ML20116B157

From kanterella
Jump to navigation Jump to search
Svc Water Through Wall Flaw Evaluation
ML20116B157
Person / Time
Site: Point Beach  NextEra Energy icon.png
Issue date: 07/19/1996
From: Jun Lee, Newton M
WISCONSIN ELECTRIC POWER CO.
To:
Shared Package
ML20116B150 List:
References
96-0149, 96-149, GL-90-05, GL-90-5, NUDOCS 9607290120
Download: ML20116B157 (15)


Text

-

NUCLEAR POWER BUSINESS UNTT CALCULATION REVIEW AbV APPROVAL I - Calculation #

ih-O/V9 Nurnber of Pages om sarer +

6 + 9 Arracume,tr Title of Cniculatica: (a sac 8 $ttatLE wATtK ~rutouGB coa LL LCM tvA Lu AT tre rJ ji( Original Calculation ,E[ QA-Scope O Revised Calculation. Revision #

D Superseding Calculation. Supersedes Calculation #

Modification #

Description:

N/A "YA I Other

References:

wepc. prer g sracn acuet .ac acoo2.3 f g ., . s, z g r,4T  % '/ 56 7

m . A . v CwteeJ *Tuty 19 1996 This Calculation has been reviewed in accordance with NP 7.2.4. The review was accomplished by one or a combination of the following (m: checked):

A review of a representative san:ple of repetitive N A detailed review of the original calculation.

calculations.

A review of the caleu!ation against a similar A nylew by an alternate, simplified, or calculation previously performed. approximate method of calculation.

! Comments: y YfG I

l i

Dste: A roved B . Date: 4 Reviewed By:

Y Yy h Y Gjt " b ~ l'? /ff%

QUf~ !**

V 1M i,s ps N 60s Refence(* FP7.24  ;

Revision 1 02/27/95 j f

9607290120 960719 PDR ADOCK 05000266 P PDR l I

4-CALCULATION SHEET d Shut No.1 of 5 )

. Refers to : Calc 96-0149 Service Water Made by _f . w. Date suv it 1914 l Throuah Wall Flew Evaluation Checked by -r. w G Date r / s9 in {

l PURPOSE: The purpose of this calculation is to document the acceptability proposing a non-code temporary repair to piping with a through wall piping leak in the service water system. The piping is 6 inch, schedule 40, ASTM A106 grade B. It is the service water supply to the decontamination area and is not typically in service.

This acceptability is based upon the criteria of Nuclear Regulatory Commission (NRC) Generic Letter 90-05 as detailed below. This method may only be used for piping flaws. l l

ASSUMPTIONS: 1) The wall thinning conditions are documented on the attached sketch.

I 2) The wall thinning has resulted in a through wall leak.

l

3) The piping item is carbon steel or low alloy steel.
4) The piping is ASME Section XI code class 3.

l 5) The piping is ferritic or austenitic stainless steel.

6) The flaw has originated from the inside diameter of the piping.

[

REFERENCES:

a) NRC Generic Letter 90-05, Guidance for performing temporary non-code repair of ASME code class 1,2 and 3 piping.

l b) USAS B31.1 - 1967, Power Piping c) ANSI B16.9 Factory-Made Wrought Steel Buttwelding Fittings d) WEPCo piping stress analysis report, WE-300023 e) As noted elsewhere in this calculation.

ATTACHMENTS: 1) Nondestructive Evaluation Report of wall thinning and location,1 page  ;

2) Bending stress documentation,8 pages. I l

l lNPUTS,; 1) As documented in the calculation section.

CALCULATION: Flaw Evaluation using the "Through-Wall Flaw" Aporoach '

Terms and Variables; ,

tnom = design nomincl thickness of the piping item R = pipe outside radius

' min = calculated minimum wall thickness for the piping item determined from the ASME B31.1 -1967, section 104.1.2 P = design pressure SE = Sh = stress allowable at design temperature Ac = corrosion allowance y = thin wall approximation coefficient Do = nominal outside diameter of pipe d = nominalinside diameter of pipe K = stress intensity factor F = geometry factor Ta = 2a, total flaw length. The total flaw length,2a,is determined as the maximum length of the portion of the fiaw that extends below tmin independent ofits orientation on the pipe.

i a = one half of the total flawlength, s = stress at the flaw location. s is determined considering the maximum combination of desoweight, pressure, thermal expansion and safe-shutdown earthquake (SSE). I A, B, C factors in the calculation of the geometry factor F l c = the ratio of a to x*R l r = the ratio of R to tmin Pc = pipe circumference

1

. t

]

CALCULATION SHEET  !

Shsst No. 2 of 5 ,

Refers to : Calc 96-0149 Service Water Made by m r . Date am is atts l

Throuah Wall Flaw Evaluation Checked by Date I I

Flaw aeometry lt i

J l

l l

1 o

)

I I

i Service Water 6 inch Elbow and Approximate Flaw Location i

)

i J

0.5 in 0.5 in  :
l I 0.156 in -+ ~

+--0.25 in--+

u ,,

a-tmin. 0.092 in f

' 's 4'

/ 's 0.169 in 0.225 in \

0.257 in s 0.249 in

/

,f 1'

[ ,

/  :

/ \

'A

,,_ i j

i Flaw Profile i

i

5 -

1 CALCULATION SHEET Shut No. 3 of 5 Refers to : Calc 96-0149 Service Water Made by . ,_, . Date emv is i99c l Throuah Wall Flaw Evaluation Checked by Date Term values; tnom :=.280 inches Do := 6.625 inches P := 120 psi l Ac := 0.065 inches, conservatively added y := 0.4 SE := 15000 psi, ASTM A106 Gr. B, <650 degrees F, from USAS B31.1-1967 D

unin :: Ac tmin = 0.09142 inches 2 (2-(SE + P y))

]

R := b *

  • R = 3.1725 inches 2 2 Ta := 0.25 inches I 2a, or Ta noted above, was determined in this case by assuming the variation in wall thickness l

from the closest scale point to the center of theleak ( 1/4 inches away) is linear. The wall thickness at 1/4  ;

inches from the center of the flaw is nominally 0.197 inches. Minimum wall thickness, tmin,is about half i of this thickness so it is estimated that the total length of the flaw which is less than tmin is 1/4 inches.

This dimension is the total flaw size 2a.

a := 3 a = 0.125 inches  !

2 s := 1420 psi, from WEPCo piping stress report WE-300023. Node points A10 and A20 represent the elbow ends. 3 The elbow has a stress intensification of 2.27. The stress value is calculated using ASME Section 111-1978 equation 9C and is the maximum value for the elbow location.

d

[ a STEP 1: Generic Letter 90-05 Limitations if flaw length 2a exceeds either 3 inches or 15 percent of the length of the pipe circumference, the flaw is not acceptable by this appraoch.

Ta := 0.25 inches Pc := 2 n R Pc = 19.93341 inches L := 0.15-Pc L = 2.99001 inches i

el F:

f 4;

CALCULATION SHEET Shut No. 4 of 5 Refers to : Calc 96-0149 Service Water - Made by r. -re., Date sua at 11L Throuah Walt Flaw Evaluation Checked by Date f

STEP 2: Evaluation of Geometry Factor, F  ;

e:=- - c = 0.01254 nR .

r= r = 34.70419 l tmin 2 3

A
= (- 3.26543) + (l.52784 r)- (0.072698 r ) + (0.0016011 r )

2 3 l '

B := (11.36322)- (3.91412 r)+ (0.18619 r )- (0.004099 r ) l 2 3 C :=(- 3.18609) + (3.84763 r)- (0.18304 r ) + (0.00403 r )

i A = 29.12222  !

i B --71.55564  ;

) i C = 78.33509 i F := 1 + (A cla) + (B.c23) + (C c #)

3 j

} F = 1.03966 STEP 3: Evaluation of Stress Intensity Factor, K I K := 1.4 s F-(n a) #

3 "

K = 1.2952 10 psi K = 1.3 ksi l

For ferritic steel, the calculated stress intensity factor K should be less than i 35 ksi* square root inch, which is consistent with the lower bound fracture toughness propertyin ASME code case N-463.

For austenitic stainless steels, the calculated stress intensity factor K should be less than 135 ksl* square root inch, which is consistent with the lower bound fracture toughness property used in Article IWB-3640 of ASME Section XI.

1 If the above requirement is not met, this approach cannot be used.  !

l l

k e

'l

CALCULATION SHEET -

6 Shset No. 5 of 5 Refers to : Calc 96-0149 Service Water Made by r .. r s ~ _ Date mv #1 sf fC Throuah Wall Flaw Evaluation Checked by Date 1

RESULTS:

The result of this calculation is that the stress intensification factor K calculated for this piping flaw is less than the fracture toughness value lised in NRC Generic Letter 90-05.

This result is based upon the calculations detailed above subject to the assumptions made in this evaluation.

i CONCLUSIONS:

I The piping flaw meets the criteria of NRC Generic Letter 90-05 "Through-Wall Flaw" approach. l A temporary non-code repair may be proposed.

l l

l l

l l

h t

1 i

{ .

i i

.. JUL-18-98THU14:59 'PBNP SECURITY FAX NO. 414 755 6583 P.02/02 catc . 16 o#9 9 ,

AttAcN g,, r A

  • P Ac. ( p or 9

.nsr

\x ._

N i

.- .nst

._ .225"

-\.

hstaz ,

nr /

/_ .4.r

,_ .249"

_ .243-I

~

SPECIFICAT10NS WISCONSIN ELECTRIC C4.CKED BY TITLE SERVICEWATER xsrm n m .= , , u ..<

= rsa a x,,,,,,,,,,,

)

\

, {ALb 96 0199 A*ris cu mE uT A l l

'PAGC 1. OP R .

, , ;, 7 .. .

. . . p g .: ;, r . .-

.r- <

l 3 :;. ;E',  ; ; '. 5; ; .. 0;;c?";;t;;: r ;;;:P :: E , , ;; , ..  ;; 2 . .

r , '. 47/ E ';',. M E:

c.- E;: : ( ','. . ? H '

5. . . . ' . ' . . ' . . :" ' ;oN E:::: 5'; E A
.; ..r

.. . ~ v. ; : % . . :

i 1

. 5&EGEN1 E'O LYD7 ENGINEERS .

. IN*EGaATE3 PIPING ann6 YSI5 3E05::M e

. PIP 5YS/PC FIP037026140 .

. PRCGRAM EATE JUN 22, 1990 14:39:05 1

. .. . ................. 1 1

~ l NUCLEAR CL ASS 2 5'GE55 AN8 LYSIS 04/15/91 l IN ACCORDANCE WITH $ECTION ;I*, DIV;$10N 15'.05EC11CN N: OF THE ASME COILER AND PRE 55 LEE VESSEL CD E WINTER 1975 AD0ENDA P.114 ZONE C.7 BRAN;H A l 1

l

... CONTENTS OF FILE 13 ...

LCAD DATE COMMENT, DATA 04/15/91 WEPCD SERVICE WATER W1 1 04/15/91 DEAD WEIGH 1 }

DI 1 04e25/91 SEISMIC ANCHOR MOVEMENT 5 2 SE 1 C4/15/91 OBE Y Y ANALYSIS 3 SE 2 04/15/91 CBE Y 2 ANALYSIS 4 i

MAXIMUM NUMCER OF ANALYSES THA1 CAN EE SAVED FCR THIS SLD5Y5?EM 25 20

', t.'s,? ... .. . 1 ~
r ' .j
t .: ,1 . .>, ',

5:;;EN* C.v0Y ENGINEED5  ::.'.1.:" N'. ;3(? cie;;: FA;34: ::~r '..i. .'C ;4 :" -

. S':E55 : (N; !6CC) E V A . '. I ' ' . '. . .E*;1'; C:5;; ;*:E5.

.;;4 E NE C.* Es:N;w &

2N291 ;4f &Ma'; * .N F CR 5'8 Ei5 ' .S* ~ '.'. ~

i r aa. -.r iren -e c,--.r +  ::- ce"r rr : .e r r~:r :5 :r .

- r:

CALC 96-O/47 NrTAc e cyv A ,

'PAGE .7 O F 9 l

. , , . :, e . . s . w . v . .i .,s;,... - .i l

Sc; GEN' ttvDY EN0; NEE &5 8 4 %; " M '.: . O'J03Nic;;: ;45 ' ~v . '. ii. . eu ;;:?ini 51aE55 C (NC.36001 Evai'.I' ; e :r MN D:5:5 ';E5: i P.;;c Z;NE C.? CD:N'N

  • l
Navi sv::Mm:N rca 5 aE55 . ::. :

l LCAO TI1LE LCAD ID i:8D '";E *E";EE 1'.*E

."UL T r' ; . SAVE 72rE LAL E

' u f 4 '*:. . . 5

)

CEAD WEIGHT W5H1 W 1.00 WT 1 SAM CBE SAMO J 1.00 DI I SAM 55E SAMS D 2.00 DI 1 OBE X.Y RESPONSE CBWY  ? 1.00 SE 1 CBE Y.Z EESPONSE CBY: 3 1.00 SE 2 SSE X.Y RESPONSE 55%V D

^

2.00 SE 1 SSE Y.Z AESPCNSE 55YZ 2.00 SE 2 ZEGO THERMAL t10DE ZE;C i 0.00 lH 0 70. 0 1

PAE55VRE MCDE DalA NO:E ND TITLE ID END PGE55 LEE (PSI)

....................................'..Si 21 ..... ............... .. .

1 CPERA11NG PRE 55LAE CP45 8tt '6.

2 DESIGN PRE 55 LEE CP25 8.L 125.

l ALLOWEBLE 51RES'.c5: .

'..ia:NED LOADS 15000. PSI l OCCASIONAL LCADS SE 61CE LEVEL A/B 15000. P5I OCCASIONAL LOADS SERVICE LEVEL C 27000. PSI i i

OCCASIONAL LOADS SERVICE LEVEL D 36000. PSI 1HERMAL EXPANSION R ANGE 5 A.F e(1.25 5C.O.25eSH) 22500. PSI 1HERMAL EXP ANSION R ANGE . SU5T AINED LOAD 5 SA 5H 37500. PSI

, STRESS GEDUCTION FAC10R F 1.00 LCAD CCMBINATION INFORMA1]CN ND. SL E;UATION LCAD COMBINATION I B DPRS. WGHT 2 B 9 . OPAS. WGH1. CBXY. SAMO 3 0 9 . D825. WGH1. OBYZ. SAMD A C 9 .

DPRS. WGH1 55XY. SAMS

. , ,a':,T i...... .;i ?: .'  :: , . r: g a., ;, s . .~ . .

, . c-

  • r  ;  ; .  ;;&;. W ye* . . ..

i t'.. .'

l l

l .

l l .

l cAcc 96 0/4tT A v v Ac W r= & T A j

  • PAGE 4 of 9  !
, , :.! e.:'.; : ;f Yo .'  ::. ;?:c .; .! : r. ;;: ,q .
  • j i

i l

l i

pn5EN' r. WOY E4MNEE25 PG';5 M ';3. P;PC17(26 40 DAC*EAP 03'E .J.N 22. ; HC !4:3 r:e

  • 51;E55 C (40-3600) EV A d' A1 * ;'; * ;E5 GN CASIS SicE55 l P.1:4 L*,NE t ' Cal';*H A , j N'4L E A4 "LA55 2 51EESS AN:t<H S PAXIF'# 4%E POINT STEE53E5 at; PSI 191 N 51EE55ES IN PSI " $ED CN NC.!650 I N;CE FACTC4 EQ (s) EC (!) E2 (?) EG (9) EQ (10) E2 (11) >

DESIGN LEVEL C LEVEL C LEVEL D L EVEL A.C LEVEL A.D  !

.. ..... ...... ............................ ....................................... i

[

A10 2.,27 $58, 1120 1370. O. O. O. PA55 i .

  1. 20 2.27 739. 1080. 1420. O. O. O. PASS A25 1.00 913. 1210. 1500. O. C. O. PASS A30 2.27 S03. 1560. 2320. O. C. O. PASS i

A40 2.27 773. 1610, 2450 O. O. O. PASS  :

845 2.27 755, 1670. 2550. O. O. O. PASS l A55 2.27 762. '1750. 2740 O. O. O. PASS  !

A60 d.27 540, 1850, 2930. O. O. O, PA55 )

A70 2.27 912. 2040. 3170. C. O. O. PASS 732, 1610, l A75- 1.00 2480. O. C. O. PASS j ASO 2.27 779, 2330, 3330, O. O. O. PASS I A90 2.27 746, 2340. 3930. O. O. O. PA$5 A95 1,79 744, 1980. 3220. O. O. O. PASS A105 1.79 625. 1570. 3050 0. O. 0. PASS l

Allo 1.00 834 1700. 2560. O. O. 0. PASS A115 1,79 705. 1540 2970 O. O. O. PASS A125 1.79 873. 2030 3190. O. O. O. PASS Al3o 2.27 768. 2340. 3920. O. O. O. PASS A140 2.27 725. 2220. 3710 O. O. 0. PASS A145 2.27 946, 1530, 2820. O. O. O. PASS 8155 2.27 1260. 2440. 3620. O. 0, 0. PASS l

l l

l.

3 i .. ..;,v.... . .; 1 ,i ra .a tri ;. ' .

  • v . 9 j 4

18:5EN* 8 .Y;F f';};NEED;. * * * ; ; * * *. * . P

  • rs ? '* *;*. M** .3*- *
  • !.*
  • Ee : ; ;N* !tCC) E *. A . '. A * . *. *. * ;E!;;.N E* Q. 1 ;;*:, E .' .

G.;;4 ;Nr ;. cs84;9 8

cAic 96-0W9 An Acerw t A 74c,c r os- 9

.e ...'.; . U '. ? " . : . . . , .

. ,, : -- :;*;E .1 ;[r;.

;;4 s-..'-
[:c,;.  ;: r:
  • j' 4' O 4  ; ; "..C C . . C .
  • c ' '

a  ; 2 C C 0

, 15.579 .3~5 ;4.COC la' D!;E

F-
' . . 72.145 .it0 t.t25 6 A;PC

, 3 i?t.C?? . 4CC 6.625 6'- 1W117 V"..

! F1 ; 4 221.000 . 4CC 6.625 6' IW326 :.~'

r. 5 00CC C000 .1...;

c5 .CCCC ':

~C  :;0 s 0 15

  • - s15 c .00C0 1. 4 NC -2.5BC0 0 750 15 20 s 0 125 ..

"3 i5 i s

3.$750 .CCCC .0000 0 :15 [

4 t;r 0 25 is :3b

40 0 3.8750 .CCCO .CCCC 0 "5C f.2 5 16 9 0 350 1- 45 9 0 A35 13 A50 0 .0000 -2,3300 .0000 0 750 335
9 A55 9 0 #65 20 &60 9 0 A50 21 865 0 .71C0 7100 .00C0 0 750 850 22 A70 9 0 A75 23 A75 1 .0000 -2.7100 .0000 001000 A65 90 19-N-24) 24 ABO 9 01C000 A75 HC 19 w-1(.B 25 ABS 0 .CC00 1.;700 .0000 0 750 A75 26 190 9 0 A95 27 A95 7 0000 0000 .9800 0 ABS
3 A105 7 00C0 0000 .6800 0 A95 29 Allo J 0000 0C00 .B500 110C00 A105 H9 19-5 651 30 A115 7 00C0 0000 .5C00 0 Allo 31 1125 7 0000 .C000 1.3400 0 A115 32 8130 9 0 A125 33 A135 0 .000C .C000 1.'50) 0 75C A125 34 Also 9 010000 A150 JD 2-H-35A 35 8145 9 0 A135 36 A150 0 0000 7.0000 .0000 0 750 A135 37 A155 9 0 A160 36 A160 1 0000 .0000 2.0000 010000 A150 JB 2-H-35 39 A165 1 0000 0000 4.6675 0 A160 40 A170 1 0000 0000 4.6675 0 A165 41 A175 1 0000 00C0 4.6675 0 A170 42 Alto 1 000J 0000 4.6f75 010000 A175 JB 2-H-36 43 f,155 .0000 0000 3.5300 110C00 44 1 AISO JD-2-5-653 E A190 9 000000 A155 JD-2-5 653A. 5/6' 01D X f. Y '

45 A195 0 0000 0000 4.6700 0 750 A385 46 8200 9 0 8205 47 8205 4.7500 .0000 .0000 C1:000 1 A195 JB-2.H-37 45 A210 1 4.$350 .0000 .0000 0 A205 49 A215 9 0 A210 50 A220 0 5.5850 0000 .0000 0 750 8210 51 5225 9 0 A230 52 A230 I 0000 i.3!00 .0000 101000 A220 JB 2 N-246 53 A235 7 0000 4.6700 .0000 111111 A230 JB 2-REPCC-471 54 8240 1 1.5000 00C0 .0000 0 AS 55 8245 1 1.5000 0000 .0000 0 A5

!6 1 AS A10 1 2 57 2 A10 A20 1 2 AIS 55 3 A20 A25 1 2 u; ,.;,.. , 7- ...m..'-

f

. 4 et 5 :!C ::C . . :"

t; 4' ~45 ti

(' ;45  ?!S

"I L3 i L55 at0 ,

I

% 'ce 1 1. Xw .- .ccco O AS

% 1 A5 A10 1 2

. .- 57 2 A10 A20 1 2 AIS 50 3 A20 $25 1 2

. l l

i I C A L.c 9 6 - 0 1 4 9 1 i

A TTA CN MCt/T b l PAQC & or 9

. ..,,.. , . .t. . . -

r. 4 1;5 :30 i c:  : :. !c 2 4,? - :"

t! ISO I45

(- Aar ;i5

  • c; . , :r f3 f :St ;f0 . i to k tto L7C 1 i i5 65 10 A7C ;75 , 2 f6 11 A75 ISO 1 i 12 830 "90 67 2 50 te 13 A90 A95 I J 69 14 895 A105 1 3

'O 17 A105 8110 1 2

?! 18 Allo A115 1 i

?? 19 A115 A125 1 4 73 12 A125 A130 1 2 74 23 4130 8140 1 2 8135 75 24 4140 A145 1 2 76 25 A145 A155 1 2 A150 77 26 A155 A160 1 1 78 17 8160 A165 1 2 79 28 A165 Al'O 1 2 80 29 A170 A175 1 2 el 30 A175 AISO 1 2

$2 31 A180 A185 1 2

$3 32 AIS5 A190 1 2 54 33 A190 A200 1 2 Ali5 55 34 A200 A205 1 2 f6 35 A205 A210 1 2 1 57 36 A210 A215 1 2 l SS 37 A215 A225 1 2 A220 l 89 33 A225 A230 1 2 90 39 A230 A235 1 2  ;

91 40 A5 A240 1 1 1 92 41 A5 A245 1 1 93 15W227 14 94 15W326 19 95 51A11C DEAD WEIGHT 96 WEIGHT 97 0 0 0 1 0 0 0 96 A160 27 99 51811C SEliFIC AN'.W:4 tiCVEM 475 100 DISPLACEFENT 3 101 1 102 A5 0. O. O.

103 1 104 A5 0. O. O.

105 1 106 A5 0. O. O.

107 CYNAFIC CEE Y.Y A N AL YS.i s ICS 0 0 0 0 1 e 0 3 109 25 0 2 0 5 .005 1 0 llo 8160 27 27 27 All AESPONSE SPECTR A F CR CCE A CLD5 CENTR AL ELEV 26' (202) 112 12 113 1 0, .1 114 2 .08 .1 115 3 .247 .37 116 4 .237 .37

. . . : 4, , . . . , . .r...'.

. ..a ':'

... 5 ..~. .-

11e 4 .357 .37 l.*

1 C C L C. 96- 0149 An Aca m fr+T A i

, PAGC 7of9

.. 't..

I 1

l l ..', I -'{i '. I,il

'; E

'. P 4 'iH dc  ? 435 . :3

I ) 541 .H 1;2 IC .i 9 ..

1;3 .. .?69 .C5 1;4 12 10. O.

125 3 C. 5 126 .

1;7 2 1. ..?

8 I IC. O.

129 3 130 1 0. O.

131 2 1. O.

132 3 10. C.

133 EESP"'ili

, 5;ECW f C4 :CE "'J L 35 CENTRAL E;tV 44.!' (2C31 134 12 135 1 0. .31 136 < .053 .11 137 3 .317 .265 138 4 .133 495 139 5 .376 495 14C 6 .231 .33 141 7 .352 .33 142 B 429 1.C35 143 9 .556 1.035 144 10 .661 125 145 11 .5 .C6 146 12 10. O.

147 3 148 1 0. .19 149 2 1. .19 150 3 10. O.

151 3 152 1 0 O.

153 2 1. O.

354 3 10. C.

155 DYNAMIC CEE Y.Z ANALY$13 156 0 0 0 0 1 0 0 1 157 25 0 2 0 A .005 1 0 ISS A160 27 27 27 159 EESPCNSE SPEC 14A FCA CCE A'M SLDG CENTR AL ELEV 26' (2021 160 3

.61 1 0. O.

162 2 1. O.

163 3 10. O.

164 3 165 1 0. .19 166 2 2. .19 167 3 10. O.

16S 12 169 1 0, .1 170 2 06 .I 171 3 .347 .37 l'2 4 .287 .37 1*3 5 .222 .315 1's 6 .257 .315 t

.. . ;; s . . . ,- , .. . . 4, . .

l l

..c - ,-. ,.c k

'h* .

  • .-, 2 r. ~;

l'4 t- .sb: I h ')

r 1

C At.c 96 - Ol'/ 9

'ATTAcWmcc A PAGE ? o*~ 7

. . ,, e : . . . ,f 2 . . .: r

  • 4. ' - * * -
5

~

.3^4 4;!

7 5 43r 97

.-- 2 e4; a

's IC . f
- ..
'? 11 .ff9 f5

[ '. M A r .5 M.  : , P.* *E':'aA E El 44.3- < N3; fk ;E S ?;*G E

ft 3
33 1 0. O.

154 2 1.  ;

185 3 10. C.

196 3 187 1 0 10 185 2 1. .

159 3 10. G.

190 ;t 191 1 0. .1; 192  ; .053 .11 193 3 .117 .265 194 4 .133 495 195 5 .276 295 196 6 .231 .33 197 7 .352 .33 199 5 429 1.035 199 9 .556  ;.035 200 10 .t61 .125 2C1 11 .6 .06 202 12 10. 0 203 51EE55 C DE51GN BA5~5 51aE55 204 ALL 0 0 7 2 0 5 4 0 11500v.15000. 35000.

205 CEAD WElGHT WGHT W 1.00 W1 1 206 SAM CBE SAMD D 1.00 DI 1 207 5AM SSE SAMS D 2.00 DI 1 20$ CBE %.Y RESPONSE C0YY D 1.00 SE 1 209 00E (.Z RESPONSE CCYZ D 1.00 SE 2 210 SSE X.Y RESPONSE 55%Y D 2.00 5E 1 211 SSE Y.Z GESPONSE 55YZ D 2;00 SE 2 212 - CPER ATING PRE 55VGE CPAS I 213 ALL 76.

214 DESIGN PRES.(UAE DPAS 1 215 ALL 125.

216 6 . DPRS. WGH1 217 9 B . CPRS. WGH1. CCXY. SAMD 218 9 B . DPRS. WGHl. CDYZ. SAMD 219 9 C . DPAS. WGH1 55%Y. SAF5 220 9 C . DPRS. WGH1 55YZ. SAFS 221 Sur.M S DESIGN BASIS C0FBINED GEAC11CNS 222 7 5 3 1 2 13HC19AAp.114 223 CEAD WEIGH 1 W;W1 W 1.00 W1 1 224 SAM CCE SAMO D 1.00 DI J 225 SAM SSE SAM 5 D 2.00 D1 1 226 CBE x.Y GESPONSE CBXY D 1.00 SE 1 227 CBE Y.2 RESPONSE CBYZ D 1.00 SE 2 226 55E %.Y GESPONSE 55%Y D 2.00 SE 1 229 SSE Y.2 GESPONSE 55YZ D 2.00 SE 2 230 A . WGHT 231 B . WGH1. OCYY. SAP; 232 S . WGH1 00VI. 5AP;

. ,.4,,.. , ,. . . : r ;. ' -

j??  ; . .;ye . ;;v . _A i ?4 ,,

. .;yd' . 5 .3 c ~ . ;;"

?5 *! IvE
:E:. ;.' .. . '- .. :

.v. t-rc .:. . cr ..: -

g?/ b . WW41. (,0 2. $ 1 ."0 '

t A

l l

calc 96- 014 9 i

. i ATT ACN M W A l

~ PAGE 9 er 9  :

l

. . .. : r . : 1

.. , . : s . . :. . . .; , ,

'I i

t i

i i

tt

,. s

. .;. .,u . ;$. r.*. ;;s.;.

.<.. . . , : .t..s .

o.,.., .

<.s-t ,. (

. ,.,,s, ->,ur.* ca u

.s

r. a...

. g. .

.ca.-..

v....,..

...a . . . . -

...t-a 23' ?5 zuo.,3 w ;49 23!  !!; mB ;9.P.IC! i

???  :: 0 /wi: 19 5-t,52 i 240  :::C "B 19 5 65 i

t;4c LE.2 H.35s  ;

242 5160 Lg.;.u.35 a 2:3 :E0 LD.2 H-36 l 244 a:!5 */J0 2-5 653 =

145 5115 2-5-ES3 ;f 2LL 2C5 LC.3

% 2.H 3'  ?

247 22C5 Z..D-2-H 37 ,

24S 4230 LB 2 W 246  ;

24? :2?O Z.E-2.H-246  !

I

& a n.1 7 t

r P

r l

,I s

i i

i i

I

r. e . :. ' i . : . .. . . '
. q . . .. :, r : y .. . .s ;.

1 1

+I a

3;:.'f **,: ip :, , " ;

r. .g. p .,

r..- :-

. .. .. . t : . . r..

f ,'....

4

, - ,