geo.dcpp.o1. 0 iz13vision 1 attacment 6faiz makcdisi input parameters for calculations geo.dcpp.o1....

GEO.DCPP.O1. 3 0 IZ13VISION 1

ATTACMENT 6

PAGE 31 OF 81

Pacific Gas and Electric Company Geosciences245 Market Street, Room 418BBMail Code N4CP.O. Box 770000San Francisco. CA 9417

Fax415/973-5778 GEO.DCPP.01.3 0

REVISION

DR. FAIZ MAKDISI \GEOMATRDX CONSULTANTS2101 WEBSTER STREETOAKLAND, CA 94612

October 25, 2001

Re: Input parameters for calculations

DR. MAKDISI:

As required by Geosciences Calculation Procedure GEO.001, entitled Developmentand Independent Verification of Calculations for Nuclear Facilities," rev. 4, I amproviding you with the following input items for your use in preparing calculations.

1. The shear wave velocity profiles obtained in borings BA98-1 and BA98-3 in 1998are presented in Figure 21-42, attached, of Calculation GEO.DCPP.01.21,entitled 'Analysis of Bedrock Stratigraphy and Geologic Structure at the DCPPISFSI Site," rev. 0, and can be so referenced. These profiles were previouslypresented in Figure 10 of the WLA report entitled 'Geologic and GeophysicalInvestigation, Dry Cask Storage Facility, Borrow and Water Tank Sites," datedJanuary 5, 1999.

2. The average unit weight of rock obtained from the hillside has been determined tobe 140 pounds per cubic foot, as documented in a data report entitled "RockEngineering Laboratory Testing - GeoTest Unlimited."

3. Regarding the time histories provided to you on 8117/01, since the tectonicdeformation will be to the southeast, the positive direction of the fault paralleltime history is defined as to the southeast, as described in Geosciences CalculationGEO.DCPP.01. 14, entitled "Development of Time Histories with Fling," rev. 1,page 4.

4. The source of the shear modulus and damping curves are Figures Qi 9-22 andQ19-23, attached, from PG&E, 1989, Response to NRC Question 19 datedDecember 13, 1988, and can be so referenced.

Regarding format of calculations, please observe the following:

PAGE 320 Fo 81* t2fflfm.doc:rw:10t25/01

Faiz Makcdisi Input parameters for calculations

GEO.DCPP.o1. 3 0 REVISION j

Contents of CD-ROMs attached to calculations should be listed in the calculation,including title, size, and date saved associated with each file on the CD-ROM. If thenumber of-files is considerable, a simple screen dump of the CD-ROM contents issufficient.

If you have any questions regarding the above, please call me.

IC-

ROBERT K. WHITE

Attachments

PAGE 3 o OF 81

GEO.DCPP.01. 00 0 REVISION I

ATTACHMENT 7

PAGE 34 Op 81

Pacific Gas and Electric Company Geosciencos245 Market Street, Room 41.BMail Code N4CP.O. Box 770000San Francisco, CA 94177415/973-2792Fax 415/973-58 GEO.DCPP.01. 3 0

REVISION 1

DR. FAIZ MAKDISIGEOMATRIX CONSULTANTS2101 WEBSTER STREETOAKLAND, CA 94612

October 31, 2001

Re: Confirmation of preliminary inputs to calculations for DCPP ISFSI site

DR. MAKDISI:

A number of inputs to calculations for the DCPP ISFSI slope stability analyses havebeen provided to you in a preliminary fashion. This letter provides confirmation ofthose inputs in a formal transmittal. A description of the preliminary inputs and theirformal confirmation follow.

Letter to Faiz Makdisl from Rob White dated June 24, 2001. Subject:Recommended rock strength design parameters for DCPP ISFSI site slopestability analyses.

This letter recommended using * =50 degrees for the preliminary rock strengthenvelope in your stability analyses, and indicated that this value would be confirmedonce calculations had been finazed and approved. Calculations GEO.DCPP.01.16,rev. 0, and GEO.DCPP.01.19, rev. 0, are approved and this recommended value isconfirmed.

Letter to Faiz Makdlsi from Rob White dated September 28,2001. Subject:Confirmation of transmittal of inputs for DCPP ISFSI slope stability analyses.

This letter provided confirmation of transmittal of cross section I-I' and time histories,and indicated that these preliminary inputs would be confirmed once calculations hadbeen approved. Calculation GEO.DCPP.01.21, rev. 0, is approved and section I-I' asdescribed in the September 28 letter is confirmed. A copy of the figure from theapproved calculation is attached. Calculations GEO.DCPP.01.13, rev. 1, andGEO.DCPP.0 1.14, rev. 1, are both approved and time histories as described in theSeptember 28 letter are confirmed. A CD of the time histories from the approvedcalculations is attached.

PAGE 3O F81

page 1 of 2 kr2W.doc:rkw:10/31/01

si4.

Faiz Makisi Confirmation of preliminary inputs to calculations for DCPP ISFSI site

GEO.DCPP.01. t 0 REVISION IEmail to Faiz Makdisi from Joseph Sun dated October 24, 2001. Subject:Ground motion parameters for back calculations.

This email provided input for a back calculation to assess conservatism in clay bedproperties in the slope. Inputs included maximum displacement per event of 4 inchesand a factor of 1.6 with which to multiply ground motions for use in the backcalculation analysis. This letter confirms those input values, with the followinglimitation: these values have not been developed under an approved calculation,therefore should not be used to directly determine clay bed properties for use in forwardanalyses, but may be used for comparative purposes only, to assess the level ofconservatism in those clay bed properties determined in approved calculations

Letter to Faiz Makdisi from Jeff Bachhuber dated October 10i 2001. Subject:Transmittal of Revised Rock Mass Failure Models - DCPP ISFSI Project

This letter provided you with figures indicating potential rock mass failure models assuperimposed on section I-I'. This letter confirms PG&E approval to use these modelsin your analyses. These figures are labeled drafts and are currently being finalized in arevision to Calculation GEO.DCPP.01.21. Once this revision and the included figureshave been approved, I will inform you in writing of their status.

ROBERT K. WHITE

Attachments

PAGE 3 3 OF 81

page 2 of 2

?fIlqr

ATTACEMET 8

of 52GEO.DCPP.01.30, Rev. 3

Attachment 8LIST OF FILES FOR GEO.DCPP.01.30REVISION 3

FILE NAME DESCRIPTION LINK

README 30.DOC README file

Subdirectory. DEFORMP files

DEFORMP.EXE program_SETiEE.XLS rotated earthquake motionSETIEE.PRN ASCII from EXCEL/input for SETIEEXLS

DEFORMP EESETI?.1NPSETILL.XLS rotated earthquake motionSETILL.PRN ASCII from EXCEL/Input for SETILLXLS

DEFORMP LLSET1 ?.INPSET2EE.XLS rotated earthquake motionSET2EE.PRN ASCII from EXCEL/Input for SET2EEXLS

DEFORMP EESET2?.INPSET2LLXLS rotated earthquake motionSET2LL.PRN ASCII from EXCEL/Input for SET2LL.XLS

DEFORMP LLSET2?.INPSET3EE.XLS rotated earthquake motionSET3EE.PRN ASCII from EXCEL/Input for SET3EE.XLS

DEFORMP EESET3?.INPSET3LLXLS rotated earthquake motionSET3LL.PRN ASCII from EXCEL/Input for SET3LL.XLS

DEFORMP LLSET3?.INPSET5EEXLS rotated earthquake motionSET5EE.PRN ASCII from EXCEL/input for SET5EE.XLS

DEFORMP EESET5?.INPSET5LLXLS rotated earthquake motionSET5LL.PRN ASCII from EXCEL/input for SETSLL.XLS

DEFORMP LLSET5?.INPSET5MM.XLS rotated earthquake motionSET6EEXLS rotated earthquake motionSET6EE.PRN ASCII from EXCEL/input for SET6EE.XLS

DEFORMP EESET6?.INPSET6LL.XLS rotated earthquake motionSET6LL.PRN ASCII from EXCEL/input for SET6LLXLS

DEFORMP _LLSET6?.1NPSET6MMXLS rotated earthquake motionEESET1N.INP input for DEFORMPEESET1NDAT output from DEFORMP EESETIN.INPEESET1 P.INP Input for DEFORMP ___

EESETiP.DAT output from DEFORMP EESETiP.INPnESET2NJNP Input for DEFORMPI

EESET2N.DAT output from DEFORMP EESET2N.INPEESET2P.INP Input for DEFORMPEESET2P.DAT output from DEFORMP EESET2P.INPEESET3N.INP Input for DEFORMP_EESET3N.DAT output from DEFORMP EESET3N.INP

of 52GEODCPP.01.30, Rev. 3

Attachment 8LIST OF FILES FOR GEO.DCPP.01.30REVISION 3

FILE NAME DESCRIPTION LINKiESET3P.INP |Input for DEFORMPEESET3P.DAT output from DEFORMP EESET3P.INPEESET5N.INP Input for DEFORMPEESET5N.DAT output from DEFORMP EESET5N.INPEESET5P.INP Input for DEFORMPEESET5P.DAT output from DEFORMP EESET5P.INPEESET6N.INP Input for DEFORMPEESET6N.DAT output from DEFORMP EESET6N.INPEESET6P.INP input for DEFORMPEESET6P.DAT output from DEFORMP EESET6P.INPLLSETlN.INP Input for DEFORMP _____

LLSETIN.DAT output from DEFORMP LLSETIN.INPLLSET1P.INP Input for DEFORMPLLSETIP.DAT output from DEFORMP LLSETIP.INPLLSET2N.INP Input for DEFORMPLLSET2N.DAT output from DEFORMP LLSET2N.INPLLSET2P.INP input for DEFORMPLLSET2P.DAT output from DEFORMP LLSET2P.INPLLSET3N.INP Input for DEFORMPLLSET3N.DAT output from DEFORMP LLSET3N.INPLL-SET3P.INP Input for DEFORMPLLSET3P.DAT output from DEFORMP LLSET3P.INPLLSET5N.INP Input for DEFORMPLLSET5N.DAT output from DEFORMP LLSET5N.INPLLSET5P.INP Input for DEFORMPLLSET5P.DAT output from DEFORMP LLSET5P.INPLLSET6N.INP Input for DEFORMPLLSET6N.DAT output from DEFORMP LLSET6N.INPLLSET6P.INP Input for DEFORMPLLSET6P.DAT output from DEFORMP LLSET6P.INPEES5CL.INP Input for DEFORMPEE5SMC00.QSC Input for DEFORMP EES5CL.INPEE5SMC00.DAT output from DEFORMP EES5CL.INPEES6CL.INP input for DEFORMPEE6SMC00.QSC Input for DEFORMP EES6CL.INPEE6SMC00.DAT output from DEFORMP EES6CL.INPLLS5CL.INP Input for DEFORMPLL5SMC00.QSC input for DEFORMP LLS5CL.INPLL5SMCOO.DAT output from DEFORMP LLS5CL.INPLLS6CL.INP Input for DEFORMPLL6SMC00.QSC input for DEFORMP LLS6CL.INPLL6SMC00.DAT output from DEFORMP LLS6CL.INPDCMMS5.INP Input for DEFORMPDCMMS5.QSC Input for DEFORMP DCMMS5.INPDCMMS5.DAT output from DEFORMiP DCMMS5.INPDCMMS6.INP Input for DEFORMP _ _ _

DCMMS6.QSC input for DEFORMP DCMMS6.INPDCMMS6.DAT output from DEFORMP DCMMS6.INP


Attachment 8SETlER EXLS

with fling FP posfflve to south,E-E' positive up-sklpe338-180 35 DP-EE=123

deg rad sin123 2.146753167 0.838672NPTS =

DTa

Tine (sec)0.0000.0050.0100.0150.0200.0250.0300.0350.0400.0450.0500.0550.0600.0650.0700.0750.0800.0850.0900.0950.1000.1050.1100.1150.1200.1250.1300.1350.1400.1450.1500.1550.1600.1650.1700.1750.1800.1850.1900.195020002050.210

96250.005

FNFauit Normal

0.00074050.00074660.00073800.00074410.00073550.00074150.00073280.00073880.00072990.00073590.00072690.00073290.00072380.00072980.00072060.00072670.00071730.00072350.00071400.00072020.00071070.00071710.00070760.00071450.00070520.00071290.00070420.00071310.00070560.00071620.00071050.00072400.00072130.00073880.00073920.00075940.00076210.00078520.00079200.00082260.00083970.00088330.0009121

FP.tiing E-4 (4 rotate) E-e (with -FN)Fault Parallel

-0.000585 9.251991E-04 -3.168063E-04-0.0005585 9.303486E-04 -3.219558E-044.0005616 9.248114E-04 -3.131181E-04-0.0005656 9.321193E-04 -3.160253E-040.0005727 9.287153E-04 -3.049202E-040.0005787 9.376315E-04 -3.061352E-04

-0.0005858 9.335936E-04 -2.954963E44-0.0005878 9.397258E-04 -2.994282E04-0.0005858 9.311950E204 -2.930977E204-. 0005808 9.334347E244 -3.008382E-04-0.0005747 9.226197E-04 -2.966242E-044.0005876 9.238011E404 -3.055069E-040.0005608 9.123354E-04 -3.017423E4440.0005515 9.124251E-04 -3.117335E44-0.0005393 8.980999E-04 -3.106103E44-0.0005212 8.932807E44 -3.255942E204-4.0004949 8.711118E-04 -3.320296E44-0.0004575 8.559249E-04 -3.S75489E444.0004070 B204701E-04 -3.771025E440.0003424 7.905065E04 -4.175496E-04

4.0002666 7.412325E-04 -4.507882E2044.0001919 7.059357E-04 -4.969038E-044.0001303 6.643797E-04 -5.2245802E-44.0000990 6.530971 E-04 -5.452807E44-0.0001020 6.469729E-04 -5.358559E44-0.0001384 6.732085E-04 -5.224855E-04-0.0001990 6.989674E-04 -4.822344E-04-0.0002707 7.454540E244 -4.506090E-04-0.0003384 7.760364E-04 -4.074802E444.0003828 8.091216E-04 -3.9215802444.0003878 8.071167E-04 -3.846523E440.0003454 7.952933E-04 -4.190360244-0.0002545 7.435801E-04 -4.663378E44-0.0001263 6.881949E-04 -5.506739E-040.0000253 6.061939E-04 -6.336981E440.0001828 5.373472E-04 -7.364775E440.0003151 4.675338E-04 -8.107862E440.0003878 4.472591E-04 -8.697236E440.0003909 4.513286E-04 -8.770936E8240.0003434 5.028962E-04 -8.769533E-040.0002717 5.562935E-04 -8.522386E440.0002101 6263476E-04 -8.551825E-040.0001939 6.5936982E44 -8.706020E-04

------- LINES SKIPPED------

I


Attachment 8BETILL.*XLS

S&1: urammft~AwlomThmHAOUS

with fling FP posiltve to south,L-L' positive up-slope338-180 67 DP-LL9g1

deg rad sin91 1.588248278 0.999848NPTS =

DT z

Tlme (sec)0.0000.0050.0100.0150.0200.0250.0300.0350.0400.0450.0500.0550.0600.0650.0700.0750.0800.0850.0900.095O.1000.1050.1100.1150.1200.1250.1300.1350.1400.1450.1500.1S50.1600.1650.1700.1750.1800.1850.1900.195020002050210

96250.005FN

Fautt Normal0.00074050.00074660.00073800.00074410.00073550.00074150.00073280.00073880.00072990.00073590.00072690.00073290.00072380.00072980.00072060.00072670.00071730.00072350.00071400.00072020.00071070.00071710.00070760.00071450.00070520.00071290.00070420.00071310.00070560.00071620.00071050.00072400.00072130.00073860.00073920.00075940.00076210.00078520.00079200.00082260.00083970.00088330.0009121

4

FPflmg L-L' (* rolate) L-L' (Wth -FN)Fault Parallel

0.0005585 7.500942E-4 -7.306003E-04-0.0005585 7.652333E-04 -7.367394E-04.0.0005616 7A77174E-04 -7.28117SE-04.0.0005656 7.538770E-04 -7.341364E-0440.0005727 7A53517E-04 -7.253643E-04.0.0005797 7.515142E-04 -7.3128OOE-04.0.000585 7A28712E-04 -7.2242566E04.0.0005878 7A8905E-04 -7283894E-040.0005858 7.400117E-04 -7.19566E0-04

4.OOOB8 7A58726E-04 -7256O32E604.0.0005747 7.368083E.04 -7.167504E-04.0.0005676 7.42640E-04 -7.22872SE-04.0.0005606 7.334820E04 -7.139176E-040.0005515 7.393324E404 -7.2ODs3E-04

40.0005393 7299123E-04 -7.11O062E-04-0.0005212 7.356541 E.04 -7.174645E604-Q.0004949 7.258173E-04 -7.085442E-04.0.0004575 7.313242E-4 -7.153554E-04.0.0004070 7209644E-04 -7.067582E-04.0.0003424 7.2608%4E-04 -7.141353E-04-0.0002666 7.152049E-04 -7.058986E-04.0.0001919 7.203497E-04 -7.13651SE904.0.0001303 7.097359E4 -7.05188s6E-04-0.0000990 7.160685E-04 -7.126139E-04-0.0001020 7.06852SE-04 -7.032924E-04-0.0001384 7.151562E-04 -7.103267E-04-0.0001990 7.075750E-04 -7.006305E-04.0.0002707 7.176851 E-04 -7.08237SE-04-0.0003384 7.113871E-04 4.995780E-04-0.0003828 7.227510E-04 *7.09390SE-04-0.0003878 7.171700E-04 -7.036336E-04.0.0003454 7.298777E-04 -7.17821SE-04-0.0002545 7.25661sE-04 -7.167785E-04-0.0001263 7.40607E-04 -7.362743E-040.0000253 7.38646sE-04 -7.395281E-040.0001828 7.561241 E-04 -7.625046E-040.0003151 7.5644sE-04 -7.674931E-040.003878 7.782722E-04 -7.918087E-040.0003909 7.50383E-04 .7.98680SE-040.0003434 8.165220E-04 -8.285074E-040.0002717 8.348708E-04 -8.443534E-040.0002101 8.794594E-04 -8.867916E-040.0001939 9.086170E-04 -9.15382E-04

---------- LTXIS SKIPPED ----------

Page S of 52GEODCPP.01.30, Rev. 3

Attachment 8SZT2EE.ZLS

Gd~ dmd HdcYarlmca (rotated to FN, FP)

NPTS .8000DT r 0.005

FNTime (sec) Fault Normal

0.000 -0.0012450.005 0.0012270.010 -0.0012260.015 -0.0012080.020 -0.0012080.025 -0.0011910.030 4.0011910.035 4.0011740.040 -0.0011750.045 -0.0011590.050 4.0011810.055 -0.0011460.060 -0.0011490.065 -0.0011340.070 -0.0011380.075 -0.0011240.080 -0.0011290.085 4.0011160.090 4.0011220.095 4.0011110.100 -0.0011180.105 4.0011080.110 4.0011170.115 -0.0011080.120 4.0011190.125 4.0011120.130 4.0011250.135 -0.0011190.140 -0.0011340.145 -0.0011300.150 -0.0011470.155 -0.0011440.160 -0.0011630.165 -0.0011610.170 -0.0011820.175 4.0011790.180 -0.0012010.185 -0.0011980.190 4.0012200.195 4.0012140.200 4.0012350205 4.0012260.210 4.001244

FP-EE=123

deg rad123 2.146753167

FP(par., ling) E-EFault Parallel

0.0077200.0076860.0076510.0076180.0075840.0075510.0075180.0074860.0074540.0074230.0073920.0073620.0073320.0073040.0072750.0072490.0072220.0071980.0071730.0071520.0071300.0071130.0070950.0070820.0070690.0070610.0070550.0070540.0070540.0070610.0070710.0070890.0071100.0071410.0071760.0072220.0072740.0073390.0074130.0075010.0076000.0077170.007848

-' (4 rotate) E-E' (v.th -FN)

-5.248704E-03 -3.160412E-03-6.215032E403 -3.157267E-03-5.194964E-03 -3.139044E43-5.162191E-03 -3.135793E-03-5.143080E-03 -3.117520E43-5.111263E-03 -3.114219E43-6.093135E-03 -3.095755E43-5.062191E-03 -3.092487E43-5.045161E-03 -3.073947E-03-5.015313E403 -3.070602E-03-4.999520E-03 -3.051957E43-4.970883E-03 -3.048648E403-4.956383E-03 -3.029955E403-4.929126E-03 -3.026851E-03-4.916399E-03 -3.008086E-03-4.890719E-03 -3.005218E-03-4.879991E43 -2.986606E203.4.856282E43 -2.984032E-03-4.847947E203 -2.965632E-03.4.826690E-03 -2.963665E-03-4.821312E-03 -2945707E-03-4.803044E43 -2.944716E-03-4.801188E-03 -2.927428E-03-4.786446E-03 -2.927782E-03-4.788986E43 -2.911535E-03.4.778307E43 -2.913604E-03-4.785752E-03 -2.898909E43-4.780040E43 -2.903261E43-4.793269E43 -2.890826E43-4.793403E-03 -2.898508E-03-4.813517E-03 -2.889269E43-4.820209E-03 -2.901496E43.4.848204E-03 -2.896951E43-4.862534E-03 -2.915474E-03-4.899434E43 -Z917317E43-4.922427E-03 -2.944169E-03-4.969371E-03 2.954547E43-5.001892E-3 -2.992603E43-6.060278E-03 4.014422E43-5.103809E-03 3.066843E43-5.175038E43 -3.103687E435.231070E-03 -3.174647E43-6.317565E-03 -3.231118E43

- -LZES SKIPPED ----------

of 52GEODCPP.0130, Rev. 3

Attachment 8SBT2sLL.ZLS

nasmTh estaimYarlmca (rotated to FN, FP)

NPTS =8000DT = 0.005

FP-LL91

deg rad91 1.588248278

Time (see)0.0000.0050.0100.0150.0200.0250.0300.0350.0400.0450.0500.0550.0600.0650.0700.0750.0800.0850.0900.0950.1000.1050.1100.1150.1200.1250.1300.1350.1400.1450.1500.1550.1600.1650.1700.1750.1800.1850.1900.195020002050210

FNFault Normal

-0.001245*0.001227-0.001226-0.001208.0.001208.0.001191-0.001191-0.001174-0.001175-0.001159.0.001161-0.001146-0.001149.0.001134-0.001138.0.001124-0.001129-0.001116-0.001122-0.001111.0.001118-0.001108-0.001117-0.001108.0.001119-0.001112-0.001125-0.001119-0.001134-0.001130-0.001147-0.001144-0.001163-0.001161-0.001182-0.001179-0.001201-0.001198*0.001220.0.001214-0.001235-0.001226-0.001244

FP(par., ffing) L-L (4 rotate)Faslt Paraflel

0.007720 -1.379531 E-030.007686 -1.360744E-030.007651 -1.359031 E-030.007618 -1.34085SE-030.007584 -1.339758E-030.007551 -1.322198E-030.007518 -1.321811E.030.007486 -1.304766E-30.007454 -1.305096E-030.007423 -1.288766E-030.007392 -1.289914E-030.007362 -1.274305E-030.007332 -1.276273E-030.007304 -1.261388E-030.007276 -1 .264483E-030.007249 -1250428E-030.007222 -1.254657E-030.007198 -1.241638E-030.007173 -1.247209E-030.007152 -1.235339E-30.007130 -1.242464E-030.007113 -1.231857E-030.007095 -1.240749E-030.007082 -1.231519E-030.007069 -1.242498E-030.007061 -1.234761E-030.007055 -1.247843E-030.007054 -1.24182E-030.007054 -1.257133E-030.007061 -1 .252759E-030.007071 -1.270430E-030.007089 -1267434E-030.007110 -1.287206E.030.007141 -1.285233E-030.007176 -1.306751E-030.007222 -1.305250E-030.007274 -1.327965E-030.007339 -1.325796E-030.007413 -1.348877E-030.007501 -1.345116E-030.007600 -1.367344E-030.007717 -1.360480E030.007848 -1.380667E-03

L-L' with -FN)

1.110090.E031.092482E-031.091996E-031.074976E-031.075075E-031.058640E-031.059426E-031.043477E-031.044946E-031.029681 E-031.031932E-031.017346E-031.020378E-031.006466E-031.010570E-039.974295E-041.002699E-039.904219E-049.968493E-049.857231E-049.935958E-049.836059E-049.931112E-049.843431E-049.957610E-049.883001 E-041.001614E 039.95S369E-041.010922E-031.006297E-031.023620E-031.020018E-031.039039E-031.036013E-031.056289E-031.063191E-031.074070E-031.069639E-031.090151E-031.083315E-031.102080E-031.091 147E-031.106754E-03

-__-- LnS SKIPPED-


Attachment 8SET3ZE *fL~S

AmTw~cMnH~ck

NPTSDT

Time (sec)0.0000.0050.0100.0150.0200.0250.0300.0350.0400.0450.0500.0550.0600.0650.0700.0750.0800.0850.0900.0950.1000.1050.1100.1150.1200.1250.1300.1350.1400.1450.1500.1550.1600.1650.1700.1750.1800.1850.1900.1950.2000.2050.210

with fang FP-EE

deg rad2.1467531674391 0 123

0.005FN FP(pr., fling) e-e(4 rotate) E-E with -FN

Fault Normal Fault Parallet0.0019045 0.0000172 1.587899E-03 -1.606601E-030.0018992 0.0000192 1.582353E-03 -1.603257E-030.0018916 0.0000222 1.574329E-03 -1.598533E-030.0018890 0.0000232 1.571599E-03 -1.596902E-030.0018842 0.0000263 1.585923E-03 -1.594527E-030.0018846 0.0000273 1.565708E-03 -1.595413E-030.0018828 0.0000293 1.583098E-03 -1.595003E-030.0018864 0.0000293 1.566118E-03 -1.598022E-030.0018879 0.0000293 1.567376E-03 -1.599280-E030.0018949 0.0000253 1.575447E-03 -1.602951E-030.0018999 0.0000202 1.582390E-03 -1.604394E-030.0019105 0.0000091 1.597331E-03 -1.607233E-030.0019191 -0.0000061 1.612795E-03 -1.606194E-030.0019330 -0.0000303 1.837655E-03 -1.604650E-030.0019445 -0.0000606 1.663802E-03 -1.597792E-030.0019603 -0.0001050 1.701257E-03 -1.588839E-030.0019727 -0.0001606 1.741911E-03 -1.566984E-030.0019873 -0.0002333 1.793761E-03 -1.539623E-030.0019954 -0.0003242 1.850062E-03 -1A96908E-030.0020012 -0.0004383 1.917086E-03 -1A39613E-030.0019942 -0.0006757 1.986027E-03 -1.358931E-030.0019756 -0.0007434 2.061741E-03 -1.252018E-030.0019321 -0.0009403 2.132525E-03 -1.108269E-030.0018593 -0.0011736 2.198540E-03 -9201445E-040.0017377 -0.0014423 2.242879E-03 -6.718398E-040.0015520 -0.0017524 2.256014E-03 -3A72227E-040.0012705 -0.0020958 2.206958E-03 7.589186E-050.0008608 -0.0024796 2.072410E-03 6.285023E-040.0002682 -0.0028906 1.799247E-03 1.349434E-03-0.0005750 -0.0033259 1.329224E-03 2293629E-03-0.0017646 -0.0037602 5.680425E-04 3.527882E-03-0.0034253 -0.0041844 -5.937041E-04 5.151699E-03-0.0057049 -0.0045874 -2.286056E-03 7.283018E-03-0.0087388 -0.0050136 -4.598367E-03 1.005960E-02-0.0126050 -0.0055691 -7.538292E-03 1.360462E-02-0.0172980 -0.0064852 -1.097525E-02 1.803943E-02-0.0227180 -0.0080588 -1.466382E-02 2.344206E-02-0.0287730 -0.0105858 -1.836567E-02 2.989653E-02-0.0354910 -0.0141208 -2.207457E-02 3.745602E-02-0.0431510 -0.0183295 -2.620659E-02 4.617244E-02-0.0519270 -0.0223432 -3.138074E-02 5.571865E-02-0.0612440 -0.0250086 -3.774297E-02 6.498423E-02-0.0689540 -0.0252126 *4.409801E-02 7.156150E-02

---------- L S SKIPPED ----------


Attacbment 8SET3LL.X LS

semupc

NPTSDT z

Thie (sac)0.0000.0050.0100.0150.0200.0250.0300.0350.0400.0450.0500.0550.0600.0650.0700.0750.0800.0850.0900.0950.1000.1050.1100.1150.1200.1250.1300.135.140

0.1450.1500.1550.1600.1650.1700.1750.1800.1850.1900.1950.2000.2050.210

wfth ffing

43910.005FN

Fault Normal0.00190450.00189920.00189160.00188900.00188420.00188460.00188280.00188640.00188790.00189490.00189990.00191050.00191910.00193300.00194450.00196030.00197270.00198730.00199540.00200120.00199420.00197560.00193210.00185930.00173770.00155200.00127050.00086080.0002682

-0.00057500.0017646-0.0034253-0.0057049*0.0087388-0.0126050-0.0172980-0.0227180-0.0287730-0.0354910-0.0431510-0.0519270-0.0612440-0.0689540

FP-LL

deg Rd91 1.588248278

FP(par., fing) L-L(+ rotate)Fault Parallel

0.0000172 1.9039108-30.0000192 1.898576E-030.0000222 1.890924E-030.0000232 1.888307E-030.0000263 1.883455E-030.0000273 1.883837E-030.0000293 1.882002£-030.0000293 1.88502E-030.0000293 1.887101-E30.0000253 1.894171E-30.0000202 1.899258E-030.0000091 1.910050E-0

-0.0000061 1.918914E-03-0.0000303 1.933234E-03-0.0000606 1.945261E-03-0.0001050 1.961835E-03-0.0001606 1.975202E-03-0.0002333 1.991069E-03-0.0003242 2.000754E-03-0.0004383 2.008545E-03-0.0005757 2.003943E-03-0.0007434 1.988272E-03-0.0009403 1.948215E-03-0.0011736 1.679498E-03-0.0014423 1.762605E-03-0.0017524 1.582344E-03-0.0020958 1.306880E-030.0024796 9.039697E-04-0.0028906 3.185736E-04-0.0033259 -5.168314E-040.0037602 -1.698711E-03

-0.0041844 -3.351756E-03-0.0045874 -5.623976E-03-0.0050136 4.649976E-03-0.005591 -1.250589E-02-0.0064852 -1.718218E-02-0.0080588 -2.2S7391E-02-0.0105858 -2.858388E-02-0.0141208 -3.523917E-02-0183295 -4.282458E-02-0.0223432 -C.152918E-02-0.0250086 -6.079825E-02-0.0252126 -6.85031E-02

L-' With -FN

-1.9045108-03-1.899246E-03-1.8917004-03-1.889118E-03-1884371E-03-1.884789E-03-1.883024E-03-1.886624E-03-1.888124E-03-1.895052E-03-1.899963E-03-1.910368E-03-1.918702E-03-1.932177E-03-1.943146E-03-1.958168E-03-1.969597E-03-1.98282E-03-1.989438E-03-1.993248E803-1.883850E-03-1.962327E43-1Q1C396E-03-1.838536E43-1.712266E03-1.521183E-03-1.233733E03-8.174281E-04-2.176848E-046.329135E-041.829951E-033.497801E-035.784087E-03

8.824963E-031.270027E-021.740854E-022285517E-022.895335E-023.573202E-024.3464308-025230901E-026.167110E-026.938349E-02

----- LINES SKIPPED ----------


Attachment 8SETSEE.XLS

iEiftf w ng FP-EE=123Aw&azknumHdat

deg radNPTS = 4000 123 2.146753167DT= 0.010

FN FP E-E'(f rotate) E-E wlth -FNlime (sec) Fault Normal Fault Parlelfling

0.000 -0.0026956 0.0018180 -3250874E-03 1.270572E-030.010 0.0026859 0.0032331 -4.013483E-03 4.916933E-040.020 0.0026741 0.0046518 -4.776235E-03 -2.908517E 040.030 -0.0026602 0.0060633 -5.533335E-03 -1.071267E-030.040 .0.0026439 0.0074701 -6.285887E03 -1.851160E-030.050 -0.0026255 0.0088678 -7.031648E.03 -2.6277832E030.060 -0.0026045 0.0102091 -7.744599E.03 -3.375959E4030.070 -0.0025811 0.0114251 -8.387210E-03 -4.057820E.030.080 .0.0025554 0.0125160 -6.959822E-03 -4.673539E-030.090 .0.0025272 0.0135885 -9.520283E-03 -5.2B1302E2030.100 0.0024970 0.0147773 -1.014243E-02 -5.954109E2030.110 40.0024650 0.0161536 -1.086521E-02 -6.730557E-030.120 0.0024315 0.0176736 -1.166491E-02 -7.586453E-030.130 -0.0023974 0.0191830 -1.245840E-02 -8A37142E-030.140 4.0023629 0.0205885 -1.319496E-02 -9.231561E-030.150 -0.0023281 0.0219632 -1.391452E-02 -1.000950E-020.160 4.0022933 0.0234179 -1.467758E-02 -1.083093E-020.170 4.0022582 0.0251074 -1.556831E-02 -1.178053E-020.180 0.0022210 0.0269818 -1.655796E-02 -1.283259E-020.190 -0.0021800 0.0287436 -1.748312E-02 -1.382651E-020200 -0.0021323 0.0301943 -1.823325E-02 -1865665E-020.210 .0M020716 0.0312083 -1.873459E-02 -1.25981E4020.220 0.0019869 0.0318577 -1.901724E-02 -1.568453E-020.230 0.0018631 0.0322602 -1.913264E-2 -1.600758E-020.240 40.0016795 0.0327022 -1.9219382E2 -1.640228E4020.250 0.0014206 0.0337911 -1.959534E-02 -1.721250E-020.260 0.0010901 0.0361952 -2.062752E-02 -1.879952E020.270 0.0007060 0.0404655 -2.263107E-02 -2.144693E2020.280 40.0002328 0.0462256 -2.537140E-02 -2.498098E-020290 .0004952 0.0522430 -2.803817E-02 -2.886883E-020.300 0.0016827 0.0674921 -2.990110E-02 -3.272356E-020.310 0.0032301 0.0617259 -3.090923E-02 -3.632722E-020.320 .0045224 0.0655207 -3.189223E-02 -3.947784E-020.330 0.0048251 0.0694387 -3.377224E-02 -4.186559E-020.340 0.0041308 0.0730410 -3.631651E-2 -4.324528E 020.350 0.0035948 0.0751345 -3.790640E-02 -4.393577E-020.360 0.0049291 0.0746148 -3.650412E202 -4.4771S1E-020.370 0.0089773 0.0721844 -3.178532E-02 -4.684333E-020.380 0.0146650 0.0699841 -2.581684E02 -5.041508E-020.390 0.0194580 0.0698739 -2.173709E402 -5.437484E-02OA00 0.0210520 0.0714485 -2.125782E-2 -5.656924E-02OAO 0.0190370 0.0726945 -2.362634E02 -5.555793E-020.420 0.0142240 0.0723661 -2.748405E-02 -5.134258E-02

---------- -L S SKIPPED ----------

of 52GEO.DCPP.0130, Rev. 3

Attachment 8BET5LL .XaS

s:& E 03rtro

NPTS eDT =

Time (sec)0.0000.0100.0200.0300.0400.0500.0600.0700.0800.0900.1000.1100.1200.1300.1400.1500.1600.1700.1800.19002000210022002300240025002600270028002900.3000.3100.3200.3300.3400.3500.3600.3700.3800.3900.4000.4100.420

wrth flnig FP-LLw91

deg radE1 t.5882482784000

0.010FN FP L-L' R otate) L-L with -FN

Fault Normal Fault Parallelflling-0.0026956 0.00181804.0026859 0.0032331-0.0026741 0.0046518-0.0026602 0.0060633-0.0026439 0.0074701-0.0026255 0.0088678-0.0026045 0.0102091-0.0025811 0.0114251-0.0025554 0.0125160-0.0025272 0.0135885-0.0024970 0.0147773-0.0024850 0.0161538-0.0024315 0.0176736-0.0023974 0.0191830-0.0023629 0.0205885-0.0023281 0.0219632-0.0022933 0.0234179-0.0022582 0.0251074-0.0022210 0.0269818-0.0021800 0.0287436-0.0021323 0.0301943-0.0020716 0.0312083-0.0019869 0.0318577-0.0018631 0.0322602-0.0016795 0.0327022-0.0014206 0.0337911-0.0010901 0.0361952-0.0007060 0.0404655-0.0002328 0.04622560.0004952 0.05224300.0016827 0.05749210.0032301 0.06172590.0045224 0.06552070.0048251 0.06943870.0041308 0.07304100.0035946 0.07513450.0049291 0.07461480.0089773 0.07218440.0146650 0.06998410.0194580 0.06987390.0210520 0.07144850.0190370 0.07269450.0142240 0.0723661

-2.726916E-03-2.741913E-03-2.7S4872E-03-2765606E-03-2.773859E-03-2.779852E-03-2.78=264E-03-2.780086E-3-2.73428E-03-2.763948E-03-2.754499E-03-2.746523E-03-2.739552E-03-2.731798E-03-2.721831E-03-2.711028E-03-2.701818E-03-2.696007E-03-2.691522E-03-2.681274E-03-2.658898E-03-2.615902E-03-2.542548E-03-2.425791E-03-2.249932E-03-Z010075E-03-1.721579E-03-1.412018E-03-1.039410-E03-4.165514E-046.791481E-042.152426E-033.378305E-033.612586E-032.655527E-032.282875E-033.626242E-037.716238E-031.344147E-021.823566E-021.980194E-021.776551E-021.295897E-02

2.663463E-032.629069E-032.592514E-032.S53984E-032.513135E-032.470348E-032.425943E-032.381328E-032.336593E-032.289682E-032.238740E-032.182726E-032.122707E-032.062271E-032.003249E-031.944463E-031.884284E-031.819706E-031.749801-E031.678062-031.605052E-031.526667E-031.430647E-031.299842E-031.108557E-038.306924E-044.582886E-04

-3.127286E-07-5.739613E-04-1.406841E-03-2.685741E-03-4.3067902-03-5.665117E-03-6.036144E-03-. 4048152-03-4.905230E-03-6.230457_-03*1.023563E-02-1.588406E-02-2.067441E-02-2229565E-02-2.030270E-02-1.548470E-02

---------- LINMS SKIPPED ----------


Attachment 8SET5MK.ZLS

SetS: El Centro with flingAcceleration Time Histories

FP-MM'=100

deg red100 1.745327778NPTS=

DT =

Thw (sec)0.0000.0100.0200.0300.0400.0500.0600.0700.0800.0900.1000.1100.1200.1300.1400.1500.1600.1700.1800.1900.2000.2100.2200.2300.2400.2500.2600.2700.28002900.3000.3100.3200.3300.3400.3500.3600.3700.3800.3900.4000.4100.420

4000 40.010

FN FP M-M' ( rotate)Fault Normal Fault ParaIleIfling

-0.0026956 0.0018180 -2.970338E-03-0.0026859 0.0032331 -3206522E-03-0.0026741 0.0046518 -3.441244E-03-0.0026602 0.0060633 -3.672659E-03-0.0026439 0.0074701 -3.900901E-03-0.0026255 0.0088678 -4.125471E.03-0.0026045 0.0102091 4.337716E-03-0.0025811 0.0114251 4.525812E-03-0.0025554 0.0125160 4.689940E-03-0.0025272 0.0135885 -4.848401E-03-0.0024970 0.0147773 -5.025095E-03-0.0024650 0.0161536 -5.232580E-03-0.0024315 0.0176736 -5.463516E-03-0.0023974 0.0191830 -5.692041E403-0.0023629 0.0205885 -5.902125E-03-0.0023261 0.0219832 -. 106578E-03-0.0022933 0.0234179 -6.324897E-03-0.0022582 0.0251074 -6.583707E-03-0.0022210 0.0269818 -6.872552E-03-0.0021800 0.0287436 -7.138105E-03-0.0021323 0.0301943 -7.343049E-03-0.0020716 0.0312083 -7.459343E-03-0.0019869 0.0318577 -7.488697E-03-0.0018631 0.0322602 -7.436673E-03-0.0016795 0.0327022 -7.332609E-03-0.0014206 0.0337911 -7.266738E-03-0.0010901 0.0361952 -7.358723E403-0.0007060 0.0404655 -7.721928E-03-0.0002328 0.0482256 -8.256147E-030.0004952 0.0522430 -8.684129E-030.0016827 0.0574921 -8.326171E4030.0032301 0.0617259 -7.537467E4030.0045224 0.0655207 -6.923761E-030.0048251 0.0694387 -7.306004E-030.0041308 0.0730410 -8.615293E-030.0035946 0.0751345 -9.506875E-030.0049291 0.0746148 -8.102398E-030.0089773 0.0721844 -3.693666E-030.0146650 0.0699841 2289701E-030.0194580 0.0698739 7.029015E-030.0210520 0.0714485 8.325381E-030.0190370 0.0726945 6.124633E-030.0142240 0.0723661 1.441765E-03

M-M' with -FN

2.338959E-032.083670E-03I .825706E-03I .5 891E-03I1.306567E-031.045756E-037.921493E-045.579841E-043.43216BE-04I 1=1128E-04

-1.069640E-04-3.7'74762E-04-6.743950E-04-9.700638E-04-1.2481 19OE-03-1.621115E-03-1 .807977E-03-2.1 35920E-03-2A498034E-03-2.844342E-03-3.143237E-03-3.379087E-03-3.575267E-03-3.76708111E-03-4.024639E-03-4A468702E-03-5.21 1645E-03-6.331458E-03-7.797699E-03-9.559523E-03-1 .164044E-02-1 .38952E-02-1.5831 15E-02-1 .680960E-02-1.675138E-02-1 .658686E-02-1 .781083E-02-2.137550E-02-2.659472E-02-3.129577E-02-3.313898E-02-3.137095E-02-2.657405E-02

------LINES SKIZPPED------


Attachment 8SET6EE . LS

Sd.Avg~mh~ FP-EE=123

deg rad123 2.146753167NPTS a

DT'79890.005FN FP E-E (4 rotate) E-E with -FN

Time (sec)0

0.0050.01

0.0150.02

0.0250.03

0.0350.04

0.0450.05

0.0550.06

0.0650.07

0.0750.08

0.0850.09

0.0950.1

0.1050.11

0.1150.12

0.1250.13

0.1350.14

0.1450.15

0.1550.16

0.1650.17

0.1750.18

0.1850.19

0.1950.2

0.2050.21

Fault Normal Fault Paraflel,fling0.0003884 0.00128470.0003895 0.00128270.0003896 0.00128170.0003919 0.00128170.0003934 0.00128270.0003970 0.00128370.0003998 0.00128670.0004050 0.00128980.0004096 0.00129380.0004167 0.00129990.0004235 0.00130690.0004334 0.00131500.0004437 0.00132410.0004581 0.00133420.0004740 0.00134530.0004956 0.00135850.0005207 0.00137160.0005538 0.00138670.0005933 0.00140190.0006440 0.00141800.0007050 0.00143520.0007813 0.00145240.0008729 0.00146960.0009853 0.00148670.0011182 0.00150490.0012779 0.00152210.0014645 0.00153820.0016841 0.00155340.0019361 0.00156750.0022257 0.00157960.0025523 0.00158970.0029217 0.00159680.0033316 0.00159980.0037835 0.00159780.0042749 0.00159280.0048091 0.00158070.0053765 0.00156450.0059700 0.00154030.0065813 0.00150890.0072144 0.00146850.0078687 0.00141910.0085457 0.00136050.0092267 0.0012908

-3739331E-04 -1.025480E-034.719440E-04 -1.025269E-03-712932E04 -1.024820E-03-3.693475E-04 -1.026765E-03-3.687067E-04 -1.028506E-03-3.661705E-04 -1.032143E-03-3.654808E-04 -1.036133E-03-3.627616E-04 -1.042153E-03-3.61179SE-04 -1.048135E-03-3.585003E-04 -1.057416E-03-3.566563E-04 -1.066961 E-03-3.527290E-04 -1.079689E-03-3.490079E-04 -1.093312E-03-3.424822E04 -1.110839E-03-3.351730E-04 -1.130250E-03-3.242340E 04 -1.155492E-03-3.102925E-04 -1.183735E-03-2.908005E-04 -1.219730E-03-2.65974SE-4 -1.261058E-03-2.321965E-04 -1.312439E-03-1.904477E204 -1.372891E-03-1.357498E-04 -1.446291E-03-6.632082E-05 -1.532423E-031.664476E-05 -1.636092E-031.181775E404 -1.757428E-032A27620E-04 -1.900715E-033.904567E-04 -L066012E-035.663777E-04 -2.258436E-037.700218E-04 -2.477482E-031.006300E-03 -2.726962E-031.274709E-M -3.006373E-031.580664E-03 -3.3200292-031.922785E-03 -3.665451E-032.302881E-03 -4.043347E-032.717755E-03 -4.4527192-033.172374E-03 -4.94137E-033.657038E03 -5.361198E-034.167991E-03 -5.845747E-034.697724E-03 -6.341374E-035.250690E-03 46.850334E-035.826387E-03 -7.372123E-036A26073E-M -7.907999E2037.035164E-03 -8.441178E-03

------ LnM~S SKIZPPED------


Attachment 8SET6LL . iS

SoM &rgapAhe~nmHoiti

FP-LLi41

deg rad91 1.588248278NPTS =

DT r79890.005

FN

4

FP L-L'( rotate) L- with -FNTime (sec)

00.0050.01

0.0150.02

0.0250.03

0.0350.04

0.0450.05

0.0550.06

0.0650.07

0.0750.08

0.0850.09

0.0950.1

0.1050.11

0.1150.12

0.1250.13

0.1350.14

0.1450.15

0.1550.16

0.1650.17

0.1750.18

0.1850.19

0.19502

02050.21

Fault Normal Fault Paraflefling0.0003884 0.00128470.0003895 0.00128270.0003896 0.00128170.0003919 0.00128170.0003934 0.00128270.0003970 0.00128370.0003998 0.00128670.0004050 0.00128980.0004096 0.00129380.0004167 0.0012999

0.0004235 0.00130690.0004334 0.00131500.0004437 0.00132410.0004581 0.00133420.0004740 0.00134530.0004956 0.00135850.0005207 0.00137160.0005538 0.00138670.0005933 0.00140190.0006440 0.00141800.0007050 0.00143520.0007813 0.00145240.0008729 0.00146960.0009853 0.00148670.0011182 0.00150490.0012779 0.00152210.0014645 0.00153820.0016841 0.00155340.0019361 0.00156750.0022257 0.00157960.0025523 0.00158970.0029217 0.00159680.0033316 0.00159980.0037835 0.00159780.0042749 0.00159280.0048091 0.00158070.0063765 0.00156450.0059700 0.00154030.0065813 0.00150890.0072144 0.00146850.0078687 0.00141910.0085457 0.00136050.0092267 0.0012908

3.659611E-04 -4.108006E-043.670562E-04 -4.118252E-043.671938E204 -4.119275E-043.695135E-04 -4.142472E-043.709156E-04 -4.156846E-043.745774E-04 -4.193816E-043.M7141E-04 -4222241E-043.824705E-04 -4.274862E-043.869093E-04 -4.320660E-043.939324E-04 -4.393007E-044.005980.E04 -4.462130E-044.103855E-04 4562825E-044.20553E-04 -4.667796E-044.347269E-04 -4.812936E-04454606E-04 -4.974151E-044.717981E-04 -5.192109E-044.967152E-04 -GA45862E-045.295257E-04 -5.779256E-045.686954E-04 -6.176240E-046.191756E804 -6.686682E-046.797967E-04 -7298886E-047.558554E-04 -8.065466E-048.470919E-04 -8f83823E-049.592351E-04 -1.011125E-031.091768E-03 -1.144292E-031251144E-03 -1.304267E-031.37433E-03 -1.491121E-031.656735E-03 -1.710952E-031.908450E-03 -1.963160E-032.197795E-03 -2.252927E-032.524169E-03 -2.579654E2032.893389E-03 -2.949121E-033.303174E-3 -3.359012E-033.755040E-03 -3.810808E-034.246453E-03 -4.302045E-034.780784E-03 -4.835952E-035.348379E-03 -5.402983E-035.942212E-03 -5.995970E-036.553965E-03 -6.606630E.037.187674E-03 -7.238929E-037.842738E-03 -7.892266E-038.520657E-03 -8.568140E2039.202769E-03 -9.247820E203

---------- LINES SKIPPED ----------


Attachment 8SET6MM. ILS

Set6: SaratogaAcceleration Time Hlstories

FP-MM-100

deg rad100 1.745327778NPTS =

DT=79890.005FN FP M-M(O rotate) M-M' with -FN

Time (sec)0

0.0050.01

0.0150.02

0.0250.03

0.0350.04

0.0450.05

0.0550.06

0.0650.07

0.0750.08

0.0850.09

0.0950.1

0.1050.11

0.1150.12

0.1250.13

0.1350.14

0.1450.15

0.1550.16

0.1650.17

0.1750.18

0.1850.19

0.19502

0.2050.21

Fault Normal Fault Parallel,fling0.0003884 0.00128470.0003895 0.00128270.0003896 0.00128170.0003919 0.00128170.0003934 0.00128270.0003970 0.00128370.0003998 0.00128670.0004050 0.00128980.0004096 0.00129380.0004167 0.00129990.0004235 0.00130690.0004334 0.00131500.0004437 0.00132410.0004581 0.00133420.0004740 0.00134530.0004956 0.00135850.00052Q7 0.00137160.0005538 0.00138670.0005933 0.00140190.0006440 0.00141800.0007050 0.00143520.0007813 0.00145240.0008729 0.00146960.0009853 O.W148670.0011182 0.00150490.0012779 0.00152210.0014645 0.00153820.0016841 0.00155340.0019361 0.00156750.0022257 0.00157960.0025523 0.00158970.0029217 0.00159680.0033316 0.00159980.0037835 0.00159780.0042749 0.00159280.0048091 0.00158070.0053765 0.0015645O.0059700 0.00154030.0065813 0.00150890.0072144 0.00146850.0078687 0.00141910.0085457 0.00136050.0092267 0.0012908

1.594514E-04 -6.056262E-041.608461 E-04 -6.063194E-041.611396E-04 -6.062622E-041.634244E-04 -6.085469E-041.646474E-04 -6.101207E-041.680961 E-04 -6.139202E-041.703176E-04 -6.171940E-041.749223E-04 -622851 OE-041.786622E-04 -6.279940E-041.846316E-04 -6.360680E-041.900908E-04 -6.439825E-041.984669E-04 -6.551647E-042.070713E-04 -6.669261E-042.194397E-04 -6.828021E-042.331984E-04 -7.004193E-042.521608E-04 -7.239415E-042.746487E-04 -7.509895E-043.045954E-04 -7.861976E-043A08055E-04 -8.276692E-043.879981 E-04 -8.804741E-044.450209E-04 -9.434599E-045.172492E-04 -1.021651E-036.044268E-04 -1.114792E-037.121968E-04 -1 .228525E-038.398914E-04 -1.362533E-039.941837E-04 -1.522789E-031.175143E-03 -1.709360E-031.388776E-03 -1.928255E-031.634492E-03 -2.178882E-031.917588E-03 -2.466186E-032.237472E-03 -2.789579E-032.600033E-03 -3.154594E-033.003179E-03 -3.558793E-033.448565E-03 -4.003477E-033.933376E-03 -4.486535E-034.461565E-03 -5.010515E-035.023152E-03 -5.566489E-035.61 1844E-03 -6.146763E-036.219294E-03 -6.743339E-036.849792E-03 -7.359806E-037.502745E-03 -7.995572E-038.179633E-03 -8.6521 15E-038.862388E-03 -9.310668E-03

---------- LINES IPPED ----------


Attachment 8E8SET1N. TNP

ZEsZTIU.dat*tl8Z .pr7,9625,0 .005,5,0. 03,1. 01t63,113.6)setlZRprn7,9625,0.005,5.0.04,l.0(t63,Ilel.6)setlZR.prn7,9625,0.005,S,0.05,1.0(t63,1*13.6)satIZ .prn7,625,0.00.5,0. 06,1.0(t63,1213.6)setlZZ.prn7,3625,0 .005,0. 07,1.0(t63,113 .9).tlB .pr=

7,625,0. 005,5, 0.0,1.0t63,1.13 .6)otlS3.prn

7,3625,0.005.5,0.03,1.0Ct63,1613.6)astRi .p.r7,3629,0.005,5,0.10,L.0(t63,1013.6)setln.prn7,3625,0. 00,5,0 .11,1.0Wt63,1*13.6)etIi .prn

7,3625,0.005,5,0.12,1.0(t63,1013.6)estl] .pr=7,625,0. 005,5,0. 13,1.0(t63,1*13.6)*etum.prn7,625,0. 005,0. 14,1. 0(t63,1213.6)setl=Z.prn7,9625,0.005,5,0.15,1.0(t63,1*13.6)sotlR .prn7,9625,0.005,5,0.16,1.0(t63,1.13.6)wetlZZ.prn7,3625.0.005,5,0.17,1.0(t63. 113 .6)s*t1Z.prn7,625,0.005,5,0.16,1.0(t63,1e13.6)*etllZ.prn7,9625,0 .005,5,0. 19,1.0Ct63,1s13.6)setl]Z.prn7,625,0 .005,5,0. 2,1.0(t63,1023.6)etl=. prn

7,3625,0.005,S,0.25,1.0(t63,1013.6)setfln.pra7,3625,0 .00,5,0 .32,1.0(t63, 113 6)vstIn .prn7, 625,0.003,,. 0.4.1.0(t63,1013.6)aetl=.prn7,3625,0.005,5,0. 5,1.0(ts3,113.6)GtlB3pr1

7,625,0.005,5,0.9,1.0(t63,113.6)setuZZ.prn7,625,0.005,5,0.7,1.0(t63,1.13.6)*e .prm7,3625,0.005,5,0.6.1.0(t63,1013.6)

:1 dawnslope din.


Attachment 8EESET1P *Imp

*e.stlp.dateet"mpy7,925. 0.005o5,0.03,1.0(t04,8*13.6)metlmZ.prn7,3625.0.005,5,0.04,1.0

048,1*13.6)*otlOz.prn7,621,0.005e,s0.052..0(t48,1*13 6)uetlR .pn7,3625,0.005,,0. 06,1.0(04S,1*13.4)mstl .pr=7,9625.0.005,3,0.07.1.0

Mt4S,1*13.6)utoO1Z.p=n7,925.0.005,5,0.08,1.0(t48,1*13. 6)satIlZ.prn7,625,0.005,5,0.09.1.0(043,1*13. )oetlzz.prn7,3625,.0005..0.10.1.0(t4g.1*13.6)astl=prn7,9625,0.005,5,0.l1.1.0(tis,1.1 .6)otil= .p=7,3625.0.005.5.0.12.1.0(t4S,1.132.)*etl=.pz7,9625,0.005.5.0.13.1.0(048.1.13.6)aetlz .px7,962s,0.05,5,0.14, 1.0(t48,113.6)sotllZ.psn7,362S,0.005,5,0.15,1.0(t48,113 .6)setlZ .prn7,625,0.005,5,0.16,1.0(048, 1613.6)sutUE.prn7,3625.0.00e,5,0.17,1.0(048,1.13O6)

setin .pz7,625. 0.005,5,0.18,1.0(048,1*13 6)sati .prn7,62.0. 005,5,0 .19,1.0(048,1.13.6).t2lZ .pr

7,9625,0.005,5,0.2,1.0(048,1.13.6)sotiZn.prn7,925, 0.005,5,0.25.1.0(048,1*13 6)metliE .p7,3625,0.005,5,0.32.1.0(048,1.13.6)smtilz .prn7,3625,0. 0035,0.4,1.0(t048,113.6)Betin .pm7,3625,0.005.5,0.5,1.0(t4,1 13 .6)sotlE .prn7,3625,0.005,5,0.0,1.0(t48,113 .6)ootlz.prn7,3625.0.00s,5,0.7.1.0(048,1*13.6)sati .p=7,3625,0.005,5.0.8,1.0(t48,1.13.6)

*l.0 downalop dis.


Attachment 8EESET2N. XNP

UZRZ2n .datset2Z .prn7,7200,0.005.5,0.03.1.0(t63,1013.6)ast2lB.prn7,7200,0.005,5.0.04,2.0U63,1e13.6)

Gst2ZZ.pr7,7200,0. 005,5, 0.05,1.0(t63,1e13.6)s*t2ZZ.prn7,7200,0 .005,5,0 .06,1.0(t63,1613.6)a$t2ZZ.prn7,7200,0.005,5,0.07,1.0(t63,113.6)a*t2ZZ prn7,7200,0.005,5,0.08,1.0(t63,1613.6)s*t2ZZ.prn7,7200,0.005,5,0.09,1.0(t63,1013.S)set22 .prn7,7200,0.0055,0 .10,1.0(t63.1e1.6)sat2.prn7,7200,0. 005,5,0 .11,1. 0(t63,113.6)set2Z .prn7,7200,0.005,5,0.12,1.0(t63,1*13.6)set23Z.prn7,7200,0 .005,5,0 .13,1. 0(t63,1*13.6)sot2Z .prn7,7200,0.005,5.0.14,1.0(t63,1*13.6)set2n.xprn7,7200,0.005,5,0.15,1.0(t63,1.13 6)*st2ZZ.prn7,7900,0.00I,5,0.16,1.0(t63,1*13.6)*et23 .prn7,7200,0.005.5.0.17,1.0(t63,1.13.6)set21.prn7,7200,0.00S,5,00.1,1.0(t63,1.13.6)set2K3.prn7,7200,0.005,50.19.,1.0(t63,1e13.9)sat2R.prn7,7200,0. 005,5,0 .2,1.0(t63,1*13.6)set21 .prn7,7200,0.005,5,0.25,1.0(t63,113 .6)not2ZZ .pr7,7200,0 005,5,0 .32,1. 0(t63,1e13.6)set23 .prn7,7200,0. 005,5,0.4,1.0(t63,1e13.6)set2U.prn7,7200,0 .005,5,0 .5,1.0(t63,1e13.6)ast233.pz7,7200,0.005,5,0.6,1.0(t63.1613.6)et2ZR.prn

7,7200,0 .005,5,0 .7,1.0(t63,1013.9)set2n3.prn7,7200,0 0055,0. 8,1.0(t63,1.13.6)

sl &mmlop* dim.


Attachment 8SESET2P .ZNP

*eset2p.dataet2ZZ .pz7,9000,0.005,5.0.03,1.0(t48,1.13.6)set2ZZ.prn7,5000,0.005,5,0.04,1.0(t4S,1.13.6)Bst2Z .pra7,8000,0.005,5,0.05,1.0(t43,1613.6)set2ZZ.prn7, 000,0.005,5.0.06.1.0(t48,1013.6)et2Z .prn

7.8000,0.003,5,0.07,1.0(t48,1213.6)ast2ZZ.pru7, 8000,0 005,,0.08,1.0(t48,1213.6)ast2Zz.prn7,8000,0 .00,5,0 .09,1.0(t48,1*13.6)st2Zz.prn7,00, 0.005, ,50.10,1.0(t48.1.13.6)met2Z.prn7,8000,0.005,5,0. 11, 1.0(t41,1*13. )sgt2z .prn7,8000,0.005,5,0.12,1.0(t48,1e13.6)sst2Z .prn7,8000,0. 00,5,0 .13,1.0(t48, 113 .6)at2ZZ prn7,8000,0. 005,5,0 .14,1.0(t4,1013 .6)et2Z.prn7,8000,0.00S,5,0.15,1.0(t48,1*13.6)wst2RZ.prn7,8000,0.0035,,0.16,1.0ft4g,1*13.6)set21 .prn7,8000,0.005,5,0.17,1.0(t48,1*13.6)ast2SE.prn7,9000,0.005s5,0.18,1.0(t4S,113 .6)set2ZE.prn

7.8000,0.005,5,0.-1,1.0(t48,1*13.6)st2zZ.prn7,8000,0. 005,5,0 .2,1.0

t448,I3.6)set2RE.prn7,8000,0.005,5,0.25,2.0(t4S,1e13.6)sst2Zz.prn7, 000,0.005, 5,0 .32,1.0Mt4S,1613.6)set2n1.prn7,8000,0.005, ,0.4,1.0(t48,1e13.6)sot2ZZ.prn7,5000,0.005,S,.o.,L.0(t48,113.6)sbt2ZZ .prn7,8000,0.005,3,0.6,1.0(t48,1213.6)set2ZZ prn7,8000,0.005,5,0.7,1.0(t4S,1e13.6)get2ZZ.prn7,8000,0.005.5.0.8,1.0Ct48,1213.6)

sl donmalops dis


Attachment 8EESET3N. INTP

asset3n.datsft3ZZ.prn7,4391,0. 005,5,0. 03,1.0Mt63,1S13.6)set3Z .prn7,4331,0 005,5,0. 04,1.0(t63,1a13.6)et313.prn

7,4391,0.00,53,0.05,1.0(t63,1*13.6)set3ZE.y=7,4331,0.005,5.0.06.1.0(t63,1e1136)set33 .prn7,4391,0.005.5,0.07,1.0(t63,11.3.9)st3ZZ.pr=7.431,0. 005,5,0.06,1.0(t63,1*13.6)ast3ZE4,rn7,4331,0.005,5,0.09,1.0(t63,1.13.6)set3ZZ.prn7,4331,0.005,5,0.10,1.0(563,1.13.6)ast3ES.p=7,4391,0.005,5,0.11,1.0(t63,1.13.6)ast3Zz.prn7,4391,0.005.5,0.12,1.0(t63,1.13.')ast3ZZ.prn7,4331,0.005,5,0.13,1.0(563,1.13.6)ast333.prn7,4391,0. 005,5,0. 14,1.0(t63,113.6)ast3Z .prn7,4331,0.005,5,0. 15,1. 0(t63,1.13.6)met3Z3.prn7,4331.0.005,5,0.16.1.0(t63,1e13.6)ast3Zz.prn7.4391,0 .005,5.0 .17,1 .0(t63,1*13.6)wst3RZ .prn7,4391,0.005,5,0.18,1.0(t63,1*13.6)et3Z3.prn

7,4331,0.005.3.0.13,1.0(t63,1.13.6)ast3zz.prn7,4391,0.003,5.0.2,1.0(t63,1123.6)set333.p=n7,4391,0.005,5,0.25,1.0(t63,1.13.6)ast3ZE.prn7,4331,0.005.5,0.32,1.0(t63,1213.6)set331.prn7,4391,0. 00,5,0 .4,1.0(t63,1.13.6)met3Zn.prn7,4391,0.005,5,0 .5,1.0(563,1.13.6)set3Z .prn7,4391,0 005,5,0. 6,1. 0(563,1.13.6)met3Bs prn7,4391,0.005,5,0 .7,1.0(t63,1.13.6)set3z .pr=7,4391,0.005,5,0. ,1.0(t63,1*13.6)

l downslop. dis.


Attachment 8ERSET3P . P

*sset3p .datES.31Z.prn7,4331.0.005,5,0.03,1.0(t48,2*13.4)not3Zz.prn7,431,0. 005,5,0. 04,1.0(t48,1*13 .)set3R .prn7,4331,0.005,,0.03,1.0(44,1e13 .t)set3n2.ps=7,4331.0.0035,0.04, 1.0(t48,8113.6)set3ZB.prn7,431,0.0055,,0.07,1.0(t48,1e13.6)set31D.prn7.4331,0.005, 5,0.08,1.0(t48,3113.6)set3 Z..prn7,4331,0.005,3,0.03,1.0(t48,113 .S)w*t31.p=n7,4331u0.005,5,0.10,1.0(M48.1.13.4)not3fl.pn7,4331,0.005,5,0.11,1.0(t4.,1*13.6)et33.prn

7,4391,0 .005,5,0 .2, .0(448,1.13 .)*.t3n2 .pzn

7,4391.0.005,5,0.13,1.0(448.1.13.6)

set3nR .pz=7,4331,0.005,5,0.14,1.0(t48,1*23.6)a.t3nRpr7,431,0.005, 50.15, 1.0(t#8,1*13.4)met3n2.pm7,4331,0.005,5,0.16,1.0(t44,le3.4)s*t3R .prm7,4331,0.005,5,0.17,1.0(t48,2e13.6)set3R.ppm7,4391,0.005,5,0.1.12.0(M44,1213.6)set3ZR.p=7,4391,0.005,5,0.13,1.0(tUS,1.13.9)set32n.pm7,4331.0.005,5,0.2,1.0(t48,1.13.4)*.t3n.pmx7,4331,0.005,5,0.23,1.0(t48,1*13.C)set3n p=7,4391,0.005,5,0 .32, .0(48,U113 *6)

*.t3U .prn7,431,0 .005,5,0 .4, .0(448,1*13 .)et31 pzm

7,4391,0.005, 5,0. 51.0(448,1.13.S)

set3l .pmn7.4331,0.005,5,0.4,1.0(M44,1*13.S)set3nRp=7,4331,0.005,5,0.7,1.0(t48,1.13.6)set3n1.pr7,4331..000, 5,0.8,1.0(448,1.13X.)

*l downulope die


Attachment 8ESETTSN. INP

sast5n dataetszz.prn7,4000,0 .01,3,0. 03,1. 0(t63,fl3.6)setSZZ.prn7,4000,0.01, ,0.04.1.0(t63,fl3.6)astSl .prn

7,4000,0.01,S,0.05,1.0(t63fl3 .6)*ets5Z.prn

7,4000,0.01.5,0.06,1.0(t63,fl3 .6)3.tSSZ.prn7,4000,0.01,5,0.07,1.0(t63,f13.6)at33Z .prn7,4000,0.01,5,0.08.1.0(t63,f13.6)sat533.p=7,4000,0.01,3,0.09,1.0(t63,f3.6)set5ZE.prn7,4000,0.01,5,0.10.1.0(t63,f13.6)set53R.prn7,4000,0 01,5,0. 11,1. 0(t63,fl3.6)

otSRR .prn7,4000,0.01,5,0.12,1.0(t63,fl3.6)setsfEpzrn7,4000,0.01,5,0.13,1.0(t63,fl3.6)set513.prn7,4000,0.01,5,0.14,1.0(t63,t13.6)atszz.prn7,4000,0 .01,5,0. 15,1.0(t63,f13.6)sat53n.prn7,4000,0.01,5,0.16,1.0(863,813.6)ot53Z .prn7,4000,0.01,5,0.17,1.0(863,13 .6)aet5n.prn7,4000,0.01,5,0.13,1.0(t63,f13.6)Not5Z.prn7,4000.0.01.5,0.19,1.0(t63,fl3.6).t5Zn .p=n

7,4000,0.01,5,0.2,1.0(t63,fl3.6)set5ZZ.prn7,4000,0.01,5,0.23,1.0(t63,f13.6)s.t5Z.prn7,4000,0 .01,5,0 .32,1.0(t63,fl3.6)sotSZz.prn7,4000,0. 01,5,0 .4,1.0(t63,fl3.6)tSB2 .prn

7,4000,0 .01,5,0 .5,1.0(863,13M.6)

.1 donalops din.


Attachment 8EESET5P . XNP

esetiP datstBX .p=7,4000,0.01,5,0.03.1.0(t4l,fl3.6)astSU.pri7,4000.0.01,5,0.04,1.0(t4,fl3 .6)t5szz .prn

7.4000.0.01,5,0.03.1.0(t48,913.t)at5sz .p=7,4000.0.01,s,0.06,1.0(t4g,fl3.6)atSet .pr7,4000.0.01,5.0.07,1.0(t4gZl3.6)sat5ZZ.prn7.4000,0.01.5,0.00,1.0(t4g,fl3.6)st5SZ .prn7,4000,0.01.5,0.09,1.0(t48,fl3.9)setSZ.prn7,40000.01,5, 0.10,1.0(t48,fl3 .)stSZZ .pru7,4000,0 01,5,0. 11,1.0(48,f13 .s)setsR .pr7,4000.0.01,5,0.12,1.0(t4,fl3 .6)

t5z .prn7,4000,0.01,5,0.13,1.0(tis,£12.6)et5s .prn

7,4000,0.01,5,0.14,1.0(t48,fl3 .6)

et55ZR.pr7.4000,0.01,5,0.15,1.0(t48,fl3 .6)

et5sZZ .prn7,4000,0.01,5,0.16,1.0

4S,M£13 .6)aetSfl.pzn7,4000,0. 01,5,0. 17,1.0(t4B,fl3.6)et5S .prn7,4000,0.01,5,0.18,1.0(t48,fl3 .6)s*t5i .pr7,4000,0 .01,5,0 .19,1. 0(t48,fl3 .6)sft5sz.pzM7,4000,0.01,5,0.2,1.0(t48,fl3 .6)

setSZZ.prn7,4000,0. 01,5, 0.25,1.0(t48,fl3 6)set5s.prn7,4000,0.01,5,0.32,1.05t48,fl3 )

tSsR .prn7,4000,0.01,5,0.4,1.0(t48,£3.6)stSe .prn7,4000,0.01,5,0.5,1.0548, 13 .6)

il downslepe dis.


Attachment 8ZESBET6N. ZP

*eset6n.datsetgZs.pr7,7989,0. 00,5,0 .03,1.0(t63,913.6)*tCzS .p=7,769,0. 005,S,0 04,1 .0(t63,fl3 .6)pet61 .prn7,7989,0. 005,5,0 0S,1.0

3t62,fll.6)wet6B3.prn7,7398,0 .005,5,0 06,1.0(t63,f13.6)set6z.prn7,7363,0.003,5,0.07,1.0(tW3,fl3.6)s*t6Z .prn7,7383,0.005,5,0.08,1.0(t63,fl3.6)ast6ES.prn7,73990. 005,5,0.03.1.0(t62,f13.6)not6RZ.prn7,7396,0.005,5,0.10,1.0Mt63,413.6)a.t63.prn7,7983,0 .005,3,0 .11,1.0t63,f13.6)

t6nZ .pra7,7383,0.005,5,0.L2,1.0(to3,f 1.6)sst63 .prn7,7383,0.005,5,0.13,1.0(t63,fl3 .6)not633.prn7,79839,0 005,5,0. 14,1. 0(t63,f 1.6)set6nZ.prn7,799,0 .005,5,0. 15,1. 0(t63,f13.6)sotEZ.prn7,739,0. 005,5,0. 16,1. 0(t63,f 1.6)et6Z.prn7,7383,0.005,5,0.17,1.0(t63,f 1.6)not63R.pr7,798,0 .005,3,0. 1,1 .0(t63,913.6)set63z.prn7,7938,0.005,5,0.13,1.0(t63,fl3 .6)get6ZB.prn7,7989,0.00S,S,0.2,1.0(t63,fl3 .6)set6nR.pz7,7339,0.005,5,0.25,1.0(t6,f2 M.6)swtnf.pn7,7963,0.005,5,0.32,1.0(t63,fl3.6)aet633.pr7,733,0. 005,,0 .4,1.0(t63,fl3.6)set633.pr7,739,0. 00,5, 0.5,1.0(t63,413.6)

sl don dlope dLs.


Attachment 8zzSBT6P . InP

*aset6p.dats.t61M.py7,7989,0.00S,5,0.03,1.0(tIt!f13.6)ast6l .prn7,7983,0.005,5,0.04,1.0(t8,f3 .6)*.t6BzB.pr7,7389.0.005,5,0.03.1.0Mt48,fU3.6)Not62.p=7,719,0. 00,5,0 006,1.0(tiW,413 6)sst6Kz.prn7,7989,0.005,5,0.07,1.0Wt4Sl3. 6)

aet6Zz.prn7,7989,0.00s,5,0.08,1.0(t48,L13.6)not633.prn7,7389,0.005,5,0.09,1.0(t48,f3 .6)ast6l .prn

7,7989.0.005,5,0.10,1.0Wt48,f3t.6)s*t6Kz.p=n7,7389,0.005,5,0.11,1.0(t48, 13 6)set6BZ .pm7,798990.003,5,0.12,1.0(t4SM13.6)set68E.prn7,7919,0.005,5,0.13,. 0(t48,fl3 .6)

set6Ml .pm7,7919,0 .005,5,0 .14,1.0(t4,13 C.6)ot631 .prn

7,799,0. 005,5,0. 15,1. 0(18, 13 .6).t6Z .prn7,7989,0.005,5,0.16,1.0(48,413.6)

se616 .prsn7,7989,0.005,5,0.17,1.0(14S,M13.6)ast62 .prn7,7989,0 00,,0 .18,1. 0(148,1M3.6)set6ZE.prn7,7989,0.005,5,0.13,1.0(t48,f13.6)sat6lK .prn7.7989,0.005,5,0.2,1.0(1484,8316)s*t631.prn7.799,0. 005,5,0 .25,1.0(t48,fl3.6)set6Zz.pm7,7989,0.005,5.0.32,1.0(t48,f13.6)aOtSR.prn7,7989,0 .005,5,0 .4,1.0(t48,fl3 .)set6zz.pzn7,7919.0.003,5,0.5,1.0(148,13 .6)

si dolm.cpe dis.


Attachment 8LLSET1N. NP

LLSZTln.dat*tlLL .pr7, 625,0. 005,5,0. 03,1.0(tW3,1613.6)satlLL.prn7,9625,0 005,5,0 .04,1.0(t6l,113.6)*ut1LL pzn7,9625,0.005,S,0.05,1.0(t$3,1e13.6)aot1LL.prn7,3sS,G. 00o5,50.06,l.0Ct63,1e13.6)tlLL.prn

7, 625,0.005,5,0.07,1.0Mt63,1*13 6)*ntILL .pr7.625.0.005,5,0.08,1.0(t63,113 .6)*.t1LL.prn7,9625,0.005,5,0.09,1.0(tC3,1313.6)mot1LL.prn7,3625,0.005,5,0.10,2.0(t63,1.13 6)metlLL.prn7, 625,0.005,5,0.11,1.0(t63,1013.6)atlLL .prin7,9625,0.005,5,0.12,1.0(t63,1.13.6)*stILL pr7,62,0.005.5,0 . 13,1.0(t63,1*13.6)stlLL .p

7,9625,0 .005,5,0. 14,1.0(t6,1.13 .6)nstILL .prn

7,3625,0.005,5,0.15,1.0(t63,1013.6)setlLL .pr7,3623,0.005,5,0.16 1.0(t63,1.13.6)

tlLL .pr7.3625,0.005,5,0.17,1.0(tC3,1.13 6)istiLL .rn7,9625,0.005,S,0.1S,1.0(t63,113 .6)*st1LL.prn7,625,0. 005,5,0. 1,1.0(t63,1.13.6)matILL.prn7,9625.0.005,5,0.2,1.0(W63,1.13.6)matiLL .prn7.3625,0.005,s,0.25,1.0(t63,113 .6)otlLL pr

7.3625,.005,5,0.32.1.0(t63,1213.6)astILL .prn7,3625..0005,5,0.4,1.0(t63,1*13.6)soU LL p=n7, 620. 005,5,0.5.,1.0(t63,1.13 6)*atlLL.pr7,3625.0.005,5,0.6,1.0(t63,1s13.6)-stILL pmn7,3625,0.005,5,0.7,1.0(t63,1*13.6)totlLL.prn7, 625,0.005,5,0., 1.0ft63,1*13.6)

*I downlope die.


Attachment 8LLSET1P . XNP

Lsitip .datsot1LL.prn7,9625,0.005.,0 .03,1.0Mt48,l.13.6)setlLL.prn7,9625.0.00S,5,0.04,1.0t48i,1i13 .6)

saetlLL.prn7.9625.0.005.,30.0,1.0(t48,1*13 .6)motiLL.prn7,9625,.0 005,5,0.06.1.0(t48,113 .6)notiLL .prn7,9625.0.005,5,0.07,1.0(t4,1.13 .6)*etILL.prn7,625.0.005,5,0.08.1.0Mt4,8,13.6)oetlLL prn7.9625.0.005.,,0.09,1.0(t48,1*13.6)notXLL .pn7.962,0. 005,5,0 .10.1.0(t4S,113.6)satILL .pr7,962.0. 005,5,0 .11,1. 0(tMB,1.13 .6)motlLL.prn7,9S25,0.005,5,0.12,1.0(tMS,1*13.6)ostILL .prn7,9625,0.005,5,0.13.1.0(t4MS,113 .6)satiLL .prn7,9625,0. 005.3,0 .14.1. 0(t4g.1*13.6)stILL .prn7,9623,0.005,5,0.15,1.0

t4S,1.13 .6)stlLL .prn7.9625.0.005.5,0.16,1.0(t4S,1s13.6)setILL.prn7.9625.0.005,5.0.17.1.0ft4B,1*13.6)sat1LL.prn7,9623,0.005,5,0.18,1.0(tMS,1*13.6)*otILL.prn7,9625.0.005,5,0.19.1.0(tiS,1s13.6)sot=LL.prn7,9625,0. 005,,0 .2,1.0Ctis,1.13.6)sst1LLpzrn7,9623,0.005,5.0.25.1.0(tiS,1613.6)set=LL.prn7,3625,0.005,0,0.32,1.0W8i,1 13.6)

mat1LL.prn7,9625.0.003,5,0.4,1.0(t48,1*13.6)stLL .prn

7,3625,0.005,5,0.5,1.0(t4S,1.13.6)sotlLLprn7,9625,0.003,5,0.6,1.0(t4S,1.13.6)otILL .prn

7,9625,0.005,5,0.7,1.0(t48,1.13 .6)stlLL .prn7,9625,0.005,5,0.8,1.0(tUS,1613.6)

sl.0 downslep. 4di.


Attachment 8LLSET2N. XNP

L8JM1T2n.dat*t2LL.prn7.7200,0.005,5,0. 03,1.0(t63,1.13.6)sit2LL.prn7.7200,0.005,5,0.04,1.0(t63,1613.6)not2LL .prn7,7200,0.005,5,0.05,1.0(t63,1el3 6)sst2LL.prn7,7200,0.005,5,0.06.1.0(t53,1013.6)bet2LL.prn7,7200,0. 005,,0.07,1. 0(t63,1013.6)sst2LL .p=7,7200,0.005,5,0.06,1.0(t63,1.13.6)st2LL .prn

7,7200,0.005,5,0.09,2.0Mt63,1613.6)*t2LL.p=7,7200.0.005.,50.10,1.0(t63,1.13.6)*et2LL.prn7,7200,0. 00,5,0 .11,1.0(t63,1013.6)*st2L .prn7,7200,0.005,5,0.12,1.0(t63,113 .6)set2LL .prn7,7200,0.0055.,0.13,1.0(t63,1.13.6)set2LL.prn7,7200,0. 005,50 .14,1.0(t63, 113.6)set2LL.prn7,7200,0.005.,5,0.15,1.0Ct63,113 .6)s$t2LL.prn7,7200,0.005.5,0.16,1.0(t63,1.13.6)not2LL.prn7,7200,0.005,5,0.17,1.0(563,1.13 6)met2LL .prn7,7200,0.005,5,0.16,1.0(t63,1.13.6)*st2L .prn7,7200,0.005,5,0.19,1.0(t63,113 .6)a*t2LL.prn7,7200,0.005.5,0.2,1.0(t63,1.13 6)set2LL.prn7,7200,0.005.5,0.25,1.0(W63,1.13.6)*.t2LL .prn7,7200,0.005,5,0.32,1.0(563,1*13.6)set2LL.prn7,7200,0.005,5,0.4,1.0(t63,1.13.6)met2LL .prn7,7200,0 .005,5,0. 5,1.0(t63,1*13.6)st2LL prn7,7200,0.005,5,0.6,1.0(t63,1.13.6)not2LL.prn7,7200,0.005,5,0.7,1.0(t63,1.13.6)sot2LL.prn7,7200,0.005,5,0.6,1.0(WS3,1s13.6)

31 downslope dis.


Attachment 8LLSET2P. . IP

LLost2p.dataUt2LL.prn

7,000,0 005,5,0 031. 0(548,1.13 .6)*ot2LL.prn7,000,0. .05,5,0 04,1.0(t48,1.13.6)*ot2LL .prn7,6000,0 .005,5,0 .s,s1.0(M48,1.13.6)*et2LL.prn7,8000,0.005,5,0.06,1.0(54S,1.13 6)met2LL.prn7,8000,0. 005,5,0 .07,1.0(548,1.13.6)*ot2LL.pr7,6000,0.005,5,0.08,1.0(t54,1.13.6)st2LL prn7,6000,0.005,5,0.09,1.0(548,1.13.6)bot2LL.prn7,6000,0.005,5,0.10,1.0(t48,1.13.6)*ot2LL.prn7,$000,0 .005,5,0. 11,1.0(546,1613.6)set2LL.prn7,6000.0.005,5,0.12,1.0(t48,1e13 6)set2LL.prn7,8000,0. 005,0. 13,1. 0(t4S,1.13.6)sat2LL.prn7,t000,0.005,5,0.14,1.0(t48,1.13.6)*ot2LL4prn7, 000,0.005,5,0.15,1.0(ti4,1.13.6)set2LL.prn7,6000,0.005,5,0.16,1.0(548, 13 .6)met2LL.prn7.000,0.005,5,0.17,1.0(548,1.13.6)ast2LL prn7,6000,0.005,5s,0.16,1.0(t58,1s13.6)oot2LL.prn7,S000,0.005.5,0.1S,1.0(t4s,1.13C6)ast2LL.prn7,8000,0. 005,5,0 .2,1. 0(t48,1.13 6)set2LL prn7,8000,0.000.5,,0.2,1.0(t48,1*13.6)m.t2LL.prn7,6000,0.005,5,0.32,1.0(t48,1e13.6)ast2LL.prn7,6000,0 .005,5,0 .4,1.0(t48,113.6)ast2LL.prn7,6000,0. 005,5,0 .5,1.0(t48,1.13.6)set2LL.pr=7,6000,0.005,5,0.6,1.0(t5S,113 .6)xot2LL prn7,6000,0. 005,5,0 .7,1.0(548,1.13.9)s.t2LL.prn7,6000,0. 005,5,0 .,1.0(t48,1613.6)

I1 dowslops dig


Attacbment 8LLSET3N. INP

LLast3n .dat*St3LL.prn7,4391,.005,5,0 .03,1.0(t63,1613.9)set3LL.pr=7,4391,0.005,5,0.04,1.0(t63,1.13.6)set3LL.Vrp7,4391,0.005,5,0.05,1.0(t63,1e13.6)ast3LL.pr7,4391,0.005, 30.06,1.0(t63,1e13.6)ast3LL.pr7,4391,0.005,5,0.07,1.0(t63,1e13.t)ast3LL.prn7,431,o0.005,5,0.0S,1.o(M63,1*13.6)not3LL.prn7,4391,0.005,3,0.09,1.0(t63,1.13.6)*et3LL.prn7,4391,0 005,5,0 10,1. 04t63,1a13.6)met3LL.prn7,4391,0.005,5,0.11,1.0(t63,1*13.6)met3LL.prn7,4391,0.005,5,0.12,1.0(t63,1013.6)set3LL .prn7,4391,0.005,5,0.13,1.0(t63,1*13.6)ast3LL .pr7,4391,0 .005,5,0. 14,1. 0(t63,1e13 .6)set3LL.prn7,4391,0.005,5,0.15,1.0(t63,1&13.6)set3LL.prn7,4391,0.005,3,0.16,1.0Mt63,113 .6)ast3LL.prn7,4391,0.005,5,0.17,1.0(t63,1.13.6)set3LL.prn7,4391,0.003,5,0.1S,1.0(t63,1.13.6)set3LL .pn7,4391,0.005,5,0.19,1.0Mt63,1*13.6)set3LL.prn7,4391,0.005,5,0.2,1.0(t63,113 .6)set3LL .pr7,439.10.005,5,0.23,1.0(t63,1*13 .6)set3LL.prn7,4391,0.005,5,0.32,1.0(t63,1*13. 6)not3LL .pr7,4391,0.005,5,0.4,1.0(t63,1*13.6)net3LL.prn7,4391,0 .005,,0. ,1. 0(t63,113 .6)set3LL .prn7,439S,0. O5,5, .6,1.0(t63,1613.6)*t3LL.prn7,4391,0.005,5,0 .7,1. 0Mt63,1.13.6)set3LL.prn7.4391,0.005,5.0.8,1.0(t63,1213.6)

s1 downslop. din.

of 52GEO.DCPP.01 30, Rev. 3

Attachment 8LLSET3P . 3I:P

LLst3p .dat*.t3LL .py7,43914,0.005,,0.03,1.0(t48,1.13.6).t3LL.prn

7,4391,0.005,,.0.04,1.0(tI4,113 .6)*et3LL .prn7.4391,0.005,s,0.05, 1.0Mt48,1413.6)et3LL .prn

7,4391,0 005,5,0. 06,1.0(t48,1.13 6)t3LL .prn

7,4391,0.005,5,0.07,1.0Mt48,1*13.6)met3LL.pra7,4391,0. 005, 5.0 .0,1.0(t4S,1123.6)t3LL.prn

7,4391,0.00o,5,0.09,1.0(t4, 113 .6)ast3LL .pr7,4391,0.005,,0.10, 1.0Mt1, 1.13.6)st3LL.pr7,4391,0 .005,3,0 .11,1.0Mt48,1*13.6)set3LL .pru7,432910.005,5,0.12,1.0(tU8,1613 6)et3LL=.pe

7,4391,0.005,5,0.13,1.0(t4B,1.13.6)set3LL .pr7.439l,0.005,5,0.14,1.0(t49,1213.6).st3LL.prn7,4391,0.005,5,0.15,1.0t3, 1.13. 6)

met3LL .prn7,4391,0.005,5,0.16,1.0(t48,1*13.6)sst3LL.prn7,4391,0.005,5,0.17,1.0(tM9,1613.6)set3LL.prn7,4391,0.005,5,0.1S,1.0(ti ,1.13. 6)set3LL.prn7,43291,0005,1,0.13,1.0Mt48,1613.6)

&*t3LL.prn7,4391,0.003,5,0.2,1.0t48,113 .6)

*st3LL.pr7,34291,0.0055,0.25,1.0(t48,1e13 .6)set3LL.prn7,4391,0.005,5,0.32.1.0(t43,1123.6)ast3LL.prn7,4391.0.005,5,0.4,1.0(t48,113 .6)ast3LL.prn7,4391,0.005,5,0. 5,1.0(t48,1.13.6)set3LL.prn7,4391,0.005,5,0.6,1.0(t41,1*13.6)set3LL.prn7,3291,0.005,5.0.7,1.0(t48,1*13.6)setLL.prn7,3291,0.005, 5,0.8,.0ft48,1*13.6)

e1 dow.slops dis


Attachment 8LLSETSN. INP

LLutSt datGSt5LL.prn7,4000,0 01,5,0 03,1 .0(t63,f13.6)*.tSLL.prn7,4000.0.01,5,0.04,1.0(t63.£13 .6)*otSLL .prn7,4000,0 .015,0 .0,1. 0(t63,fl3.6)setSLL.pSD7,4000,0 1,5,0. 06,1.0(t63,£13.6)setSLL.prn7,4000,0.01,1.0.07,1.0Ct63,f13.6)metSLL.prn7,4000,0 .01,5,0. 0,1.0(t63, 13.6)s*tSLL.prn7,4000,0.01,5,0.09,1.0(t63,fl3.6)UstSLL.pra7,4000,0 .01,5,0.10,1.0(t63.fl3 .6)not5LL.pra7,4000,0 .01,5,0. 11,1.0(t63,fl3.6)setSLL .pr7,4000,0. 01,5,0. 12,1.0(t63.f13.6)sat5LL.prn7,4000,0 .01,5,0. 13,1. 0(t63.£3.6)etSSLL.prn

7,4000,0.01.5,0.14,1.0(t6O.M3.f)sotSLL.prn7,4000,0 .01,5,0. 1,1.0(t63,13 .6)oetSLL.pru7,4000, 0. 01,5,0. 16,1.0(tU3.13.6)r-tSLL .prn7,4000,0.01,5,0.17,1.0(t6M3.13.6)setSLL.prn7,4000,0. 01,5,0. 1g,1.0(t63.£3 .6)sot5LL.prn7,4000,0. 01,5,0. 19,10(t63f13 .6)sat5LL.prn7,4000,0 .01,,0 .2,1.0(tM3.13 .6)stSLL .prn7.4000,0.01.5,0.25,1.0(t63.l3 .6)uetSLL.p=n7,4000,0. 01,5,0. 32,1.0(t3.£13M.6)setSLL.prn7,4000,0 0.1,,0.4,1.0(tC3,fl3.C)sotSLL.pr=7,4000,0. 01,5,0. 5,1. 0(t63,f13.6)

*1 dovnslope dis.

of 52GEODCPP.O1.30, Rev. 3

Attachment 8

LLSETSP . 1IP

LLUse5t.dat 1 downslops dis.

sst5LL.p=a7,4000,0 .01,5,0 .03,1.0(t43,£13.6)*otSLL .prn7,4000,0 01,5,0. 04,1.0(t4,£13 .6)*ot5LL .prn7,4000,0.01,5,0.05,1.0(t8,f13 .6)et5LL.prn7,4000,0. 01,5,0 .06,1.0It48,tl3.6)oetSLL .pn7.,4000,0.01,5,0.07,1.0t48,913 .6)stSLL prn7,4000,0.01,5,0 .08,1.0(t48,f13.6)setSLL.p=n7,4000,0.01,5,0.09,1.0(t48,f13.6)ast5LL.prn7,4000,0 .01,5,0 .10,1.0t48,f13.9)

sotSLL.Vpn7,4000,0.01,5,0.1, 1.0Ct48,fw3.g)sot5LL.prn7,4000,0 01,5,0 .12,1.0Mt48,f3 .6)ootSLL.pr7,4000,0.01,5,0.13,1.0Mt84,f13.6)

uet5LL.prn7,4000,0.01,5,0.14,1.0(t4g,£13.6)set5LL.prn7,4000,0.01,5.0.15,1.0Mt8,13 .6)sotSLL.prn7,4000,0.01,5,0.16,1.0(t48,fl3.6)xut5LL.prn7,4000,0.01,5,0.17,1.04t48,£13 .6)n*t5LL.prn7,4000,0.01,5,0.18,1.0Mt48,913.6)..t5LL.prn7,4000,0.01,5,0.19,1.0(t48,fl3.6)setSLL.prn7,4000,0 .01,5,0 .2,1.0t48, 13.6)

set5LL.prn7,4000,0 01,5,0 .25,1.0(tS, 13 .6)setSLL .prn7,4000,0.01,5,0.32,1.0t48, £13.6)

oetSLL .prn7,4000,0. 01,5,0. 4,1.0

Mt48,413.6)uetSLL.prn7,4000,0.01,5,0.5,1.0(t48,fl3.6)


Attachment 8LLSET6N. XNP

LLUstgn.datset6LL.prV7.7333,0.005,.0.003,1.0Mt63,f13.6)sIt6LL.prn7.7333,0.00,5,50.04,1.0Mt63,13 .6)met6LL.prn7,7933,0.005,5,0.5, 1.0(t63,fl3 .6)SMt6LL.prn7.7933,0.005,5,0.06.1.0(t63, l3 .6)Ot6LL.pm

7.7333,0.005,0.07.01.0(t63.613.6)set6LL.pru7,7383,0.005,5,0.08,1.0(t63,f13.6).t6LL.prn

7,7333,0.005,5,0.03,1.0Mt6SSl3 .6)set6LL.pr7,739,30.005,5,0.10,1.0(t63,f .. 6)Ot6LL.pr

7,7339,0.005,5,0.11,1.0Ct63,13f.6)sst6LL.prn7.733, 0.005, 5.0. 12,1.0(t63,f13.6)etSLL .prn

7,7383,0.005, 5,0 .231. 0(t63,f23.6)st6LL.py7,7333,0.005,5,0.14,1.0(t63,f13.6)*et6LL.prn7,7333,0.005,5,0.15,1.0(t63,£3. 6)^*t6LL .pr7,73S3,0.005,,0. 16,1.0(M62,613.6)sot6LL.prn7,7989,0.005,5,0.17,1.0(t63,fl3.6)set6LL.prn7,7333,0.005,5,0.18,1.0ft",M13.6)set6LL.pmr7,7333.0.005,5,0.13,1.0Mt63f13t.6)ast6LL.prn7,733,0 .005,S,0.2,1.0(t63,13S.6)*t6LL .p7,7333,0.005.5,0.2S,1.0("t3,fl3.6)sot6LL.p=7,7333,0.005.5,0.32,1.0(363,13 .)set6LL.p=a7.73,0 .005. 5,0.4.1.0(363,M13.6)

Wt6LL.pzs7, 733,0.005,5,0., 1.0(M63,413.t)

sl downslopo dis.


Attachment 8LLSET6P.* IP

LLUt6g dat*et6LL.pzn7,7989,0.005,5,0.03,1.0(t49,f1S.6)set6LL.p=7.7089,0.005, 5,.004,.0(t4l,fl3.6)sot6LL.prn7,7389,0.005,s,0.05,e.0(t(S,fl3.6)set6LL .pr7,7399,0.005,5,0.06,1.0(t4S,fl3.6)ast6LL.prD7,7989,0.005,5,0.07,1.0(t48,fl3.6)sot6LL.prn7,7989,0.005,5,0.0S,1.0(t4g,f12.6)ast6LL .prn7,7989,0.005,5,0.09,1.0(t48,fl3 .6)set6LL.prn7,79s9,0.005,5,0.10,1.0(t48,fl3.6)set6LL.pm7,7389,0.005,3,0.11,2.0(t4S,fl3.6).Ut6LL.pm7,7389,0.005,5,0.12,1.0(t4M,813.6)sgt6LL.prn7,7389,0.005,5,0.13,1.0(t48,f13.6)*et6LL .prn7,733, 0.005,5,0.14,1.0(t48,fl3.6)set6LL.pru7,7989,0.005,5,0.15,1.0(t48,M.S)b*t6LL.pr27,7989,0.005,5,0.6, 1.0(t4S,fl3.6)x*t6LL .prn7,7989,0.005,5,0.17,1.0(t4,fl3 .6)st6LL .prn7,7989,0.005,5,0.18,1.0(84S,f 16)set6LL .prn7,7389,0.005,5,0.9, 1.0(t48,f13.6)vlt6LL.prn7,7989,0.005,5,0.2,1.0(t48, 13.6)mot6LL .p=7,7989, 0. 00o,5, 0 .25, 1. 0(t48,fl .6)ast6LL.prn7,7389,0.005,5,0.32,1.0(t48,fl .6)*et6LL.p=

7,7989,0.005,5,0.4,1.0(t48,fl3 .6)*t6LL .pr7,7389,0.005,5,0.5,1.0(t4,fl3 .6)

*1 dowmslope dim.


Attachment 8EES5CL. ZNP

flSUICOO .ST

5, 4000,0.001,5, 0 .03,12..0(Sf10.6)

5SMC00 .QSC5,40000 .01.5,0.04,1.0(Sf1o.6)

U58XC00 .OSC5.4000.0.01,5.0.05.1.0(Sf10.6)n5sxC00 .0SC5,4000,0.01,5.0.06,1.0(Sfl0.6)

n3ZBCOO .QSC5,4000,0.01,5,0.07.1.0

(Sfl0.6)3258XC00 .QOC5,4000,0.01,5,0.09,1.0(Sf10.6)

Zs58=00.osc

5,4000,0 01.5.0.10e . 0(Sfl.6)32533C00 .OSC

5,4000.0.01.5,0.1,1,. 0Sf10o.6)ZZSONCOO .OSC

zzssxcoo.Qsc5.4000,0.01,5,0.12,1.0(Sflo.6)3z53xc00 .oscs,4000,0.01e,50.13.1.0(Sf10.6)9239KC00 .00c5,4000,0 .01, 5, 0.14,1.0(Sf10.6)32s!sCOO .QSC5,4000,0.01,5.0.13,1.0(Sf10.6)xsSXCoo .QsC5,4000,0.01,5,0.16.1.0

ns9xcoo.osc5,4000,0.01,5,0.17,1.0(5110.6)

325CC0200.08Cnssxcoo.QBc5,4000,0.01,5,0.IS,1.0(511o.6)nszcx00.05c5,4000,0.01,5,0.15,1.0(Sf10.6)3sssxcoo.csc5,4000,0.01,5,0.32,1.0(Sf10 .6)

z5Sxc00 .OSC5,4000,0.01,5,0.2,1.0(Sf10.6)

R25gxC00.03c

5,4000,0.01,5,0.32,1.0(Sflo.6)ZZS0c0oo.Qsc5,4000,0.01,5,0.5,1.0(SflO.6)

ZZSSKCOO .0SC5,4000.0.01,S,0.4,.1.0nsoxcoo.asc

5,4000,0.41.5.0.93.1.0(Sf10.6)

5, 4000 .0 .01,5,0.6, 1.0

(Sflo.6)Xzssxcoo.QSC

3Z5S3XC00 .OSC

5,4000,0.01,5,0.2,1.0(5fl.6)3z53xc00 .@Bc

x5,4000,.02,,0S,.(Sf10.6) l~~es~~

o1.0 dowelops dis. fr= T.1.


Attachment 8BERSMC00 .QS

ZxSSCz1Ro 3-K', SZ3 5 3(ONTItSeBsmlc CoeffLcient Surface Eistory

Time Stop - 0.010 SeaSurface 1

0.000001 0.0000050.000106 -0.000009

-0.004573 -0.003520-0.011533 -0.012134-0.018959 -0.0207s8-0.034246 -0.033942-0.031443 -0.028463-0.009792 -0.007851-0.006093 -0.007184-0.036841 -0.043077-o.057971 -0.035313-0.045274 -0.047073-0.042046 -0.039042-0.010936 -0.006539-0.010938 -0.0176c3

0.000014 0.000031-0.000253 -0.000673-0.006473 -0.007435-0.012693 -0.013280-0.022743 -0.024740-0.037343 -0.038240-0.025452 -0.022497-0.006327 -0.005271-0.008817 -0.011248-0.048792 -0.053601-0.052131 -0.045881-0.048740 -0.043780-0.035830 -0.032577-0.003112 -0.000896-0.026037 -0.03s596

0.000055-0 .001250-0 .008372-0.013971-0.024720-0. 038433-0.013677-0.004715-0.014864-0. 057213-0.044033-0o 04877-0e 02891-0. 000033-0.045737

0.000087 0.000119-0.001364 -0.002776-0.003271 -0.010111-0.014842 -0.013953-0.026355 -0.030349-0.037796 -0.036328-0.016e34 -0.014438-0.004606 -0.004851-0.013113 -0.024487-0.05e437 -0.060266-0.044200 -0.043470-0.048e71 -0.047203-0.025013 -0.020574-0.000545 -0.002467-0.055732 -0o0 0650

0.000136-0 .003653-0. 010870-0. 017331-0. 032419-0. 034144-0.012017-0. 005355-0. 030311-0. 05714-0.043315-0.044813-0.015772-0.00oes8-0. 073773

... . .. ZB SM"XI

-0. 0031580 .0011210.0167330.005756

-0 016224-0. 010630. 0064760. 0110320.008714

-0.007173-0.0134030.0004430. 0081600. 003822

-0 *00186

-0. 0037360. 0013420.0038330. 002603

-0.000732

-0.0079670.0045860. 0164920.003057

-0. 017516-0 0016670. 0077730.0111400.007470

-0 .00241-0 .0123690.0022770.0073640.003130

-0.002645-0.0031420.0023e30.0033100.002142

-0.000845

-0.0075370.0074170.0158580.000122

-0.018163-0. 006260

0 008780.0112030.005931

-0. 011031-0 0110130.0033120. 007830. 002552

-0. 003312-0.002422

0. 0027370.0033400.001648

-0. 000844

-0.0068390.0101140.014832

-0 .00269-0 .018185-0.0031160.0095420.0111340.004111

-0.012476-0e 00390

0.0053110. 0070630.001393

-0. 003852-0. 0016230. 0030150.0039080.001244

-0 .000732

-0. 00s330. 0124870.013636

-0 .00610-0.017607-0.0014060.0100790.0110780.002045

-0.013526-0.0075610.0064430. 0064520.001139

-0 004230-0. 000780.0032380. 0038040.000653

-0.000s15

-0.004611 -0.002s6s0.014389 0.0157350.012102 0.010285

-0.009138 -0.011930-0.016507 -0.0149720.000834 0.0030100.010451 0.0107070.010813 0.010357

-0.000204 -0.002556-0.014146 -0.014324-0.005592 -0.0035530.007290 0.0078500.005733 0.0051240.000463 -0.000310

-0.004416 -0.0043940.000005 0.0007460.003424 0.0035840.003620 0.0033550.000133 -0.000137

-0.000213 0.000143

-0.0007050. 01.6040 .00171

-0.014332-0 .0130970.0048840.0108310 .009668

-0.o004n3-0.014068-0 .0015250 .0031330 .004465

-0.001104-0 .0041630.0013360.0037220.003013

-0 . 0005120. 000529


Attachment 8ER5SOCOO .DAT

BZ5sMCOO.DATS-rla of Pemanent defoen-tion from Nemark's methodSlip A.(g). Slip/Amx. Blip D.(0t), A, Scaling V., file

0.03000 0.03203 0.31373+02 0.93665 1.00000 3395MC00.QSC0.04000 0.04271 0.26513+02 0.93665 1.00000 Z3BXSCOO.QSC0.05000 0.05333 0.2312Z+02 0.93965 1.00000 3Z5SXC0O.QSC0.06000 0.06406 0.20413+02 0.93665 1.00000 13S5MCOO.QSC0.07000 0.07473 0.1799Z+02 0.93665 1.00000 53SMICOO.QSC0.08000 0.08541 0.1596Z+02 0.93665 1.00000 WSZMCOO.QSC0.09000 0.09609 0.14253+02 0.93665 1.00000 3SS1C0O.QSC0.10000 0.10676 0.1279Z+02 0.93665 1.00000 ZS3MCO0.QSC0.11000 0.11744 0.115.Z+02 0.93n65 1.00000 USzMICO.QBC0.12000 0.12812 0.10623+02 0.93665 1.00000 5SMCO.QSC0.13000 0.13879 0.97193+01 0.93t65 1.00000 Z35S3COO.QSC0.14000 0.14947 0.88813+01 0.93665 1.00000 1353SC00.QSC0.15000 0.16015 0.80963.01 0.93665 1.00000 3zssxcoo.osc0.16000 0.17012 0.74373+01 0.93665 1.00000 Z9553C00.QSC0.17000 0.18150 0.68613+01 0.93665 1.00000 h3M5SCCO.QSC0.12000 0.19217 0.63471+01 0.93665 1.00000 z35sxCOO.QSC0.19000 0.20285 0.3867Z+01 0.93665 .ooooo Z3SSXCOO.QSC0.20000 0.21353 0.54171+01 0.93665 1.00000 Z5SC0O.QSC0.25000 0.26691 0.37173+01 0.93665 1.ooooo n5smCOo.QSC0.32000 0.34164 0.22563+01 0.93663 1.00000 3 5aCOO.QSC0.40000 0.42705 0.1271Z+01 0.93665 1.ooooo n5SCO.QSC0.45000 0.41044 0.8730z+00 0.93565 1.00000 Z35M(C00.QSC0.50000 0.53382 0.818+3.00 0.93665 1.00000 3Z5ZSCOO.QSC0.60000 0.64058 0.2314z.00 0.93665 1.00000 o 31UsCOO.QSC0.63000 0.67261 0.1710z+00 0.93665 1.00000 3 3zCS0co.QBC0.70000 0.74734 0.81421-01 0.93665 1.00000 XUSMICO.QSC0.80000 0.85411 0.20OZ-01 0.93665 1.00000 n5SBCOO.QSC


Attachment 8ERS6CL . INP

nCSXCO .DIATn6SmCOO .0sC5.7384.0.005.5.0.03,1.0(8110 . 6)n6sxCoo.0sC5.794,0.005,5,s.04.,.0(810 .6)ntsxcoo.osc5.7334.0.005.*0 .05,1.0(3flO.9)16CXCOO .Osc

5.7984.0.003.5.0.06.1.0(8f11.6)n6sxCOO.QSC5,7984,0.005,s,0.07.1.0(3110.6)n6sYCoo.QSC5,7384.0.008.5.0.08.1.0(8flO.6)

U68YCOO.QSC3,7184,0.005,5.0.09.1.0(8flO.6)3z6SxCOO.QSCs,79s4.0.00,5,0.10.,1.0(Sflo.6)6sXCOOc.aSC

5.7334,0.005,5.0.11,1.0(SflO.6)Z6SYCO0.Q9C

5.7384.0.005,3.0.12.1.0(Sf10.6)U6KC004.Q8C,7934.0.005.5.0.1L.L.0

(8flO.6)n6sYCoo.asC5.7384.0.005.5.0.14,1.0(8flO.6)ntsxcoo.osc5,7384.0.005.3.0.15,1.08flO.6)

326sYC00.OSC5,7934,0.005.s,0.16,1.0(810o.6)

36SxCOO.QSC5,7384.0.005,5.0.L7,1.0(3fl.6)n6aXCOO.QsC5,7314,0.005,5,0.18,1.0(8f11.6)

336sxCoo.QsC5,7984,0.00.35,0.13,1.0(8110.6)

zz69xCOO.QSC3.7384 .0005,5.0.2.1.0(8110.6)zsSXC00 .e9C

5.7384,0.005.5.0.25,L.0(Sf1o .)

9l6SXCOO.QSC5,7984.0.00.,5.0.32.1.01fle.6)3963XCOO.QSC5.7384,0.005,5,0.4,L.0(8f10.S)n6sxCoo.QSC5,7384,0.005.5.0.43,1.0(3flO.6)nCSxCO0.QSC5,740.00.ee 5.0 .3.1.0(8fl0.6)Z6SXCOO.QSC5,7384,0.005.5.0 .6. .0(3fl1.6)n26sxC0c.0sC5,7384.0.005.5,0.63,1.0(SflO.6)n6sxCOO.esC5, 73,4 .005,5,0.7,1.0(I110.a)u6sxCOO.asC5,79S4.0.005.5,0.S.1.0(8110.6)

*1.0 dnmmlope die. fx F.R.


Attachment 8ZE6SMCOO .QSC

X36BMCsPROFlLM Z-X', 8ES 5 11TI010Ieismic CoeffLcliit Surface llftory

Sim Step * 0.005 Secsurface 1

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... . ..LZ IX 1MD

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Attachment 81E6BSCOO .DAT

326sMC00 .DATSuary of vermanent deformation from Newmark' methodBlip A. (g), x1ip/Amx, Blip D.(ft), Axt, Scaling F., file

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0.15000 0.1847n 0.47932+01 0.01176 1.00000 zsm69coo.gsc0.16000 0.19710 0.4458U+01 0.31176 1.00000 ZX6SKCOO.QSC0.17000 0.20942 0.41392+01 0.81176 1.00000 X2S6COO.QSC0.13000 0.22174 0.36402+01 0.81176 1.00000 Z6SKMCOO.QSC0.19000 0.23406 0.36032+01 0.61176 1.00000 =6MCO0.QSC0.20000 0.24633 0.3360Z+01 0.81176 1.00000 =6BMC00.08C0.25000 0.30797 0.23194+01 0.81176 1.00000 2261MC00.QSC0.32000 0.32420 0.13702+01 0.81176 1.00000 UESU(COC.QSC0.40000 0.43276 0.75692+00 0.81176 1.00000 Z=62MC0O.0SC0.45000 0.55435 0.50341+00 0.81176 1.00000 ZZ6SMCOO.QSC0.50000 0.61594 0.32182+00 0.81176 1.00000 3261MC0O.QBC0.60000 0.73913 0.10162+00 0.81176 1.00000 226GMCOO.QSC0.63000 0.77609 0.64602-01 0.81176 1.00000 US6XMCOO.Q8C0.70000 0.36232 0.18492-01 0.81176 1.00000 GE6IMCOO.QSC0.60000 0.96551 0.16332-03 0.31176 1.00000 82662C00.QSC


Attachment 8LLS5CL.* IP

1LSXCOO.QSTLL!8Kc00 .QSC.4000 ,0.01. ,0.03.1.0

(9flO-C)LL5SXCOO.oSC5,4000,0 .01, 5,0 .04, 1.0(Sflo.6)LL5SNCOO.OOC1.4000,0 . i, 1,0.03,1.0(oflo.6)LLSBKCOO.OSC5,4000,0.01,1,0.06,1.0(SflO.6)tLSBXCOO.QBC5,4000,0.01,1,0.07,1.0(Sfl.6)LLSBNC0OD.QSC154000,0.01,910.031.0(Sf1o.6)LLSOXCOO.OQC1,4000,0.01,1,0.0.,1.0

LLSKCOO .O9C

514000,0. 01, 1,0.2101.0(Sf10.6)LL5OXCOO.QOSC

5,4000,0 .01,5, 0.11,1.0(Sf10.6)

LL5SBCOO.QSC1,4000,.01e,1~.lS.13.0

(Sf10.6)LL3neo.osLL5OKCOO .QSC

1,4000,0.01,5,0.14,1.0(sf0o.6)

LL53KCOO.O9C5.4000,0.01,1,0.151.0(of0 .6)LL56mCOO.aSC5,4000,0.01.5,0.14.1.0(Sf10.6)LLSSXCOO.QSC5,4000,0.01,3,0.17,1.0(Sf10.6)LLSOKCOO.OSC$14000,0 .01, 1,0.15,1.0(Sf10.6)

LLSSKCOO.QBC5,4000,0.01,1, 0 .13,1.0(f10 .6)LLSXCOO .QSC5,40000.01, 5,0.2,1.0(Sf10.6)LLSXCOO .QSC5,4000,0.01,1,0.25,1.0(Sf10.6)LL5BXCOO .OSC5,4000,0.01,5,0.32,1.0(efl0.9)LLL5SXCOO .QSCS,4000,0.01,3,0.4.1.0(Sf10.C)LLSSXCOO .OSC5,4000,0.01.5,0.43,1.0(If10.6)LL5SXCOO .OSC5,4000.0.01,s,0.42,1.0(Sf10.6)LL5SXCO .QSC5,4000,0.01.5.0.1,1.0(SflO.6)LLSS3COO.QSC1,4000.0.01,.S0.6,1.0(SUf 06)LLSOXCOO.QSC5,4000,0.015, 0.7,1.0(Sf10.6)LLSB=COO.BSC14000,0 .01,1 0.5.1.o(Sfl.6)

,1.0 doqmmlove dig. fm 1.1.


Attachment 8LL5SMCOO .QSC

LL5EKCtfO1L L-L', SZT 5 KOTICOSeismic Coefficient Surface 3istory

Time Step - 0.010 secsurface 1

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-0 .0000050.0000070.0013150.002334

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-0.001149 -0.001844 -0.002S13 -0.003494 -0.004539-0.010411 -0.011832 -0.012892 -0.013432 -0.013368-0.00O0L1 -0.006036 -0.004032 -0.002340 -0.000337-0.001261 -0.002370 -0.005110 -0.007456 -0.003715-0.017207 -0.019080 -0.021300 -0.023923 -0.026182-0.037360 -0.038211 -0.038120 -0.036738 -0.034019-0.010289 -0.002563 0.004800 0.011171 0.016035

0.017373 0.013880 0.003317 0.003878 -0.002222-0.025333 -0.023465 -0.031068 -0.030513 -0.0276510.002345 0.012380 0.022668 0.031322 0.0383380.043970 0.033882 0.034228 0.027441 0.023766

................... LXRS SXPPZD

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-0.005071 -0.005233 -0.005237 -0.005103 -0.004741 -0.004243-0.002279 -0.001574 -0.000891 -0.000250 0.000336 0.000856

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0.002112 0.002832 0.003474 0.004006 0.004338 0.0046300.004271 0.003822 0.003241 0.002562 0.001820 0.001055

-0.001010 -0.001517 -0.001285 -0.002131 -0.002220 -0.002162-0.001216 -0.000702 -0.000227 0.000481 0.001033 0.001680

0.0305880.008015

-0.0222430.0063020.013133

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0.0326460.001231

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-0.004611-0.0023730.0017000.0030330.000346

-0.0027S10.0013430.004565

-0.000334-0.0016450.002670


Attachment 8LL5SMCOO .DAT

LL5gCcO0.DATxu3uary of t anent deformation from Nwmmark's methodall A.(g), Slip/Auz, slip D.ft). Azz Bealing F., fIl-

0.03000 0.02965 0.4104Z+02 1.01137 1.00000 LLSBMC0O.QSC0.04000 0.03953 0.34312+02 1.01187 1.00000 LL5SMCOO.QSC0.05000 0.04941 0.2937Z.02 1.01187 1.00000 LLSSKCOO.QSC0.06000 0.05930 0.2590Z+02 1.01187 1.00000 LLS5MCOO.QSC0.07000 0.06911 0.2233Z102 1.01187 1.00000 LLS8MCOO.QSC0.08000 0.07906 0.20293.02 1.01187 1.00000 LLSMCOO.QSC0.09000 0.03994 0.1830Z.02 1.01137 1.00000 LL5(COO.QSC0.10000 0.09383 0.16621+02 1.01187 1.00000 LL5SXCOO.QSC0.11000 0.10871 0.15142.02 1.01137 1.00000 LLSSXCOO.QSC0.12000 0.11359 0.13851Z02 1.01137 1.00000 LL5BXCOO.QSC0.13000 0.12348 0.12732.02 1.01187 1.00000 LL58MCOO.QSC0.14000 0.13833 0.11742.02 1.01187 1.00000 LL53XCOO.QSC0.15000 0.14824 0.10341+02 1.01137 1.00000 LLSSKCOO.gSC0.16000 0.15312 0.1003Z+02 1.01187 1.00000 LLSSKC00.QBC0.17000 0.15801 0.92921.01 1.01187 1.00000 LL5SMCOO.QSC0.12000 0.17739 0.3531Z+01 1.01137 1.00000 LLS8MCOO.QSC0.190l 0 0.13777 0.79491.01 1.01137 1.00000 LLSMMCOO.QSC0.20000 0.19765 0.73421.01 1.01187 1.00000 LL39MC00.QSC0.25000 0.24707 0.48591.01 1.01127 1.00000 LLSSXCOO.QSC0.32000 0.31625 0.26403+01 1.01187 1.00000 LL5SMCOO.QSC0.40000 0.32521 0.14743.01 1.01117 1.00000 LLSSKCOO.QSC0.45000 0.44472 0.10201+01 1.01137 1.00000 LLSSMCOO.QSC0.43000 0.47437 0.81591.00 1.01117 1.00000 LL5SMCOO.QSC0.50000 0.49414 0.70113.00 1.01187 1.00000 LLSSMCOO.QSC0.60000 0.59295 0.3053Z100 1.01187 1.00000 LL5SMCOO.QSC0.70000 0.69179 0.1155Z+00 1.01187 1.00000 LL5SMCOO.QSC0.30000 0.79062 0.33931-01 1.01187 1.00000 LLSBXCOO.QSC


Attachment 8LLs6CL.* IP

LLESMCOO.DLTLL6SXcOO.OSCs,7984,0.005,5.0.03,1.0

LSLONCO.QSC5,7984,0.005,5,0.4, 1.0(SM10.6)LL6SXCOO OSC5,7934O.0.05,,0.0.5.1.0

LL6SXCOO .OSC3.7984.0 .005,5,0.06, 1.0(Sf10.6)

LL6SXCOO.OSC5,7934.0.005,5,0.08,1.0(8118.6)LL68XCOO.QSC

(Sf10.6)LL6SXCOO .OSC

£,79S'.,0.005,5,0 .09.1.0(510.6)LL6SNCOO.OSC5,7284,0.005,5,0.1..1.0(Sf0.6)LL6SXCOO.OSC5,7984,0.005,3,0.13,1.0

LL68KCOO.QOC5,79s4.0.00s.5,0.13 1.0

LL6SXCOO .QSC5.7985.0.003.5.0.13,1.0(Sf10.6)LL6SXCOO .OSC5,7984. .00,5,.0.14.1.0(Sf106)LL6SXCOO .QOSC5,7984. .005,5,0.15,1.0(Sfl.6)LL6SXCOO .OSC5, 79540. 0.05, 5.0.214,1.0

N~fleoQLLCSXCOO .QSC5,734,0 .005,s,8.1.1.0(Sf10.6)

LL6SXCOO.QSC

5,7984,0.005, 5,0.13, 1.0(S10.6)LLtSXCOO.OSC5, 794 0 .005 .0 .2 1.0(OflO.6)LL6SXCOO.OSC5,7984,0.005.5,0.2,1.0(f10.6)LL6SXCOO .OSC

5, 793840 .0055,0.4251.0(Sf10.6)

LL6SXCOO .OSC5,7984,0.005.5.0.3,1.0(SflO.6)LL6SXCOO .SC5,7934,0.005.5,0.4,1.0(Sf10.6)LL6SXCOO.OsC5,7984,0.005, 5,0., 1.0

(Sf10.6)LL6SXCOO.QSC5,7284.0.0035,,0.5.1.0SflOO6)

LL6SXCOO .OSC

LL6SXCOO .OSCS75 s4,e.ee550.5 ,|1.0(;fl0.6)

l.0 dfmeuslopo din. 9rcz F.S.


Attachment 8LL6SMCOO .gSC

LLWSMCPROFXZLZ L-L, SZS 6 4XOcNBlesmic Coefftcient Suface Nistozy

Time Step - 0.005 SScSurface 1

0.0000000.0000050.000032

-0.000003-0.000353-0.001549-0.004411-0.009027-0.013208-0.013332-0. 0079920.0000860.0065330.0101400.013839

0.000000 0.000000 0.000001 0.0000010.000007 0.000009 0.000012 0.0000150.000035 0.000037 0.000038 0.000036

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0.000002 0.0000030.000019 0.0000230.000032 0.000024

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0.0000040.0000270.000013

-0.000213-0.001325-0.003942-0.008404-0.012138-0.013626-0.008199-0.0009150.0059130. 0097650.0132720.020271

................... L8N1B SX12ND

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-0.000719-0.001089-0.000873-0.0002670.0003200.0005500.000362


Attachment 8LL6SMCOO .DAT

LL6OKCOO .DTsmary of peruanent deforuation from Newmarkes methodSlip A.(g), Slip/Am, Slip D.Cft), Amx, Scaling F., file

0.03000 0.03419 0.12556102 0.87745 1.00000 LLE2MCOO.OSC0.04000 0.04s55 0.1344Z+02 0.87748 1.00000 LL69COO.QSC0.05000 0.05690 0.1176X+02 0.87748 1.00000 LL6SXCOO.QSC0.06000 0.06838 0.10372+02 0.87748 1.00000 LL68BCOO.QSC0.07000 0.07977 0.92230+01 0.37748 1.00000 LL69KC0o.0SC0.03000 0.09117 0.32023+01 0.87748 1.00000 LL6a(COO.QSC0.09000 0.10257 0.73412+01 0.37743 i.@oooo LL6SMCOO.QSC0.10000 0.11396 0.6775Z+01 0.37743 1.00000 LL6SMCOO.QSC0.11000 0.12536 0.62413.01 0.0774s 1.00000 LL6IMCOO.QSC0.12000 0.13675 0.57355+01 0.87748 1.00000 LL69MCOO.QSC0.13000 0.14815 0.53061+01 0.87743 1.00000 LL62MCOO.QSC0.14000 0.15955 0.49242+01 0.87748 1.00000 LL6SNCOO.QSC0.15000 0.17094 0.45902+01 0.37748 1.00000 LL68MCOO.QSC0.16000 0.18234 0.4294Z+01 0.87748 1.00000 LL6$MCOO.QSC0.17000 0.19374 0.40212.01 0e.774s 1.00000 LL6SMCOO.QSC0.13000 0.20513 0.37642+01 0.87743 1.00000 LLUS C00.03C0.13000 0.21635 0.3529Z+01 0.37748 1.00000 LLtMXcO.QSC0.20000 0.22792 0.3343X+01 0.87743 1.00000 LL63MCOO.QSC0.25000 0.28491 0.25532+01 0.17748 1.00000 LL6SNCOO.QSC0.32000 0.36468 0.1635201 0.37741 1.00000 LL6SNCOO.QSC0.40000 0.45535 0.9174Z+00 0.87741 1.00000 LL62MCOO.QBC0.43000 0.54702 0.4615Z+00 0.87748 1.00000 LL68KCOO.QSC0.s000 0.5S6981 0.39SM320 0.87741 1.00000 LL6SNC0O.QBC0.60000 0.63377 0.1450z+00 0.87748 1.00000 LL6SMCOO.oSC0.70000 0.73773 0.34952-01 0.87748 1.00000 LL6mMC0O.QSC0.30000 0.31170 0.2749Z-02 0.37743 1.00000 LL6SOCOO.QSC


Attachment 8DOWS5 . INP

dC=5 .qsC324000.0.01,5,0.03.1.0Wt12.1flO.6)

dccs5.qsc

(tu2,ltlO.s)dcM5 .qgsc3.40000.01,5e,0.05.1.0Wt12,1f10.6)

(~msi .qtC2,4000,0.01.5,0.06,1.0

dcsS .qsc3,4000.0 .01.,5.0.07. 1.0

dcoS.qsco4000o0.01,e5,e0.081.0MILU.nO.6

dc5S. pcMu2,10.6)dcMa5.qsc

2,4000.0.01,5,0.e0,1.0

(M2,1f10.6)dcS .qvc.4000.0 .01.5,0.10,1.0

(12, f1.0 6)dcs 5.qsc3.4000,0.01.5.0.11.1.0Mt2,19flO.6)

dcMS5.qNc2.4000,*0.01.5.0 2.14.1.0(tl2,lflO.g)dc(nS .qsc3,4000,0.01,5,0.13,1.0(t1.ltlO.6)d(mmS.qsc3,4000,0.01,5,0.14.1.0

M211fno.9)dc(nS .qxc,4000,0 .01.5, 0.1,1.0

(tl2.lflO.6)dciiS .quc2,4000,0.01.5.0.16.2.0(t12,lflO.S)

(t12,1f0.6)dcm5 *.qc,4000,0 .01,5 0.2.1.0

(It2,1920.6)dcm= .qsc3,4000.0.01.5,0.e1,1.0

(tU2,llO.6)dcms .qsc3.4000,0.01,5.0.3,2.0

4t12,Mf 0.*6)

dcenS .qsc2,4000,0.01.5,0.33.1.0(2,1210.6)dc(iS .qsc

,4000,0.01,5, 0.35,1.0(2,1910.6)

acmms3.qsc

3,4000,0.01.5.0.4,1.0(112,1110.6)

dcns5 .qsc,4000.0.8.1,.0.33,1.0(tl2,lC.6)dc(nS .quc3,4000,0.01, 5.0 .4.1. 0

(112,1flo.6)dc3 .qsc

3,4000,0.01,5,0.8.1.0

(12,1210.6)

.1.0 dnlaps d-ie. r~ T.s.


Attachment 8DCMMS5 .QSC

DCO(SsIPROWTLZ K-WI,

Ucismic CoefficientTime-sec Block 1

0.00 o .eooooo0.020 0.0000000.030 0.0000000.040 0.0000000.050 0.0000000.060 0.0000010.070 0.0000060.030 0.0000130.s03 0.0000540.100 0.0001230.110 0.0002230.120 0.0003420.130 0.0004060.140 0.0003520.150 0.0001230.140 -0.0001250.170 -0.0004070.130 -0.0006680.130 -0.0003030.200 -0.001171

ST 5 3MOTIONftrface Kiutoriss

............ . LMZS MPIM

39.31033.32039.83039.84039.85033.86033 .170

33 .88033.83033.30039.31039.32033.J3039.94039.35039.3603 .37039. 8039. *90

40.000

0.0010330.0010620.0010980. 0011500.0012210.00130E0.0014020.0014910.0015640 .00161t0 .0016270. 0016140.0015790.0015330. 0014870.0014510.0014340.0014380.0014620.001497


Attachment 8DCSS5 *.DAT

dcis5.DAs1razy of Wermanait defoaatIan from Nemzark'a cethodSlip &.(g), 11ip/a=x Slip D.(ft). ax, scaling F., file

0.03000 0.03219 0.38451+02 0.33193 1.00000 dcams.qzc0.04000 0.04292 0.3211Z.02 0.93193 1.00000 dc5s.qsz0.0000 0.05365 0.26761.02 0.93193 1.00000 dcmS.qsc0.06000 0.06438 0.22541+02 0.93193 1.00000 tciS.qsc0.07000 0.07511 0.1343Z102 0.93193 1.00000 dc ms.qsc0.08000 0.08354 0.1690Z.02 0.93193 1.00000 dcm zS.qsc0.03000 0.09657 0.14901.02 0.33191 1.00000 d35.qac0.10000 0.10730 0.13231+02 0.33193 1.00000 dSm5.qsc0.11000 0.11803 0.1176Z+02 0.93193 1.00000 dA S.qsc0.12000 0.12877 0.10531+02 0.93123 1.00000 dc S.qsc0.13000 0.13950 0.3457Z+01 0.93193 1.00000 deS5.qsc0.14000 0.15023 0.85452+01 0.33193 1.00000 dnns5.quc0.1000 0.16096 0.7741Z+01 0.93193 1.00000 dcs3.qsc0.16000 0.17169 0.7010Z+01 0.33193 1.00000 dcs5.qsc0.17000 0.18242 0.64311+01 0.93193 1.00000 ds S.qsc0.13000 0.19315 0.3942Z+01 0.93193 1.00000 d sS.qsc0.19000 0.20385 0.14341.01 0.93193 1.00000 d S.qxc0.20000 0.21461 0.49631+01 0.93133 1.00000 6ca .qSc0.25000 0.26826 0.30921.01 0.33193 1.00000 dc S.qac0.30000 0.32191 0.18671+01 0.93193 1.00000 dcs5.qxc0.33000 0.35410 0.13621.01 0.93133 1.00000 dcms.qsc0.35000 0.37557 0.11141.01 0.33133 1.00000 dcinS.qsc0.40000 0.42922 0.64452+00 0.33133 1.00000 d0 S.qsc0.30000 0.S3652 0.26743.00 0.93133 1.00000 dciS.qsc0.60000 0.64383 0.9964Z-01 0.93193 1.00000 dciS.qsc0.70000 0.71113 0.2598Z-01 0.93133 1.00000 dc 3S.quc0.80000 0.58544 0.49532-02 0.93193 1.00000 dczS.qsc


Attachment 8DCMINS6 . NP

dcms6 .DTdcmug.qsc3,7384,0.085,5.0.03.1.0(t2.lflO.6)dcx6 .qsc3.7384,0.005 .,0.04.1.0(t12,1f10.6)dcs6 .qc3,734.0.005,5,0.05,1.0(t%2,lflO.f)dcm6.qsc3,7984.0.0051o.0.09,1.0t2.12.0.6)

dcms6.qsc3,7334,0.0055.0,.07.1.0(t12,1f10.6)dcms .qsc1.7984.4.00s.5,0.03.1.0'tl2,1flO.6)dc6 .qsc3.7934,0.005.5.0.09,1.0(tl2,Lf1O.6)dc 6.qsc3.734,0.005 ,5,0.10,1.0(tl2,Ifne.Sdc=6 .qsc3.7334,0.005.5.0.11.1.0(tl2.1f10.S)ins6.qsc

3.734.e0.00s5,30.12.1.0(tl2.1flO.6)dcms6.qsc3,7984.0.005,5,0.13,1.0(tl2.tfl1.6)dc=6.qgc3.7384,0.005,5.0.14,1.0

Wt12,1910.6)dc6m .qsc3,7384.0.003,5,0.15.1.0Ct22,1flO.6)dms6.qsc3,7n34,0.005.e.0.16,1.0(tl2.1flO.6)

dcMM .qsc3,12S4.9.005,S.C.17,1.0(tili.fle.6)dcm6 .qsc3.734 ,0.005.,50. 1,1.0Mt12,110 .6)

dcms .qsc3,7334,0.005.5.0.13,1.0(t12,1110.6)

dcmm .qsc3.7384,0.005.5.0.2,1.0Mt12,1f10.6)

dcmx .qsc3.7384,0.005 .,0.25,1.0(t12,1fl0.6)dcm 6.qsc3.7934,0.00,5,.0.3,1.0

Etll,1t10.6)dc 6 .qsc3,7984,0.005.5,0.35,1.0ftl2,lfl*.S)dc46 .qsc

3, 7334,0 .005.3.00.45.1.0Mt2.1910.6)dCMu6.qac

3,7384,0.005e.S04,1.0

Mt2,ltlO.6)dms6 .qsc3,7384,0.0054A.S..0(t2l,1no0.9)dcms6.qsc3,7334.,0.05,5,0.7,1.0(tl2,111O.6)d6ig.qxc

(tl2.lflo.g)dcM6 .qsC3,7134,0.005.5,0.1,1.0(t12,1110.6)

31.0 ddnslcpe dis. *rz F.t.


Attacbment 8DClMS6.QSC

DMO=6 srFILZ K-K, SET 6 K* ONgiumic Coafficient surface zistoriosTim-coc Block 1

0.005 0.0000000.010 0.00ooo0

0.025 0.0000000.030 0.0000000.035 0.0000co0.040 0.0000000.045 0.0000e 0

0.055 0.0000000 . 060 0.0000000.065 0.0000000.070 -0.000010.075 -0.0000040.010 -0a0000100.015 -. 0000o240.09 -0.000049

0.100 0.e000154

................ ....... LDZ m=

39.105 -0.000256

39.911 00025639.615 -0.000255

39.825 -0.00025339.525 -0.00025139.630 .0.00024733.s35 -0.00024239.640 -0.00023639.845 -0.00022939.950 -0.00022239.655 -0.00021439.6 -. 020539.665 -0.00019739.870 -0.00011139.875 -0.00017939.810 -0.00017139.815 -0.00016239.890 -0.00015539.895 -0.00014739.900 -0.00014139.305 -0.00013539.910 -0.00013039.915 -0.00012639.920 -0.000123


Attacbment 8DCM C6 .DAT

dss6. DATSumay of eramaaent deformation frbm 7ewmark's methodSlip A (g) lpBIWax. Blip D.(ft). Am, scaling F., file

0.03000 0.03393 0. l11.+02 0.8239 1.00000 dcmms6.qsc0.04000 0.04S30 0.1415Z+02 0.88298 1.00000 dcmms6.qsc0.05000 0.05663 0.12573,02 0.88298 1.00000 dcumas.qsc0.06000 0.06735 0.11212i02 0.88298 1.00000 dkmnS.qsc0.07000 0.07928 0.10033+02 0.88298 1.00000 dckmga.qsc0.08000 0.0060 0.8933Z+01 0.88298 1.00000 dca6.gsc0.09000 0.10193 0.80773.01 0.18298 1.00000 dl6C .qsc0.10000 0.11325 0.72693.01 0.88298 1.00000 dzmmsS.qxc0.11000 0.12458 0.65171+01 0.88231 1.00000 dcimsg qsc0.12000 0.13590 0.8333,01 0.88298 1.00000 dla6.qsc0.13000 0.14723 0.3335Z+01 0.18298 1.00000 dmmns6.qxc0.14000 0.15855 0.49452+01 0.88298 1.00000 d-mC6.qsc0.15000 0.16988 0.4600Z+01 0.88238 1.00000 d-m-C6.qsc0.16000 0.18120 0.42823+01 0.88298 1.00000 dc ms6.qsc0.17000 0.13253 0.40042+01 0.88298 1.00000 dcsC6.qsc0.l8000 0.20386 0.37512+01 0.88298 1.00000 dcmmz6.qsc0.19000 0.21518 0.3515Z+01 0.8u298 1.00000 da6.qs c0.20000 0.22651 0.3292Z+01 0.88298 1.00000 dcms6.qsc0.25000 0.28313 0.24033+01 0.88298 1.00000 dc9s6.qqc0.30000 0.33976 0.17992.01 0.18298 1.00000 dcmas6.qsc0.33000 0.37373 0.15012+01 0.88298 1.00000 dkmsg.qsc0.3S000 0.33639 0.13271+01 0.88298 1.00000 dckmJ6.qsc0.40000 0.45301 0.95463+00 0.88238 1.00000 dixms6.qzc0.50000 0.56626 0.46125+00 0.88298 1.00000 dcmms6.qxc0.60000 0.67952 0.24231+00 0.88298 1.00000 dAm6.qsc0.70000 0.79277 0.98562-01 0.88298 1.00000 d==s6.qsc0.80000 0.90602 0.15923-01 0.88298 1.00000 dzmms6.qsc

ATTACHMENT

7-2


PACIFIC GAS AND ELECTRIC COMPANY

GEOSCIENCES DEPARTMENT

CALCULATION DOCUMENT

Calculation Number: 29

Calculation Revision: 3

Calculation Date: 03/17/2003

ITR Verification Method: A

1.0 CALCULATION TITLE:

DETERMINATION OF SEISMIC COEFFICIENT TIME HISTORIES FOR

POTENTIAL SLIDING MASSES ALONG DCPP ISFSI TRANSPORT ROUTE

2.0 SIGNITURES

Printed Name

VERIFIED BY: __ .____ Scu

Printed Name

APPROVED BY: 411Ai

Printed r~ame

DATE

Organization

DATE 3 47/

Organization

DATE -

Organization

'T qh/olo)I

of 39GEO.DCPP.01.29. Rev. 3

3.0 RECORD OF REVISIONS

Rev. RevisionReason for Revision

No. Date

0 Initial Issue 11/21/01

Revised to address comments from 6/4/2002 NQS Assessment Report01339023.

I Removed superseded figures from attachments. 06/25/02Added new attachments (e.g. list and excerpts of input and output files).Numerous editorial changes.Replaced CD containing revised README file. Edited page 12 of

2 calculation to show revised CD label. Edited page 72 show only 12r20/02input/output files and executable on CD.

1. Add analyses for a new section M-M' along the transport route.2. Re-calculate seismic coefficient using updated version of

QUAD4MU (replaced average acceleration method used in revisionI and 2) for cross sections L-L', M-M' and E-E'.

3 3. Attachments 1 through 9 are copied from GEOJDCPP.01.29, revision 03/17/031, no changes were made in these Attachments.

4. Attachment 10 is new for this revision which includes excerpts offiles used for the seismic coefficient calculations for sections L-L',M-M' and E-E'.

I

I

I

of 39GEODCPP.01.29. Rev. 3

4.0 PURPOSE

The purpose of this calculation package is to provide the seismic responses and seismic

coefficient time histories for potential sliding masses along DCPP ISFSI transport route.

The calculations reported in this package were performed in accordance with the

requirements of Geomatrix Consultants, Inc. Work Plan, Revision 2 (dated December 8,

2000), entitled "Laboratory Testing of Soil and Rock Samples, Slope Stability Analyses,

and Excavation Design for Diablo Canyon Power Plant Independent Spent Fuel Storage

Installation Site" for sections L-L', E-E' and D-D' along the transporter route as identified

in in calculation package GEO.DCPP.01.21 and GEO.DCPP.01.28, revision 3 (section M-

M').

In response to PG&E AR A0574914, the analysis of a fourth section (Section M-M')

representing the northern end of the transporter route was made. In addition, all cross

sections were re-analyzed using the boundary force approach to calculate the

corresponding seismic coefficient time histories of the sliding masses.

These analyses included two-dimensional finite element analyses of the representative

sections along the transport route. Dynamic analyses were performed at these sections for

two purposes: (a) to estimate earthquake-induced seismic coefficients within the profiles

for evaluating the stability of typical slopes along the transport route at the full level of

ISFSI design ground motions; and (b) to estimate rock-to-soil amplification of ground

motions at full and reduced levels of ground motion.

5.0 ASSUMPTION

1. All sections were analyzed using two-dimensional cross sections. It is considered

as a reasonable approximation for the DCPP site.

2. The response of a potential slide mass during the strong shaking can be reasonably

represented by the seismic coefficient time history computed by dividing the

I


summation of the boundary forces time histories acting on the block by the

corresponding mass of the slide.

6.0 INPUTS

1. Plan and three cross sections along the transport route (Sections D-D', E-E', L-L', and

M-M') from calculation package GEO.DCPP.01.21.

2. Plan and cross sections M-M' along north end of transport route from calculation

package GEODCPP.01.21, and .GEO.DCPP.01.28, revision 3.

3. Five sets of rock motions originating on the Hosgri fault: Transmittal from PG&E

Geosciences dated September 28, 2001 (Attachment 2).

4. Azimuths of three cross-sections along transporter route: Transmittal from PG&E

Geosciences, dated November 12, 2001 (Attachment 1).

5. Orientation (azimuth) of the strike of the Hosgri fault: Transmittal from William Lettis

& Associates dated August 23, 2001 (Attachment 4, as confirmed in Attachment 7).

6. Direction of positive fault parallel component on Hosgri fault (Attachment 6).

7. Rotated motions from Sets 5 and 6, from calculation package GEODCPP.01.30.

8. Reduced peak bedrock acceleration of 0.15g: Transmittal from PG&E Geosciences

dated May 28, 2002 (Attachment 9).

9. Rock properties for dynamic analyses (Attachment 8).

Selection of Sections for Dynamic Finite Element Analyses

Four cross sections along the transport route (Sections D-D', E-E', L-L' and M-M') were

considered (see calculation package GEO.DCPP.01.21, and GEO.DCPP.01.28, revision 3).

These are the powerblock section (section L-L'), the warehouse section (section D-D'),

and the parking lot section (section E-E'). The north end of transporter route (section M-

M') represents the typical section along the transport route that overlies bedrock. Analysis

for this section was performed to address concerns raised by NRC reviewers regarding

potential sliding of bed rock masses along clay beds. The powerblock section L-L'

represents the typical slope profile above power block units 1 and 2. This section also has

a thick colluvium deposit on the slope, and was selected for the dynamic analyses to

estimate the seismic amplification effects along the colluvium slope. The parking lot

I


section E-E', between elevation 180 feet and 220 feet, is generally similar to the profile in

the vicinity of the transport route at section D-D' (the warehouse section). Section E-E'

also has a thicker colluvium deposit than that at section D-D', and was selected for the

dynamic analyses. It is estimated that seismic amplification effects at section E-E' would

be higher than those at section D-D'.

Dynamic Properties for Finite Element Analyses

Properties required for the dynamic finite element analyses include the unit weight,

Poisson's ratio, shear modulus at low shear strain, G., and relationships describing the

modulus reduction and damping ratio increase, with increasing shear strains.

Unit weights

Unit weights of rock mass were based on field investigations for the ISPSI site as reported

in Attachment 6. The unit weights for the colluvium fan underlying the slope above Unit 2

(sections LL' and M-M'), and the marine terrace deposit underlying the colluvium at

sections D-D' and E-E', are reported in calculation package GEODCPP.01.28, revision 3.

These unit weights, along with associated shear strengths, are presented in Table 1.

Shear Wave Velocity and Shear Modulus at Low Strain

Shear modulus values at low strain (G,,) can be measured in the laboratory using resonant

column tests, obtained from field shear wave velocity measurements, or estimated using

published correlations with other properties, such as shear strength. When available,

estimates of G. based on field shear-wave velocity measurements are preferable to

laboratory test data. The shear modulus at low strain is related to the shear wave velocity

by the following relationship:

G = L(V,g

where: G. = shear modulus at low strain

y = unit weight of material

g = acceleration due to gravity

V5 = shear wave velocity

I


Results of shear wave velocity measurements performed in rock at the power block area

are presented in Attachment 8, from the Long Term Seismic Program report and related

responses to questions from the NRC. Based on the results of these investigations, a shear-

wave velocity distribution with depth, along with associated Poisson's ratios, was selected

for use in the dynamic analyses, and is shown in Table 2. These shear wave velocity values

are also indicated on the finite element representations for sections L-L', M-M' and E-E'

in Figures 1, 2 and 3 , respectively. The shear wave velocity in the upper 15 feet was

conservatively reduced from the value of 2600 fps listed in Attachment 8, to a value of

2000 fps based on judgment. Shear wave velocities for the Pleistocene colluvium were

estimated based on published correlations between G. and shear strength (Egan and

Ebeling, 1985) and the above relationship between G,. and Vs. For shear strength of

3000 psf, G. varies between 1500 and 2200 ksf (Figure 3 of Egan and Ebeling), and Vs

varies between 1130 and 1350 fps, averaging about 1200 fps. Velocities for the

Pleistocene marine terrace sands and gravels were estimated from Seed and Idirss (1970)

for sand and Seed et al. (1986) for well-graded gravel. For dense sand and gravel, the K2 .,.,

was estimated as 70 to 120, so that the average shear wave velocity for the Pleistocene

marine terrace sands and gravels was chosen as 1200 fps. Values of Poisson's ratios for the

Pleistocene soils are commonly used for soils under unsaturated condition.

Modulus Reduction and Damping Relationships with Strain

In the iterative equivalent-linear procedure used in QUAD4MU, relationships of the

variation of modulus reduction factor and damping ratio with shear strain are used to select

strain-compatible shear moduli and damping ratios for each element. The variation of shear

modulus reduction factor and damping ratio with shear strain for rock in the vicinity of the

power block area was estimated on the basis of cyclic triaxial and resonant column tests

performed on rock cores in 1978. The data are presented on Figures 4 and 5, from

Attachment 6, for the modulus reduction factor and damping ratio, respectively. The

modulus reduction curve shown on Figure 4 (identified as rock curve from the manual of

the program SHAKE) was selected for the current analysis, and roughly corresponds to the

middle of the range obtained from tests on the DCPP rock cores shown on Figure 5

(reported in the LTSP 1989 report). For the variation of damping ratio with shear strain,

I


the curve defining the lower bound of the shaded zone for the DCPP rock, was selected for

use in the current analysis. Modulus and damping curves for the Pleistocene colluvium and

marine terrace deposits were based on relationships for similar soils published in the

literature. These relationships are also listed in Table 2.

7.0 METHOD AND EQUATION SUMMARY

Earthquake-induced seismic coefficient time histories (and their peak values km,,) for

potential sliding masses within the selected profiles were computed using the two-

dimensional dynamic finite element analysis program QUAD4MU (the updated version of

QUAD4M, Hudson and others, 1994). This is a time-step analysis that incorporates a

Rayleigh damping approach, and allows the use of different damping ratios in different

elements. The program QUAD4M and the updated version QUAD4MU were verified in

calculation package GEO.DCPP.01.34, revision 3 and revision 4, respectively. The

seismic response parts of the two programs are identical. However, the seismic coefficient

calculation function used in QUAD4MU was based on summation of forces acting on the

boundaries defining potential slide masses in the finite element mesh as detailed in its user

manual. This calculation approach is consistent with that requested by NRC reviewer and

the option in QUAD4MU was specifically verified in GEO.DCPP.01.34, revision 4.

The program uses equivalent linear strain-dependent modulus and damping properties and

an iterative procedure to estimate the non-linear strain-dependent soil and rock properties.

Selection of Input Motions

Geosciences department of PG&E developed five sets of possible earthquake rock motions

for the ISFSI site (Attachment 2 as confirmed in Attachment 3) to be used as input to the

analyses. These motions are estimated to originate on the Hosgri fault about 4.5 km west of

the plant site. Both fault normal and fault parallel components were determined for each of

the five sets of motions. The fault parallel component incorporated the fling effect and its

positive direction was specified in the southeasterly fault direction (see Attachment 5, as

confirmed in Attachment 6). The fault normal component has a direction normal to the

fault, and its polarity can be either positive or negative depending on the assumed location

of the initiation of the rupture. Based on Attachments 1 and 4 (as confirmed in Attachment

I


7), the direction of movement along cross section L-L' (which as shown in Figure 5 has an

azimuth of 67 degrees) is 91 degrees (counter-clock wise) from the direction of the strike

of the Hosgri fault. The fault normal component can be at + 90 degrees from fault parallel

direction, that is 91+90 = 181 (or 91-90 = 1) degrees from the direction of section L-L'.

From these relations, the ground motion component along section L-L' can be determined

from the specified components along the fault normal and fault parallel directions. Similar

computations are made for section M-M' and E-E'. Section M-M' is about 100 degrees

(counter-clock wise) from the direction of the strike of the Hosgri fault. Section E-E' has

an azimuth of 35 degrees, and thus is 123 degrees (counter clock wise) from the direction

of the positive fault parallel component of the Hosgri fault. The computed motion along

the directions of sections L-L', M-M' and E-E' will be referred to as the rotated

components.

The rotated component along each of the specified section is the sum of the projections of

the fault normal and fault parallel components along the direction of the section (Figure 6).

The formulation is as follows:

Rot+ = F, cos(O) + FN sin(o)

andRot = Fp cos(4)) - FN sin(¢)

in which the Fp and FN are fault parallel and fault normal components of the acceleration

time-histories, Rot' is the component along the section when considering the positive fault

normal component, and Rot is the component along the section when considering the

negative fault normal component. 4) is the angle between up-slope direction of the section

analyzed and the fault parallel direction (to the southeast). The five sets of earthquake

motions on the Hosgri fault are now rotated to earthquake motions along the up-slope

direction of cross sections L-L', M-M' and E-E'. For a given angle between the analyzed

section and the fault direction, there are 10 rotated earthquake motions, because for each

set, the positive and negative directions of the fault normal component are considered

separately.

I


The response of the slopes were computed using, as input, control motions specified at the

horizontal ground surface in the free field away from the toe of the slope. The originally

developed five sets of earthquake motions (sets 1, 2a, 3, 5, and 6) all fit the ISFSI design

spectrum. These motions were first rotated to the directions of the two cross sections

analyzed as described above. Then, approximate earthquake-induced displacements were

initially computed for each set using a rigid sliding block model based on the Newmark

approach (see calculation package GEO.DCPP.01.30). The set of rotated motions that

produced the highest deformation in the rigid sliding block analysis was selected as input

motions for the two-dimensional dynamic response analyses. For a representative yield

acceleration of 0.5g (based on the results from calculation package GEO.DCPP.01.28 for

sections E-E', L-L' and D-D'), and a yield acceleration of about 0.3g for section M-M'

from the same calculation package, rotated motions from sets 5 and 6 (both with a negative

fault normal component) provided the greatest deformation. Thus, two ground motion sets

(5 and 6) were selected as the input motions and used for the dynamic analyses. The results

of the dynamic response analysis as described in this calculation and the subsequent

deformation analyses (described in calculation package GEO.DCPP.01.30) indicated that

the input motion for set 5 produced the largest deformations of the two sets. Accordingly,

the detailed results for ground motion set 5 are only presented in this calculation. However,

because the direction of section L-L' is 91 degrees from the direction of the fault, the

rotated component along this section is almost identical to the fault normal component

(with a reversed polarity).

The rotated acceleration time histories (from set 5) along the directions of sections L-L',

M-M' and E-E' are presented in Figures 7, 8 and 9, respectively. The positive values

indicate motions in the up-slope direction of the section. The acceleration response spectra

of the two motions are presented on Figures 1O, 1 I and 12, for sections L-L', M-M' and E-

E', respectively. In these two figures, the response spectra of the original fault normal and

fault parallel components of set 5 are also shown for comparison. The rotated motions

along the sections show some variations from the originally developed fault normal and

fault parallel components.

I


Because the base of the finite element mesh is at a depth of about 300 feet, and because the

QUAD4MIJ program only allows the input motion to be applied at the base, the base

motion was first computed by deconvolving the surface ground motion. The control

motions specified at the ground surface (in the free field beyond the toe of the slope) were,

deconvolved using a one-dimensional wave propagation analysis, SHAKE (Geomatrix

version, 1995, see SOFIWARE section), to obtain input motions at the level of the base of

the two-dimensional finite-element model. Calculation package GEO.DCPP.01.34 shows

that, when using the base motion developed from SHAKE, the program QUAD4MU can

produce reasonably similar surface ground motions in the free field. This calculation

package verified that the deconvolved motions could be specified as input (outcropping)

motions at the base of the two-dimensional model. The rock below this depth was

modeled as elastic half-space that has the same shear wave velocity as the rock just above

it.

Finite Element Model and Boundary Conditions

Finite element representations of the slope profiles along sections L-L', M-M' and E-E' are

shown in Figures 1, 2 and 3, respectively. The minimum thickness of the mesh layer (8

feet) was selected to allow propagation of shear waves having frequencies up to 25 Hz.

The bedrock underlying the slopes was modeled to a depth of about 300 to 400 feet below

the horizontal firee field near the toe of the slope. The base of the finite element mesh is

treated as an elastic half space. For the nodes at the two lateral boundaries, the dynamic

displacement is only allowed in the horizontal direction when the horizontal input motion

is applied at the base. A better choice is to use transmitting boundaries on both sides to

avoid wave reflections from the vertical boundary. However, the program QUAD4MIJ

does not have this option. In order to avoid unrealistic reflections from the lateral

boundaries, the lateral boundaries were extended horizontally to a significant distance on

both sides of the transport route. The finite element mesh was extended in the horizontal

free field, a distance of about 400 to 700 feet from the toe of the slope for the three

sections. In the up-slope direction, the profiles were modeled for a distance of about 600 to

1 100 feet beyond the edge of the transport route (Reservoir Road). Beyond that point, the

ground surface was leveled-off and extended horizontally to additional distances where the

lateral boundary was placed. Because the response is only needed for potential sliding

I


masses in the vicinity of the transport route, the laterally extended portion of the mesh

need not accurately match the topography beyond a distance of several hundred feet from

the edge of Reservoir Road. The extended boundary is used only to improve the numerical

accuracy of the response in the immediate vicinity of the transport route, and not to model

the response of the entire hillside.

8.0 SOFTWARE

Computer program QUAD4MU was verified in calculation package GEODCPP.01.34,

revision 4. In applying the program to compute seismic coefficient time histories for

sections L-L', M-M' and E-E', the coordinate system, and the procedure to define a sliding

block are in compliance with the 'LIMITATIONS' stated in calculation package

GEO.DCPP.01.34, revision 4. Computer program SHAKE (Geomatrix version, 1995) was

verified in calculation package GEO.DCPP.02.02. A list of the QUAD4MU and SHAKE

input and output files included on the enclosed compact disc is attached (Attachment 10).

Key excerpts of files are also attached.

9.0 BODY OF CALCULATION

The input information was incorporated into input files for program QUAD4MU as listed

in the Attachment 10 and contained in the CD for this calculation package. The critical

sliding surfaces for the three sections analyzed (L-L', M-M' and E-E') were those

determined from calculation package GEO.DCPP.01.28, revision 3. These sliding blocks

were approximated by elements and its boundaries. The seismic coefficient computation

was performed by executing the program QUAD4MU on PC's under the DOS window.

10.0 RESULTS AND CONCLUSIONS

Response at ISFSI Design Ground Motion Levels

The results of the dynamic analyses provide a distribution of the earthquake-induced

accelerations at all nodal points of the modeled slope profile. The analyses also provide

estimates of the seismic coefficient time histories within specified potential sliding masses.

I


Using the rotated input motion developed from set 5, peak accelerations within the slope

(in the vicinity of the transport route) were computed for sections L-L' and E-E' only. The

contours of peak accelerations in the soil deposit are presented in Figures 13 and 14 for

sections L-L' and E-E', respectively. As expected, the input motion was significantly

amplified in the colluvium deposit within the slope, with computed peak surface

accelerations of about 1.7g and 2.Og for sections LL' and E-E', respectively. The

response at section M-M' resembles that of the input time history more than those

computed for Sections L-L' and E-E' because the material underlying the transport route is

mostly rock.

Specified potential sliding masses as shown in Figures 15, 16 and 17, for the three sections

analyzed. These sliding masses have the least computed yield accelerations as estimated

from calculation package GEO.DCPP.01.28, revision 3. Seismic coefficient time histories

were computed using QUAD4MU for each potential sliding mass at sections L-L', M-M'

and E-E' for input motions set 5 and set 6. Figure 18 presents seismic coefficient time

histories computed from input motion of set 5. The computed peak values of the seismic

coefficient time histories for the set 5 motion (for sections overlain by softer colluvium)

are of the order of 0.93g to 1.0g, and show an amplification of peak acceleration of about

20 percent compared to the input bedrock motions. The time histories shown in these

figures will be used to estimate earthquake-induced deformations within these potential

sliding masses as described in calculation package GEOXDCPP.01.30, revision 3.

Response at Reduced Ground Motion Levels

Dynamic analyses similar to those described above were performed, but in this case the

ISFSI design rock motions were scaled to a peak acceleration of 0.15g (Attachment 9) and

for sections L-L' and E-E' only. The computed peak accelerations along the surface of the

slope are presented in Figures 19 and 20 for sections L-L' and E-E' respectively. The input

motions were amplified mainly in the colluvium zones along the slopes of both sections.

The greatest computed surface accelerations are of the order of 0.26g and 0.31g at sections

I


L-L' and E-E', respectively. For comparison, the computed peak surface accelerations for

the response using the full design input motions are also shown in Figures 19 and 20.

Amplification factors for peak accelerations along the slope surface (normalized to the

peak input bedrock acceleration in the free-field) were computed for the two slope surfaces

and are presented in Figures 21 and 22 for section L-L' and EE', respectively. For section

L-L', the maximum amplification factor is less than 2. For section E-E', the maximum

amplification factor is less than 2.2. For comparison, amplification factors were also

computed for the response using the full design input motions and are shown by solid lines

in Figures 21 and 22. The maximum amplification factors for the full ground motions are

of the same order of magnitude as those computed using reduced input motion with peak

acceleration of 0.15g.

Because the computed peak accelerations for the reduced input motions are lower than the

estimated yield accelerations for the potential sliding surfaces (computed in calculation

package GEODCPP.01.28, revision 2), the expected earthquake-induced displacements

will be negligible. Accordingly, there was no need to compute the corresponding

acceleration time histories for potential sliding masses for this level of input motion.

11.0 LIMITATIONS

Seismic response of the transport route traversing colluvium and rock are reasonably

captured by the dynamic response analysis of sections D-D', E-E', L-L' and M-M'

presented in this calculation package.

12.0 IMPACT EVALUATION

The computed seismic coefficient time histories are the basis for the evaluation of

earthquake induced deformation at the transporter route. The results of this calculation are

used subsequently in calculation package GEODCPP.01.30, revision 3.

13.0 REFERENCES

I

of 39GEO.DCPP.O1 29, Rev. 3

1. Egan, J.A. and Ebeling R.M., 1985, Variation of small-strain shear modulus withundrained shear strength of clays, Second International Conference on SoilDynamics and Earthquake Engineering, pp. 2-27 to 2-36.

2. Geomatrix Consultants, Inc. Work Plan, Laboratory Testing of Soil and RockSamples, Slope Stability Analyses, and Excavation Design for Diablo Canyon

Power Plant Independent Spent Fuel Storage Installation Site, Revision 2, datedDecember 8, 2000.

3. Geosciences Calculation Package GEO.DCPP.01.21, revision 2, Analysis ofBedrock Stratigraphy and Geologic Structure at the DCPP ISFSI Site.

4. Geosciences Calculation Package GEODCPP.01.28, revision 2, Stability and YieldAcceleration Analysis of Potential Sliding Masses Along DCPP ISFSI TransportRoute.

5. Geosciences Calculation Package GEODCPP.01.30, revision 2, Determination ofPotential Earthquake-Induced Displacements of Potential Slides Masses Along

DCPP ISFSI Transport Route (Newmark Analysis).6. Geosciences Calculation Package GEO.DCPP.01.34, revision 3, Verification of

QUAD4M computer code.7. Geosciences Calculation Package GEODCPP.02.02, revision 0, Verification of

computer code SHAKE.8. Geomatrix, 1995, SHAKE.9. Hudson, M., Idriss, IM. and Beikae, M, 1994, QUAD4M (program and User's

manual) Center for Geotechnical Modeling, Department of Civil & EnvironmentalEngineering, University of California, Davis, California.

10. PG&E, 1988, Diablo Canyon Long Term Seismic Program, Response to NRCQuestion 19 dated December 13.

11. Vucetic, M., and Dobry, R., 1991, Effect of soil plasticity on cyclic response:Journal of Geotechnical Engineering, American Society of Civil Engineers, v. 117,

Paper No. 2541812. Seed, H. B., and Idriss, I. M., 1970, Soil moduli and damping factors for dynamic

response analyses: Report No. EERC 70-10, Earthquake Engineering ResearchCenter, University of California, Berkeley.

13. Seed, H.B., Wong, R.T., Idriss, I.M., and Tokimatsu, K., 1986, Moduli anddamping factors for dynamic analyses of cohesionless soils, Journal of

Geotechnical Engineering, ASCE, Vol.112, No.GTl 1, pp.1016-1032.

I


14.0 ATTACHMENTS

1. 617/02, PG&E Geosciences, Robert K. White, Re: Determination of azimuths for

cross-sections D-D', E-E', and L-L' for DCPP ISFSI transport route stability

analyses

2. 09/28/2001, PG&E Geosciences, Robert K. White, Re: Confirmation of transmittal

of inputs for DCPP ISFSI slope stability analyses.

3. 10/31/01, PG&E Geosciences, Robert K. White, Re: Confirmation of preliminary

inputs to calculations for DCPP ISFSI site.

4. 08/23/2001, William Lettis & Associates, Inc., Jeff Bachhuber, Re: Revised

Estimates for Hosgri Fault Azimuth, DCPP ISFSI Project.

5. 10/18/2001, PG&E Geosciences, Joseph Sun, Re: Positive direction of the fault

parallel component time history on the Hosgri fault.

6. 10/25/2001, PG&E Geosciences, Robert White, Re: Input parameters for

calculations,

7. 11/1/2001, PG&E Geosciences, Robert White, Re: Confirmation of additional

inputs to calculations for DCPP ISFSI site.

8. 5/29/02, PG&E Geosciences, Robert K. White, Re: Transmittal of PG&E August

1989 response to NRC question 12 of 1 June 1989.

9. 5/28/02, PG&E Geosciences, Robert K. White, Re: Transmittal of additional inputs

for DCPP ISFSI transport route analysis.

10. List of input and output files on enclosed CD ROM and key excerpts from files.

It. CD, entitled . GEO.DCPP.01.29, rev. 3, Dated 03/17/2003.

I


TABLE 1

SOIL PARAMETERS FOR STABILITY ANALYSIS

SLOPE SECTIONS D-D', E-E', L-L' AND M-M'

From calculation GEODCPP.01.28I

Geologic Description Density Shear Strength

Unit** In-Place, pdf Parameters

af Artificial fill 115 S. = 3000 psfoc. Ohf Quaternary colluvial fan, Holocene 115 Su = 1500 psf

alluvial fan

Qpf Pleistocene colluvium 115 S. = 3000 psf

Qptm Pleistocene marine terrace deposits 130 c = O psf, 4 = 400

TOfb Miocene Obispo Formation 140 c = 4000 psf; 4 = 350

Cross sections shown in GEODCPP.01.21 and GEODCPP.01.28, revision 3. I

I


TABLE 2 I

MATERIAL PROPERTIES FOR DYNAMIC FINITE ELEMENT ANALYSIS,SLOPE SECTIONS L-L', M-M' AND E-E'

DIABLO CANYON POWER PLANTI

Layer Unit Shear Poisson's Modulus and DampingMaterial and Weight Wave Ratio Relationships

Thikness' (pci) Velocity(h) (fps)

Qpf - Pleistocene Surface layer 115 1200 0.35 Clay (PI=15),Colluvium Vucetic & Dobry,19912

Qptmn - Marine between Qpf 130 1200 0.35 Sand (Upper Bound Modulus andTenrace Deposit and Tofb Lower Bound Damping),

Seed & Idriss,19703Tofb - Obispo below Qpf and 140 2000 0.4 Rock, LTSP SSI analysis,

Formation Qtm, h=15 feet PG&E, 1988Bedrock _ _ _ _ _ _ _ _ _ _ _

Obispo Formation h=20 feet 140 3300 0.4 SameBedrock

Obispo Formation h=125 feet 145 4000 0.37 SameBedrockl



Elastic Half Space below 150 5900 - linearElevation.- 300 feet

' Thickness below horizontal ground surface in free field2 Vucetic, M., and Dobry, R., 1991, Effect of soil plasticity on cyclic response: Journal of GeotechnicalEngineering, American Society of Civil Engineers, v. 117, Paper No. 254183 Seed, H. B., and Idriss, I. M., 1970, Soil moduli and damping factors for dynamic response analyses: ReportNo. EERC 70-10, Earthquake Engineering Research Center, University of California, Berkeley.

Final report of the long term seismic program submitted by PG&E to the NRC. On July, 1988.

I

( C (

to'2.04r-

Show Sftrn (%)lele tort 1

11

Figure A Varation of shear modulus with shear strain for the site rock based on 1978 laboratory test data.4

~T1aM

0O vt') nP..-

nO "

00* j wWo

( ( (Showr Strur (%)la-

110� IY I

IEmP

* Dymmn Tdodd Tao R~snmi Zm~_ Ahon w" toalw A&own h &O25L

- .uf ci .

20 1

I to L

j

00 0 0 *6

to

S

0 00 0 0

a

Figure X Variation of damping ratio with shear strain for the site rock based on 1977 laboratory test data.5

OA)

00a..

* qw'D


N

Section E-E'Az= 350Az= 3380

Section M-M'Az= 58°

.e

- Section L-L'<rfi= 67

N

, - / " Motion, A

Figure %t Orientations of Section E-E', Section L-L', Section M-M' and Hosgrl Fault.6

(.

1.0

= 0.5CD

0

0 0.00

-0.5

-1.0

1.0

c 0

goo0D

8-0.5

-1.0

1.0

C 0.50

0

8-0.5

-1.0

0 10 20 30 40

0 10 20 30 40

0 10 20 30Time (second)

40

. IQ

4 0 °

b* w

w anFigure 7. Acceleration time histories of fault normal, fault parallel, and rotated L-L' componenets of Set 5.

( C (1.0 _

0"O 0.5 -

C0.0-0

§-0.5 _

-1.0 _

0

1.0 _

' 0.5 -0

0.0 i0

a-0.5

-1.00

1.0

es 0.5 -0

i 0.00)

8-0.5

-1.0

10 20 30 40

10 20 30 40


40 i

o

_ ND

. ww loFigure 8. Acceleration time histories of fault normal, fault parallel, and rotated M-M' componenets of Set 5.

( (. (1.0

0-

I 0.0

0.5

-1.0

1.0

0C .0

0'S 0.00

8-0.5cc

-1.0

1.0

0.50

i~ 0.00

8-0.5

-1.0

0 10 20 30 40

0 10 20 30 40


40 |-.j40B

0- O

0%w0Figure 9. Acceleration time histories of fault normal, fault parallel, and rotated E-E' componenets of Set 5.


Section L-L': 91 degrees from FP direction…- Fault normal (FN) component- ---- Fault parallel (FP) component (with fling effect)

4.0

3.5

3.0

0>C

0

IDK:1U

CO)

2.5

2.0

1.5

1.0

0.5

0.00.01 0.1 1

Period (see)

Figure 10. Acceleration response spectra of Input motion set 5 for cross section L-L'.


Section M-M': 100 degrees from FP direction-- -Fault normal (FN) component

-- --- Fault parallel (FP) component (with fling effect)4.0 - =- _ _ _ -= _ _ _ -_

3.5 -

3.0- = = _ _ -_ _ _ _ _ =

2.5 -

CD

2.0 -

co

1.0-_ _ _-Y,_=_ f _ _

0.5 ____________ A

0.0 = - - _ _ _ _ - - _ _ _ _ _ - -

0.01 0.1Period (sec)

Figure 11. Acceleration response spectra of Input motion set 5 for cross section M-M'.


4.0

3.5

3.0

C0

0

C.Ki

2.5

2.0

1.5

Section E-E': 123 degrees from FP direction… Fault normal (FN) component

- ---- Fault parallel (FP) component (with fling effect)

=-________ _ =-__-___

a__=_____ =- -____ - a , -.

_ =-_ _ =-_ _ __ = _

1.0

0.5

0.00.01 0.1 1

Period (sec)

Figure 12. Acceleration response spectra of Input motion set 5 for cross section E-E'.

300 l I l -

280

Dashed line: potential sliding surace26iS

240

.1

20-

0 20

10-

10-

120.

350 400 450 500 550 600Horizontal Disa , feet

Figure 13. Contours of peak accelerations In coluvium zone, cross section L-A'

( (

250C

200

150-Le0

50-

r'

1 l l i l l l l lr

Dashed line: potential sliding surface

700 750 800 850 90 950 1000 1050 1100 1150 1200 1250Horizontal Distance, feet

Figure 14. Contours of peak accelerations In cot uium zone, cross section E-E'

-I-

~-_ C

^0sow

* ww to

(

I a I - I I I I I I I

(

-

to- ---

260-

240-

.4.220-

20

mi 180-

160-

140-

d0%

v J_,, ,1 -, ~

,f^ I , , , S

A0_ f I I I I I I 4

- I I I I4 - I I49- ._ § e @ W I I I 1

p.4. - I - I1 4 I 1I 4I 1 i

I

_ e § I I I I I 1

_e I I I I I I I 1 g

^ I I I I I I I I

1 I I . -1-4-4-1 4-4- L __

I I I I I I JF

t -~ -I '

- -I

I~le *? I._

300 I I I I I_ -320 340 360 380 400 420 440 480 480 500 520 540 560 580 660Horizontal Dtance, feet

0 Ipiw- i

.w %4

Figure 15. Potential Sliding Mass to Compute Seismic Coefficient Time Histories for Cross Section L-'.

( ( C

IIII I II I IIII I:40law l- I

320-

300-

S 280-

Is0 280-Ela

240-

220-

_ . . .

I'A1/_ - * ,.- -, ,

Of l l l He

7/he , , . . ..

r

, ,,

%L44zI - I 4 - 4 - - I - c

�1- I - I-� - I

_

In II-- V I

100 120 140 10 180 200 220 240 20 280 30 320 340 30Horlzontal Dfstance, feet

__

380 400

0

o AFigure 16. Potential Sliding Mass to Compute Seismic Coefficient Time Histories for Cross Section M-M'. T a,

.w w-%YOLA

( ( (

za l

Z4u 1 I II r

220

200-

s 180-

0 160-

I 140-w

120-

100-

I

.. q, IloK00

u i I I I I650 700 750 800 850 900 950 1000 1050 1100 1150 1200 1250

Horizontal Distance, feet

Figure 17. Potential Sliding Mass and Node Points of Computed Acceleration Time Histories for Cross Section E-E'.!T2a

-

. w

* ww W

(1.0

C0.50

la0.00ID8-0.5

-1.0

1.0

e 0.50

;0.0CD

8-0.5

-1.0

1.0

c 0.50

e 0.0

8-0.5

-1.0

C (

0 10 20 30 40

0 10 20 30 40

40m- a

w40

*w

w %D

0 10 20 30lime (second)

Figure 18. Seismic coefficient ti me histories of potential sliding masses using Input motion set 5

2Full Input motion

---------- Reduced motion (scaled down to 0.15 g)tm 1.5 ISurface elevation oyf section 1-12

0.5-0

T I -600

t~4 | <~ 400

U)F~- 0.5

0 Zo

200

-500 0 500 1000 1500 2000Horizontal Distance, feet co

Fiaure 1 9 Variatinna of fUnmuu nook l s.3…- -w - o . .. -_ __ . w.. W L- .-. W, �1 I 9jwA%.1wA FUUM CX%,%,e1etUvns tuoug slopis suiTace cyrsewon L-1:.

2

( (Full input motion

------ Reduced input motion (scaled down to 0.15 g)Surface elevation of section E-E!

e0ax

cC0

I,CL

1.5

1

0.5

.__________ - __.-

0

0-P

CE0

w10

800

600

400

200

0 P

* ,)ww'D

0 500 1000 1500 2000Horizontal Distance, feet

2500

Figure 20. Variations of computed peak accelerations along slope surface of section E-E'.

(I C (2 Full input motion

_\---------- Reduced input motion (scaled down to 0.15 g)Surface elevation of section L-L'

L1.5

CL

0.5 I

0

600

| / 4e 400

Qpf Zone_

III I1I- I.--I I I II--500 0 500 1000 1500 2000

Horizontal Distance, feet

0Figure 21. Variations of cornputed amplification factors of neak scc elrations alonannafac elrfir- nf er-iftn I _1 w %O

- - - - - - - - W_ __._ -"II �%~ %#I I .

2

( CFull input motion

-- Reduced input motion (scaled down to 0.15 g)Surface elevation of section E-EN

UCoL-

Q.C0(aU

1=

1.5

0

0.5

!

0

.6-Sax

0w

mDQpf Zone

800

600

400

200

8

t4 O

* wW OD

0 500 1000 1500 2000Horizontal Distance, feet

2500

Figure 22. Variations of computed ampiTfication factors of peak accelerations along slope surface of section E-E'.

CALCULATION PACKGE GEO.DCPP.0129REVISION 1

ATTACHMET 1

PAGE3 2 op17i

Pacific Gas and Electric Company Geosien245 Market Street, Room 418BMail Code N4CP.O. Box 770000San Francisco, CA 94177415/973-2792Fax 415/973-5m

GEO.DCPP.0l.2 9

REVISION I

DR. FAIZ MAKDISIGEOMATRlX CONSULTANTS2101 WEBSTER STREETOAKLAND, CA 94612

7 June 2002

Re: Determination of azimuths for Cross Sections D-D, E-E', and L-L' for DCPPISFSI Transport Route Stability Analyses

DR MAKDISI:

For your use in DCPP ISFSI transport route stability analyses, we have determined theazimuth of each section from Figure 21-3 of Geosciences CalculationGEO.DCPP.01.21, rev. 2, as follows:

Section D-D': 38 degreesSection E-E: 35 degreesSection L-L': 67 degrees

If you have any questions regarding this information, please call.

ROBERT K. WHITE

PAGE 33oF171

page I of I a o2ftM.doc-kw:6nt02

CALCULATION PACKGE GEO.DCPP.01.29REVISION 1

ATTACHMENT 2

PAGE3 4 oiR17i

Pacific Gas and Electric Company Geosciences245 Market Street, Room 418BMai Code N4CP.O. Box 770000San Francisco, CA 94177415/973-2792Fax 415/973-5778

GEO.DCPP.01- 29

REVISION 1

Dr. Faiz MakdisiGeomatrix Consultants2101 Webster StreetOakland, CA 94612

September 28, 2001

Re: Confimnation of transmittal of inputs for DCPP ISFSI slope stability analyses

DR. MAKDISI:

This is to confirm transmittal of inputs related to slope stability analyses you arescheduled to perform for the Diablo Canyon Power Plant (DCPP) Independent SpentFuel Storage Installation (ISFS1) under the Geomatrix Work Plan entitled "LaboratoryTesting of Soil and Rock Samples, Slope Stability Analyses, and Excavation Designfor the Diablo Canyon Power Plant Independent Spent Fuel Storage Installation Site."

Inputs transmitted include:

Drawing entitled "Figure 21-19, Cross Section I-I'," dated 9/27/01, labeled "Draft,"and transmitted to you via overnight mail under cover letter from Jeff Bachhuber ofWLA and dated 9/27/01.

Time histories in Excel file entitled "time histories-3comp revl.x1s," dated8/17/2001, file size 3,624 KB, which I transmitted to you via email on 8/17/2001.

Please confirm receipt of these items and forward confirmation to me in writing.

Please note that both these inputs are preliminary until the calculations they are partof have been fully approved. At that time, I will inform you in writing of theirstatus. These confirmation and transmittal letters are the vehicles for referencinginput sources in your calculations.

PAGE 3 5 oFI71

page I of 2 g oufm1.oc:rkw:9/=8t1

Confmation of transmittal of inputs for DCPP ISFSI dope stability analysts GEO.DCPP,01. 2 9REVISION i

Although the Work Plan does not so state, as you are aware all calculations arerequired to.be performed as per Geosciences Calculation Procedure GEO.001,entitled "Development and Independent Verification of Calculations for NuclearFacilities," revision 3. All of your staff assigned to this project have been previouslytrained under this procedure.

I am also attaching a copy of the Work Plan. Please make additional copies formembers of your staff assigned to this project, review the Work Plan with them, andhave them sign Attachment 1. Please then make copies of the signed attachment andforward to me.

If you have any questions, feel free to call.

Thanks.

ROBERT K. WHITE

Attachment

cc: Chris Hartz

..

PAGE 36 OF 171

page 2 ot 2

CALCULATION PACKUE GEOlCPP.01.29REVISION 1

ATTACHMENT 3

PAGE 3 7 F171

Pacific Gas and Electric Company Geosciences245 Market Street, Room 418BMail Code N4CPAO. Box 770000San Francisco, CA 94177415/973-2792 GEO.DCPP 01- 2 9Fax 4151973-5778

REVISION j


October 31, 2001

Re: Confirmation of preliminary inputs to calculations for DCPP ISFSI site

DR MAKDISI:

A numbei of inputs to calculations for the DCPP ISFSI slope stability analyses havebeen provided to you in a preliminary fashion. This letter provides confirmation ofthose inputs in a formal transmittal. A description of the preliminary inputs and theirformal confinmation follow.

Letter to Faiz Makdisi from Rob White dated June 24, 2001.. Subject:Recommended rock strength design parameters for DCPP ISFSI site slopestability analyses.

This letter recommensled using * =50 degrees for the preliminary rock strengthenvelope in your stability analyses, and indicated that this value would be confirmedonce calculations had been finalized and approved. Calculations GEO.DCPP.01.16,rev. 0, and GEO.DCPP.01.19, rev. 0, are approved and this recommended value isconfirmed.

Letter to Faiz Makdisi from Rob White dated September 28,2001. Subject:Confirmation of transmittal of inputs for DCPP ISFSI slope stability analyses.

This letter provided confirmation of transmittal of cross section -1' and time histories,and indicated that these preliminary inputs would be confirmed once calculations hadbeen approved. Calculation GEO.DCPP.01.21, rev. 0, is approved and section I-I' asdescribed in the September 28 letter is confinned. A copy of the figure from theapproved calculation is attached. Calculations GEO.DCPP.01.13, rev. 1, andGEO.DCPP.01.14, rev. 1, are both approved and time histories as described in theSeptember 28 letter are confirmed. A CD of the time histories from the approvedcalculations is attached.

PAGE 3 80P O7Fpage 1 of 2 Itr2fm3.doc:rkw: 10/31/01

4.:. /4 (:f

GEO.DCPP.o1. 2 9

REVISION I

Confirmation of preiay Inputs to caicuilations tor kR4wSSI SiteFaiz Makdisi

Email to Faiz Makdisi from Joseph Sun dated October 24, 2001. Subject:Ground motion parameters for back calculations.

This email provided input for a back calculation to assess conservatism in clay bedproperties in the slope. Inputs included maximum displacement per event of 4 inchesand a factor of 1.6 with which to multiply ground motions for use in the backcalculation analysis. This letter confirms those input values, with the followinglimitation: these values havenot been developed under an approved calculation,therefore should not be used to directly determine clay bed properties for use in forwardanalyses, but may be used for comparative purposes only, to assess the level ofconservatism in those clay bed properties determined in approved calculations

Letter to Faiz Makdisi fkrm Jeff Bachhuber dated October 10, 2001. Subject:Trlnsmittal of Revised Rock Mass Failure Models - DCPP ISFSI Project.

This letter provided you with figures indicating potential rock mass failure models assuperimposed on section I-I'. This letter confirms PG&E approval to use these modelsin your analyses. These figures are labeled drafts and are currently being finalized in arevision to Calculation GEO.DCPP.01.21. Once this revision and the included figureshave been approved, I will inform you in writing of their status.

ROBERT K. WHITE

Attachments

PAGE 3 9 Op 1 71

CALCULATION PACKGE GEODCPP.0129REVISION 1

ATTACHMENT 4

PAGE 40OF171

- X- - . t..- b b- Sss

GEO.DCPP.01. 29

*i RE3VISION I WilliamLettis IcAssocdates, Inc'.

t =, -| z !177 entBolho brive, Sulhe 262. MIMIu CMA~, C211-ntim %94S69w: ~Votc: M95) U%4 PAX NS2) W-W76

MEMORANDUM

TO: Dr. Faiz Makdids - Geomatrix Consultants, IT1.FROM: Jeff L. &~chbubcr - William Lettis & Associates, Inc.DATE: August 23,2001

RE: Revised Estimates for Hosgri Fault Azimuth, DCPP ISFSI Project

FAIZ:

This memorandum provides a revised strike azimuth of 338' for thc Hosgri fault forevaluation of ground motion directional components for slope stability vialyses at thePG&E DCPP ISFSI site. The revised azimuth presented in this memorandum supercedes

* the previous estimated azimuths (328° to 335W) presented in our memorandum datedAugust 8, 2001, and is based on a reevaluation of fault maps in the PG&E LTSP (1988),and 1SFSI project Calculation Packago GEO.01.21.

The revised estimated average strike for the Hosgri fault nearest the ISFSI site (betweenMorro Bay ad San Luis Bay) 1J 338e. Figurc 21-23 of Calculation Packae GEO.01.21,which previously showed an azimuth of 340 for the JHosgri fault, will be revised tocorrespond to tiis r-interpreted average strike. Discrete faults and local reaches of thefault zonc exhibit variations in strike azimuth between about 32' and 338', but theaverage overall strike of 338° is believed to be the best approximation for the groundmotion modeling.

Please call me if you have any questions or require further input for this issue.

Jeff Bachhuber

Cc: Rob WhiteBill Page - PG&E Geosciences

PAGE 4 10o 171

CALCULATION PACKGE GEOG3CPP.0129REVISION 1

AITACEMENT 5

PAGE 42OF171

GEo.DcPP.ot 2 2 9 REVISION I

Ptcific Gas & Electric Cozmpany

I z3 Geosclenees Department

P.O. sox 770000, Mail CW...Sar Francisco, CA 94177Fax: (415) 973-577

I UL' %x ,i

TELEFAX COVER SHEET

.MMOMMOWN-00 --- W�- -

To:

;U-

Phone: -t(b) 661- U41

Fc: ( 4

Date: trt fS 'o --

Number of pages includingcover sheet.'

From:

CompanY: PG-:&

Phone: (41 g) 273- 24D

Fax: (415} 973.5778

REMARKS: o Per request a For reiew O3 Reply ASAP Q Please comment

P@c ;i tn Al &¢ 41- O"4a*a e4. tsXIP £Lj719 fJ/tJ fi pz&ek*

(3 . .frrA -Tn;,Mf-, 1..~ da~~e

PAGE 43oFi7icwalaft3 --. WC

GEO.DCPP.OI. 29 REVISION

PACIFIC GAS AND ELECTRIC COMPANYGEOSCIENCES DEPARTMENTCALCULATION DOCUMENT

PREPARED BY: ___ __ __

RCvision dDate 410 4. /IM z/ Of

Cslc Pagcs: 2.AVerif cation Mcthod: Avyeificazon Pages: j7 4 f Ahdnm&

k )-S Cs, L-0A -. !;E

D.ATE 0 C4-'W (fj Tei/

,>zeK ya i&-&sodPdntcd Name Oranization

VERFIED BY:

APPROVED BY:

PdntedA( A=

P~osIVc.,,L~

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DATE 0tedrt 1.a4 (

Ogamiztin

DATE

OrgnizaTion

PAGE 44o 17171A*('i:Zfn W '%kJ:m U

'{ -0 falslr10- pgX- If--/6 00 Z

et^ n* _1 . ,

GEO.DCPP.ol. 2 9E%.Vd'REVISION I

Calc Number: GBO.DCPP.01.14Rev Nuber: I

Sheet Number; 4 of 26Date: 10/1=21

6. BODY OF CALCULATIONS

Ste, 1: S-wave arrival timesThe approximate arrival times of the S-waves is estimated by visual inspection of thevelocity time histories (gures 1, 2,3, 4, and 5). The selected arrival times are listed inTable 6-1.

Table 6- 1. Time of Fling

S Reference trme History Appoiate Arvalie PolarnteAzrival timof of fling (t1 )

. LuceeS-waves (seI Lucerne 8.0 7.1 -12a Yzrimca 9.0 8.5 -I3 LGPC 4.0 3.45 El Centro (1940) 15 0.0 I6 Saratoga 4.5 3.7 -1* The polarity is applied to the fault parallel time history from calculationsGEODCPP.01.13 (rev 1) to cause constructive interference between the S-wave and theflng (eq. 5-2).

A flig arrival time is selected by visual inspe6on of the inteiference of the velocity ofthe tUansent motion and the fling (Figures 1, 2, 3, 4. and 5). The selected fling arrivaltime are listed in Table 6-1.

Since DCPP is on the east side ofthe Hosgri fault and the fault has right-latral slip, thepermanent tectonic defomation at the site will be to the southeast In the ti historiesthe fling has a positive polarity. Since the tectonic deformation will be to the southast,the positive direction of the fault pamallel time histoy is defined to the southeast

Step 2: Flzn Time HistorM *Using the values of A. ol, and Tgiuz given in inpt 4-1, and thi values oft1 given in Table6-1, the fug time history is determined using eq. (5-1). The computed fling timehitories for the 5 sets are shown in FgSurs 1, 2, 3, 4, and S.

PAGE 45 OF 171

-

CALCULATION PACKGE GEODCPP.01.29REVISION 1

ATTACHMENT 6

PAGE 4 6 oF171

Pacific Gas and Electric Company Geosciences245 Market Street. Room 418BMa0i Code N4CP.O. Box 770000San Francisco CA 9417- GEO.DCPP.OI. 29415/973-2792* 415/935773 REVISION i

DR. FAIZ MAKDISI VGEOMATRDX CONSULTANTS2101 WEBSTER STREETOAKLAND, CA 94612

October 25, 2001

Re: Input parameters for calculations

DR. MAKDISI:

As required by Geosciences Calculation Procedure GEO.001, entitled "Developmentand Independent Verification of Calculations for Nuclear Facilities," rev. 4, I amproviding you with the following input items for your use in preparing calculations.

1. The shear wave velocity profiles obtained in borings BA98-1 and BA98-3 in 1998are presented in Figure 2142, attached, of Calculation GEO.DCPP.01.21,entitled "Analysis of Bedrock Stratigraphy and Geologic Structure at the DCPPISFSI Site," rev. 0, and can be so referenced. These profiles were previouslypresented in Figure 10 of the WLA report entitled "Geologic and GeophysicalInvestigation, Dry Cask Storage Facility, Borrow and Water Tank Sites," datedJanuary 5, 1999.

2. The average unit weight of rock obtained from the hillside has been determined tobe 140 pounds per cubic foot, as documented in a data report entitled "RockEngineering Laboratory Testing - GeoTest Unlimited.

3. Regarding the time histories provided to you on 8/17/01, since the tectonicdeformation will be to the southeast, the positive direction of the fault paralleltime history is defined as to the southeast, as described in Geosciences CalculationGEO.DCPP.01.14, entitled "Development of Time Histories'with Fling," rev. 1,page 4.

4. The source of the shear modulus and damping curves are Figures Q19-22 andQ19-23, attached, from PG&E, 1989, Response to NRC Question 19 datedDecember 13, 1988, and can be so referenced.

Regarding format of calculations, please observe the following:

PAGE 4 7oFP171.doc:xk:W25/0

Faiz Makdisi Faput parameters for calculations

GEO.DCPP.oI.2 9 REVISION I

Contents of CD-ROMs attached to calculations should be listed in the calculation,including title, size, and date saved associated with each file on the CD-ROM. If thenumber of-files is considerable, a simple screen dump of the CD-ROM contents issufficient

If you have any questions regarding the above, please call me.

216,+ I6 a_

ROBERT K. WHITE .

Attachments

PAGE 48 o017i

CALCULATION PACKGE (3E0.DCPP.01.29REVISION 1

ATTACHMENT 7

PAGE 4 9 0p 171

Pacific Gas and Electric Company Gemim=245 Markt Stret, Room 418BMail Code N4CP.O. Box 770000 GEO.DCPP.01.29San Francisco, CA 94177415192792 REVISION ]LFax 41513-578

AT T A L- h i \k° -


November 1, 2001

Re: Confirmation of additional inputs to calculations for DCPP ISFSI site

DR. MAKDISI:

Additional inputs to calculations for the DCPP ISFSI slope stability analyses have beenprovided to you by Jeff Bachhuber of William Lettis Associates. This letter providesconfirmation of our acceptance of those inputs in a formal ransnmittal. A description ofthose additional inputs and their formal acceptance follow.

Letter to Faiz Makdisl from Jeff Bachhuber dated August 3,2001. Subject:Ground Motion Directional Components.

This letter recommended using an azimuth of 302 degrees plus or minus 1O degrees forthe orientation of the most likely failure surfaces, coinciding with Section I-I'. Weconcur with this recommendation based on the discussion on page 53 of the approvedCalculation GEO.DCPP.01.21, rev. 0, and verification of the orientation of Section I-I'on Calculation Figure 21-4, attached.

Letter to Faiz Makdisi from Jeff Bachhuber dated August 23,2001. Subject:Revised Estimates for Hosgri Fault Azimuth, DCPP ISFSI Project.

This letter recommended using an azimuth of 338 degrees for the orientation of theaverage strike of the Hosgri fault We concur with this recommendation, based onverification of the orientation as presented in the LTSP plates and as shown onFigure 21-36, attached, of Calculation GEO.DCPP.01.21, rev. 0.

ROBERT K WHITE

Attachments PAGE 5 ° OF 171

page I of I p o2ft4.doc:r1w: IJ/WI

CALCULATION PACKGE GEODCPP.01.29REVISION 1

ATTACHMENT 8

PAGE 5 1 OF171

Pacific Gas and Electric Company Geoscieum245 Market Street, Room 418BMail Code N4CP.O. Box 770000San Franesw, CA 94177415/973-2792 GEO.DCPP.01.2 9Fax 415/973-577I

REVISION 1


29 May 2002

Re: Transmittal of PG&E August 1989 Response to NRC Question 12 of 1 June1989

DR. MAKDISI:

Please find attached one copy of the above-referenced Response.

If you have any questions regarding this information, please call.

ROBERT K. WHITE

Attachment

PAGE 52 OF 171

page I of I e 1ftM.doc:rkw:5flIm

GEO.DCPP.Ol .2 9REVISION j

RESPONSE TO QUESTIONS 1, 2, 3, 4 5, 7,10, 11, 12, 13,14, and 16

August 1989

This volume responds to 12 of 19 questions asked of PG&E by the NuclearRegulatory Commission (NRC) on June 1, 1989. Responses to the remaining 7questions will be submitted later. These responses provide data requested to augmentor clarify information regarding seismic ground motions presented in the FinalReport of the Long Term Seismic Program, submitted by PG&E to the NRC on July31, 1988, and in the responses to Questions 4 through 18 and 20, submitted by PG&Eto the NRC in January and February 1989.

PAGE 53 OF j171

Paciflc Gas and Electric CampanyDablo Canyon Power Pant

Long Term Seismic Program

GEO.DCPP.01I 2 9 RIEVT.Znw - _Ouestion 12. Aueust 1989 L.Pn

QUESTION 12

To aid in assessing the proposed lack of topographic effect at the Diablo Canyon site.provide a numerical study using vertically polarized shear waves with ground motionamplitude referenced to sea level.

The lack of significant topographic effects on ground motions at the Diablo Canyon site wasdemonstrated using finite difference modeling for SH waves. The results were presented in the FinalReport, July 1988, and in our response to Question 17a, January 1989.

In response to the present question, we have made two additional studies. Both studies were basedon SV waves incident on a cross section selected to have the maximum topographic relief in the sitearea. Furthermore, rock properties identical to those used in the soil/structure interaction analysespresented in the Final Report, July 1988, were incorporated into this cross section.

The first study described below extended our earlier finite difference modeling to using SY pulseshaving Gaussian Fourier acceleration spectra. This study was made to assess the sensitivity ofpotential topographic effects to incident wave type and wave frequency, as well as incidence angle.The second study was based on finite element modeling using one of the site-specific accelerationtime histories used in the soil/structure interaction analyses as the input control motion. This studywas made to show potential topographic effects on the site-specific ground motions for the DiabloCanyon site.

The results of both studies, as presented below, further confirm the lack of significant topographiceffects on ground motions at the location of the power block structures at the Diablo Canyon site.

Finite Difference Modeling

In this study, the effects of topography on ground motions at the site were investigated using finitedifference calculations that assumed linear elasticity of the foundation rock. A site plan showingthe location of the cross section analyzed is shown on Figure Q12-1. A topographic profile of thissection is shown at the bottom of Figure Q12-2. The material properties of the rock are summarizedin Table Q12-1. The input ground motion was a Gaussian pulse whose Fourier acceleration spectrumwas centered at a frequency of 2.5 Hz, which is comparable to the Fourier spectra of the suite ofempirical strong motion records used to develop the input spectrum for the soil/structure interactionanalyses. An example of the accelerograms calculated for a vertically incident SV wave is shown atthe top of Figure Q12-2. The delay between stations 15 and 1 represents the propagation time ofthe wave between sea level and the elevation of the top of the ridge. Peak amplitudes are shownto the right of the accelerograms for station locations along the topographic profile shown at thebottom of Figure Q12-2.

Figure Q12-3 shows the response of the site region for a series of different input ground motions.The response is represented by the ratio of peak acceleration for the model having topography to thepeak acceleration for the model having no topography, which defines the free-field control motion.The response of the site region to a vertically propagating SV wave shows a slight deamplificationat the base of the sea cliff and a peak amplification of about 17 percent at its crest. The motion atthe location of the power block structures is generally deamplified; at its greatest, the deamplificationis about 15 percent.

The sensitivity of this response to incidence angle is illustrated using an SV wave incident from theleft (ocean side) at 20 degrees from vertical. The response is quite similar to that for verticalincidence, but the regions of amplification at the crest of the sea cliff and the crest of the ridge, andthe region of deamplification at the base of the ridge are extended toward the east due to theexcitation of Rayleigh waves. The location of the power block structures is again within a regionof mostly deamplification, which in this case now extends farther right to the lower part of the ridge.

PAGE 5 4 OF 171a scablo SBa ve r Powe ra P nin3 Factfc Gas and Electlc Company bUng TeSeismic Progrm

GEO.DCPP.01.2 9 REVISION 1Pare 2ffniaeutien 12A Avieivt 109 I0

Figure Q12-1

Site plan showing location of cross section A-A' analyzed for topographic effects on ground motionsin the Plant area.

PAGE 55 OF 171I PacHic Gas and Electrc Company

Diablo Canyon rPwer PintLong Tam Selsmic Program

GEO.DCPP.0 1.2 9 G D9 REVISION N1 Nve 3nuevatiout 12 Ateti 1080

Time (sec)

0.6 0.9 1.20.0 0.3 1.5 1.8

Station no.

23456789.I0l l12131415

PGA / PGA(Control Motion)

0.980.981.171.121.03

0.920.870.970.991.01I.000.991.051.13

0.97

1000

Ia,

Soo

0

-500

Distance (fit)

Figure Q12-2

Accelerogram calculated for a vertically incident SV wave, andtopographic profile, cross section A-A'.

PAGE 56 OIF 171I acfc Gas and Electrc Company

Diablo Canpo Pow PlantLmn Tom Selsmic Pogram

GEO.DCPP.01. 29 REVISION 1V) A .. o- 10114 Deem A

Table Q12-1

ROCK PROPERTIES USED IN ANALYSIS

DepthNOtL

LayerThickness

(ft)Density

(neff'

Shear WaveVelocity

(fntsPoissones

Ratin

IS 140 2600 0.45

15

20

35

125

160

140

145

150

ISO

3300

4000

4800

5900

0.40

0.37

0.35

0.22

100

260

00

PAGE 57 oF 171i Pacnfc Gas and EleCtic Company

Blabl Ca"pu Powr PlatLu Tom Sem c Pmgram

GEO.DCPP.o1. 2 9 REVISION 1tlviestin 12. Ativivt 1090

.- afK VI-x .

I

C0

0

-

C0

CDC-

CD

I

"f==f= 0-

_/'11

_WWM

SV, 20°

SV. 0°

SH , 00_ _ _ _ _ _ _

SV, higher frequency

0

1000

C

.92

I.1

500

0

-500

Distance (ft)

Figure Q12-3

Response of the plant site region for different input ground motions.

I Pacfi Gas and Electric CompanyPAGE 58 op 171 iabloe Canyon Power Pant

lon Tarm Sdsmlc Program

Question 12. August 19g9 'GEO.DCPP.Ol .2 9 REVISION 'Pavc 6

The sensitivity of the vertically propagating SV wave response to higher frequencies was examinedby increasing the center frequency of the Fourier spectrum of the input pulse to 3 Hz. The responseof the 3-Hz pulse is very similar to that for the 2.5-Hz pulse. The main effect of shifting thefrequency content to higher frequencies, as shown at the top of Figure Q12-3, is to deepen andbroaden the troughs at the base of the sea cliff and at the location of the power block structures, andto move the latter trough to the left.

The response to a vertically propagating SH wave is very similar to that for a vertically propagatingSY wave (Figure Q12-3). For both SY and SH waves, the topography causes amplification near thecrests of the sea cliff and the ridge, and deamplification near the bases of the sea cliff and the ridge.

For the entire range of input motions tested in this sensitivity study, the effect of the topographyis to generally deamplify the ground motions at the location of the power block structures withrespect to free-field conditions.

Finite Element Analysis

To further aid in assessing possible effects of topography at the plant site, we conducted a two-dimensional finite element analysis using vertically propagating SV waves. The cross section (FigureQ12-l) was selected to traverse the area of maximum topographic relief. The finite elementdiscretization of the cross section was constructed to transmit ground motions having frequencies ashigh as 25 Hz. A viscous boundary was provided at the base of the finite element model to simulatean elastic half-space below. Transmitting boundaries were provided on the right tide (uphill side)and left side (ocean side) of the model. The analysis was made using the computer programSuperFLUSH (Earthquake Engineering Technology, 1983).

The low-strain shear wave velocities and Poisson's ratios of the site rock used in the analysis are thesame as those used in the soil/structure interaction analyses, summarized in the Final Report, July1988. These properties were used throughout the two-dimensional model at the depths below theexisting ground surface indicated in Table Q12-1. Below a depth of 260 feet, the shear wavevelocity is 5900 ft/sec. This velocity was also used for the half-space below. The strain-dependentvariations of shear modulus and damping ratio for the site rock used in the analysis are also the sameas those used in the soil/structure interaction analyses. Values of strain-compatible shear modulusand damping ratio used for the two-dimensional model were estimated on the basis of a one-dimensional ground response analysis of the site. The results of the one-dimensional analysis showedvery minor strain-dependent effects, with reduction in shear wave velocities less than 6 percentbelow the low-strain values.

The input control motion used in the analysis was the same horizontal motion used in thesoil/structure interaction analyses. This motion is a modification of the longitudinal component ofthe Pacoima Dam record (1971 San Fernando earthquake), which matches the median site-specificacceleration response spectrum for the Diablo Canyon site. As was done for the soil/structureinteraction analyses, this motion is specified as a free-field control motion at the ground surface(Elevation 85 feet). Using this motion, the outcrop motion of the underlying rock half-space wascalculated and used as the rock outcrop motion of the half-space of the finite element model. Theinput motion was applied in the direction of the plane of the model, thus representing verticallypropagating SV waves.

Results of the analysis in terms of peak ground acceleration and average spectral acceleration (Spercent damped) in the 3 to 8.5 Hz range versus location along the cross section are shown in FigureQ12-4. Values of the peak acceleration and average spectral acceleration of the free-field controlmotion are also shown in these plots for comparison purposes. In Figure Q12-5, these results arenormalized to the control motion, that is, divided by the corresponding amplitudes of the controlmotion at the ground surface in the free field. Figure Q12-S shows that ground motions at thelocation of the power block structures on the average are about 10 percent less than the controlmotion. Ground motions near the crest of the sea cliff are amplified by about 25 percent. Theseresults show trends almost identical to those obtained from the finite difference calculations shown

PAGE 5 9' OF 171 UlahibCanyo PowerPlantF cl Pafic Cas and Elecic Company Lung Term Sere c Program

GEO.DCPP.01. 2 9 REVISION 1f%9%e#tLf V) A evn~e 10R0 Veno Ivu<;OtZ5 A. RZUYUA> p rpY 8 0L.

3

o 2.25NIeo 1.5

v6uA .75

01

.8

Cr.6

a. .4

.2

01000

500

0

C0

0

0

0

C)

-5000 500 1000 1500 2000 2500 3000 3500 4000 4500

Distance (ft)

Figure Q12-4

.~ Effects of topography on peak ground acceleration andhorizontal motions along the ground surface.

spectral acceleration values for

PAGE 60 OF 1 71I Palilc Gas and ect Company

oae Canyon Power PlantLong Term Soisic Program

GEO.DCPP.O 1. 2 9 REVISION iPe RA2iouertin 12 Atimict 1010

N

Ix 20U

r')

0

-

0C.)0

tno0

2

C

c

1 .o

I U

1

0

1000

C)

I S

I 00

a4.

500

0

- 50 0 I I ' I i ' * ' * ' ' ' ' ' ' '0 500 1000 1500 2000 2500. 3000 3500 4000 4

Disthnce (ft)

Figure Q12-S

Effects of topography on normalized peak ground acceleration and normalized spectral accelerationvalues for horizontal motions along the ground surface.

500

PAGE HIOF 171I Pacfllc Gas and Electrc Company

Diable Canyon Power PlatLong Term Slsiolc Pogram

GEO.DCPP.0 I 2 9 REVISION -'Pe 9nhi.est;Vn" 12 A ittst 19R0

on Figure Q12-3.

Figures Q12-6 through Q12-8 show response spectra (5 percent damped) of ground motions near thecrest of the sea cliff, at the location of the power block structures, and at both the left and rightboundaries of the finite element model. The response spectrum of the free-field control motion isalso plotted in Figures Q12-6 through Q12-8 for comparison purposes. The comparison in FigureQ12-7 also illustrates that ground motions at the power block structures are very little different fromthe free-field control motion. The ground motions near the crest of the sea cliff are amplified atfrequencies higher than about 2 Hz (Figure Q12-6). However, the ground motions at the leftboundary (ocean side) and the right boundary (ridge side) are equal to or slightly lower than theinput free-field control motion (Figure Q12-8). Thus, the analysis indicates that topographic effectson ground motions at the location of the power block structures at the Diablo Canyon site areinsignificant.

REFERENCES

Earthquake Engineering Technology, Inc. 1983, SuperFLUSH1 Volume I - Basic Users' Guide;Volume 2 - Theoretic Manual; and Volume 3 - Verification and Example Problems: San Ramon,California.

PAGE 620oF 171fib Caeoa PowerlntLong Taom Semlc PrInramPacifPc Gas and Electric Company

GEO.DCPP.01. 29 REVISION 1Page 10irlviatAinn 111 Aveivat 10l90

2.5

2

,7,-

C0

0

I1

1.51-

I . . . I., . . I

NODE 162CONTROL MOTION

I

. . I . . .. .. I

. . . . . . ........ ... ...... [, . . . . . ..... . I

1

%I% I

.5

A

Response Spectrum (5% Damping)

. . . I . . . S . .. .1v

.1 .2 .5 1 2 5 10 20 50 100Frequency (Hz)

600

c 400

* 200 NODE 162

0

cn -200Surface Profile

-400 I * . I .0 500 1000 1500 2000 2500

Distance (ft)

Figure Q12-6

Comparison of response spectra of the control motion and computed horizontal motion at node 162.

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Figure Q12-7

Comparison of response spectra of the control motion and computed horizontal motion at node 302.

PAGE 64 OF 171Pacifc ta and Eect Companq

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Figure Q12-8

Comparisons of response spectra of the control motion and computed horizontal motions at the leftand right boundaries of the model.

PAGE 65 OF 1711 Pacic Gas a Elc Company

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