AEP-NRC-2010-76, Core Operating Limits Report, Cycle 19
| ML103410152 | |
| Person / Time | |
|---|---|
| Site: | Cook  |
| Issue date: | 11/24/2010 |
| From: | Gebbie J Indiana Michigan Power Co |
| To: | Document Control Desk, Office of Nuclear Reactor Regulation |
| References | |
| AEP-NRC-2010-76 | |
| Download: ML103410152 (18) | |
Text
INDIANA MICHIGAN Indiana Michigan Power One Cook Place POWERO Bridgman, MI 49106 A unit of American Electric Power Indiana Michig an Power.com November 24, 2010 AEP-NRC-2010-76 10 CFR 50.4 Docket No.: 50-316 U. S. Nuclear Regulatory Commission ATTN: Document Control Desk Washington, DC 20555-0001 Donald C. Cook Nuclear Plant Unit 2 CORE OPERATING LIMITS REPORT Indiana Michigan Power Company, the licensee for Donald C. Cook Nuclear Plant Unit 2, is submitting the Core Operating Limits Report (COLR) for Unit 2 Cycle 19 in accordance with Technical Specification 5.6.5.
Revision 0 of the Unit 2 Cycle 19 COLR is provided as an attachment to this letter.
There are no new or revised commitments in this submittal. Should you have any questions, please contact Mr. Michael K. Scarpello, Regulatory Affairs Manager, at (269) 466-2649.
Sincerely, Joel P. Gebbie Site Vice President DMB/jmr Attachment c: J. T. King, MPSC, w/o attachment S. M. Krawec, AEP Ft. Wayne, w/o attachment MDNRE - WHMD/RPS, w/o attachment NRC Resident Inspector M. A. Satonus, NRC Region III P. S. Tam - NRC Washington DC pc) 1
ATTACHMENT TO AEP-NRC-2010-76 Donald C. Cook Nuclear Plant Unit 2 Cycle 19 Core Operating Limits Report Revision 0
D. C.COOK UNIT 2 CYCLE 19: Revision 0 D. C. COOK UNIT 2 CYCLE 19 Revision 0 Donald C, CookNuclear Plant Unit:2 Cycle 19 Core-Operating Limits Report (COLR)
-Revision 0 Page' 1 of 16
A C. COOK UNIT 2 CYCLE.19 Revision 0 D. C. COOK UNIT 2 CYCLE 19 Revision 0 1.0 CORE OPERATING LIMITS REPORT This Core Operating Limits Report for the Donald C. Cook Nuclear Planit Unit 2 Cycle 19 has been prepared in accordance with the requirements of Technical Specification 5.6.5.
The analytical methods used to determine the core operating limits shall be those previously'reviewed and approved by the Nuclear Regulatory Commission (NRC) in:
- a. WCAP-9272-P-A, Westinghouse Reload Safety Evaluation Methodology, July, 1985
- b. WCAP-8385, Power Distribution Control and Load Following Procedures - Topical Report, September 1974
- c. WCAP-10216-P-A, Rev. IA, Relaxation of Constant Axial Offset Control/FQ Surveillance Technical Specification, February 1994 d, WCAP-10266-P-A, Rev. 2, The .1981 Version of the Westinghouse Evaluation Model Using BASH Code, March 1987.
- e. WCAP-12610-P-A, VANTAGE+ Fuel Assembly Reference Core Report, April 1995
- f. WCAP-8745-P-A, Design Bases for the Thermal Overpower AT and Thermal Overtemperature AT Trip Functions, September 1986
- g. WCAP-13749-P-A, Safety Evaluation Supporting the Conditional Exemption of the Most Negative EOL Moderator Temperature Coefficient.Measurement, March 1997 The Technical Specifications affected by this report are listed below:
2.1.1 Reactor Core SLs [Safety Limits]
3.1.1 SHUTDOWN MARGIN (SDM) 3.1.3 Moderator Temperature Coefficient (MTC) 3.1.5 Shutdown Bank Insertion Limits 3.1.6 Control Bank Insertion Limits 3.2.1 Heat Flux Hot Channel Factor (FQ(Z))
3.2.2 Nuclear Enthalpy Rise Hot Channel Factor (FNaH) 3.2.3 AXIAL FLUX DIFFERENCE (AFD) 3.3.1 Reactor Trip System (RTS) Instrumentation 3.4.1 RCS [Reactor Coolant System] Pressure, Temperature, and Flow Departure from Nucleate Boiling (DNB).Limits 3.9.1 Boron Concentration Page2 of 16
D.C. COOK UNIT 2 CYCLE.19 Revision 0 2.0 OPERATING LIMITS The cycle-specific parameter limits listed in Section 1.0 are presented in the following subsections.
These limits have been developed using the NRC-approved methodologies specified in Technical Specification 5.6.5.
2.1 SAFETY LIMITS 2.1.1 Reactor Core SLs (Specification 2.1.1)
In Modes 1 and 2, the combination of thermal power, pressurizer pressure, and the highest loop average temperature (Tavg). shall not exceed the limits as shown in Figure 6 for 4 loop operation.
2.2 REACTIVITY CONTROL 2.2.1 SHUTDOWN MARGIN (SDM) (Specification 3..1.1)
Shutdown margin shall be greater than or equal to 1.8% Ak/k for Tavg > 200OF Shutdown margin shall be greater than or equal to 1.0% Ak/k for Tavg
, 200'F
.2.2.2 Moderator Temperature Coefficient (MTC) (Specification 3.1.3)
- a. The MTC limits are:
The BOL/ARO-MTC shall be less positive or equal to the value given in Figure 1.
The EOL/ARO/RTP-MTC shall be less-negative or-equal to -4.10E-4 Ak/k/°F.
This limit is based on a Tavg program with HFP vessel Tang of 571.0 to 576.0 OF Where: ARO stands for All Rods Out BOL stands for Beginning of Cycle Life.,
EOL stands for End of Cycle Life RTP stands for Rated ThermalPower HFP stands for Hot Full Thermal Power.
Page 3 of 6f1:6
SD.C. COOK UNIT 2 CYCLE 19 Revision 0'
- b. The MTC Surveillance limit is:
The 300 ppm/ARO/RTP-MTC should be less negative or equal to -3.20E-4 Ak/k/ 0 F at a HIFP vessel Tav, of 571.0 to 576.0 'F
- c. The Revised Predicted near-EOL 300 ppm MTC shall be calculated using Figure 7 and the following algorithm:
Revised Predicted MTC = Predicted MTC + AFD Correction + Predicted Correction*
- Predicted. Correction is -0.30E-4 Ak/k/lF.
If the Revised Predicted MTC is less negative than the Surveillance Requirement 3.1.3.2 limit (COLR 2.2.2.b) and all of the benchmark. data contained in the surveillance procedure are met, then a MTC measurement in accordance with SR 3.1.3.2 is not required.
- d. The MTC Surveillance limit is:
The 60 ppm!ARO/RTP-MTC should be less negative or equal to -3.90E-4 Ak/k/i F at a HFP vessel Tavg of 571.0 to 576.0.°F 2.2.3 Shutdown Bank Insertion Limits (Specification 3.1.5),
The shutdown rods shall be withdrawn to at least 228 steps.
2.2.4 Control Bank Insertion Limits (Specifications 3.1.6)
- a. The control rod banks shall be limited in physical insertion as shown in Figure 2.
- b. Successive Control Banks shall overlap by 100 steps. The sequence for Control Bank-withdrawal, shall be Control Bank: A, Control Bank B, Control Bank C, and Control Bank D.,
2.3 POWER DISTRIBUTION LIMITS-2.3.1 AXIAL FLUX DIFFERENCE (AFD) (Specification 3.2.3)
- a. The Allowable Operation Limits are provided in Figure 3.
- b. The AD 'target band is +5% fora: cycle average accumulated burnup
,. , MWD/MTU [Megawatt Days/Metric Ton Uranium].*
>0.0 Page 4 of 16-
COOK UNIT 2 CYCL E49 A&4sion 0 D. C. COOK UNIT 2 CYCLE 19 Revision 0 2.3.2 Heat Flux Hot Channel Factor (FQ(Z)) (Specification 3.2.1) for P > 0.5
- CFQ F*c (Z) < 2CFQ. K(Z),
for P
- 0.5 F (Z)_< CF *K(Z) for P > 0.5 P
Fo (Z)*<_ 2
- CFO *K(Z) for P< 0.5 Whiere: P=- RATED THERMAL POWER THERMAL POWER
- a. CFQ 2.335 b K(Z) is provided in Figures 4.
tolerance .
- c. F4(Z) is the measured hot channel factor including a 3% manufacturing uncertainty and a 5% measurement uncertainty.
- d. W(Z) is provided in Table 1 for +5% AFD target band.
- e. Q(Z) =*Q (Z) x W(Z) x FP The W(z) values are generated assuming that they will be used for a full power surveillance.
When a part power surveillance is performed, the W(z) values should be multiplied by the factor 1/P, when P is> Q.5. When P is:< 0.5, the W(z).values should be multiplied by the factor 1/(0.5), or 2.0. This is consistent with the adjustment'in the FQ(z) limit at part power conditions.
Page 5.of 16
D. C. COOK UNIT 2 CYCLE 19 Revision 0
- f. For Cycle 19, Fp = 1.02 for all burnups associated with Note 2a of SRk3.2.1.2, except as shown in the table below. When no penalty is required, Fp 1.00.
Cycle Fp-Burnup Penalty (MWD/MTU) Multiplier 0 1.020 150 1.032 317 1.040 484 1.039 651 1.037.
818 1.035 985 1.032 1153 1.030 1320 1.028.
1487 1.026 1654 1.026 1821 1.027 1988 1.029 2155 1.032 2322 1.034 2489 1.036 2656 1.038 2824. 1.039 2991 1.039 3158. 1.037 3325 1.035 3492 1.031 3659 1.028 3826 1.023 4000 1.020 The burnup range only covers where Fp exceeds 1.02,. Linear -interpolation is adequate for intermediate cycle bumups.
2.3.3 Nuclear Enthalpy Rise Hot-Channel Factor (lH )(Specification 3.2.2)
FN*AH-- CFA * (1 + PFA *(1-P))
THERMAL POWER "
Where: =.RATED THERMAL POWER-
- a. CFAH 1.58:.
- b. PFH= 0.3 Page 61of 16
SD.C. COOK UNIT 2 CYCLE 19 Revision 0 2.4 INSTRUMENTATION -
2.4.1 Reactor Trip System (RTS) Instrumentation (Specification 3.3.1)
The Overtemperature AT and Overpower AT setpoints are as shown in Figure 5',
2.5.1 RCS Pressure, Temperature, and Flow Departure from Nucleate Boiling (DNB) Limits (Specification 3.4.1)
- a. Pressurizer Pressure shall be Ž 2172.4 psig +
- b. RCS Tavg shall be < 580.1 °F +
- c. RCS Total Flow Rate shall be > 366,400 gpm 2.6 REFUELING OPERATIONS 2.6.1 Boron Concentration (Specification 3.9.1)
The boron concentration of all filled portions.of the RCS, the refueling canal and the refueling cavity shall be greater than or equal to 2400 ppm*.
+ These are Safety Analysis values. With readability allowance, the corresponding values are 577.8'F for Tavg, and 2200 psig for Pressurizer Pressure.
-- This concentration bounds the condition of KI < 0.95 which includes a 1% Ak/k conservative allowance for uncertainties. The boron concentration of 2400 ppm includes a 50 ppm conservative allowance for uncertainties.
Page 7 of 16
D. C. COOK UNIT 2CYCLE 19 Revision 0 FIGURE I MODERATOR TEMPERATURE. COEFFICIENT (MTC). LIMITS 1.0 0.5 u-0 C6
() 0.0 xt H-0,
-0.5
-1.0
,0,. 10. 20 30 40 50 60 70 80 90: 100 Percent Rated Thermal Power Page 8.o 1'.
D. C. COOK UNIT 2 CYCLE 19 Revision 0 FIGURE 2 ROD BANK INSERTION LIMITS VERSUS THERMAL POWER 250 225 200 175 150 0~
125 0,
- D z0 100 0
O-
.75 50 25 0
0 10. 20 30 -,40 50 .60 70- 80 90 :"100 POWER (% of Rated Thermal Power)
~Page 9of,16
D. C. COOK UNIT 2 CYCLE 19 Revision 0 FIGURE 3 AXIAL FLUX DIFFERENCE LIMITS AS A FUNCTION OF RATED THERMAL POWER (RTP) 100 90 X
80 N
70 60 CL 50 140 0
30 20 10 0
FLUX DIFFERENCE (DELTA-I)
Page"10 of 16-'
D: C. COOK UNIT 2 CYCLE 19 Revision 0 FIGURE 4
.]K(Z) - NORMALIZED FQ(Z) AS A FUNCTION OF CORE HEIGHT 1.2 1.0 (0.0, 1.0) __ __(6.0,_1.01 (2.0, 0.925) 0.81
(.9 uJ w 0.6 z 0:4 0.2 0
- 0 2 4 6 8 1.0 12 CORE HEIGHT (FT)
Page J1 of-16.
D.C. COOK UNIT 2 CYCLE 19 ' Revision 0 FIGURE 5' (Page-1 of 2)
Reactor Trip System Instrumentation Trip Setpoints Overtemperature AT Trip Setpoint F 1_+/--r1-S 1 Overtemperature AT AT [K1 - K2 (T-V) + K 3 (P-P) 41 (A1)]
Where: AT = Measured RCS AT, °F ATo = Indicated AT at RATED THERMAL POWER,.OF T = Average temperature, °F
= Nominal Tavg at RATED THERMAL POWER, (< 576.0-F)
P = Pressurizer Pressure, psig P1 = Nominal RCS operating pressure (2235 psig)
I+-TIS] = The function generated by the lead-lag controller for Tang dynamic I + riS compensation
,2 Time constants utilized in the lead-lag controller for Tavg
> 28 secs. t2 < 4 secs.
S Laplace transform operator, sec K, < 1..19" K2 > 0.01331/°F K3 > 0.00058/psig fm (Al) = -3.5 { 3 3 %+ (qt - qb)} when qt - qb < -33% RTP
..0% of RTP: when -33% RTP < qt - qb< 6% RTP 6
+1.0 1(qt4qb).- %}. when qt:- qb > 6%RTP where qt and are percent .RATED THERMAL POWER. in the upper and lower halves of the core respectively, and qt t qb is total THERMAL POWER in percent RATED THERMAL POWER.
- This is a Safety Analysis 'value. Refer to,.Technical Requirements Manual for nominal value of this coefficient used. in programming the trip setpoint. "
Page 12 of 16:-
D. C, COOK UNIT 2 CYCLE M. .. Revision 0' D. C. COOK UMT 2 CYCLE 19~ Revision 0 FIGURE 5 (Page 2 of 2)
Overpower AT Trip Setpoint Overpower AT _<ATo [KC4 - K' L i2(ADIT -S 6(T - T11)
Where: AT = Measured RCS AT, IF ATo - Indicated AT at RATED THERMAL.POWER, -F T = Average temperature, .0F T":. = Nominal T,,g at RATED THERMAL POWER, (< 576.0 °F)
K4 < 1.16*
K15 0.02/°F for increasing average temperature; K5 = 0 for decreasing average temperature K6 0.00197/°F for T greater than T" ; K 6-0 for T less than or equal to T" 3S - The function generated by the rate lag controller for Tavg dynamic compensation 1+ rS "T3 Time constant utilized in the rate lag controller for Tavg; ' 3 > 10 secs.
S = Laplace transform operator, sec1 f2 (AI) - 0.0
- This is a Safety Analysis value. Refer to Technical Requirements Manual for nominal Value of this coefficient used in programming the trip setpoint. .
Page 13 ofD1
D. C. COOK UNIT 2'CYCLE 19 Revision 0,-
FIGURE 6s Re-actor Core Safety. Limits
.660 650 640 630 U- 620
> 610 1--.
Cn 600 590 0 0.2 0.4 0.6 0.8 1 1.2 Power (fraction of rated thermal power)
DESCRIPTION OF SAFETY LIMITS P RESSURE Power Tavg Power Tavg Power. Tavg F[
Power Tavg (psia) (frac) (S F) (frac) ( F) (frac) ( F) (frac) (F) 1775 0.00 615.4 0.98 583.8 1.02. 580.9 1.2 558.1 2000 0.00 631.8 0.86 605.8 0.96 597.5 1.2 568.5 2100 0.00 639.1 1".2" 0.82 614.0 0.96. 601.6 573.1 2250 0.00 649.2. 0.72 628.6 0.98 605:2 1.2 580.4.
2400 O.rOO 659.0 0.62 642.0 1.1 599.0 1.2 588.1 UNIT 2 ReactorCore Safety:Limits Page 14:of 16.
AD.
C. COOK UNIT 2"CYCLE 19 .Revision 0 FIGURE 7 Unit 2 Cycle 19 Predicted HFP ARO 30 PPM MTC Versus Burnup
-2.34E-04
-2.36E-04
-2.38E-04 cý _2.40E-04 0) 04
-2.42E 0)
L)
..- 2.44E-04 CL E
o-2.46E-04 0)
- 0 .
-2.48E-04
-2.50E-04
-2.52E-04 4-15000 16000 17000 18000 19000 Cycle Bumup (MWd/MTU)
Burnup,. MTC. MTC (MWd/MTU) (pcm!F) (Ak/k/°F)
.15000 -23.526 , -2.3526E.04:1:..
16,000. -23.935 -2.3935E-04 17,000_': -24.331 -2.4331E ,-04 18,000 -24.726 -2.4726E-04 19,000 -25.1-08 . -2.5108E-04 Page -15 of 16&
D. C. COOK UNIT 2 CYCLE 19 Revision 0 TABLE I Donald C.. Cook Unit 2 cycle 19 W(Z) Function Node Height Bumup (MWDIMTU)
Point (ft) 150 1000 2000 3000 4000 5000 6000 8000 10000 12000 14000 16000 18000 20000 20790 1 0.00 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 2 0.20. 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 3 0.40 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 4 0.60 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1:0000 1.0000 1.0000 1.0000 1.0000 1 0000 1. 0000 5 0.80 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1 0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1 0000 6 1.00 1.0000 .1.0000 1.0000 1.0000 1.0000 1.0000 , 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 7 1.20 1.1187 1.1172 1.1156 1.1144 1.1135 1.1129 1.1126 1.1130 1.1151 1.1191 1.1249 1.1324 1.1411 1.1476 . 1.1502 8 1.40 1.1173 1.1150 1.1129 1.1113 . 1.1102 1.1097 1.1097 1.1114 1.1146 .1.1190 1.1245 1.1312 1.1387 1.1447 1.1471 9 1.60 1.1154 1.1126 1.1100 1.1080 1.1068 1.1063 1.1067 1.1095 1.1138 1.1185 1.1236 1.1293 1.1357 1.1412 1.1433 10 1.80 1.1131 1.1101 1.1072 1.1051 .1.1039 1.1035 1.1042 1.1076 1.1124 1.1171 1.1217 1.1266. 1.1318 1.1367 1.1386 11 - 2.00 i.1103 1.1078 1.1054 1.1036 1.1026 1.1024 1.1031 1.1063 1.1106 1.1148 1.1187 1.1229 1-1273 1.1314 1.1331 12 2.20 1.1071 1.1054 1.1039 1.1027 1.1021 1.1021 1.1026 1.1051 1.1083 1.1116 . 1.1149 1.1183 . 1.1221 1.1255 1.1268 13 2.40 1.1036 1.1027 1.1019 1.1013 1.1011 1.1012 1.1017 1.1034 1.1057 1.1081 1.1106 1.1133 1.1162 1.1188 . 1.1199 14 .2.60 1.0998 1.0997 1.0996 1.0997 1.0998 1.1001. 1.1004 1.1014 1.1026 1.1041 .1.1058 1.1076 1.1097 . 1.1115 1.1122 15 2.80 1.0956 1.0963 1.0971 1.0977 1.0983 1.0986. *1.0989 1.0990 1.0991 1.0996. 1.1005 1.1015 1.1027 1.1036 1.1040 16 3.00 1.0913 . 1.0928 1.0944 1.0956 1.0965 1.0970 1.0971 1.0964 1.0955 1.0950 1.0949. 1.0951 1.0953 1.0953 1.0952 17 3.20 1.0874 1.0895 1.0916 1.0932 1.0943 1.0949 1.0949 1.0937 1.0920 1.0907 1.0899 1.0892 1.0886 1.0877 1.0874 18 3.40 1.0850 1.0872 1.0894. 1.0910 1.0922 1.0927 1.0926 1.0910 1.0890 1.0877 1.0870 1.0867 1.0864 1.0858 . 1.0855 19 3.60 1.0854 1.0873 1.0891 1.0905 1.0914 1.0916 1.0910 1.0888 1.0867 1.0864 1.0877 1.0903 1.0935 1.0952 1.0959 20 3.80 1.0870 1.0884 1.0898 1.0908 1.0912 1.0910 1.0902 1.0874 1.0854 1.0862 1.0895. -1.0948 1.1014 1.1053 1.1069 21 4.00 1.0894 1.0902 1.0909 1.0913 1.0913 1.0909 1.0898 1.0872 1.0857 1.0875 1.0922 1.0995 1.1082 1.1138 1.1160 22 4.20 1.0918 1.0918 1.0918 1.0917 1.0914 1.0908 1.0899 1.0880 1.0876 1.0905 1.0964 1.1048 1.1148 1.1216 1.1243 23 4.40 1.0940 10932 1.0924 1.0917 1.0911 1.0905 1.0899 1:0892 1.0904 1.0944 1.1012 .. 1102 1.1209 1.1285 . 1.1315 24 4.60 1.0960 1.0943 1.0927 1.0914 1.0905 1.0899 1.0896 1.0902 1.0929 1.0981 1.1056 1.1152 1.1263
- 1.1347 1.1380 25 4.80 1.0977. 1.0951 1.0927 1.0909 1.0896 1.0890 1.0891 1.0910 1.0952 1.1014 1.1095 1.1196 1.1311 . 1.1401 1.1436 26 5.00 1.0991 1.0957 1.0924 1.0900 1.0885 1.0879 1.0883 1.0915 1.0971 1.1043 1.1130 1.1234 1.1350 1.1445 1.1482 27 5.20 1.1000 1.0959 1.0919 1.0890 1.0872 1.0866 1.0873 1.0917 1.0987 1.1068 1.1159 1.1264 1.1380 1.1478 .1.1517 28 5.40 1.1006 1.0957 1.0910 1.0876 1.0855 1.0849 1.0860 1.0916 1.0998 1.1087 1.1181 1.1286 1.1401 1.1501 1.1541 29 5.60 1.1007 1.0950 1.0897 1.0858 1.0835 1.0829 1.0842 1.0910 1.1004 1.1100 1.1196 1.1298 1.1410 1.1512 1.1552 30 5.80 1.1002 1.0942 1.0885 1.0844 1.0819 1:0814 1.0829 1.0903 1.1004 1.1103 1.1199 1.1300 .1.1408 1.1509 1.1549 31 6.00 1.0992 1.0931 1.0872 1.0830 1.0805 1.0800 1.0816 1.0894 1.0997 1.1097 1.1192 1.1290 1.1394 1.1494 1.1533 32 6.20 1.0976 1.0914 1.0854 1.0811 1.0786 1:0782 1.0799 1.0878 1.0984 1.1083. 1.1176 1.1269 1.1369 1.1465 1.1503 33 6.40 1.0954 1.0892 1.0832 1.0789 1.0764 1.0759 1.0777 1.0858 1.0963 1.1061 1.1150. 1:1238 1.1332 1.1424 1.1460 34 6.60 1.0926 1.0864 1.0805 1.0762 1.0737 1.0733 1.0750 1.0831 1.0935 1.1030 1.1114 1.1197, 1.1284 1.1371 1.1406 35 6.80 1.0889 1.0829 1.0772 1.0731 1.0708 1.0704 1.0721 1.0798 1.0898 1.0987 1.1066 1.1141 1.1219 1.1300 1.1331 36 7.00 1.0853 1.0794 1.0737 1.0696 1.0672. 1.0668 1.0684 1.0759 1.0856 1.0941 1.1016 1.1086 1.1161 1.1237 1.1267 37 7.20 1.0843 1.0779 1.0717 1.0672 1.0646 1.0640 1.0657 1.0736 1.0836 1.0922 1.0993 1.1059 1.1127 1.1200 1.1228 38 7.40 1.0871 1.0799 1.0729 1.0678 1.0649 1.0643 1.0663 1.0755 1.0867 1.0953 1.1015 1.1062 1.1108 1.1168 1.1191 39 7.60 1.0895 1.0824 1.0757 1.0708 1.0680 1.0675 1.0695 1.0785 1.0892 1.0972 1.1024 1.1061 1.1094 1.1145 1.1165 40 7.80 1.0911 1.0847. 1.0786 1.0741 1.0715 1.0711 1.0730 1.0812 1.0910 1.0980 1.1025 1.1054 1.1079 1.1121 1.1138 41 8.00 1.0925 1.0866 1.0810 1.0769 1.0746 1.0742 1.0759 .1.0835 1.0924. 1.0986 1.1022 1.1042 1.1057 1.1090 1.1104 42 8.20 1.0934 1.0881 1.0831 1.0794 1.0773 1.0770. 1.0786 1.0854 1.0933 1.0985 1.1013 ' 1.1025 1.1031 1.1056 1.1066 43 8.40 1.0938 1.0892 1.0848 1.0816 1.0797 1.0795 1.0809 1.0869 1.0938 1.0981 1.1001 .1.1005 1.1003 1.1019 1.1026 44 8.60 1.0938 1.0898 1.0860 1.0832 1'0816 1.0815 1.0828 1.0882 . 1.0941 1.0974 1.0983 1.0975 . 1.0960 1.0965 1.0967 45 8.80 1.0928 1.0897 1.0867 1.0846 '1.0834 1.0833 1.0844 1.0888 1.0935 1.0963 1.0974 1.0971 1.0964 1.0971 1.0974 46 9.00 1.0929 1.0903 1.0879 1.0861 1.0852 1.0851. 1.0861 1.0899 1.0942 1.0972 1.0991 1.1002 1:1010 1.1027 1.1033 47 9.20
'1.0962 .1.0932 1.0904 1.0884 1.0874 1.0876 1.0890 1.0940 1.0995 .1.1031 1.1049 1.1054 1.1054 1.1068 1.1074 48 9.40 1.1015 1.0982 1.0951 1.0929. 1.0918 1.0920 1.0934 .1.0988 1.1047 1.1083 1.1099 1.1101 1.1096 :1.1109 1.1114 49 9.60 1.1066 1.1030 1.0997 1.0974 1.0962 1.0962 1.0977 1.1034. 1.1094 1.1132 1.1147 1.1146 1.1139 1.1151 1.1155 50 9.80 1.1112 1.1075 1.1039 1.1014 - 1.1001 1.1002 1.1017 1.1076 1.1140 1.1178 1.1191 1.1188 1.1177 - 1.1186. 1.1190 51 10.00 1.1156 1.1117 1.1079 1.1053 1.1039 1.1039 1.1055 1.1117 1.1183 1.1221 - 1.1233 . 1.1227 A1.1213 1.1221 1.1224 52 10.20 1.1196 1.1155 1.1116 1.1088 .1.1073 1.1074 1.1090 1.1154 1.1221 1.1260 1.1273 1.1266 1.1251 1.1258 1.1261 53 10.40 1.1231 1.1189 1.1148 1.1120 .1.1105 1.1105 1.1122 1.1186 1.1255 1.1294 1.1306 1.1297 1.1280 1.1287 1.1289 54 10.60 1.1258. 1.1215 1.1175 1.1146 -1.1130 1.1130 1.1147 .1.1212 1.1282 1.1322 1:1334 1.1326 1.1309 1.1316 1.1319
-55 10.80 1.1283 1.1239 . 1.1198 1.1168 1.1152 .1.1151 1.1168 1.1234 1.1304 1.1343 11353 1.1343 1.1323 1.1328 1:1330 56 11.00 1.0000 1.0000 1.0000 .1.0000 1.0000 :1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 57 11.20 1.0000 1:0000. 1:0000 1.0000 1.0000 1 0000 1.0000 1.0000 1,0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 58 11.40 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000" . 1.0000 59 11.60 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1 0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 60 11.80 1.0000 1.0000 -10000 .01.0000 1.0000 1.0000 1.0000 1.0000 10000 1.0000 1. 0000 1.0000 1.0000 1.0000 1.0000 61 12.00 1.0000 1.0000 1.0000. 1.0000 1.0000 - 1.0000- 1.0000 1.0000 1.0000 1 1.0000
.0000 1.0000 10000 10000 1.0000 Top and bottom 10% of core excluded.
Page 16 of 16.