ML20213E579

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Response to Util Second Set of Interrogatories Re Reracking of Spent Fuel Pools.Equations of Motion Appear in Encl Computer Program.W/Proof of Svc
ML20213E579
Person / Time
Site: Diablo Canyon  Pacific Gas & Electric icon.png
Issue date: 11/06/1986
From: Grueneich D
GRUENEICH, D.M. (FORMERLY GRUENEICH & LOWRY), Sierra Club
To:
PACIFIC GAS & ELECTRIC CO.
References
CON-#486-1440 OLA, NUDOCS 8611130220
Download: ML20213E579 (21)
v • d • e


Text

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J446 DOCKETED UNITED STATES OF AMERICA USNRC NUCLEAR REGULATORY COMMISSION 86 A'0V 10 P4 :35 BEFORE THE ATOMIC SAFETY AND LICENSING BOARD OFF:: ._ r - -- -

C0CU F iv. y

) .

In the Matter of: ) Docket Nos. 50-275 and 50-323 O d

) ,

PACIFIC GAS & ELECTRIC COMPANY ) (Reracking of Spent Fuel Pools)

)

(Diablo Canyon Nuclear Power )

Plant, Units 1 and 2) )

)

SIERRA CLUB'S RESPONSES TO PACIFIC GAS & ELECTRIC COMPANY'S SECOND SET OF INTERROGATORIES

1. The freebody diagram is attached as Figure 1. The equations of motion appear in the enclosed computer program at lines 2790 and 2800. Moments and rotations are not included.
2. The moving mass of fuel was chosen to be that of 55 fuel elements, half the total load of the 10x11 rack. The other 55 are assumed fixed with respect to the rack base. This assumption was used by PG&E in its analysis. A.I. Soler and K.P. Singh discuss the choice of the fraction of moving fuel in more detail in " Seismic Response of a Free Standing Fuel Rack Construction to
  1. -D Motion," Nuclear Engineering and Design 80 (1984), 315-329.
3. The initial velocity used in developing the plots shown on Figure 1 was 1.0 ft/sec. The velocities for Figure 2 are listed on Figure 2 (e.g., 0.2 ft/sec.). No displacements per se were "used in developing the plots" shown on Figures 1 and 2.

The analysis did not assume a particular displacement as an input but rather assumed that displacement is such that a collision 1

8611130220 861106 PDR ADOCK 05000275 G PDR 3 Sc 3

i does occur. If PG&E wishes to determine the displacements that ,

i would occur, it can determine them with the enclosed computer l program.

4. No plots (i.e. graphs) of the displacement exist.

Velocity time histories are shown in the enclosed print-out as variables VRWX and VRWY.

5. See Attachment A.
6. The diskette is enclosed.

Dated: November 6, 1986 GRUENEICH & LOWRY By e i Dian Mi Grueneich 2

WALL mP m fLA.CL t m P-KACK ~ ~

)GtIc Tt D +J

L- =

h stR/GHT JVOKm A L-F

-f~a ArJ tm P

'.': P fh t~ L RCS6ODY .1> 18 G K A*) FO n. C04e4OCo F<4x4r 1.

l I

ATTACHMENT A There has been some discussion in the literature regarding the modelling of fluid coupling effects for the analysis of fuel rack motion. (See Ref. 1 - 4.) These effects can be described as a buoyancy effect, due to the acceleration of the pool and its contents, and a " squeeze film" or " gap closure" term arising from the differential motion of a rack relative to a neighboring wall or other rack. (Ref. 2,3)

An expression for the squeeze film effect can also be obtained from a Bernoulli principle argument as follows:

A moving rectangular object of width L, height H, speed V approaches an infinite wall bounding a fluid of density r. The wall and object are parallel and the motion is assumed normal to the surfaces.

The instantaneous separation between the wall and object is

h. As a result of the relative motion, fluid is flowing out of this space. For the purposes of this argument it le assumed that the fluid flows only the the Chorizontal) x-direction and is anti-symmetrical, so that the fluid speed at any point in the gap vCx)

=-

vC-x) and vCO) = 0. (See figure 1) The generalization for two dimensional flow results in a simple correction factor as shown in reference (2), eq 19. Given the presence of the base plates and girdle bars on the Diablo racks, the assumption of horizontal flow is perhaps more appropriate, especially for small gaps.

1

U h

1 L/, X i

i O

H v

V L

u M c a.et I.

2 1

The fluid is assumed frictionless and incompressible so that resistance to the flow is neglected.

The function vCx) can be found directly from the continuity conditions, (1) vCx + dx)Hh -

vCx)Hh - VHdx from which it follows that (2) dv/dx = V/h and vCx) = Vx/h since vCO) =0 Neglecting potential energy terms, Bernoulli says (3) pCx) + dECx)r/2 - P + v 8CL/23r/2 where P is the Cambient) pressure at the edge of the object and pCx) is the local pressure at x.

The net force on the object is then r4 2 2 ms (4) F= I CP 7= ) AA

" N $ywa (7 ~ * ;

from which we see that (5) F = rV C H/12h*

The result of equation (5) is to be compared with the expression (26) of Reference 1. This agreement is to be expected since both the Bernoulli and Lagrange arguments are based on energy considerations.

The similarity of equation (5) to that of expression (19) of Reference 2 is perhaps surprising. There are important differences, however, in that the present expression involves object velocity while that of Reference 2 involves object acceleration and was derived for small vibrations and large gaps.

The use of these expressions, whether alone or in some combination, to model the fluid coupling forces on fuel racks is still in some doubt (Ref 2, p 318). In the absence of experimental 3

verif1 cation the use of either expression in critical safety calculations raises serious questions.

4

/ / fri a s - - . 3334 'D L

.O REM /* "D3 SLIDE" COMPUTES MOTION OF RACK CONSIDERING 5 DOF */

O REM /* ROTATIONS NOT CONSIDERED */

'O REM /* STRUCTURAL DAMPING NOT CONSIDERED */

40 REM /* FLUID COUPLING NOT CONSIDERED */

hOREM/* FRICTION FULLY ACCOUNTED FOR */

30 REM /* INTERNAL MOTION OF FUEL ACCOUNTED FOR */

iOO MU = .2: GEE = 32.15 i p10 MR = C26000 + 55

  • 1616) / GEE: MF = (55
  • 1616) / GEE: MTOT = MR + MF '

B20 DELT = .001: NUMDIVS = .01 / DELT

$30 B40 KIX = 154000!

  • 12: KIY = 127000!
  • 12

$45 GAPX = .302 / 12: GAPY = .302 / 12 850 DIM EWHSTACNUMDIVS): DIM NSHSTACNUMDIVS): DIM VZHSTACNUMDIVS) 860 OPEN "I", #1. "B:EWHSTA" B70 OPEN "I". #2. "B:NSHSTA" l880 OPEN "I", #3. "B:VZHSTA" l 8

'90 ' I NOO FOR TME = .01 TO 24 STEP .01 h10 GOSUB 900

$20 '

l

$O0 REM /* CALCULATION LOOP */

$20 FOR J = 1 TO* NUMDIVS

$30 AWX = GEE EWHSTACJ): AWY = GEE

  • NSHSTACJ): AWZ = GEE
  • VZHSTACJ)

$40 *

$45 GOSUB 1400: REM /* NORMAL FORCE */

@50 GOSUB 1200: REM /* FRICTION */

I60 GOSUB 1000: REM /* FUEL ACC */

70 GOSUB 1300: REM /* RACK ACC */

80 VWX = VWX + AWX

  • DELT: VRX = VRX + ARX
  • DELT: VFX = VFX + AFX
  • DELT 90 XWX = XWX + VWX
  • DELT: XRX = XRX + VRX
  • DELT: XFX = XFX + VFX
  • DELT BOO VWY = VWY + AWY
  • DELT: VRY = VRY + ARY
  • DELT: VFY = VFY + AFY
  • DELT

%10 XWY = XWY + VWY

  • DELT: XRY = XRY + VRY
  • DELT: XFY = XFY + VFY
  • DELT

'S13 VUZ = VWZ + AWZ

  • DELT: VRZ = VRZ + ARZ
  • DELT 016 XWZ = XWZ + VWZ
  • DELT: XRZ = XRZ + VRZ
  • DELT G20 VRWX = VRX - VWX: VRWY = VRY - VWY 630 XRFX = XRX - XFX: XRFY = XRY - XFY R40 XRWX = XRX - XWX: XRWY = XRY - XWY

'@O0 NEXT J 910 PRINT USING "###.###";TME; TABC9);XWX; TABC18); VWX; TABC27) XRWX; TABC36);

VRWXS TABC45); XRWY; TABC54); VRWY 915 LPRINT USING "###.###";TME; TABC9);XWX; TABC18); VWX; TABC27) XRWX; TABC36);

V_RWX; TABC45); XRWY; TABC54); VRWY 81"Y IF TME*100 MOD 60 = 0 THEN LPRINT:LPRINT:LPRINT:LPRINT:LPRINT:LPRINT 520 NEXT TME 950 CLOSE: END 560 '

300 REM /* LOADS ARRAYS */

B10 EWHSTACO) = EWHSTACNUMDIVS): NSHSTACO) =

NSHSTACNUMDIVS): VZHSTACO) = VSHSTA (NUMDIVS) 020 INPUT #1, EWHSTACNUMDIVS): INPUT #2, NSHSTACNUMDIVS): INPUT #3, VZHSTACNUMDI

.VS) 930 FOR I = 1 TO NUMDIVS -1 940 EWHSTACI) = CI / NUMDIVS)

  • CEWHSTACNUMDIVS) - EWHSTACO3) + EWHSTA'CO) 950 NSHSTACI) = CI / NUMDIVS)
  • CNSHSTACNUMDIVS) - NSHSTACO3) + NSHSTACO)

,960 VZHSTACI) = CI / NUMDIVS)

  • CVZHSTACNUMDIVS) - VZHSTACO3) + VZHSTACO) 970 NEXT I 980 RETURN 990 o 1000 REM /* FRICTION CALCULATIONS -- RETURNS WITH FRX, FRY */

'1005 MUNORM = MU

  • FRZ

7 k

T 10 VRWXY - SOR(VRWX^2 + VRWY^2) 20 IF VRWXY > .0001 THEN GOSUB 1050 ELSE GOSUB 1110 e40 RETURN s 50 REM /* RACK SLIPPING */

60 FRX = - MUNORM

  • VRWX / VRWXY: FRY = - MUNORM
  • VRWY / VRWXY

$70 RETURN 380 * ,

390 '  !

100 REM /* RACK NOT YET SLIPPING */

110 FRE0X = MR

  • AWX + FFX: FRE0Y = MR
  • AWY + FFY 120 FREQXY = SQRCFREQX^2 + FREOY 2) 130 IF FREQXY > MUNORM THEN RATIO = MUNORM / FRE0XY ELSE RATIO = 1 l 140 FRX = FREQX
  • RATIO: FRY = FREQY
  • RATIO '

150 RETURN 200 REM /* FUEL ACCELERATION CALCULATIONS a/

210 REM /* CALL BEFORE FRICTION CALCS */

220 IF ABSCXRFX) - GAPX < 0 THEN FFX = 0 ELSE FFX = KIX

  • CABSCXRFX) - GAPX)
  • jGNCXRFX)

[230 IF ABSCXRFY) - GAPY < 0 THEN FFY = 0 ELSE FFY = KIY

  • CAESCXRFY) - GAPY) *S iNCXRFY) 240 AFX = FFX / MF: AFY = FFY / MF l 250 RETURN  ;

300 REM /* RACK ACCELERATION CALCULATIONS */ l 310 REM /* CALL FUEL ACC AND FRICTION CALCS FIRST */

320 ARX = CFRX - FFX) / MR: ARY = CFRY - FFY) / MR: ARZ = FRZ / MTOT - GEE l 330 RETURN 400 REM /* NORMAL FORCI CALCS */

410 FRZ = MTOT

  • CAWZ - GEE) 420 RETURN

XW VWX xwX vwx xgoY dy

{

m. U t) U+/s) (s v) Gun (e t ) cws l O.030 0.000 0.000 0.000 -0.000 o . . ,0 0 0.000 0.020 -0.000 - 0. O u O.000 0.000 0.000 0.000 0.030 -0.000 -0.030 0.000 0.000 0.000 0.000 ,,

J O.040 -0.001 -0.050 0.000 0.000 0.000 0.000 b yf4 f a r__

O.050 -O.001 -0.069 O.000 O.000 O.000 0.000 O.000 -0.002 -0.007 O.000 O.000 O.000 O.000 gar p u. i-- 1 0.070 -0.003 -0.105 O.000 O.000 O.000 O.000 -

(

O.060 -0.004 -0.121 0.000 O.000 O.000 O.000 i O.090 O.100

-0.005

-0.007

-0.136

-0.150 0.000 O.000 O.000 O.000 O.000 O.000 O.000 O.000 g g/f ' g g/ K ,v I

O.110 -0.008 -0.163 0.000 O.000 O.000 O.000 'p O Dl dl6 F MN 1

O.120 -0.010 -0.174 O.000 O.000 O.000 0.000 y E W.

O.150 -0.012 -0.184 0.000 O.000 O.000 O.000 g/o c. ;p/*

O.140 -0.014 -0.192 O.000 0.000 O.000 O.000 O.150 -0.016 -0.199 0.000 O.000 0.000 0.000 O.160 -0.018 -0.204 0.000 O.000 O.000 O.000 N2 E e N b O.170 -0.020 -0.207 O.000 O.000 O.000 O.000 m p. ,(:sp.v ve.l 0.180 O.190

-0.022

-0.024

-0.209

-0.210 O.000 0.000 0.000 O.000 O.000 O.000 O.000 O.000 Pd "

E LJ N/

O.200 -0.026 -0.21O O.000 O.000 O.000 O.000 0.210 -0.028 -0.209 O.000 O.000 0.000 0.000 -

O.220 -0.030 -0.207 O.000 O.000 O.000 O.000 O.230 -0.032 -0.204 O.000 0.000 O.000 O.000 K k W 'I" , M " 'I O.240 -0.034 -0.201 0.000 O.000 O.000 0.000 g g, s, 9 9. vej [

0.250 -0.036 -0.197 O.000 O.000 0.000 O.000 i O.260 -0.038 -0.192 O.000 O.000 O.000 -0.000 r C I ed t*' C E [* *

  • I O.270 -0.040 -0.188 0.000 O.000 O.000 -0.000 g/ g-O.280 -0.042 -0.183 0.000 0.000 O.000 -0.000 0.290 -0.044 -0.179 0.000 0.000 O.000 -0.000 0.300 -0.046 -0.174 0.000 0.000 0.000 -0.000 O.310 -0.047 -0.170 0.000 0.000 0.000 -0.000 O.320 -0.049 -0.166 0.000 O.000 O.000 -0.000 O.330 -0.051 -0.162 O.000 O.000 O.000 -0.000 O.340 -0.052 -0.158 0.000 0.000 O.000 -0.000 O.350 -0.054 -0.154 0.000 0.000 O.000 -0.000 O.360 -0.055 -0.149 O.000 O.000 O.000 -0.000 O.370 -0.057 -0.145 O.000 0.000 O.000 -0.000 0.380 -0.058 -0.139 O.000 O.000 O.000 -0.000 O.390 -0.060 -0.133 O.000 0.000 O.000 -0.000 O.400 -0.061 -0.127 O.000 O.000 O.000 -0.000 0.410 -0.062 -0.120 0.000 0.000 0.000 -0.000 O.420 -0.063 -0.113 0.000 O.000 -0.000 -0.000 O.430 -0.064 -0.104 O.000 O.000 -0.000 -0.000 O.440 -0.065 -0.094 O.000 O.000 -0.000 -0.000 O.450 -0.066 -0.082 0.000 O.000 -0.000 -0.000 O.460 -0.067 -0.068 O.000 O.000 -0.000 -0.000 O.470 -0.068 -0.053 O.000 O.000 -0.000 -0.000 O.480 -0.068 -0.036 O.000 O.000 -0.000 -0.000 O.490 -0.068 -0.018 0.000 O.000 -0.000 -0.000 0.500 -0.068 0.001 0.000 -0.000 -0.000 -0.000 O.510 -0.068 0.022 0.000 -0.000 -0.000 -0.000 0.520 -0.068 0.044 0.000 O.000 -0.000 -0.000 O.530 -0.067 0.066 0.000 0.000 -0.000 -0.000 0.540 -0.067 O.007 -0.000 -0.009 -0.000 -0.005 O.550 -0.066 O.109 -0.000 -0.021 -0.000 -0.015 O.560 -0.064 O.131 -0.000 -0.039 -0.000 -0.026 0.570 -0.063 0.154 -0.001 -0.056 -0.001 -0.036 O.580 -0.061 O.177 -0.002 -0.066 -0.001 -0.042 O.590 -0.059 O.197 -0.002 -0.063 -0.001 -0.040 0.600 -0.057 O.217 -0.003 -0.044 -0.002 -0.028

NM )( W X VWX gg M)( VWX XRWY M7 .

O. 630 -0. OM U.235 -O.003 -0.007 -O.002 -0.004 O.a 20 -O.053 O.252 -0.003 -O.012 -0.002 -0.006 0.630 -0.056 0.264 -- O . 0 0 3 O.002 -0.002 v.001 O.640 -- 0 . 0 4 7 O.283 -O.003 O.003 -0.002 O.004 O.650 -0.044 O.295 --0.003 O.001 -0.002 v.010 O.660 -O.041 O.304 -0.003 -0.005 -O.002 -0.007 0.670 -0.030 0.311 -0.003 -0.000 -0.002 -0.004 O.600 -0.035 O.317 -0.003 -0.000 -0.002 -0.001 O.690 -0.032 O.322 -O.003 O.001 -0.002 0.001 0.700 -0.020 0.325 -0.003 0.000 -0.002 0.003 0.710 -0.025 0.325 -0.003 -0.003 -0.002 0.005 0.720 -0.022 0.321 -0.003 -0.007 -0.002 0.006 0.730 -0.019 0.313 -0.003 0.003 -0.002 -0.008 0.740 -0.016 0.303 -0.003 0.003 -0.002 -0.001 0.750 -0.013 0.290 -0.003 0.000 -0.002 0.004 0.760 -0.010 0.277 -0.003 0.011 -0.002 0.001 0.770 -0.007 0.264 -0.003 0.005 -0.002 -0.003 0.780 -0.005 0.252 -0.003 0.000 -0.002 0.001 0.790 -0.002 0.240 -0.003 -0.005 -0.002 0.006 0.800 -0.000 0.230 -0.003 0.006 -0.002 -0.006 0.810 0.002 0.220 -0.003 0.009 -0.002 -0.003 0.820 0.004 0.210 -0.003 0.006 -0.002 -0.000 0.830 0.006 0.202 -0.003 0.017 -0.002 -0.001 0.840 0.008 0.193 -0.003 -0.004 -0.002 -0.000 0.850 0.010 0.183 -0.003 0.009 -0.002 -0.000 0.860 0.012 0.170 -0.003 0.007 -0.002 0.000 0.870 0.014 0.155 -0.003 0.009' -0.002 0.001 0.880 0.015 0.141 -0.003 0.006 -0.002 0.001 0.890 0.016 0.130 -0.002 0.017 -0.002 0.002 0.900 0.018 0.121 -0.002 0.014 -0.002 0.001 0.910 0.019 0.112 -0.002 -0.004 -0.002 -0.000 0.920 0.020 0.102 -0.002 0.008 -0.002 0.001 0.930 0.021 0.091 -0.002 0.004 -0.002 0.001 0.940 0.022 0.078 -0.002 -0.005 -0.002 -0.001 0.950 0.022 0.063 -0.002 0.010 -0.002 0.007 0.960 0.023 0.045 -0.002 0.010 -0.002 0.005 0.970 0.023 0.022 -0.002 0.011 -0.002 0.006 0.980 0.023 -0.002 -0.002 -0.005 -0.002 -0.002 0.990 0.023 -0.027 -0.002 -0.003 -0.002 -0.000 1.000 0.023 -0.050 -0.002 -0.001 -0.002 -0.000 1.010 0.022 -0.078 -0.002 0.004 -0.002 0.001 1.020 0.021 -0.111 -0.002 0.014 -0.002 -0.003 1.030 0.020 -0.148 -0.002 0.005 -0.002 0.001 1.040 0.018 -0.186 -0.002 -0.002 -0.002 -0.000 1.050 0.016 -0.223 -0.002 0.014 -0.002 0.000 1.060 0.014 -0.255 -0.002 0.002 -0.002 0.001 1.070 '

0.011 -0.283 -0.002 0.009 -O.002 0.003 1.080 0.008 -0.311 -0.002 -0.006 -0.002 -0.001 1.090 0.005 -0.342 -0.002 0.002 -0.002 0.000 1.100 0.001 -0.376 -0.002 0.012 -0.002 0.004 1.110 -0.003 -0.411 -0.002 0.002 -0.002 0.000 1.120 -0.007 -0.447 -0.002 0.010 -0.002 -0.008 1.130 -0.012 -0.484 -0.002 0.003 -0.002 0.001 1.140 -0.017 -0.517 -0.002 -0.001 -0.002 -0.000 1.150 -0.022 -0.547 -0.002 -0.001 -0.002 -0.000 1.160 -0.028 -0.574 -0.002 -0.001 -0.002 -0.000 1.170 -0.034 -0.597 -0.002 -0.001 -0.002 -0.000 1.180 -0.040 -0.618 -0.002 -0.001 -0.002 -0.000 1.190 -0.046 -0.636 -0.002 -0.001 -0.002 -0.000 1.200 -0.052 -0.650 -0.002 -0.001 -0.002 -0.000

m

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r QUALIFICATIONS OF DR. RICHARD B. FERGUSON Dr. Ferguson is a professional physicist, Vice-Chairman and Conservation Chairman of the Sierra Club, Santa Lucia Chapter, and a Pacific Gas & Electric Company ratepayer. He received a Bachelor of Arts degree, cum laude, from Amherst College, Massachusetts in 1960 and a Ph.D. in physics from Washington University, St. Louis, Missouri in 1967. Dr. Ferguson taught on the physics faculty of the University of California at Los Angeles from 1967 to 1970 and of California Polytechnic Univer-sity at San Luis Obispo from 1974 to 1984. He resides in San Luis Obispo County at Rocky Canyon Star Route, Creston, Califor-nia 93432.

On behalf of the Sierra Club, on February 10, 1986, he requested a hearing and filed a petition for leave to intervene in the NRC proceeding related to PGGE's request for a license amendment to permit reracking of the spent fuel storage facili-ties for the Diablo Canyon nuclear power plant. The Sierra Club filed its petition because of its concerns about the environment and public health and safety.

PROOF OF SERVICE Of.

I, Deborah M. Hunt, declare that on November 6, 1986, I deposited copies of the attached Sierra Club's Reggo g 4)ty gggific Gas & Electric Company's Second Set of Interrogator:.es in the United States mail with postage thereon fully prepaid and addressed to the parties listed below: CFF!Cf. < ui 00CKEli% r. seacI Dr. Jerry Harbour Mr. Leland M. GustaINhn, Administrative Judge Federal Relations Manager Atomic Safety & Licensing Board Pacific Gas & Electric Co.

U.S. Nuclear Regulatory Comm. 1726 "M" Street, NW, Suite 1100 Washington, D.C. 20555 Washington, D.C. 20036-4502 Glenn O. Bright Philip A. Crane, Jr., Esq.

Administrative Judge Pacific Gas & Electric Co.

Atomic Saiety & Licensing Board P.O. Box 7442 U.S. IMclear Regulatory Comm. San Francisco, CA 94120 Washington, D.C. 20555 Mr. Gordon A. Silver Henry J. McGurren, Esq. Ms. Sandra A. Silver Lawrence J. Chandler, Esq. 1760 Alisal Street Office of the Exec. Legal Dir. San Luis Obispo, CA 93401 U.S. Nuclear Regulatory Comm.

Washington, D.C. 20555 Ms. Laurie McDermott, Coordinator Atomic Safety & Licensing C.O.D.E.S.

Board Panel 731 Pacific Street, Suite 42 U.S. Nuclear Regulatory Comm. San Luis Obispo, CA 93401 Washington, D.C. 20555 Mrs. Jacquelyr. Wheeler B. Paul Cotter, Jr., Chairman 2455 Leona Street Administrative Judge San Luis Obispo, CA 93400 Atomic Safety & Licensing Board U.S. Nuclear Regulatory Comm. Dr. R.B. Ferguson

. Washington, D.C. 20555 Sierra Club / Santa Lucia Chapter Rocky Canyon Star Route Atomic Safety & Licensing Creston, CA 93432 Appeal Panel U.S. Nuclear Regulatory Comm. Ms. Nancy Culver Washington, D.C. 20555 192 Luneta Street San Luis Obispo, CA 93401 Bruce Norton, Esq.

NORTON, BURKE, BERRY & FRENCH P.O. Box 10569 Phoenix, AZ 85064 I am, and was at the time of the service of the attached paper, over the age of 18 and not a party to the proceeding.

I declare under penalty of perjury that the foregoing is true and correct.

i _C .

Ueborah M. Hunt

._ ---

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