ML20064N347
| ML20064N347 | |
| Person / Time | |
|---|---|
| Site: | Catawba  |
| Issue date: | 03/21/1994 |
| From: | DUKE POWER CO. |
| To: | |
| Shared Package | |
| ML20064N338 | List: |
| References | |
| NUDOCS 9403290269 | |
| Download: ML20064N347 (21) | |
Text
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Attach' ment I ' Marked-up Techtlical Specification Page 4
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i t i I 4 I 4 9403290269 940321 n PDR ADOCK 050004135 P PDR '; i
p POWER DISTRIBUTION LIMITS 3/4.2.5 DNB PARAMETERS LIMITING CONDITION FOR OPERATION
- 2. Within 24 hours of initially being within the region of prohibited operation specified on Figure 3.2-1, verify that the combination of THERMAL POWER and Reactor Coolant System total' flow rate are restored to within the regions of restricted or permissible operation, or reduce THERMAL POWER to less than 5% of RATED THERMAL POWER within the next 2 hours.
SURVEILLANCE REQUIREMENTS 4.2.5.1 Each of the parameters of Table 3.2-1 shall be verified to be within their limits at least once per 12 hours. 4.2.5.2 The Reactor Coolant System total flow rate indicators shall be sub-jected to a CHANNEL CALIBRATION at least once per 18 months. The measurement instrumentation shall be calibrated within 7 days prior to the performance of the calorimetric flow measurementif 4.2.5.3 The Reactor Coolant System total flow rate shall be determined by precision heat balance measurement *at least once per 18 months. M [bp, (A.nT 3 C//Cl3 g atjdy RCS FWG) SHgc 86 MCAsO%D 05 //v6 CD4 (6G GLfold 1p/D bps, Aht?f1j1L/EEh 120 , l CONS 171AK3 6EMVEA [80/4 AVERA66f] VAL //J cal.0lW1Ef/(lcs
- FRoM PREV /ws ur)ats CATAWBA - UNITS 1 & 2 3/4 2-14 Amendment No. if/ (Unit 1) l Amendment No.Jtit (Unit 2)
g 4 4 Attachment 2 -
a , l Evaluation of Fossible RCS Ilow Reduction llelow The Technical Specification Minimum Measured Flow I imit The purpose of this evaluation is to demonstrate that the Catawba Unit i RCS 110w of 379,285 gpm, as detennined by a calorimetric, is acceptable for plant operation at 1(XFL power.11te Technical Specification minimum measured llow limit is 382,(XX)gpm, which means the RCS llow ' measured by the calorimetric is 0.71'1 below the minimum measured flow limit required for plant operation at 1(XY1 power. The current Catawba Technical Specification flow uncertainty as given in Figure 3.2 1 is 2.2'I flow. All existing Chapter 15 analyses account for this 2.29. Ilow uncertainty. The actual calculated flow measurement uncertainty is 1.939,110w, which means there is as much as 0.27'h flow margin available in the current uncertainly allowance of 2.29, flow. Since the Catawba - Unit I measured RCS Ilow is 0.71'L below the Technical Specification minimum measured flow limit, and there is potentially 0.27'1 flow matgin available, there remains a net flow reduction of behvcen 0.719, and 0.441 ilow which must be evaluated. The impact of a 0.719, flow reduction on the analyses documented in Chapter 15 of th - Catawba hclear Station FSAR is discussed below. Impact On DN13 Lirnited FSAR Chapter 15 Events The Catawba Unit i Cycle 8 (CIC8) reload report states that out of the total 10.79. DNB margin there is 4.6'1 margin availabic. The Instrumentation /Ilantware DNB penalty reported in the CIC8 reload report is a combination of two separaic penalties. The Instrumentation penalty accounts for instmmentation biases at Catawba and has a value of 2.8% The liardware penalty, also 2.8% accounted for a change between the original mixing vane grid design in the Lead Test Assemblics and confirmatory CIIF test section and the production grid design. A CilF testing program undertaken by B&W and DFC in 1992-1993 tested both grid designs and showed no significant difference in CilF perfonnance. This means that the llantware DNB penalty was in fact never required for production Mark-BW fuel. The 2.8'1 DNB flardware penalty for Mark BW fuel given in the CICS reload report is not required for CIC8. This conclusion was documented in late 1993, after the reload report for CIC8 was submitted. Therefore, the total Mark-BW DNf3 margin available for ClC8 becomes 7.#1 with the removal of the 2.8M. liardware penaity. Adequate cycle specific margin exists between the design (1.55) and statistical (1.40) DNBR limits to compensate for the DNB penalty associated with the possible reduction in flow below the Technical Specification minimum measured flow limit at full power. Of the 10.7'h available Mark-BW fuel DNB margin,7.49 currently remains unused. This available 7.4'h DNB margin represents 3.3% flow margin. 'lhe small percentage flow decrease of 0.71% llow, which conservatively translates to a 1.6% DNB penalty, can be compensated for by this available margin. For fresh Westinghouse OFA fuel, no margin is available. Catawba Unit 1 Cycle 8 contains only 9 OFA assemblics in the core and these assemblics operate at relatively low power levels. Using the sensitivity of radial peaking (Fall) to DNB a 1.6% DNB penalty will result in a Fall peaking penalty of 0.6% This means that as long as the OFA fuel assemblics in CIC8 are at least 0.6% lower in peak than the most limiting Mark-BW fuel, sufficient margin is available to compensate for the possible reduction io flow without using any of the 10.7% DNB margin between the design and statistical DNBR limits. The Fall of the highest peaked OFA fuel assembly in CIC8 is 19%
p , 5-lower than the most limiting Mark-BW fuel assembly and is therefore, non-limiting with respect to . DNIL Those transients in Chapter 15 which are DNB limiting have sufficient margin available to account for this small possible reduction in RCS flow. The following DNB limiting transients will - therefore not be af fceted by the small flow reduction below the Technical Speci0 cation minimum measured flow limit.'
- 15.1.1 Reduction in Feedwater Temperature 15.1.2 lucrease in Feedwater Flow 15.1.3 Excessive increase in Secondary Steam Flow -
15.1.4 Inadvertent Opening of a Steam Generator or Safety Valve 15.1.5 Steam Line Break I5.2.8 Feedwater Line Break 15.3.1 Partial Loss of flow 15.3.2' Complete Loss Of Flow 15.3.3 Locked Rotor 15.3.4 Reactor Coolant Pump Shaft Break 15.4.1 Zero Power Bank Wididrawal 15.4.2 Uncontrolled Bank Withdrawal at Power 15.4.3 Rod Cluster Control Assembly Misoperation 15.4.4 Stanup of an inactive Reactor Coolant Pump 15.4.7 inadvertent Loading of a Fuel Assembly In An Impmper Position 15.4.8 Rod Ejection Accident
- 15.5.1 Inadvertent Operation of ECCS During Power Operation .
15.6.1 Inadvenent Opening of a Pressurizer Relief Valve 15.6.3 Steam Generator Tube Rupture Impact On Secondary System Peak Pressure FS AR Chanter 15 Events The turbine trip peak secondary pressure analysis (15.2.3b) is perfomied with a sensitivity study on reactor coolant flow. A change of approximately 12% flow causes an increase in secondary pressure of approximately 2 psi due to increased primary to secondary heat transfer, and therefore the results of this analysis are not affected by the slight flow reduction. Furthermore, this demonstmtes that the flow assumption does not sufficiently affect heat transfer to sign 10cantly affect the results of peak pressure analyses. 3 Impact On Primary System Peak Pressure FSAR Chanter 15 Events - As stated above, a small change in RCS flow does not significantly impact the primary to secondary heat transfer. 7herefore the peak pressure analyses are not affected by the small change in RCS flow. In addition, the peak primary pressure analyses assume 15% steam generator tube plugging to decrease heat Imnsfer. Actual tube plugging is about 8%, and the margin of 7% tube plugging more than offsets the impact of 0.71% flow deficit for the following peak primary , pressure analyses: L
-' em+ g - , - - - j y rpq=-Tr
15.2.2 Loss of Extemal Load 15.2.3a Turbinc Trip 15.2.4 Inadvertent Closure of Main Steam Isolation Valves 15.2.5 Loss of Condenser Vacuum and Events Causing Turbine Trip 15.2.6 Loss of Non-emergency AC Power to Station Auxiliaries 15.2.7 Loss of Nonnal Feedwater Flow 15.3.3 lacked Rotor 15.4.2 Uncontrolled Bank Withdrawal at Power The following transients do not benefit from the steam generator tube plugging margin as discussed ' for the transients above. The peak pressum for these transients is reached so quickly that the heat ~ transfer impact of steam generator tube plugging and a reduction of flow below the Technical Specincation minimum measured flow limit will not affect the peak pnmary pressure results. In addition, significant margin to the acceptance criteria for these transients is available, the zero power bank withdrawal and rod ejection transient peak pmssure margin is 48 psi and 242 psi respectively. 15.4.1 Zero Power Bank Withdrawal 15.4.8 Rod Ejection Imnact On FSAR Section 15.2.8 Feed. water 1.ine Break Long Term Core Cooling Armlysis The Feedwater Line Break Accident, FSAR Section 15.2.8, long temi core cooling case will be , affected by a reduction in RCS flow below the Technical Specification minimum measured flow limit. Low flow reduces primary to secondary heat transfer, so a reduction in initial flow increases the likelihood of hot leg boiling. However, since die analysis assumes that reactor coolant pumps are tripped early in the transient (15 seconds), any penalty of the reduced flow is minimal on the long tenu core cooling case, in addidon, the analysis assumes 15% tube plugging to degrade primary to secondary heat transfer. The actual tube plugging is less than 8%, which is a benefit for the entire duration of the event compared to the short duration of the reduced flow penalty. The lower tube plugging is also beneficial since the loop flow resistance during natural circulation is lower, which will cause a lower temperature during the long temi com cooling case. Imp.act On FS AR Section 15.6.3 Steam Generator Tube Ruptum Dose Analysis Reduced RCS 110w may affect break flow rate slightly, but since the break flow rate is primarily dictated by the pressure difference across the break, the reduced flow effect will be small. The reduced flow will cause a reduction in the heat transfer capability and result in a decrease in secondary side pressure in order to transfer the same amount of energy. The decrease in secondary side pressure increases the break mass flowrate. Ilowever, the increase in break mass flowrate causes a more rapid depressurization of the primary, which results in an earlier reactor trip. The earlier reactor trip offsets the larger break flowrate so that the total mass transfer is essentially unchanged by the reduction in RCS How, in addition, the reactor coolant pumps are (dpped on loss of offsite power coincident with turbine trip on reactor trip. This means the post trip transient . behavior will not be affected by the reduction in RCS 110w Therefore, the SGTR dose analysis
. +.
will not be af fected significantly by a 0.71% reduction in RCS flow below the Technical Speci0 cation minimum measured flow limit. hnstet On FSAR Section 15.6.5 Loss of Coolant Accidents
'lhe large and small break Loss of Coolant Accidents wen: evaluated by Westinghouse for a reduction in RCS flow of 1% below the Teclutical Specification minimum measured flow limit.
The possible reduction in RCS How will result in a Peak Clad Temperature (PCr) penalty ofless than 10 F for both the small and large break LOCA. The current Catawba Unit i FSAR large break LOCA PCT is 1985 *F. A 10 F PCT penalty applied to this temperature will result in a PCI'of 1995 *F. This PCT is still 205 F below the 10CFR 50.46 acceptance criteria of 2200 F.
'Ihe Catawba Unit i FS AR small break LOCA PCT of 1440 *F would increase to 1450 F which -
is well below the acceptance criteria of 10CFR 50.46. Recent reanalyses of the large and small break LOCAs have been performed for steam generator tube plugging percentages of 18%, and will be included in the October 1994 Catawba FSAR update. These analyses resulted in PCTs of 2022 'F for the large break LOCA and 1235 F for the small break LOCA. A 10 F increase in these PCrs will also remain well below acceptance criteria of 10 CFR 50.46. In addition, the effect of a 10 *F PCT increase will have a negligible effect on the other 10CFR 50.46 acceptance criteria. hupact On FS AR Section 15.4.6 Boron Dilution Events There is no impact on the loron dilution events. These transients are not affected by a redaction in the minimum measured flow since they do not contain a flow assumption or use Dow as an input parameter. Sumany All of the Catawba FS AR Chapter 15 events have been evaluated for a flow reduction below the Tecluilcal Specification minimum measured flow limit. Margin exists for each of these transients i I to account for the small RCS flow reduction and allow Catawba Unit I to operate at 100% power.
'the margins available to account for an RCS Row reduction below the Technical Specification l
flow limit for FSAR Chapter 15 analyses include:
. Flow uncertainty margin, up to 0.27% flow.
. DNil margin in the Catawba Unit 1 Cycle 8 reload design,7.4% DNIl.
. Steam generator tube plugging margin, (15% for analysis vs. 8% actual). ,
. Margins to acceptance criteria,(PCT and peak pressure) -
For some FS AR Chapter 15 transients, RCS flow is not an important parameter and results in no impact due to a flow reduction below the Technical Specification minimum measured flow limit. 1
'lherefore, a reduction in RCS flow of 0.71% below the current Technical Specification minimum measured flow limit will not significantly impact the current FS AR Chapter 15 safety analyses.
'Ihese analyses have sufficient margin available to account for a flow reduction of 0.71% RCS
- 2. flow below the now limit and allow plant operation at 100% power. All FS AR transient analysis acceptance criteria continue to be met and the results of the analyses in the FSAR remain valid.
'The margin of safety as defined in the bases of the Technical Specifications will not be reduced.
1 4 1 Evaluation of Catawba Unit i Primary 1,oop ilydraulie Configuration Changes During the End-of-Cycle 7 Outage j I _ Core Reload Cycle 7 was designed with 49 Westinghouse fuel assemblies and 144 B&W fuel assemblics. Cycle 8 was designed with 9 Westinghouse fuel assemblics and 184 B&W fuel assemblies. 'Ihe pressure drop across a B&W fuel assembly is 2.4% less than across a Westinghouse fuel assembly. Consequently, core flow resistance decreases in proportion to the percentage of B&W fuel in the core. With an increase of 40 B&W fuel assemblics during the outage, the pressure drop scmss the j core at constant flow will decrease by approximately 0.11 psi. In reality, the reactor coolant pump operating point will shift to a slightly higher flow. 'this increase in flow will be indicated by an increase in the cibow tap AP itxlications (in absence of other hydraulic changes). The analytical ihmici assumed that 1/3 of the core (64 fuct assemblies) was Westinghouse fuel, whereas the actual number in Cycle 7 was 49. 'lhe analytical model also assumed that Cycle 8 was entirely B&W fuel, rather than including the 9 Westinghause fuel assemblics. This , . simplifying assumption resulted in a pressure decrease across the core of 0.18 vs. 0.11 psi, which j is not large in either situation. i l
&catm GenerqlorTube Pluccine The steam generator tube bundle pressure drops are affected by the number of tubes plugged and/or sleeved during each outage. Plugging and sleeving of tubes in the steam generators causes a reduction in the flow area which results in an increased pressure drop across the steam generator tubes. The number of tubes plugged and/or sleeved expressed as a percentage of steam generator tubes (4674 for Catawba Unit 1)is used to calculate the flow area through the steam generators in cach loop. "Ihe calculated steam generator tube plugging percentage assumes that 18 sleeves is equivalent to i plugged tube.
1 Given below are the Catawba Unit i Reactor Coolant System resistance changes and corresponding pressure drop changes as calculated by the RCS Ilow correlation described above. , 1 l 4 2
'l l
e j IICS Pressure 1) rop Changes For Changes In RCS Flow Resistance November 1993 EOC 7 Itefueling Outage
- 1.oop A Loop 11 Loop C LoopI) l Total SG Tube Plugging, % 6.95 3.47 11.17 10.06 3 Change in SG Tube Plugging 2.51 1.91 5.15 5.96 From Aug-92 Outage, %
SG Pressure Drop Change, psi + 1.28 + 0.94 +2.63 +2.91 Pressure Drop Change for 11&W -0.74 -0.69 -0.96 -1.01 Fuel (2/3rds to Full core), psi Total Change In RCS Pressure 40.54 +0.25 +1.67 + 1.90 Drop, psi Change in loop flow, % 0.32 0.15 1.00 1.13 l' 44
tVR-21-1994 L13:19 FROM ctg SYSTEMG DGltEERItG TO 93027052 P.02 Catawba Unit 1 Elbow Tap Tech Spec Chango NC Pumos No work was performed on the NC Pumps that could have contributed to a reduction in flow. fjbow Tao DP Data
- Average daily data was found that goes back to 1/1/92. We plotted it on two graphs.
one for cycle 6 and the other for cycle 7. We cleaned up the data by deleting bad data and data at off power days (<99%). Channels A1, C2, and C3 had drift problems during this period. They have been replaced in the last outage. On 8/5/93 all the trends go down by about 0.3%. The OAC scanner was recalibrated that day and it was out of calibration a small amount. Not all bad data was removed. The small dips you see in the negative direction were due to bad averaging. Occasionally a point will read invalid by the computer and this will be recorded as a zero reading for the 5 minute period in question. This will cause the daily average for that day to read low a slight amount. Rutledge Scarborough Catawba Systems Engineering l f l 1 03-21-1994 12:56PM 1 803 831~3462 P.02 !
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- ASO 308.24 297.91 305.0s 34567 341.05 337A2 i 307.78 318,40 294A3
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% 5/t M? 322.64 336A5 334.64 308.30 29?I46 305.16 345 93 341.11 338.53 307.77 31828 294.38
~ 6/1
~p43 322.43 33826 334A3 30826 297.66 306.11 345 78 340.92 33841 307.60 318.02 294.14 6/1893 32233 336.10 31429 308.13 29766 MS.03 345.52 34031 237AS 307El 317.94 293 99 5/1993 322.67 '
336.33 334.52 308,31 297A7 306.15 34576 340A8 33825 307.61- 317.96 294.08
&2093 322 A2 33037 334 55 30823 29715 305.09 34587 341 03 338 35 30788 318.19 294.23 S/2143 _ 322.76 338.32 33451 30822 297.68 005.05 345.86 341.02 338A0 307.76 317.83 293.98
~5/2243 322.82 336.36 334 55 30324 297.09 305.03 34511 34090 338.51 30745 317.97 29420
&2343 32218 336"33 334 56 308.31 29774 305.16 345 82 34037 33865 307.66 310.09 294.37 F24 93 322 71 33626 33447 30e09 297.67 304D4 345.76 340 93 336.43 307.50 317D4 29423 s/26Nr3 322.54 33633 334.53 300 30 297.72 305.12 345 88 341.06 33835 307J4 318.17 294.37
~ 5653 5 ~ E2 3 -71 336 30 334A9 308 28 29714 305.00 345.82 340.99 338.61 307.67 318.17 294.42
~dfif/65'3iF3 338 51 334 68 300.48 297A4 305.23 346 00 341.19 238.65 30714 $1825 294.55 Y28S3 322A5 03635 33413 308.45 29F88 30526 34i69 341.34 33858 30712 318.25 294 47 5/20S3 32245 336.04 33422 308.06 297 54 304.88 345 64 340A0 338.05 307.47 317.96 29420 6/30/93 322.60 33EOS 33422 306.15 297.67 304.94 345.69 34036 338.15 307A3 317.99 294 23 Mih3 32235 336.02 33421 308.03 297.50 304.80 345 68 34018 338.02 307A4 318.04 29427 G1/93 32230 336.09 33427 307.87 29756 304 90 346.62 34021 330.07 307.61 318 06 294.31
&2SI 32229 335.90 334 07 308.11 297.55 304.90 34$.56 340.68 33809 307.66 319.03 294 24 336.08 33423 308.18 297.51 305 03 345.66 340.90 338.14 30~7.63 318.04 294.29
&W3432262
&493 32214 336 07 334.18 30004 29713 304.92 34&78 340.95 338.03 307.60 318.09 29436 6/543 330D6 343.56 341.58 313.96 303.46 310.81 353.08 34822 345.22 31359 324.31 300.18 96M 328 94 342 48 340.50 313 25 302 59 310.10 352 06 34724 344.10 312.61 323 50 299.36 6/7N3 322A6 336.31 334.39 308.37 297D1 305.16 345.88 341D3 338.18 307J7 318 25 29447
&693'^~322.'70 3kOS 3N 24 308 21 296.82 305.01 345 82 341.02 338.00 30771 318.15 294 39 6/9&3 32738~5d19 338 83 311 81 301 A6 300.68 360 32 34551 342 60 911.37 321.96 298.00
&1%3 32512 339A6 33754 310.93 300.27 30719 349.08 34425~340.99 31021 320.93 296 99 W1143 322 55 336.31 334.39 308 30 297D1 30G7 345.77 341.00 3N01 307J2 318.18 294.38 6/12/93 ~ 32.09 3 345.87 343.79 3T5 82 305.42 312.68 35&15 360.35 347.03 315.18 326.08 301.79 6/13393 394 30 410.33 40733 375 18 36428 37331 419 88 416 91 409 99 374.33 387 96 358.95 W1493 158 29 167.94 18720 42502 412.94 42132 171.98 169 93 16748 42174 436.87 '406.21 915&N 4 38 10.04 1204 457A2 444.38 455 82 10 48 8 92 1020 45522 471.99 436 94 6/16/931 3 94 9 84 10.57 458to 444.73 46633 10 45 9.13 10.11 45929 475.33 440.18 6/1743! 3.87 9 93 10 73 460 10 446 71 45829 10 30 9 07 10.17 461.61 47719 44258 6/1893: 3.96 9 83 1067 461.57 448.06 459.82 10.37 9.08 10.09 462.69 478.94 44314 W1Q43! 3 64 9 87 10 78 463 21 449 53 48125 10.18 926 10.19 48429 460 59 445.35-
&2093i 3.81 972 10.64 464.58 450 99 462 85 10 24 8.94 10.03 46570 482 05 446.65
&21Mi 306 66 401.95 39928 430.46 417.03 4275a 22.02 20.57 21.69 426 02 44011 40847 6/22/93i 401 25 416 96 414 40 382 89 370 s? 38025 -
387.10 38364 38128
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381.38 39438 365.76 6/23/9 % 354.11 36858 366 37 33E66~ 32i55^ 36f77~5t7.82 373.51 Sf16U 336J9 348.56 32210 W24934_331.84 34487 343.14 31620 305~30 31DI35U6 349.73 3463 4 315.39 326.00 302.06
&2%1 329 66 34245 34046 314.37 30333 310.97 3E222 347.50 34587 313.30 324 04 200.17
#2&V3 32328 3f410 334.57 309.30 298 43 305 90 346 14 341.41 33645 308.19 318 82 295.16 6/27N3 322.91 335 77 33423 308 93 29626 30549 345.76 341.12 338.89 307.94 318 53 294.81
~M&93 32274 336.66 334.06 30813 298 06 145.39 345.85 340 97 33872 307A3 318.33 29466 629/93 322 66 33570 334.01 30664 297.95 305.40 345.74 341.07 338.48 307.14 31827 294.54 6/30@3 32328 33595 334 19 30650 298 02 30539 34&90 34126 338 53 907A4 318.40 294 68 7/1M; 323 51 335.89 334.12 306 31 296 05 30528 34533 34122 338.50 307A5 31823 294.55 7/2h3 323 05 35530 35390 308.21 EW52 30520 34669 341.12 338 28 307.69 31814 294.39 7/393 32343 (1 335.95 334.13 GM29 297 91 305.27 345 a3 34127 338.36 307.83 318.14 294.52 7/493 32351 336 82 334.06 308.37 297.96 30526 345.94 341.38 336 41 30772 318.00 294A3 7/W3! 326 03 338.03 33626 310.18 299.72 307.01 348 03 343 43 340.37 309 40 319 87 298.03 7/643i 330 65 343 78 341.99 314 80 304.16 311.82 35312 349 03 345.85 31311 324 47 300.42 7/7Mi 330 78 34330 342.17 314.94 304.17 31145 353D3 348.39 34584 31326 324,63 300 49 7/B93~ 330 95 344.08 34222 31475 30424 311.65 364.00 34944 345A4 31323 324.64 300.56 7N 93 330.33 34325 34135 313 89 303At 310 92 35111 348 45 344 90 31320 323.92 29941 7/1093 329 89 342.14 34023 313.02 302.69 310.05 352 07 347.51 343.85 312.42 323.05 299.04 7/11M 324 00 33821 334.35 3C4 26 2ffse 305.21 340.25 _ $41.85 338.02 30755 318.06 294.43 7/12/93i 32370 33618 334.19 308 01 29743 304.99 346.10 341.60 338.20 30780 31633 294.62 7/1W3y~323.21 333.54 308.13 297 68 305.06 346/>6 341.56 337.92 307A3 317.95 29429
'fIiVD3 52332-336.00 33E63 334.13 308.02 297.72 304.99 346.02 341 46 337 92 307h1 317 A t 294.18 7/15/93P053 42 335 88 308.05 297 60 305A9 345 87 341.38 337 90 30724 317.85 294,24 33394^
7/16M 323 03 33515 333AS
~ 3Df.95 297.64 30I62 345.90 34T58 337.07 30732 317.84 29421 7/17/93: 52f40~ 551/
3 3f3 8I57D3 2f737 304.90 345DO 341.38 337.85 307A2 317.95 29426 7/18/931 32448 337.02 335.10 30679 296 41 305 74 346.99 342.45 339.03 30021 318.82 295.08 7/1(av3! 331 49 S44.10 342h4 314.35 30579 311.55~35f0F~3558 34555 Si3.56 324 38 30029 7/2693! 32T63 33t.60 335.64 30W22 296.98 308 21 347.61 343 03 339 34 30s.53 S1920 295 47 7/2t/93 323C3 336 01 334 b9 367T6'2 297.63 304&3 346 00 335.34 331.30 36E35 317.81 2M.1T 7f2293! 323 48 33C8$ 333 94 307 96 297.52 304 90 345 95 341.39 33776 30724 317.84 29426 03-21-1994 09:32Ft1 1 803 831 3462 P.02
t1@-21-1994 - 09156 FROM OE SYSTEMS EtGINEERING TO 93827852 P.03
- Trno Al A2 i A3 B1 1 B2 B3 I C1 02 C3 1 D1 I D2 l D3 W2393 323 44 335D0 1 333 97 30603 [ 29748 304 94 ] 346.03 341.53 337.8) 307.37 I SW.93 J 29426 7/24&3 323 34 33522 '~ 333 88 307A4 297M 364C 345.47 341.32 337.79 30729 317.78 ~ 2942F 7/2WlE3 353.24 33556 333A4 307.91 297M 304 79 MSAS 341.31 337.86 30724 317A3 294 26 7% 93 323 18 335.72 33320 307.86 297A6 304 80 345.86 34142 337.75 307.31 317A0 294.29 7/27& 3 323 09 335 66 33373 307.75 2R11 300.44 34573 32709 %420 308.D9 3iff8 294 31 7/2W3 323 60 33627 33435 308 16 29fA7 305 19 346 42 341.95 338.25 307.78 318.32 294 T7
-7/2W93 g 334DS 29fh6 36I96^^535.15 341 64~~330.04 307.42 317.96 25I22-323 32~33592~~335796~306.02 7/30651 32357 33553 305W ~297 A9 304 96 345 s4 34145 337.91 207A0 817 92 294 38 7 /3143l 323 27 335.84 333D8 307.96 297A1 304.87 346.00 34130 33787 307A1 317.82 294.25 6/140! 323 44 336 00 334 11 30155~~2975f~30l58 346 01 34149 337.98 307A1 31f98 29f3d~
335.69 333D4 30D3~ 297.53 304D5 345 90 341.34 337.84 307.30 317.78 294.13 8/2/93 ( 323 47 8/M93 3E3 40 335.53 33383 3062'5 ~ 297W~36I47 345A6 340.11 337.84 307.32 317.80 29420 8/4kJ 32328 335.33 2362 36798 29737 304.70 345.62 341.04 337A9 306.95 81740 293.91 8 @ 93 322.96 334D9 33321 30785 297.19 304.61 34528 340A1 33725 306A2 317.1s 29370 6/6_/93g322 84 M5.03 33346 307 80 29724 304 49 34623 340.80 33f37 t 306.78 317.31 293 62 8/7/9 31 5 2.61 335.00 333 30 307A6 30454 34520 340.73 337.10 , 36576 317.16 293.76 W8/95F5i2 51 33492 33323 307.80~29728 297.17 363.51 34526 340.76 337.26 ! 306.66 317.13 293.72 8/993i 322 69 334.06 333.34 307AS 29724 304A9 345.30 340.78 337.27 i 306.72 317.11 293 82 8/10/93 322.65 335.01 33317 307 80 297.39 30449 34539 340.88 35127 i 30682 31724 293D2 8/11 322.87 335D7 33345 307D3 29735 304.60 345 41 340 80 337Al ! 306.84 31727 293 93 8/1265 322 78 335.18 333 53 307A4 29734 304.61 34542 340.89 337AS ! 306.76 31728 293.94~ 8/1343; 322.78 33509 333 43 507D3 29f51 36f62- ~5559 3 340.85 35f51 ! 365 52 3172D'~29355
~EIM5~322.64 335.05 335 F ~307.89 297.32 304 A9,_34529 340.72 33726j .. 306 79 317.18 293 85 8/1593 322.85- 335.14 33350 308 01 304 60 345A5 340A4 337.32 306.88 31745 294.05~
~5W8/95~325t0 '~35F9' 3 -33530 30797~~29729734 A13M 54 34534 340.77 33731 306.81 317.10 293~84 0/1743 322.18 33488 33329 307A1 297.16 304A1 346.12 340 61 337.12 30680 $17.11 293.69 t/16437~322.38 334D8 333.35 307D1 297.27 36i32 34825 340 73 337.11 306.78 317.18 293.79
~ T/9 0 7 532.50 335.01 333.38 30s.03 297A2 304 63 34548 340A1 337A2 306.92 317.15 293.84 8/20/93! . 322.89 33525 33358 307.99 29750 20461 346 64 341.00 33744 307.08 317.39 294.00 8/21/931 322.75 335 30 333.66 308.15 297.M 304.70 345.70 341.09 337.70 307.03 317 47 294.15 e/22&3 322A1 M498 33338 307.90 297.36 304A6 345A1 340A1 337.31 306.81 317.18 293D9 a/2WJ 322 42 334 87 33326 307.66 297.12 304 39 34622~ 340.68
~
33726 306.71 317.11 29335 8/2493 322 44 334.94 33333 307A4 297I2f ~ 304.39 3if20 340.64 337.36 307.09 317.00 29379
~iV255i~322.57 334 92 33331 30790 297.10 30438 34534 340A3 33732 306.76 317.14 293 93 8/2693 32256 33499 333.33 308 01 29726 304 57 345 37 340A3 33732 006.99 317.19 294.04 W27&3 32257 33455~~353.33 308D6 29f29 304.58 34543 340D'7~ ~ 35731 308.93 31725 294.03 M E93 322.54 334.94 333 30 307.97 29738 30450 34540 340 88 337.35 306 99 31724 29397 8/2943 33514 333.51 306S7 29725 36E58 3i5 53 341.08 33724 306.90 317.33 294.12
~8/30/93~322.46322T54 335.18 2351 308.03 29737 304.60 34547 340 89 337.37 306D9 317 26 25f6F~
8/3193: 352.76 336.12~ 333.44 307.96 2975f'56456 34545 340A6 337.35 306.87 317.25 294.10 Q/143~352f61 335.~04 ~ 3 539 30F07 29733 504 63 S452f '32678 33f53 36 (85 317.16 293 94 W2/93 322 43 334 83 333.16 307.82 297.12 304.37 345.17 340.64 337.01 506.81 31TT3 294.00 S'S93 322 51 I 334 90 $3326 307.82 297.09 304.34 34518 340.60 337.20 306.85 317.06 29386 9'493 _ 322.72 33438 33323 308.01 297.09 30451 34523 340.72 33726 300 86 317 33 294.12 l@ 93 ^ 322 90 553 s3 33329 30746 297 02 30439 34527 340.77 33726 30s.83 317.18 293.9s 9/GV3 322 98 334.95 333.31 307D8 297.09 3M 49 345.14 340.61 337.17 306.77 317.09 295 W
~Ih&3 323.15 334.94 33329 307D4 297.12 304 47 34520 340 44 337.02 30682 317.13 293.98 9/a&3 322.71 1 334 97 33330 307D2~ 29723 30395 34529 34022 336.79 306A9 317.12 293.91 QG93 322 40 i 35I 54~335}f 307D4 29721 304 49 34E00 340.00 336.72 306.97 317.07 293.96 W10/93 322 59 ' 334 99 333 39 307.99 29723 304 44 34528 340.10 336.68 307.04 317.18 294.13^
9/11/93 322.64 i M4.92 333 42 56fs4 29f06~ d4 3 42 3452f 340 14 336 74 307.02 317.03 25 I99 35dW
~
~5/ifr95^322 61 353 46 308 05 29722 30450 345.35 340.19 336 82 30T63 317T4' ~59Tif 9/13 S 3 322.46 334.99 333.46 30739 29720 30452 34546 .e40.33 336A8 306.65 317.23 294.19 71795 ~322 41 3505~ ~535'57 30ii2- ~29721 304 54 34547 34029 336 S4 56E95 31726 2diW W1593I222 52 334 85 333.44 307.86 297.15 30427 34535 340.14 336.62 336.93 317.09 294.19 W1693g 322.53 334.76 33335 307D4 29746 30429 345.17 33944 33649 306.40 3'7.01 294.00 W17/95 32252 1 334.79 33340 307$8 29747 30439 34629 340 01 336.54 306.76 3'7.03 2945f" b1893I 322.36 M4 69 33329 307.94 297.01 304.39 34522 339.92 33624 306.65 3'6.87 293.91 9/1W93l 322.19 334.79 33341 337D1 297.03 30435 34527 339 95 338 40 306 73 317.08 294.04 W20/93i 322 22 334.67 M3 30 307.94 297 09 30426 34503 33978 33645 306 67 316 95 293D4 9/21 &3 32234 334 82 33342 308.11 297.06 30448 345.36 340.05 33646 306.79 317.07 294.17 M2&3 323.14 334 81 333 43 308.04 297.12 304 43 34525 339.92 336A3 306.75 317.05 294.16 W2193 f t2 61
- 334 82 333 41 307S3 297.04 304.32 34528 33923 2644 306 71 316 93 294.02
_ W9r2543 24/93]Qb_3343'3483 333A4 30726 29f03 30428 34525 35 W~35656 366.64 31f93 2M W 322 35 t 72 43.17 307.98 297.10 304 44 345.06 339 85 33637 006.6& 317.04 293S8 9/2&93 322.62 335.00 333 45 306.03 29734 30450 345.32 340.13 336.53 306.87 294.06 lirJ793, 322.89 33i50 333]55 30f58 29720 304A8 34523 340.09 33640 30E76 $17.14~55597~ 317 63 M9/93 322.63 335.01 333.45 308.03 296.02 30448 34524 340.10 33654 306.75 317.11 293D9 W29&3 325 44 33748 336.01 310 06 299 45 30657 347D9 342.76 338.99 30692 $19 32 296.03 4 9/3093 330.17 342.39 340.63 313.73 302 98 31624 362 69 34734 343 02 312A3 323 06 29950 10/1&3 323.46 3E69 334 01 30s.61 297 83 30511 34596 340 84 336 76 307.48 31T83 294.65 1Crb93 322 77 3M 15 333 33 307.84 297.09 304 A3 345 41 340.19 33579 300D5 31722 294.11 10/W3 322.96 335.10 33325 307At 29747 304 42 345.42 33999 335.8F 306D0 317.31 29423 Id/U95~323T67'~3' 3 f0f'~355.21 307.78 297.02 304 30 34521 340.02 33547 306A0 317.16 294.12 10/593 323 43 i 334.91 333.18 307.58 296A9 304.16 345.12 33317 331 D3 306.69 317.01 293.96 , 10/6/93 323.11
- 334 57 332 79 307.46 296.75 303 99 344 s0 340 70 336A2 304 59 316A1 293.69 4 10/7/93 323.31 ! 334 83 332.98 307.62 296.85 304.14 34496 34089 336D6 306.67 316 95 293.81 )
60/8/93 322.96 i 335 05 33320 307.71 297.04 M425 345.11 341.06 336.S4 306.91 317.17 294.14 l 10hb93 32144 i 335.02 333,16 307.90 298D5 304 47 34523 341.18 337.17 306.93 31722 294.17 j 10/1393 321 43 ! 33514 333.29 307At 297.12 304.36 34525 341.15 337.19 1 306.97 31722 294.18 I 10/1143 3213a 335.13 333 30 307.96 297.12 304 44 ~35.33 34125 33721 i 307.02 31725 294.12 l l TOTAL P.03 1 03-21-1994 09134fd 1 803 831 3462 P.03 { l
MAR-21-1994 09:40 FROM CtB SYSTEMS B EINEERING TO 93827852 P.10
- Twne [ At i A2 A3 l St B2 B3 C1 C2 C3 01 1 D2 D3 10/12/93' 32139 j 335.05 333 20 ] 30781 297.02 304,33 345 22 341.06 33707 306A8 317 24 294.11 1t/1&93 315.11 l 331.70 32812 ' 30445 29520 300D9 340.07 335.88 335.98 306.60 314.71 292.76 10/163 321 70 , 336 09 333.26 30'7.85 297 06 304.40 345 20 341.10 337.07 306As 317.18 294 04 70 3/5 32125 i 334 95~ 333.13 307.81 297.03 304.34 34524 341.16 336 99 306D6 31723 294.07 10/1053' '321.79T335V5 ' ~333Ti I~30DI~296T9f' ~36O1 34518~ 34t.Os 336 91 36sha 3ifbo 293 65-10/11/93 32160 e 33489 333.06 307.75 297.06 3G428 34512 341.05 336.97 306A2 347.09 293 90 10/1M3 321.66 I s35 01 333 20 307 86 297.07 304.33 345 54~ 34124 337.12 306D0 317.16 it9( C 317.16-293.96
~
76/Ts53 3aE90 1 334.97 333.16 307.79 297.05 36426 34ti7 341.14 SWod-~306 8) 10/2650 321 59 335 06 33325 307.71 297.11 30423 845.32 34122 337.09 306.85 317.15 294 00 10/21/93 32148 334 97 333.16 307.73 297.06 30420 345 35 341.51 35E06 306.86 317.11 293.94 10/22,93 321 87 33508 333 28 30736 2ifi9 304.33 34537 341.32 33722 306 93 317.18 294.03 36/2'W3 _322.11 .. 33C37 333.66 306.11 297.32 304.69 346.68 341.63 337.46 30122 317.46 294.27 10/2493 322 44 j 335.48 333 62 306.18 297.43 304.64 345.83 341.77 33T65 307.31 317.46 29424 10/2993 322.36 i 336.45 333.64 366.14 297.33 304.64 54s80 341.72 337.71 307x 317.50 29425 10/26/93 322 34 i 335.52 333.71 308 M 297.53 304.83 34593 340.71 337.71 307.42 317.68 294.43 10/27/93- ' 32 2 56 335.70 333 91 30857 29714 305.03 340.10 341Do 337.80 207.67 317.68 294 63 10/28/93 322 62 .i 335 79 334 00 308 46 297.75 304 91 346 07 341.98 338.16 f 37.73 317.78 294 50 03-21-1994 09:17Ft1 1 803 831 3462 P.10
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