =...,- -- -y - ..e im- . ;ry -600 1 - # = _-. - , -, ;=; -.. _"1

y..

g.w _f, -.-..=i=u...= I -..g. ym. ...=

===.a=.-., s f g g. mm---m-- . l, a

== .--...s..-..--- -..5 --.m --me...-=. ex me - _1 _.. _ " _.. - x, _.-l-- -. = - -l--.-- g .a - s = -400 -..w-..-._.=_===.=....... - -...-.- -. - CD, ..um..-===m. __...--__.g - ma ( l ..... -.-. am g -y....... g ...........mm... ........m ,..g.. .= .w %-mm -m m.mm e...e.- .. -.-,,n ..-._m.-.4....... . - - -.........m....u.m... ....a .--mm mmm... .. _. m.m. . - _ 5. -.._. .._mm_ .mu_s --m. --....mm.. -200 e. m_,--......--.......... .smann -.. -. -. -. r. A.--- ...-...r.-.. E.. -.. -... -. _ --.....3....... .... - -= F -...e.. I -.. -..=me...e.-..m.mm. ........e-u .. es a..m f l 6....-.- 4. ...a.. _...., ...mm. i .........-ta-...m-- 4 --m 4.-a. [ m - -m ..-..u-m-g.m. ._. =. ..--m.... e ..u.. 4 w ...a-0 e- .m.. .=.um=..........m. ..un.mm...g......g....- ...--l..m......-.- .. mm. . _..3._.-.. ..mm e

==m--.m.. ..m...... ...m. .....mm ..mm. 6 - ...-q. l .m......-....e.. -m.. .m-.....-.e.mm. m .m..==...u.... .u.m. I eue. s... mme........ s---....u m. ......................,..........==me....... .g.... .m. 4.... .-.....me. ...m ..e.e u. =u .. - = =....--....- 6. -.g= 5. ...-..e +200 m. .m............-..m..- ..m. ..mm...m..u-u-u ..m..mm. .....g__.-g. -_....s-a.........en.=.m,. .g. m. .. = = .. t _.. "" vu2 *"1 C"T* f*N*2' rt-i t _ rTnUIT1.1.f 11'"T1 t11 tifit818Hutu ris t e isi e sti;t-rie tr tt pipt g 0 100 200 300 400 500 550 R.P.V.' Temp 'F l m

^ PATA SMIT U6 Spee. 9645.M.275.0 r-PRE-OP. THRMAL MOpfTORING APPendia O Rev. 10 R E AT-m sheet 1 ef 6 0 Pre-ep Iso. N..__M-1ssa Rrv.s ...C ~ Laeyerd No. hiil10mM 'ht_v Stress Prob.No. w

3. P_.9Ao 6-Lttri.*_ t e _ua i.l uu im -

-+n test sw rtstr -.. ; m- -:tm.. _ -. = _:-, _ E: Mwat. from computer output G

==- =_ Analytical Va ues _ __. __n _=== Espected Lgeito -1000 =_ Acceptable Limite -------- _ p_._.._.. _ _- _-t - e -800

p. _

i _i_ _i a .gnq _ _. _._.._ __ _-i _ _ _., _ _ _. _ _.i. _ _J__ 1 _.,..__y_.=- a. i _._ ~_ 400 m ~ _ ~ _ _ ca _._.w._. .__a_._.._ __. _ _. _ _ c _s.. _ _ .___._.______.i_____. i _._ _1 ,r=. _ /... i t _ =. l -200 _,, _ __ s__. .r._ a. _ _n _ .._ _ t...... s __. ...,;ms.. _. ......s. _,.L...- 0 ._.i .... _...s _ __._ __._a. . _a __. l ... T 't '3.""1.""T* , r* C. ":""1*"*"1 ~:l"...-".* 3.*:T'. *.;""U"I* t'f fif e*i3 1 *i1y -*81-.. ,iti;t* '1 C l f"11 lt U l r, t j 0 100 200 300 400 500 550 l I R.F.V. Temp 'F m

i l i DATA SMEt? 5.6 Spec. 9645-N-275.0 1 I_ PRE-OP. TIERNAL NoltITOR11tG A yendia 5 Rev. 10 P 0'** m-'n ss..t 4 9.e & o Pr..o,i... s.. M-issu. Rtv., Lanyers No. N 11Goofo 3.DW -i-Stress Prob.No. 1,4 3.P. Bo I:"" =- "' 4 - s 1200 imiwtiumuu sto--+ p-n im a. a.u - _A._.._ '-.- {- -- a ____.4 ....._ i j - _e_._. _m = i .= Mwat. free computer output G

'=-

._..__h_=_ i Ana yt ca a ues = _._ _- _ ___ i.. .,_._.___.3 = Espected Limits Acceptable Limits -------- = =_- P=.._.._ .=. e __...,._.._ _ _.~_,_ _ 800 1--

i

~ f a . _ _ g._ _..y. w___ -600 _-1 _ _'1 _. ~ _ M_ ___2._._._._._.__i.- _.._4 ,.a" .__..._~._. f.- _ _.. s.. 2 .g,nn t-__._.__ n_.. m g.__ _ __.._-. _ _ _._q__ ...s i ___ /...__ .~s ._ f _.._... ~_. _ _ _ _. _ _..,.._,..,a......._ o. .. _ _....._.s__. ._._ _ a _ r-- _c_ .ee...._.._.__. f._ _ __.._..s._- J. _ ,.s. m, . _. _......._._i_..... _ q _ __ _._...__l_... ._..._.-..__.._.._.:._._._._._......a. i. 0 ._...._.._._.__1._......._i.._._...._._....._. ..._._i._....... _. __. :2_.__. __,l________...... _ _.. _. _.... _ i MOD s _.. _ _. _. _. _...._..s_. -- mis - r- : :.. :- t-i =. =. rr. - 1 r r tr t. a m p f t n l. ::... i.;t ir:;r;1r puerii 0 100 200 300 400 500 550 R.F.V. Temp 'F m r f l ~.

t i l BATA SMrET // / Spu. m3.M-US.O APP *d iR U Rev.14 ' FR2-OP. TmMAL NOltTTORT1'G Sheet M et 49 t-Power Ascension / System Neatops ,n......, m.m, Pre Ise. No. 9 1654. Rev. ? -v. sE:f 3,anyard No.M (GOOlO3DLY I stress Prob.Wo. 12 3 y. 80 A =- h --4 -1200 l am..u_m._ius, s_ca._=_n=.a=s aseste a,.t_m__iu:r - - =. - - . =. _ . _ _. _ __ _ r ._ _w.... = EE Mwet. free computer output G .__J____..__-.. _ _.. - ca a ses -1000 Espected Limits = Acceptable Limits -------- _=- -i ._ _.i_._ - 00 _._....u. _ _ _=::.._. =J - -i -i a i_- ___._i_ 00 -4 - - _.. _. _..._.. ~ _.._f._ .._...1_._.. w _.._. _ _ __ _ m - ---mm &_ _ w-- i w w _m_. a _ _... _..._...il _.t .___a.__ ._..._m. ..s__ - 00 _ _._ _i-- ._... =m m_ _ t._ _ o..._ __m. ...s . _ = _ _w..._.. 0 ........s.. _ s _.. s.. . ~.. _t.._..._..__..._ ,,.. =........... _....... _.. _ _. _ :n. _......._.... _..._........ _._i__.._.._. _. _ _ 200 8.. _._..l.._.. _....I

ri 1'st:r f'1'11-lrtTt1TT-T!?t:TWIrtl@lp 14111rf'11 111Ittf11 tifI'IttI rt1Ittsieittottth fif't"T'1 ettIf11!1 0

100 200 300 400 500 350 N. P. Turtdne Casino *Tsup *r m _. _ -. - _.. -. - - _ - -. -, - - -. -. - _ _. _., - - - _ _ - _ - - - ~.. = - -. m.--

DATA SIBIT U.6 spec. Mel-N-175.0 APP **di8 9 Rev. 10 t-PRE-OF. MML MMMORING pcuan MAT-m sheet 5 2er 6 o Zee. No. M1G54 REV.2 ........,m, tre-*P Lamyerd No. N 11 G 00104_TRE ~== l = = Stress Prob.No. M p.p. MB 1200 -..a utmea um..._u m_ia - *teu n.;n s n_._ Mvet from computer output O = =. =. =_ Analytical va oss _ _ _.. _ _...___..s E..E-Expected Limite Acceptable Limite = P._._.. _3 e. __._.,r_a_,. _.. - -800 f _....g_.___ y -D =.i i ~ -20 i _m __v__. .__... __,._.__.._._,a__ l___.._ --_.__y_____-- -400 m _.___8___.._ g _ _. _ _ _ _1_ _a._.-_ i. L. as _.. _. _..p ._. 7.. 1___ _ f. ____._.___.._..._I_.._. _..... 1_ _ 1200 .. g .m ....t__._._.__.___ _._t.. ...._s __ _ 4,_. ..__t_.._ ....._v_ E

"m_

_._._._._._..#(_._ ...._s_.._. ._m-. f._.... s.._ i _ .._.i i .. ~.

* * ~ _ _ _... "

g .l _.. 8_.. --*"_"!~..."..'.__.."."..' . _...L_ i .3.. e_........._.., a..... .,A.._S. ..l. .. =... l _._l_._.__._.._..... l ~ __,__.._.t_.__.._._.n_-...... e200 ...._.-g _ _.g _ _._ _. ._._......_t... n u ua ?".2 f;"T1 f* t". 4......-EM tm l.'Tf". * *"I f"]) I 1 fif ataistl111ll *tt t'l: t es alli.t ' 'i tilf"If 01111* H 0 100 200 300 400 500 550 c l i o m.r.v. T =, r m, i n.

DATA SEET U.7 Spe c. 9643.M.275.0 f-PRI.op. TMrmy.AL McN1Tontwc Aprendin y gay,11 Power Ascension / System Heatups Sheet of.N M.1654 Rev.2 Pre-or Iso. No. l Lacyste No. N I i G Lh.J I D 4 D LX .=. _ =s=='-__ =:r:rsa' Stress Prob.No. p-g.P. l 2 6 1 - ~' ~M - 200 ._.. _ i..._.... __ : _._. te. m.r t,w-n u.1 n: _..=.__. .:- = t ...i . _m==4 e r. from computer output O

m _- :.=

=- E nected Limita = -m r. -.rr.W... J..

.- Ana'ytical va ues t_ _-

.- a s - 2000 ". : =T Ac c ep t able Limit e -------. r_ ....t_.__.._.... .__i _...-..-.._.._.T..=...._r.. _., _. _.,. _ - - = ,.,.3_....... 4_- .""."'M ..._. L _ 1 ...... _..1 .....-_.e ..e a ._..r..........._-, .'2. _-._ as .. 1 _. ~.,,,,.:a* 7. . m _._4 a... ........ 1.. _ 6. _._._e_ _. _. _4 _. - _p_ _._t._ ._..t... _._._ap.__ ...._....._...__wm et,s _.....s. w - -, _..._ _- ....._.i.___. g ~ . _ 8_ _..!_._ J __J.._._ .__-_.._t.__ _. _ _ . J. ( a. . _.. t.. _ __u... _ 3. _ _ _ a _.. 8- --._.a.. .._.l_.. _. - ....t._ .......A_. ...e _-. t K_. __.. __. s...__.

1...

_ i _... __. ..._f.".-...t. .s _._..t-- .._._1..._. .. _ t. __. ..._1- ..__4 = ._..J.. l \\ ,,, _. _.1 J._.. l ..l,... ..W_.._. ...._.B.... ".""T_. ....9 f'"P.*T 1 ~~~* *""il l 3"11 Tm i te1M* t 1 '1111!!,11111101t1 flteittontt ettto 1* fMT9 41 t t tia ' ::W st 1-T1i i 100 200 300 400 300 550 N.P. Turt ine. Casins Tes?

F mr-I l.- - - -.

""-=*---'m .i.7

,p.,,_.

DATA STEXT U.6 spec. 9645-M-275.0 3-PRE-0P. TERMAL IGITTORDIG APPendia U Rev. 10 occt'" "AT-un ss..t52 f Go Pre-op Iso. No. M-1ssia RN 7 . m lanyard No. NilGooloM I)LY

t

Sttoeo Prob.po. 12, 3.p. 'RRy i_ tut r2s _wt.i u u _W e *

n e tzer x -

e = Mwat. from computse output G L _.m . _"a = Analytical Values .4000 .f_.

==-- Expected Limits _= Acceptable Limits -------- ER r-- J e ,e n age = s-9'- n 4__._. .m ^ . _ _ _.. - Je_. _ _ 2400

_ =._t. __ __.._ __ _ _ -.

~ ~ _ _ _ _ L_ .m-.. _ m,- _._ _i. .e_._. . _. _____.g____._____. _ _ .. _ _ _ -1600 ,m _.w_ _w c w.__ .se.._._____...._. c___.. _ - _.. _. _. _ _ - _. _ _ _. _._.....i___._._______.. _.. __ _ _...._ ___..._i_.._.... .... _.._r._.._ 800 ......_-_._._e_.._ _w._.._.., ....O _..._.__i_.__ ___..._.s._ _ _. _.._...s...... . _... t. _.._1__..,._ _.__i._._.._.__. _._. _.._.._... .... _ _.. _.. _.. _.. _...... _ i. _... _.... _....._...... .... 1 __ _._.. _. _. _ _._._. _ _._s..... _ _... _ _. +500 .... a. 3 f"*1."'"T.. f* *. ;.. .a.. :."11":73 3.:'"*. * -".".1""f1 ITT f17.'1111111T16 "!!Ill i' e s e ' e lli t ! ' f'l fTlf;1 lf1]11 ll 0 100 200 300 400 500 550 l l l R.P.V. Temp 'T m r

d r l DATA $1EIT U6 Spee. 9645-N-175.0 PRE-OP. TIEIGui. MONITORD80 Appendia U Rev. 10 f. I "D Sheet M of N 1 ) i l Pre-o, re.. m.. M-M854 9En Lanyard No. N itGOOlod htV 3_

3==

Stress Prob.N.. 12 D.P.449 1200 i tamt.i.u._m...u_uIm _--+uttu n a.i m i j = Mvut. from computer output G

==.

=- Analytical Values 1

.=_ _. _.. ._s

== 1000 j

==. Espected Limits i Acceptable Limits -------- j g,,:l _ -. _ = j .l__ 3.__ _ _ r_. __, - -.< ._. _ _. _ _. __..__._..u,,~... _,, ..s._ 4 00 P_-- .....1.;pc:=;p _ ~. i -1 __=.a m._ _- = __i a \\ c_. ~ _ __... _. _ _.__i___ _._3. g.__ _ _g7._.__. -600 5 1 _m l . _ _ g.. p. _._=;;;p _____t.____ ....._._.__m j

s. _.._

.er_ .f_. _.

__. _.. ~

a. - _ _.J._f_-____,#._,u_=._ -400 ta gi .- _- _ _ _. _ _. _... _.. _ z. ._.._t.._..__..___.._._._.-._ c:... .. _ _ _.. _.. _.. _ _. _ _ _ _ _ ?t __ _ T_d ... ac t__ .....r.=_ .t._..._..._ _ _.. _. _ a, g..._ _ _... ._i...._ ___..__ c. : .(_.. e._. _. _ _ _c . y. _,J_.._._ l ..._.._.i._.. -200 . _ _ _.. _ _..._ _ i. _ . _ r..... _.. _.... _ ~ _... l g. _ i _ _... _. _.....s ..__.._s.... n _n _.. _.. s.... __m_.. .g._...__.._.._..._._ ..g...__.._.._. l . _. g _.: .g 0 ...._4_._. .._3 g .. _ i. I "" 1.-""T* t r* " -" =*. :'7":;.;t".;;- ;;'"r t** fit.*ts!t:18tip ".se .'I::t " r:I f"111111 t t e,i 0 100 200 300 400 500 550 1 R.P.T. Temp. 'P m I t ) ,,._.__m.

i mATA SMEET (l. '* Spes. H43.g.275.0

g-M*0FEMAL MMEEE APP'* U 5 Rev.14 Fever Ascensies/Syste Westeps Sheet 5 7 of_ 99

-,g ml Pre ep Iss. No. M.1654. Rev. 2 .......... " usam -a - Lamyerd No. N i l G O O 106 l_ Y .=. ' - " ' * - S"'""_. - .7. " Stress Prob.pe. 12 9.t. 9 9 9 u;. s.um..u n s_es._:.= p= =. etas ri.t_misar

== _..=.s==L.v. _- ~ .i _. < - - = i. = w.=: t-.1=:s z:sss - *:="".' "__.J:E:-= < Mwat. from seepster output G =. = =- _.=.=.=. Analytical Values

. =

-1200 =._ .=_ Expoeted Limits = Acceptable 1.inita -------- = 's:.s.~ =-- 2_ -i .._."m.... ~ ..e. i -1000 _....1.-------_ I.. I. =3"""* P.=. = " " .i i e-= N --- M

==" n i 6_~ 8" 3 .au m. .g g =g; *,.,- N _.-"_"*.;*:"~~'"I-- ..,..... ". i *.MM*=,.** _ : e e800 - _J _ w w =- .-.m_ _-t_ %__i ..g. _- m _.-_1.."..'.E t.- f ... 1. s 1 _ l=_=.. =. e._.-'._.d_'_m. a__,_ - _.. - _.. ' ". ". ".. = _ _ - " " " " ' _ ,... ~. _ -i_. ww -1=_=.==_-.' " :l ;:=; ': I.. - _=====. ' _. -ru ':=" - } ~_^:_." =.-w .I -..,=': - t.= :==._.. g =. ,...=..=l. =.==8 a nw _ m g.. _ ..m. w. 3 _'.=.=.e -%_ 8. - -. r

1

_--___-._.4.- . ~ c u

4_=. } _'" 7..t=' ":_"'",==';. =". 8 :" *."=.;Z." "M.

_.' *.":"l."J.: :.".""". ":.:" %'. ;.7. * "".*.. ' ". : "l.".".".;.* 6. __ w _. ~ ..j..3..'- ....._..........4..-e SE._..._ -._.. m,...._....... -........i._.. :3 5E.. ""e..r-.. 4 00 = _.t._.. _.. ...l_ . _...l

4. _..._

- s....._ _.....w m '"""-"N " - --. p.

s;.

_....._...._.:.:-= =... _ ". " *. ---==:: t-

- T -

.t. _.......... %._.A...,_ .t=*. ...._..t.. ......_.....4......4 .... -.._f. .....8 .;*.: ::. '7. =. *. = :.= ~ 3* 4...* t.._J;

3..

.'l..-.

=* :

4 '".. :l.

t

l...

E l *4 :"=: l*".*..

4 2 ;.* L:2 4."44*. -.-. ~ :- A. v ":: 4.*.;i. R .i. :. 8

2 =_.. :..-. -

4". '". 4= . :.: =.;... .- :.; t.:w.

=..* :1'; :":.

.;.:.:'=: =_-- - _....._w. ...._l... _.e t. .f.""....... 0 4. =,. 3 J 't."... f.* =" 4i.:.*

.;;

J I

" *4*!" 'I.. ' 4

- E"W 4f
flifDlrt:11WTITUT171rt 1721ffft tutflff1I tittttflitill111111 ftlltItttt toItIh r1f m tlifiltitiI,u 0

100 300 300 400 $00 Ho N. P. Turtdne Casinq ~TwP

F m

r

i l 1 1 I BG. SIEET U.6 Spee. 9645-N-275.0 PRE-OP. THERMAL MONITORnec Appendia U Rev. 10 W W 1 NEAT-M {, Sheet M et 6 0 t l Pre-ep see. us. M _1 4 s u o tv.s .e:e. - Lanyard No. hlHGootot 2Lv Stress Prob.Wo. 1,9

3. y. gt.,

=Z= l= =: ~ =_. ~ -1200 s.tmes s _u_ai.s _u o_aw-+-am tzt. zu-rnai.inetteer .m_- i i = _1==. i EE Mwat. from computer output G

=-

=_ Analytical values _..u_--4. _.. .=- Expected Liette Acceptable Lietts -------- =:- _ P=u.- --_- _._ _ a ..=.________.J, ... _.. _ = _. _.. _ _.. -800 4_.._ a _ _.. _ = _ = = _.. -600 .___:_.__ __ m. ___4.__. i 1 __._.... _, _ _t_ _g_ ~ ~ _ _s ___..-.a__ 1 -400 na,,, _. _ _...,....__._____3.__.___.__,__.__ a g_ _ m__..__ _ _.. _....... _-. _ s. __. _ _- _ ___ f__.....__.___..... _.. ._...:_._..-______._...._._ar a. i ... _... _ _ s. .. _ _ s_ e t- _ _- _1 _ ... ;;r--. _. _. -200 ._ w . _._ _ _.. __....._._,_..,_,r, ~. _. _ _.. _. ..r.. ~.. - - _.__,__ n.. _. _ _ _.. __i

r. __.

i n .t__.._2.__..._.__.___.__ .._.,____.s_.__..._..__.._._._... _.......... _. _... +200 f._... _ _. _. _.. _ _. _ _.. _a - : r tn --.. r-r :.. : t = i :nt n.:.

1. v m tit. iisiottohm...

.uite ir o-imsierei 1 0 100 200 300 400 500 550 I R.P.V. Temp 'T m r ..n.--

.-n.--.--

1 MTA HEET u. 7 Spec. 9643.w.175.0 g-FRE-07. TE R MAL MONff0 RING APPeadia g 3.,, 14 Power Ascensies/ System Beatsps Sheetfgy,,ef 85, 9 Pre-ep Ise. No. 51654. 'tev. 2 1 ..m umum m _ g,g Emeyard Be.N I I GOD 07DLY =._ Stress Prob.5e. 32 3,y.g 2 . P_._ i_""*.= -1200

. rue.s_um...u_s.I._n._u_.=: u: nu urtes nur_must a=,..__-

- =- =.== Mwat. free seeputer sutput =_ i =

=-

_J. =_ Analytisa va mes

=z

_.=9 .__..a =_= Expeeted Lim to - - 000 =.

=:

Acceptable Limits -------- E:_:

=: :.a=_.:=.=

i -800 -- l- - =: .=. 1__ p.in ._. _._ ~ _ _ ._...l____.__._______<_ _....._.m_ _ _. _ _. _ _ i t _4 o i __ _.____.i___._..___.__ _.1m. _e_r.._. _m___ __._.__m .__.m,,_. _., - - -. _ _ _ _ _._...._ _. _ .i ______i___..._...___ _.t..... _ _.. __. _ _ _.._..._ _ _ __.s...._ -200 ..=.._._..__.._.__i_..._. J ......a, __._i__..__.__.. _.. _.... _._ :......_i__._.._. .s. . z- .... s. ..._i...... _ _.. . _.J.. 0 ..._....._.._..= _ _.._.s....... s_ _-.......... _. ..............................._m... I ......i.. '"~r1"tTtf trflff'ti rt laf7*11TL"f1T1FI 17DifffitM111FT'11 1111tf f t111ttl11til filllitttttt'f f f th rif1f ff11 att tfitit 0 100 200 300 400 300 550 p N. P. Turbine Castne fnip 4 m I l e------ g

wy-p

,v.-, y ,,-.-w. ..--.,,,_,,...y ,,,p,,,,,,..,,,,.,wg,,,,,,f-y. m .--_w. _ _ _ -.,, _. _._ -.____w,.- --w _.--mm__, - - _

l BATA SEET V,6 Spee. M45.M.273.0 f- ""'t-OP. THERMLL MONMORING APPeedia 5 Rev. 10 W *W ~ Skeet h et 6 0 Pre-ep Ise. No. M-1654 D 9 lanyard No. N:stiamea hw j . Stress Prob.be. - 2 D. P. 63.1 ~-~ m - 1 w .W IBFlWl: Us t.l W U. 15'_* + ** W 2.fFE2r 9 = Mwet. free computer output G =- _-.--d_

== Analytical Values

==: Espected Limite = -= Acceptable Limite -------- _ _ a.._ .- _ _ _, ~ _ -800 =. __3-: a = - 4 00 _. m.. __._=_-s.__ _ _ _., _.. _ _..__._i-_ _..4 _a t, ~.:=:s 4 00 .m o z_"_._._ .__... _ _.._ _s..._ _. a. _.._...__._.._s... e_.. _ _..... _. _ _.... _.,..._._,.r"._.. _-_ s _. _ _ v".___... 4gn _.. _... 2. " l__ _. __._. _.__.._. _. a .t, _... _ _ _ se- _._.. _. __._..-e. ..s, .e_. ,..e ._4 g _.-.m p,_ e_ e p h. 0 g g . _.. _...F.,_._..__i W _. E=._.__...._.... _.. _. _.. ..L._._ ._.3.._.. _ aw " ._u....._._._. _ _. _--._.._T ___.e. _3 __.. . w. _ -.., **- h _...- _._l.__._i_t__......... _... _i__..__.1 .g. _ t.__... _. _.. _._._._. _ 4 T""1"U3 *:"1.""T1_ _f" *'". *:"" t,.. '""J t *T"". * -"*1 [""11 111 tif ettttIl1ftll *llt's sIII.f

1 t'11*"t1 g el a t s, e e

0 100 200 300 400 500 550 R.F.Y. Taup 'F m r l .-- m

MTA SWTT U. 7 Spes. W5 M.273.0 t-Fu.et. Tup w1.tuertToarNG Appendia y 3,,,14 Sheet,,{, Leg 59 PWeer Assenstes/ System Beatops Pre-ep Ise. No. '4 1 M4.itev. 2 m'=' ' ' ' - m - ' " = ml manau-Easyard No.h IiGGD 0MDLY 4 ~~ 3tross Prob.Wo. 12 9.P.E M .i 600 g.

.suce.i.m.,..m. 1_su_=n.:n.=.juriss nu.mus

_m i- - = _ u=.==u= ' M = = = = =.u .=E EE Mvet. free seeputer output G . -.. -: ru _m. Analytical Values =. x=: - _- _

== 400

==: Impested Limits Asceptable Limits -------- i = a_.3 =.: g ~ ~ .m e ) _-L_ .,1__ _,._._ =. = _ -- t, =g = =..... _. _ _ 200 j=lJ".'""*.".

""1" _

s ...g -1__ l n ._.0 5 e .a c .n=: _ _ ww --a ...g. ,.... " " -."*;l=4 =" =:. t== - r_ .m _... L" =.': = 2:.".".':". = _.,._.t..' m- _. J _l-g

':" =". *_P ____ g _.

{- ...i__ - -I00 j p m - %.-g 4 g

L as

. "1." : : :'_""." "".1.;* ; _.. ...--*'".".'.".i." J_=.._... ."=:"_="""a.::".:" = - ; ; : .l*. 3.__ .... e -... g .g . g ...4 ..-.i.. .... -.......I. .._ v.. .....1 m ..t..... L.., f _ J .....t.- 9. ..._iam ..4....

4.......

....._l. -400 8 t....

3............

_..I._.. _t."."................g........-.................. -800 .;:3.3 ' ' ' l.*

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F m

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DATA SMEET U.4 Spec. 9645-N-275.0 t~ FRI-OP. THERMAL NONITORING APP **di8 U Rev. 10 R AT-m SheetMof_66) Pre-op Iso. No. M.icas4 thv.m Lanyard No. N11 G OO 10 cn Tws Stress Prob.No. Lt D.P. 64 _ __d -2400 utnten_um.._uu _im +,,- ~ nrner tme ._ r-- ~- ~~ ~--- ._.- ~.e EE Mvet from computer output G i_ _ -? -=_Anal tical values _4_ ._== Expected Lim 1ts - __ g'_.' _.- -2000

==- Acceptable Limits -------- _=_=: 4_ -7m'_ - h. +. -t i_ .__.__.t==.t..=_. i -1600 c 4_

=.jt.-- =_:-fr_ _. _ _ _ _ _.

c_,t. - - .-o _ :c. _ _a-- m .p. a _.,e, ._s__.___ __ _ n 1200 5 . _ _. _ _. _ _.. _ m_. o.-._ _.-...__,r As -800 .un l .C3 ._.._..._.._..t..__._._._.._a_.s._._ _ .__. __.__.___.a...__.. ____.___r..._ -400 ___i__..._.. _... _. -... _ _. __.. ..._r....._ _._._._......_.i._____._...l_._:-_.... _.. _ _.. ... _.... _. __ _...i_..._._. _. .n . _..._..s._..._._ . _.~ ..._.__2 .....___._.._.__1,.___........... +400 "!"l1"11 tillf il ""='T"in "". T"T". f* "U.... i. i =*. 1"":1.*:".*;"1.7 lit fif.tt ttttil1l[ ::s tt e se allt t i 0 100 200 300 400 500 550 R.F.V. Temp 'F m r-t i I ---.--,,,,,---,---.,n.----

DATA SHEET U.6 3pec. 9645-N-275.0 PRZ-OP. THERMAL Molt!TORTNC Artendia U Rev. 10 I M*D Sheethof M Pre-ep Iso. No. M-ins R tvs ,,,, v ~- Lanyard No. NM o o *D11L2 _~ Stress Prob.No. 19 D.F. &BS +2400 ist e:u i _u s o.. u_: r_e s._c -

nu C _m,. __ts u:-

-_._r_--

. _._.. p.. _.: =_

-3____

==. Mvut. from computer output O . u=, = 4_ Analytical values = __._ _._a +2000 E.E._E:Expected Limits Acceptable Limits -------- = __.J____. _ _ _. _._. _ _ _ _ _. _... _. y . _......_____g_____ +1600 4._- :gP _. _ y_ _ n_ _e _ = = - s g,. e 4 __. _ =._.___ _._ ___ _.e__.,- .S .-g _. ...,.L.__ _. _.. _ t +1200 E _ _ _.j _.- _ p. __ _. ~_- i . u_ __ _ e.. _ _ _ _. _. _.. __._._._.__.]___.__ _#..._t ___.._...i_._._.__._...___. _- _ _ o: _ i___ ___.,s,,. +800 a,. ._. _.,f_- .1_ __..... _. _ _. _ _ r.__._... si __.m._s_.._... m._._s...____.__

t..._.._

a. .._...__i_._.....

_1:.__. _

. _ _.___w r_._. _.. _ _.... _. _ _ _. _._.___.._._._..__y ..._i 4 00 gt_.,,___._.____ ___.__....._......J__.____. _i.__._._... .s-,._ .__s .__i._. _ L__..... 0 .._._.._.._.._.i._.. . _. _. _. t _ _._..... _ _._. _. _ s. t ... _ ~. _ _.. ...___....:__...s 1 -400 - : tmm:..-*T t r* : :- t-m.

n.1 ltti t.T *
s t.t:9tyl :ll-ei.'s ue

.f if 9 t'Itte e 0 100 200 3C0 400 500 550 t v. R.F.V. Tewp 'r m r l l l 1

DATA $EET U.6 SPee. 9645-N-275.0 PRI-OF. THEEtnL_MgtITOMpg APPendia U Rev. 10 I N Shest M of [ O Pre-op Ise. No. M 4 GE B FM v..e <.. -.. = ,i Lamyard No.N1i('ko M o m y ~ Stress Prob.No, is 3.y.Ctb t A== -1200 mesm.u..w_u me_enmaiu st-u.t-m __.a----<

==._;. _ =.

=

E Mwat. from computer output 3 =_ -n E_ Analytical values .c, .._ a

== Espected Lietts

=_, Acceptable Limite --------

=.:: t-.2_. - -_2 a-I ~ _ _ _....___ __.~_._. _- % f ~ 800 L_... _ t = _:"rf l ,g_. : 10#- ~ i m

=

5 _ g... _. _. _ _ _.. a e.e - _.y. -600 . r_= _._ _ __ __y...... r__. _ __~1_-.._ w_ _f___.__. g-. ,,r.._ _._.w..,s_ a -_e._.- _i.. -

.m _ _j. - _

s., _

.-.-.=.._a 4 00 m.,e ,n. _e ,t_- -. _ _... _. _.. _.._ __._ __p__ .s_..___,s g3 ..y _.g __._._ _. _.._.._._ _.... _ _ gjM%. 6 ..._..3.__-._.__.__ _ _s. c. g,

_...__._t_-_._.__.___

ss____....... _ .4 m,__.. .._t.... ,g _._3.._......... i .- s _.__ _. _ . ~.. g_...~.___._ .2._. i_....._..... .._._.I___. pr _ l__._. ..._s--._._ ......_ _e..__. . _......_.__.8. _... _.. J.. _1 _...... _ 1. _.... _.... _. _..._3 _.... L- _ _.. _.-......._.1 . __....I._ _2 _.._....- .._t.... _a_..._ ...._.i_..._...__._... ___,.._I_...g.-.._..._-_. ...._mp___ .g. +200 f. e'Id ^ '18" I t"" T lt1II f *, t .. _.g 7"tI*.*T"':7""T". f* :". *:"""1"""."1 :"...**":1.":T.* 1 ;"T I11 f 4.* 8 III; t f T H T 8 il' I e 0 100 200 300 400 500 550 R.P.T. Temp 'F m r

i l i DATA SMEET U.6 Spec. 9643.M-175.0 PRE-OP. THERMAL NONITORDIC Appendix 5 Rev. 10 N R EEAT-M Sheet M ef $ll> e Pro **P Iso. No. M-im RW 2 =.... imzau Lanyard No.,,glRoodo1.'D 1 Stress Prob.Wo. i_2 g,P. R gs

s=:1: ::

_= __ ittt112'llin.it.J:.s its.s!_. 2=p ***n IL., fl=2tta.E _ =

,5

=. ~.

""="_x.,

_: =_7_ q_.__~

=

Mwat. from computer output G

==s =._ i--4. _ ._....=_m

=-

==. Analytica va vos +1000

==._sExpected Limits

=-

Acceptable Limits -------- r_

w. _ _

=:.:: __4_ = o _e.._ _ _. _ _ _ 4. _ _

::-g: _----#'. =t

4_ _ a-: r,_ =c ; - - w _. ___.._~ w _.m..- + - - -_ * = = _ 7 ~~ .. _ _. ___.t _ _ ~_._ .___.g. _ - - - -_...__. g._ j _ __. _ _ _... _ _ m,- _ __, ~._ _ 4400 \\ i 1 _ s__._ g3 _.. m _,, a. p:- _._. __ ____ _ _ _.__ _., ..4

==_._. _;--__.._.__.__

+200 ..._-_.r_-.... _. s _. _._..__...__s_.__......._ _.. .__t..._..._._.._.__ ..._.._.J.... 0 . _ _.._.a_....._ _. _ _. _. _ _. _ _ _ _.._.___.i_._.._._.._.._... _. _.. _. _. _ _ _ _ _ t -2 .....i t f !*"."I*T* . l*.* *T"1"*."1"L"il O"31. T".* L*l.""Ti IP te f. 's t e ti f s t.1 ii 1 - i'itii'l*t r*I lit Iti e e.,i 0 100 200 300 400 500 550 e 1.F.V.* Temp 'F m r

1 1 I 1 8 ec. 9645-M-275.0 DATA STEIT M P Appendix 5 Rev. 10 l t-M *0Fe TWOMs WITORUG t ( Sheer M et h e ( Pro **P Ise. No. M -1 s c o p a v. 2 t m. Lanyard No. NilGQQ40{ 3L X

8

Stress Probopo. 12 3,y, 7p 4 800 e-itettaen _u.m.. u u _uis.-tez.e ,t w e._ em

== Mwat. from computer output G =- ~~' Anal tical Values -..a 4 000 = 7 Expected Limits .._.= _==- Acceptable Limite -------- = _ = _.,. -m -._-....e.. ..J_.m - ,1 og _.m. _.e.

1

.+ -..m._ __ =.; -i ^ p-_t= 5., _t_..-_....-_ __ i = --r: -2400 5 __e. =_ ::n : __ -.. pt.::.= _- - -i== --E . - = ammm _4'p .-5' -*.='."""t-eu

==.-m. a .-.m au .W. -m. m...

==. -m. am--me .m.-. mmm.mm. - emum --..-. 8 u_ a.-. + l l __.--e.-- l.. _ 4 .-..A _..d s p- _ _ _ -.u.--- -1600 m g ( i. a .._a-._.... __ - -l_-.4_._- e -. m

==--t. a......e..-=---.

m. 7

,==-.=.mu.. .M -....-me.--mm- _j __. .g _ a-3- _ g w. e. m.. g .mm m.... -4:".. -. ..e-I. e.. g..em .. m ens..... .g ..=....e M mm--m-- - = = =, = - -==.en- .-ms. --mem.- ..._..._......_.s.._- g--.. ...am-. .e... ...sm e . _W. _ . -....t m.............. ( .-Am .-... i.-...... .-em-. .m-. l .a ee o...m. mm..ee- -.-.m.. em..p - 0 -. m 5... a.mmmu ......*"T - m e. amumm. . enu .em e _._e. .... au..e _...--.m.m.mm.e.i=.e... mo. m.e.. e..mm am. amn

a. =.

-...amm. a.==a m. a... a . e. ..e es i,...m.m.. m. ummm- ... mo ammm. ..a...- -....e -...9

==m.e....a.... e. e. ..-....6.-5..m.s g..me _..,... -..I.--....-- i_ a. ens. eu-su. --..e a.._n an l a. - _ 4

e. e=amm.

p. - -.mmmm.

.an de.....,. = g.--..,- ]"--- -. ..-me.. 3 ame..e-- .-e. = =.. g- ...as

e. _ l.ame. e........

m an .e .e..e.. g- .e -m .m.. emme - e..- B..

e. xm-a

.e a--.- .eesm Q --...ee

a. m.

m...aumm....

4 m. e.s-.. e. .es .a... n e.. e a -........e. 5. e ..e e i ..e. e... --..e...i .'uman amm. e... g e e. .e . g.e am.-m .-m e. ..m.... e, m.. m.. e-mmmu e u em .m..m..-

e.. --mm an U

e3 -......e.m s e a=m= .e......... -a- ........ -. e a.u. a ..e..me....._.-. . amm

.e=

s .......e w .m.mmme.ee.e. e e. e. a.--. em. e.- .m.e..

e..mmmm mmam.e am.e

==. . au m. = eme. .a. .mm.e. a m ..- m . - mm.. - e. e. e.m. e. s .... j.. I.. a== .,,....e.e.e... . ame. - ....e . emm..eum. e..,- ..m. a-...m.. i...a-... ge... =....= =. =. =.. l ..-..e...e. a. o.... a. 4.e.. u g... .m i =-. .... amme an-... mm. -m. . i .a..e...e.. eme...me. e s. s.. .. 3 a**I e ann.- ..mm..

g.=.m.

... *e=*e.e.e.,e.-- 1 a . mn U.

==..m... .. +800 .._l e _ - ame-m em. am im.m..me.e. m l3.":'fM ITT flT e tI...... t.llilitT1 t hitifili s t' e llt W. nf711 tThnitril -- : - _. - e -...:..... .-J1f-':T'T. l r':": *:'"1-"T t =t i I21.TTl e" - 0 100 200 300 400 500 550 R.P.V. Tamp

F m

DATA SMEET W.6 Spee. H45-N-273.0 m -OF. Tusam t yperTommo Artendix e new. 10 (NUC'12A1 MAT-UF) gggg Pro-op Ise. No. M-1659 Rrye = _.... _. __ Lanyard. No. M ila004012L A Stress Prob.Wo. 1.2 p.y.M3 i === - +1200 ~ _ _ -. =. _ c, M=rmt2

.tx?t:.tu_LuI.i.U_u. &_-

-m Mwat.when F014A is open 6 F0145 is closed. =" E._E Mvut. when valves F014 A & B are closed O _EE@..-. C.... a +1000 Analytical Values =' .=--. Expected Limits = Acceptable Limits _== .o +800 y. 4 3 em 5 _ = _.... _ _. __..__a g ( _ _..- _ i _ _. 6 _._.=.;r < - -. = _ . y_.. _ t. _ _ t_ g=_ g. ..a i-- _-_ _.,J. g_..__._, _ _ 1 _ _ - __... _ _,....e_.-___..._ _ 4n _..._.,.,_a.r...-.. sa ,i. __ --_.._s.___ _1. ___ _ _. g .) _i ._.... =_ _ _ _ _.._.. ~_..__ #. ...C.._ I ...... __ _...c: .o .. r. . -.-..pd C.. s. ... + ^ w ....E..,... ..p mm.. y - _p... - ....d .A e. t._.. _. E e g.pss--... -- - ... m... .s fy .-.._ h_ J-i av lm e... --.I. .e. .-..3-r

s. e

.-M........... -...!........ pr..., aumm. -- i ... a s.- .,a_..- 6 ..............4 ,s... I....... e 4,.. -. - .. l.... J.. i n ....I .. w.- . U w......... 4 ..3..=..=... .a........... 4.g.. l._........ -........... .Q ....-.s. l e. l. -... -.l-. .-_l..... 8.. n=. : r t r =:= i =n-ru. 21. r.. m. p m ti r. n m ut n :: n n.. o i m p - .rn.m pmeo 0 100 200 300 400 500 550 .r R.F.Y.* Temp 'F m r

Spec. 9645-N-275.0 ' DATA SEET U.5 Appendix g Rev. 10 e g.5RI1m n 1 8 3 G i 64di mis 2 - "- a s on.amros, U.El' M Y s D IIr'sfaN[re M & 2 f5014 ~ me me. ,,,ome, /8 u =r pas-as unu runan demanumwa e,.se, no summer 1 PRt 09fE0.$ M 165S" 9 I IUyyaps t u nn se e3D1 hL L. w,w,, s a > s,.. I 5 0 E'XM1_fAen_pLaman eurprr I e 7 i i (,d)._, Ans.srica as.uss / ExMc.tto souttoAny units e is I is --- --AMEFTA61.5 BOAMPAM tatuTS i \\ II i l 340-l i / is i g I, # . I,_ :1 3} p. I !. 1._ I.._5 ' .11 L ;_i_1_.._1._;_! i A l l V, / te i i / i '.. T' l --. +, 7 2t' t i ~* I e s 1 l l .,l- _.,t _.... 7 / I .&.. _.!.. 4.j lE e i m ... au j,m; / 28 i" l +! I f es / T l l / / 22 l*L.,.. i.,:,.i _ l' / / n / l qi '~# ""e~~ / ,o }mf-H / /

'. =

s. / m 7 jf' / / m W / as 31 m a o a gg---< s--- 4e,--<..,_soo._4 44o ft RPVJEM9.!F I I l l t l I ! 'i o,....,,,,

DATA HEI1_.L{ spes. 9645 M.175.0 J FRE-OF. TIEIDEL NOFITORDIG APP 88di8 9 Rev.10 g- ' Sheet h et S O I Pre-op Ise. no.M-1655 REV. 5 muurinne m namnsansmas = l Lanyard No.FZ GOO 2UZ D _f Stress Prob.Wo. 53 D.P.M

8

+1300 - > - - ~_ Lunwus.anuu nu ~ ~w n. ;a uw ~ EE Mwat. from computer output O =_ 1 --"T.=J : =. Analytical values 4 +1000 _-= Espected Limits = =_= AccaPtable Limits -------. .. _. ~. _ h. Bh.i. _ I _ eb m ^ m.E. _.im. -.m.* .e N a w._. _..__..._s.mmed_ _--.mm.g..--- . _6 mme........ . muss u.ms. _ . W" .mh ee._ puum mum._ ums .m=_ 5_ -.mm. i =_e .m. 6 3 s_ miimmu um .mim N- .g _ 5 e M00 i ._.I.- 6 mm. m.u_..i ._i.EEm. i .anp _$ e_ W -.m. .mm. i .N N _.N .m.g l p M_,III*M. j u 5. _.m_m_- ._.e.=.m. um.m--... I _ e.n_-.._w; --M ..mm.*._ _..mm m .mmmm.

m. mum.._ ee_5

e. In.m*

.m_.e. 5 um e_ .ummmm. _ g...m. w es. e_ t*** M ei. ._.mm. 4 00 L _.,em..-- gh _ A... _ _.. _.. i .ms.* and .-.._."._w.. e -- -.. _- -. I. ..m.....pu. 3. - + ...I._.u g..._._ _..1-__m. . e. .m-.m.-. ._m(_ ......um. ...m_ me.

.u

...s .musumt =. .-e ..m. ..mm e_emmmmme w. e.~. .mu m ..=_mus.l._m._m._ .6.m_. e... ..mm. W . e.m w_... _ em._ j e....mu. .-e_..- I.. am. m.mm w..e _.im.me.i.m. sum... .me. e__.. immmm.=. mmune. - _ pum_mmm.. ep. .mmm _ . uusa. 0 w..... .e m.. ....ummm e. _.. _...m. .s_ ... s ... I_. m._. a .__.mm..=._-.. _.,r.. .......e... m. .e_ J .... _.m g.- g ...M m.. _ - g._ p 6.- g. _.ee

p. m..._=_:.=.

_.=:-_ j -. r_;;.i_m_.

u..:_- _

.. : m. :n..:. r. .uum...e_...m.-..-- .i e _.6 ...m. .e.. ._.... _ - - -..S.M. ,m... N .._e. mm . e6 )a p .mm .m.e .......=.._Ee.6...m.m.m.._._ . e.. e. p.6 - e. _e ._-e. . gnum. ...a e 5.... emp - W _e_ N4 m.. _._.N.._ a. ___..".4 '- 4. s_uus"77.'. F.~. m-- .m.... ..e m._. l . _....s...... _ 3. _..f.... _. _ L _.... I

a.........

.. ~.. _........ 8 __...._..._m..__.._...._.._. .....s ......:m :.- r. r-=: .... xn nm i.ar.um,-n, m termiumin, nisini. inmm nnom imim 0 100 200 300 400 500 550 R.P.Y.* Temp 'F m i e [ - -.,o.m - - -.,, - ~ _._-. ___ _ - - - - - _ _ - -,. _ - -,. _.. -, -. - ~

i spec. 9645-N-275.0 DATA SPEET U.S Appendix U Rev. 10 l9' T / &

t. -l l 83,

.a _ 4 i 4 ** un 2- 's a 1 un ENE*M Y E*T U r's d fI*e#PmIIT s 2

5016 me w.

m er /Z er n m er enn-as unu wnnu maannusos e,,ees mo s l t l I I i I aggp'JjgJ M 1851 lle'v$ i a 1 yy'yf,j' E 12 He30134.Y ' i a l i .b.9 3T ' 2Nsss_9Aos.$ 60 ' l l l l 1 l l !i l s NY ; O avsr_easar_.secam4_e.*r.nr I !e l i l i l i I i l

i i

i l l 1 l l(+). l ANAtNTicas. VAuass i l w Ex?f.C.TED Sodet3 ART uMnts i u

Acc.EFTAbt4 touMDAmi umns I,,,,

I l I i l l l l i l i! ,1 u I i 3// u l j I I l l l I I </- 1. i f,, i i i i i i i i i //f i i l i j l .l s W // / l

- w soo l

l e e q a e // i / !t j l i i l l T,j u !// l i(d I t i j !'I l l 1 l i is oo Ml l i I lf! ' /"',- i i I i 8 w i i i j 1, [f 20 l { l ( ~ E Moo l l t i ~. i l/. i I j Il l i i //l / i I '/e I j l l 4 j 25 Ti I i j l l J/ WI W! l = 3,, as g lI ll ff / l 1/ P'i l l t I f / / 'i i i I g4 ,o = 'g i)[ / //* 11 l i l m //,# [' m 3.. 8' JD d f .s rp fA = a Vf l 60 l , l l m n m l I. I d' 0 8 p go goe Joe ' , deo - , 500 a = !l l l \\ liI I i I afy_Tre@ I i l as g g g .an.

_._.~ MM REIT W.6 spee. M 45-N-175.0 I_ FRE-CP. TEERMAL W Attendia W Rev.10 ' E& W Sheet M of 8 0 Pre-ep Ise. me. 4145 4 RLVA Lamysed No. I.'.9 M c o Ars3.b 6 Stress Prob.Wo. gl a

3. y. A*4

+1200 ~ ums. rim _.iuo _m _ ~ ~a n.ca -._ E= Mwat. from semputer outpot G Analytical values _=.- ,_a i =_ . ~. _- +1000

=== Espected Limits Acceptatto Limits --------

=_

== p = g t o. E. I _gm .e g=,_ sm J_ +600 ,_.r_ : _, _w- =.:=.z = 6=-- . w =_-i=_.._ _.__!. _m A 4.._ _-W:;m r_ 4400 ,__._._m

s. _ ~ _

._,e. _,. _ _. _ _ _,c=.._.__.__..._..__-- sa, ..._3 se,g ,n,g ,._. _ a , _ f._w._.c_ _. _g n_.t._..__._.___ .. _...... 1.. +200 ,..4- _. __ __. _.......=.t_. __l_.__. r_ ..___..s_..._. _....t... .. ~...... __..s..._. . 0 _......s.__ _._....s... _ _. _.....__..._._.0_... _... ....._.s...... _,_._.._.__._._..u._. ...a. s. ..._1__..._.._...__._..__._._._ -200 q .a..._ e m n rmffTrti fm:n.rt Int-sz1 rzztpzD.*.m1f711 11P f 8Ti titill11Til fi t t ill o i s t' e li t il' ru'11r;T) relimit . 0 100 200 300 400 500 350 m.r.v. temp *r m --....---. -c-.. -- ,, - -. _ -. _,.,. -., _ - - - -. -.. - _. _ _ _, _ ~

Spec. 9M 5-N-275.0 DATA SHEET U.S Appendia U Rev. 10 t- ,e,..,,,[vhb%214 .,,.z-W - % . R AL al t41n o,, W::l'8lft'l m,'8lifL*Rit'I a 2 seoss ~ sumact putt - Ap hr#M Twssmst meama ramma gessy nsa /8 OF J3 I N t_:0 0-. RL_g M'-ICC& t L d App' Ap 3 j' E/Z'Gd/S~dMiY l 2lrntsi_rpegj l 10!! I '.a.9 2 Si l II i !ll j i h riva_py lpge u pas h g4 ' perpyy; l l l 7 A l !) e n , go, e 3 j .- At4AL1TICAL VALA&&b ![ l l I,, EAPEctED g>ouM3ARY btMsti, f' l so ,o I-----AccserAn,i.s sounsAsv umte, i / i i u I I I I. u i i o i i i l i l I i I /< if i i I 14 l I l i iI l T / u a ii' I 'l I 'i I i j/ fi l 13 p, ~i l I I I i I i 1/ / G i' i = Ml l i I // / I' o, l n - i A I I l' II /> /~. I) I = TE ~ l . I i i l i -l,flf . / t- #i i = II //' f M I Ti d.. I i = i i i p / fi ri 3 d. !i / >~ / / l = = a

n/

e l/ K / / = .,s. __E / W / = / ) W = ,,e ' / p = = ' / m. 3 II [ W 31 I n 'en s O up ame see 4po soo N IddIOP_.N m l -.wi ions

area S M T 5.6 Spee. 9E S-N-175.0 ru-or[ mmu immpazes Appeans a see.10'

~

wtaan mg ,,,,,,g4,, go .1 i Pre-ey Is.. so. M-tss's Rcv2 asaminus wuvener, ee Lamyerd me. K12Gottet D w Stress Prob.s+.

01 3,y. _pa W:

M200 = ummu.u_n..t u-.u. i_dL-m +- Ce 1 =:=. EE Mwat. from coryster entput e -+-- _ _a _= as t as a mes e +1000

== Expected Limite

= Accoptable Limits -------- _ - -. gy __~_ g-p.l. _= O ge p .m _._.mm.mm .m ._.e-e.. _..--m_ mmm. ..._e u- _6 m_.-- .um .._ #5 .m i _e.m.. i-. _f. -: ^.. 9% _...._-m.i q_ 'e _M .p. _g.-m ..m_ mm.. .mm -mem. ~ ..m mi MN ~. - -, ~ Py' ~- -. m -l _m W .5 . _ -===_-m.e. i -p ___g__ -.a_=.i __ q-_ g _g.. .- -.e m ...... = _. m. .e. .h. hw. _ _. .... _ ~ - g g, ._ _i ... F". t .mm.mm_..._ ..-.g6....M.m._. -... M.

=

_ _.. '.- _ _. _. _....-gp=._' 6 -.M

=

==- __.!=. 6.- ....m.m.m.m.!_........._==_.*-.. .e . W.._M.-_ ...i.. .M. 6._. __... ._.m. .mm.mm m_m...M ...e..mm.. .L.-.._ 5.. M.. .M .u.... .e .m. .m m.m.m. m. .....m...m--.. m. do. .m. .umm _ _... _.e...m.=.m._m. .e _._.mm. .m m... ^.mmmm .ee .m -.m.m... ...u.m g .u ..h eu.e_ _ m. e_ e e s .m.-...._m.m.em m.. m. .m _.W -....uem M. Me...... e...n WW. ._+. 6 e- .m_ m

6. mum

g. m.-

_..m amm G.- 8..W. _M.* 4 p. e m. .m. e ..e6 66. m.m 3m._ e.u-. e q..... .m.-.,. g. m ...M_l.6 6__ -..p ..-m. a ._m _m_...._-i-..m.._e.e... D E. emmmm .m ..e._.e.._6 ....s .m_e ..e.....mmm.._.mm.. .e . a ..m ._..u-l ...m... N..m..- m -_0 .M. ..m. M. W W. m ..e i 1-- _.. _. _... _......._..t...._. ...l. .._4 ...I..- t... t...... .t........ 2...... .l.__._._ l . o m nn nTrt. p r.:.4......., un pna 4.;W1 rm EtiTHlis11111ii rnitp.o. pie,p ruf1f;T1 f fi tir.11 O 100 200 300 400 500 550 I R.P.T. Temp 'F J m ~ -. - ~ - - - ,__n.,

DATA SEIET 5. 5 Spec. 9645-88-175.0 AppeedLa g Rev. 10 L: 4tr.m::Mem.catero ~# S A L ,. - W 4 / f3 W e- %5 ~ .n 1-t4-t 3 ,..u i I1

F %3 me
- - - - " " " ' " " * " * " " " ^ = =

aneeet no i \\ l s M a-as 11_j, M 144 dyygj,, el ar t2 Sc't 9 0:!D J l a .nVakd.r'nea j t all l n.o 2 5 s l I ( O mm raen m.mm mnr e 7 i 1m e ~ --ANAL 4TICAL, WAW&b se EgPECTED touttDAM Ltmgts _s n --- - --Acca?rAmLE sounaAav tmits e '3 l s ,y,, ti i / _ ,s 14 \\ I 16 I s. i -Q ,r is M: y -.I l g i 1. l l-gl t, l .m .e 9,- .g, . 4.. -.,ii' l 22 2' A !l J,o f c y 9 i = gy I a g g 'm m s 31 .- ye INp 6 O M D og Jie 400 m N APV 1 f$'# 'E8 k m ePD tatt i KIB

1 BM IM_ W.6 Spee. M45-N-273.9 y. Pas-ot. immemL nowrvoazza Appendia s ano. to W

- W Shes$et SO J

T .4 Pre-op Zoo. 38. M*IssK k.M Lanyard - No. Ettrao1504 DL1L Stress Prob.No. iot p.p. 33 =m +1200 -l __r-- mrim _w n. _u u m ' - - amr 1 i _s E_E Mwat. free esapeter output 9 4 ~~

. Anal tical Values

= a +1000

E: Expected Limite

-== Acceptable Limits -------- _== == e ^ g , _ W. _ l _. =. g __ =: t t i t.__.._ _.. _. _. _.. g a .g e. .___-...__1__ .m- +200 a_z _m .... a ......_.v _. _...__i.._.._,

n e =..._ __. _.. _.. _..........

_.. _ =. _..._ ....__i.._ _ ~. _.._i._.._.

i..

=:. c:= __...... ._._i 0 _..,......-m_ ...._._a_.. - m__ __.s. _ _.... _1 . _. _.. _...I.... ......t...... ,_.._.____..........___._r.".Y_ m....... __l.._._ w. . P. e.,,. __f."."__. 3.... _.. 4 .......h._ ITTrt23 fTI3fffft : ff tl".**.g21 Ir71 Ert ciratizzs.*.4ttirITI IT1:f tfilltJil1171# ft s t elle. s e

sit e tt i l'ir11., f It1111:st 0

100 200 300 400 500 550 R.P.Y.* Temp

F m

.~. Spec. H45-N-275.0 DATA SEET U.5 Appendia U Rev. 10 f.

M m

IIIII'MII' dei *eir'sIIIII D a a/fl _e escasoII~ ~~ 9 SLL J///

mes 1 83 J

use

5036 j

mm l0~ o'

EE~D*

NNN '"M **^ L * * * ^ * * * ^ * ^ *

menEt one

. numacs J l e' f*l1 Cr.I: llll C v. S Nty02 ]4 9 / LitM.1ME S p' E'14(a 018 04 DL4 ! i I 5A'S I 1'rANSAJDACB$ 'TC2 .a.R III III I l i i i urnr. i I O Avsz !caen_we.ina l1 ! I i i j l l j g l a i l AN AL1TL CAL VAktAtb l se EEPEC-TED todetDART 46Mith !l l i si - -- - - --Ace.orTAsts, m.ounoAny umns l I 1 l l l 3 l i l i i iI i i I i i i I f i i i I I I i i; ~ l i w I l l l l I i i ss N ,e l i t l I i j se J I 17 E l !i3 l 1 i l I i,1 l l l l u w i l l i I ,o l l l 1 l l7 r E (+ ) l = -*J, 4 M, >o- [ E j h / j D p= ,i / = l w l m j - u 4 b p' l f Y O p f, &,f' ,s' / l m m l I I = i l l I p f.g ~ - af, i- - T wr; - i po; = i -1 io< '- A *1. 1Ee* *F 2 i

am SEET W,6 Spes. H45-N-275.0 f. PRE-0P. TEERNAL SERITORING Afteadia g Rev. 10 c - im a urar.ar) ,,,,gg,,, go Fre.ep Ise. No. M -is'ss R Ev..n Lamyard NJ. K12GO1EOdtLM ~*~ Stress Prob.No. 1o2 g, y,1 M i +1200 unriwi _wu..u.nm: - ~ m nermer ertimr s i = levat. from seeputer output G = .-4 Analytical values a

=== Expected Limits +1000 = Acceptable Limits -------- e_, = _. t_ _m._.. _ _ _ 4 00 ...i _3 e +

i. _... _

M00 5 i

=:

.:l' __._ j j i .._ l ___._ _.- -1.. _._. t. _. p, ._.____t-_ 1 ,_ __ _t. _ p _e_ i ,m 6 }._. y 'l . - = =. _ _. __ _m sa. _l ...m.m._-_e... i _. _.p 3.. ]_ _.i _ _ .i._._ - -.. _ _ _ .m.._ _ar... _._3.__. y 1.._. _,. .l 3 .m..-.s..-.I. _...a.i. ..m. g g, ..md. _ .._,___.__.m. e ..e.-._.. .... 0.. un..._ ..e. -.m_-. _.m_ .mmmm. _mm _. 5 ....mmmm ..-_..mm e mm. _ _..m..m.g ..a_. m..mm-.__._ m. _..._m. ._e...... _ .... as I +200 ....l..--."p.._. l... _.. _..1 .M%..m h. [ mmm. p I mm . + - _s- .. w l _., l

t.. _... M_.

I -m .p ...- 4 7_ l F_.mm.. M p .mmm.__g.mm ymmmmmmm m._...0. ...e ...mm._mm_. g._.... .mmm._.m.. if .m. -_..m. g_.. _ _ m. m. _ I.mm 3 _ .m .m. i .m _..m. .e I C_ _.. ___.__ .._-l._..., _.....

4..

...-5_....... ". -- a .m_.... ...,...5-T..". W m _._._.8._...__ _ _ t. t n _..._...... __J__.. __. :2_... 4 ._.._.l.... ....s.. _.__l_.___._.. .m.__. .._ a..... I _g_... _._... _.._....,__._._ _ g_......._..-. t.

r.. _.......

-200 t g............i _.__._._e...._..i_. "WT"L 3 f fEl.'T"T1 ;l f'".: 'T:T1 :m":'.1 :T31.'TD.*.41lr1 T"T11 tTt fif o l g li g t j ti g l_ 't i t e l p i s e ' i ll l { t i fiff11'lT1 ff1 lit it i 0 100 200 300 400 300 350 j j 1.F.T.* Tamp 'F m l r ~.. - - - _-m,_ ..-_,w--,w-

1 S ec. 9645-N-275.0 P l r-M TA SilEET U.5 Appendia U Rev.10

SNS4L '

use-=i]H lf) _ oesu n 0 SkO M use Sm'\\\\'03 enmson INO NII' cTr'sNE$$s E!*Is't if026 - no, emancy N ap 3.3

mane, par-as muu rmsammi menanum wm eiseg =

y PRQ09149-O M*' csk Rl,v s i 3 a (, 3 tj yy4j,3_j' lEsa Goh6miCy ! &phss_ppog.yl I i103 .p.9

t1l a; I l

l l l l l l l l ;# f j l l s l ' O E v s r !aa'e n' eqeepyyt,s.4 ' /

d l.l l

l l i ' /, i i ? ot ts u, e i i i I I

//i

. - A,q n tg r i c a g, y g m s g l,' If i j l e sa o EJLPEcTED bdhAMDART MMtT%i l si [ 58 u -- - -ACCEPTAtit E SouMDARY U MtTS '[I l l I I i If/ i u = 7a o I i.IiiiifI

)D i

_j i I I i a i lI i l l li f l w f i il u I isa? I i i l i 1,1/1 I Ii y 1 --c = s I l I, '/ !/l I iJ l I i l n t i I l [ l// Ai! '/: 'l ~17FF l l <ff!I I f I f I.A I l a i I '/ y\\ /.t n I !l \\ -%ft /Y l/ ]/ l l 8 l so FF e i i 3 y l f ,f f f 3 l s ( / / R a s {' t/ / s' ' 9* a ,7 c I // = y / // =

i..o f f, ;,

= / /' ~ ~ = f' as los at l l l I = \\ O W A@c J88 408 l l #00 l l 680j = i 1

=

vs a 's.W 6 i

4 I MH REIT W.6 Spee. 9445-M.275.0 t-FRE-OF. THRML DEErITORINg Appendia W 3ev. 10 A Mafg sheet-IS of 60 Pre-ep Isa. No. M-1 cgs Rtva = - - -. Laoyard No. t to c.amarmw Stress Prob.Wo. tot 3.y. nur i ~ NM ume n i um.. u_u _J a n-++==

* * = > + + + ' La

a.. _

~ l \\ _EE Mvet. frem samyuter estput 9 Anal tical values . - -.r +1000 = Espected Limits

== Acceptable Limits -------- o .i. _ _ m_ .=.7 M_ ^ + - -qsp _js f_._.._ --. t.. - n +430

-..4=:.-

_ _t, 4 _... -A .=. : - _ _ = =. _ _ =_ ~ 1 _ _ n e.. _-n _ _e _ _.. g. _ l ^ l _'_ _,l..___g_,_ -- TEE==_ M-H _ ~ ....s.. 4 00 .g___.__ ga. .._ e _-.-_ _. _ s. _ _._ _- s i _ [#'_'==p __ i n, 4 ...e.. _. _. _. _. _.._t... t200 .._.m_c. ....._.t_. 1_ _.._.i .__.g,.. 1-. 1._._ _ = _._r_ _ _...._......_..m_._. _..8...._ e.. 0 . _. _. _..... _ _ ___ _ I..._._._......_t_._.. 4 ........_4_. 3 _1 ..... 3........._.. ..s. s. ........a....... t........ =, _. _. _.. t_. _._. -. _..... _....... _......I___.. t. . _... g ~~nTrtritmrtfrie fT=.:tytt sm m :220tm.*iWirTT1 f71 fIDifItiliffti 't iIilI h e e 'I!I t iI' fif11*iT1 If1 tll' e 1 0 100 200 300 400 500 350 R.P.T.* Temp

F m

r n.

Spec. 9645-M-275.0 DATA SIEET L'.5 Appendix U Rev. 10 g ~' ..NJ M n 2.. I1. s 3 G s &di un 3-u-e2 IIEi'85ffn0lT*.fr'se".fli.'83!"I a. s

soas 22 os u me, pas-as unu vnssnet 1

I I I I i i MLid 70' .I I Mi-op_Jio.g, E i L3M.YAA3.2 p 2 f,or,s oh sty 1 3 i l i l I .s7488JfA03 p i 66 .a.R ao' i_ i s i l l l l l I i l I I I ! I W L i- , O yyggeq g,,ipn g p,.per e L l i I' i !u I I i I i ,ei i I i l l I 1 i j I e-l l l i i i i.;i. i i i I I so l l i---

AHAWTicAt 9Auas,s.

8 u i i l u rst.TED enounu ny u w:e, i I - - - - -Ac.4.s era am s o ummy um, e, / I I is l i i l i -l 8 i, ., e / I i iz ,.< /- I i i is -- W i ,/- i -.-y ,/ I se !a i --e - 9w-i _ r /, f i n .n i is i t I i i l t i l I l i ,, '/ s 'g __. v.-__ 8 i i=.7.. /,. /' i i f. .+. I i .... _' _ i i i i i. 1I i i l l ._...t,i ...i._ _ _., i < m 1 I ,/ i 2 u e t l I l i / l l l l l }/ l l _..= ,} l l l l l 1 8 gg i 22 i ~" Pg Y l l J l f. :' I I I = 1 l l Y / X,' ' t a'.L l = ~t~ ,y /,/,' ~ = ,/ /l I = ~~ f o' A' i l l n = vf f I , g s \\ 1 m V AJ m l l M l l 1, I I p go aoe Joe ' doo ' l 800, i 1 888; = j l I apy:_ TEMP _38 a l 0P0 1321 18/75 i n. m --+--.- %w.. ,.-y--_-----..m,-w.-..w.w.. ---...,.------w .m%. -, - - - - m. m..,.---,,. ---m.-

RAM SEIT W.6 Spes. M45.u-275.0 f-PR2-OF[ TEREL MNITORINE A Pendia 5 Bev. 10 P MAT-M Sheet M et S O ers, s. M-ism ma ennemma g pmaremensam z Looyard me. EMGoise2 tw - -~ Stress Prob.go. 3.y. o +1200 a.ms w o.w._ o.. u._u .s m -++-r-semer = -~ =:t _ _ a. EE Mvet, from computer output 6 .. " ",. " ' ~ ', EE' Amelytical Values +1000 EE: gapected Limits EEE Acceptable Limits -------- g. g ._ a_m. ._., a J _w = doth u= t 4sm: - :. = ;,e= = - +400 g__; _w ar _- s.._r.__ _: _= ___.-._.__-;~_ _.-.__

l

_._ i _ _ se . 3_ _ t.. mi. _ _ _.. _ t _.t._._._ i s._._ I ...._s...._._._ +200 . _ _... _. _.._...._.7 s. _s......._.._..s.. _._i._.._ __.m_.. =:=z== ___.. .s _ 0 _...___t__.. = __ _n_.._.... .._s............. ._r _....s.._ .. _.t _. ..__i._ i i. ..i__. i "turt Ultm #TTrf i f*=: u n u i w nq1.III.*.priITTI 871 :ITaIiti1111fIl 't tillIe ie'ItIti!' rusMT1 IfIllittt l 0 100 200 300 400 500 550 ( 1.P.Y.'Tapp

F m

DATA SHEET U. 5 Spec. 9645-M-275.0 g, Appendix U Rev. 10 on,o nary >%m f cars '2-t '5-9 3 catcstep cars J/M'/N Stabo O&2 @A0 pacascf Jos me. m es 9lt E - DP NNN THanMAL name van rAr a engasneo 3o er 33 l i pqg.0Pg9 hi l[Y[Id a = - i ' t w_ yan a p\\ nk s'ao1461os V I l l is A lim a,p 24'3I ! p a n _r' os y l i I l l i i i i i i i I i I i d ii O nsMr_'eien ambe.id earnr i I I I I I i i !,1 l_ l 1 i i i i i I i l l i j i i 48 As.sn en vas.as s io DMctso sounnamt umrt, I ii _ _. Accemun manaa.x umre. I -- (._) Tiit i i i i n i i i i i j i i I i i i l u i i i i l l' I j i l se i I l is e i p.._. I I I i is a I i l i i .....e i tr E ,i l i i l -..v.. I4,, [ l l te l i il i 6 i i- __ j i l 's i i j .t 20 E i l l l i j L' -.,i l I i l a. .a i i ,I i i l 2i u = o a i I i i., ._. 4 .g ___T_..,'__...I i l l 1 l l l 3 !/. l A M. 22 i N

J bac i

l .I h l l l[ I,[ i I l l' -- s l __I E I /'/ l 6 /,,Al ,, raat m L m ~ rr l ~ f j AM / W l / A l 2 ~ ((j q l r se r 1 I 9% s 8' I, i l 1 l as an O MD AM Joe i 400 l #00 l d'c o Se l R9V T W 9_W I a ,,;,,,j

1 BATA SIEIT U.6 Spes. H45-N-275.0 FIII-OP. TIIERMAL MWIITORIIIG APPendia W Rev. 10 l

**W skeee.-[uket GO 1

j l 4 n pre-ep too. No. N-MM A arv. 2 m m m m aanpi-l Laeyerd No. B EiiOZ4 01DL.Y I l Jtress Prob.No. #3) 3.p. 243 =* ~ 2400 sane um.. u u f =_-===. swratt

== .r-i ..m. ..m = = Mwat. from eemputer output 0 = i = Analytical Values -- - -2000 = Especte Limite -m 1 -= Acce table Limits -------- 2, = =p=-

== i } ~.. e. I h . ". ". "....... M.. -... 5fi. -w - -1600 M.

'"* ""1 M.

t .e--.mm. .m. --.e.- M. -m. 1 W-4ll.16 . es l d- .= j ..mm- = _ _.mem .e-p._..m.m. mm ..m.. m__ -1200

.E....

--g.-.. ..----.E s --n----. j ....-.U..._..... I..-.m.--- - N..".M ' M,.id.r-i..m. .e -q-.-.

== m.- - ..mm -_..1. -.. _ -.am t.==. 3-g -= __g. ,ggg 4 mmm. ..e - -.s ..~......-_-.3-- - mes.. ..~1----- s a =. -.. -.,__.. g, w..!.- .....m.. =. m 2 _...,-.M.. . = =.... -400 .g....- --n.. .M.-.- ss -..,.-.mm....... ......m.- .m. --.I 2 p ..p 5..... -.. a.m.m.m.... .--m-.. ..-,_.._..-.a m.s . I... b....... .= .1-.._.. -.. -.... -.s-. -g s a. .. = -. = =. = * * .m.......... .=...e. =.. =. y ._ m_..... g ......I. . i.-=.=.=.. i.m-.. .m.me.. w -. .m---.... -.--m. .. I. I. ...m............,...... ....m..... =n.............. ... - I a -.... ......n .....mm I."..*. .m.... m.... -.. 4g =. - "*L"1Tm."T1 ff"FT : ff et.....i E". I*""J 4.'IE:.*.;"]I"11 til fI f.11 It11lflg ii1{tt,eeeei1Ilt' fif:1T111' 0111Fi1 0 100 200 300 400 500 550 m.t.v. Temp *r m ,n. n-n.- ~ ~ ~

DATA SHEET U. 5 Spec. 9645-N-275.0 h g$ - f-Appendia U Rev.10 N-Date J88N on,ci ayon 1/ M, .21 f oate 2 f 5_B_I cwecsec Nr $ nW if024 &2 Joeseo. peoJacy oussecs tents-Do nauw rusann ma ranwa enserneo 3* OF 13 i ( l I I I l l l l l e 4 ' Rat..opJie IM - \\ 4 M tif i I L AMyAA.B __.p' ad 3 3 doHdl DI.E ' 8 a i [ l I i s.rnen PAQs.9 ' 15 8 I '.D.9 'T s A l s i l i l l l i l l l I i i j d i i i i l l ' Q_hivmdaear_,cempeyaq _evrfer ' l a g i ? l I l 4 AM AbMMb VAbnAth e e l I 1 .-a e ~~ e i '. ~ ~ EAPECTBD boue9D AsW Limsts l -~ - - - --Aces TTA%a e,onoam 6mirg j g i; u e i 1 i j e t.:.c4. s 'i l i l l 8 u 'I te 8 l l is i i _. y 1 . _g s,C.- 't t i .v. i l is 4 so E l i l -~ c; 2s e.n s .. _ _ I n 4 -.s I i 9' m i i e i i l 8 7 _._. se l l .,, { l l 8 -..g-1A_ _... _ _. * .. --... y l_. - i I kJ II i _i _ ' Ii i 't i i i i i i

' [ !

I l l l 8 .I i l.I 87 I ~g i i i si-l l i 1 s m e (' l l t __.#

l i-I.!

l l 7 __ t 1 3 ~ y' r_ l l l i l l N. I i m I 1..r s l l l i ..l..e-__.____.__..__s, l l l l Il l -.i I l i Il 8' J I i l l l l l 1 2 L.-x i [ i i i ll m 8 0 loo 1 200' i ! Joe > , 400, too, I l. L i _a_.I.!,i i l i I II Arv: frana.v. i I I I i l I I I m

iij i

i i nao.i n i sn.'* I _ _ _.. -, _ _ ~.. _. _ _

D N SIERT W6 Spee. 9645.M.275.0 rRE.0P. THEIDEL letTTORIIIG epPeadia U Rev. 10 OlUC12AR W.AT-OF) sheet et Go H 1 Pre, see. No. M-I6968 Re v.1 maggg y c gi1 1 Laayard No. S M fr Dilo1 O L F J Stress Prob.Wo. Mg 3.p, it A- .=sras +1200 j ~

=n.i utru.ris.we.w. n. nwa -

i = - - EE.i Mvot. free computer output G i .._aa +1000 Ana 1tical values _= Espected Listto Acceptable Limits -------- = .) 7- ) . ~~ __..._.._ m. -- +400 _3_ A +600 i __r _--. _ l __ _... _. _. -. _ _ _. --._i =s _ _ u_ ._t.._._. r. 1._ l- __,.___-.____s_. q 5 ..t.__ m__.._ . _.. _ _.. _ _ ~ _.. _.----e. a . _ _. _._ _.1____ _ __i_ _ _ _ g __ t. a. _._ a. _1__ t n .~. _ J.. -1.._._ ,I -.__t_-_ _~ ~.....-,,u +200 ..._.. __.: _ =g ._ _~.... .._.s................_ ....._._..__-._,.=3 __a._...._ _._._ a_.t _ _.- . _.. _ _....L. _ i a _6.__.... _.._u _ _. ~. _ _... _. 0 _... _ _..._.s._.._ e - _ _ _ _...l. , _ s.. !....... __..__ s. -....a,. _t_ _....._.__a _.. -, r_. i 3_. _..... _. i w._. .='-==.l_._I.. . = =....=8 ( .g....-..... -.. _... _ _ "......_g

.n._...

._.__I_..___......... b.e - .g l l _....._..a.i....,%. I e r... t. i, _....i___._.

eW

.4 an,,. _.

- I*T.'*1f.23.*1Tf'1. (m*I:3)*Tr=1 trif r3=.= 3f33.*.HI1(TT1 I?t.f #f stitif ttiff elrttilet t'e ss'# tilli fTf42 f f111s il

..3__.._. _._._3.....l ..I._.............. 0 100 200 300 400 500 330 m.r.v. Tem, *r m - -. - -, - -. _. _. _ - -. - _ _ -.. - - _. -., - - _. _... _., _ _. ~.. _ _ _ -. -

i i l

l s

DATA SEEET U. 5 spec. 9A45-N-275.0 A edia O Rev.10 , A.STL,,, 2l w n - ~ a s u-u,. s-r-as j M:U'8ltf*imir'siifL'8"Jt"I a n ssoae ~~ \\ ram-no uun vunnan mamwn me,no 1e or n a ) m es_ 1 9)ti..ot.1EL_b M' 1686

twya\\

si am im eo mit m, m., 4, , m ,,,,l l 1 s t 6 Mwaw paen sampet na seire'rr _I_, 1 i i+ 1 r [ --AHAtyti c.AL 4AWEh so St l l EMEC.Tp a.ouMDAm4 units. r 1 ,--- --AccarTAsts acasAay umsvg i / r j pe - I. 1 13 l I J 1 se l l / Jl l l l l is 1 b. i i i i l [v I c / i et n.. te l l j r. --. 19 3 l r, a t __e _2 -- iD l* l l j j_. zi

_m.

1 i l E

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ptvat when valve F063 is open ._ ___ ~_ Ptvut. vhen va ve 63 e e osed m e _--n a +1000 _& _. ~ _ Analytical Values _5_.. :- Expected Limits =. e _ _ _ _ _ _. _ _ _ _ ~ _ -- Acceptable Limtts + r t- _.f:. ; i__ _r e e.._ _-_../_, +600 .___.__i____ i . +. _ + _A __s__ s _ _. + t_ _ __._ _ _ _....... _ _ _. _ _ _... _ ~ _ -~ _ _, __.._._ _. __..-__..._ m_ q. f _ m _.._s.__._ __ __ _ _ _-..g _ _.__..._ _._._......_..g_.g__ c==_____.____.._._.+_._- .A _ _ e, _s.._._ .e 3._ ._...._.. __. _.. + ( ..__t~... _.. _ _4_r __t__.__..___..._ __.w__. .. _......... _ g._._ _. l ..s n.._.._. _...... ._.4 \\ n_._..._ w.

1......_

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'"1 E"t t:231. T".tu)""f1 sti f t t.* t t l111]t ti ':: :te is e*le,t* "t f1] 11 IM pi et 0 100 200 300 400 500 550 R.P.Y.' Temp

F m

DATA Sur.ET U. 5 Spec. 9645-M-275.0 ,$I ippendiaU Rev. 10 z/i4 /rs, mA~ 2-m-s2 .no = ....r IND'MII'mDIIr'sNEI5 *83!*I a n fIdaP me. c, ,,sa c, npan-ar wun rusann maunoua e, es no 2L ne n4 1 1 3 M J1J 'M-15 75 l 8 ta as j #i ts lMC45491)LH I I d4asj_p5hp [_ 2 2 di I in 1,M l l l e I O M y eer._ r p M. ca m m sa se ' E' P i 2 i a l iI I I I I I s y / I~l' AMAmic.As wAsuas e m to EAPGC.TED SouMDART kmg% i 11 - --- -ALC.EPTA tibE bo4MDAM blM tT6 j i i-us..I I I l l / i n l 13 14 l l l n I 1 i l l l 'O --- _11 &.. p 1. _l gl g a

_a _

e . i t...i.. i, 3-- i n q ~ se ~ -.-.J g,) 1e Q l Qw#, r r r i =E I m r ** ,6 ..i_ ...i,i._ l l l l si __,N. M _j l

4...!

i l l.. as N l _'_g._-i ~ ~ t = c t E E i B "I T 8 1 l I as l m at -Jaa Im 640 l o ga g >e se 400 m N l R P V _TEP'?_*f l as g g g g -g po tali

nata surrT v.6

Pee. sens-n-trs.o

~ FU-0P[THERMALMstiT0MER APPendia 5 Rev. 10 OaAa mg sh e44.t 60 I l t l Pre-, ree. me. M-1675 REV4 -*~ Lanyard No. E %IG OO4 SA9DLI Stress Prob.No. 28 p.y, 4Ach i=== h- .m ~. " -1200 _r;- s,armsauswi e -encrett.ru- -..m W Hvut when valve F0 EFis open Hvut. when valve F063 is closed d ~_~ _, - _-. .m.. ..mm Analytical values _ = _ ' Expected Listits ' Acceptable Limits O -800

1..

..m n 3 ~ _e_-_e. g .a.._-... - ..-e._ ,gg lu. _.I--4 6-h e.U E- -m-6-. I-e m.j N-e-N8 6 e.. .ee .m.M. .6=._- m.m e.- N -g, M -( me.--.-. 4 - -mme - - = = - -...l.umum. h em.m. ..-==maa-a .mm .. =. 3 amm-. - .e..- e.amem,, - = amm -3 a-e u.. e.m.. . asum-e m ams.= en M ..Nm _M M 6 -. _ g _- _ .mm- =_==e_-...e_==.= g __.>-,s-..a.m. .e 40 ,m. a. .u-..._ m -m..__e. .-.e.-- cb m ..s .a-.u - __.w-- .....-.....m_. _-= .==9.-...-n. 4 g e-5 .-.e.. ass a....a..mm.mm

d. e-au-

-...-L ..e_- 3.m.us.. - a __ = mum. - -- _. \\ .m.. n ..._..._..,.._.a..am.i...=..=. g . = =. eom.,.- . =...a. .l.--=_===== ems...... .e-ea ..o. . am .. -umme.. ...mu e--me g...o. am.me. e.m.. e. m ..- e -. asum. --(- a-

a. e*

..m*. . enum.- -m .m e m. =. es.e. e.. am.me.... ,y am.... e =.=.m.

== -m---- e -...-a--m-m em.summ amm.. e -.an-. n- - -..a-me ene.mm e... em.. i e am. .-g -.. e - .4..e.._ m.e s amme um emunu a. e e...am. -200 .m..my ... u. e. _a.m.mu.m

4. em.

m. u.mm..am.m.m.. s_u a...

_m., go.e.. e.._ _ _ emmmma -e. am we. e._. _, _....ammm.. .em. e....e -. ammm - es....ee...e..m.. .a .mmm.. e -.am...

e...a-e.sse--e - 5

_. wess i as-- .Ie.e.-- .p g e.. m......e...e.mm e e. a- -mm.p ema. ...e... a. ,.....em =w m . em m.m g - n-.. e.m. ...w. ..m--. m...e. .e. eum. 6 .m F_ .m .e.. m. W m. of um mm-. M* * - "* ..N 6.."e""6"*- a*** ""W"" M M W""- e""6"*""""" - e.. m-.m.. gem. 3 -m-- ... -_-g W .N.-. .....5-...mem.M M..emm. -..h.M. q mm. 6. -mm me -.==

e. e... a em. e W"'

m.S......e...a..=

m. em e m.. ama.. - m-. -

6... e-e.

== ..e. gum. m ..m_ m--- e e m.. .ammmed. ens..- umme. en-mom...... em M ... au e.- a.s-me. a.m. au m-a s... ame ..=.amm-'>=..m.'mi.me.. e.e.....e ,e pf.. num ww wi6.... u- .e..mm.e.sm. .m . ea-

m...ep.

e.a...,e. ama e. .e. m.e...e 4.. e... ee-e e.. e.. -um he-ammmmm. anum.m.m. amm e e . am. a.m -e g am = -. amame eee........m. .em =. a 5....ge

a. g Me. 66..-..m...

.1

6.. e

-M..' W.. = 6-g g g g g.. .M e g O m m. M...... h m.o.. .S= G - 6 a ....e.. .M e.......*. e.. .e..M. .e. e.m*.N-. m.. -a- .a..__ -i. i .e3...... e.... emme. - ......+.. e. I..=.=. .e........ ,===...e.. . m.e..... enan %n...2....... .e ami ..m =. = e.m..em. e e.. ..a= .mm...mm. .-=.m= .am e.m men--- -- g an...- t _. _..- .ema..-.5 m..... _ = =4e-..== =...... m..m..

...a.

a. .a .g....-- e...-.. ~~ i e. ......-g._g..-..... esamm e....... ime._ M00 m e-se -. ee ...... em. e e-e T--tw?:st--r. r r.m-- tv r: unr.1.r=1m1 rit tqeii qttpu erirI..t..si,ie ys - nrT?pem;ar,i l l 0 100 200 300 400 500 550 l l a.r.v. 'r=, *r m

DATA SMEET g, 3 Spec. 9645-N-275.0 A pendia g Rev.10 b ~< 14 4 OATE T-lO-0 3 C**tCEED AA4 t* WATE IIII /f'l omiciseA70s I!!ni'MH'Ee*THe'sFAfM6Rt"I a n trold # ' ~ m.a 2 $ OF 35 9AR = 09 ' NNM TN22NAL Nene van sso n Hgigen m es i M Id 75 MtgoEla._d, I EGI GC04sMLG La A ts_. p $n o _r'nos.p I 2 24

' n,o S A H I li l

l 0 evAr_rnees so.eren earrar ri n i. s I --Attatssicas 4Asuss l i i setac.tso sounmAm uruts I l,' I I i '-----As.c4rtAe,a s ou.oAm u uvs '/ in ~ ~ .l . _ I' i. l / l l. I u n i i I i I r I 's s j-ag _'4 h ' _L.i ' l I I /,I /j I is t i i / i1_1,l / f Y _1' - 'I 'e -- r ' 'l

t i

/- / ie .~g /- i i l l / / / IE ao _I..T~g' ..i.,. j i l _7 f ',7 i n =. _... --,s..-. -, .I l I / / l r -. s.i,...... .j ! r , /,, n - N.- - C a g ~~ m -w a B m ar ,~n p go ago J<e 4ao tw 6'c o as ~ a SvJlwr a I I I I I ano.iasi i ns

DATA SMIT W.6 spec. 9645.M.275.0 f. FRK-OF. TMDOSL MCRITORING APP **diR R Rev. 10 N MAT

sheeIfe60 Pre-ep Iso. No. N - I M SV A

"=nassan, s: Lanyard No. Ec; t Go ed SA84.tij, ~__ Stress Prob.Wo. J pat 9.7..%A" M400 =4.=,._-. _ m-tussw.1 unsuu ses ~~~+eu tu.u n,..w_ 1 ._.._i. j ._m _3 _ _. _ = Mvat, then valve F063 is open 6 M:r=m:1: ~ Mvet when valve F063 is closed O __..J._.. +2000 - _J - ::s = l =_ 1 = Analvtical Values - - y _. = _~ -~ l h pected Limits =: Acceptable Limits

=_

=

.,s=-- +-__ +1600 s-..,.. g_- = -w: - _. /. _ e 5 _.-._-t, %..._.... - +1200 5 .-__._._.__n_."_"f --- -p- ...I__ _.i.__ _. _... _. __..m .._1_..__ . _ e.._ ..._.t.___ ._l,__ __ __ _. ..__ _ _ _..._.-e i __ a. t e sa . _ _ _ _ g_...:g.?- _,r _ _ _-..._._._. J.E__....___..__ _._a._._.{._._ l. _ _._. _.I _ m, t_.....__......._.... r _.. 1 _._._ __._ _ _.. ....._ s._ ... __ s. .. _ _ _ _. _ _... _ _. _ =. _.... _._.._. _ :::a._...._. ... _ i_........._ _. _ +400 _ l._ _. _..... . _.;;aq . _,.. i.,e _ _ _ .M_*"....__. _. _.. t. .s.._...__._.. e.r, _....__..2....... _.... __ Aam'... s... _.. __. _ i. _

-.r

. ~ _.. .. _....._._._.2.... 0 .._.._._...._......_._..._.__1.. _t ..._ t._.. m._._._. _.__s._.__.__.._._._.._. .._.__._v._._......._,...... t _ -400 i u...n.::1.:-rt:l_r r.:...:. i-::.t:: 23.r.t. :n: 11:st tir.*ityppuP:as" m eity'- nepp1 im o 0 100 200 300 400 500 550 t R.P.T. Tsup ,F l m r e

t~ PATA SMET W.6 Spes. M45.M.273.0 . ru-or[ tusamt sprricazzo Arte=dia s new. 10

=^* =Ar-nn 6.et_4L.,e M !675 REyd

,r..., 1... Lanyard me.E31G00401 D LY = Stress Prob.Wo. 69 8 p.y. 997

3

= = = :- - +1200 w teits Lt m e n w i.u. n. I m * = ' * %a . _ - =. = . -n 5 Mvut., Valve F045 open A - _ = ,=4: Mwat., Valve F045 elosed' O ~ ... m +1000 =_= Analytical values Expected Limite 1 =

==.z-=.:=, Acceptable Limits -~~ ~ ---- ~ e g i r _.-v t _1_: .m

J.

+600 5 i __a_._.__ 1 _._t..__. __.._..f~._ -t.__.. i _ g ___ s . _. _. _ _. _.._J .t__ n. _1_..- _..i ..._s. w.._-._.... .s. _ __ _....._1_..__.,, +200 r _... _..__ _ __.. s... ._s__... .... _.. _= __. _. _ _ _ _..... _ _ _ = _. _ _. _ _... ._. _._.......c .= s_. __m .. _ __i..__ ,.,. _.L.. g. y.,. m. ___f__.__..,..__s._.._.

smaus

_..i__. m_Ltf __._s..... ._._.I__ 1 _ 0 \\ ..._.l.._._. ...:n __... l \\ ......__.a........=.. _ s_ g \\ ....._.._v .. i _ _._ .._...g.._. I ... ormirrr: r :tzm-un-srs tz: itze..;igt; Tl ITi fl7:1111111111 "Ittitli.it sistet' n Iflits t' 1 \\ O 100 200 300 400 300 350 R.P.Y.' Temp

F m

f 1 n ,m..

I l i DAT.A SETT U.7 Spec. 9645.M.273.o t. PRI-oN TE10%h MONITORING APP *odia y as,. 11 Power Ascenaton/ System Meetups Sheet l ef 8.9 (Steam Condeastog Mode) M-16 M srv? m:._ ,.m.._.. Fre-ep Ise. N.. No. I E 16 C O IC4.'h 7 Lanyard Stress Prob.No. p.p. 4 00 1 =- % --4..._ __ ___::=-i _. _ -12o0

: :c....a_. i_m_._e - :. tet er n tn_tu.t:t

. =. - .=:== h __ _::.=.=- - - _. _.c.=_ =. _t____ t _ _,.._..

_ =_,

E Mvut. free computer output O =---1-- -a = Anal tica a uss .._._J__ _1000 _--- Eapecred Limits Acceptable Limits -------. -*= =-

=.-

,=_.:: = _, _1 _....I_. _ _ _ _ _ _. _ _, __ __ - 800 q_ _._______._..q.__ a _a__- _.s ..__i .__r g A 1 4 --i--; i_..... =* 7 _.-l_. --w._ _ __ _I ___ __, _._i _... _. _. _4 . _. _ _ ~. _ ~ _ _ ~ .. _ ~... .1_.__ ~ _t.'~.____ _ ' ' ~ ' ' " _.._ _. ^ __ ___f__ t_._ _. _ _.... _.. _ - a __l__.__ _3._ _._._.g_.__..._. . g...... _ a. _.__._,_3_.._..__. f _._._.-.___.t.__.__..._.__ _ _ a. _.._ .I ___s. e ._...,,_._._..._.8_-.-___ . _.._._._s_____ _~._.. ..__t~.~~..._ .t ......... _..t __g_._ .m__ _........._i_....._ ...v_-... p _. ...._.._.J._ o e J... _.... ...m 3 ___. ..*"."7.t.... .. l..... g .. _ j _._.._._.._....3._.. ..t._._._.... _r...... 00 ._s...._.t_.. tW,.tT",flUrft f1F1117DIITTl11J111f711 111I tt f eli t tI Hi s t ti l i II t t, at t. i t t t t i f1 fii fT11. t111!11i L ' 'L'17'U I f:71 l'It71 : o too zoo soo soo soo 330 E5lG00102TT 'T=P *r m

BAT.A SIETT U.7 Spec. 9645-N-275.0 FR3-OF[ TIERMAL NONTTORDeg Appendia g go,, 11 Power Ascenaton/ System Esatupe Sheet 7 of II (Stese Condenalog Mode) i Fre-ey tee. se. M-I M4 REV3 m m _,um Lanyard No. E G 16 O C 1C ? 1,g.,,,,, .=. _ =$ " Stress Prob.No. /: 4 9.P ?51 8 =- h--d____..__. ~1200 . =: =......>.., u._ _:.=_ ~ - _ em. u__s_u r .==t."____=_=.=.== _t___.._._.

=_ PNat. from computer output G i__

- -f - -- .:.= = - := -__..._J_._ _ __ __ m. _.. t ca a ves na --T-- i _ __. _- =, _ : _ t Expected Limite - 1000

==

9_..__ _:=: Acceptable Limits ~ ~------ =__:

.:=.__.

_1 _==s. ......i_.___-___i____. , __ _ r e i _ _ _- 1 _..._ _ _ __ _.~m ._w __l__.__ i _ _ _ _ _ _. _ _ _. _.. _ _.__ _m .i_..._.,__ .>.__s_____ _1...__.~_~_~.*~~~.~_~'.~_~_.__~~~._~~__~~_~.~~.. .. ~.. ~ _ _ _ .. _ _..._ _...........'~_...__ . ' * * ~ _.._ _ u_.. __.._.a._. ..a___._.._.._._._ ,..i_- _ _0 _.. __ s. _ _.=_...._- ___i.__.....__u..s__..._.._._.____._.._._..._..._.__.. 1 .~.. _.._,_._.___.s._,.._.... _.. _ _. _.. x _.. _.. _ _ _., _ _. _... _ r..- s_.. 0 ~*"I."W 3 f.F flit' fin:'7 :'It;-*1 itT31 TTT1114111 fT11 111tf tfiltlit tutti filttttlief t tttist ri f'l!?T'1 811 t tit t i E u O 100 200 300 400 500 550 l l l E51 G00lO2TT

Ta'r *r i

1 l

DATA STEET n_7 Spec. 9445-M.275.0 I FRK-OP. THE10%L teONTTORING APPendia y 3.,, 11 Power Asceasten/Sy' sten Bestups Sheet N of IT (Shutdoes Coeltag/ Steam Ceedessing Stede) pre-., s ee. No. M _ l 6 6 3 R Ev. 2 g.=._ _..... j 1,anyard No. H 2 30 0901 DLT Stress Prob.No. 9/ p.p. 4 l 1_ 1200

. :.w. e _u...o_. I_cu_= c.:.=.=.1
.w ti_c'rt_ ism___.=._ _=e_ -t_: _. _ m_ =

d _ _t____ ..=t=:t

== 9tvet, free conPuter output G i =:==1 -- _== ___J__., nelytica Values _ _. __. a

=:=._ _.

1000 i Expected Limite

=_

=.- Acceptable Limits -------- - ^_.__._ _1 _. _ _ _H. __ _,.. _ _ _-.. _._i__.,._ 2, _ 800 __r__ ._.__.1.__ _ = _. =. _. - l- - dm _r 5 I a .__ -_ 1.____._.__ __. i E I _._]. __i__.__ __-. v _. _. _ t. _ ___-.... _ _. _ _ ._ _ _ i. ____._ _. _ _ _. _ _-1 ___._._. _ - ,____._._._L.__ .___._ s _______.__.._...._*:. _.__P_._____.___.__.___ a ._.a_.. _.,t __ _ ~._ t__ _. _ _. k.. l ....... _._.._.a.,_._.. _ ~.. _.. _ ar.s __ _ ..__...s __..__.__,n ,;s_e=._. s 203 ,_ _ _i _.,,etr_.. _._ _.. _ _... _.....__. _.r... .._.,_._._..f r._..__.... _ JEM.. ... w_- r_... .O . s _._........_ . l..._._ _. _ ) ____.,__l_._...t.___._ ._.__g_....._.._._._.._.............l.. . _._._e...._..:--. 200 ....=.. ' '""i" *. :.3 :'1 " t l' m r' 1 *: *1 firi l :17'It tffh14111tT1t 111111f t11111tulig f1tittfiting etttt! f1filfT11 I111tif 1 l W 0 100 200 300 400 500 550 E12G00901T T TaiP 'r m ..-.-._..,._...-._n- .c

DATA S WET..n.1 Spec. 9645-M.275.0 FRE-OP. THERMAL NOMITORTNG APPendia y 3.,, 11 power Ascension /Systen Neatups $heet M of $i (Shutdows Cooltag/ Steam Coedessing Mode) pre.., z... se. M _ f 6 6 3 R E V. 2 _,.=._ .. m.. Emyerd pe. Etze O902 DLY =s -' i Stress Prob.Wo. 97 3.P. 76 1~ =- h-4._-__.,.__ 1200 w. ..:= c.:.= : :. s..a tt.t.*.m im==== =. .=.:. t _. :s = _._..m.__---

.:. 2. c.

4. _. _- =. _ -.,._.__t_-__ _.. _.. --t= =. Pvot. free computer output G =_- ._J__ Ana )tical Values ..m =:. -:9 _..a 1000 = Expected Limite ~ -m ="- Aeceptable Limits -------- -1 ....i.. .:.J 800 t ~. _.,, _,,, __Q__%.,. =. = -i... ^ a --_i ...-a _ _ r. _._. m ._f-e i .,,e ,e _.C _._..r _. m _="1. www i ,p .,p.. p_, ~ 'O_ I. .-.-l' _p. M [ l 4 I _._ _l._... ._-. _. g, # pi_.._... .m 1.t.. m. g.. _ r ,p. -.- -

1. _

_ 4. -..- - _.1 t,, ~-_._._I._._. - _. _. _. _ _-_.-u a 4 ._!~, _._.$ = _. _. f w,- _ _- j _..._.,6.- S. ...l,...... d":" _.... _... _.f s . _.GE ff _...a.,._.

s..

300 .-....-.._l_-., 8 -. I._....

1.. _-

p-- s-.

1....

I._. _4 a ..3... .f....... 1..._.., 0 ....W.. _ - _ _.J._.... .m.. 3_........ .r.. _.l....... -..I__.._.._.... g......._. . _. ) .. _ f.".."...j...._...._. - -200 .. _.... -..J8....-l._. . s p's?.T."1*T* FT '.'m""-MFH f fftf ffflit411tif'l !?f f fff #1f t f ruff # ri g g iv in gj g o r ist. n f11TT11 e11tt 111 300 400 $00 550 ~0 100 200 E12 GOO 90lTT

Tar *r m,

1 i BATA SWET n.7 Spec. 9643.M 273.0 I FM-07. TERMAL NON1toRTWG APPendia g 3.,, 11 ~ Fever Ascension / System MeetuPs Sheet 12 er 59 ~ (Shutdown Coeltag Mode) pre _e, see. No. M-I6 6 2 REV.2 ,,,,.=. _=8-' .m..,_......m -l 1,anyard No.E!2GOIOOf fR 2 Stress Prob.Wo. 46 p.p.e s$ lr- u --d.._ __, - 1200 =._ =a.=_ h =_._::. =.=7-z c. ,._4. .a_.._2._a= -

r } tsyter n ;.*.m. im

-. := t==:==..: --- n - ~ = = t := _= _ _ t _~=

-- -.:a

= twat, free computer output G =:=1 - -

. =

E_" Ana1ytical values _ _ ' -.=_r._=_..._.,_-)=_.._ . J: Expected Limite - 1000 =_ -*:==' Acceptable Limits -------- =: =_-i ~ ___= _. j i r M :_. - =i=- =. =sE 5=::E: =.J=i-r.=_-= -l== =a - s00 < _. _. ___ _ r__ _._..,.__...._i.. t = : =,.

- = _=_

m __. __ r. r1 .g 5 L._ - _=_,. =- -= - _ _ ; __ - ( 0 0 = a._ _.: _ = E -. _- 3 _ -- =.:-f _ -. = = - = I =.__ 5_=_J. =__. =_ i. = = '. __ _._ =:- - - a - -- - + =_.Z_iJ E;=< '.9 - _ _T.. __:._=, _.__t..___...,._=s _____l=___=l=__==._.%__ _ _. _ _ _ _ _ _ _ _. _. _ =. _ _. _, -_-. _.__:____ ___l_... _ ,,4 -":8 a E f = : = i. =. - -- _ _..__ ;c:.---:-- =_.-._.=.- r.i. _". '.. __. !.5. E i t',

~~~~_ !.._..__=.F. = =

_8 - -- 1-_ _-m _= ~ _ _5_:. i. a. =._ _ : __..._.: l _ =_ __ a: : _= :i.:_ e. : _._s=-a_iEI m. _.ar. __. ___. _. _:. - -..._.:_... _. _... _.. _. _. _... _ = ___ __ T. - - : -.=- = :: _- _ =. _ =.- - - _ - - r.=:. = c _#:.J._ -200 =

t =- -- - --

-r--- =:

- :-: - =- -

c.... _.a._:.: l __- _.... _.. l.. :.:. =._ :-

.~.. . - - l . r...

s

. pr r-f-.:.- = =:..----- -- -r: : . _. = _ =.. _:...:.s. n_ .. r. _.= =. : __ - _. __ r _--_i_._. - =_.,_ s ar _._ m ,........._a_.r_._.___. _.__. n _.___...._:=__.._...:._ e _. : _. 2._...- =.._-=.._:

=:

=:~di:ii:3::.1 -ii:y@ :li:ig[:_ '==.,_:. "-i.:-W.::::- i

7. j,:3 ip: 4

= .._._.:.=._.___.:_..._..._r_._.p.._.=.... ..i _: _ _=. - =.=__. __..::. ___ :.._.: r. _.:.=_.=_.. : : =.__. =. _.: _.. _ :.=..... : 33 ..e._.. .:: ;_ _s.....:.:s._ . =_

T 'l

!;:.f..*]*1 '. ft 1.;*T :'1 1*1't T*J't l1ft1t ffT)ilJ111 ff11 tti111f fItIitttjf ti ft It t t t t, et 3.t1itt t ft flim1 ett tttIi 0 100 250 330 400 500 550 E12G012RB7TT Ta'P 'r m, I l

SATA 11En Q Spec. 9645-M-273.0 FRE-OP. TIERMAL Monrl0Ml!G APPendia g me,,11 Power Ascensies/ System teature Sheet b ef U (Steam Condeassag Mode) Pre-op Iso. No. M-16 6 2 P EV 2 2= ~ ~ ....._,o,

u. nam-Lanyard No.H M oo.PDLv

=. Strees Prob.Wo. 69A 3.P. 34 9 _ _ t -.____.m-t1200 . _..=.:_=h._ _- - = - - -

.r.:.:. i. "...a i.c : _a.= c.:.= m.1trtte nim._nat

_.__._____.t__ _ _. r.

_..M.__

N PNat. from computer output G

== = _=_ Analytical Values

:::e=,

. _.__i___.__.,__._..a t 1000 E-Expected Limite - ' = = " E Acceptable Limits --- _---- ., _...m _.- _h i ,L_. -_-..-i._ _ _.=1'__.___a.__ _,__ _ 1, 800 <. _.. _____ P_.. :r

1. _. _

, __ _ r. _W_ _ _- = _ _ =. _ '. d c . _... m. + 600 5 _ m ~_ - _. .i .__.a_- +.. _. _ __ __ i. __..___ _ _ a _ % _ _ _ _ _._._p_,___ l _ __..__i_.___.__.....,.__ _._. _ _ i _ _ _ _ __ - -.j _ _ .3. _.r _-__._._1.___.__ +.400 m _,_ __-. - m __ _..__.. t, \\ __,.___.____._s._._,- _.,.c.._._.._. ___i___..___ a. _s......__ _ _. _.. _. __. _ _.. _. __._.._i._____.__s..____s.___.. r ._. s.. s_

z __..... _..._..__... _._.._.. ___.___ _.

c:. __.s._ _.._ ... _.............. _..i.__. __ __.... _ s. s. _. r.. _ t-200 . #_i.______.__ _ _. _.. . _ _ _... _ _.. _.._._.._.r_. ..__r.-._ .s_._ _ _ _._ _s.__ _. _.._.._.._._._, _ _ _...._i_ _. ._.___t....___._.._._.._._..._. _ _ _. _ _. _ ._.._.4.._. .0 . _.. _ _.=.... _ _ _............. _ m ___..... _.._i__.. _.g. _3 - 200 ..._.. __s. s...._..i._.... - n r nm inm-r i-=-mritimirmiummi mmimimuto nnuinm unn nmmuming 0 100 200 300 400 s00 550 E12601002 TT T=, 'r m, i i .--r=-r. - - - - -,. +, .r _,--..-.--_-.----wre-.r.,--

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I BATA SWE7 n.7 spec. 9645-M.275.o t-APPendia g 3.,, 11 PRE-OP. THERMAL NONITORTMG Power Ascension /systen meatups Sheet N of M (Shutdown Cooling Mode) Pre-oP 1s0. v.M_1662 REv. 2 mgm.m. mm unna M -L-2- Lan1ard No.El2GOIDO2 D,A 8 -*a..=.'~"*"- Strees Prob.Wo. 69A D.P. l- _1 3 + 1200 .s.:.. . 3 g .c,.:.gE n 2.=.:.y y.t'I"$! _..= 7 = *= ti"= ~=i? :-N ~" _ _ t=== N:i =_i= t _ _= --r=.hN. ~-i::" :. i - := = t== .~- EE Mvist. free computer output G J==-

. =

-= ._...d_ Analytica values _..... -..z . _/ _ _ .9.. +1000 EE-E Peeted Limits EE Acceptable Limits -------- --J- _h._.._ c _= q g p. ~ ~.d m_. _4 a ~t ~_;

-J

--~ ...-. _..._..... J

l3. _ _ p =..

._....*.._-'._-d. +800 ..i... - /:". f. "- ___ __.-.1 i .-.p -e- .- r r- -m [ ":"l" : =.) - l--- - i 4._. 1_ _ ( q a e a .____.i__ a,.e. __9_.-l__-- -r600 o f_ J _ e a _. _._ ___a p - __. 4 _ _ L. a_ _ w _.... _-_ __.I___,

T _

_q __. - 4_. _ 4_.._ _ -_t._.._ _ _. _. ______1.___._,-,. - -.._. _.i._. _ - _.- w ...._. _ I _.. -. 6. w_ _, _ _ _ _ -. _15 T_ _ s p. cb .- 3 '..J._____.___... ..__J.__.___.. s. ..g... ..g_- 3, .I.._ .. - _ __ _.J..._ _ g.f .'. --.- - _ _.._. _.. _~ _.._.. .. t.... -.-ty-203 .._..l_._ .............u_y._.... . _ W_ __.. ..e a_ _ _, _ __ _........_.-._ ..._f.".*.._ .I. . j _ _ _ k _... s_. ._f._.....-..l_... _.l._. s .......J - 0 3.

l.....

_..._i__.._. . i. _.. . -200 . _.. _.. _.. _........... ~.... .__r..._...... _..__._......._.i_. ......_i.. ~~ri"'.* s t T flifi I ri f11TT"1111:ri nlr11 t IT3 f fffi tid 11l f711 t11tfif t1It'lt1111f rllttt tisert ettth ri fit fT111. t11 t t t t < t o too zoo soo soo soo 350 E12GOI2RB7TT 'Te-P 'r m,

l l BATA SIEtt n5 Spec. 9645-N-275.0 - PRI-OP[ TMEMAL Nori!TORDIG APPendia y 3 y, 11 Power Ascension / System Heatups Sheet 2 5 of 39 (Shutdown Cooling Mode) Pr. ,t...u..M I662 REV. 2 m... _ _m m, _ =. _==f Lanyard No.El2GOIDOS DL K stress Prob.Wo. 69 A s.t. 2 6 5 i-- =- <,__"..._ _ __ =1_ __ 1 - 200 .. _..__t=== .= = t. _. _:.:= _=. =-. - = L=. w.s u_...n__.s m._a.= .ce I ra t.*t_t_s 1.tst _ =. _ ti ,._ _ _ _ _. _.. _ _ _ = .=t= r_____.___._._._.. =_ Mvat. from computer output G =:=1 -- ! _ = = ._.._J._._., Ana 1e ca values ._....._a - 1000 Expected Limits

== 9_ :-:- E_ AccoPtable Limits -------- =_.: ___,_____.._i__. __....i_._.__ _.= p__ _. ___ _,. _ -. _soo ____t'_- _. _._..,._ _ _. =:=., - i- -- ; _ r, 3 .p.... _soo 5 _ _ i __ _ __ _, ___i.__.________._.___,_ _._i.___.. _.... _ _ _ n,. _.._.. _ __ _ _ _ _ _ _ ____ _...___i. __ _g3 ._._-r_______._______._.r__ .__m ~_ .r_. .__._.___g ...i._ _ s ___ _. _ _. _. _ _. _____....,c_ -200 _i_______...__.._ _. _. _......._.-.. _. _._ _ ... _ _. _ s _... __ =-11 = _ _. _. _.. _ ..__r....._ _.. =. _ _ _.___l_____..._._._,... ..... _.....a _ _. ~ _ _ _. _ _ _. _. _. _ _ _ .._i.__._.__.._.... ...._._.._.a._ ._..._i._.___.._.i_._..__ . _.. _. l ___i._...__.._.__.....___.__.__._... _ _ _. _ _. _ _ _. = _..... _ _.._i_._._ _____r..___..._.. _.+200 i. _ _.. i___. - IN-*.*st.T..' lift s alm *7*'UTUf'IN111173e rTTil1411t ffil Itt if flit t f

t t'ltif fit tt'f t ritt 8f fle, r)nimi tittfitil 100 250 300 400 500 350 El2GOl2RB7TT ~ T==P
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l BAT.A SETT r.7 Spee. m 3-M 273.0 t l t-PRI-07. THERMAL MONITORTWC APPendh y 3.,, 11 I Power Ascension / System usatups $ beet 27 e' 39 (Shutdeva C.oiing Mode) rr..., zs.. s.. M-I662 REV.2 =....... e.m %=. _ =l tanyard. N.. E 12GO 100 S D L Z stress Prob.n.. 69 A s.t.265 i: 5E:. -'--4..._____._. - 1200 u w.s._...a._.. m_ _=_ r.=m. w. m _m _e _ _ __ ._.._._.==__k__.__=. _==_ .. u=: t. _ _. 1 -== Mvat, from computer output O- _.m _ _ _.r. Anal tical values .a...._. =_.._ _,_.:-_._...3 - 1000 7 EnPected a.inits = Acceptable Limits -------- _-i e ._.....,. _ _-___.7____.3_-_,_.-.____.__.. _..=i. .._J __, -800 __ j _. 3._ _.. i__ 1_._ ,-_r 5,. 1 - 600 5 4 I __. __ i___ ._._.._..,__.._4 _ _l_ __l.___.___.I__,__,_._____1.___._.__ __.._--_._t.._... t ] _ f.0 0 .._..f.__--. Ch __.__f..___.___._4___.._ #_ __J_.___., l._..._. ___ _ _ _ _. __._.g_-__._3._ . I. a. _._....-E."...._._. .. _.. I. ..._..._.____s....__ . _~. ....__1.__._..I__-.._._I___ _ _..g.... . _.... ~.... ...__s_. _.. =200 r _.4..._. ..._t_..._ l e._..._. _ m_. _.. __s... .._.a__._..a l__ __.... _.. ._...s- _l.... _. _... r.....t. _ _. -.. ~ _..... . _... t_ _ _. -.__6._ i .. _.i s_.. J.. ..t _c -- __l_...e ._._.J. ... _ ~.... \\ 0 ..w. _ j __.. _ _....... _. _ ' _.... _. _.l._._. _. _..l... m__.... l _..{ J l .._.._......t 1.. l 1 .__'.'T..N., l .. t 1h... A _..... _. _ _. _ _.. _ r. A 4 _l._. _.. s....._.3-... . a. i. 4 *. T..*1111 s1 tM f7"a t c 71 pri l l1111 tTT) i141111 f 11 tillflf ilf f tt thfil filltf f st ett 'Ittt' r1f1'fT11 stfif tti t O 100 250 300 400 500 550 E12GOl2 RB7TT

T=P 'r m

l i DATA SMt? nM $Pec. 9645-M.275.0 FRI-OP[ TIERNL NORITORDIC APPendia y Rev. II Power Ascensios/ System Heatups Sheet /k of N (Shutdown Cooling Mode) pre.., z... p.. M-f 661 RFV. 3 ,,m.._,m. o,_ ., - = = _ =8 Lenyste - No. E 12 601701 DLX stress Pre.n* 69 C s.t.355 '=- - _e__...__ =__..--n.- 1200 a=. - h _ - i _=.= - - 2 _. ._a. w. _= m_u_=

== wem.m _m mt e

p . a. :- ie e ... _.a -T: =., _-_.a_=_1 L - _me -.m= - - _.a . mm .en- - e e Mvet from computer output G i__ ' *M-H

== E ...e

=-

m,_...a .es._ _ -J._._., _ e m.. - nel tica va ues am. .e. 1000 _=m.:Expeeted Limits -.-me., m. __a.m.

== = Acceptable Limits -----~ _._m..-..a-eg = :ll "mmmme - eummmmmu I -.a=-a - amamme g V .----._am-n 'm amme ammmmme e_ e-

====m=-5 _ am- -i_m. 1- -' _ w - a,m- --m__._-.ae. ..m.- .a.mm e. e...e m.. e. e ..e .-e e m --- .me._ www ( e mo .ammen e.

e. e

-... - a.m =. i... a_.m. s ....q. a-m em, g-p--e. e-m eme a e. ' " " " ~ ~ 5 . am +.. ammas( amm--m yu M e"""" .e-I e.-- . en me==u-mm- - g - m.mm, a--==m-e.m.em e.mm m..e.en .e e-3 eme..e..e.me ee e--., g am.m._...-

- emme I-.mmmm.

_m= = = = = = a amm== 600 e--. --- _ f _ - -..e --.m._- -e.__. am.m. . e -( .. eme-._ e enama mmean.--B m.- - - - L-g.-- e-_.-. --==== I-amum.. - t=====a-= .---===**""T* = .= =.m. - = =

==eum amuse. amm-amme ammmmmme -.. as i e-s. ammme e e d. e.mim e.mmu eau . am . -. eum.e e ane ame - eu .-m-. m-. .sm - au.m .l m-e.-m. -- amm-asumme.o - amm-u_aa__ e -. _.. am_m-ame e__ _e-e e. i e t.00 m .e

e. _ _

-e_eme .m_.- ..am. m.___.._e.=as- ._e -.m-._.e,.4 -e._. _ _. ee.-.- .e g .. -. = _- ._..a.m.- .e-- en - .a. a.- en . m a.m--.- =#... -mm .{_....a-.--e_ e - n a-a m-e. g am _.

==a- .e. - -.a.. --m-.---=.==e.am-e--.m.e-.--a-I -. emmum e m-= e----u g me m. e... ammum .-. au-a l e. -e.mm.ius.uu .am.. em.m.- e-.a.= -e = ._..-en am ' ammmm .3.e.m. aum. e -e. m.

====.m===.. asume... .,e .e.mm. gee.m. ammu.amm e .eum en = = eem .. 4..mm- ...- -- 4 e .smay e

=

.e g m . muse--.. amm = m-e em.. ens - em "[ .am.me asuu.m

m.mmme-e.

e. a.u en..am e

e. e. e a.n e e

em a.am.mmme -se...e-p .m - am.mn. - amm. am--mea- =.m. . mmemme.. -m-.m a---. e. em-e.mm.m-- -a===mm..e. M. a.umm me umm..

e. m.. emme - e amm amme.

em e. e a.-e.. e.m e.- 200 e.am.. a. e..- - _ e i _. ..m.-. -- -... . = = =... . au = e-- 5 am mme ammmme... - g e .e...am.. .. am em - em s. ---m. a .... -...am.... - .-m. .em .amm em.ms e.. e.- amum 6. f,T M -. .e.. m.u-......e- . ame emme... amen. m. a- ..== =- en u.m .eamm-..e. .g. ameem --. 9.m-p ._.e. ammm-. se se e am== a===.M g_ amme.W=.. am-ammmme== w ammum e. ou .emme .. g -.emmme e.- . = = === y.e..amo ausse. -..- ..m e.m.mm. amm _ -.-2 aman p.==e

===.am[M 4 %. a _,p _ emmumi emme e.eum ee mem 5 - ama.m

==-au_=mm . ammmua am e - um esp.. e M_..*- am. .a_m-.. .am y -se'""E-em -.... g - * -..... am fu em 5e

.....e...

g M. enn e sus .m.... ...e _ um an a. un-* amm. a.mm . em . an emmum

==

e l ame l ... _. -.== ..... an. emm en.. es..... .. -. am . am amm am e ao m-..am e .-.ume. am e e..e..m.. h. am .. - emmm.e. amme amm. e.m..e _ .am_mamo.... . men. am.. e.mpem... ex-e. a-e.. .a.m am.me-e.o p. ame.n emme - -mum . ama e w e a- . en am. -e.. en-ammmmme. e.... - 1_5%_% "WB..=.. = = - _. e. .-e i mee. e.......e....... e.

==_====._.....a m.. "'.9m _.!.....e.m.. - "Lem. .e... e. .e. --e ..-.e. a .... e e. e......... _--_._. - ..mim. ... _e.,. am...m.. e-e,_ _.._._.e e. _...

e. m

.m.. es. a a.m _ as m..m.... e e.m_.. ._......_am -.....ne.-.- m.__ _.. _m.._a.m_..ee. _. >m..ag..m. . e.e _ e. ._ _ -200 m .o m e. e e m.m ....m.. e. ' :.W a r.T M*T* on:*3""W 1*U11tTT11TTNJ111ff t1 1111tif t1It'I f *lHI fif f f f f u til !!!!h A f1MT11 'tif f ff d 0 100 250 300 400 500 550 E12G012 RB7TT'mp *r m,

BATA SIIEtt UJ Spec. 9645-M.273.o FRE-oP.' THERMAL MorritonLwn Appendix g me,.11 t' i Fower Ascensten/fystem Meetupe Sheet _,{er89 (Stees Condensing Mode) pre.eP use. so.M _16G i REV. 3 ........ um. tan ir.nau. -,st:rgg =...,

===s Lanyard No. El2GOl2OI DLX . =. _ Stress Prob.Wo. 69C o.t. 355 ':- - -'--8.._.___-_.. -12oo w.:... _.....a_. i _=_>.2 =_: n.:.s. =.:. itu-t te r.i.tmitatt - ;=:. _.=.::= t _=:. _=_===;== i i_. _. _._. . I_'. =_ =. ,.______t____ .__..-=-=

==. Mvat. from computer output G -m -- -= _._J._._.__.._._.,__.._._..= Analytical Values _._.9 _. _. _.m .-= -looo Expected Limite Acceptable Limits -------- 1_.. _ _ =_.: . _ _ - _.__I.__._. - Soo _ t._ _ _ _ t= __. _i__- __= _ _ r, 5 _ _ _ u_ _ -soo 5 i _ __ -. _ w __i______.___. 4 .___i___.._.________._ _ _ _ _. _ _ __7__._____ -400 m., _._._ ____i_.___ _ _._ _.__m___..___.._._.___ ,._.._._.__._.__._._,--.i.___.. _. _ _ _., _. __... _ _ ___a.._._. _. _.. _. _.. _. _. _ _ ._s.______s _ _ s __ _ _._. _ _ _ _ _, _. _ _. _ _. _. _ _ _ _... _ _ _. _e =__,..._. _. _ _.. _.. _.. ...__i__ _.._ _._.__ __i.__..__._____._._.___._s_ - _i. _=.__._....__ _.. _._ __._ = __ _._. _....__.._ _ _.... _.... __.. _. _ _ _ _. _.. _.- _ _ _i __._.___ _..,. _ ... _.__.... _..__r_.-..._ .i ..- =:. _._i___._. ___. _ __ _ _. _ _. _..._i_ _- _. g_.

1. _ _ WEiiipr _-". __.

..._.._.2._. u _....i._....._._.._......... _... _....... _ _ _ _. _.. _ _= _ i..... _ .._--_m__.. _ _. _ _. _.,_. _. _. _... _.. _..,_ _ _._......._.._m _t_,00 1, _.. _......... _. _ _. __._._......_.i_._. P"* :.i "" I t'.;*T 1'***1 *"3'll t mi fffiltalb f* t t 1111tif tillitt11111 fit t tt teinit !!tte-r f1r1!t!!.41 t j o too zoo soo soo 30o 33o .I i l El2GOl2OI T T ~T**P *r m

e DATA $NIET 11 7 Spec. 9645.M.275.0, FRE-OP. THERMAL NONTTORING APPendia y gay. 11 Power Ascension /Syste Heatupe Sheet D of N (Shutdown Cooling Mode) pre..,s..se.M.lG61 REV 3 n g.=._ .. m., _.. m on-

==8-Lanyard No. E12 GOIP A2DIY stress Preb.No. 69C D.P. 3 70 ='- ~~-"... __-._ 200 _ =. - .=.: ._.. -_..=.=4== =: .,_._._i _im.2=: r:. te s a n t_*m urr u.: w. _.4..o . __.f=k,-_. __=__-t.=~ f, r- =~ -- = Mvat. from computer output G ..=.. :.. a = Analytical value =_; b.. . _-9 E: EnPected Limite 1000 ~ E Acceptable Limits -------- _w..-.._ _ y_ ^ ._ _...~.l,~,, s. ,,_.__,,,._j ___i._._...__"' ~ t = __ _ __ _=. l. 800 --.I__. l' - e. f"__._ _....1._-=.-. s a s -i _ = =.2 s e. . _...w nns i 4 4 .As...... _.. _... _ e.e s m WVw . _ _ =.. _.. _.. __4 _l___. __L__ y..

g.. a # _

_1._._ m _ p +. 4-i_...__ =__....e,.__. e _---.e . -. 1 __. 1 g._ g ...__.._._g. ,y 1.... _. __. _ g. .j. _m.. . _ua 1.. ....,I.. __r- ...._-.._ _ _._8. _.= ~ =.- __ I__= _- - __. ~ ~ ~ - - 200 l...

r.._...... _ _.. _ _ _._.... _.

..._._e_____ ..f.".'*..._ 1. _ h_...._ _...._ _. _4 _._s_. ..._. A_. .._i_._ ..._.4_._..._...._.... ... _ -.J... .. _s.... 0 .3_._. __..._.1..... ..l__... _ _. _.. _..... _. _. _... _.. _.... ..I.... .......l.__....s... " 31".* 4 f.T. ?)* T* t r? :'U W'I. "Pm i t T"Il fTT1141Ti f711 80 t til#111tif *11It fillf f f fi111 'lf fi' n fP f711. tll t fIf r t 0 100 250 300 400 500 550 E l 2 G012R.B 7TT ' 7m *r m

DATA SHEET U.7 Spec. 9645.M-275.0 t-FRI-OF. TMER. MAL MONITORTWC Appendia y psy.11 Fower Ascension /$ystem Meetups ~ Sheet 3 of M l (Steam Condensing Mode) i i I i tre, Iso. me. M-1GG1 REVE =.... g Lanyeed No.E M.ZOZ. PLY . =. _ 8--' '= = Stress Prob.Wo. 63C 3.y. No I- - h,_-_4 _ __i___=_ 1200 v._ __._. _.. _._.. tes t.e l.i.t.t_m_tm _.__p._...__-_ ..._..s_... __.__t=__ = = Myst. from computer output G __r----I-- =.===t--. Analytical Values -J-Espected Limits 1000 4 AcceFeable Limite -------- =T _--t =._a _ __._ _ t __.__._.._.. _ _J, _ _ ___ _..j___ . _. _ _..._____.u_.__. _ _.. =y. _...._...... SCO _,. +, i w_ t= g-.. .._. 3._ _...i__. _ + _ _a _ . _. _ L. _ n . _.__-_._4____i___--._____. ,i l 600 E __._[_ __.___._:.____._____._.___._.__._._._.-_i e.____.._ 4 i l y. __i__. _ -4.. _,_ - _i_ _ .,+._-1 n. s un __.__.._._._._.._.r_ ._,J _.__ g,.w__ _ a i.__.__ t_ a, .. _. _ _ _ s. _.. .___s.____. .t_.._..___._ ...__ _. _ _ _i __ ___.. __.. _. _ _.. _ _- s _ r...i.. .._._s._._. . _ _ _. _..._ _ _._.._.._i__ _. _.. _ __. s.._.. ___ _. _-... .._8_.._. _..._a-0 ___..I _.. ..-_..._.t_.__ _...a._. __m _.... ........ _ _. _ _ _ _ ~ _ _._ s. i. _.. _...i.__.. 203 .-......:._._.._....._.a-.. " " t".". '. T *1"" t r ".. '7""l *-** *:71 l :1'"1l fiTil411t f711 tit t f t t ilflilt's tri fif t tt fit att.tif s t r finT'1.nitit ~ 0 100 250 300 400 $00 550 E12r,01201 T T **

F

,m . ~. - - - - -,, _. -.. _ - -. - - n n

l l r. DATA 31ETT IL1 Spes. 9645 N 173.o FRK-oP. TIE 1uut MOWIToM18G APP **d LE W Rev. 11 l Power Ascension /systen Beatuss Sheet @ of N (Shutdown Coeting Mode) Pre-ep Ise. No. N '661 REV.3 . mp ,.m. q.=._==5 - Ianyard No. E i2 GO Qm DLY Stress Prob.Me. (6 p.p.720 1: ::. -< - -l. _ !. _ . s 1200 . _.=a. -# .:..=.= -. 'r r.w.s u_.N...u. au..u.= c=.= r trite ti.te tear u _s _=== _,-g._.__ _=E Mver. free computer output G i__ ' = M -- --...J na t ca a ves ._._.4 1000

==- Espected Limits Acceptable Limite ----~~~- e _ _.... _-1 _...._..___-_.__i.___.__.. gg _....1._ =:=.; - i m _ _ i _ _. 600 _5 ..-4 _ -l_ -, .o i... . _. _ _. _ _. _ _ __1_ __l.___.._-_-,_-,_._ ._f.__._.. ...._ g_ e. 400 g3 4 _. _ _ _ _ i - -- _. M_.._ __ __ ___.-__._3._._. ._W._.._.__,....... .., e.. _ __ g, _ _.. _._-__4._.....___., ... i __. _. 1 _ _ _.8. t .,=F._.__.._..... 200 i .-s._._ ..t_ ( ._. _ i _ _..i___._......_... 8 i t I _-_t...__ .... l ........ _ _. _ r. y.w. _.- _-.. v .e .._T_* _. __ JE*....m. _ _e._< s_.. _..y ..._._.. _... 4 urs m_ s .._.J. 0 ....._..3 .. _ t ~_ 3.... ._....__r, __. _f.._.. i .._i_.._.. _._l..._, .... _....... _.. _....8._............... t. _r.. _ _. t.._.. . _.. _.. _..8... _.. "L"W il m l1171 ' ri f12 ff"f1 TL"7171ri h Tfil lTTH u 11 t fT11 1111!!!i11111111111 riit tf li t :13.tittt i n fiMT11 tt'If f fi t o too zoo soo soo too s5o El20012RB7TT r= *r s

+ am surr na sp... sus.n. n.o l rar-or.' turannt nourrone rt App **dia e an,. 11 s r a. t /sy. tam masup* sh..t,,$,, e 39 l (sn td c tsas mad 6 Pr., z... s. M.166 i REV. 3 ,_,,_,g.=.- .m

==nm &asyand s.. E 12G01204 DL Z =- stress Preb.W. 46 3p.565 __ _ _.[

.nrw.s.u..w I_n:._us:n.:n m.

. s.i.t.mitasr

==.:
=.a=.: =._.

- = - 1200 _ _N C ':2:i:= - --= a- _ :. ~ :. n:=:'._-t = =- 3 = Mwat. free..mPuter output G -s r u = _-._.__J_.=_-

5. i:= _ -

=- Analyticat Tatu..

.=9 r._=._.:= - 1000 = =_: Empest d Limit. i = Acceptable Limit. -------- -E =. : __....I. _ _-< .____r,__,_._____._._ _...=.._. _.. :s. 1

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--. ~, 4_. J. _ _ - _ 1*00 = .? =: Acceptable timits -------- i <.. - ^ - - r ~ _... #. - =

=::

N @ "" 6* p- -. ._d (- --g 3 . sus ..mse. g. .m.- ..mm - - }..- d.. q m.me .sL..m. m I, .g..-.-. m.- -WW -m.. _- - a .h.a::W 7. _.1 _-~. i__. 5 ~ - + -3=.. Uh. h P. - .l. e. g - g .mm ..__e.-& M~._ h r. +-m. ..- M_ ......N p.. y .6 ..m._-...h.... --4" .9. ,-.h f 4__ - .-.-e- .d d ~ ,J m.m. l.m. 3-W: + f -.{-- q.. .... _W --3,. .p. _ y. _. _ g A ,~f.."-.. g --m. r- - -u_. ..e., ed -.u ......g. ..m a .ai J d h _.e .6

h

__._A,._.__.g_ .M_ 6 M I-g _=....._,- .m .mme.m _sm.._...__..,._.._.-mm.m.m.m. gg, ,._.m_. _- _. @.. .g hl. L_... _. w..~._...-3_...._.....-. g.m_ E ms... .......n. .m. -- 6 ..M..-.. _..._...., g, t M.. r ...._,Am_. l -m .p .-..e. .e.s..., m.u m... -.m.mm... 4 . gr p. .i...m._ w .....m.u-... ..m. .mi.... .......mm.... .i. h. 5....._. .i.mm... u--...- .m.m. ..a O ._..m.m .-.=4.n.m..... e mm. .....m.m i ..m...--.. .--.L.-. i .I ....-m.- .--g.. .F -. e.....m.m.. m.....mmm-.. .....M.. .s.m -..m-4.mm. s f mm ...g.. .mmmm. m. -e. .-.n .m.... ...mI _.... mumm. -mM. i ...,m.. pr I ._-m_.. ....g..

e. -

game._. e.-. - g _m....m u N...e.... .....m.. mem.....s ....--..mm.. ..mmm 0** .g. OW W p. .e y . e.... .....m_. .= . - *. -

j- _ _

6 N*.. ee - -...M- .M* ..*e6-ge....-..... _. -.. -. M.- .-. mum.*a. M.-.- 6* J m.- e g..-- e e..m "d -. m p.. p E oumpu e. m... .m..g .M M. -. tM..._W .mmm ...mm - *.. .m- .._e... m ...m. ge p-. em.m l. .m.n.. .e.... a. l

e
.g

..ma .p-..u.. ..,_.e., p.u.m.mm. m ...u... m.m 1 -.3...__.-.-. --. m-.- -....m. ....m....... .3 ._m..-. ._._.m. l. g-l ..l...._...................... a_... ....._-r..-...m..._.I.- g. ..-m. .-. s..... {. -...... -....... ..EW" *3""".."Wl ; ff.*:U""I'.U:'1"T.11"."31."1 1.*4*.C e"T ITI'Il{ I'llllll{Ill 'llllll1 H tillgli "Ifilf,'Tl (Tilll*ll 0 100 100 300 400 500 550 sucot3nsn Temp *r v w, -..,, - -.. - - - - - -. - -. _ -...,. - - - ~- -. - - _ - -.

MTa SMEET U.6 Spec. 9645-M-275.0 PRE-OP. '3.ERMAL MONITORING APPen$ia U Rev. 10 E I E*D SheetiI er 60 Fre-oF Iso. W. N-16BO REV-? _ Lanyard No. PalCro. PACS L*M : Stress Prob.Wo. .p t st D.P. R O F ~ i__ - 1200 EEh_ e.J_:H_m._= n:zu2J n:.2dAT2tzt " = ~ _. _. _ _ =.. =. _ -g EE Mvat. from computer output G i--

==- Anal eteel values ____m_..__ _ _ _,. _,. - 1000 Expeete

Limits EE:

Acceptatale Limitts --------

_ s _-

_d.._e_

== _. _. 1 - ___r______ __.___t._._- n ..__._1..._ __._i_.__ _. l.~.~__~_~._~.~.~_~_~__~~~__ _ _~. _ _ ~ _ ~ _. ~. _ _ _, - ~ - ~ '. ' - ~ ' _._.4 , _.. _.. _. _ _.. _4 = _.s._..._ m._ _____ _ _ .__ _ _ _._t__. i ... _ _. _.... _._._..._... _= _ - a. vs, g a. E'___._._..__....._ _ -_. s _ r........ s-_._-_.____-... _... ... _. _ _._ _ _.. _. _..._.._i___. _1 ..._r____ .. _ r .1 .p _...__.._..._..__v_._ _ _. _. _.. _ _ _ a_..__,__ -a m _ _. _ _ 0 = _. _.... _. _ _.._ar __ _ m. _s. . __..a.._.... _ _ _ _... _... _... _. _...... __. _.,._....__...I...._.._ ene.. _= e.. ..._I."...... 9. n l

9. p ww

._..-..__..___g..... - zn. u:-..- n. r :::Um =m ::n s =::i. n. trU.T1 IT tit s'llit s spit "t t t tt p i' Hi t' i nt 01 P1 m,1 t 0 100 200 330 400 500 550 321C02303TT Temp

F m

I i 1 ll DATA S ETT g,$ Spec. 9645-N-275.0 f_ FRK-OL ' DERMAL Nettttgam_eq APyendia W Rev. 10 R EAT-M Sheetier 60 - Pre-ep Iso. 5.. M.1mo REv3 ~ ~" , = Laayard No. R2 tGo3M 4 DLL M Stress Prob.Wo. .png - 3.P. % E- -1200

r..

smet wi m_i..s u_u_m_o-~~ cu.. s,e. rtist:r f p e.__._ = EE Muut. free cementer output G ~~ =J: Anal titel Values =_ ..--n- - 1000 =::: Espected Limits EE Acceptable Limits -------- = =. _ r. _ _1 a i .w .o A. .,,- -800 I__ _,._._ -. 7 "t 7 -. _ _ '.. ( - _ - > _sm - .._. 7.._ - s.m 4 W. = _ - se i a g f ___.a -m t _. _ 3 _ _ _ _, ..._.e. ..r_.. _-. 1 _. _ _ _,1 .ns.. _ W52.- __ Eb.Pll=1. _ / _e_ _L_ ..--1_._.__ g e ,_-s es _ -. ,. + _ ._,sr WI _.p _ _._._____1__

v. g _ --- _f._._.._

a y.. . _......g-_ _... _. p as ......._._t... _....1.., .._ua.r.._._._ . - C"._.W.... _. . - 200 .p._- v .... n. P...g.;, ..__=g.. _.___..pr. y = s_i_. . 4.......... ..-l.... '"".Ml:. _.... . 1

6....

0 .r.... _. _..........l..._.. _3._,.. . _........4... n._.. ..t....... .t.... 1......... _... _. __. L _ r _.... _.. _... _. l _m__...- _. l 200 )

i...

a.f5.*lWi e l'f.: ne..... i.. II:3 n."ED.*.iWif"Tl IWi1THilill11111 3 181881 teIIItal' 'I t'll"m it111t' tl i l 0. 100 20 300 400 300 550 i 1 321002303TT

Temp 'F j

m r --_--. ~.,..--.- - - ---c-

] l BATA SWE7 U.4 Spec. M45-N-275.0 1 1 t-M-Oh TERMAL MOMTORDG APPendia g 3,. 10 Sheet 14 er 60 Pre-op Ise. pe. M-1491 REV 9 Laeyard me. mig OS401 AA -~ 5 tress Prob.No. Jtg o.P.9g =2--- +1200

ntima um u n ns. ~~onnz:t.r.i.r29tzt:r

= l = ptvet. tres computer output O-E_E Analytical values - =J: ~_.. E., \\ + 1000

.

F.mpact.ed Limits M Acceptable Limits -------- .-=: -ag, i e>.p M4' _' m g .I d- ' .e. t -.=I Y_5 ~ ~ ~~ M$~) ~__._f 9,_- sin p i g i m h r w .imd. -...e m p... ..p 4 I _M_ am a~ p..... _sp.---- -a. H_ +_._f. I. .w. i .-.,_..... -........ q .-.-6-.--, ^ I__"- s.._ -.m -.-..-.-%w%1 -ms- --m -.w ,g ' '8 Vw 6.A. 1 -a..-- ..m. i ...l - - - - + M_ j g _m & -.:.",~F.__'...-- m D -.. _...--..I..-._- .,-f.-. r -..-v .ms".

j. _..-

......q._..-. .y. 3 .=.=. se . /-~.." -.._l.......-.3.--. .e- ...-....e..- .w I-s.p.. -.,a.. 'M. -,.+.,F...-3....._.s....... -.-...I.... 5..-.- + 200

.a

-n.. ....m....... I .-mme =.. ._. A -. 4 .m. . =... . P..I ....f.-.< .m _. -....i....r.-..-. ,,.,,i""."."r--.. -.e..--. A s..-. ..a......- ..I....... 4 .r .....-...I...._ .I e. g. m . = _. - i . 3...... 3.. r ..m .t..... i .-m 1 t .m.-._......~._.._......... m i. a ... l t. 1 .3. - 00 ~ i - xrt =a r.. m : rT= u....u... w i = 31.rTt.*.itn r:m tit 'ts N e tit:11tn 4:s tip iritte.t fy";T1 F11 tnt 4 o 100 200 300 400 500 330 i i i s2:co24om T, *r m -.--. ~. ..----__,,..--__n.

BATA S MIT_ P.6 spes. 9645-N-175.0 FIE-0F[ TRIOmL MONITQRIBE APPendia g Rev. 10 j r-OroclzAa MAT-w) sheee.[$, e 6 0 1 Fre.ep Ise. No. F -1M1 RNJ .l Laayard No. B.M G o.M o#'Putim x Stress Prob.Be. ,,2 [8 p.p. Jg

=:"a

. - 1200 art w n _w w u i_ m +- ~ ~ j n u, s - .a ,2 _i E Mwat. free computer output 6 - = ..=J=_..- ..=: E Analytical Talues = - 1000 =

==.: Espected Limite

.=_=-Acceptable Limits -------- =_:.: 4 -=u f 300 i.___ .~ ~. _... _.

===z==:. t ) om 1 ._.= . _... __~ = __._.1__._. . _. _, _ ~ _ .. _ _ _ _ _..__t.-. ... _....u_ ...._. _ 1__. _. _ _w ..__.g a __1__ .... _.. __3. _ ___ ..._. % y.w.-p........ %_4,____.___._3._. _.. _. g._ S. -__. _.._.....__3__-._.._._. ........I.- .... s __t.__. ..... _ _.. _.4........ _ _.._ _ _.. _..- _ _. 1...__ _ .......*M _...... _...-........w.."g _...,..._...._____._8.____.._._#r.. _f _. M ....._ f"."". *1. s . _.._...=...3"".P.*.'."._. _. _.... ... _ _.. _....1... (__.._,_'""".J f. _e ,...i ...4........ .. N. ._..o. ._l. 0 ""Ml*. ....3 .._.B= 8 ....._.E. %.. -......... t...... %...

a....

-.i_. n. ~..... =. 1 ( _.. _ _..._t."."_.. 200 ..t. i .........i.........1 ....g.-.. -.M.. I. h. l h fl h l \\ l l e 0 100 200 300 400 500 550 321G02402TT

Temp 'F m

-..,--,..n-- --- - ------..- - - n. ..,,,---..---,.--n

1 DATA $1EET U.6 spee. 9645-M-275.0 t PRI-OP. THERMAI. MONITORTNG APPerdin y gay, 11 g-NE M*D Sheet 16 or 60 Ib Pre-op Iso. No._ N ~1 6 9I i UVI .-...in m vi w w=8 ~ = I,anyard go. p_W-M d71 t L (v i =- -_ _[_. _ Stress Prob.Wo. 918 DYP. F5 I 35:. % __4.. / + 1200 _.. _....a_.,. i _... _,.._. . c_ _ n,. :m _ =- __ . ___.T_._:=_. E Mvut. fros computer output 0 i__ " _...- f - - _1.... Ivtical values +1000 =- ~- k.xpected Limits %.7_,q _ c -m E Acceptable Limits -------. __.._s. =- . =..._i t _~ ^ _t . 800 ..3.__...._;... __e.__ .2 _ n. ~ 3 _. __.,y 4.- . _. _.._-_.._g ._ 1 _.;.g

=_ __..

g. _. + .-i 2 , ~_ __. ._...._....._. __ _._ __n__..... _,_i. _._ _....__..._+s-y J L..,,.. _f.. .a.... _._~.___..._--....4_ h. , le m,. _.._.n_.. _.,r_- _m t. ..a. n.- p.f.-.t'--.----..- _ ~. _ -.... _ -.. Q 8._._ b.J. _. _ l. 4f ; 3 g, c".' _" __.. _,.... .; _ ). _- _ ._.l_.. _. _ ._. __.4...-_ _ _ r_ _ L." , 200 __e.... ... _.. _ = _ _ ._._e_._ ._.1_.____... l. ........8_._...,.. .I. I ..__s. s_._. l.. _m._... r=. ,._...~ _._- - 203 =_s p. l - .m..'-..'"- r :n =-: n. -.. e.... -.; l...s *: : --:'.m -v n ti f m o'n i "* o ' " ' m-UN r -

~ -

i 0 100 200 300 400 500 550 1 321G02402TT 'Terp 'T m 7 - - _..__- -.- -,__-.-_ __ __.- _ _ -. ~___ .-,_____-.m,._m_.- .m

l i l I l IIATA 375tf M Spec. 9645-N-275.0 FRI-OP.' TIIIlOpL MRf1TORING APPendf.m W Rev. 10

- W Sheethet GO

\\ l i I Pre-ep Ise. se. W 1s es Rrvi i Lesyard us. RE U Mem oi btr N Stress Prob.ne. MJy 3.y.1M ~ smi m u.um...u_u _m ' +-- - w w +1200 __m 5 Muut. free computer output G

=.

Analytical Values =.=_ +1000

=

Ezyeeted Limits Acceptable Limits --------

== p

==

g a __ g_ e i +600 g=:.:- _. _ _.. __~ ._= _m. i_ t _a _-._ =_. - __ i 'l g __.i___ i _._3.__. ...__g_a_ .g. _m._ n... _.. ....._g w i Se. .... _......a _.L._ -..9."."..,.._...\\.._ __... +200 s._.._ _..a.__ _._I___.. ...3....... . 1. _... -._ - _.-i._ _... _............. s. .-._._.... J_. ... n..__a-. I _a_. ..._.J._......... m.m > L m._ ___.8..._ ....I. 4.-........ _. _ 4,. _.... .. 1. T"". .1..... ~ u ..w ._......S..m.M..,. g_......M. ._.g.. N, .M h Ste.... . =.... *. ..._.....3_._ I M... .=. =. ..e ....-_I."." ....a..=. =... =. g eg.L .... _...g...i................. - zmt:rtrm.'TTrt: rt::t::21-=T m rz:2irtz:.:.;wirTt m.tiFi111111m rtie:Iti. m otitt' ftstirift ImIr #1 0 100 200 300 400 300 350 n.r.v. 7.=, *r c 1 I

4 i RATA SIETT RJ Spes. 9445-N-273.0 t-i - - FM-OP. TERMAL MONMOME Appendia y go,11 Power Assensisa/ System Easteps Sheet,I [,ef N i 4 j Fre-ep Iso. No. f-1696 REV.1 m =l i..... c. ... n &separd No. E M to M.U I)t1 q.=.- =s " MMQ Sitess Prob.Wo..po.M p. p, 1 9 s'

.=.

- - = - - 1200

==m.=._--

s i

p:.:s.m.w. i_s:._= cm n:jte ite ninnu:r o. , _ ::= _ _ g=== m m==- f=._==. - - :=- h =

4

---u=w

== :-- - - "" 9 J i = p!vot. free seeputer output G = m ram =~

=::-,J.

Anal tical values t =..- : : 7

== Empecred Limits 1000 = i

=*

Acceptable Limits --------

ll= = a:. =J.*i_

==

g-.- g _.= m --e j A e .i....._.. 2 _. ~, _ _. . :=Q' _ ~.1_- S=.""7 1 4 800 - -..I'.** I i M _.-. P.- _._..*1 s . _mp.. s -e.-- .-a i..,. m. -M-- O' :==J l J-_ 1 .w.6:.

==.==.*J=, l _- - - ] A e-" __f_r.. _. _. = _,.. 5., j __4. _. __-L.

== _.: _. _ _ r g .G ,-Q-t

===== aus j = = l r_ -- =. _., a._ - ..= L _ E=== i =_ =. _ = '. _ i=_1=J - W ._.p:.:.E. j I:= < "+ - .=* F _. C _. -.-"4".._"" :=, .._ i _. ' _. '. _... i.. g l, _.= _"_lll: 1 _...

_.y""* i _

._ __., _5:==, "_""._._._'*_'.._._".;_=L._ _j d ... -.... p_ * - _. _ g = _=, T :' :'l" ; - .._._.__.g__ .=* O ""~~~*?** 2""""*.**. O i

*: --l".

, =

j.__. __- e. _ _... - A,y

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I'"; * *"" 1 "" *. *

=": =" * - * * *? : "=" =lll *-"'" t =" ""- - ":" :

98n I

4 &.g.. X_ eww ......l_.. .8 __. 1....... -...- -.. - - = 1.- =. fM-. =4 J.:4. 7 ;;.=. l.;.

...... l. =. * =*'*: :"$

,-. l =.. :.". ! *. =.Ef. F. i * *- *.. : : - *= TV -. ~. ' n. = -- : -- - m - . -.. l __. ......_ 8 2 " "." ' ' F * -""...._1-l l=".= _ :-".".=l._ ........w... ._....4.._........_._. 3 . _._i. ......]8._....... '....

8. JaZ..........y..

8 'J. ; ;..* ' *J.. *.* :*..:.. _._ : l:= :.*.* *.*.":._;.*.. ._.l... l l ....l" ............=:.=.. .6 it' J:J '" t.g= * ::? !. 3".*. """ y./ -... _.,_ iaJ ;

:.;*.=: j l

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. = ;. '....

!, J".;.; ll*J. l'.. '

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.;. = g W'87 F f1Wli r!U ft"I'm: rtTTI 11Dinfigu11t ffli tilf ff f t1titif fJtti fif tttttf rit.ittlet r)ruffitf eff tfihil i l i i e soo soo soo soo soo ssa l I l E32Gl0901TT wp *r m i i l l l , - - - - - - - -. -.. - - -. _.. -. - - - -. - ~,, - -. - _. --..r,- .wm.-

BOP Piping Thermal Expansion IC88-ST05 i J 1 5 APPENDIX II I NPE CALCULATION MC-Q1111-830027 PIPING THERMAL EXPANSION E\\'iLUATION DURING NUCLEAR HEATUP i 4 i t t l 4 l i i n ? i i 1 )

NUCLEA R PLANT ENGINEERING " f!*n*/ p n9 =n ns m DESIGN CALCULATION / ANALYSIS i PIPING THEFF.AL EXPANSION EVALUATION DURING NUCI. EAR HEATUP TITLE: J C ALCULATION/ AN ALYSIS NUMBER: Mc-01-111-830027 REVISION: 1 AFFECTED SYSTEM (S) : Multiole GRAND GULF NUCLEAR STATION, UNIT: 1 Q STAMP [. X SAFETY R, ELATED Q-NON SAFETY RELATED FOR SAFETY REULTEC DESIGN VERIFIERS STATEMENT: THIS CALCULhTION CONFORMS TO NPEAP 01-305, REVISION 5 , DATED 3/5/e4 THIS CALCULATION SUPERSEDES CALCULATION NUMBER "~a PRELIMINARY CALCULATION FINAL CALCULATION X J!/2 I PREPARED BY: DAT E: (RESP NS16LE ENGIN EER) b DATE: VERIFIED BY: / / /Aff$ 'A R EVIEWED BY : DATE: gg REVIEWED BY: D A TE: ( PFt l N 't A L EN INEER) DATE: O REVIEWED BY: / 't ouAcl TY TNG6N E / "w" #4 APPROVED BY: D ATE: NGE[' " / eenu se.,, pgv 3 a- - - -

CAICLuTION NO.: MC-01-111-830027 REVISION NO.: 1 SHErr II COh'I. ON SHEET III ORIGIE"DR A DATE 3/a.//y DESIGN VERIFIER prz, DATE w/fz/py l REVISION STAIUS SHEET DESIGN CAIfUIATION/MG1YSIS EVISION SLWARY REVISION DATE DESCRIPTION O Dececber 19, 1983 Issued For Use 1 March 12, 1984 Revised Design Verification Checklist SHEET REVISION STAIUS SHEET REVISION I 1 II 1 III 1 IV 1 1 and 2 1 3 thru 21 0 21A and 22 1 APPENDIX /ATTACEMEN'T REVISION STATUS 1 APPENDIX REVISION l A (Sheets 1 thru 167) O B (Sheets 1 thru 82) O C (Sheets 1 thru 26) 0 D (Sheets 1 and 2) o E (Sheets 1 and 2) 0

CAICULL"7ON NO.: MC-Q1-111-830027 REVISION 10. 2 1 SM III COTE. ON Sm IV ORIGIIMOR #46/ DATE 3//z.//</ DESIG VERIFIER #>s DATE g/fr/fy PROCEDUFAT., CDGIJANCE STATD'DE Calculation MC-01-111-830027 has been revised to correct deficiencies identified by NPEI 84/0147. The calculation meets all the technical requirements of NPEAP 01-305 Rev. 5. Please note that the heading on the old calculaticn sheets have not been changed and Design Inputs is Sheet IV of the calculation; these changes do not impact either technical content or nu.ccedure cca:pliance of NPEAP 01-305, Rev. 5. (See NPEAP 01-305, Rev. 5 Paragraph 6.10.1 and NPEI 84/0383) O O e S O e

CAICUIATION NO.: tr-01-111-830027 1 REVISION NO.: 1 SHEET IV CONT. ON SHEET 1 ORIGINAIOR der DATE _y//z//y DESI@ VERIFIER ATu DATE 3h2/PV b DESIGN INPUTS DESI @ INPUTS:

1) - Bechtel Specification 9645-M-275.0, Rev.13 2)

GE Test Specification 385HA710, Rev. 1 3) GE Test Specification 385HA710AA, Rev. 0 4) GE Acceptance Criteria NEDE-25388 5) IVDR JB1-1961, Rev. 0 6) NPEI 83/1020, Trending Plots for NSSS Piping Thermal Expansion 7) FSAR Sections 14.2.12.4.3, 14.2.12.4.5 and Q&R 110.33 8) NPEI 83/1017, Histograms taken during nuclear heatup NOTE: All Design Inputs are final J e e i i r i 1 --~,----. -. _---,~,,,_ --.- .-_.-,_.,,n,,-~ n.-,-

l CAIfUIATION No.: MC-01-111-830027 REVISION NO.: 1 SHEET 1 CONT. ON SM 2 ORIGINAIOR A DATE 3)e/jy DESIG VERIFIER pr u DATE 3/n /pv /~/ TABLE OF cot 7fDCS l PAGE COVER SHEE.T I REVISION STAIUS S M II PBOCEDURAL CDMNCE STA"AT2ET III DESI@ I! GUTS IV TABLE OF CONTDCS 1 ~ SECTION 1.0 PURPOSE 2

2.0 REFERENCES

/ SOURCES 2

3.0 PIPING EKPANSION ACCEPTANCE CRITERIA 3 4.0 PETHODOLOGY 3 5.0 EVALUATION-RESULTS 5 6.0 DISCUSSION 20 7.0 ASSINIIONS 21A 8.0 COTt.TER CAIfUIATION 21A

9.0 CONCLUSION

22 APPDDICES A DATA SHEETS B TRENDING PIDIS C NUCLEAR HEATUP EVALUATION SGERRY D SCRIBE FRRK DATA E AMBIDTI IOG l i l .~,. -..,- - -.. _ _ _.

CALCULATION NO.: MC-Ql-lll-830027 REVISION NO.: -e-/ p,f ORIGINATOR'S NAME M 4. M,,qgk//2.//5-/g 3 SHEET 2 0F 22 DESIGN VERIFIER'S NAME # A lf/ p mjy DATE: /1 /i_r,Ny ~ f M-1.0 PURPOSE The purpose of this Calculation is to evaluate the piping thermal expansion data recorded during nuclear heat-up. Piping movements were recored at locations identified in specification 9645-M-275.0 (REF 2.1) for Non-NSSS Piping and Specification 385HA710 (Ref. 2.2) for NSSS Piping. Evaluation of the data for Non-NSSS piping was performed by Nuclear Plant Engineering with Assistance from Bechtel, GPD, however, NSSS Piping expansion data was evaluated by General Electric (San Jose).

2.0 REFERENCES

/JouRCES g

2.1 Bechtel Specificatio'n 9645-M-275.0, Rev. 13. "Preoperational Piping Vibration, Thermal Monitoring and Dynamic effects testing of piping systems." 2.2 General Electric Test Specification 385HA710, Rev. 1. " Piping Startup Testing." 2.3 General Electric Test Specification 385HA710AA, Rev. O, " Piping Preoperational and Startup Testing." 2.4 General Electric Acceptance Criteria NEDE-25388, March 1981, " Acceptance Criteria for Vibration, Thermal Expansion and Strain Measurement for Preoperational and Initial Start-up Testing of General Electrics Class I Piping Systems." 2.5 NPEI 83/1020, General Electric Memo to all STD&A Lead Engineering from 0.C. Islas, dated May 4, 1983 and May 19, 1983 and Memo to T. R. Enright from M. R. Hieb, dated May 18, 1983. 2.6 FSAR Section 14.2.12.4.3, 14.2.12.4.5 and Question and Responses 110.33. 2.7 Project No. NPE-3-223, Calculations referenced in Section 5.0. 2.8 Startup Procedure IC88-ST05, Rev. 2, " BOP System Piping Thermal Expansion Monitoring Program." 2.9 Startup Procedure 1-000-SU-17-H, Rev 1 " System Expansion Heatup." 2.10 NPEI 83/1018, Speed Memos during Piping Thermal Expansion Program. 2.11 NPEI 83/1017 Histograms during Piping Thermal Expansion Program. 2.12 NPEI 83/1019, FDDR JB1-1961, Rev. O, General Electric (San Jose) response to thermal expansion data taken during nuclear heatup for main steam and recirculation systems. 2.13 MPB-83/0522, Feedwater whip restraints 8A, 83, 10A and 10B

s. REVISION NO.: O SHEET 3 0F 22 j ORIGINATOR'S NAME W./_/ /C / z./ g /y ; DESIGN VERIFIER'S NAME pen ja f-DATE: /z/Le,41 2.14 NPEI 83/1019, FDDR JB1-1961, Rev. 1, General Electric (San Jose) i response to thermal expansion data taken during Nuclear Heatup for main steam scribe marks. 3.0 PIPING EXPANSION ACCEPTANCE CRITERIA Thermal expansion acceptance criteria for Non-NSSS piping and NSSS piping is described below in Sections 3.1 and 3.2 respectively. 3.1 Non-NSSS Piping Piping Expansion Acceptance Criteria for expected and acceptable limits was generated by Becheel, GPD in Specification 9645-M-275.0 (Ref. 2.1). The expected thermal boundary limits are based on 225 percent of the analytical value at rated condition. The acceptable ther=al boundary limits are based on 2 0.25 inch or : 25 percent of the analytical value, whichever is greater, at 550*F Reactor Pressure Vessel reference temperature, unless other wise specified. It should be noted that the acceptable limits are not code allowable limits. Also, recorded piping thermal expansions are acceptable when they are within expected limits and/or are within 1/8 inch ot analytical values. This is to account for tolerances for temperature distribution, transducer resolution and temp <arature resolution. When recorded thermal movements exceed expected values, stress analysis has been performed by utilizing existing temperature distribution, recorded piping movements at monitoring points and snubber / spring readings as applicable. Recorded movements will be acceptable if stresses in piping system are within code allowables. 3.2 NSSS Piping Piping expansion acceptance criteria for Level 1 and Level 2 conditions was provided by General Electric in Specification 385EA710AA (Ref. 2.3) and acceptance criteria NEDE-25388 (Ref. 2.4). Level 2 criteria is based on calculated movement plus tolerances for temperature distribution, transducer resolution and temperature resolution. Level I criteria is based on the code stress allowable for a predicted movement plus tolerances for temperature distribution and transducer resolution or predicted movement plus a tolerance for temperature resolution, whichever is greater. 4.0 METHODOLOGY The process of piping thermal expansion evaluation and the methodology for evaluation of data at intermediate temperatures is described in Section 4.1 and 4.2 respectively.

RiviSEEEs0.: 0 ~' "~ SHEET 4 0F 22 ORIGINATOR'S NAME M /J /a dr-/$3 DESIGN VERIFIER'S NAME A/URT"~ DATE: /24c-/n 4.1 Evaluation Process Beginning at 200*F reactor recirculation suction temperature, piping thermal expansion data was taken at approximately 50*F intervals and at other temperatures requested by Nuclear Plant Engineering. Recorded data (HISTOGRAMS) was delivered to Mike Meier of Nuclear Plant Engineering from Mike Hieb of Startup. Thermal displacements were determined for each temperature interval at all monitoring points (Lanyard Pots) using data sheets for data reduction (Appendix A). The displacements were then plotted on trending plots (Appendix B). At each plateau, engineering evaluations were made for all recorded data and were documented on the Nuclear Heatup Evaluation Summary (Appendix C). The results of the engineering ~ evaluations were transmitted to the startup supervisor via speed memos (Ref 2.10). If at anytime during Nuclear Heatup, a new ambient reading was needed to be established for a particular data point, the new ambient was recorded in the Ambient Log,(Appendix E) and the subsequent thermal expansion data sheets were revised. During the evaluation it was determined that data recorded near main steam guides was incorrect due to the faulty installation of the lanyard pots. Therefore, data was taken manually at these locations using scribe marks (Appendix D). 4.2 Evaluation of data at intermediate ta=peratures. 4.2.1 Non-NSSS Piping 2 If the recorded thermal movement was within the expected boundary limit, the testing continued without further evaluation. If the movement was within the acceptable limit but exceeded the expected limit, the testing continued but the data was evaluated. If the data was outside the acceptable boundary limits, the plant.was put on hold in order to evaluate any i potential problems. In the evaluation process, the following considerations were made: a a. The recorded data was checked for reliability b. The assumptions (line temperature distribution and anchor movements) used in generating the acceptance criteria (Ref. 2.1) were compared against the recorded plant condition. c. Walkdowns were performed to identify any interferences. d. The recorded data was compared with snubber and/cr spring readings taken in its vicinity as applicable. \\

REVISION NO.: O SEEET 5 0F 22 ORIGINA!0R'S NAME g. /(.A // /a//4/n DESIGN VERIFIER'S NAME 2rf'dl.<_)_it-DATE: n hs/a ~ / If the data was questionable, then ano'her histogram was taken. t If that histogram still showed the data to be questionable, then the lanyard pot was checked for operability. If the lanyard pot was demonstrated inoperable, the testing continued and data at this location was disregarded until the lanyard pot was replaced or corrected. If the lanyard pot was determined to be reliable / correct, the recorded plant condition was compared against those used in the specification (Ref. 2.1) and where applicable, the snubber and/or spring readings were taken in the vicinity of the pot. If the assumptions used in generating the acceptance criteria was different from the recorded plant conditions, the recorded condition was evaluated for its.effect on the trending plot. If it was judged that the recorded data was compatible with existing plant condition and the trend was as expected, the testing was continued. When the recorded data was not compatible with existing plant condition, walkdowns were performed to identify any possible interferences. If interferences were, identified during the walkdowns, they were removed in most cases. In some cases when interferences could not be removed, a stress analysis was performed at existing plant condition and at rated plant condition assu=ing those interferences. If the stresses were determined to be within code allowables at existing and rated plant conditions, the testing was continued. 4.2.2 NSSS Piping If the recorded thermal movement was within the Level 2 limits, the testing continued without notification to GE. If the movement was within the Level 1 limits but exceeded the Level 2 limits, the testing continued and GE was notified. If it appeared that a Level 1 limit was exceeded, the testing was put on hold pending GE approval. 5.0 EVALUATION RESULTS Evaluation results for Non-NSSS piping and NSSS piping are described below in Sections 5.1 and 5.2 respectively. 5.1 Non-NSSS Piping

5.1.1 System

B21-Main Steam Relief Valve Discharge to Suppression Pool. Stress Problem Number: 215 and 218 Pre-Op. Isometric Drawing: M-1680 and M-1681 Calculation Number: M-275.0-215-1-T and M-275.0-218-1-1 j

REVISION NO.: 0 SHEET 6 0F 22 ORIGINATOR'S NAME A/4 /b /z3'4/BT DESIGN VERIFIER'S NAME M f// W DATE: / z/d-Mf3 / Evaluation Results Summary: Acceptable. Piping thermal movements were recorded by six Lanyard pots at two locations in various directions. Recorded thermal movements are within acceptable limits for three Lanyards, outside expected but within acceptable limits for two Lanyards and outside acceptable limit for one Lanyard. The data outside the acceptable limit can be explained as a result.of a fast transient (approximately 120 seconds) which did not allow the line temperature to stabilize. It should be noted that the recorded line temperature at the monitoring points were significantly smaller than design temperature. Therefore, the piping thermal movements during Nuclear Heacup are acceptable. The evaluation result for each Lanyard pot is given below: a. Lanyard Number: 321G02301DLA ~ Pre-Op. Isometric Drawing: M-1680, Rev. 2 Sheet 36 of Appendix B Evaluation Result: Acceptable. Recorded ther=al movement is within expected limits. b. Lanyard Number: B21G02302DLL (H) Pre-Op. Isometric Drawing: M-1680, Rev. 2 Sheet 37 of Appendix B Evaluation Result: Acceptable. It should be noted that recorded thermal movements are outside expected limits but still within acceptable limits. However, since expected thermal movements were small and recorded movements were within 1/16 inch of analytical (Calc. No M-275.0-215-1-T) values, piping ther=al expansion is acceptable. c. Lanyard Numbe,r: B21G02303DLL (?j Pre-Op. Isometric Drawing: M-1680. Pes. Sheet 38 of Appendix B ~ Evaluation Result: Acceptable. It should be noced that recorded movements are outside acceptable limits. However, because of piping geometry and fast transient (approximately 120 seconds), which did not allow line temperature to stabilize, piping thermal expansion is acceptable. It should also be noted that recorded movements are with 1/8 inch of analytical (Calc No. M-275.0-215-1-T) values.

LALccLAAAud Av.: au vi. 4-caww-. REVISION NO.: 0 SHEET 7 0F 22 ORIGINATOR'S NAME //r/ 4 M /2 //4 /f' DESIGN VERIFIER'S NAME 7%9/)M DATE: /g/g& t / / d. Lanyard Number: B21G02401DLA Pre-Op. Isometric Drawing: M-1681, Rev. 2 Sheet 39 of Appendix B Evaluation Result: Acceptable. Recorded thermal movement is within expected limits. e. Lanyard Number: B21G02402DLL (H) Pre-Op. Isometric Drawing: M-1681, Rev. 2 Sheet 40 of Appendix B Evaluation Result: Acceptable. It should be noted that recorded thermal movements are outside expected limits bute still within acceptable limits. However, since expected thermal movements are small and recorded movements are within 1/16 inch of analytical values (Calc. No. M-275.0-218-1-T), piping thermal expansion is acceptable. f. Lanyard Number:' B21G02403DLL (V) Pre-Op. Isometric Drawing: M-1681, Rev. 2 Sheet 41 of Appendix B Evaluation Result: Acceptable. Recorded ther=al =ove=ent is within expected limits.

5.1.2 System

B21-Feedwater Piping Loops A and B Inside Contain=ent Building. Stress Proble= Number: 74 and 75 Pre-Op. Isometric Drawing: M-1653, Rev. 2 Calculation Number: M-275.0-74-1-T, M-275.0-75-1-T, and STR-20. Evaluation Results Summary: Acceptable. Piping thermal movements were recorded at ten locations. The recorded thermal movements at rated vessel condition are within the expected limits at six locations, outside the expected but within the acceptable limits at two locations, and outside the acceptable limits at two locations. The data outside the acceptable limits are within the code allowables. During walkdown, at intermediate temperatures, various interferences were identified and removed. Also, during a walkdown of the Feedwater piping at rated vessel condition, it was found that the Feedwater pipe was touching whip restraint 8B in the +y (upward) direction. A stress analysis (Calc. No. STR 20) was performed by utilizing recorded line temperature and design cold gap (3/4 inch) in +y direction for whip restraints 8A and 8B. This analysis has shown that the stresses are within cede allowables. It should be noted that the necessary design change will be made to remove this interference and the piping movements will be monitored during the next heatup.

cnctonaizua av.: at ws ...-sswo., j REVISION NO.: 0 SHEET 8 0F 22 7 ORIGINATOR'S NAME /P/M /IM /2/4/# { J DESIGN VERIFIER'S NAME JF?Lf t /4ma_7 l r / / /2 e/7' 2 / DATE: Since all recorded movements at rated vessel condition are approximately within 1/8 inch of analytical (Calc. No. SIR 20) values, the piping thermal movement is acceptable. It should j be noted that the temperature distributions used to generate t the thermal expansion trending plots for the acceptable and expected values were significantly different from the recorded temperature distribution. Since the line temperature was changing unpredictably, a unique trending plot for each lanyard could not be generated. All recorded data has been evaluated for the rated vessel condition and the evaluation result for each lanyard pot is j given below: It should be noted that in addition to the originally provided. six lanyard pots, four more lanyard pots were added and ther=al movements were recorded. All recorded data at rated vessel condition for these additional lanyard pots are within expected limits. l a. Lanyard Number: - B21G02601DLY l Stress Problem Number: 74 Sheet 42 of Appendix B Evaluation Result: The recorded thermal movement is i outside acceptable limits. A stress analysis was { performed by utilizing recorded line te=perature and I design cold gap at whip restraint 8A. From this anlaysis, l the stresses were found to be within the code allowables 4 and the recorded thermal movement at rated vessel condition is within 1/8 inch of the analytical value l (Calc. No. STR-20). Therefore, the' recorded pipe movemer.t I during Nuclear Heacup is acceptable. t b. Lanyard Number: B21G02602DLX i i Stress Problem Number: 74 l Sheet 43 of Appendix B l Evaluation Result: Acceptable. The recorded ther=al l movement at rated vessel condition is within expected limits. c. Lanyard Number: B21G02605DLX l Stress Problem Number: 74 Sheet 44 of Appendix B 1 I

s REVISION NO : 0 j SHEET 9 0F 22 ORIGINATOR'S NAME 4 / # s /a/4/3 ~ DESIGN VERIFIER'S NAME WAl. srr-DATE; /2/ #//t / < s Evaluatien Result: Acceptable. It should be noted that clie recbrded thermal movement is cutside she expected i limits but still within the accept'able limits. A stress

analysis was performed by utilizing recorded line tarperature and design cold gap at whip restraint 8A.

From this anlaysis, the stresses were found to be ' within the code allowables and the recorded thermal movement ar rated vessel condition is within 1/8 inch of the analytical value (Calc. No. STR-20). Therefore, the recorded pipe movement during Nuclear Heatup is acceptable. d. Lanyard Number: B21G02604DLY ~ Stress Problem Number:. 7S Sheet 45 of Appgndir. 6 Evaluation Result: Acceptable. The recorded thermal movement at rarel vessel condition is within the expected I limits., e. Lanyard tsueber: 321G02606DLY Stress Problem Number: 75 Sheet 46 of Appendix B c Evaluation Result: The recorded thermal novements is outside the acceptable limits. It should be noted that the recorded data from 500 to 540*F RPV reference t couperature shows the effect of the whip restraint interference with the pipe. A stress analysis was perfor=ed by utilizing the recorded line temperature and design cold gap at whip rest:4dnt 8L From this analysis the stresses were found to be.within code allowables and the recorded-thermal movement at ratee vessel condition is within 1/16 inch of analytical value' (Calc. No. STR-20). This shevs that the whip restraint interference.directly effect thermal movements at this point. It shculd be noted that the necessary design . change will be made.te remove this interference and the i piping movements will be motitored during the next heacup. l f. Lanyard Number: B21G02603DLX 4 I Stress Problem Number: 75 Sheet 47 of Appendix B i j

SHEET 10 0F 22 ) ORIGINATOR'S NAME /M.8 /4//I//7 l DESIGN VERIFIER'S NAME y # A f r DATE: A>/,, /p g 7 Evaluation Result: The recorded thermal move:ent is outside expected limits but still within the acceptable limits. A stress analysis was performed by utilizing the recorded line temperature and the whip restraint 83 interference at rated vessel condition. From this analysis, the stresses were found to be within code allowables and recorded thermal movement is within 1/8-inch of analytical value (Calc. No. STR-20). It should be noted that the necessary design change will be made to remove this interference and the piping movements will be monitored during the next heatup.

5.1.3 System

333-Recirculation system. BOP piping, KER suction from Recire Loop B. Stress Problem Number: 323 l Pre-Op. Isometric Drawing: M-1661, Rev. 3 Calculation Number: M-275.0-323-1-T Lanyard Number: B33G023RB6DLX Sheet 52 of Appendix,B Evaluation Result: Acceptable. The recorded thermal =ovements are within the expected limits.

5.1.4 System

E12-Residual Heat Removal System Stress Problem Number: 139 Pre-Op. Isometric Drawing: M-1693, Rev. 1 Calculation Number: M-275.0-139-1-T Lanyard Number: E12G02101DLZ Sheet 53 of Appendix B Evaluation Result: The recorded thermal movement is outside the acceptable limits. However, testing was continued en the basis that the test temperature distribution was significantly different from the one used in the analytical model and the i fact that the piping thermal movement during Non-Nuclear Heat-up was acceptable. A stress analysis was performed by utilizing recor'ded line temperature distribution at rated vessel condition. From this analysis the stresses were found to be within the code allowable and the recorded thermal movement at rated vessel condition is approximately within 1/16 inch of the analytical (Calc. No. M-275.0-139-1-T) value. Therefore, the piping thermal movements during Nuclear Heatup are acceptable. It should be noted that, since the line temperature was changing unpredictably, a unique thermal expansion trending plot could not be generated. It should also be noted that no interferen:: or blockage was identified during n ikdowns. ~

E_.;S[0hh0.: b SHEET 11 0F 22 ORIGINATOR'S NAME # 4 / /1/A./83 DESIGN VERIFIER'S NAME 7Fd/d4# DATE: /zde-dy ~ 5.1.5 Systa=: B33/G33 - Recirculation System. BOP Piping, Reactor Water Cleanup. Stress Problem Number: 138 Pre-Op. Isometric Drawing: M-1696A, Rev. 2 and M-16963, Rev. 1. Calculation Number: M-275.0-138-1-T Evaluation Results Summary: Acceptable. The piping ther=al movements were recorded at two locations. The recorded thermal movements are outside expected limits but within the acceptable limits at one location and outside acceptable limits at the other location. It should be noted that the recorded move =ents are similar to. recorded data during Non-Nuclear Heatup. Therefore, it appears that all the insulation interferences identified during NNH were not completely removed. Piping insulation will be modified to provide sufficient clearance prior to the next heatup and the pipe thermal movements will be monitored and evaluated during the next heatup. However, since the trend of recordet data during this heatup is good and similar to the analytical values, the piping thermal expansion during Nuclear Heatup is acceptable. a. Lanyard Number: B33G02401DLY Pre-Op. Isometric Drawing: M-1696A, Rev. 2 Sheet 54 of Appendix B Evaluation Results: The recorded thermal movement is cutside acceptable limits. It should be noted that the recorded movement is similar to recorded data during Non-Nuclear Heatup. Therefore, it appears that all insulation interferences identified during NNH were not completely removed. Piping insulation will be modified and interferences will be removed prior to the next heatup. The pipe thermal movement will be monitored and evaluated during the next heatup. It should also be noted that, RWCU thermal movements are greatly influenced by RECIRC thermal movements. Since RECIRC ther=al movements are less than the predicted values (ref.. Sheet 25 of Appendix B) and the trend of recorded data during this heacup is similar to analytical values, the piping thermal expansion during Nuclear Heatup is acceptable. b. Lanyard Number: G33G01101DLZ Pre-Op. Isometric Drawing: M-1696B, Rev. 2 Sheet 55 of Appendix B

.-s-SHEET 12 0F 22 ORIGINATOR'S NAME A/./) d /2 /A. /# 3 DESIGN VERIFIrR'S NAME > F M L X M DATE: /1//, 7 / Evaluation Result: Acceptable. The recorded thermal movement is outside the expected limits but within the acceptable limits. It should be noted that the ther=al movement is too small to be measured accurately.

5.1.6 System

B21 - Standby Liquid Control Stress Problem Number: 2047 Pre-Op. Isometric Drawing: M-1688A, Rev. O Calculation Number: M-275.0-2047-1-T Lanyard Number: B21G16301DLL Sheet 56 of Appendix 3 Evaluation Result: Acceptable.- The recorded thermal move =ent is within the expected limits.

5.1.7 System

E32 - MSIV Leakage Control Stress Problem Number: 2027 Pre-Op. Isometric Drawing: M-1686, Rev. 1 Calculation Number: 't!-275.0-2027-1-T Lanyard Number: E32G10901DLX Sheet 57 of Appendix B Evaluation Result: Acceptable. It should be noted that recorded ther=al movements are outside expected limits but within acceptable limits. However, the recorded ther=al movement at rated vessel condition is within 1/16 inch of analytical value. Therefore, the piping thermal movement during Nuclear Heatup is acceptable.

5.1.8 System

E12 - Residual Heat Removal Stress Problem Number: 101, 102, and 66 Pre-Op. Isometric Drawing: M-1666, Rev. 3 and M-1670, Rev. 3 Calculation Number: M-275.0-101-1-T, M-275.0-102-1-T, and M-275.0-66-1-T. Evaluation Results Summary: Acceptable. The piping thermal movements were recorded-by five Lanyard pots at four locations in various directions. The recorded ther=al movements are within the expected limits for four Lanyard Pots and outside expected but within the acceptable limits for one lanyard pot. A stress analysis was performed by utilizing recorded line temperature distribution at rated vessel condition for proble: 66 and 102. From this analysis the stresses were found to be within the code allowables. Therefore, the piping thermal expansion during Nuclear Heatup is acceptable.

SHEET 13 0F 22 ORIGINATOR'S NAME 4/ 8. #M /2/4/#y DESIGN VERIFIER'S NAME 3C//Z of-DATE: /thr//3 The evaluation result for each lanyard pot is given below: a. Lanyard Number: E12G01501DLY Pre-Op. Isometric Drawing: M-1666, Rev. 3 Sheet 58 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. b. Lanyard Number: E12G01502DLX Pre-Op. Isometric Drawing: M-1666, Rev. 3 Sheet 59 of Appendix B Evaluation hasult: Acceptable. The recorded ther=al i movement is within the expected limits. c. Lanyard Number: E12G01504DLZ Pre-Op.IsomethicDrawing: M-16 66., 'Rev. 3 Sheet 60 of Appendix 3 Evaluation Result: Acceptable. It should be noted that the reccrded thermal movements are outside the expected limits but within the acceptable limits. A stress analysis was performed by utilizing the recorded line temperature distribution at rated vessel condition. From this analysis the stresses were found to be within the code allowables and the recorded thermal movement at rated vessel condition is within 1/16 inch of analytical value (Calc. No. M-275.0-102-1-T). Therefore, the piping thermal movement during Nuclear Heatup is acceptable. d. Lanyard Number: E12G01505DLY Pre-Op. Isometric Drawing: M-1666,.Rev. 3 Sheet 61 of Appendix B Evaluation Results: Acceptable. The recorded ther=al movement is within the expected limits. e. Lanyard Number: E12G01602DLY Pre-Op. Isometric Drawing: M-1670, Rev. 3 Sheet 62 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. i , - ~ _

w n_....s.......... ...y. REVISION NO.: O SHEET 14 '0F 22 ORIGINATOR'S NAME g. 8 4 / 2 / A /jp - DESIGN VERIFIER'S NAME / MIL M DATE: n/er/M ^

5.1.9 System

E21 - Low Pressure Core Spary Stress Problem Number: 55 Pre-Op. Isometric Drawing: M-1655, Rev. 3 Calculation Number: M-275.0-55-1-T Lanyard Number: E21G00202DLL Sheet 63 of Appendix B ~ Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. ~ 5.1.10 System: E22 - High Pressure Core Spray Stress Proble= Number: 60 Pre-Op. Isometric Drawing: M-1657 Rev. 4 Calculation Number: M-275.0-60-1-T Lanyard Number: E22G00302DLY Sheet 64 of Appendix B Evaluation Result: -Acceptable. The recorded thermal movement is within the expected limits. 5.1.11 System: E51 - Reactor Core Isolation Cooling Stress Problem Number: 69B and 229 Pre-Op. Isometric Drawing: M-1675, Rev. 4 Calculation Number:. M-275.0-69B-1-T and M-275.0-229-1-T Evaluation Result Summary: Acceptable. The piping ther=al movements were recorded by four lanyard pots at three location in various directions. All the recorded data are within the expected limits except at one pot, where the recorded movements are outside the expected limits but within the acceptable limit. During a walkdown of RCIC piping inside containment, various interferences were identified and removed. After removal of i these interferences, the recorded movements at rated vessel condition for lanyards E51G004SA9DLX and E51G004SA9DLZ were questionable. Therefore, snubber movements at rated vessel condition were recorded. A stress analysis was performed by utilizing recorded line temperature distribution at rated vessel condition. From this analysis the stresses were found to be within the code allowables and all the recorded snubber movements (ref. Startup Test Report No. 1C88ST05, Data Sheet

15) are approximately within 1/8 inch of analytical values (Calc. No. M-275.0-229-1-T).

Therefore, the piping thermal movements during Nuclear Heatup are acceptable. l l i

...u..... s. RFilSION NO.: O SEEET 15 0F 22 ORIGINATOR'S NAME # /9 4 /2.//4/g-DESIGN VERIFIER'S NAME A96A4f-DATE: 12/ir/23 The evaluation result for each Lanyard is given below: a. Lanyard Number: E51G00401DLY Stress Problem Number: 69B Sheet 65 of Appendix B f Evaluation Result: Acceptable. The recorded ther=al movement is within the expected, limits, b. Lanyard Number: E51G004SA9DLX n Stress Problem Number: 229 Sheet 66 of Appendix B Evaluation Result: Acceptable. It should be noted that the recorded thermal movement is outside the expected limits but still within the acceptable limits.

However, since the expected thermal movements are small, the piping thermal movements are acceptable.

It should also be noted that recorded m'ovement at rated vessel condition is questionable based on the snubber movement readings. c. Lanyard Number: E51G004SA9DLZ Stress Problem Number: 229 Sheet 67 of Appendix B Evaluation Result: Even though the recorded thermal movement at the rated condition is within the expected limits, the data is questionable based on the snubber movement readings. Stress analysis (Calc. No. M-275.0-229-1-T) was performed by utilizing recorded line temperature at rated vessel condition. Stresses are within code allowables and recorded snubber movements are approximately within 1/8 inch of analytical values. Therefore, piping thermal movement during Nuclear Heat is acceptable. d. Lanyard Number: E51G004SA8DLY Stress Problem Number: 229 Sheet 68 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. 5.1.12 System: N11 - Main / Reheat Steam Stress Problem Number: 12 Pre-Op. Iso =etric Drawing: M-1654, M-1658, and M-1659 Calculation Number: M-275.0-12-1-T, STR-17, and STR-19 .__ _ _ _. _ _ _ _.- _._._,_ ~ _ _. _. _

_CULATION NO.: MC-Q1-lil-630v41 s RE71SION NO.: O SHEET 16 OF 22 ORIGINATOR'S NAME /// 4 M /2,8 /f3 DESIGN VERIFIER'S NAME 18' 414,f DATE: /Llf/r3 / Evaluation Results Summary: Acceptable. The piping thermal movements were recorded by fourteen lanyard pots at thirteen locations in various directions. The recorded thermal movements are within the expected limits for seven lanyard pots and outside the expected limits but within the acceptable limits for four lanyard pots. Even though the remaining three recorded data are outside acceptable limits, stresses were within the code allowables. During heatup, at on.termediate temperatures various interferences were identified and removed. Also, during testing, x-snubbe-N1N11G001R01 was found to be locked af ter i 1/4 inch travel.

2. stress analysis (Calc. No. STR-17) was performed assuming a locked snubber at the rated vessel condition.

From this analysis the stresses were found to be within the' code allowables. This snubber will be replaced and the piping thermal movements will be monitored during the next heatup. In addition, a stress analysis (Calc. No. STR-19) was performed by utilizing the recorded thermal movements at all the locations for the rated vessel condition. From this analysis the stresses were found to be within the code allowables, therefore the piping thermal expansion during Nuclear Heatup is acceptable. The evaluation result for each lanyard pot is given below: Lanyard Nu=ber: N11G00102DLY a Pre-Op. Isometric Drawing: M-1654, Rev. 2 Sheet 69 of Appendix B Evaluation Result: Acceptable. It should be noted th.at the recorded thermal movement corresponding to rated vessel condition is just outside the expected 11=lt but still within the acceptable limits. A stress analysis whs performed by utilizing the recorded thermal movement at the rated condition. From this analysis the stresses were found to be within the code allowables. 1 b. Lanyard Number: N11G00107DLY Pre-Op. Isometric Drawing: M-1654, Rev. 2 Sheet 76 of Appendix B Evaluation Result: Acceptable. It should be noted that the recorded thermal movement is outside the expected limits but still within acceptable limits. A stress analysis was performed by utilizing the recorded thermal movement corresponding to rated vessel condition. From this analysis the stresses were found to be within the code allowables.

3 -- CULA!luN NO.: MC-QA-6AA-eacuti LE*lISION NO.: O SEEET 17 0F 22 ORIGINATOR'S NAME A#' M. MM /2/A // 3 DESIGN VERIFIER'S NAME #d/AM DATE: /dffy 4 c. Lanyard Number: N11G00108DLY Pre-Op. Isometric Drawing: M-1654, Rev. 2 Sheet 71 of Appendix B Evaluation Result: Acceptable. It should be noted that the recorded thermal movements is outside the expected limits but still within the acceptable limits. A stress analysis was performed by utilizing the recorded thermal movement corresponding to rated vessel condition. From this analysis the stresses were found to be within the code allowables. d. Lanyard Number: N11G00101DLX Pre-Op. Isometric Drawing: M-1654, Rev. 2 Sheet 72 of Appendix B

Evaluation Res 11:

Snubber NIN11G001R01 was found to be locked after a 1/4 inch of travel. A stress analysis (Calc No. STR-17) was performed for the rated condition assuming a locked snubber. From this anlaysis the stresses were found to be within the code allowables. It should be noted that, after second cool down, the recorded pipe movement and the snubber reading showed that the snubber was unlocked and moved as predicated.

However, this snubber will be replaced (DCP 83-4088) and the pipe movement will be monitored during the next heatup.

e. Lanyard Number: N11G00109DLZ Pre-Op. Isometric Drawing: M-1654, Rev. 2 Sheet 73 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. f. Lanyard Number: N11G00103DLY Pre-Op. Isometric Drawing: M-1654 Rev. 2 Sheet 74 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits.

s EEVISION NO.: O SHEET 18 0F 22 ORIGINATOR'S NAME M.#./M /z/4 /#3 DESIGN VERIFIER'S NA".E <#442 /s- /2//f 3 ' ~ /d DATE: g. Lanyard Number: N11G00104DLX Pre-Op. Isometric Drawing: M-1654, Rev. 2 Sheet 75 of Appendix B Evaluation Result: Acceptable'. It should be noted that the recorded thermal movements are outside the expected limits but still within the acceptable limits. A stress analysis was performed by utilizing the recored thermal movement corresponding to the rated vessel condition. From this analysis the stresses were found to be within the code allowables. h. Lanyard Number: N11G00105DLX ~ Pre-Op. Isometric Drawing: M-1654, Rev. 2 Sheet 76 of Appendix B Evaluation Result: Acceptable The recorded thermal movement is within the expected limits. 1. Lanyard Number: N11G00106DLY Pre-Op. Isometric Drawing: M-1654, Rev. 2 Sheet 77 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. j. Lanyard Number: N11G00301DLZ Pre-Op Isometric Drawing: M-1658, Rev. 2 Sheet 78 of Appendix B Evaluation Result: The recorded thermal ecvemen't is outside the acceptable li=its. A stress analysis was performed by utilizing the recorded thermal movement corresponding to the rated vessel condition. From this analysis the stresses were found to be within the code allowables. It should be noted that snubber (NIN11G003R06) reading shows 1.2 inch pipe the'rcal movement at this location (ref. IC885T05, Rev. 2, Data Sheet 13). This reading indicates that pipe thermal movement is within the expected limits, and the recorded data may be questionable. k. Lanyard Number: N11G00302DLY Pre-Op. Isometric Drawing: M-1658. Rev. 2 Sheet 79 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits.

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REVISION NO.: O SHEET 19 0F 22 ORIGINATOR'S NAME AV./7. M4/[J DESIGN VERIFIER'S NAv.E' yFJ O E / 2_ / re,// 7 / DATE: 1 1. Lanyard Number: N11G00401DLZ Pre-Op. Isometric Drawing: M-1659, Rev. 2 Sheet 80 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. It should be - noted that at 400*F, interferences were identified. After removal of these interferences, the pipe moved as predicted, m. Lanyard Number: N11G00402DLI Pre-Op. Isometric Drawing: M-1659, Rev. 2 Sheet 81 of Appendix B Evaluation Result: Acceptable. The recorded ther=al movement is within the expected limits. It should be noted that during heatup between 350 to 450*F, ~ interferences wyre identified. After removal of these interferences, the pipe moved as predicted. n. Lanyard Number: N11G00403DLZ ~ Pre-Op. Isometric Drawing: M-1659, Rev. 2 Sheet 82 of Appendix B Evaluation Result: The recorded th'ermal movement is outside the acceptable limits. A stress analysis was performed by utilizing the recorded snubber (N1N11G004R05) movement and line temperature distribution at the rated vessel condition. From this analysis the stresses were found to be within the code allowables. It should be noted that the temperature distribution used to generate the thermal expansion trending plots is different from the actual test condition (i.e. Valve F014B was Open and Valve F014A was Closed) and the recorded snubber reading shows 0.3 inch thermal movement at this location (ref. IC885T05, Rev. 2, Data Sheet 13). This snubber reading indicates that the pipe therm'al movement is within the acceptable limits. 5.2 NSSS PIPING Recorded data for NSSS Piping was transmitted to GE through reference FDDR (Ref. 2.12) for evaluation. GE has completed their evaluation and recorded data is acceptable. It should be noted that all deviations from Level 1 and Level 2 limits at intermediate and rated vessel condition are acceptable (Ref. 2.12, 2.14)

3 ...s.

.eVISION NO.:

O SHEET 20 0F 22 ORIGINATOR'S NAME /fd'. /J dd *. /:L//4/gj DESIGN VERIFIER'S NAME #Mi'ar- ~ jn//f/81 / DATE: 2.0 DISCUSSION The evaluation process started at 200*F reactor recirculation suction temperature by plotting recorded data on thermal expansion trending plots. The process, as stated in Section 4.1, was continued up to the rated vessel condition. During testing at intermediate temperatures, several walkdowns were performed to identify any blockage or interferences. During these walkdowns, many insulation interferences were identified and all potential interferences were either removed or stress analyzed for acceptance. The following are the major observations made/ problems identified during nuclear heatup. 1) At approximately 250*F recirculation suction temperature, it was suspected that three (3) of the four (4) Lanyard Pots at the moment guides of the main steam line (NSSS) had less thermal expansion than expected. After confirming no interferences, General Electric consented to continue heatup. Upon reaching 365'F, it was concluded that a potential exists for overstressing the pipes if recorded data was correct. It was decided to remove insulation, make scribe marks on the main steam lines near the moment guides and cooldown to approximately 250*F to observe pipe movement. After removing insulation, it was observel that the installation of all four pots was faulty and recorded data was incorrect. Upon cooling down, the scribe marks verified a correct trend, therefore the scribe marks were read manually from 265'F to rated te=perature (approximately every 50*F) and at cooldown (approximately 80*F). The evaluation results of the data taken from the scribe marks are in Reference 2.14 and are acceptable. 2) During the course of nuclear heatup, several Lanyard Pots deviated from their predicted (analytical) move =ent due to interferences from insulation. These type of interferences were more prevalent on the main steam lines (N11) in the Turbine Building. In most cases, upon removing these interferences, the measured thermal expansion trended toward that predicted. l 3) At 300*F recirculation suction te=perature, the Lanyard Pot N11G00101DLX on main steam C showed no moment. A val,kdown verified that the snubbers on pipe support N1N11G001R01 were locked up. A strass analysis (CALC NO. STR-17) was performed for the existing and the rated plant condition assuming a locked snubber. From this analysis the stresses were found to be within the code allowables. DCP 83/4088 was issued to l replace the snubbers. i

REVISION No.: O SHEET 21 0F 22 ORIGINATOR'S NAME M 27. / M /s Az/#y DESIGN VERIFIER'S NAME A?./dBf ~ DATE: n/fg/rt ~' 7 4) In order to maintain the required reactor vessel water level during nuclear heatup, feedwater flow was less than normal due to the water level being mantained by the startup level controller. Due to this condition, the temperature of makeup water to the vessel by feedwater lines (Loop A and B) was unpredictable for the R.W.C.U. System was added at a higher temperature. This caused the temperature of the feedwater lines to vary from 100*F to 250*F. It should be noted that R.W.C.U. temperature was from 70*F to 450*F while the temperature of the feedwater' system was from 80*F to 130*F. Because of this rapidly varying unpredictable conditions during nuclear heatup, a trend could not be established for some pots ~ (B21G02601DLT, B21G02605DLX and B21G02603DLI) during intermediate temperatures. 5) For ease of evaluation of the feedwater lines during nuclear heatup, in the vicinity'of RPV nozzles four (4) te=porary Lanyard Pots were installed. These Lanyards are B21TIO7DLY, B21TIO8DLY, B21TIO9DLY and B21TIl0DLY (See Sheets 48, 49, 50 and 51 respectively-in Appendix B). The recorded data at the rated vessel conditfon for these additional Lanyard Pots is within the expected limits and is acceptable. 6) At the rated vessel condition, it was observed that the feedwater pipe was touching whip restraint 8B in the +Y (upward) direction. A stress analysis (CALC. NO. STR-20) was performed and the stresses were to be found within the code allowables. Since feedwater whip restraints 8A, 8B, 10A and 10B in the +Y direction were eliminated from the analysis (Reference 2.13), DCP 83/4100 was issued to remove these interferences. It should be noted that during the walkdown only whip restraint 8B was interfering with the free pipe movement. 7) After the vessel reached the rated temperature and pressure and all the testing was completed, the vessel was cooled to a recirculation suction temperature of 100*F. A histogram was taken at this temperature to complete the thermal cycle as requested in Section 5.3.1.2 of Reference 2.1. During the evaluation, one (1) Lanyard Pot exceeded its original ambient reading by 125 mils (1/8"). This Lanyard Pot is E51G0045A9DLZ. E51G004SA90DLZ exceeded its ambient reading by 306 mils. This is partially due to an interference (insulation) that was removed at rated conditions. k .I i i

CALCUIATION NO.: MC-Ol-lll-boC047 REVISION NO. : 1 i SN 21A CCNT. CN SHEET 2? ORIGDL"GR A/M DATE 3/n./ty DESIGN VERIFIER #E/ D7E /,,, /> v 7.0 'ASSLW rIONS Ncne 8.0 COMPT 7rER CAICUIL".ONS Even though Nuclear Plant Engineering did not perfom any carnter calculations for piping ther:ral expansion data evaluation, Bechtel GFD stress group performed various emputer calculations using Bechtel program ME101. All cmputer calculations are referenced in Section 5.1 as applicable. e e e 8

i .--ovcA41vd Av. : su w. 6..-:avs., IVISION NO.: 4r l SEEET 22 OF 22 AM 5//k8# ORIGINATOR'S NAME #.// //a MA/6-DESIGN VERIFI 'S NAME R u % r-EWu.,'h /A//q pd DATE: +re-SUM %RY OF RESULTS/CONCI.USIONS Piping thermal expansion was recorded for fourteen (14) syste=s during nuclear heatup at sixty (60) locations. Eighty-two (82) Lanyard Pots were utilized for data recording. Thirty-five (35) Lanyard Pots were mo'unted on NSSS piping systems and forty-seven (47) Lanyard Pots were mounted on BOP piping systems. During nuclear heatup, walkdowns were perfor=ed at inter =ediate and rated temperatures. Various interfarences were identified and re=oved if necessary. Snubber and spring readings for various systems were taken at rated condition for ease in evaluation of recorded data. L The evaluation has been perfor=ed by taking into consideration errors involved in data collection (transducer resolution, temperature resolution), ~ temperature distribution during testing condition versus that used in analysis and other relevant informations such as locked snubber, identified interferences, etc. The evaluation of thermal movement,s for NSSS piping was perfor ed by GE (San Jose) and is acceptable. As stated in the final disposition of References 2.12 and 2.14, the deviation in inter =ediate Level 1 and Level 2 are acceptable. The evaluation of thermal movements for 30P piping was perfor=ed by Nuclear Plant Engineering with assistance from Bechtel (GFD). The piping ther=al movements recorded by twenty-seven (27) Lanyards are within expected li=its; twelve (12) Lanyards are outside expected limits but within acceptable limits. The remaining eight (8) Lanyards are outside acceptable li=its. A stress analysis was performed if necessary by utilizing the recorded line temperature, snubber and spring readings and any interferences identified and not removed during nuclear heacup at the rated vessel condition. Frc= these analysis the piping stresses are within the code allowables for all =enitored systems. Based on the above, it is concluded that recorded piping thermal =ovements during nuclear heacup at all locations are acceptable. l l l l

BOP Piping Thermal Expansion IC88-ST05 4 APPENDIX III NPE CALCULATION MC-Q1111-85039 PIPING THERMAL EXPANSION EVALUATION DURING POWER ASCENSION TESTING i i t

1 NUCLEAR PLANT ENGINEERING Plant gner nno ENGINEERING CALCUL ATION ~ i nurrt.26T I To 76'I S(o lo09M ! ! rlsGE t CF IM TITLE : Pms Tmmt Evenstsrou Evaumon Donuc PowtR kscGMsToN IESU"MG CALCULATION NUMBER : MC-Q \\ \\ li-8 503c) REVISION : O THIS CALCULATION SUPERSEDES CALCULATION NUMBER NOME AFFECTED SYSTEM (S) : YARTous GRAND GULF NUCLEAR STATION, UNIT : 1 (sg \\ SAFETY RELATED I l' \\ Q5 ,f i i D NONSAFETY RELATED FOR SAFE 7 REL ATED ^ PRELIMINARY CALCULATION FitlAL CALCULATION PREPARED BY: k DATE: l'29-8L (RESPONSIBLE ENGINEER) VERIFIED BY : 7 DATE: !2k'b / l-30-S$ REVIEWED BY : DATE : (SUPERVISOR) REVIEWED BY : "N' ' DATE: - D' " ~ (QUALITYj ENG 4EER) APPROVED BY : DATE: - (PRINCIPAL, ENGINEER) e d feT3 M YeY V VY eVW k

CALCULATION NO.: MC-Q1111-85039 7,77. - 7 REVISION NO.: O SHEET 2 CONT. ON SHEET 3 TO PWI 86f009 ORIGINATOR ff@ DATE l-29-ec png 1 CF l'il DESIGN VERIFIER gp/# DATE f.2 9 - fl, REVISION STATUS SHEET DESIGN CALCULATION / ANALYSIS REVISION

SUMMARY

REVISION DATE DESCRIPTION O February 3, 1986 Issued for Use SHEET REVISION STATUS SHEET NO. REVISION SHEET NO. REVISION 1 0 14 0 2 0 15 0 3 0 16 0 4 0 17 0 5 0 18 0 6 0 19 0 7 0 20 0 8 0 21 0 9 0 22 0 10 0 11 0 12 0 13 0 APPENDIX REVISION STATUS APPENDIX REVISION A 0 B 0 C 'O l l

CALCULATION NO. MC-Qllll-85039 REVISION NO. 0 ",.,. 7 SHEET 3 CONT. ON SHEET 4 F: PMT glo g a-l t ORIGINATOR ff% DATE I-2 7-f f. q g. 3 ,7 g g j DESIGN VERIFIER -ift// DATE /-z J -fru TABLE OF CONTENTS SHEET COVER SHEET 1 REVISION STATUS SHEET 2 TABLE OF CONTENTS 3 SECTION 1.0 PURPOSE 4 2.0 REFERENCE / SOURCES 4 3.0 ASSUMPTIONS 5 4.0 PIPING EXPANSION ACCEPTANCE CRITERIA 5 5.0 METHODOLOGY 6 6.0 EVALUATION RESULTS 7 7.0 COMPUTER CALCULATIONS 21 8.0

SUMMARY

OF RESULTS/ CONCLUSIONS 21 APPENDICES A DATA SHEETS B TRENDING PLOTS C POWER ASCENSION EVALUATION SUM!MRY n

1,_,.. CALCULATION NO.: MC-01111-85039 I ' ' ' REVISION NO.t 0 'P W 3 4 l o 09 all l SHEET 4 CONT. ON SHEET 5 8 ^ N , '] g g ORIGINATOR if/TYi DATE i-M g(, DESIGN VERIFIER 'Zy/p DATE /.2 7 -f7, 1.0 PURPOSE The purpose of this Calculation is to evaluate the piping thermal expansion data recorded during power ascension testing. Piping movements were recorded at locations identified in specification 9645-M-275.0 (Ref 2.1) for Non-NSSS Piping. Evaluation of the data for Non-NSSS piping was performed by Nuclear Plant Engineering with Assistance from Bechtel, GFD.

2.0 REFERENCES

/ SOURCES 2.1 Bechtel Specification 9645-M-275.0, Rev. 17. "Preoperational Piping Vibration, Thermal Monitoring and Dynamic effects testing of piping systems" 2.2 PSAR Section 14.2.12.4.5 and Question and Responses 110.33 2.3 Startup Procedure IC88-ST05, Rev. 2, " BOP System Piping Thermal Expansion Monitoring Program" 2.4 NPEI 85/2001, 12-13-85, Ambient Histograms for Power Ascension Featup Testing 2.5 NPEI 85/2002, 12-13-85, Histograms Taken During Power Ascension Testing for Piping Thermal Expansion Program 2.6 PMI 85/0510, 1-9-85, B.O.P. Thermal Expansion Data at 50% Power Level 2.7 PMI 85/0573, 1-14-85, B.O.P. Thermal Expansion Data for Lanvard Pot N21G00101DLX 2.8 PMI 85/0608, 1-17-85, Thermal Monitoring of Feedwater Piping Lanyard Pots N21G00101DLX, N21TIO3MLX, and N21TIO2MLX 2.9 PMI 85/1455, 2-7-85 Thermal Expansion Monitcring During SRV Actuation 2.10 PMI 85/4137, 4-24-85, B.O.P. Thermal Expansion Data at 75% Power Level 2.11 PMI 85/11,132, 12-19-85, B.O.P. Thermal Expansion for Shutdown Cooling and Steam Condensing Modes 2.12 PMI 85/6128, 6-17-85, B.O.P. Thermal Expansion Data for Steam Condensing Mode 2.13 PMI 85/5382, 6-3-85, B.O.P. Thermal Expansion Data for Shutdown Cooling Mode 2.14 NPEI 85/2000, 12-13-85, Speed Memos during Piping Thermal Expansion Program 2.15 Project No. NPE-85-013, Request No. 4. Bechtel Response No. 1. Stress Test Run, STR-108, Referenced in Section 6.0, MPT 85/2033 2.16 Project No. NPE-85-013, Request No. 4 Bechtel Response No. 2, Stress Test Run, STR-117, referenced in Section 6.0, MPT 85/2261

CALCULATION NO.: MC-Q1111-85039 An;,;fNE"i REVISION NO.t 0 SHEET 5 CONT. ON SHEET 6 TO PMT Q 009 M ORIGINATOR gf#tyl DATE /-2196 FA3E 5 0F lti DESIGN VERIFIER gjff DATE f.2 9-//, 2.17 Project No. WPE-85-013, Request No. 4 Bechtel Response No. 2, Stress Test Run, STR-118, referenced in Section 6.0, MPT 85/2261 2.18 Project No. NPE-85-013 Request No. 4, Bechtel Response No. 4 Stress Test Run, STR-123, referenced in Section 6.0, MPT 85/2572 2.19 Project No. NPE-85-013. Request No. 4, Bechtel Response No. 5 Stress Test Run, STR-118 Rev. B, referenced *in Section 6.0, HPT 85/2909 2.20 Project No. NPE-85-007, Request No. 1 Bechtel Response No. 1 MPT 85/0190 2.21 Project No. NPE-85-013. Request No. 5, Bechtel Response No. 1, Stress Test Runs, STR-124 and STR-125, referenced in Section 6.0, MPT 85/2945 2.22 Project No. NPE-85-013, Request No. 5,' Bechtel Response No. 2, Stress Test Runs, STR-124 Rev. B and STR-125 Rev. B referenced in Section 6.0, HPT 85/3064 2.0 PrPIs Tntnu. Eons-Dm,46 N*.an Iken Ttsitus, cauma MC-Quy-gge30,2u, o 3.0 ASSUMPTIONS 3.1 None 4.0 PIPING EXPANSION ACCEPTANCE CRITERIA Thermal expansion acceptance criteria for Non-NSSS piping is described below in Section 4.1. 4.1 Non-NSSS Piping Piping Expansion Acceptance Criteria for expected and acceptable limits was generated by Bechtel, GPD in Specification 9645-M-275.0 (Ref. 2.1). The expected thermal boundary limits are based on 125 percent of the analytical value at rated condition. The acceptable thermal boundary limits are based on 1 0.25 inch or i 25 percent of the analytical l value, whichever is greater, at 550*F Reactor Pressure Vessel reference i temperature, unless otherwise specified. It should be noted that the acceptable limits are not code allowable limits. Also, recorded piping thermal expansions are acceptable when they are within expected limits and/or are within 1/8 inch of analytical values. This is to account for tolerances for temperature distribution, transducer resolution and temperature resolution. When recorded thermal rovements exceed l expected values, stress analysis has been performed by utilizing l existing temperature distribution, recorded piping movements at monitoring points and snubber / spring readings as applicable. Recorded as sements will be acceptable if stresses in piping system are within code allowables. i ~..

[........__ CALCULATION NO.: MC-01111-85039 REVISION NO.: 0 , 7 ".; PMI f(p l co l E"} SHEET 6 CONT. ON SHEET 7 C ORIGINATOR j f9y1 DATE /-M d4 p.y 4 'f' gg g DESIGN VERIFIER -29f/p DATE /-2r pro f-5.0 METHODOLOGY The process of piping thermal expansion evaluation and the methodology for evaluation of data at intermediate temperatures is described in Section 5.1 and 5.2 respectively. 5.1 Evaluation Process Thermal Expansion Data was recorded at 25%, 50%, 75% power levels and at rated plant power for Feedwater Main Steam, Condensate, and Feedwater (B31.1) piping. Thermal Expansion Data was also taken for Safety Relief Valve Piping, Main Steam Isolation Valve Leakage Control Piping, and Shutdown Cooling and Steam Condensing at pressure setpoints, normal system operation, and rated flow, respectively. Thermal displacements were determined for each temperature interval at all monitoring points (Lanyard Pots) using data sheets for data reduction (Appendix A). The displacements were then plotted on trending plots (Appendix B). At each plateau, engineering evaluations were made for all recorded data and were documented on the Power Ascension Evaluation Summary (Appendix C). The results of the engineering evaluations were transmitted to the startup supervisor via speed memos (Ref. 2.14) or PMI's (Ref. 2.6 through 2.13). If at anytime during Power Ascension the plant shutdown and the pipes cooled off, new ambient histograms (Ref. 2.4) were recorded. 5.2 Evaluation.of Data at Intermediate Temperatures 5.2.1 Non-NSSS Piping If the recorded thermal movement was within the expected boundary limit, the testing continued without further evaluation. If the movement was within the acceptable limit but exceeded the expected limit, the testing continued but the data was evaluated. If the data was outside the acceptable boundary limits, the plant was put on hold in order to evaluate any potential problems. In the evaluation process, the following considerations were made: a. The assumptions (Line temperature distribution and anchor movements) used in generating the acceptance criteria (Ref. 2.1) were compared against the recorded plant condition, b. Walkdowns were performed to identify any interferences. c. The recorded data was compared with snubber and/or spring readings taken in its vicinity as applicable. d. Lanyard pots were tested for operability, e. Temporary lanyard pots were used when necessary.

CALCULATION NO.: MC-Q1111-85039 I REVISION NO.: O fg 7. - n:g SHEET 7 CONT. ON SHEET g 70 ?MI $hJO09 Cl ! ORIGINATOR /FM DATE /-M,9(. .,q -)

.,d 31l l

DESIGN VERIFIER //44' DATE /-29 -F4 If the assumptions used in generating the acceptance criteria were different from the recorded plant conditions, the recorded condition was evaluated for its effect on the trending plot. If it was judged that the recorded data was compatible with existing plant condition and the trend was as expected, the testing was continued. When the recorded data was not compatible with existing plant condition, walkdowns were performed to identify any possible interferences. 6.0 EVALUATION RESULTS Evaluation results for Non-NSSS piping is described below in Section 6.1. 6.1 Non-NSSS Piping

6.1.1 System

B21-Main Steam Relief Valve Discharge to Suppression Pool. Stress Problem Number: 215 and 218 Pre-Op. Isometric Drawing: M-1680 Rev. 2 and M-1681 Rev. 2 Lanyard Pot Number: B21G02301DLA, B21G02302DLL, B21G02303DLL, B21G02401DLA, B21G02402DLL, and B21G02403DLL Sheet 24 to 29 of Appendix B Evaluation Result: Acceptable. Piping thermal movements were recorded by six lanyard pots at two locations in three orthogonal directions. This data was recorded during Safety Relief Valve Actuation which is a fast transient event. As a result, the pipe temperature recorded by the thermocouples do not represent the true pipe wall temperature. Therefore, the average pipe wall temperature is expected to be somewhere between the maximum fluid temperature inside the pipe and the pipe surface temperature recorded by the thermocouples. Because the recorded thermal movements are within the limits for a temperature between the recorded surface temperature and the fluid temperature, the recorded thermal movements are acceptable. Therefore, due to the nature of this transient the thermal expansion is acceptable.

6.1.2 System

B21-Feedwater Piping Loops A and B Inside Containment Building Stress Problem Number: 74 and 75 Pre-Op. Isometric Drawing: M-1653, Rev. 3 Calculation Number: STR-108 and STR-123

i, CALCULATION NO.: MC-0.1111-85039 REVISION NO.: 0 SHEET 8 CONT. ON SHEET 9 TG P M'I-8(o l Oo9'l ORIGINATOR ff% DATE /-2f- # L .,.g g g gg DESIGN VERIFIER M DATE.gr.g f Evaluation Results Summary: Acceptable. Piping thermal movements were recorded at six locations. The recorded thermal movements at the rated plant power are within the acceptable limits at all locations except at three locations (B21G02601DLY, 321G02604DLY, and B21G02605DLX) which are outside their acceptable limits. Stress analyses (Calculation No. STR-108 and STR-123) were performed by utilizing the recorded line temperature and the recorded nozzle movements. (Recorded line movements were incorporated when necessary.) These analysis have shown that the stresses are within the code allowables and that all recorded thermal'uovements are acceptable. It should be noted that in addition to the originally provided six lanyard pots, four more lanyard pots were added and their thermal movements were recorded. All recorded data of rated plant power for these additional lanyard pots are within expected limits. The recorded movement by lanyard pots B21TIO7DLY, B21TIO8DLY, and B21TIO9DLY vere utilized to determine the vessel expansion. All recorded data has been evaluated for the rated plant power and the evaluation result for each lanyard pot is given below. s. Lanyard Number: B21G02601DLY Stress Problem Number: 74 Sheet 2 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the acceptable limits. A stress analysis was performed by utilizing the recorded line temperature and the recorded vessel thermal expansion. From this analysis, the stresses were found to be within the code allowables and the recorded thermal movement at the rated plant power is acceptable (Calc. No. STR-108). b. Lanyard Number: B21G02602DLX Stress Problem Number: 74 Sheet 3 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the expected limits but still within the acceptable limits. A stress analysis was performed by utilizing the recorded line temperature and the recorded vessel thermal expansion. From this analysis, the stresses were found to be within the code allowables and the recorded thermal movement at rated plant power is acceptable (Cale. No. STR-108).

CALCULATION NO.: MC-Q1111-85039 l REVISION NO.: 0 "7 l SHEET 9 CONT ON SHEET in 9 ? WI R(p I009 M ORIGINATOR IF??? DATE /.2 S.9 f,

7. < ; q g[

l 2. g DESIGN VERIFIER #44# DATE /-2F.-A', c. Lanyard Number: 321G02605DLX Stress Problem Number: 74 Sheet 4 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the acceptable limits. A Stress analysis was performed by utilizing the recorded line temperature, the recorded line movement, and the recorded vessel thermal expansion. From this analysis, the stresses were found to be within the code allowables (Calc. No. STR-108). Therefore, piping thermal expansion is acceptable, d. Lanyard Number: 321G02604DLY ~ Stress Problem Number: 75 Sheet 5 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the acceptable limits. A stress analysis was performed by utilizing the recorded line temperature, the recorded line movement, and the recorded vessel thermal expansion. From this analysis, the stresses were found to be within the code allowables (Calc. No. STR-123). Therefore, piping thermal expansion is acceptable, e. Lanyard Number: B21G02606DLY Stress Problem Number: 75 Sheet 6 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the expected limits but still within the acceptable limits. A stress analysis was performed by utilizing the recorded line temperature, the recorded line nevement, and the recorded vessel thermal expansion. From I this analysis, the stresses were found to be within the code l allowables (Calc. No. STR-123). Therefore, piping thermal expansion is acceptable. f. Lanyard Number: B21G02603DLX Stress Problem Number: 75 Sheet 7 of Appendix B Evaluation Result: Acceptable. The recorded thermal l movement at rated plant power is within the expected limits.

CALCULATION NO.t MC-Q1111-85039

T: : P mI 8_(p ' o06 1 !

SHEET 10 CO.. ON SHEET 11 REVISION NO.: 0 l ~ j p~ go ,-]p'lti j ORIGINATOR / DATE /-2f-ff. DESIGN VERIFIER @// DATE /-3P-ft

6.1.3 System

E12-Residual Heat Removal System Stress Problem Number: 139 Pre-Op. Isometric Drawing: H-1693, Rev. 1 Calculation Number: STR-117 Lanyard Number: E12G02101DLZ Sheet 8 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the acceptable limits. A stress analysis (Calculation No. STR-117) was performed by utilizing recorded line temperature distribution at rated plant power. From this analysis, the stresses were found to be within the code allowables and the recorded thermal movement at rated plant power is acceptable.

6.1.4 System

N21-Feedwater Ourside Containment Building Stress Problem Number: 139 Pre-Op. Isometric Drawing: M-1694, Rev. 2 Calculation Number: STR-117 Lanyard Number: N21G00101DLX Sheet 9 of Appendix B Evaluation Result: Acceptable. In addition to the original lanyard pot, three more lanyard pots were added and thermal movements were recorded. All recorded data at rated plant power for these additional lanyard pots are acceptable. The recorded thermal movement for lanyard pot N21G00101DLX is considered questionable and the recorded thermal movements by lanyard pots N21TIO2MLX and N21TIO3MLX, which are located on either side of this pot were used to evaluate the pipe displacement in the X-direction for this pipe segment. A stress analysis (Calculation No. STR-117) was performed by utilizing recorded line temperature distribution at rated plant power. From this analysis, the stresses were found to be within the code allowables. Therefore, piping thermal expansion is acceptable. I

6.1.5 System

E32-MSIV Leakage Control System Stress Problem Number: 2027 Pre-Op. Isometric Drawing: M-1686, Rev. 1 Calculation Number: STR-108 Lanyard Number: E32G10901DLX Sheet 10 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the acceptable limits. l _ _., -. ~. _ _ ~.. _.. _.. _. _.. _ _. _ _. - _ _ _ _ _ _. _ _ _ _ _ _ _. _ _ _ _ _ _ _, - - _. ~ _,. _ _ _ -

CALCULATION NO.: HC-01111-85039 ! ;;c;; :;;.lE;.T REVISIOW NO.: 0 ~ SHEET 11 CONT. ON SHEET 12 .Tc P o'n %. cc3 d ORIGINATOR gm DATE I.2f-9(. 1l OF l'Ll l DESIGN VERIFIER g/// DATE A27-/W A stress analysis (Calculation No. STR-108) was performed by utilizing recorded line temperature distribution at normal system operation. From this analysis, the stresses were found to be within the code allowables and the recorded thermal movement at normal system operation is acceptable.

6.1.6 System

N11-Main / Reheat Steam Stress Problem Number: 12 Pre-Op. Isometric Drawing: M-1654 Rev. 2, M-1658 Rev. 3, M-1659 Rev. 3 Calculation Number: STR-118 and STR-118 Rev. B Evaluation Results Summary: Acceptable. The piping thermal movements were recorded at eleven locations. The recorded thermal movements at rated plant power are within the expected limits for five lanyard pots and outside the a:ceptable limits for six lanyard pots. Stress analyses (Calculation No. STR-118 and STR-118 Rev. B) were performed by utilizing the recorded line temperature distribution, the recorded RPV temperature, and the recorded main steam turbine casing temperature. (Recorded line movements were incorporated when necessary). From these analyses the stresses were found to be within the code allowables and that all recorded thermal movements are acceptable. 4 I All recorded data has been evaluated for rated plant power and the evaluation result for each lanyard pot is given below. a. Lanyard Number: N11G00107DLY Pre-Op. Isometric Drawing: M-1654, Rev. 2 Sheet 11 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is just outside the acceptable limit. A stress analysis (Cale. No. STR-118) was performed by utilizing the recorded line temperature distribution, the recorded RPV temperature, and the recorded turbine casing temperature. From this analysis, the stresses were found to be within the code allowables and the recorded thermal movement is acceptable. b. Lanyard Number: N11G00108DLY t Pre-Op. Isometric Drawing: M-1654, Rev. 2 Sheet 12 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. l

CALCULATION NO. MC-Q1111-85039 ',7.....,' REVISION NO.; O i SHEET 12 CONT. ON SHEET 13 ~ 19 P MI $hlOCg M ORIGINATOR j fG1 DATE t-M-% g7g DESIGN VERIFIER #/;// DATEp.2b/6 f. c. Lanyard Number: N11G00103DLY Pre-Op. Isometric Drawing: M-1654, Rev. 2 Sheet 13 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. d. Lanyard Number: N11G00104DLI Pre-Op. Isometric Drawing: M-1654, Rev. 2 Sheet 14 of Appendix B i Evaluation Result: Acceptable. During the period that 100% power level thermal expansion data was taken, this Lanyard ~ Pot was not operating properly. However, thermal expansion data at 75% power level at this lanyard pot had similar hot conditions to the hot conditions at 100% power level, this indicates that the piping was allowed to expand thermally to its maximum position. The recorded thermal movement at 75% power level is within the expected limits, therefore the piping thermal expansion is acceptable, e. Lanyard Number: N11G00106DLY Pre-Op. Isemetric Drawing: M-1654, Rev. 2 Sheet 15 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. f. Lanyard Number: N11G00102DLY Pre-Op. Isometric Drawing: M-1654, Rev. 2 Sheet 18 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. g. Lanyard Number: N11G00301DLZ Pre-Op. Isometric Drawing: M-1658, Rev. 3 Sheet 19 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the acceptable limits. A stress analysis (Calc. No. STR-118) was performed by utilizing the recorded line temperature and the recorded line movement. From this analysis, the stresses were found to be within the code allowables. Therefore, piping thermal expansion is { acceptable. i

j CALCULATION NO.*t MC-Q1111-85039 y i,TTlr/T;T REVISION NO.r 0-IO D %00C l SHEET 13 CONT. ON SHEET 14 i ORIGINATOR jfQ)') DATE /.M.% PA?E l3 0F l2l lJ DESIGN VERTEIER # 4 v DA"'E j.r p -sc 'h. Lanyard Number: N11G00302DLY Prn-Op. Isometric Drawing: M-1658, Rev. 3 i Shee.t 20 of Appendix B Ersluation Recsit: Acceptable. The recorded thermal-mowment 10 outside the acceptable limits. A stress analysis. TCalc.' No. STR-118) was performed by utilizing the recorded line temperature, the recorded RPV temperature, and the turbiue casing temperature at' rated plant power. From this analysis,,the stresses were found to be within the code 4 i allowablesLund the recorded thermal movement at rated plant power is acceptable. 1

i. Lanyard Number: N11G00401DLZ Pre-Op. Isometric Drawing: M-1659 Rev. 3 Sheet 21 of Appendix B_

Evaluation Result: Acceptable. The recorded thermal movement is within the axpected limits.

j. Lanyard Number: N11G00402DLX Pre-op. Isometric Drawing: M-1659, Rev. 3 Sheet 22 of Appendix B

Evaluation Result: Acceptable. The recorded thermal movement is outside the acceptable limits. A stress analysis (Calc. No. STR-118) was performed by utilizing the recorded line temperature, the recorded RPV temperatute, and the recorded' turbine casing temperature. From this. analyr:1's, the stresses were found to be within the code - allowables and the recorded thermal movement at rated power is' se c ~-p t abic. k. Lanyard Number: N11G'00403DLZ / Pre-Op. Isometric Drawing: M-1659, Rev. 3 i Sheet 23 of Appendix B .e Evaluation Result: Acceptable. The recorded thermal movement is outside the acceptable limits. A stress analysis (Calc. STR-118 Rev. B) was performed by utilizing f the recorded line temperature and the recorded pipe displacement. The results of this analyisis indicate that i the piping strences are within the code allowables and also all nozzle and support loads are less than the previous design loads. Therefort, pip'Ing thermal expansion is ( acceptable. \\ l

l",.-.......,_ j CALCULATION NO.: MC-Q1111-85039 REVISION No.: 0 TO ?tv\\I g(,l goq M : SHEET 14 CONT ON SHEET 15 ~ s ORIGINATOR Jf@l DATE t-1f-St. I U N Y I DESIGN VERIFIER #d,rp# DATE /-274/,

6.1.7 System

N19-Condensate System Stress Problem Number: 1129 and 1194 Pre-Op. Isometric Drawing: M-1695A Rev. 1, and M-1695D Rev. 1 Calculation Number: STR-108 Evaluation Results Summary: Acceptable. Piping thermal movements were recorded at two locations. The recorded thermal movements are within the expected limits for one lanyard pot and outside the expected limits but within the acceptable limits at the other lanyard pot. A stress analysiIs (Cale. No. STR-108) was performed by utilizing the recorded temperature distribution. From this analysis, the stresses were found to be within the code allowables and that all recorded thermal movements are acceptable. All recorded data has been evaluated for rated plant power and the evaluation result for each lanyard pot is given below, a. Lanvard Number: N19G00101DLZ Stress Problem Number: 1129 Pre-Op. Isometric Drawing: M-1695A, Rev. 1 Sheet 16 of Appendix B Evaluation Result: Acceptable. The recorded thernal movement is outside the expected. limits but still within the acceptable limits. A stress analysis (Calc. No. STR-108) was performed by utilizing the recorded temperature distribution. From this analysis, the stresses were found to be within the code allowables and that the recorded thermal movement is acceptable. b. Lanyard Number: N19G00401DL7 Stress Problem Number: 11'4 Pre-Op. Isometric Drarin a V,5595D, Rev. 1 Sheet 17 of Appendix 'b Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits.

6.1.8 System

B33-Recirculation (Shutdown Cooling) Stress Problem Number: 323 Pre-Op. Isometric Drawing: M-1661 Rev. 3 Calculation Number: STR-125 Lanyard Number: B33G023RB6DLX Sheet 30 of Appendix B

CALCULATION No.: MC-Q: 111-85039 lI,, ' /.? REVISION NO.: 0 C SHEET 15 CONT. ON SHEET 16 TO P N %_..OO l2q ORIGINATOR II@l, DATE /Wi.86 p;al 15 07 111 DESIGN VERIFIER pg/ DATEgg N o Evaluation Result: Acceptable. The recorded thermal movement is within the expected linits for the line temperature distribution.

6.1.9 System

E12-Residual Heat Removal System (Shutdown Cooling) Pre-Op. Isometric Drawing: M-1661 Rev. 3, M-1662 Rev. 3, M-1663 Rev. 2 M-1664 Rev. 2, M-1665 Rev. 2, M-1667 Rev. 2, M-1693 Rev. 1 Calculation Number: STR-125 Rev. B Evaluation Results Summary: Acceptable. The piping thermal movements were recorded at fifteen locations using nineteen lanyard pots. The recorded thermal movements are within the expected limits for three lanyard pots, outside the expected limits but within the acceptable limits for six lanyard pots, outside the acceptable limits for four lanyard pets, and six lanyard pots did not receive a thermal load. Lanyard pots E12G00901DLY, E12G00902DLY, E12G01401DLX, E12G01402DLY, E12G01403DLX, and E12G01404DLZ did not see any temperature increase due to the over sizing of the RHR Heat Exchangers. Therefore, a walkdown (Reference 2.11) of the lines in cuestion was performed by NPE to determine if any interferences exist. It was determined that no interferences exist and that the pipe will move as expected. Therefore, no thermal expansion data needs to be taken for these lanyard pots. Stress analyses (Calculation No. STR-125 Rev. B) were performed on the remaining lanyard pots by utilizing the recorded line temperature distribution and the recorded line movements. From l these analyses the stresses were found to be within the code allowables and that all recorded thermal movements are acceptable. All the recorded data has been evaluated and the evaluation result for each lanyard pot is given below'. a. lanyard Number: E12G01203DLY Stress Problem Number: 46 Pre-Op. Isometric Drawing: M-1661, Rev. 3 Sheet 31 of Appendix-B Evaluation Result: Acceptable. The recorded thermal movement is outside the expected limits but within the acceptable limits. Incorporating the recorded line temperature distribution, the recorded pipe thermal expansion is found to be within the expected limits. Therefore, the piping thermal expansion is acceptable.

l ~. m.......... j CALCULATION h0.: MC-Q1111-85039 REVISION NO. 0 To PMI g(p loo )2 7 ; SHEET 16 CONT. ON SHEET 17 c ORIGINATOR J Fed DATE / 9 6 i' Ib 7 MI DESIGN VERIFIER Mff DATE AzS./t b. Lanyard Number: E12G01204DLZ Stress Problem Number: 46 Pre-Op. Isometric Drawing: M-1661, R w. 3 Sheet 32 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. c. Lanyard Number: E12G01201DLI Stress Problem Number: 69C Pre-Op. Isometric Drawing: M-1661, Rev. 3 Sheet 33 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the expected limits but within the acceptable limits. A stress analysis (Calc. No. STR-125 Rev.B ) was performed by utilizing the recorded temperature distribution. From this analysis, the stresses were found to be within the code allowables and therefore, the recorded thermal movement is acceptable. d. Lanyard Number: E12G01202DLY Stress Problem Number: 69C Pre-Op. Isometric Drawing: M-1661, Rev. 3 Sheet 34 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the acceptable limits. A stress analysis (Calc. No. STR-125 Rev. B ) was performed by utilizing the recorded temperature distribution, and the RHR Heat Exchanger calculated nozzle movement. From this analysis, the stresses were found to be within the code allowables and therefore, the recorded thermal movement is acceptable. e. Lanyard Number: E12G01001DLZ Stress Problem Number: 46 Pre-Op. Isometric Drawing: M-1662, Rev. 3 Sheet 35 of Appendix B Evaluation Resulr* Acceptable. The recorded thermal movement is within the expected limits. f. Lanyard Number: E12G01002DLY Stress Problem Number: 69A Pre-Op. Isometric Drawing: M-1662, Rev. 3 Sheet 36 of Appendix B

CALCULATION NO.: MC-Q1111-85039 REVISION NO.: 0 f TT A0iGT.~ SHEET 17 CONT. ON SHEET 18 ~, g;L'l _ ORIGINATOR fF)7) DATE f-2.'J 9(. ,O ig gg ~ (1 ar 118 ] DESIGN VERIFIER g/// DATE j.z ?-P(,

h. -:?

Evaluation Result: Acceptable. The recorded thermal l novement is outside the acceptable limits. A stress analysis (Calc. No. STR-125 Rev. B) was performed by utilizing the recorded temperature distribution, and the RER 1 Heat Exchanger calculated nozzle movement. Trom this analysis, the stresses were found to be within the code allowables and therefore, the recorded thermal movement is acceptable. g. Lanyard Number: E12G01005DLX Stress Problem Number: 69A Pre-Op. Isometric Drawing: M-1662, Rev. 3 Sheet 37 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. h. Lanyard Number: E12G01005DLZ Stress Problem Number: 69A Pre-Op. Isometric Drawing: M-1662, Rev. 3 Sheet 38 of Appendix B Evaluation Result: Acceptable. During this rode of operation, this lanyard pot was not operating. However, a walkdown (Reference 2.11) of this line was performed by NPE and no interferences exist. Therefore, the pipe will move as expected. 1. Lanyard Number: E12G01901DLY Stress Problem Number: 69A Pre-Op. Isometric Drawing: M-1657, Rev. 2 Sheet 39 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the expected limits but within the acceptable limits. A stress analysis (Calc. No. STR-125 Rev. B) was performed by utilizing the recorded temperature distribution and the recorded line movement. From this analysis, the stresses were found to be within the code allowables and therefore, the recorded thermal movement is acceptable. J. Lanyard Number: E12G01301DLX Stress Problem Number: 69C Pre-Op. Isometric Drawing: M-1664, Rev. 2 Sheet 40 of Appendix B t

+ l CALCULATION NO.: MC-Q1111-85039 ,n,---- REVISION NO.: 0 [IcPmragco, SHEET 1 CONT ON SHEET Ig ORIGINATOR ffpl DATE f.M.% I NCE 19 'Ci Ill DESIGN VERIFIER x(/// DATE gf.pc, / Evaluation Result: Acceptable. The recorded _ thermal movement is outside the. expected 11iiifEs bE within the. acceptable limits-A' stress analysis (Calc. No. STR-125 Rev. B) was, performed by utilizing the recorded temperature distribution and the recorded line movement. From this analysis, the stresses were found to be within the code allowables and therefore, the recorded thermal movement is cceptable. Lanyard Number: E12G01302DLZ Stress Problem Number: 69C Pre-Op. Isometric Drawing: M-1664, Rev. 2 Sheet 41 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the expected limits but within the acceptable limits. A stress analysis (Calc. No. STR-125 Rev. B) was performed by utilizing the recorded temperature distribution and the recorded line movement. From this analysis, the stresses were found to be within the code allowables and therefore, the recorded thermal movement is acceptable. 1. Lanyard Number: E12G01303DLY Stress Problem Number: 69C Pre-Op. Isometric Drawing: M-1664, Rev. 2 Sheet 42 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the expected limits but within the acceptable limits. A stress analysis (Calc. No. STR-125 t Rev. B) was performed by utilizing the recorded temperature distribution and the recorded line movement. From this analysis, the stresses were found to be within the code allowables and therefore, the recorded thermal movement is acceptable. m. Lanyard Number: E12G02101DLZ l 1 Stress Problem Number: 139 Pre-Op. Isometric Drawing: M-1693, Rev. 1 l Sheet 43 of Appendix B t Evaluation Result: Acceptable. During this mode of operation this lanyard pot was not operating. However, while at rated power this lanyard pot was operating properly I and the recorded movement was determined acceptable, see Section 6.1.3. This indicates that the piping was allowed to expand thermally and is acceptable.

3 I*TT'*"?D.T g CALCULATION NO.: MC-Q1111-85039 REVISION No.: 0 SHEET 19 CONT. ON SHEET 20 TO ? N_ Qh,o_% ORIGINATOR g@77} DATE /-M.fC inE W 0F l'11 DESIGN VERIFIER M/ DATEj.2/ Wa 6.1.10 System: E51-Reactor Core Isolation Cooling (Shutdown Cooling) Stress Problem Number: 78 Pre-Op. Isometric Drawing: M-1674, Rev. 3 Lanyard Number: E51000101DLY Evaluation Result: Acceptable. The lanyard pot did not see any temperature increase due to the over sizing of the RER Heat Exchangers. Therefore, a walkdown (Reference 2.11) of this line was performed by NPE to determine if any interferences exist. It was determined that no interferences exist and that the pipe i vill move as expected. Therefore no thermal expansion data needs to be taken for this lanyard pot. 6.1.11 System: E12-Residual Heat Removal System (Steam Condensing) Pre-Op. Isometric Drawing: M-1661 Rev. 3, M-1662 Rev. 3, and M-1663 Rev. 2. Calculation Number: STR-124 Rev. B Evaluation Results Summary: Acceptable. The piping thermal movements were recorded at five locations. The recorded thermal movements are within the expected ibnits for one lanyard pot, outside the expected limits but within the acceptable limits for one lanyard pot, outside the acceptable limits for one lanyard pot, and two lanyard pots did not receive a thermal load. Lanyard pots E12G00901DLY and E12G00902DLY did not see any temperature increase due to the over sizing of the RHR Heat Exchangers. Therefore, a walkdown (Reference 2.11) of the line in question was performed by NPE to determine if any interferences exist. It was determined that no interferences exist and that the pipe will move as expected. Therefore, no thermal expansion data needs to be taken for these lanyard pots. Stress analyses (Calculation No. STR-124 Rev. B) were performed on the remaining lanyard pots by utilizing the recorded line temperature distribution and the recorded line movements. (Calculated movements of the RHR Heat Exchanges based on the i l inlet and outlet temperatures were incorporated were necessary). From these analyses the stresses were found to be within the code allowables and that all recorded thermal movements are acceptable. All the recorded data has been evaluated and the evaluation result for each lanyard pot is given below, i

CALCULATION NO MC-Q1111-85039 g /J ;//I..d.1 REVISION NO. 0 i SHEET 20 CONT. ON SHEET 21 TO E N 8lelO M M i ORIGINATOR g 67f/ DATE /-25-9(, PIM 2D CF 11: DESIGN VERIFIER #4// DATE /-27->te a. Lanyard Number: E12G01201DLX Stress Problem Number: 69C Pre-Op. Isometric Drawing: M-1661, Rev. 3 Sheet 44 of Appendix B Evaluation Result: Acceptable. The ' recorded thermal movement is outside the expected limits but within the acceptable limits. A stress analysis (Calc. No. STR-124 Rev. B) was performed by utilizing the recorded temperature distribution, the RER Heat Exchanger calculated nozzle movement, and the recorded line movement. From this analysis, thh stresses were found to be within the code allowables and therefore, the recorded thermal movement is acceptable. b. Lanyard Number: E12G01202DLY Stress Problem Number: 69C Pre-Op. Isometric Drawing: M-1661, Rev. 3 Sheet 45 of Appendix B i Evaluation Result: Acceptable. The recorded thermal movement is outside the acceptable limits. A stress analysis (Calc. No. STR-124 Rev.B) was perforned by utilizing the recorded temperature distribution, and the RHR Heat Exchanger calculated nozzle movement. From this analysis, the stresses were found to be within the code allowables and therefore, the recorded thermal movement is acceptable, c. Lanyard Number: E12G01002DLY Stress Problem Number: 69A i Pre-Op. Isometric Drawing: M-1662, Rev. 3 Sheet 46 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. 6.1.12 System: E51-Reactor Core Isolation Cooling (Steam Condensing) Stress Problem Number: 64 Pre-Op. Isometric Drawing: M-1674 Rev. 3 Calculation Number: STR-124 Rev. B Evaluation Results Summary: Acceptable. The piping thermal movements were recorded at two locations. The recorded thermal movements are within the expected limits for one lanyard pot and outside the expected limits but within the acceptable limits for the other. I I i 1

CALCULATION NO.: MC-Q1111-85039 } REVISION NO.: O t ...,.,. :.f. SHEET 21 CONT. ON SHEET 22 TO Y M I 8(,!O D W ORIGINATOR

1. W\\

DATE 84 NE ?.1 j l7l DESIGN N FIER W DATE /-MG Neither lanyard pot saw very much temperature increase. Therefore, a walkdown (Reference 2.11) of the line in question was performed by NPE to determine if any interferences exist. It was determined that no interferences exist and that the pipe will move as expected. All recorded data has been evaluated and the evaluation result for each lanyard pot is given below, s. Lanyard Number: E51G00102DLZ Sheet 47 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is outside the expected limits but within the. I acceptable limits. Since a walkdown (Reference 2.11) was performed and no interferences were identified, the piping thermal movement is acceptable. b. Lanyard Number: E51G00103DLY Sheet 48 of Appendix B Evaluation Result: Acceptable. The recorded thermal movement is within the expected limits. 7.0 COMPUTER CALCULATIONS Even though Nuclear Plant Engineering did not perform any computer calculations for piping thermal expansion data evaluation, Bechtel GPD stress group performed various computer calculations using Bechtel program ME101. All computer calculations are referenced in Section 6.1 as applicable. 8.0

SUMMARY

OF RESULTS/ CONCLUSIONS l Piping thermal expansion was recorded for twelve (12) systems during power ascension at forty-eight (48) locations. Fifty-six (56) Lanyard Pots were utilized for data recording on the BOP (Non-NSSS) piping systems. During power ascension, walkdowns were performed at intermediate and rated temperatures. Few interferences were identified and removed if necessary. Snubber and spring readings for various systems were taken at rated condition to supplement evaluation of recorded data needed. The evaluation has been performed by taking into consideration errors I involved in data collection (transducer resolution, temperature resolution) and temperature distribution during testing condition versus that used in analysis. l The evaluation of thermal movements for BOP (Non-NSSS) piping was performed by Nuclear Plant Engineering with assistance from Bechtel (GFD). The piping thermal movements recorded by thirteen (13) Lanyards are within expected limits; sixteen (16) Lanyards are outside expected limits but within l l l l

CALCULATION NO.: MC-Q1111-85039 ,7T*.:...*[ :T REVISION NO. 0 + SEEET 22 CONT. ON SHEET N/A E Sb,l0 N q ORIGINATOR fFM DATE I,M.fr,, i

icg QQ, N 111 I

DESIGN VERIFIER -/24f/u DATE /-]t.h acceptable limits, eighteen (18) Lanyards are outside acceptable limits, and nine (9) Lanyards had no thermal load. Stress analyses were performed if necessary by utilizing the recorded line temperature, snubber and spring readings and any interferences identified during power ascension at the rated vessel condition. From these analyses the piping stresses are within the code allowables for all monitored systems. Based on the above, it is concluded that the recorded piping thermal movements during power ascension testing at all locations are acceptable. .}}

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2.0 REFERENCES

9.0 CONCLUSION

2.0 REFERENCES

5.1.1 System

5.1.2 System

5.1.3 System

5.1.4 System

5.1.6 System

5.1.7 System

5.1.8 System

5.1.9 System

SUMMARY

SUMMARY

2.0 REFERENCES

6.1.1 System

6.1.2 System

6.1.3 System

6.1.4 System

6.1.5 System

6.1.6 System

6.1.7 System

6.1.8 System

6.1.9 System

SUMMARY

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