Text

Prying Effect on Concrete Expansion Anchor Bolts Due to Pipe Support Base Plate Flexibility
	ML20065H646
Person / Time
Site:	Seabrook
Issue date:	07/20/1979
From:	Galunic B, Mckenna M, Rigamonti G; UNITED ENGINEERS & CONSTRUCTORS, INC.
To:	;
Shared Package
ML20065H623	List: ML20065H620; ML20065H646;
References
	NUDOCS 8210050206
	Download: ML20065H646 (88)
	v • d • e

{{#Wiki_filter:* i 9 mited e.,ncn0incers a conr.vucw g .s - e a' = - e PRYING EFFECT ON CONCREIE EXPANSION ANCHOR BOLTS DUE TO PIPE SUPPORT BASE PLATE FLEXIBILITY O JULY 20, 1979 / e Prepared by 4/C B. Galunic / ~ Reviewed by 8h /MM__m - M. McKenn Approved by ,,Jaga r. >6f, p. monti ! e-8210050206 820930 I l-PDR ADOCK 05000443 PDR A r-- e ---y, -n --~m

i l = O x: r 4 TABLE OF CONTENTS I.f.lk.

SUMMARY

OF RESULTS AND RECO N ATIONS 3 INTRODUCTION.. 2 3 BACKGROUND PHYSICAL DESCRIPTION OF PROBLEM 5 -i ANALYTICAL APPROACH 7-I 8 p. RESULTS k t i CONCLUSIONS S REFERENCES 22 + e I h l e 4 4 + 9 i i 0 0 --. - ~, -, n p 4 y -

9 9 e e e LIST OF TABLES W TABLE 1 20 4 ~ O e O P 0 e e

(

SUMMARY

OF RESULTS AND RECOMMENDATIONS An investigation was made on the prying effect on concrete expansion anchors used with flexible base plates. A total of 26 supports from UE&C standard designs were analyzed and the prying factor "a" was calculated. Prying is shown to be strongly affected by the type of installation, the stiffness of the plate and the stiffness of the anchor. Prying is assumed to occur only for the self-drilling anchor bolts which require no preload to make them work. Calculations show that though the largest prying factor was 0.18, most base plates did not exhibit any prying action. However, in tha absence of verifying field test data, it is recommended that a prying factor of 0.20 be used for all base plates in design regardless of installation procedure. = 4 r a W h b e 1 6

~' 1,.- .h j } INTRODUCTION . UFAC Bulletin (Ref. 3) recosamends the use of a factor a = 1.2 ,.. r. to account for the effect of prying in the design of expansion anchor used with pipe support base plates. This report provides technical i hustification for the above recommendation.. 7 nu ..u-In.. assessing the ef fect of prying, two different kinds of anchor.s and installation comonly used have been addressed. First, the self-drilling or sleeve type anchors (e.g. Phillips Red Heads). These anchors are installed in such a way (Ref. 1) that there is no need to apply a preload on the bolts to attain the anchor's full design load capacity. t In this case, if it is assumed that the nut used to connect the base plate to the anchor is only hand tight, the plate can rotate and cause = :.:.2. - a prying force on the anchor. Second, the wedge-type anchors (e.g. Bilti 4 4 O Ewik-Bolt) have been addressed (Ref. 2). -These bolts are installed in such a way that a considerable amount of. preload must be applied in order w __:.. . ~... to activate the wedges which grip the concrete. Since a large compressive 4 -.3.e ::. force is applied on the plate from.the nut and..the washers, potential - rotatiohl of the plate is negligible until the preload in. the bolt is nearly. In this situation therefore, prying is negligible until the 7 overcome. preload in the anchor is overcome. E-The recommended value for a to be used in design calculations has' ~ been computed based on an assessment of the. relative importance of arious v i parameters in pipe base plate configurations.- l

c;...

,-- ---- n .- :.+.--: i o -.; l!- i 5 g k-

. ~. - L e 9 .h BACKGROUND Design' of pipe support base plates have generally been based on the-principle of column base plate design. However, due to the nature of the ~ loading (moments are relatively more important than compressive forces), pipe support base plates are generally thinner and more flexible than ' hose employed in the column base plates. Flexibility of the base plate t introduces design consideration which are not necessarily addressed in the design of the column base plates. Flexibility, however, can affect f significantly the bolt design loads and must be properly accounted for. Column base plates supported on concrete are used to distribute the To do this large compressive forces of the column to the concrete. effectively, the plates nead to be very thick and therefore very stiff.' When a bending moment is applied to a stiff plate, it-behaves very nearly O ^ as a rigid body. When the tensile load in the anchors needs to be calculated, the assumption of plane sections remaining plane is usually e made and some variation of the concrete beam theory is used to calculate ~ f the anchor bolts tensile load. Prying in these stiff plates does not occur. In flaxible support base plates,the assumption of plane. sections t rema%ing plane after bending is no longer valid. The implication of this is that the centroid of the compression reactica is closer to the. neutral' axis than was with the case of a rigid plate. Also, there is a potential for prying to be induced in the tensile part of the base plate which would 4 - induce additional load into the anchors. The method of accounting for the. t t first effect has been described elsewhere (Ref. 3).- A method for accounting ' for prying is discussed herein. l (, ,. Q;. . :. l s t I i 5 2-

a (~') BACKCROUND (Continued) 'v In s, teel connection designs, equations have,b_cen developed (Ref. 4 and.@ jo, account for,t_he, prying effect when calculating the force,on the bolt. The, presence of prying in those connections with flexible plates have been verified by tests. These tests indicate that prying introduces bolt loads in addition to those which can be calculated with a rigid plate theory and that these additional forces reduce the capacity of the bolt due to static or fatigue type behavior. However, these results cannot be applied directly to the problem of base plates on concrete. The most important difference between them is that the expansion anchors in concrete are much longer. Also, the reaction of the anchor is in the interior of the concrete.- Because of this, the stiffness of the anchor due to tensile loads is much smaller than the stiffness of the bolt in a steel-to-steel connection. As will be shown below, theprying force is significantly reduced n the stiffness of the anchor is reduced. ? G +A MH W e 6 elUmma** g M6 m m b e ', Q,/, ~ ~ 4_ f

~ J I g ' (] PHYSICAL DESCRIPTION OF PROBLEM V An example of a support is shown below. Dimensions given are representative of actual supports presently used in UE&C design. Other supports with similar dimensions have been analyzed and are shown in Table 1. 12" a o Ii W65(2 h 'D O O 0 F d' 2 - D" v. V m e j f T 34 l fe.1 h) l D .o.0 J1. ' s. u-L O'p b ,0 .g o b-G, - f,, o = 'nu 0 0 ~ S' - e

~ ~ ' (~ )N ANALYTICAL APPROACH r F The mathematical model used to calculate the prying force is shown p i below. It is assumed that the plate is fixed at the point where the support f 5 member is attached. Rotation of the fixed end is neglected. In this model, f F is the shear at the fixed end. It is equal to the reaction in the bolt when prying is neglected. Q is the prying force. R is the reaction in the anchor. The width of the beam is assumed to be "2a". The stiffness r of the anchor is K. t I brdh : 2a, j } Q ~ t k t Q \\ I g 3 b 1, O In the steel design the prying force Q may be calculated by using the formula found on p. 207 of Reference 5: Q=aF where: a =( ) 3 3 / and the anchor reaction is: = (1+c;)F EQ. 1 R3 Alternately, an analytical solution using conventional beam theory may be used to calculate Q. (Similar to approach in Ref. 6.) The resulting equation is: Q"GF 2 a 2 2 03= 6ET (2a +6ab+3b ) f + ht (a+3b) and the anchor reaction is:- ( R2" (1+0 )F EQ. 2 2 ~ - 6.-

i ~ ~ ~ ~ ANALYTICAL APPROACH (Continued) t The main difference between the two equations is that the stiffness i t r j of the bolt'is explicitly accounted for in the latter. _ 1 I r I j I 3 s s I i i ( - ~ j i t I L 6. i 7 i [ 1, .i l t O '_,l 1 e d. p s. [ 4 t 1 t j I .s i i I 4 1 I I [ f 9 i 4-s ~ l 1 L > = g' k

r ' /~,Y. RESULTS \\;j The results of analyses are tabulated in Table 1. R is derived from y thecodeequation[Ref5). R'2 is the bolt red'ction calculated from Eq. 2 ~ ~ (yassumingK=a. R " is a tabulation of anchor reactions by including 2 the stiffness of the anchors. The anchor stiffness of R " was calculated 2 by assuming the anchor pinned a distance L from the top of the concrete (i.e. K = AE/L). No preload is assumed in these calculations. R '" is a 2 tabulation of anchor reactions calculated by including theeffect of concrete on bolt etiffness. Tests done by the Tennessee Valley Authority (Ref. 7) l indicate that the stiffness of the anchor in concrete is approximately 0.4 times the value of stiffness calculated in R " above. 2 t I t ( t i. ...~ ~ .c-be f e.-== m.. -....* 96 f t-o a e. -. s m ~ L. 1

g 4

.o .{ CONCLUSION From the R '" tabulation,it can be seen that the maximum anchor 2 reaction factor is 1.18 while all others are-1.00. Based on these results, ~ r it has been concluded that a = 1.2 represents a realistic value for the prying factor. .e.; a. .,e 9 t 4 e a t e ,h g e -+, m D f I ? k T 9 ) +,, '6 1 l 1 b t k 4 e + m-4 e6 e e \\ / ? e k I P e I r. d ge p-e-

b p .t. y; j '~ 3 .[ i 1 PART NO. t L d b a R1 R2' R2" R2'" t 105-1 0.375 2.5 0.50 1.0 1.0-1.50 1.53 1.37 1.18 Dimensions [ l 105-2' .625 4.5 .625 1.375 1.125 1.45 1.48 1.14 1.00 in inches 4 306-1 .50 2.5- .50 1.0 1.0 1.36 1.38 1.15 1.00 i 106-2 .625 2.5 .50 1.5 1.0 1.55 1.61 1.26 1.00 j 106-3 .625 4.5 .625 .875 1.125 1.28 1.27 1.00 1.00 l 1 106-4 .75 6.0 .75 2.0 1.5 1.48 1.53 1.22 1.00 ~ 106-5 .75 6.0 1.00 1.5 1.5 1.35 1.38 1.17 1.00 l i l 107-1 .75 6.0 .75 1.5 1.5 -1.35 1.38 1.04 1.00 l 107-2 .75 6.0 .75 1.0 1.5 1.23 1.22 1.00 1.00 i 107-3: .75-6.0 .75 1.5 1.5 1.35 1.38 1.04 1.00 l + i 107-4 .75 6.0 .75 .5 1.5 l'10 1.10 1.00 1.00 ^ 107-5 .75 6.0 .75 1.0 1.5 1.23 1.22 1.00 1.00 -f 1 107-6 1.00 6.0 1.00 1.25 1.75 1.22 1.24 1.00 1.00 { ~ ~ 108-1 .75 4.5 .625 .8125 1.125 1.25 1.25 1.00 1.00 108-2 .75 6.0 .75 2.00 1.50 .1.48 1 53 1.22 1.00 { 108.75 6.0 1.00 1.25 1.75 1.29 1.30 1.08 1.00 [ ] 108-4 .75 6.0 1.00 1.25 1.75 1.29 1.30 1.08 1.00 108-5 .75 7.0 1.25 1.875 2.25 1.28 1.28 1.04 1.00 j i 108-6 .75 7.0 1.25 1.125 2.25 1.26 1.26 1.08 1.00 108-7 .75 7.0 1.25 1.125 2.25 1.26 1.26 1.08 1.00 i 108-8 1.00 7.0 1.25 1.875 2.25 1.30 1.35 1.13 .1.00 l 4 108-9 1.00 7.0 1.25 1.75 2.25 1.28 1.32 1.10 1.00 108-10. 1.00 7.0 1.25 1.75 2.25 1.28 1.32 1.10 1.00 [ I 110-1 .75 4 '. 5 .625 .875 1.125 1.27 1.27 1.00 1.00- ~ 110-2 .75 6.0 1.00 1.25 1.75 1.29 1.30 1.08 1.00 110-3 .75 7.0 1.25 1.25 2.25 1.29 1.30 1.08 1.00 ~! s. t 3b t F l (1+at)F = 1' + -( g g ) R = 7 a ~ 8 f .(1+8 )F = -1 + 6EI (2a2 + 6ab + 3b ) F j 12* 2 3 y +3gg_(a 6 b j ag' => g = m.._ gf '. ]# az" => K = AE/L ~ 8 02"'-+ K = 0.4 (AE/L) 4 s .Q. - < IR -l b _ .g-Ah. f _ 10 -- r 32 [- ~

o. 32FERDiCES (q 3 J is Concrete Anchoring Handbook and Specifiers Guide, Phillips Drill ~ Division, Michigan City, Indiana, 1973. 2. Hilti Architects & Engineers Anchor and Fastener Design Manual, Hilti Fastening Systems, One Cummings Point Road, Stamford, Connecticut. 3. UE&C, POWER DISCIPLINE TECHNICAL BULLETIN #7B, " Design Criteria for Concrete Expansion Anchor Bolts Used with Pipe Support Base Plates," May 2, 1979 4. AISC, Manual of Steel Construction, 7th Ed., American Institute of Steel Construction, N.Y., N.Y. 5. ASCE - Manuals and Reports on Engineering Practice - No. 41, Plastic Design in Steel A Guide and Commentary, ASCE, WRC, 1971.

6.

McGuire, W., Steel Structures, Prentice Hall Inc., Englewood Cliffs, N.J., 1968 7. TVA Division of Engineering Design Thermal Power Engineering, Civil Engineering Branch, Research and Development Staff, Anchorage Tests of Load Transfer 2 trough Flexible Plate Interim Report, CEB Report No. 78-21, July 26, 1978. ~ 3: { j. g e e l , U.D l f

0 - p a p .e g e e e e m -w EXHIBIT 210.70-2

913 Tampa Road ? Knoxville, Tennessee 37923 \\" May 21, 1981 Mr. Branko Galunic Structural Analysis Group United Engineers and Constructors 30 South 17th Street Philadelphi E Pennsylvania 19101

Dear Branko:

~ ~ Enclosed are copies of the data obtained from the tests performed on May 7,1981, when you visited our laboratory. These tests were performed under the authorization of P.O. No. 9763.006-210-9, Serial No. SNH-683, and were tests i ~ to detennine the prying factor for Part No. 807-2 subjected to bending about the j ~ strong axis of the attached steel W-section. Also enclosed is a copy of one i sheet of notes along with a graph showing the variation with applied moment of j L the load in the top two bolts of the four-bolt attachment. The results of the first tests in the project designed to measure prying factor were encouraging. The method of gaging the bolts and the plate was [ satisfactory, and the test results appear to be reasonable. Based on the test results, part of which are illustrated on the enclosed sheets' noted earlier, the following conclusions are drawn: ) (1) There was no evidence that any prying occurred at any stage of the testing. The plots of bolt load versus applied moment, as shown on the enclosed graph, indicate that the sum of the loads in the top two bolts increases linearly [ after the load in each bolt exceeds the applied preload. There is no sharp in-t crease in bolt load at any stage.as one would expect if prying occurred. Also, a study of the strains in the gages located along the diagonals near the top i -corners of the plate (Gages 4 and 7 on the data sheets) indicates a very small tension in the plate at these locations; if a prying force were acting at the top corners of the plate, these gages would be expected to read compression. Thus, po the conclusion is that no prying occurred in these three. tests.

2 (2) As indicated and discussed on the enclosed sheets, the straight O line portion of the bolt load vs. applied moment curve did not pass precisely through zero. The reason for this is believed to be related to the definition of "zero" for test purposes and the stress condition in the anchorage system when the instrumentation was zerced. In any event it is clear that in the straight line portion of the curve, the ratio of the change in moment at the face of the concrete block to the change in load in the top two bolts is equal to the effective moment am of the resisting couple. This moment ann was 8.48-in. and 8.79-in. for the two applicable tests, with an average for the two of 8.64-in. The moment ann predicted by UE & C Power Division Technical Bulletin No. 7 is 8.5-in., remarkably close to the value obtained from the test results. (3) In Test 81-8-1 the bolts were torqued to 192 ft.-lbs. as specified in " Installation of Concrete Expansion Anchors," No. 9763-006-18-17, Public Service Company of New Hampshire, Seabrook Station, United Engineers and Constructors O Inc., aenuery 4, 1980, aevision 1. There was e time iapse of approximeteiy four hours between the application of torque to the bolts and the performance of the test, sufficient time to permit a large part of the loss in bolt tension to occur and for the curve of bolt stress versus time to level off to a stress that was decreasing very slowly with time. As shown on the enclosed graph, the load in the top bolts at zero moment is approximately one and one-half times the design load in the bolts and increases only a nominal amount as the moment is increased to the design value. Thus, it appears that in a correctly installed anchorage, the magnitude of the preload in the bolts is greater than the design load in the bolts and that this load does not increase appreciably as the moment on the anchorage. is increased to the design value. As we have discussed, this situation is a desirable one, particularly where dynamic loading is possible. Our next step in testing will be to test the same attachment with a pre-0 O load in the bolts of approximately 4,000 lbs. Then, we will rotate the block 90 L I

3 and test weak axis bending. Next, we will cut off the steel beam and perform j b a tensile test. Finally, we will weld the steel beam back together and test a cantilever beam in strong axis bending to failure. I will be in touch with you at every step of the testing program, and we can modify the planned order of tests if it seems advisable. I look forward to our continued effort. l Sincerely, j Edwin G. Burdette 4 Consultant - Enclosures. EG8/vaw i O l, I l i [ t 6 + t rr, .re.i, , - - +, y

3 l I 4 g.,.. -.,a. ,........i,. r .. 3 ..-..4 i. 7.... a .6 .u., Q'T...4,,..,,......, L. .4 g y. g.y. 1 5.- ..._d.....e,.-' e.

m.,

,( 7 ..w .. L. ,u.,.

1.,.,.,,.,

. -..q.u.-%.. .2 f ...6 6.., .i. .= 1,,._., .d....y.... .~.6--.4-. .k6...., ..# e... - .p .....4 J .( 4...c

p.. '

L ...6g .",4-

4-

.,a.. u.. t..~# a.. C... u ;[. i tl g *.. j- ..._.s... .r 4,. .L. a k.1.

4...

,4 .l. 6 i. L. i. n, 1 it. ..,.1,3. [,q..

5. "

4.: .. i-. ,,-s.. = 4 ., +...,.s,. L.,,.... T....

s... l.

..y. .. yl ...a. ..i.. ,.. i.,J,. a.. 6 e, . s. 4 ,6,.. $ .-o, 43.a .t.." - - -., td.6

- , e. ' *.***6..'.r.

~! .L

3. %,

...p t. 4 m .. a .t. i,,. ~,. 3 4.... qt. s.-* 6 gt. .4.. .o 4

i. f.

+i.. e: .4. <e t. --

6 l.-

.4 4 as

Y 6

.,t

p. 7

-. ( 4'..,.. _g t= . r& a t4 .....,N.,.,,.....*,..i. +.*.,:.... Ng .4 ..et +, , 5.- - y i.... w, s.. q ).61.l_ ., e. .,.7 ---s.... . 7. ..teef g ' ^ s. .l ..N .(4 . ( #... ..t ..I,.e.n.,.. 8 .,.v ,L .6. .4 1 6 l.T.u. -. ,..j. t 4 .6. (4 5. o. et9 .- f .,9 4..1. 9_. e,. 3 .gg. 4t.4 .q .t., ..Lt p4. .6 4... )A 44. t. . 4,.4 44, g. ? t.L.. tJ..;.. .y1 ..~ , 4 4.. ,. 4_. L. 44: ii ..a ,a m.4 ,,.. 4 .&..l,...... ...r 6_

s.,

.6. m. .....a.

b..

. ~. . 9 1... .c. 4 .a. .; -.~ ... w. 7..

4. 4. y

.i,6 3.,.. 6.. f. ..c a... .6.. ,...;a .t. .., u.. s... ; .4.: g... e 2 ,1 .r,..p r.. g ..6.. 6. s . 7.

.... 4......

4 4.,,. 4... ....&..m g.__ p... c...]. ? 4.e-4 4 .a .y ... ~... _ t' ' ._,.4 t. .~ 4 ., ;,, g,, r, -, .i, [... t p., j .g...,..,.. 4... 4._,,,, .4. .a. - g.... s. -..{. a u., . i

2....

. i.,..,u.a_. ..m.. 1....,.u ..s,

n. ;,,

g.* c.* -.t,---- _1...._ m-H e,. g, u. ,r. g, ; . g-4.- t ,.., _,u c . f, r, c-1 s.. .. r.. 4. I.. .._.g.. a.., a. ......n a 1.,. = 6 .i...; ..5. .i.. . u... a.. +l.. ..4 . s op.. .to.,...-.....s. ,a t.:. .e f e...- . L_..,..; i. ,r......- 4 s... ,d- .....#_ 5 u..,. .g gj. . m ..l g ... 9 .g. 4.. e..g,,.i.. } [ g.. r _...'..4. i -6s:. .s . i is i..., i t. .g. 1 L ..y . j '. p ..).J .,,e ..l-s, a-S., .6 e ,+d.,.,.,c S 6.,.,.. 4 . v... I 4.,. g y i &,- . r. et i.9

- .--f 7.e.*'

i a. ..n ...,i .y .,. 4 .,g -[.... g .g ...a. .. n. f.. 4

e. e. e.

ee. 3 4. w d.

j,.t.

6 e.... 4_ ,n ,..y. c.s L* t.6* '*'T.'e.+. S. '

F..

+ .,,t a L. + ',s,' , 9;.,.. a6.. ..&.a.; .f ..- r - t. '6 i, t.- ". 's. t' P. 4 I.,. ..r* .6 ..k s l ,(

5.. h

{ r*** 1,._. ta. .4 g ......-*~.i.. d..4 4 + - * ~ e

. -. - *..-.e...,' t. -+i i

4. e i s...2 ; i....., .....-e- '..I ' ;t-2.. .e2

6.

i n L , e4 .i 1 ....). .4 a. 49 - +. ". . h.gu,.. F. i. . -.....a.. - e .wI r 4.. 4 + g e, t. 4 4 -4. > .- e. .O..'. y' e, 'b, '. + i. e.i 4.I.s.. k, "'~**%- W . p 7 t.

1. !

- -,r, 1 .h.-- .,t j 1 ,_ y o;- 3g,.y _.i t ., l, f n.,. ...a... . _..i.. .._ %e -- s 1 . 4 s - w y. 2.... _ _. 4. ..m.4._s 4... ...p.... t t.. .u. .._.A a... .,v ..s e.. q..u..., 4.- 1... .g g ... j ..s s +v.,- .Y. ... +,. a,. i 8 .u _.., t.a.vI,.,...,; .. i. _,.. .i a-. ..,7.,...... g + 3- .~.r 6 . ' ' -. * * I ~ ' * + - - -" ... w7.. t. . y tc g ti ..t. .,.g., .f. .Ig T M. -

-'ti:

e o. r. g v. i. i..t ,i,ee t 5 s.. ,.p, ..+ +r x p l ..w v- , r7 -c.,.76... - -..q.. ..g .+A..- a. q.-.. i.4. 3 y.-.-

e..

,--t-.-** ..w ,e. g .6 ,. y ...p..,. _...,.y I 3.,.....r-It _..v.6, .e.-< i .....a ... 4 ,v., W M"W \\ . I,.. e.1~.".+ 9,., 7.. ' ', +7;*4.4+4 7 ..n. 6-H T "s.. p 4". 'i ~... ~c. ~ .. ~ ~ ~ t ~~, 4 g ..a.,_.,,. '.- %. !..- I, l 6. .+,.-,L ~....a.'... 6,.. l L ~ ..,. " ~~} e ~ M i' .. 6 .W_

t. -

8 Mi "g *tT l e ,- i. I. +t.. *f -[p 'l 4.1i ..e ,. 3,- 4..*< P. r. - n. ,i re .L 6.- a. q t . t g "+r . i. l, ..t: .o l6 .e, L.

I. e e i. *,

s .r. e L..

.e.

J l... }. .g. ' i.. i .) is

e 3,

?. 8 ;-2 4 I -t ,.W +4. j 1. u, d ',1.g :

g t.,,

..n,-.,,.p.. -

u. 6 i-.P ~a.

.r tm , +. , r t-e..-o+ +* e o. m,. e,,. . -........g.

n.,,

r ,1...,. ) }.L4...,.. '.. .t...,... _. _.,...,.I. a..' 6 .~ :. .- e. at .2 .a 4

e..t.

.1.,, .O,. . ;I.{u.,j WL.i i ,a j g . i m i.. r. I.,. ,-.. M .,,r ...}. - 14 n . +.- -,r ,...p. .d,,. y n,...e. 4,,.,,... e. ~,. - ...L,r,.f u. .,-t 4. t +-r u. + t ++*+ t . _, ;y . L+ !.. "~ +, - --r i' .q.,

g.. i ;.. +..

.r L. >i.. -r 4 i --

6t [in

. +. ~ +.,. .t. , g., 4 5.. . t ..Tt.s. i,,P ..,i. ,, +., .. e +. - + e.. ..i g . b.%. . i t

i

....3

Tn r.!>-

,t th ; 7 ~ if t W-'rt' mat ]. t; nM i !r4 * ' i,,.. -d,4.,.3 :~. i ...a.. 6_.4 d-9.N d

i, t ; ri -T-

.i t

+.. -,.T, g t,s r.

y 1 6 ri,.. _. _..,... m.,. f .. 4, [ p.., i ..: _.v,,. L. y

9. p,

4 s + 606 4M

1 e.i 4,,

F.. ... ;...,r.,.,..g; ,.y i-i.. .-,)y." A.a}

'6 r ;P,
. J s

~ a2+.- J.', l.a.,.

. 6....

.. ' '+ L., 'I. ' H.. v. L-- ~.-. L -6 ' e 6 D,.. t } al~e. it. (. 4, .c""... ?e, -.t.. 6-- 'tr .A 6, 4-. ....l,!s' i.{..-' 2.t - . J ', e - i i..., -==C 1 5.;. i,. I '. (. .s, i 4.'.r. t.- d 9 4 a 4 o 4 4 4 ,.o I o o r ,' m a I ,o 9 9 s g o N i 4

g N "~ * ~ * *

. w q O .)

i C-G et _..._. l l

. _... TusTs o.4 S.m.T td 8 o 1 2_

I . _.... T:._. _. ( Tes-rs 8 W -t i 81 - e-. e, 4 el-e-3) - - MD SI -- j - --

E

......ScA p.Dov/i3~ t----- ..........VCW k --.. l. -. q ' o )k... .a..._. -i,. [ O ._.,s-. _... _. 7..i -... -.-{ f y. 8 i G \\u g _t i u v,.. -.r~~,.--- t-r-. -- M s. - -. t j i Coew.. 9F . - ----{ bt.V. . ~ ~. -..~.-.-_ I l

r. _ _...

-_ - (. W b l f4 8 e .i 6 6 8 i l l , i /ZW M M

O 5

L' . _- I. ., a _. _... 4 -- _ _... - h.. 4 ..l_._... ... i J - -- - $_. 'r-L ; --- p r_.. .1 .3 .1-.. '_ - _. ' 8 _.._.4.. j c._.l oAo 14 . L...... e e - i T o P_.._. ...'..._.4;. . _ __htT. S t..... i ..l.__'..... 7.... -. p _. .. x' t_.. .. 6 _.l.ENEL._. cF . kN t a.. _ _ ..,_ bN. Moge4] ARtAof: ..Pir nLCA.D gp p: gg7 g - ' ~ ' ~ ~ ._. i_. @e%AVloW tF No Ps"v.Lc::AD i ._,.____.....a-. _,l L p) _ __. / ~. ~ ' G-. WMU.14T. AT FME cP' B:4 oc\\< .e i _ __.... ;. \\Ot A1_t 2'Et~:> E:eWANt ova. oT:. As 3 c.AopGE N 0 TE <.~.ai ...L .. _ h.... _... 3 .i... _. .1D A<;TOA.L- *iWHA.vtce_ of: h c3e: ts snob! M Y:tGs. l. Tl4e ... 5~U2',.W.m R~[- Lule P o ta.7 t o k1 er: Tue L m:> vs. Momr t4T. .. _..__.-.....$tEL.AitoM5 HIP Do E.S mot PAM.Thqu.7Me. CR.tC 1 J. 3 . (lL).P-.eASod5 9:o;:t/BfEthAvtog. tao te :> tW.*l Axe PeoeAt>LY .Fa.ut.A tsD To Ten c.a4omoM A7

Entac::/ N tge Te.9TC A Loc.ATioM os:..P

. SMALL OPwA.wp loa.D WNS M te_.p AT tus ..AT TRe "Een.o* 5. tac-n= ; NOTS werc.e Loosmaeo, wo AL! MSTRO W2NTA~Tt od WA.3 2Er2_c=_t:r.TSEQ The Et::LrS Wt='EE ToRadsb T6 T~4 e ne 51 seep vme. l (,N MOMENT A;aM =.<b.4c3e W MoMe4T. <::-'ge tW bot.T t_cW:>s .. g o eo E 48,

== TEST 2 1 - 6 z. : Ax m = ch/' 30 , Avg. = 8./o4i, - (~) Te *T Et 3 : A s=. M==

ot st o -- = ?. 19" 1 o

s if Y~EcM UE&C Pouez.'Dtsc.wt.me Teta,Buu_Pl : AsM = BS

g, t

=:.'s i

..s-F'- ' ' L 4 .La... -.p_4_ '.._ .1. -

_L c

.LL ._L {'. . __,_L -="* ...l}g._.. LbH- ..L 32 200 L4.-. C,,_a; _.L;. at. a _ _. L;._._ __. L4_L ..E__._. L._. 4 .j :i

- i i

_ FL ..b -.. [. __ . 4 L t _. _._7 -..y_ 5 i t -H_pj_.[

_7 L'.

_ _7_L _L. a . -t '- 4- -l- -l l 3 - .} i.L-.- __ _. _Ly* I A i.._ 9 .:.y i . _ g.}_{ ,!O. __..6- .._i_____.4_}_ _ d.. g I, L- ....____q ). jj { 1-,_,a_ _ j .l, l; t i i h-j ,'l_, . j: _E-~{ - --, ~.,_,y_f._.H4h -i .Lp4_4 .e 4. L .t a _p 4_ '._j 0 4.-.. l i Q 4- '!L c_ i -- _j _k. -.----- y 'r_ l l,, I N 2._ L._4 .7 Os i t'-~.._d'__ ~~~~ -YF O _ _"-.- [ ~ a-jM, N_.'4.hY. f l! 1 !iI h: ;-'l'! i!'l ___h Z-hTy 8C , i. ._m,y_ i -f"_-j i .a, I Y~Y 4.O O'S b,' -j L---l h__-h-rrh - h i 1 .I'i_Z t I _ gp. i 9, g j_.___rtf i' i i I (CJP ~ N-I !!.h! --t i i ri 1-- , ' TL f ,_.' :.4. C p l 6 e i t 'i . h,_..- 4.-Q -p 4 a.pi a L._}ch__p j Ly_ ' _. _ .y. Lj l, .y- _f_--_1 4 ,i. 1. ll'h 'l}l -p - - 'l } }---- -b -b - D-h @0 l i

'3

i H h

h !r-- 4' '- ++"L-_ i, L, G,. ;.._1 a I b 0 _l+- F1_X _! _'i ' L L ;, A, D 'p. - j~i-i ll-7 i \\.... _._ -g __.._C___.__ Y (ri .L L 1 + r --1i.. .t\\ r n -t vr 7 rr,, i -," ' rr A-HN / - .l!; IrrF E:.! +- j_-H.-_7-4 + Fy, e ii 1l m._r_- . 6' -.-- i,.c_.H._i t' i'. ,g (3 t

g b r[4.L.

e " F -H.-t-l i 'i l t r-( ll'T y %+H-j-1 d l j l' l ,0NL tti-,y 1{-.-- - MP - %~ i,i -tY vQ l. l tn 8 i i,t i k' M& I+b r- 'I [ ,I ![ ,l Y 3-ii f Lr-- r H ![5 . _.L._ d.Uj _-- :-- /. _ - -h., _,;.E [;i [r -t1l'_ 'l' 'I l l ..O..

L.5_

_..o. : E i j_p.. __Lf.. i / .i i t Ti, J't La[_ _ _m--- q < i,1._q. ' i ii .._g j. i 1 e i i ii. _ s - i 1.d ._4-2. - 0 H._ _..__p.- QL_. >T< p La_ _. j.p. j j ! }. i_.pi_ > i _Lll*

,._L

._LA. . t_L, - h.__'FH i .pl L. '.j,-.,[ +rl, ~t yi l - -h._ _.__8h ..p _4 g.- g: y, g; .._ _ _ L, _\\.y , bi 7 _g y --1 i -Qy I a i i 4. . rb'r. - tr i, y W-1j t -- ; t ,g rM -,ii, ei i i iii -hp, i F%, i ~ ~ ~ _g ._._[ _.4%._._FF3- _..__ h-._p ;T y.i_ l f i '. PI ) -'~ g... ;.p. 4. .Lp%.. L U1 2 _ _ }_ J _j p _.} q,' ;! T rli m. ._._t. 4 __. _i. i-b - :- ill ~,1

bt*LY--Y, L

---f l -r ggf l . r-t tr~' O i <(;, i,r _L._) .. u n a. c. '_pp u.._._ y_ L {.p .[ _ 4q +i l 3:\\v t-__ __. pet. -F 4_1. %_ #g__ --+ t r

'--t '

6-0 %- J _ ;. +. 4_ r 44",Z.;. q*, r __ j 1 + - jj.u___ _.4 - -- r -r- _. t_ ;7 ._,_, A _.._,_ L _q _p..._ a _ 4 F.. H_,._H.....,-r. - E!. o .L j_ :-,_ __.. a _____ }. ..g _. . p.,7 [ ji .l. H + p.,.- _ _._t._._ _ _.. ?._.

b 3

l l.Q_.. _.a .. [j...p.;-q_ _h, H p p. 9 -r-vr j' ..+_L -. y _ pg L. g . J. L..___pt 2.

.._p.

4 .:. LL5 m LL _< _L4.igI.., }..M q.4_ Lj..g. [.. a a.,C_. __..}t _ _. .1.;a j _L2.._ _ . _ __:. Ly..,_L ! _;... 1 _..L _L ..t _L _.. }.-. {.. .,p., l .g.pp. ;._.pt _.4pj... , _1 4. z _. . L.a ..p pq,. _, y _.. _g.i. l -p. 4..y ,O,'' 4.:,,. g; -..__44 .._._._l.__._y____.,. g - .._ _ j. _.. _y.._ _ LL' -_.._.p___. g. q.,, yL < ......... 4,. 3.... p..____,.___p Q.., . _ _. }.. . p _....,r,... e_. 6 3< __u-v .._...i a .7 M__,p.4;L. s. L+g.4 ,[...... q .t.. 1y..l..... .l _wLL,.. W ',i . L.{...g..._. 4 ..h....( i. .-._..g. 7 _ 4p .. _.7 +1, 3. g.l _.1. [._ .t, p.,. .._..l.._... .} y t _.pq.L \\ i.. ..L i _L__. ..p. g4 .;.... O.... _... 6 5. :. E S - '.1 j g. ' .b'.. {F....'...... + iO. S g..... .D' g Q... - i L! j. .Q

D.

g ._3 .g .., Q g .g .g. ....a -., j. __._

[NOC

,- a .w o i , _.1,.',, .. V... __. g i- .% _.. r-tO.J :.a.N f* ~~- 1 -- .Q. .r* _f. /} {_l. '.?"~7 { ., t.J j . j,..i.,E.(4.. 'IM.. A pcf. OM_} ] dol N WNCq. =io, ; 4.r. q. ,i G4

q. _ q1,..;

y- - ,) I ..s..,, t 3 sm8 f

+ 6 D. C opt.EY 1/*Tro Ensmens Aa0 Co asrxuerox s A tw u c /scr.*n '7'e sT s C. N>. 1 y el-8 -/_ (C-7-81) l 73 sr w i'Qf 2 AYTAC HMEnT rJO: 8 07-2. S.TACM A Xls SENOtuG 61.ocr<. :.sTV Os

$.~..y g.

ieC$ ..... A.;.. A ,? t 15.I j 1 t.=.t E5 sg.

c. es" i

g 4 f*ti + WE ( P q 4567 6/ ? ~ t t c o g w c 7 pin "3j GA4E. => On l D .. ~.. ~ l'E,5 7' .SB 7~-up h b 5 +- f k $. Ql$b hMh //7 1 3 /0 T har es .2 4 e 6 O' y t SEc~r A-A 6 AGE A AY ANGEnteNT -s ? o + 4 m h

N qNo* k l

f. '.

j (,, ',' f I h N 7 D I }: i-3 3 ON a g d,k k i. k E f '1 O a p E U =Y g4 8 4 3 8 D 3 3 R 8 8 a 2 !3 } b o b p 9 O O O O O O cN O k k g N N,5) N O O D b o to O O o O b h o k A N "o' M 8 D 0 k h $$ 5, 3 4 1 o 3 g k N N N N N ( . o d o i I -2 gli, I ^ o o o o 4 a w 3 o o g n i x s1 4 4e o n m n d s 4 a o @: ta a s '3 D O 9 4 4 g 0 e N t o 4 g q v (g in [ N N N N N N N N N \\ N l s g. y Q *A 2 8 3 2 h k S h l A A' h ',U 3 ( 4 R e R R R N N 1 s s a R ei s k I.- O h h O g b . 'D D Q h o o 4 t a a %s k h k 4 o a e a w w o a o e o e g x n, N O O O k 6' Q p G Gi i "' g nN 4 ! I N f 16 y of;C. 3 h O o O O h G O g 0 ( 0 0' .g g 4 t 4 g 4 G q n 4 0 g d. s g 4 { k k k S S S S k k Q D N k t g n O k tk k* +k i.4 I-feq k M k i i( [a d C v + e 4 w +. w %v s% s w k, \\ s N N N N N N N N N N

N 6

L/. L ~ p $N k k k h b 4 o n ri r4 N N-N 'l N c4 ' in d 'X $ 6" h N' Q N s N N N N N N N 1 N D $ N Q i N r r g o D h o o G o 'a O I t 3 5 Ns ( g 0 g o g ei o o o O 0-3 o g 0 Q D ln W p a w g E .. x {I k ( -Q R O' ( k k k k k !Q ' .,._ : { n k 7 0 0 h* I $D 3 4-b' ^ o <0 N s m o e o r1 b @ Gl O

$o l

E D d 5 8

N d

a d N N ni m m en m .d' 4 g e-t h 0 I h N o I, i 0 o y C t 4 g g L 'D -D O o n n g n n ~ s I y O O 9 0 0 0 0 0 o ,f r R h

g s j

3y dd N n d d d N n n N N ' lE o I d .I f?t [0 o o s ~ N n m m o e 1 o o O o o o o 0 o o o c. .R ~ gg y n 4 .g g n a, e n 6 a n N n n ; ~ n n n y n A o u N O S N- a4 0 .i d 0 0 0 0 0 ' O ! g Q O 4 0 h y

A EI O

o 0 0 D t K(( 0 g g -o O 9 c O O j n to t-w N m e S S n y g q o 'n l, ;. A 's 4 .e o o i 8 n a w n N N s o b f, 3 k, t n3 t t t e e w m N 4

m. -

~ y, h i i 132 g l N '^ 9 + b h 3 $ 1.._ A...k 4.N. _. 3 J._._ ICE N b 3 _ _ t-5 3 D h b 3 O g e Y

( Gs &ua w s~r tM D. J Q .,w u.. 3 }. '6.+- 7 .,.I,L.,. ....6. t 4 v :. ....:. a.. l.i t; .;6. .11.j. f!T I,.t. 4 i t

t.'

N.,1 4 J 1.' .. t l 5.i .%. A.it ad

.r.

-. Lo-1. .t ,1. .4 w ..I,;a 13.i.v...,

+

a s sti. i 1. .: a. am 41 .r.t1 .f q-Sg w:. p %..a .m I 3,t g p.

e.... - m..,

.g 31. [-4.g. .T! 1,.,.- 4., ,..r-..e- ~.. s.a.. ..m .i,e g

..c.

r.., y.g-3

p..

p.a.,677:...~.. n .p -

.r.-

p4 .j. 3.... s.s .4

g. il 01 7.,.4,.6 pr i...

.+

.r-4 _.4

. -v g a 1 ,. n q - I iII' . E' ' '.lL i l' I' rd '6I.!]- l eG.,l., ', j,!

'li I.. M,...i '..I Il !

j.l Q }ft' Il lik I. '. d. L..;.! 'T t t :ll] 1. ., J.,-.1 list M., 4T 1 - e. 2;,. t.e i<4

r

,t i t I. A 41 ..;4 j ++.' i re. , j.1

p

.s. i o. ..v t e..

*U.Jghl 7

,,.14- , b.a+ t,q ..J. L ..,.1 X.. t.f. 1.t,.., 4..,, i I. ( *i.- 2 m, y w.. i. , 7.1g.. 6 s t-oY, l h... g. a. p.. s. .t,,l. mt..4 }.t.'.

, p.

i.l{

i. t *.

t is t S. n '. I e, < 4 i

1. 9. h

'o

.l 5.....a.. 1... ,..A.s.. s.n ,.. L<.t.,tr e ~* .A i 4 .~. ..y ~j . t..! *

i.. t

+t.,h.&.- U.g.It..'*..,..t,- . { i. j.. ., U. '< ~i -f.. 4' i 2.e

l 1.P.

.a.tt. J.-*..i 1.'..*.t i t..-.. o- .4ayg 6 y i, t. ~cJ- .4... g,, 6 9.Ii.t i. .n..., 7 -.p .e.,3. &, .pu..s 4..... . ctT.I.1.. w.., j'u.,. ...4 a.t4...

.i i t,.,,

T,. 4 t ..a o 7.j. ., ;e e 6 .,. v.s, t..

m...

u t s > ... t,,. -.a.E, t 4 q.. y. .i..r ....an 4.- o.. A. e. ..,- 1 . n .H. .+.... ; y j, it I A.. L.,,.t.,...I .*a h. w.1-. ,t.. t 1 4 .R. . h... .a..

1..

+:#r 9 I. T, -.4{J .e..-. i..t. . t p. 4 2.4..- .g. -w .....1. j. . p. q.. h...tt. 6 m_-#., u,.. y .i .m u -.. l%... '. i * *e.. ",. - .4 n -- v.- n..5, 4. .s ,w ..n. 4. f,. %.e i.,.. .~ ....r...-',.- 1 .._.g_. ..w u

g. o M

.: Tw, a o.7i. .,3,, W

o.. p n....

.gy .n p.a...,.. ..g., i> .2ia ..J j i.g ..e.. . n.. p. .g

l. t.,i.e.

- i.. .i g.,. }., 4.. i. ? .. t. i.; i s g.r.. .ia a. ,i. i y.. .e.

1. j..

.. t. j :,,. t . u.=.+p_ u, q.. .a at 1 y g - W.. .e. .i i..l ,. 2. g ,s. ..l .;4.. .i .v l.., t h. I G.} . g., ..i' {.: g. .[.; t. ..,.,.,Q.a .t . s,.q.s....... S.,. . r. e,, l i.]t. L. ti,...g. i,. 6,j. . 64 .4.. eg 3,. e .p;. s+.... .. u..:.: l, a.

..4

. _..,...!....i. _.. ;...2_...-,,.+ i,.***. 'L*.. a t-- L .p..... II.. l.r., '..1*.

4. 4 1

+,. - H e.t. ,4.,- ._.3.c.0. d.. *T 6 W.

h..f.

.s i .,.r .p. 9 \\ ..,,4,. e...

5. 3.~,

s.. ,.,+,, 4

p. (trJ. L.

., L..... e._ a.4 , $"4 g ..h:. ~.. .,1 o. s .A 4 ...e ...j.

r..

g . y.. ..a ./- g ,,i, 1 ;. 9.. O, .p..!. . T,2., p, r...

g. 3.r.

..a. ..i. ,+; .. {,.,l.., ..i.. 1.,. .i.1 1... T!1.11. g ,p).,,.., _.p a. i .. l. .4.. 42 ,o w i.- -..-,-

a e... - -,..4**
.,....e..

..i. .- T. ,.c-..- ....H eu..., a..,. .. t. r, I^ 5 s. \\... t. 4 . \\*. .. l ,.,. L, 4.,. 5 ..9 6........ .r..1s g.,.},.....4. ..p6....,.4 ....j ..g 4.. .1 , 9. g L A .4.. .., L.L,,. 4, g + .... L.. J. 4 1 a . g t. i# .,q.. r. .k. .e. ,...,....h_,. !p. .,.i. ,e q. l ~,.. ..~ ,a,. J .,. p. i,, .p... r g... .,.,5. .t.. a ..,2 .,. J,. . %.....,,a, N,.. e,. L.,..., t. 4. i... I.,.' .,a._ J. m .u. 4....,...._ g o 7.,....,, ., t- . t,. .w .t . I,.4.,. ,p, } +.... L..,. JT..... e. .,. ~... .i..u.,,.,. .,3 r

m..

... -7 y. ..a.. .m _ u. 7y v. i

. - 4.:.

l .. l i. l o, 1,.;.; i 1....,.. 1,. fl. i.. 11 ,.4..,.. J.,t. . i. i.... l. : l '., I 2 i ,-i ,I i.. i, 4,. 6 .e.1 i s ..i. 2 .414 .a, ..a. ..C*. ..,,i .,1

1..,.a

..,..,r,.,.r.!... .:t .. ~ 3. u .i. i..... 4

3..

,2

4..,

a..

.4 t. 3.. .'~'I~. !.,.3.g..,. .' '.p.' 4 n . ~. ' - ~~. *. * * '

. ~, ~ ',. '. ~.

~ '., *. * '.. ~. '.. '. 2,...l'.'._..TL.'..~. ~. '. '. '. ~ ...y l ..T.,*. . e ,...g ..t.

_J_,

,4 2:.. .us .. I._...i.... L. m

a.............

., s. 4o w. ,..,. _.u, .a. 2... t .3.,

4....

.T i 11.pJ... .n l. .,. e c... 1. . ti ; ...4 s. 4 u l... 3. L ,i. . : Fl _ i..: .,a .. s,. .e.- .,.... :. i

a..

u-.

p......

. '...l.' s e. 8. '.J.** I s.'

: i. '.

.t '.'. a" t.. I ' .111 .', l.'.tl 3 P.. .e. .f,! *,k-Ii,8 ' l. I 'tl.l.'.' I ~ w ] .,..... L. .it. a. f i,r.,. gb .. 1 L......:.. r. . u .q :: e .. ~....4. a 6 4 u.r...,n, .e4 a e . g. i.,... s..,.3..2 4. i.. .li . T.,.,e-.41. Q.2 ,,s

i...

.l v, J1. ..., 4...) 11,,...1 .e ..i . t.4 L,,,I ,614.,.I..%:. t... i 4.. g-

r. l j,',-4. !" t ).

4. l. J+...,.. t.

y. i p .I t.. . a...... 'e- .I. ~.M.,. gTg. i. + i. t.i -

i.. : 4-l-

j.,.. J.; ..... &,g. . l.e..,1 e,....!! t,.

i.,. 4.8 l....h ei

. e, 4, .I I. .g i .e ,., g.i g... J. a .,t e c a. ?

4., :

. g.g, g;; 4 g,.. ..a s i.; . p.., 41.. s. 6J.. .s. a .-+1

t. ':.

. v. - .6.. . H. i ..a .+

i r,, s... I'

r.-.

.-t :

e..,.

[g i. a f.,4 ,iti r' I i.e.T3 i . g-4%.- -... i. i .I,..g...,.-.4...-. .4. y., ,., A q-. a.r, 4 g. .q. g . +...,. -.-4.. + e f .T.,,. gJ.,1 ..'!3 ,...,. -.......}....... 4... ,+ 4, .., c.. 4,.. 1 r.. .i. .7 ..T' "."I- '.' 4' t.' .a p .c g 9 ... 44 ' - I

.,.]...;...,.

.f . $., -.,5,..6. , l _.., ,+ u,.

r v.,+14.1 '.-

.e. -o,- e y~ 4,...v ._l.., ....a. - y... *.. *. f l- ..6.. y j

\\ O. Coptcy ~ I 4 P M /uu~./' cron TGSTs- //p/Tro ENGINrals AA/c> Consrxacroxs / D'\\ ~;G sr 8/-8 -2_ (S~ 7~ 81) ATTACMtfENT WO : 9O7~2-STADAIC AXib S E t2 0 'MG

6) oc 6.

STLIOS ~ __.,J.a.., f *c : . 5 33{ s - ,3,,3,,3, m g q. c so" .L a A

21

+ mi P ~ alb r st" 1, s 4 I i' . i... I o~ 0 33 c GA6L s + e e L Tesr.Sar-up n.. -e.. o ggg % MV k 4 h / / 4 3 7 lO XY radt 2 9 s 7 y s (7-*d s seer a-a 9 GAGE A AY Ar1 GEM 12NT \\ I I

} 1.' .. g 1 y ?- 'h lb 'E ' o# 5 s ( k '4 i a-1 I Q i .Q R f J ,.s G h g O O b 0 0 g } - (v' y N., '+gg 9, g 10 ' o e7 b 8 9 a N \\') N N So ~ lD % gs { g ( D h h 4 4 NN^ t t t e s sg g o h b 0 h 0 g o a o o g d $p g k k k k O ON O D 0 *

c k

b rf d N D G d n G a e n ( Q f d o s k 4 4 6 h D a G o O g a 3 2 4 O o b g {' j (* s G o b 4 o O 4 e o 2 o w ggp g R R R R a. t t a 1 R N a R R R 6 s a 2 ,s s q ~ 5 3 y ? E 6 as j 1 6 a a 5 4 G g a h 's R 4 S k k k R S, S E k A N 4 q } f N R S kN N-O kgh l D 4 'k, k & sf 0 g f N N \\i h J h b[ O D N r4 e i a. a R R R R R R 'x R .s a s s R N,, s J

s t 3

A M a '. a R

l h 'd h

& {, l- 'i 0 d'm e LO da P O 4 4 'R 4 4' 4 0 R R R R. a kd 0-o k h ) %p h, O S 8 $ Q P n T l 4 a R R R R R R R =

u

? ) 'w) il s no W V 4 O o D o 0 0 o o O o % 4 .g R %s oH n o 9 o Q o o g o g ab 3 s 51 6 o o o o o o o g ig v a o o g; N X :h N N N N N N N N N N(N N N g[ is i T q r f h r' e' 3 }2. 'a,'g $0 4 ai o h; ( 0 B g ~ n 9 \\ o 4 o e n g g -9 m n s };l w <h k fi N n m o M i 4 b h h k g_. .j. 3 N 'g* I 4 1d t s k =4 yb L. E 6 o N r4 ,o -t t 3 h { -d( ,4. A M. L 2 0 o O o o o o o 4 0 9 o V v d o g M n rt a 6 6 d M 4 N N q H U h-Q .4 4 w .y '4 =? t 0 0 ru o o s q 9 o 8 o o o n ,g g I x 1 EC ,4 I o

f a 3

N N < d 6 n = RN et n N n n d to } B M 8 2 S

S 3

2 22 @* ~i \\ 4 Yy 7, g, N e u ~ + k * =' t k a A N it 's. ' 0 i is t o o e a es u o o R S 4 4 n n s m a t > ,e 4 y{ e 2 e o 2 x au 4

.+
~~.7. --- 4, ..... e.... l........ -... g ; 6,a; } pa a~~
~~s. o a..!~~
~~,4.t.,.4.,.. g w.. 4.s j gg .. ga. . q%..u g,. g~~
~~g..~~
~~..s. a. F.. g. aa 6 .. ~..a ..a.. 6. i. 4 s. ~ .L..i. .....,..,...i r. ..y-y *3...,. ..a l. t. s . i., p ..- a.a. 4. 1.t ...,.m.,...., R..J g '.-.- ~.g ;- .+ 4 +.i-4. 6.. J. r.,9'..g.. .p f e~~
~~1..:~~
~~..g~~
~~a., L 4.. 4 4.gJ.6~~
~~. L. g J~~
4.
~~A .4.-. ,.Q 4. 4 L , 9 '41, , j [:. 4. 3.. 4 ,6. ,a, I.L" 8 4~~
~~.., It.~~
~~., g I.. I., I, l,, ' r:... .. <l 1 ..,.1 r 1.- h. g.~~
. 2 8t.. '
df t..e,.. g 4. i.

M.3 r.t 4 +**.
~~-. 0 6 . t. j a r. i 84 v p,-N -h. t...... .g.... + ,r.i. p 4. - .s i.n,.~~
~~e..~~
e.
~~.. +.~~
~~a.i 2..a ... 4.,: ..s. .,.4 4 .L, -i...,w_.. 4.t. m:.. Lq 1t~~
~~a. _.,~~
~~., T.J.4,.... L.... ;. {.6 7 .w. A~~
p
~~...,.p t.h n.. a,..4.. .y... _. .u.y [. 6.. 4_ 6_ .a .T.. . g,. g .2e. 4.. u ...a... ..J 7 u. 2 j j...- 6 i. - ... i 7 *. ! ,, g,A. 1~~
t. e...

a...
~~2...;g..H. 4. ...2,.. .e, L,..... ... C .,. o. i o. t s.4 .i~~
~
i.
~~it..~~
~~7'..'.~~~
~~4,...-. ~.t.i.. *I' .n i 4,.. ...g g.,,...... '. ~.... i.~~
4
~~.P * *4... .,$!.l.~~
~~4..~~
~~s 4 ':~~
~~i. :..~~
~~.m g t* *.*g--".4.'.~~
~~- ~~~
i.p., .. 6...:tr.. r.. >. - ',t.- + ** l. g.. a ., ~.. r. "s. .y.'. i s . 3 .,*1 ...A,. .,a .l . -.......a i. s 4 .,+ i.l. j e... .. u,.%, .,i2.,i. .s.+ .,.a.. o .3 ..v......k. . 3.,- o s +.. e-m . g .6 5-. . ~..: ~.
~~t. i-9>~~
~~4. _.~~
~~. a~~
~~.a ...y. ... + g. J. l.,8. 4.9.- ,.,.a.4,. (4.,~...g ,j t. .,a.,.. L.. + g' 4 I...L,4 -: * ,3.*..~~
~~p* i-~~
~~.b ?.!..y. g p- .-* i .e- -.e]..-8 .g.. . [A.vg ..il e..g..t F 4-t.- a... ..p .4_g., p,.-q f.. 4 4 g s 4 = .t ..... %n.. _ m.....,. ....r. t.,r,g .y~~
~~u...~~
~~.n.... v,, 1..~~
~~a...~~
~~1 .t g. .,.1 -q .a. 4 ..g. l, .,.,J..3 L.... w .. t. m ....,4~~
~~9..,..~~
~~4 i. L..., -*.l. . s. - ,Ws. .L.... I,. 2. 1.. .S. i L. ag= 4 ...4.....'.t ~,.. - 1... .IA 4 g ..a .j..s .k.. 8. ... r..~~
A-
~~..J. a .h. ... ~~~
7. y

.., l a.
~~....a .... l.. -..t. .~*1,..6. u 9 ..s ,.,[ . a. 8 ..M.....y~~
~~.,... ~. :~~
~~...,.g -., p .46.,-&.. -.4.6 p... _ E,.....- 4 s. J. .a i..e .t. ..g .a. i. 66,, i. g. i .J. . ~.. ..g .4.. '.. r, I.~~
~~m..g.~~
~~.s t .s.-..~~
6

.E**
ih
~~r...~~
', '. *. **'.i,- .. *. *g . u.. ..d I. T.C) t*ir 2 a. 6.p ,e 4 I. 3...' -'.t. **..e .4: - i, .,3i -, i.e' 6. 6 4;. . T:. k-.. 4 w g. 3 [ p. .,...r. . ?:, r. u. i .n 4 3.-t 1: g vt.. .I+a. p.. . 6.,,,. d
~~1....f * '.~~
~~.r.. +l, { r? g g.,..,..,y -. M .e 37.r. ]t.. t..-,* .py ..g r ,8 ..a.. 11l. j 1 ..is ,a.~~
~~r.,i.~~
~~i :. i.. .5, i;. .asl u., ., -. 8. 4 i n...~~
~~o..~~
~~4 t,.i.. l ..l. ..L,,.. . e.,, ..I ail .6 J. .u e 4. L. -*)~~
~~5.l~~
~~...i3- *..,< t.. .;.J.. ;31 8.-..8 4h. . l.* ' 4. :...- a,. .. i 4 ,,i- - 14.i*.s.,.._...a.- t.o.5.~~
~~4. l.~~
.a r . p 4 ..e.- .t. 9, e. 9 g ;. p,. - \\ ..8.-{.. *- a ;., e ...a 6... ("".....,._i. ,,.fa r.s4 9.. ,..}4& 1. y 4:y g : n "~ f' a ~' c g .. r, - 4 4 4.4 .,,.,5,.... ...,.4. g. -- 1 .g A .,;..4 .s .....4 1.. s.r. *..... g .,. 7.. p g
~~.2 e~~
~~,,...g ..,..'{.. ..+4 ... ~ ..s,._ -. ~..~~
~~f * *- I -. -~~
~~4. y... -~~
..._.s ... -4,. s +-4-- - -. * + 3 t ,:....r.- --..r e. 1~...*. x, .,.L*~.~l...., 4...%. n. . g .......p a3 0 ...h.. 4 g ..2 ....a, , +... z,....... . A y. .a... .".,t.,. q .4,. .g.... .,7 ,.7 .... g.. p .. - L., gI .4., .t. ....; y -...p.,... :.:......4.. , l.,.. L.....J. ...i.., l'.,..s... .v... 4, . k.. L, 6.4. .s. 4.a .. f.5. 4... f 4. P,6 .\\ Q_ g.: q a t i e ..I. ,!....I2.. ,e.,
~~1..i.~~
~~4., I st i,, .3l ...s. ). t- , 4. e. It..i. s..g I. y N: i a .E g i .s e. .. +. g s... ...a. g g e. 3 .r._3,4~~
9. -.1...

u.
~~_9. n, .. g.r. e .g w g 9 4 m. y 2 ...... ~.. r u t... ~ _4. A i ..s. I t .g s T 8 ..d..._ _.l..... ".y.:. 2 ...s. .L 4 3 . r l _,. L a.p.~~
~~p. p....g~~
~~.4.. 1-.. t ... 4 _4 g f s. (.,. p. ,, b 2 u.r ..H ".a,...y- ...,,.,_i. ..g3 g .1. 1 + g ,, t .,.e t., .r . a f. e.t.- 4..1.. [.a. _...6 :,..,.~~
.r
...i.4 l-* yt. t. -,.r.r- .., __*4 4, q r.*. tv. o g gq 9 I. A .e. i f :~!... - .- l.i'-. 9 e. .,i. ,,4 ...l . *
r.
~~?+ r-a. - i~~
~~t s~~
6 4.,.. .,j a,. i.,,.s., 1 pQ. r ..-_.j.l.f 2 .i ...t 3_ ..c.e.6.e .i. p,.,..,i. .,1 . i p. 7. i. y a a. 4.4 .s a4. 4.......u... ..,. l. 4 .. a .i. 3...;.'. .. p.. .. ".. v. _.3 .4 .4, 4 4.t .2. f .,9.-. l a. ..,y. p .. _ p.. .4 .w.;., a ,r,. ! . ?.!. .: i.,. L., ; .--&]q,...,.. + t .g , 4 w,...i.t +- -.... i.. J+.~, 4 .en.3
~~1 T....ty,~~
.,. r y..t g.e. ..e.i. 3. ( + + + ,r. i., 7,,,. .....n... +.. a. 9 3.. .m....,. ,.i... .g i,,a .+, 6 4.. ~ a.... 6 g..]. f,,.. a.... i ;. ; g., u.L.,, !;a.,I n.L,.'. b., t n...; I p.. ..a,.!...i. p ,l ; a,. 6. t
~~t..~~
.u L;. L i..i. .v. +. ii4 i. .t.. i. e l-a. j p,........ _.1, o 4.... ~ .1 ., '. I. . m ..41. l ...,. _ + .I......,.. p y. ..w... ..a. .. _.a i. ...u .,. jh..... .+ a .,.3 .a.. a .4 e .. s., .m.a.......... .p.., .m .. 3 4,,...
~~r..,,~~
.... 6... q. .7 4j.p.c3, g . g.,. ..... m. , :. gg.g,, ,..e,..; g.,. ,g. ua 7# - q:. g. ,2 2.. .s ,i l 1 i 1 i s i-1 / o. o .o
m l ~ 'e O. CoPLEY //// TAD E N G/h'*f M S ^ ^ID [#^'#7"# ##~I## 0 FN'//W " TA T5 ^ C.. ....y; , ~7': 57 POl~ 0 ~k (5~ l~ 0l) ^ s MO : BO7~2. .~ A-rTAC HMEA/T STAosic AXts BENo'"G 6).0( r<. : STL/ D6
~~' ~~~
J'e : .....L...-. ...s.'.. ~ e }kk ~ . f, v:* 777 c3 Bi" 4 3 Q. J A ) -+. Esii m) P .c 6 r 6/' j a (? C )'- U l c 6 L 6AdE. " 3) D/Aa- ->^ .CO 7"Es 7".SE 7~-uP 0;ss. sest *2 j oost. GA'L *1 / / t 3 7 10 gy,,w 2 Y ) i c l t k . Scc.r A - A 1 \\ 1
I ~s g> g, e s, ON w o 3 n s I d 5 6 j 8 %q.4 { s t-1 y gg g' O 8 M 0 h h o 4 o g h d o \\ + b k N k k .ss s o o b 4 3 0 o o S m 0 0 s 4 *A a k s ( R k k O O R t E } ) o o d 4 3 a e hm O I I k h kU k {a k Q k k k { O_ k S N q w } t 9 o b
s
~~%g s x e* o u w x 9 N t S "h n A o A S N R R g M e A o o = k3 6 2. s o a v D 4* h b o w o o u M O o o O~~
\\
~~9 4 o 0 e ( 0 t} p { R q a R s* y a g s d 2 9 y o o y g o k g c O x s. e4 n en o T U o .g g *t O s g 1 R R R R R 3 a ( R R s g a' 4 j a R N 4 3 a f 5 h o k R 1 (v' R R 'A R R e t ia P g~~
~~3 4~~
~~II 7 ab k 8 [ ) a R 4 s s a R R s s c 4 4 g d O r v> e U' i EH h I p g h h 2 3 6 3 N 4 d~~
~~A t~~
~~E'x 2 {' R R R q e + i N k 7 mn a b m 8 o o N m \\) K g 9 3' 'a 'N &0 h Q h N s -0 y M + D h N N b ![ 4 5 .5 N n f 4 4 s a fC b O '\\2 N + V D kw 0 o o O c a o o e o o o y y~~
~~S t~~
<s s 3% 46 6 N N 6 N d 4 g k { g R -\\[ k sj? fo b N h a o n -e o o o 0 g .k -y y *b 44 et n 6 g o n i o n y g g, g a 4 m I o i x w 1t t 1 o $~ 1 8 1 0 D o O O o o O e {; w 3 9 0 g q q t 6 '{ .d g 3 NO R.1 4 et g 45 R O. i o k 3 u n O kk $0 { 1 9 0 o o N L3 o s m o o I 'o 0 0 8 M M k k O o e o e n 4 0 0 N 5 D m k
t
=3 h a 5 ~ ~ N T O i V.$ ..M. k. $ !C._ O NO $5 ,, m
't i / iJUL 16 RAI 210.71 ~ Provide a numerical example for each of the following flexible plate and bolt configurations showing the calculation of allowable axial loads and bending moments. a. Square plate /four bolts, either bolts. b. Rectangular plate /six bolts. Provide the loac-displacement curves for the anchored bolts on which the allowable bolt loads are based.
~~RESPONSE~~
Exhibit 210.71-1 includes calculation for the following cases: r a. Square plate with four bolts. b. Rectangular plate with six bolts. The allowable bolt loads are based on the following formula: Maximu:n Allowable Design Load = E" 4 Where Fu = Ultimate Static Capacity of the anchor based on manufacturers' static test for the applicable strength of concrete. Load - Displacement curve was not used for determing the allovable loads because the design loads are within the linear portion of the curve. b s 3
s . o., s g, EXHIBIT 210.71-1 O b e
'g a e a 4 e e A ? t I t i f l I I A. CALCULATIONS FOR SQUARE PLATE WITH FOUR BOLTS J c k e e ) I b
4 4
i m1 OF3 a.y

f., t g ogy tocS7 o g.
~~1 BOLT uncan . f p a e s T o O E T' d CONS \\oERATtO4. s / /~hoJ U5TED SoLT t MOTE-WHEEE THE USE ~ toCATioN i ; I~~
~~9. PEESEQ f 5 AM llNEEhSON~~
~~/ 9F THIS le DE516M i - ') g ABLE. 51T U AT)Ont SUCH I. _ D-l.I D i.l' ijj. CASE.WILL BE DISCLESED l ji .l p*' i .l Q-wrm THE I)EilGR '4 i g l t r su PEE.Vibo2. g O~~
(-
~~g ; .o t I a l~~
~~9 e~~
~~I j((:. .X-Q " J PH ylj j xm k ..s i. 4. ..o i My EN I q iH I /N ^ J i ,v w, .i ..i .t 'g N $ AL'L Lo A05 F'AWLTE.D t .. I m 'c : t l, i~~
~~r...~~
~~P sVa2TLoAb QM3~~
~~-- - - - -J.. [ i.. r i j i.-l - 9 N Pgs.MoRiz LOAD , 7..q t. 1 i : $ j. -t [j. .. 7.. L i t j. . k P = Diceq Taw.. y. .I ; : ...i I l ; n~~
~~: i 6.,';jli,.; !.',;~~
~~f i 'I Jg fcNTmis":,, i ; i i ' Le : 'f'. r e .i , i i (0,5. C NTMT - 3. ,- i .t, t a I }~~
f4
~~-lt I h ?~~
I
~~-b = Tuickass Ip_. .,..,..,? i f~~
~~j..~~
i. j %. i i. t ,_,.1 i. =.M..}+V .i i !i l ...s Fp=; d++ Vr m 24-f 'I i ;.. ;.;.: 2.i ..] ... l. p..j..k !.. t.J t..i !... l' ..i i .6 i i 9.i.... i .._ 4 2 TT F2 ' b+f M.: ' z. min 24. oa 76 "s0T Wok:i,! ?b+ fr j i "i" ---, - j. yo .T ,V.
~~C.To C, ALLOW gxcagD.~~
l L. (FU i !li -i i ! i T:=i P i- -! ' 4 i i '.t.J .i: . i. 4 i. ,' i.' j l l A..., ' ALLOW A.BLE. Dasl44.' j l l i . '{ 2 : M y: (Fh. - ALL 4-BOLT BA.5E $5 DESIC,N EO E CHECKED -i i v ALue.s. L' AFTER. 8/lo/8) To FUL FILL THIS CRITERI A. Tp:= P x F[xF4 i 4 i i.
~~DE s t 6tts. oF 4 Bo.LT....,.~~
~~T ; -- I ? (Te +;T + T' ): :.. r T i i B A55-Ri~~
~~- ! r. '-~~
~~l g v,.= py. (p-}...,, -i-. g T Se. AEacok. PeoJac.T j 7. .%;o, i A.UC,. t o s q sl l i V'i" P d ( F2) ; + 9 ',',,l' ~ l ~2~ g:b ' ZGS~~
~~M.J.TuLLIS iscooos. i i ! !~~
l . i...i I i ,.i. t l
t ! l,. i. : s. ;i dg 31, i,. q.,i.;ii.,i.!i i r ; ; Y,!..l'.p. :.,, i n.; j i i i . r ;
ri
~~,.. i~~
~~; i ;~~
~~4 i T 1 4 ! 4 ; 3,., i ' n '.' ". o. ;.. . l.. . c..: ;. t N, K ~ 4 1.3 }l N 8/ 7 ?'. i [ . l l l !. I l .j .i 8 i j .j. i I ./h / : !l i }..Q~j ;~~
. T.. i

t..
~~i %~~
,

i.e 4 J ;.4 i i
~~x 0,@ ]..N !.Si \\~~
~~! ; i-k l L i~~
~~-., i N.n. l.. i, r.-~~
ll i l i .,..i.. i + i ,l ga p X....\\aQiK t t- -l r. --- ! :i 4 -X. A (s . l. ;.. L. }. s 8 I t l t 0 Xt t Ur '- t .s .......n :_ ;.L..t._. - i i.t i ..i..}' i ' j_ ,. j- ,;i I i 1 i. .i_.... - _;.,... ~ _q .,i... 3.. -..
~~p. p.~~
~~7, I _..i i . - r_-.i..._t .I... 4 ._...4..._ .. :. T.. i.. i ] 1 J.. 4. -.. :~~
~~.,i....~~
~~l _ _1 .. ;._[ l _ 4 t. y .. w a... r. I t i ,. e i, i -(ty@ J. s. -]. 4.j.. }.i. -. _t~~
~~: i th '~~
~~--[- i t e-F t-j- +: ; .i.! !..~~
~~4. '..i.~~
~~7 j .jyy_, m -y .. i !. . 4 a, _. l .. !. 9 ('.i.[ _ . _...;,S .. i...;.. L. 1 .i. l.. ; f t , i j. j i . 7 7.- e~~
~~3. M h ** 2 f !~~
~~g{. ' l .. _l j,.. ..}._, ;~~
~~i. l.~~
~~L 1 I. .i _ _ _.. }' !.q g ,! l3' -j. .l : 1 : ~.L. .! - j i t 1 6 1... 4 l.J% j i ,. !.-.[ } .!i d. 3 i -s I _4~~
~~q. 4~~
~~. s , _ f... ._p 1,. q.! I y ). .i.s i h. 4 j -} l.t. 4 f' ;...i. i.. - 6 .t t i :~~
~~i l~~
~~g i l, N t t .. -, a. e. .. ) l g g 8 -- j gf i j.4 _.j. e j "I .... f._.~~
~~i f i~~
jr
~~i i~~
r 1 t;' d -;- -- -h r r 9..'....f i. I... ..). ...d. ., 4.. .p..l. .} h..I p .i , t _t. I g 4. i. a...,; i .i 2 ...i_.. g. ( , i ._.....,..,i i i t l.i -.i 9 'i t a ,a , g . i.= k TWCKMF55 17EQ' D : .g y. N i boe b 2 EFEEc.TIVE. WWW. !. t i ] _.._4._ f h......fd..;= j 2.Tj x y j q,j ' _.. _.f__:. J.. i t . i...L i 4. i. j i 1. i Tr.To TA t TEN. Fl?dM C AA.c.! !.; L !.4_ i i N i.2 T [.. i s me. 6 u toe.l iN e.s)'. _' _.....i_.i...i t ._..,i _ I 1.1.1..U.p 3 l j v .. ; 4'.e,,5 u.ow. eauwei sTeass! J ! 2. i _.j.J 4...a_.u. .'. _.I _ i .._ i...,. 3 i. ,. 7. _..,._..4 _u
~~..i ' b, t=t.mGE wip ru~~
~~',. ) !._ !.p.. i ' l S g f Ft70M cAi c s. l,;;.lj:~~
~~j. l j. j. ;,. ;. 4'.....~~
~~. pj..j., g. 1 I j t llll . i.i 6 i i, ;,; i i 4 4 ' !G M l 1,,7, i. .f[.;.1 ! n {.t ..I,, i~~
i
~~, ;,, j i. ,i, .,4 b.. .l !jl; .I ! i N ;...' THE L.WEEE OF j a ;.j ! i., !l-EITHES2. by l:og2.g,..!.i ! i i.~~
~~; I ! uSG~~

~~&,o.g, M y,.,4,.;; L,. i ;, !,._ _,j: gz.ng, nj .. forz. a c T a g. 7 + ...i . i. i.. D E.5 l EM o F'! 4. Bo LT ' 1, ;. i l ! lll LI ..:.i~~
~~4. _ :~~
~~. f. F -,. , 3 b -) [. i NOON O 1 ! j ;... .._;..; i... A a.i G 11/19 8 1 i. ...i~~
'3
~~!4 i .l~~
.j
~~. l.7 - 2 +8 8~~~
~~.j ; j y,TTyLLl5 ;,..~~
i.
~~li;,;~~
H -l t i i s**..,.H. - H, *.,.. f H. -i H -l-I - F- . i i.. _-.,.~.
!;i - i TE R OF 3 i i [ $ bile 3 EDGE DisTheocG 4 2 [ 'h 4 t i y l 3 g _.___...-_-_.g...,.. .p t ~ p.... 3 q,p 4 + f 3 m .._.....l.,... .. a.--... - -..-- - y. -. _ -. ,_4 FIEL.D Dl2iLL HOLES TO 5titT BOL7 LOCL\\ TION 5 .+1E 3 ...j %ve . -- O....,.... { _t ,A_ [ M ir4 ' E Ds c ~ o..D / 2 +pgs7gg cg y-r .,.. l
~~, ' +, *,,,._..*?$~~
A., i : @D)STAucE l ma sou r W ...3 1 . 4 BC l. ~T 5A'5E. FI'. D E.TN l L ~(FLE%lBillT1 O F Br0LT = k 1N i 2 AhBI O,1!2ECTION) I NOTE ON.THE D Est G M 5 xf TcH. S, c.A,sucok. P12 0J. t O l r s e W. r uLus 'l-24-81 SC0008 i t. g i EGS t
.~. i ',w, m a-tr GENERAL COMPUTATION SHEET l-CALC. SET NO. I Fa In22deng*nsam \\ neuu. a consvuescru anc. FINAL PSNH-SEABROOK STATION ./ - uwevis 1_&_2 V000 gI naus or couramv_ t STRUCTURAL CALCS-PIPE SUPPORT SHEET 4 0F /$ g J.0. 9 7 6.3. c o a g gy //g., gt.
~~, cour. sv cmco av ;~~
2B L. DRP DE O UN,E NO. //0/'4 BUILDING "g*jj,gg"j'i5 82 //I'M' 7 8O SUPPORT.NO i ISO. NO.- nin W-(W .]. 7) Mst- ) lssac ' L 4-to ~ % IAADS fx F, F Movement u i OBE SSE OBE SSE OBE SSE Therm other troti. 3 x i m4-so.u v i.e i i n.we. / / -/# -/74 -7 -7 [ ,3s L,,,, i, l thep.1 '/O -40 /o 48' 56 27 5 . Toe.1 rneto4e Tae n $26 $Sb ' d 0$ $l$b $ l50 $26Q
~~{g *f'@jc~~
~~~ o r,e w te PAD / TAD eK' Reqd. # lN 100 epee. Temp GOO~~
~~Ins -~~
~~IAD SAD Ref. Dwas. ** Rev.Eo. C Transient 605los 19tuQ 5~~
~~lof4c,~~
~~&dgm (4 c 3 tow 7~~
~~ELEt,~~
/0
~~j Total +~~
+'27 +53 o -/ GC /99 +%f m s 77 stec. z. -38 -99 -27o -3GG -/.57 -307 /v/447 G/6 C 7 I} w.1 - N/ Nortit f O [ g we in-i./ E4 (-M* '/%*
~~Comp., Coric.. Sc1..~~
Emb. Pl., HVAC, Elec.. ~ etc. e, p y Q w-nt_ a vtaw l 7 s o g v if o a u f ouM ut 5(-/ LOCATION PT.AN m.--- c_ -v---_.-+.,w.--,e.c. --,.,--..c.9 .-:-e-,-ce
,, h S807 "'* " GENERAL. COMPUTATION SHEET CALC. St:T NO. ntv' coase av CHAD of //rz D, R. P_ hi.n_ited e.ngineers ", _ " " ~ o mise m n o Eucor t'JNii--SEABROOK STATidMgg - #b 4' mo co m ns_ 'jg sneer A.or gifl0CTURAL CALCS-PIPE SUPPORT = ns.z ou, ^ i suaxcr
~~i. ' +j 4/~~
~~i l i i ..y - j l //2 SYSTEM l-x. AWR ( l] //f'/'4" A:1.DII.G ' "'ao/r i ., 3 LINE NO. _ . ! ! l~ i ! ..f_.. ! ! h.b~~
~~i...d. i *ii 6"'##~~~
~~SUPPORT NO. //2 4I t_i l i ISO. NO. _ ,.i. ' i <w' i,- g i . $lf,~~
~~g i~~
.I. ', i *: ~ j4 ,. s .iie , e : I ; i ...p; ; fr ' l',7 W 4*c 8. ' ! f, i .p i..,. .l_ e !' t ,.i .i .3 I. ' i J,. I,. .... l,. I. :;. l_l,l.. 1. ! , ;p..'L._,. 4ff 63,6, l~I i-I. l ~l T [.. i / i 7ve
~~- r ri t'~~
~~y j 7. r .u... g .y, l l g e I i! i gx { lj.l h"'l'!* " I W T $$n.b& _.u'. .,1 _M (s ) p_/ j c 'I s ]g i ,7~~
4. +.;. ;.

i.,
~~(' was ,\\ g 1. no l. :. u. r 4 t Q e og U~~
~~~. -[ -.~~
~~--s e~~
e. r 2..., J. ' p wlfg*Aq,. Q fvF* 'L mw\\ '/ *
~~.'~.~~
~ r f ,j W'lf V3 ag,,e G H .Fec.c & (} %-o d m,c e tr Ig&) . l-g l /"Gm:ll-i .? ? .s. _..~..a n 1 s t. 1,g .l .s,. s ( 4 a p tA t ,r g., 1 : SECT /0//. 4-4 s-/47/ A e reus s' s h'- .W/k/ Grim!d i 1 l 1 _~ ..W%,- 1 a i d 'm %.% p j hl 4 s i i i s. E m g - S c xt.n. v 7 Y v i a g;t," is,i py* mmqroy' ~ ~ts .-e :e Y c a 1, j. \\ .'o.h.T+.~<hORIGINAL' g. i ]!$,3 F CALCULATIONS t l 4 g. BASE If /) ETA- - _. - - - -.- 3.. ;,- _ _,_,./.L ,,-n
,,,y>***-- GENti.HAL. COMt*UTATION SHEET CALC. SET NO. EY Con et CHWD SY ',o.sCEmo h.m._itellengineers
~~5L D.P./?~~
~~N/82 - EUr-e2 - Q e,,"e,g PSNH-SEABROOK STAT 10N unms /b' "^ 15 x IS s str STRUCTURAL CALCS-PIPE SUPPORT m yyGy 006 suocer ,, i l.}.. ......g.~~
~~3 AWR~~
_ SYSTEM --===== = i t ! t LINE NO. //E-/4, BUILDING _capar 1 l. i t i. e o//2 SUPPORT NO. p,r.g_7 s. -y Jj is0. NO. i i C//Ect BASG k [SEE s/lesf of lk-fae'.myA/L . lI .] / h ,.rh *.l69.fll) lh 7 &g 1-f i. ! ' 6 h ) '.}l1 4j........ i, j.f) ll'f
~~f45/ g~~
~~. ll lf hh*_.%84 fit)~~
~~5We~~
~~/ fg *L.! j. p. ...i. i.'260],g hy~~
~~. !._a _.~~
i I .1. I..L L..! _.- ! I _ L.L.\\. i ' '.6 + 6 ii Li ! .... t.. ; i l[:7/45)f 6 ' _..- Q d68 4 0.6E - - - j-- -- ---. j ---l-.j - 4.-. -- l.. ]-.-. t. v.. u.. ---) - j..l l .H' l 9 [= zSo? (s.sb);20/,ne'_ ~ f /So27 age) frozpw !. _. g.o..'_. _. _._ i. p g ;ga.. . o.o -3... .u 7 g....;. 1._ i t.. :._ ;. .,t._.. _..: _J. _t. 0.61= /bfpei .!.. L L ! 1. Q = %& x 0.68 x i i i i.i
~~t i i~~
~~.'j'~=/:7(zolt/ZoW14- = __/0% W i... C..~.~.~..i~~
~~j"i ip i~~
~~- i 1. . i: .l ]-) l~[]~~l~-~[] i fi l TiI .l 7 ~I l, ~ - I i t { ! ' ; ;,/S9 (Me) t 2(411 [ T y [ )( j g g yy '% y f= Iij 1 = /20 kj- $_? / 2&DI : 3So N /I#~~
j.
~~^ .0,66 < /,o Ms 4- /bri A%. .EA = JBM 3 76 ' .j- =~~
~~p,.~~
~~3 t l 5 4 210 y-;.. i..... ; rogs Syd w/ex. i G =- l. xx B/ect / BeMo/w' s !..I j.j...l_- J. l - j [ -s= & v245/8 .,i~~
~~i O~~
~~/sycoy z2 9 'iO' 05 'O-76 ili,.I!.YIij.I!I [i!!I_ 1 L! : i~~
~~i. ;/sg.///7;//cd, /~~
l f i .,i i i, [- h. .I.. I e J s. *.. m' - n ~-.-esr-*- , --ymoyt e.e p
reeshot mA 3.n GENERAL COMPUTATION SHEET CALC. SET NO. MIc CRU 3385 PRELIM.
~~s. ~. n~~
""^' -? v PSNH-SEABROOK STATION I * / NAME OF COMPANY _ UNIT /S 1 A 9 V0iD STRUCTURAL CALCS-PlPE SUPPORT ' SHEET /.6 OF/' 7g ' * *c' J.O. 9 % 3. o o 6 m i "r COMP. BY lCHK'OBYf CC 'AWR 819 SYSTEM 3e..r -E .1 LINE NO.cc-M-*-tsi-S BUILDING CM o * g,i
^
~~f, ISO. NO: Bon Ri9 SUPPORT NO 839'RG"3 48 sr i ,u,zy / oair o.1c S'Ql.$f ~F-2/. Q l f:53 ().f f L'/-l'd R._OQ LOADS ~~~ t F F F Movement x y e OBE lSSE OBE SSE OBE SSE Therm 10ther Total~~
~~x i~~
~~i g j y .A. i al~~
~~1. cow p. /f 7 i n.wt.~~
~~- 33 -3S \\ / 70 70 i g ^ 2 - 59/ -rst \\ / -loo 4 -loo 4~~
~~Total Includes Therm~~
~~[. .[. p g safet a t 453 i/3oa \\. / t1618 tn3c sge pp sch.c.a .. D ~ PAD / TAD \\ [ ' K' Reqd. I%1OO */4-IAD \\ / Oper. Temp 3en* Ins - y - /* N. SAD s _/ Transient / \\ Ref. Dugs. **- Rev.No. l l~~
l
~~\\ PIPitt&- daE/V/ '.*2 - o-~~
[
~~k. Cohc /$/4 05 SC) [ l / \\ fLsci~ 3 ol'!*e B ? .a ~;. Total-+ +-: Lit. tl2/, L / k + 1L%6 4-33oc ///Ac,. c.g/.v 9 ,L ' e.- < Total - -/199 -192C) I ) 'A3ft - (l') 0 Korth. I .. ~~~
f
~~. c 'y~~
~~c s~~
~~~ .~~~
t,;.
Exig,tuq
~~,e, 1 y ,. 't f .D YNN (',}$T M" T A~~
~~Comp., Conc., Stl.,~~
~~S/9 /26 - 3l Emb. Pl.,llVAC, Elec., t C, * (G EL 8'-$) etc.~~
~~i. r. -~~
~~s j p Q-J o S 11 9 g/,\\. c~~
9
~~e...~~
a;. M s = y n a ~ 36 7L, g (.l. 1 1.0 CATION PLAN f- -50 A&fGb/t U / memee m emens
penissaw mor.tm GENERAL COMPUTATION SHEET CALC. SET No. arv coup ey cwxo av O s, f*
~~N""QMg$~~
~~Q g~~
~~t. bC.8/~~
/ n;-el DAT OA10 FINAL C PSNH-SEABROOK STATION _ jpg vo o ^ STRUCTURAL CALCS-PIPE SUPPORT a 9766. CO6 SWRJECT l'e i I ;il i, I ,t _._..: ' i,i-_. .l { 1 7_1___..... --. ! I t . i ! f 3 .. H.d.Qq..i,. .p. N SYSTEM C-C- ...-. 7 AWR
~~7.. ~.i.,!,_-...~~
~~LIN. E NO.CNNI ~ CN ~ BUILDING i ISO. NO. MO/S SUPPORT NO. OU-3~~

~~'- ri l~~

~~~ i ., ; t,;.; l . $4ce4 <$ (CM. ANCMax Eol7' ; _(S7.o. A147 No-607-7) 5/78',._...iGtc.c.rs negleclec A-g ~ l I 1 .. _.. _ /6 v r-F'j... l l = 1 !Is-ara - 24~~
~~i i~~
~~i l p.,ggy.f.t hynf,,%, _ _ _ _ _ = . y.. _,,_; e, n a- ~~ s Y/= C6)_%. H = 55/0, M 70/Of ~~ ~ ' t 2 / t. ry m_. J i ! t Q Q ,, i p.. s<a a = 2 2.b_.,.6 =/ 95,, ,; -y l w* I ' I i i 6 +~~
~~4..s~~
~~.a + g'.pp',925-ij.gg_gf* .g_.;-- . %. g. '-- I'~~
/
- e 5.. s y Y-d Fe-Md7SF/ W~' T : j Idj .jdl j 1 { ti~4._Y:lfc,) M ~ o i: 1 t -, o f. b . 2 d ie 2.s., s',' G o i !. t. i s. w ~I. s ; ir n fe.rricArrg g/,4...- . ~ Ni._TSo' Y(a bake is ' / ext /e, ' oc'= l 2 ., ; j_.. f k,.- ,_.' i _l,(l.e. t.u.. h..,== cj/c C/bo/h = /O G .1 .....- r l W .~.' 'O .,7, pg Q k cf-19[ = 9;25) 250 7.b~= /096 ss t . _ =. 'g ___,..u. ~ _w ._,..c.,a.. e..i.,_ 7' 0.5_/r. /! _o....ca.fcufa$2n.. ...{../>.i. _y_ -. _.,..._ .._._ _. l_'..' ; 1~.__'.So!. . __ j r i m 1i .,- 7.g.""-i, **N, u m k"" '"osic n in ll4, ## clie. '(on' e. cm. ehce-yp..r*** : f e +; ..m. e L.y____ t,3y) f ix - l-rt -r - ; /O s A g .../0_5 2 i c a. p,. n
~~i. '~~
~~g I ! l l t I .t. o' f rcc :. 2/78= 795 !_i p l...& lea, 'in C.mc. anchor.ct'a.c.f.~~
~~p..~~
u_ i1 .t (m. . i - r r ' -,e -.7/ 8 r, r 0 I e i f ... _ _ t' __. }. - t - ' -- t L3 - i - '----- L -t' -,r - t- - i-l--- i-- i --- -I------.- <5 o a n - - V & ;,n M ;h,,cf,g,((g(f Jo p ,,((, 5gg,jt,g ri i -.7 ._.- r-- l - ' .. ;.. l.._.. i _.l
~~l _. >~~
~~,. _.l.,. j. y l 1 % r i I l;.*. i I:~~
~~i. i..,,~~
i...l i .. ; 9 4, L. . g-g, t b.
4 "PP*. GENERAL COMPUTATION SHEET CALC. SET NO. trev COMP er CHro av M'" .h h*mited engineers d.' 3r FINAL tOYdet .4AT5-01 DA D I a.- ). COMPANY.PSNH-SEABROOK STATION / m a^mc ' va UNIT /S (__ saccr ?/ or /., 7 i STRUCTURAL CALCS-PIPE SUPPORT Ja 9763.CC6 sus;cCT i ..e , i i;;;i.._ i.. 5...., gi: O._, )._., i - i AWR O/8 ..C' C - .d..J A L. : ~ SYSTEM LINE NO.mB/S-?/52MBUILDING ~'~l,..,.i,...,,.. NT h ISO. NO. 000 0/8 - SUPPORT NO. 8/N'S ."l l f' 4 ' ' ;.' y
~~4....~~
~~.=.s.k,in k /t dat lo Ertronal mc.m.cnh. E6/6 i,J _ teg , yfg,,,g~~
~~-A.sclomg, coege/~~
~~-.. = - =. l y - 7, i ,L--....... b e in k / M 1; d. <rc J..._..;_ G^. G r 4 5 % /3 2 ern.=.le. I.t w. I i !;i i. i I : ! 3.~Tofaf.slae in f >> =~~79E-?/39= 397 i i i, ,,g i~~
~~j i~~
~~I&caftlboM & Tyduedica186&ctid'= e2~~
~~i. i :~~
~~O > C ~ ii.>,.~~
~~; O I?T Tgfal s/wr a,ry o =~~
/42_gi;2 - 274, i l i __t iii i : iii:;p ie i;, H,,, ;,,if. e;.scu. fa, n. -/ s/ua, r= -(727 - e67 * -r 4.._. _ ~~(.~.'A//awable ?ension valed Gf (/Mi ) dia fonc. Anc/ 4llowable.sAear-vakt cf (tj4 ") dio. Gnc. Anchas ea50 =7602 i x n.s !. :. lN iFg ACTION o*- -r 36l n0*00 kl _ ~~'~ S'OEO r k ~ ~ .j. l 750g b746 -.-? 7.. [cr>servaave, a.s C;/crcc c>/.-le etofois,el r . -...FAW & THg s- ,_s w,fa r, (c a,,.v;in. . i ; i _ _ _. _ __ ; i ~ - I. i. N /YlOYL[ts'lQ$)6a.f flG' flCC t$U ht.Csss/1cj~&'o/)ggz,{(g-0) ~ ~ ,L...}. l..[... 7. j.} }. }..., l ; (/,.33opg),x7.g5 (m,cte,.,,9,-fiu. o ..l......., so,,,, g,, c 7 _.,, ...~? ~l.' G. G[p{d &//>): /5x OW jgg y) fl'hfhg .. _f._l 9,. g _ j ..g. g l} lb 9f., SlC00 ~ = /*//OG i n,f,f ~~~
et a e 8 e 4 e I* M CULATIONS FOR REM AneULAR PLATE WITH SIX. BOLTS e 0 9 e e 6
1 i 'seem peor am 3.n - GENERAL COMPUTATION SHEET CALC. SET NO. lit dSBIS PRELIM. FINAL f ', PSNH-SEABROOK STATION USHT/S I 1 2 VOID (* asAus of COMPANY STRUCTURAL CALCS-PIPE SUPPORT SHEET 2 OF t.3 s SUSMCT J.O. 9 16 3. o c.6 .g - \\ COf.tP. BY CHX'O BY j g.g gg4 _ C,,c, ~1 '19
9F t.lt ly' LIN,E NO."'* *" BUILDING C NM

0 at<

a's A l, b2 4 -rs. n z.
~~ISO. NO: b 7 1'5 SUPPORI Nd M ' M *4 DATE 0410 6 \\"I560G 1. Dtem B.b 6% TAADS r-.u.4c. r to 4 42 A' Fx F F Movetsent y r 'b L3E SSE OBE SSE OBE SSE 'Ihem Other trotsi~~
~~i X~~
~~. c.,P . n'..ia i e s-Y . - U+' :. Mt.' .Wr f _gq _q 3,g, z 1\\uO ' \\ \\ te O~~
~~Total Includes inern~~
'gher.nl ' e4 g t gog.4 Safety Class 5 4 8*h"If Pipe Dia, t '2.** Sch./n 5 FAD / TAD ~2.% i ' Reqd. ' t O *l.. K IAD oper. Temp (A &c-Ins - NM ~ t49 }- 3g3 r O Transient Ref. Dugs. ** Rev.Ko. l \\ 0 i d.C) b 7 Qc A \\c.m d. - 6 0 41 'Z C3 4. ~ Total + (3430 - U&b 3 g o i., o 9 @) N4 N'D N 3 D9 I D 4 vcital - North j 46-sl F.';;c h PS ^itt,_1. o cmd k
i.
~~! ;*.{ f. m; V. n ', ' ' ? \\.'. l * - IS'-u ro~~
~~Comp.. Cone.,.Stl..~~
~~giI Emb. Pl., HVAC. Elec., -4 q 'P* e-et. Tis.'2. t%*Z FZ' . cmme etc. s e ). L E:\\. Qo' cD) l ~. .. / I~~
, l*
~~SO9Po9.T ~' TVD. m.A R t O' o.) ,,.7..,. t.. .,s -,;, f.,,< j 'd I~~
~~x. s ' a -~~
l 1.0CATipt! T*1.AN
ponsseer arv.7ns C ENER A1., COMPUTATION SHEET CALC. SET No. nEv coup av c,a o of gy.7_ ,.py9 ncua ioiscieuN o .intted e.mngineers o DAM 4' "8f bg"/E 04 meor PSNH-SEAB.TG0K STATION va .C cot 4PANY UNIT /S \\k7 saccr S o' 13 (~ ^ " 'd% 6.co co STRUCTURAL CALCS-PIPE SUPPORT susxcT -kWR -- N-SYSTEM M -LINE N0.cc.. Tis. z m.ra BUILDING caw'- i . iS 0. s. _..._ _.,.,.._. _..! SUPPORT NO. T 1=D.%4 0. s,e c
b

/ :..:
~~s ! i ; ,:. s i : ,i,. l ,ta... , i ! s.~~
~~_..... _. : a..,.._,,_:,i.. -. _ _. _.~~
~~i i i = l l l.,~~
1,
. ~.:. : -... -.. - n .. s,..,.....g. _. _ : 3 ! i.e= ev.2,r...a. I i m I ffI !- __._ l ;4 6a _ IP S'*IME g .I f, I i c rt w.s r.._ _. ie mp [;j -,, ec. n s u m m e _-:L__Ji 'Lt.J L_ a _ 2 >:- t m. so -e -g=, m----- y-3; i a y D-3.._ .i..."' %, gmw.ss-. i i 1 't l l i CkEd O tere: 1 kt Mr M Ef.9.5, II 8 .r/ ~ AR.f= VJ 4 s t 3 O amu 9...A,:-' s.: i NN-I . huu.v.s.d C>mcem se.. _ _. _.. _ _ sci-t. ro +, l I, c.s., _._ %g ec. _ li t i i i ene:)_ _3'- s s'- s i i !! i! i ! i i : %,! I 4.-9 I I i l 1 ii i l l i! : iT ~ PtA.a - Lec.e se,d PM t Y I - $ r.. y 2-A EYk /Vffs. /e~r % css 4 1 4XA 7 4 ,,7 g
~~p. 2 a e g~~
, L' t - ',. c,g,.og e,s, 'A vey i _., _1.. V. psm.. S 3%b'A.k A ms !\\1 ' ! i S ,A c,.e! w. 44 is o w.ss i i-j j i i< i3 ).,. s.,g,. :..,, w w. .s ..c M et> O w o.* se.. \\ U- " -r' .e \\ \\ .lJ / + i I Ll !i!'7 \\/ " ' ?' E z N II I, cc M.T.~i.a k, CT 2 '?Q yx /M'f m x s7. ' w a . es. r m ! i L, u s 3.. (M. i !. :.. :.,e /. V.Tg? 4 w g 3 '.9.NN.:,wl N /rre I 5-ej t s 1 iT1.. 6' / ^- 4 [ 1 \\. '. v' "M -I f @ .t$Ij U " M '.- _. p_ ei.n.trm)_.....'s.......s. ..f_. L i. _.. i_. L_ L. L. ';- r.. m ': - H L ._ _ j_j.!. !._. t-.m v m se a u_c, 14 ei,n i
GENCRAl. COMPUTATION SHEET CALC. SET No. at./ comp CY CHAO.CY hmited engineers 8N
~~S o~~
~~FINAL gAf g ggyg 4.G*8'l ////YA? NAMEOF PSNH-SEABROOK STATION ica COMPANY UNIT /S STRUCTURAL CALCS--PIPE SUPPORT~~
~~'3% 3.cou su m j~~
., i i.. f i, ii i __l cVSTEM. c c, _AWR n,co t IINE NO.ce M;7 ic,N-- ' D!!'G C*# ___ ~- l - - -- ~ .iS O. N O. S M --- do?PCRT NO.m.o 4 l 6Me N 'C:c.5 % s.1. SQc.s PSb C,osdeI w.mL bCab% 2 6 *t. re, "2.t.r4 Y f i, t!i c-uF c w u-t i i I _s , o w s: (w % cm.u, ' i % 5._(.a.Ml (. to 4) Lu.2s + s) (:u u. m> A. e.ao u,_tL
~~0/ ( r).s. 4 Q s~~
~~1 f _ _ p __ & _ _._ (s.svts +s'3f(2 s.euss +s')s c.,eu i i ~ i i..- ~ T.-c s.c.c.s Me D .,.d i ____ te t is, o Eh6 *' d *, 7-5. s Ii \\'2~~
~~Os O~~
~~. i i i I ___E. TAN : 2 0 5 '2.'d~~
F-T 5 17 82*
~~i I i~~
~~_ y.~~
~~-O- - -G-te u _\\b,8 3 's~~
~~M$ G> n o' V.~~
_a__. s .,o I hI .I I Ii _} I ti.'.(,s\\ cbWa l 1625 c. 643 2 9 3 5' t 3 ,'i! - I I j_ __!_ '_... Tr. s (,,2 es't.*
l 1o. 25, o. l ot, s 141*
~~I i ' -re.a_6 rio S.c.64*h1.o. iou : 2.6ct~~
i
~~__.0 1 ' i i ! ! I en -._'Tr s ).'t (<3 B5' 4-I 41 * & 7 8c>b : 466'Z ' -~ \\h :. (,V'16'l2)c.64S + (,16F.ib e f bb. 25) { ~ i~~
~~q, g C~~
~~,3 e i i h t (,,11t'l'lt) o.-}ch. + (14Eh"e j 6 3. 6.9,tr. l I I I~~
~~i. t ' i '~~
~~t I i s_ ~ %2~~
~~f l I~~
'2'- 0 72 i l l I I i i i ( l %sl dul' I i i. Y t_t1_Ll..._l_.il. - l l. I L_1 i i i ....Wr. 465?")t,8,4.o* 4 461 * / OoSc5 s O.151 !. USE \\ '@ b4 I ' i - i m __. . _.. __. __._ h __ L !._ - fi._!_.L.;_. i__. E Th. ic.k< ed ess ' P F G ' h l
~~1. _.~~
~~O ,..!._.1 Mo.. z w a, u 4use, o.v.= uo,o.w. m L V \\1 _."2 rr '( E 7. $ 4b528 v. 9.6 5' 5 B*3.~l 64's ig }. ._....L I i G 60,0 b N_/(iO,(Ocn M.6~~
~~0. M t-._~~
q i I. '2 o j yjd1_ l _-(3 s 3Joj'R9 M_4. Jk}[_19,o to e t".) __.,_ i j. p. j.. ;. i r - t s - i 1 l
' ' rann sehr ea.ute GENERAL COMPUTATION SHEET CALC. SET NO. Rn cour av CHK'O 27 (g"mited engineeca E aw/ axsaru"" F.NAL DATL D a.t..en -1 }n NAME OF PSNH-SEABF.00K STATION san . COMPANY - UMT/S SHEET to 0F l "3 ,_-SU8 JECT STRUCTURAL CALCS-Pir'E Sur' PORT '" S l u 'b. oct. ,. - + -.... _. -. __..._..-._..i_... l S..Y..ST.EM... i - - i i .j_._ _. ~AWR.. _ ne u-LINE NO.cc.mmm.12 91 DING C'"" ISO. NO. te ne--- a,PPORT NO. ne.h4 i__._..__ bes R Cx.-sG4 (C ee'b ! i:
~~1 i i~~
~~~ a - l. l~~
~~' ' l e~~
~~e r ov,3._ C.E.g re A.. bow es I i,. l I F_ i_3__ c. 643 _ __.. fI F-7.. U. ara._ h ("L 17.+ h _8 ('D.D l6.+ C )l (,7.w 9.4616 ' +b)~~
~~O.bo 8 o~~
a i! ' t i I! Tt_:_(,n,.o 66.d / t Sh.6% As 46*._ l I !i r e _ (._. 2 e s 2. p o. w o. u c s, u 2 i - ! l l -T'P t /=.no.' 3. o.l.o4"6 w c u c5._s.._2.4co' ' i I i !l l l ! i (Q ' Tr.s. b t ( 546*. &. 121 '_ 4. 't_4=oD L34 8>3 *. V i ! : i ! - i 2 l I I [Vij io'l'2) o.Le 4'h.&. (.yoF6"a l L. 6.%) t.e i.L. _ i i i. 't. +/.z) o hos.+ (,iu ar-l EnSW)s sus'. -__ W in r. ;__ - ,- r r_c m _ _._. 316'] eoGo' s O. E. E L 1. q V9.C_b 'Ua.___ r. C.. = 36 86 */ 6 EAd 4 8 ~ h !! ' l _; J'~[ l. i ; ! ; ! ;.__ l l !I k T w::.we '.c-%. I2.C.Ch' A.._. _ I I._.._'__I._.._ I M p. s 1 ~ C T-N. 2. 75 0 6 63 w 9.S"15 %. Y1,~lD">** IIIl M 13._ 2.Tt g_
_.__-7._ v. 3 to BB.w t. s..:__4'h 6 le a l !. ! ! : - '
I iI.6 = ( a m ci w d f( i e,e co, u t.c ; _ _ _.o.c>s .:.uw _WO %_ = I n _M J h et, enn 'N/ ie. sees is Y_ =_ o,_w..._. t_.._._.. hok f A4 (. t & L.M C,gt gf M ll % l( i I I Lt E j t Lii: i i a p Q j_. j i -i v,- _i s .1 -l e l [ 'l a i e .. :. l q .p. ..__.._...g...,.
' F0" GENERAL COMPUTATION SHEET -CALC. SET NO. Rtv com> of CHC0 DY . hm!tEd enginecm F c?j/h ""5 " ' " " o FINAL DATE DATE d * ' E"- W /<D PSNH-SEABriOOK STATION vwo NAME OF UNIT /S I COMPANY setti_ 11 or.. -i3 STRUCTURAL CALCS-PIPE SUPPORT w +-i uN. ce<., suaxcr = .....-.~.-s -. - - 41 ' ^ - -AWR - Tle --- . SYSTEM ~ - - ~ ~

~~.- = _._-~~

~~=... _LINE.NO.ce m '2 tM it_.' cikG. c.w,-~~
~~i i !~~
~~. - ~ ~ '~ ~ ___ s.,.90. _R_T_N. 0.. Mvs.u i~.A LSO. NO. eco-iW I "-th a % @~ teva O ier*E~ h w C % v_ enc _w l p- { t -j -t - - t - l --; 1 1--- ,t-t-T-I i iit i i l D i i t e _ o,/ 2 6 'c , W,~~
~~t_ _. _..~~
~~II I i M,._ 8 %, i _;.1 r-t -- -- i - -j i .. i.c i i I i ( ; i a I /N /\\ fl l fl ( t g I I i !I c i I I ' 1j M g i ~ i ;~~
i ii

i!
s L. t. i I I ' ; i p N l l 1-1 I.i. _ _. _._'_v ,_,v-- f , l l 4' l i e g, i . i I I I _ _. _7 ; _ _. _ ,l g, e n I L + _._ m _..__._. ,l I /% r% v U l - l l _ g r. y i .I _. - _... ~ ~ l- _..[_ _ L.. _ 1 t i I '...a.. ' I ) f - w _. - l -l- -._. s 1-f ! ,[ f. . *i {._.'.,' 1 l 4. I.__I . !.._.I l l 8 l r,.,...r {nj p .7 3 I \\-, I -f ri r-i .__. m - --l l _.4 ,l [ __ g. ).. i... ! l I .4_.~....,. ( l g i 1 I ...I I.I I.. . I ....I f. I
- dMT new.a.n GENERAL COMPUTATION SHEET CALC. SET NO. aconstructorsinc.[RSSIS Ui$3d 6C PRELIM. "f M FIN AL PSNH-SEABROOK STATION e' UNIT /S 1 & 1 VOID / NAmt or COMPANY _ .J STRUCTURAL CALCS-PIPE SUPPORT SHEET /-f OF /g% ' SUSJECT J.O. 9 7.1,3.oo o At COMP. BY CHK'OBY y AWR SYSTEM M sr-b LINE NO. C*E/9'I*B2*E BUILDING
"M'*W.

j '..y,, yQ_ q,
~~ISO. NO A~o *9 SUPPORT NO_ 8/9 26-2. s.A oiu x u r 4/.r. J. 1 -~.1. T PiPa DATE D TE IAADS - ~ ~ ~ L>f. !?...r%% /.CS(Jf' */ ~ bp% F F Movement e.,, - x v r ~' I Therm 10ther Total~~
~~OBE SSE OBE SSE OBE~~
~~.SSE \\ / X a.o 3'l it cro { -+. a s ) Y +. 8 ? 'l it !?4 l-955 . D.Wt. -9~~
)
k [ 3 3 g ,,,,3 93.p,Ns i+ f2o 59 n \\ / - st -n warurewaas nere - IS*rc*** w +sa +~nu \\ / ta+ na Pipe. Dia. Sch. Vo Seismic PAD / TAD k [ ' K' Reqd. I x 100 "- ~ J, LAD k [ Oper. Temp h ~ Ins - y a t s/ Transient / \\ ~ Ref. Dwgs. * * - .l Rev.No. I' l '\\- ~~ PIPIAl6 805/03 Q. . -../.....g, g,ye f,jgcf g .....,-j ... \\.. EL&c. * --? /a sn 9 'l . Total + - +.9ffI ti?So /- \\ + 317 + 43l S v A c. 6,q f.g 9 .2 .,.at33 _ -- W -87 M / \\..-- 3 3 $ - 647 q Apwd f., /v( 2-a.'.,. M/ .,9. g.... ..w u ~ ort 4 .S 'I / . -[s h.votD DDE TO LD A D fcrint., 44 ops *sJ ' i,*,t. to/ .\\ N i c tItge g s., e.E E ftM E. j g. S. ,- ** Comp., Cone., Stl., L.- ,*'w,- b-. Emb. Pl., HVAC, Elec., e a ,l e$ v;. etc. as -s "n. 819-%-Ll
~~c..~~
g ar, 3 ~ ~.. ? e / O j y 40,- j'* U?- LOCATION PLAN 00' lh Woi -- r - r m
,e . GENEftAL COMPUTATION SHEET ~ ,,. mtern as.n CALC. SET NO. A E' b '" [R'I3d @MfH$8l8 PREUM. a conovuctore nr.J ""^' ~~ '- ./ P5NH-SEABROOK STATION umm t.A 2 vo80 6,=== o, come.v SHEET 4a. OF 13 7 s STRUCTURAL CALCS-PIPE SUPPORT J.O. 97 C3. ooG } -t. C C-AWR-8' 9 ' SYSTEM d ^>T""T 0 LIN,E NO.C C-8 8 9 '5' 's2 - s" BUILDING
~~^ "~~
~~ISO.NO: 80 Sl9 SUPPORT.NO 819-4*L ' S 40H' W 8 M' I. Z. i un 3-t - 8 2. 3-//-$2., nu l % IssueTF'b, A '2.A -91 14 ADS F F Fz Movement x y OBE SSE OBE SSE OBE SSE Them Other Rotsl " i \\ j x 0Ao t.D5g~~
~~oye p tg~~
~~- 27 \\ / 1o to Y 077 I ' h-~~
~~8 '_3 i~~
~~3,w, Z e lli t. 46; . u s ') M 24 \\ O~~
~~Total Includes Thern~~
~ ~ thep.nl + f57 + 1tI4 safety Class +l531 t 30c4 \\ / Pipe Dia. Sch. se h fe FAD / TAD \\ [ s K' Reqd. ' k [ Oper. Temp Ins IAD Y SAD u Transtent / \\ Ref. Dwas. ** aev.wo. / l\\ / \\ ~ / \\ ~ 152.9 S o c. i / \\ 5 C7 Il24 Totsi + 1553 3o9 / \\ 554 III 3 l .i mi Nortit Af oT E *.- THE #'C V !S C O Lo&OS %VE R.G QM PREO 7 /te o tr 15 FooerO TH A. T r NITH THE oLD LOADS THE N G tM toAos A g_c gg,c y, y,3g y,
~~C mP., Conc., Stl.,~~
IMT'E t!./4 Crio p Emb. P1., HVAC. E1ce. M E#R, SWC6 ALL. THE Aorv Titsd6 ARs ve. clY Lo ta ctc. itLTson PA crocs (S PLG AJT Y el~ Mad 4tH A VA tl /GLE /3 E T M E E ra S Tf G SSS.s, TH E A C T u llt. /VirD A LLou1A li t.G OVSASrdGSC lull. L HD T* let C K G n s g-fra t.o A O THE46fotE, TilC 04ffIrlsl I AHY' MGM66 RS, T1/2 O L.O l.0 A t3r, tirl E L/fid f O*JLY. C A t. f ll L A 7 t o bl $ TO 3 H old N U M tG k C H A*J4C S
L.
c y /1 Mf[() go.g-1.OCAT1(IN l'I.AN . en.e s m ..m .y-n.
.o GENERAL COMP,UTATION SHEET CALC. SET NO. Atv' COMP eT CHWO ET 6r hu. itted e.~ngineers ",,*2 o DATE DATE / 2:' ?/ 2 4 fY *"do voio NAME OF PSNH-SEABROOK STATION UNIT /S -/_) COMPANY %HEET & ' OF &] es "^ ^" '%/ 2a 9763.CC6 STRUCTURAL CALCS-PIPE SUPPORT suoccr )_.. 3 i* AWR O/9 SYSTEM 6 C-LINE NO.Co-6/9-?-/576 BUILDING CMT -- :- 2 -r ISO. NO. SCOS/.9 SUPPORT NO. O/9'U -f _ _ E.I..T I_l / . L...-. - i : 4 i k twinQ 74V // l : - -. - t 12 NSM 's n uc;. is4nq O'nT / NFS232 ~ s. f l__2/k,V2 f
~~u. iov l~~
l ~ ms a.- 1 fMN g I / % -r. 4-I i : i i a ir L- (o.I78-t0 5 = 0 678 2 '/i t 2 20x /W -. si y ._...i. Nk82/ t \\ . _.. i.i _ _._,. L_ _ _. . _...... _,_._ b r-i - -- - -- _._ 7._!_s ' '... [S,, 3 7sw.g ' ' l -{ - -. 1- ~ftsV4-{uPS25g fbd.No-8c8-2. .r o. . _.- n... (t}'a%o)2el/4i6MsCou.kd'l*$ht" \\ (NV52M 'T ^ ~ ~ ' Hmm Emb=7h a
~~O'/0 s~~
7. y-... :....- SEC7^-1.[ r. r. l._j. 'l M>ELEV) r r -- r *: .ysv4 \\ N6le. : - or Sku.l2, O /D}~mb. Y 't I t.... i .. i I... lN8X31 prcrutc/ecl, $L /MmbWU tocuect h llu Eind 78 as .. l_.... \\. ;. .:p / 0 a7/w monM. g/wwn,a/.stys sre av dci> f e ovid ge/ l
~~...... 2 A /.5 6 W i~~
\\ Y' .(r o m) fg *.L-pr$g)GE(7 /-l .EL /O'-lo I.i ' l (, y - ( E L E (!) i n u l ll : J l'% m A-9edi
y
== tw' M
~~GENERAL COMPUTATION SHEET CALC. SET NO.~~
~~wet COMPEv CHA0 DY M[ <m NPLIND mitEd engin88tS a FJNAL DATE 'DATE' *# # ^ naut or 'PSNH-SEABROOK STATION~~
"5
~~/ gly ~-- m,3 , tg 7 va U -} Comen* STilUCTURAL CALCS-PIPE SUPP0Hl_ om om SU8 JECT i 9.i. a, 4....!. 1 i s' .6 i ~ ~ ~ ~"i - - i 4~~
~~I L_i.~~
~~i... l 1 i AWR F/9 SYSTEM 6 C-~~
~~a.. !~~
~ !'.]~l. f LINE NO.08/9'3^/5'#-8 BUILDING C7/V 7' i ISO.NO. M O/B SUPPORT NO. 8/EN A kwan m #se ~ 1.Tiw nwmder AI8 hat og?Je cz k)_ I 88 lr) / 91 Ucnctl.moucul As crXy s. i : i L FACE 78 h CONC AA/CRCg 80L7'S l-- __G l0 fsp,:(850, fy:l6 f
~~~ ~~~
11 - ' (:STD.PAQ7.NO-fy)g.g}._. fj, m j g /(y, jgl l :;. ,5 t l,, t>\\ ._... icr.cimurf mene)/ ts f _t' !' lg, ,gg o 4 'I l i, nej/cc/ec/ j i __! .s ., g i-, y s + -E-e -e- *g j O Hy l '^ I kt g _b Ih,f g -g -. '. J...... t_.. ,(fM r - - -g e 'a,f. v / q;, % s-- le __. x = 8_.,i._ q = E- -e I eN i !l .._.s._..,.,_ dNb-Ill'kfia, h,ab......kGw a= 2-hs," b = 3 7s " (N { 6 i %. A r> d er :. /w !an 'I i i . ' '. a.fb : 2 25-/ 3 75.- G, &o a
~~j..~~
~~. 4 9r4 ...... e..., g ,_ g //s o 9 7 8- // // . L... l;l i.. :_ _;... ;._. t. O. -/b )f / or 6,) 7 --. r. i. . ;:i i l l f. ~~~
~~~UO Ylle bClSe /5;/%dble, 6 l'2~~
~' 0 .l '{ lQ l paw or Ni incin.ca.f . e. gliotV = /S *Y' . l o.. p.l.. i,.. ;. ;,, j,, = i. l. l.,. . l l. ' ' f' - c/ f W = N ?'S / GE= I;I'I'G, g.. . - ;..t. c'h o.e.c /s.,.- /2. 7t. " k, la feu. In At o
E=='?'"' GENERAL COMPUTATI,0N SHEET CAtc. SET No. retv coup av cwas av d. .57-h",uNa h.u.11.ted e.~ngineers a Y'N 61 E.'b-8/ ,, m PSNH-SEABROOK STATION fg vo* NAME OF fm UNIT /S .s suter i, j i_. _ __ ., 7 _ l.. ._ ;._.: _.g ;... . _i ._ _ j AWR O/9 - SYSTEM - C C- .-. i l -: I _- - '... ; j.:. !. i 1 -~ ~j~ LINE NO.00C'/9~3'/M-A BUILDING C7W ..a _i..i._[ i.. i N' cod /9 SUPPORT NO. O/9'M ,T ',. ' ' h ISO. NO. _. 4,. 6 y l
~~q '.-~~
! l' ; g. .,. p e g en .L....;. ~ ~~ Y l l. ~~/;/ =..c_.c ~ la /t1 = /0 S '.4 _._t_ ;,i ;l: I I i i ;. b.= d+2d = 9 26-/ 2F/=- o 25 ~ ~ ~ i ,~2 I : ../4 = OS, .Calculaften. i , -. _So..m 1 i . _.__ _ _ _ g ,-;-_._ _ g.:.._;_,a fO) o inoun feincr> to..... yd'n G ric. A n.. lic t c v x __/...,... 8 5 0 //22 /89 3,.j..../ ' _ :_.1..=.7-2. 17069 x.J2.# 6.._....,...._,.. .. /O-5 ] . >..- /3-75. l .r -- I. i
i

~~I i ,1 I~~
_i i 3

,,,~
m huidnble 7e'osrckva%b cf(tiVdio(anc[dnchtl.=,6840 i i. (T i ~ e SRe clu.cfran - _Auewabhvalan: '._~_. _3.T 4s l '.De.c. valu.c.= T T5 6640 = j24l iTM., g.. A_.. .n.s _.4..., I x l YM SbCO '5.hkl.h h [i 6fCC =. e...,e $_ t i i. ........,_......_....4........ ......_v_,_.. + T;, 3/+4rio /cl/ due fa ry /r' ice.=. /G _~ 3 ~ 6
~~g__,~~
' ' ~ ~ ' - ' ~ ~ ' ' ' ' - ' - ~ " L.[_d,...h._[._.:. 7.- T- ~* ~ ~lanf s/ccor =i ? . /{'e.saf g7.3 e' 4 z 2-L..! . i ' i i y I 8 i, o .:3%>able.s/eco, valu.c cf ll4"dia &nc. anclur=scso i y v. r :t+ :c._'. je7),.jeg, g(ac = 775 gogo, 55it 3 .i p. [....,, _,. ;. ; _. <g i.. i.,. 7.. .j rj,;;i ... I.. p,. ,i .y ..,......i t, .....,..q
. - ~ 'essera8'4 *
~~GENERAL COMPUTATION SHEET CALC. !ET NO.~~
tcv Cop cv Oero EY ,,,sedmci . hmitidengineers "'.".t 'T S o a--~ ~ - m y, yE,.' o.,c F *-Y PSNH-SEABROOK STATION unmsfg voio uwc or @ Comw g.,ja j l STRUCTURAL CALCS-PIPE SUPPORT oarc o rc gg SUBJECT - 'L_L.h,_.,,._;.7.;.., i i * ' L 1. ; _. ' _., 2 ,.. r ;. __,._.,._ p. : I....,, AWR S/9 SYSTEM N- ! i -h - - - - - -- ,.I[ LINE NCN/99/6?-8 BUILDING CNT ' .!. I.... :. ; ' ISO.NO. DO/3 SUPFORT NO. M-84d ' N ~i_.. _+..T.. ~ l ; k ..}_.. L I i '- Wy ~ _.s 9/>TE4Ac7/5Ni- ..__.._n l't
~~I -!-~~
~~it M-.:._ g . _. _! _.I _' 8 l 3 i [ t., //22 4 t i. / ' I__. o I I q-_,.-- . g 424/, 56// II 4~~
~~i a~~
~~i i i l I ! l 3 t ^ l 0 l f ;l -i-i. ; j i -!-- -, - - - t l I ~ t I i ef.qjafge. i f 1 8 f e k I .f. [ -l l l I~~
~~f $~~
~~8 1~~
~~/Mcs e <7q :-~~
~~.i*IiiI ; i i~~
i
~~.l 4 g I e i Visanud absalitw ~ ci Cfille httmbcr 'i.Gfmd(a-a~~
~~I e~~
~~~ j~'g$~i' s //22 7 2 X3 75= 84/5 " fansdem$ he wie : d/dcecoen lR.E %.~.~.1-~ if, _i i ! _i_iUatu. /cHs,innmk i,_DSq..hb l'd =../ S M 6 25m i 1 M. mn3 I'l: l -F :~~
~~6.....~~
~~i m y-Lc 5 Z~~
I

'. -
g,= 84/5 2366 fd 27000 "h Gt ii' .2s _ -, _......., _, T,,. i. F, ,l l t i { l. e 6 1 i t l l l .._.4._ r.,f._ u _.r._.,_ _ r__.__.. y,.., i __._n, U N8)St ._.y t 2X /2, // 88 /20 OK ~~ ~ = j C.. _ __.,_
~~_,p_.,. f- 0 2,... _.._.._ g,~~
~~j j p__j. j._ r...___. _ t _ i_.... .. m... .:.4 i _ D c{. N T Z)E E **- - -l, - p, g, g o~~
~~p g. y I. af.st) j~~
~~~ v._,... b p _. gyy 3M.n/0(7//0 = 5'b59 mfd aj'", .g. .. y...,. g ' _j _ /ff 6XfC m',g. ;;_.../3 _...._.../2 4 '.. 1 _..._,.b E 00 i i i s r 6~~
~~,, l l i~~
~~l .'. fa$38)(/0 3 .. g..,...... i, i i j I Q l-.L. t - { l. 0 0335 ) /42SXfD '" l--{- b l l l -l /2 (4//09), 360~~
~~r.. '~~
~~... ' ' r 'i-',M -i." -*- 'l ' i '- l. 'l n. g. ..i I ..,.,.. l ;. j y. g.. ..l....l ....y....... {... }. J. !..l }. i .;l. . l...,l.. i I I l l l l l i l I i I . [. - . g. ... r J --t ~ '~~
~ - " )
~~I .....e.., I~ i i 6 4 e e a 3 1 ! 1 f j i .-) -[* g' *t s -e i f~~
(
a 7t <w< - - - - -. =. .-e--r ~v-4--i -'-r-r v
210.72 The pressuriser spray valves identified in FSAR 5.2-1 are not in-conformance with the Codes and Standards Rule, Section 50.55a.of 10CFR Part 50. These valves are constructed to Section III, Class 1 of the ASME Boiler and Pressure Vessel Code,1971. Edition, through the Summer 1972 Addenda, whereas the regulation requires these valves to be constructed to the same code and edition .through the Winter 1972 Addenda to the code. In order to determine the acceptability of these pressurizer spray valves, provide an evaluation between the Summer 1972 and Winter 1972 Addenda to the code an'd identify any differences between these ^ Addenda and assess the impact of the differe.ces on the pressurizer spray valves.
~~RESPONSE~~
The spray valves have been reviewed against the' Winter 1972 Addenda and found acceptable. The Westinghouse equipment spec. provided a level-~of quality that met both Summer 1972 and Winter '1972 Addenda. The attached table provides a comparison of these addenda with respect to the spray valves and shows no impact on these valves.- c
l r t (g h A \\ g ATTACis1tni Steesta 72 Neo WINitt 72 CODE C01pAal50N YT C00C pAaAcaApN suesta 7: vi,;ta I IMPACT ON VALVES NA-2140. St$PONSIBILITT FON COMPONENT C00C NA-7140. CAftsoallAll0N Cf 1040lNC CONDITIONS
NONC NA floo - pt5p0N5laltlii FOMrb 1 MENT C00C CIA 111 FICA 110N CIA 55tflCATION Ccaponents of a nuclear peuer system any be the rgetpment Specificatten for match the the Nr of a nuclear gemer plant directly The thmer of a nuclear power plant directly sehject to condittens wktch can be provided valves were dest 4 te (C478444 Sev. 2) ltle er throwgh his agent, small be responsible for er through his egent shall be respeasible for for la destga la order to satisfy appilcable deflees the tea condittens ead the lle deterstalagtheappropriateCodeClass(es)for deterstalog the appropriate Code Class (es) for systen safety criterte. for the purposes of stres; levels for less I Class t end Class 3 cach component of the nuclear power plant and each compepeat of the nuclear peeer plant and destga. these condittens are recognised la this valves. ThisemetstheWInter1972Adiende.
shall specify these Code Classes la the testga shall specify these Code Classes fa the Destga $ecties of the Code as fellouss I Specifications as required by NA-3253. Specifications as required by NA 3253. i (a) Class I campements and supports thereef. ; la additlen to sattsfplag stress lletts and desty rules established for the Sesign tendl. tiens defined la NS-3112. shall he evaleeted for additiesel conditless categerfsed as fellouss l Normal Canditions' upset Conditfeas:{ Incidents of floderate I frequency) i EmergencyCanditions(lafregsentfacidents) l l faultedCandittens(Llettingfeelts) 3 16stlag Conditless I I For deflattless of these leedlag condittens. l refer Ae 88-3113 PM NO-3114. sesfgn by analysts rules for ;~* of these cemettless are gfvea la f.d.3200. sith the enceptles that feelted Candittens ers'censidered le Appendte f. Addittenal er alternettve criterle are provided by the specific componeet Destga Saberticles ' he-3100 threagh NS-3600 for all but ;the f aulted Conditleas uttch are hise considered la Appendia F. It is the responsibility of-f ' O r e. to deflee the acceptability criteria to be applied for faulted Candittens la the Design Spectfl. cations. The rules la Appendia f shall be a applied la all lastances unless alternative or supplemmatory criteria, regelred by pu618s l 1ealth and safety considerattens for specific = appilcable by the Ommer's Destga Spectricattees. l g components or systems.' are defleed la and made t la ear case the type of systm analysts (elasticorlaelastic)usedbythesystesde. signer shall be ladicated la the Desiga Spectf scattens (see f.1322.1). l . (b) Core Svpport Structures 3 l 8 I g (laPreparatten), I - j-0 l e f } e
v Y e n O l M7 ]- 1 s r l Cow p m ca pu l Sima n, vintra ir 3 IMPACT ON VALVES (c) Class MC compements, la addittae to 3 satisfying stress Italts and dest p rules established for the Design Conditsens defined la 53112. shall be evaluated for the ces. dtttons defined la O 3131(c)(farthquate toadleg) l end M.3131.2 (Missilefend Jet Effects). 1 (d) Class 2 and Class 3 cespenents and the supports thereof are evaluated in accordance I wita design criterte eelch de set espilettly recognise the categerlaatten of leading con-j dlttenslathemannerdescrlhedin5A.tl40(a) for Class I compements. The specific component destga rules of this Sectien establish criterte I for the deflattien of the applicable Desige l Conditions, sad these rules coefers generally with these of N8 3111 which are applicable to I Class I cosponents, if postulated condittens ether than these considered la detemf alog the Detten Conditions are of structural significance I ^ for Class t er Class 3 compeaants or are requireda by system safety critetta er by regulatory apthertiles havlag jurtsdiction at the ecclear powr plant site, the Duner shall descrlhe the condittas and provide destge criterte as e l separate contractual requirement beyond the scope of this Sectlenlef the Code. ~ ~ ~ i MA-2Ilolcl
NA.2110f tl*
RA.2110(c)tevise to read 8MM J (c) This Section of the Code recognises that (c) This Section of the Code recogelses that (c) The Duner of e nuclear power plant. Valves era classifted ty Code Class 1. Class ; components of a nuclear pswer systes ear be composeats of a euclear powr syntes say be directly or through bis agent, shall be and Class 3. The classificatten Is accasellst subject to conditions which can be provided for subject to conditions which can be provided for responsible for applyleg such system safety by means of the valve Spec Sheet and the vale. In the design la order to satisfy safety la the design la order to satisfy safatr criteria to the esta411stment and faclettee fquipment Specificatten. criteria, for the purpose of design, these criteria. for the purpose of design, these la the Destga Specifications (see 543252)of conditions are identitled in this 5ectles of condittens are Identified la this Secties of appropriate Code Class (es) (ses RA.2170 and the Code as follows: the Code as follows: 1 A.2130) and of appropriate Destga and, when required. Deerating Candittee leisrustlen Normal Conditlens Normal Conditions (sesNA.tl40). Upset Conditleas (Incidents of Moderate IIpset Conditions (Incidents of Moderate frequency) frequency) (sergency Conditions (latreguent facidents) EmergencyConditions(lafrequentIncidents) faultedConditions(timittagfaults) faulted Conditions (timitleg faults) = Testing Conditions testing Conditlens i for deflattlons see Mt.3113 and ag.3tl4. For deflattleas see us.3113 and me.3114. t A t. L 6 I. I- \\
~~t...~~
~~4 r. 4 b i. O', e 3, i~~
~~9 l~~
i* j]: I }: jf 4 m. m, I
e ~ O C.. O \\. [ ~ ~ IMPACT ON vat.VES coot ranaceArn Stem.ir visifn af2 ma.3252 - Cont [NIS OF OtSICM $PECiflCA!!0NS RA.M52 l l~a I NA.3252(b) Add before the semicelen (see NA. Mene tech Destga Specification shall include: After (e), change period to sealcelee and 2110(c)and342140) add: NA2110[c) and '2140 are covered by the (a) The functiess of the cesponent er Talve igulpment specificatles, apeurtenancel (f) Materials requirements includies tapact (b) the design requirementst tests when applicable. (c) the enviresumental condittens, includlag raelatloat (d) the Code classificattee of the componeet er appurtenance see an.2000]t (e) the deflait en of the compement and piplap + boundertes (mA.3254). the Destga Specifications shall contata suff t. ( cleat detall to preilde a complete basis for constructten la accordance with this Sectles of the Code. as.tlle(s)(a)evise first sentence of feetaste I s mene ns.2110(al. 5 Cort 0F PRINCIPAL 1[tM5 (MPt0fte to pd tilo to read (a) The tera meterials as used in this Sectica Talve Igulpment 5fecificatten pe.ults the of the Code Drollas to these items produced to 3 ese of ASIM Mertels, Materials produced under en ASTM destgantlee the requirements of an 54, Se er 5fA Specif 8 I say be accepted as complylag with the corres-8 catlea of Sectica Il of this Code or of any pendt A5ME specificatlea provided the ASMC. ether material specl{lcaties permitted by this ?,l 6 specif cetten is destgaated as betag Identlcal ? Sectten of the Code. The tern Materials .ith'the A$fM spec ficattee for.the ode, class, i :'., , or type produced a provided that t meterial' ,d Manufacturer is defined as the Manufacturer edte produces the materials'te the requirements 8f P specificatlea by e[Certtfled Materials fest i f, is coattrued as complytag with the A5fM. '.,i ef the astertal specification lacludlag meldlag l Seport er Certillcgtlea from the Material 1 Mass. and brastag matertal. ~ ~ ~ - g I 4 e heterialproducedunderanASTMdesignetten ese AW5 specificati by a Certlfled Materials a may be accepted as complying ulth the test ert er cert ficatten from the latter spectricacloa is indicated to be s Manufacterer. correspondlag ASME specificattee provided the Meterl Identical ulth the ASTM spectficatlea and pre. vided the esterial is confirmed as complylag alth the A5in specification by a Certified Materials Test Report er certifiestion free the Materials Manufacturer. Iseldlag and beaslag materlat produced under se AW5 destgaattee may be eccepted as complylae with the correspondlag A5ME specificaties provided the latter specif t.
~~I cattaa is ladicated to be identical with the I~~
AW5 specificatlea and provided the meldlag end braslag material is confirmed as complylag with I i i ? I -.-- ---mm-.
r k. O (.. .. j s e. f"* *db '* IMPACT ON val.VE.S* i. "' '"",, pnf Jt 9, it f,., p;*g g i NS-1420. Attlulate it515 g.{4g. atipliete it$15 P Ig:H lt bevise fles sentence to reedt ' d anse v the required tests shall be condhscled for each the regelred tests shall be conducted for each The required tests Il be coeducted for each Igu**usac Specificallee lavetes me.te#3 Let of covered, flun. cered er fabricated tot ow severed, flus-cored er fabricated. let of severed fled cered. er febricated electrodes, for each neat of here electrodes, electrodes. For each flett of bare electrodes, elettredes, for each beat of here electrodes. l red er wire, for each Neat of cansameb'se laserts red er wire, for each fleet of ceneumable laserts red. er wire for metal ett unldlag er gas and for each comblaation of Meat of bare elec. and for each cambinetlen of uset of be e elec. tungsten arc isle. for each heet et con. tredes and Dry tiend of flus-els to be used for tredet and try Blend of flue-els to be used for sumablelaserts(bactingfillermetal).erfor melding. 1ests perfereed on meldlag meterial soldlag. Tests perferend on meldlag meterial each ceableattee of best and bare electrodes la the gratificatten of unld precedures will la the quellfleetten 'bf weld procedures will and dry Head of flein als to be seed la weldlag, settsfy the testlag requirements for the Lot, satisfy the lettlag requirsmeats for the tot, p heat er centlaatlen et Olset and Betch of sold. Ilset er combloatles of sleet and Ostch of meld. A'Ise eed new sutperegraft (f) to reed: by ut.400m are sede and the results conf (orm teing meterial sted,provided the tests re mired 1 lag material used, provided the tests required (f) A tot of Subse -Arc flue is,defleed by NS-4000 are ende and the results confers to 0 the requirements of NO 2431 and 118-2438. The the regattements of NS-2431 and 118-2412. The as its quantity of un produced from the 4 felle= tag definitions apply. fellenlag deffelstene apply. ease centleettee of ou esterfels ender one
~~productlen schedule,~~
(a) A Dry Batch of Covert'ag Misture is defleed (a) A Dry tatch of Covering ni t.se is; defined 8 as the quantity of dry coverlag lagredients es the quantlty of dry covering agredtekts elsed at one time la ese etsing vesselt a dry aimed at one tsee Ic ese alalog vesselt e hatch mer be used slagly or mer be subsequently hatch may be used slagly or any be subs ly subelvided late quantitles to editch the liquid subdividet inte. atitles to telch the iguld f set eines [see (c) bele= produce a number of bladers ser he added to produce a ausber of bladers may be a d to
~~.et elses (see (c) hele=].~~
J. j (b) A Dry Bleed is defined as one er more dry (b) A Bry Blend it defleed as one er omre dry hatches aimed in a mislag vessel and combined batches elsed la a afslKg vessel and ceableed J proportionately to produce a uniformity of aimed propertlenetely to produce a uniformity of assed lagredients equal to that obtained by mislag lagredlents equel to that attained by elelag the same total amount of dry lagredients at one the same total amount of dry lagredleats at one time la one slalag vessel, time la one elslag vessel. j (c) A Wet Mis is defined as the combloation of (c) A Wet Mis is defined at the costlaatlee of a dry hatch (a) er dry blend (b) and liquid e dry batch (a) er dry blend (b andlipid binder Ingredlents at one time in one minist blader lagredleets at one Slee e one m. slag i vessel. vessel. (d) A Let of Covered, flua-Cored er f abricated (d) A tot of Covered, flus-Cored er f abricated Electrodes is defleed as the quantity of elec. Electrodes is defined as the quantity of elec. 4 I tredes produced from the same comblaation of tredes produced free the same combinatten of steet of metal and Dry Satch or Dry Stead of steet of metal and Dry Satch or 3ry d1end of fles er core materials. fles or core materials. 4 ~ le) A Neat of Bare Electrode. Red. Wire or I (e) A Itest of Sare Electrode. Sed. Wire er { Consumah'. tasert is defined as the material Censumable lasert is defined as the meterial i } produce' w the same seit of metal. produced from the same melt of metal. b { o e l 1 1 l 8 4 1 i t l e f j e t i ? t 2 t i e d n 1 .t: S 4 ,__.___i--__..m . -. - - ~.. - - -.. -, ,w.+-,, ,-~..m-..--.---. wow--.--n.,-,-- ...-vw,-,-.---my.w%,------#. w, ... - -,--r w-+--%-m-~ ~,n ...-... ~. -.. - - - -
r P .m (.s 3 I l ur Coot rAancaArn Sumte 'tr Winrn ' tr IMPACT ON val.VES Ng 2432 CHEMICAL ANALT515 0F fitttt M(IAL OR NO-!4 P. CHEMICAL ANALill5 0F fittta METAL OR M8-2432 Sevise to reads e*
Wtt0 DEP05til WEtO DEp0 SITS none A cheetcal analysts shall be performed on 4 theetcal analysis shall be performed em 50-74)! CHEMICAL ANAlis,15 itsi ferrousallor Nun 6ers A7 and AS. Table 0-11.3 ferrousalley Numbers A7 and AS., Table Q-11.3 f
.-44 00EEMt~a par of the Specificatles. Cheetcal anal sis of filler metal and/or wel / cf Sectica II of this Code and alchel base alley of Secties II of this Code and aletel. base alley deposits shelk be made la accordance with applicable welding material er welalag precedure applicable weldlag materlal or meldine precedure RS-2420 and as required by the following '2.% Q weld materials for the elements re ptred by the weld materials for the elements required by the. 4 specification. The specteen fer cheetcal specificaties. The specimen for cheeIcal subparagraphs. analysis of the welding asterial shall be analysla of the welding material shall be removed free undiluted weld deposits er filler removed free endfluted weld deposits er filler 88-193I 1 atquistntuis FOR CHEMICAL AnAtt315 .etals as specified in (a) and (b) below: metals as specified in (a) and (b) belew 1 The filler metal or meld deposit shall be (a) for bare electrode, red or wire filler (a) s'ar bare electrode, red or wire filler anal ved for the elements listed la isble metal used with a gas setal. arc welding er the estal used with a gas metal arc weldleg er the 88-I II I*). The resul ts skall be for sas tungstenarc welding processes, the cheelcal gas tungstenarc welding processes,the cheetcal Informatten. e alysis say be perforse# w the electrode, rod, analysismaybeperfereedontheelec{rede. red. were or consumable lasert er an undiluted weld ulte er consumable lasert, or an endlluted weld P8-I41I ! SAMrtlMG giquiptMENil FOR fitttR deposit made with the utro er consumable laserts deposit made ulth the wire er consumable laserts METAL OR D951110 MIAL ANAlisil (b) for all ether proce! es and filler metal. Sampling for filler seLals and/or deposited I the cheelc,al analysts she il be perfereed on an metal analysis shall b4 as required oslow. (a) When censumable l(sert (backing tiller undiluted weld depostt. a edtal). bare electrode'* rede er wire filler / setal used with gas metal arc. gas tungstem arc. er plassa arc telding process:s. a cheetcal analysis shall be performed on the electrode, red, wire or consumable insert { (bactingfillermetalla er en a weld deposit s made with the bare electrode, red wire or censumable Insert. [t (b) Cheetcal analysts'.shall be performed on a weld deposit for welding materials used with processes other than these listed in (a). The sold for analysts phall be made estag the recess and the combinaties of materials I lag certlfled. I lable NS-2432.1-1 Weldine Materlat Cheetcal Analysts s l Carbea & Low Alley Materials g C.Cr.Mo.NI.Mn.51.F.5 V.Ce Chroelun and Cr.nl stataless Materlats C.Ca.Me.nl.Ms $l.p.5.v.Ch e Ta.il.Ce I sichel and NI-Alley Materials ? C.Cr.Mo.nl.Ma.58.5 Ch s Ta.Ca.fe.Ce l I i i I I e l l i i e I l I II i
lh e s 5 t f m fN A. h. p .g
~~+===u.w-~~
. t .c m m1fn*: I',' Sumt n IMPACT ON VALVES AB titt - pfAMlITID MAT [AIAL SftClf!CAil0NS j pg.)}}). pggggyTgg 34TgglAL Sf!Clf!CAi!0NS NS-2121(f) Add 33.I]!{(f) to read: Not applicable. la) pressure-retalning material and material welded therste. escept as permitted la NS-4435 (a pressure-retalning material and material I e-and escept for cladding which is 10$ er less of me ded therete, except as permitted in 54 413$} Storials for lastrument line fittings. This addresses lastrument linegaregtves hav the thickness of the base matertal and est t for claddlag which is 101 or less e
~~e. mestant plpe sla'e and less weld ends. Valves de met use i~~
3122) shall conf rm to the requireme(nts of one see Ng. materlats made to specifications. may be of the thi sets of the basa material see 88 a 3123) shall ceafers to the regulrame(nts efeedethese listed to Ap dia 1 of this Code pre-cf the s other thee. 88'pression fliting jalats. cifica lens for materials tven la Tatte I..l. Tdle I 1.2 or Table 1. 3 et of the s vided that the fit Ingh are la confermance cificatleas for materlats tven le. endia I of this Sectlen of the Code and to Table t .)e Inble 1 1.2 or Table I. 3 of with the retstrements f 38 3671.4 and the 1 of the special requirements of this Article. e la I of this Section of the tede end to materials are deteraf 4 to be adequate for the which apply to the product form la ed Ich the e lch apply to the product form te which thof the spettal regulroments of this Article service condlttees by 1%e Instrument piping materlag is used. system designer, materies is used. (b) Other material shall confom to the riquirements of the specificattens for materials (b) Other material shall ceafers te the 4 listed la Table I-1.1. Table I 1.2 requirements of the specificattens rep saterfils er Table 1 1.3 of Appendla i unless otherwIse permitted by listet in Table 1.1 of Appendia 1.1. Table I 1.2 or Table la cther articles of this Sectles of the Code. other ertjcles of this Section of the Code.enless otherwise permitted by (c) The Materials Manufacturer shall satisfy all of the requireeents of the material speelf t. (c) The Materials mnufacturer shall satisfy catten and of this Artic{e escept as provided alloftherequirementsofthematerialspectII. la MS !It!. cation and of this Article, ascept as provided In NS-2122 (d) The requirements of this Article do not epptr te items not asseclated with the pressure-(d) The requirements of this Article de est retalning functica of a convenent such as shafts apply to items set associated with the pressur. stems. tria, bearings hushings wear plates. retalning functlea of a coepenent such as shafts. ( e. i stems. tria. bearings nor to seals packing, gastats and valve seats, per to seals packing,. bushings, wear plates, l geslets and valve sea _ts. g Ns-fl60_ - DE1Ea10MIION OF MATIAIALS IN $(AVICf \\ pe-2160_ - Ofiftt0AATIQt of MAftatAL$ In $ttyltt l Consideratten of deterleratten of materials ps-1160 - At end of paragraph add the followlegs
, at this Code. caned by service la generally outside the scope Consideratles of deterioratten of metof tals nones It is the responsibility of the ravsed by service is generally setside the scope 3 ocial consideratles s 11 he given to the rbner to select materials.sultable for the of this Code, it is the respensthllity of the i fluence of elements su' h as copper and The f Ipment ese ofcepper,$ ectflestten pronthits the c
condittens stated in the De:Ign Specificattens Duner to select meterials suitable for.the phosphorus en the effects of irradiatles e.. the end. aluminia. Talve des go (NA-3250) with specific attenties belag gives conditleas stated in the Desita $pecificatless properties of materials (includlag weldlag con 9 lied with the revisten. n u the ef fects of se.vice condittens upon the (M St$0 with speelfic attentlen being given meterials) In the core h f t 11ae regles of the 9 properties of the materfals. to the e facts of service conditions open the reacter vessel. Any spettel requirements shall Properties of the materfals. be specified in the flestge specificatless. (See Rb3tt! sad 38-3114.) We se specified. the check analysts shall be made la accordence with the base metal specificatleas and le accordance with 33 2420 for the welding materials. l t 1 t t i f g I Ie i e 'I s 1 y a .t = . _.. y - s t
'~ l n p A \\ V-C00t PAnuva r l Stata 'n vl.ata 'n IMPACT ON VALVES 88-2580 - EIAMinATION OF Pet 35URE-RETAININE - leg-fl10 - tRAMIn4TICII or pais$t*E-RETAININE BR-[H1. Revise to pada mene. MATEGIAL MTERIAL t
~~ressure retalatng meterial shall be esamined by.~~
Pressure retalning meterlot shall be esamined by (e) Pressure retel og meterial shall be hH veins regardien of slae en sWjected eendestructive methods applicable to the motorial needestructive eethods applicable to the meterial esasined by sendest Live methods applicable to mondestructive esaminettens by the Equipi and product form as regelred by the rules of this sad product form es required by ll$e rules,df this to the seterial and t form as required by $pecificetten. -wherticle, except for pumps and valves ulth in. Suberticle let slping escept for pumps and elves ulth in. the rules of this article, escept for pumps 'et piping ceanectless 4 la. seminal pipe slas. connettlens 4 In. amalgol pipe sine and velves eith telet piplag connectless 2.In. valves meet the revisten. ed less and oncept for seamless slpe and less and ascept for seamless fpe tubes and fittlegs 2 In. neelnal pipe slse a tubesnd less,and fittlegs I le. nominal pipe s(vae and less, aeslael pipe sise asd less. Seemless pipe.' see hg Mill. The 2 lack site esem tubes. and fittingsJt Is. seminal pipe sise and .et apply to heat-eachanger tubing, ptlen does (seeRt.3673). The 2 lach size ademption does less need met be enemined by the rules of this not apply to heat eachanger tubing, tuberticle provided 'the requirements of NS-M73 are met. Ine2.la.!stseesemptlendoesactapply to heat enchenger tubing. \\ b) for forged and cast pimps and v61res ulth eget (plag cenasctless over 2,le.. ep to and asjed og 4 In. mentaal pipe else sognetic particeerliguldpenetrantesamInstlenspsy se performed, in lies of velimetric esaminatten. lacepttheaulding be radlegraph, ends for cast pimps and valves hel ed for e slaisum distence of L , den t is the *destge sectien thickness of he seld) from the f,laal meldlag end.
~~e-3213.21 LIMIT ANALT$l$-COLLApSt 10A0 110-3113.21 - LIMIT ANALT518-CottAF'5E LOAs N-Sill.tlRev'Iset'ereads none.~~
the methods of limit analysts are used to can. The methods of Ignit analysis arg used to ces. B0-3213.11 - Lint 1.ptALT$18-COLLAP$t10Ae All llettias stresses specified in the spec pute the osalem lead a structure ende of ideally pote the maalaun lead a structure made of.ldeally g. catles are belou er equal to the yteld stre i plasticbenstrain-hardenlag)lyplasticstructure plastle(s.onstrata-bordenlag)asterialcan' carry. The methods of 11 alt analysts are used to compute meterial can carry. the deformaticas of en Idesg Tho'deformattees df as ideally plastle structure the meelaun lead a Acombinetten of leads a lacrease ulthout bound at this Iced 'adblch is p' Increase ulthout bound at this lead..whlch is [;,structure medd ofl[deelly plastle'{eenstrale-termed the *cellapse lead *, - Of"i termed the 'es11 apse lead *. j }P '. 3 bordentag) esterlitcon carry.tThe! deformations pl ". " ofenldeellyples'tle structure leeresse ulthout bound at this lesi %Ichlattermedthe'sellepse a 1 Iced". Ament the methods used le limit analysts la e techalque unich assumes elastic, perfect 1r plastic, material Tehavler and a constant level i. ofsomenterforegpatheseredundantstructural i j elements in d ich membrane-yle14. plastic-blage 8 or critical buckling lead has been reached. Amy ~ a primary structure un P,i a failure anchantes g lactease la lead sust be ersupented by a stable i defleed by the leute bound theores of Italt analysis is reached a the primary structure. i
e.
~~i l 1 l h m. 7 * } l i e t --~ ~ ~~~
'** ~ ~

I l
1
m /N /", (% \\ .t' *.,. ) I toot pa====n Sueva 'n siniis 'n IMPACT ON VALVES ~ mene. ut-3ttl - fautite conoliscus M7 FAnite CONDITitMS. i as-3tts Revise te ree : s. s .i. ) t - IftheDesignSpecifications(nA-3250)specify if the Deslas Specificatless (NA-3250) spellfy h 'If the Destga Specifl tiens (M-3tS0) specify' 't Th' 8F'*8ticatten does,et alle the compe any f aulted Conditlens. me-3tl3.4.1the rules aar faulted Conditless NO 3113.4. the rules : C say faulted Canditless (ut-3112.4), the rules
~~ip*b tresses to esceed the yield potet.~~
tfees. contained in Appendislf per he used in evaluettag e elch mer be used la evaluettaa these cond{given l. aditch may be used in evaluellap these conditions ladopendently of all other coadilleas/ orei these faulted tendittens, lader (1y of all l. ladependently of all other coaditleas, are glyen ether Besign and Operating Condittaas.
~~I la the felleulee subseregraphs and are le the folleulse subperegreeks and are summarised la Flg. ut 3ttl-).~~
sunserfred in flg. 383225-). Bolete renegader of this paragraph lacludlag NS-3?tl.1 - PRIMART STRES$ts ut-3ttl.1 - palm RT stats 5ts figure 88-32251 i primary stresses are to be evaluated la sceer. primary stresses are to be ovelmated la accer. desce alth a llelt ' analysts precedere. RS. deepe alth a llelt analysts procehre 186 3228.2. and the specified leads are act to 3220.t and the specified leads are set td exceed 100 per cent of the lower bound collapse sected 100 per cent of the louer-bound cella,pse lead (see ut 3213.ft), leed(seeut3813tt). I Y ng-3331.3 - LintT ANALYSIS 115-3225.2 - Linti ANALYSIS I Inapplylagthelleltanalysisprecedure,the la hlylag the limit analysis prdcedure, the i yield strength value used is te be equel to yieldstrengthvalueusedistebeequelIs I 8 the greater of 150 per cent of the tabulated, the! greater of 150 per cent of the tetulate( 8 I 5 value er 120 per cent of the tetulated 5 vejue er 120 per coat of the tahalated yTeld strength, alth both vejuss taken at the yTeld Strength, alth heHi values tales at the 8 ' gpropriate temperature. appropriate temperature. ( ht-34tl.3. PtASTIC ANALYSIS DB-Nil.3. ftASTIC ANALYSIS ( - f 1. 1 AsanalternatetotheprecedureofN03225.] As an afternate to the procedure of 30-3225.1 i and NS-3ttl.I. aheve, a plastic festability and'H8-3ttl.t. aheve.'s plastic thstability analysis ear he performed, ceasleerlag the paalysis any be performed considerlag the actual strala-hardentpg characteristics of the actual strain-bordeslag characteristics of the material. but alth the yleid streagth adjusted noterial but ulth the yleid strength adjusted i~ to correspond to the tabulated value at*the to correspond to the tabulated value at the L. appropriate toeperature la Table 1 2.1 er I-2.2. appropriate temperature la Table I til = f **h I The specified leads are met te esteed 30 per imespecffledleadsaremettoexceef(WpW/ cent of the plastic festability leads. cent of the plast'ic festattlity leads. 4 i no-M M sevise to reads maae. l ns-3235. FAK ite ConelTIous 5-EM..FAutiroComolilous 4. the lletts of NS-3225 apply. The lletts of ut-3ttl apply. If the Bestga Specificatless (uA-3250] specify faulted Candittens are defleed la the anyfaultedCanditless(st-3113.4),therules specificellen alth the acceptable lletts. contalmed la Appendte f may be used la evaluating i these faulted Condittens, laderendently of all other Destga and Operattag Condittens. y i 1 j l
~~1. -~~
k 9 l I l I d f
^ m M q l ..r ,~~ C00t PAuctue SmMca n WiNitR n IMPACT ON val m ~.. IB-yG) ESIGt E QASS 1 RtPS 16-30) 0ESIGl @ QASS 1 (UfS MS-3410 - GENERAL REQUIREMENTS MS-3410 - GtNtRAL REQUIRIMENJS FUMp3 DNtf None. (a) Rules for the design of Class 1 pumps are a) Rules for the design of Class 1 pmps are NS-3400 Replace Artlcle NS 3400 with new la course of preparation. Untti these rules a course of preparation. Until these rules Article. f have been prepared any design method eAlch have been prepared any design method telch has been demonstrated to be satisfactory for has been demonstrated to be satisfactory for NS-3400 as shown lalthis Addenda the specified design conditions may be used. the specified design conditions may be used. j (b) It is recommended that enelytical and/or (b) It is reconnended that analytical and/or j esperleental stress analysis methods be used esperleenta) stress analysis methods be esed l to show that the pressure retalnlag pertient to show that the pressure retalning pertlens of the pump meet the requirements of Mt.3100 of the pop meet the requirements of Mt 3100 l and NO-3200. and ht 3200 I I MS-3541 CIN(RAL R[QUIRIM(NIS FOR 800Y WALL Ne-3541. CEN(RAL REQUIRDitNil FOR 3001 NAtt MS-3541 la third t he, delete... Ismediately No effect. INICtNESS TNICENESS adjacent to a welding end.... The mingsus wall thickneas of a valve body is The slaimue well trichness of a valve body is to be determined by the rules of MS-3542 or to be deterutned by the rules of MS-3542 or
MS-3543. encept Ismediately adjacent to a MS 3543, encept isnedtately adjacent to a welding end, where Ahe rule of NS 3544.8 Is welding end. *4ere the rule of M4-3544.8 Is to be fellowed. Addittenal metal may be to be followed. Addllional suttal may be necessary to satisfy other requireaents of necessary se satisfy other reqvfrements 6f this Subarticle er for corresten allowuce.
this Subarticle er for correston allowance. i Ns 3544.0. SCOT CONF 0URS At WELDING [N05 NS-3544.[ Revise te read NS-3544.8 Add the following at the and of Mene. paragraph' valve body centours at welding ends are to be MS-3544 j. 800T CON!OURS AT litt0lMG [N05 Equipment Specification calls for AN58 316.1 1 in accordance with ANSI Bil.5 unless otherwIse fer sectet welds la accordance with N83661.! stated in the Design Specificatlans (NA-3250). Valve body contours at welding ends are to be la for socket weld ends. -stres of nominal site Also me seclet meld is permitted of valves For valves larger than 4 In. nominal pipe slae accordance with AN51-816.25 unless otherwise 2 in. and smaller for eAlch the body cavity above 2* site. I the welding-end preparation shall not reduce stated in the Design Specifications lNA-3250). consists of cylindrjcally bored sectlens shall the body wall thickness to less than the value Local vlelation of the slaimum well thickness meet all of the falsewings required by NS-3541 withln a reglon CItser to regelrements of N8 3542 and NS-3543 is per. j the outside surface of the neck than 1 a t alssible provided that this does not occur withig (a) d shall be port drill diameter sessured along the run direction. Alignmelt a reglen closer to the outslJe surface of the (b1 IIe requirements of MS-3542.2 shall be tolerances given in figure NS-4233 1 shall nect than I a t,seasured along the run direction satisfied i apply te by-pass lines and other stallar (c) Sectet weld end valves of nominal stre attached piping assemblies. The transitten to the weld end preparation shall greater than 2[In. shall not be used for meet the requirements of N8 3544.1 and:shall be Class 1 valves) as short as possible iAlle avelding sharp [ discontinulties. Ihe additten of test collars 6 1 er bands, either as lategral er welded parts. l Is allowed, j I 1 9 i t I 4 [ l I
v j n O* 0 A \\ u Coot fAnacaAPN IMPACT ON VAL'VES ' ~ SmMrs :n vi,3g,.it l NO-M12.1 - COMP 0NfMIS WITN 5pfClflC SAllNG5 MS-M17.1. COMHR[ Mil WITN SffClflC RATINC5 NB.Mll.1 Sevise as fellows fle effect on valves. Thispertainsto9,19859 to.ere standard components are used, the pressura Where standard components are used, the pressure 1. Insert (a) before first setence ratings given as functions of temperature la ratings given as furctions of temperature la the appropriate standards listed in Table Ms. the appropriate standards listed in Table Ms. 2 Add new paragraph as follows: l 36911 shall not be exceeded. Adherence to M911 shall not be asceeded. Adherence to these standards in no way replaces or ellainstes these standards la no may replaces or elleinstes (b) Where the adequacy of the pressure l the requirements of NS-M25. Where established the requirements of NO-M 25. Where established design of a cesponent is established by burst i pressure ratings of piping components do not presture ratings of piping components da est tests as permitted in NO M49 (e.g.. AN51816.9 i eatend to the upper temperature lletts per-entend to the upper temperature llef ts per-malatsinarecordafbursttestshehasconducted,l Far. 8) the Manufacturer of the component shslI mitted by this Section of the Code for the altted by this Sectlen et the Code for.he material to be used, the ratings between these material te be used. the ratings between {hese to assure adequacy of his components and shall established and the upper temperature llelt established and the upper temperatore llait se certify. Such records shall be available to l, la this Section may be determined in accordance In this Section may be determined in accordance the purchaser. =lth the rules established in Mt.M49. ulth the rules established in MB.)t49. I 3 i 9 s.& s 6 1 s
Q
~% m m. ~~~~ ~ <v
I 5 i.' . in J; IE p Mm l to ta => .e. e a
C
~~n. e 4~~
~~2* II g g4 4. O I w.. p E** u~~
C
ag
~I gaj [ 2* n.'.- E ME t l4 2: :22228321:32* "..32 3.233:332 =.23:2382 52: 233 382352,3:: 3 ...,==.========, ,3,,= l4 33333g 23333:33:3.R.3:23 3 332:32.:22.:3..31.3.R.53233 5 2.:3:2:23 3 5 8: d Id e s = = = = = = R e s :::::: m : 3 :2 3 ::: a a r g u e.a s e r a n.3.R.3 ::::=. =.= =.=.=.:.:. I. g W 5 I Id r e s =:r = = = e s a n 3::r-32::: ===.a s :3 3 =.r a.s.a.n.= =.=.a n =..2.:.s.e = s.s e s R.a m.a g g ....,.r _u g.r e E" .E i Id 222:22*:222:43:3333:2 : 3 3 3 3 5.: 2 2.:.2 K.2: 2 2 5. 3 3 3 3 8 : 2.5 5 5.: 5 5 3 2.:.2 2.: .g t In 8 Id 22tt22:2:ssagg4:3:3 3 33 ta=sagg=33:33.:.2.:=23:3"33:35:32:23 y a .\\ - e p"s Id 222223:22*22:RR2'E:2RR::::: 2:333 3:333:3===t:23 ES ER==E 38, i ? am e j J4 .................,========= :=== ::::::::.=::::: 3 ::: 3 r Ej 32:"z..2 2.:.3.* :.523 3 2.:.3 2.:2 2.: 5 23 3 s : 5 22 : 23 5 3 52 3 3 2 3 : : : 3 ggg===gggggggggggggg; gg R : 5 5 5.:.3 3.R.E 2:3 8.E.8..E."..:.2...2 2:3 s.:"3 2 3.= =.3 3.:.s.=.=.3.:.2:2 3 3 3 3 : s, gg R e ::::::: x..3 3 = = 3. =.n.a.n.3 3..a.s.s e..3 3..R.u.s s = = =. = = = =.= = v.. i E ( ) J W 3 gg RE:R3 3 3:25 3 2 S..:.22:2.:22 3:23.E.5 5.::..".R N :s.t.3RES.E.S.S R.R.E.R .z.. k ~1 0 3s = W 2 .E .i gg 2 2 E 2 3 3 3 3 3 :E:3 3 3 3 3..2 2:2 2 2.:.2 2 3.:.3 3 2.:.=.3.:.2.:.3 5.:.5 3..2..:.2 2.: g5 g -3 u , g, anz=na=3:3 3 3=== san =s:s.sar.::.:==.a..::.: 2:33 E.nt.r.a: ) .*4 / L 3s aa aan==xxn:::::33:333:2::33:3==== 3:sstantes:Is ( 8e e==.no 4 mme i Jf

~~2:::::::::::::::m:x a n -: x an t s a s = = = = = = = = 2 h~~

3 e e e.
.O I k n. P ' 7 e. 1 o COM rAaAGaApN Siews ft viisita ft IMPACT ON VALVES a No M4g. Pet 55upt M51GN Of 6MR 79E55URE. NB: Mit. PM 55Unt M SIGN of O M A PM 55Utt. N8 364g Revise last$ sentence to reads s ede par 8Faph does not My EM htTAlntNG COMpontNI5 ATTAINING C0 WON (NIS other pressure-retalning components manufactured Othar pressure-retalning components manufactured The bursting pressure la e 816.3 type burst test l in accordance alth the standards listed in la a48Fdance with the standards Ilsted la must be equal to sr. greater than that of the i table N4 36911 shall be tensidered suitable table Ng.Mgl.1 shall be considered soltable seatest pipe to be httached to the component. for use provided the destga is coasistent with for use provided the dest a is censistent with ediere the burst preisure of the usatest pipe t the design philosophy embedled la this Secties the design phileserby embedled In this Seitlen-4 ' Is celeviated by 11 [eguatless,ks j of the Code. pressure retalalag ' s j of the Code, pressure.retalalagy { j. not included la Table Rt.36gl.1 may ' used if met:lacluded la Table NB.36g11 ser be if;[! i p* t5t/0* :. M N. ther satisfy the requirements /ef N8 3300. :The - they-satisfy the requirements of at.320dNThe', ( ,t prestore design shall be~ based en an analysis pressure destga shall be b. sed on an smalysis D - ediere consistpet with the general design philesyhy coaststent with the general design philosophF embedled in this Sectlen of the Code or espect. embedled la this Sectlea of the code er.espert. 5
specified slalaum tensile strength of maatalstressanalysisassescribedInAppendis sental stress analysis as descrlNed la Adpendte pipe materl. pel Il or en AN51 816.g type burst test. The Il er an AN51 816.9 type burst test. The j
bursting pressure la a B16.3 type burst test bursting pressure la e 316.3 type tgrst test I * "plpe. a Hed salt tMstness of i , must be equal in er greater than that of the must be equal to or rester than that of the meatest pipe to be attached to the campa=aat, seatest pipe to be a tached to tNe cespeeeet. g,,,,,gg, 49,,,,,,,,p,, g,,,,, g 48 5056 CC;i$lMRAllet of FA4ETfD Consill0N5 IIO.M56 - CON 51ptaAt:0N of FAutif0 CONeliie:5 ' & H5i Revise to read: This applies to piping. I H8.M56. I. Pf anl55tett PM55uat H5.MSL). ptanl551stt paillust gg.gg. COMstegnAll0N of FAuttle Concill0Ns t Under any faultad Conditlens specified, the Ibider s,ar faulted Canditleas specified, she if the Design Specificattees INA 3250) specifies h permissible pressure shall met escoed the destge paroissible pressure shall met etceed the deslge anyfaultedCeeditlens(NS.31l3.4)therules } pressure lp calculated la accordance with pressure calculated la accordance el h coatelned in Appendla f may be used la evaluatlag i Equation (2 of NS 3641.1 by more than 100 per fquellen of NO.M41.1 by more than i per these faulted Ceedl,tlens. Independently of all ; j cent.
~~cent, other Destga and rating Conditless.~~
l l 38 3 56.2 - ANALT5I5 Of piplNG COqp0NINIS l l 3 NO.M$$,2 ANAtillS Of piplNG COMPONENTS i g t i under any f aulted Condittens. Equatlea (g) of taider any faulted Condittens. Iguation (9) of l j NO.3652 shall be met using a stress llelt of NB.M 52 shall be met using a stress llelt of 3.05,. 3.05,. ~~ l ns.MF3 - SpfCIAL M5fGN MQuistMENIS ggy. SpfCIAL M51GN arquistNEmil No.3673 sevise as follows: This applies to piping. i l for piping compements esempted in Mt.tlle free for piplag compements esempted in NS 2510 fren 1. To speatas paragraph add designetten i ' the special esaminatten requirements of NB.2500, the special esaminatlee requirements of 118 2500 NO.MF3.1 - COWONfuis NOI EIANIMO \\ the following special design rules are applicable the following special destge rules are applicable: 1 1 2. new a (a) The design stress.latensity values. 5. of (a) The destga stress.latensity values, AppendiaIusedlathedestgaanalysisshaftbe la I used la the destga analysts sha l of P 6
~~N 8~~
.anitlpiled by 0.6t tiplied by 0.6L be g ,,.3,3,,,, ,,g m,,3 j (b) The alternettag stress.latensity vefue, b) The alternettes stresulat'ssity value SaIn deteralmed by the fattgue analple for al. determined by the fatigve ' analysis for' leiere the ficable material and prehtt e fore ensalaatt freguired under NB.2500 are na6 al pipe slees lar r than I inch shall not see 1 pipe stres larger than 1 lach shall met sceed 0.5 times the va se of 5, values for I lack esteed 0.5 times the value of 5 from the appil. performed, the full value of the design stress free the appll. able fett curves. The 5 cable fatigue curves. The Salt values for I lar% latensity. Sm. and the full fatigue curve value* l maalaal p slaeandsaaldgshall met escoed eenleet pipe site and smaller shall not escoeg 5a. mer be used la. a piplag design and analysis. l the value of 5, from the applicable fatigue the value of s from the applicable fatigue. e
~~curves, curves.~~
l f 4 i t 1 i I t L.__... i .E
~ p (' O v w. ' ' ~ wtdra 'n IMPACTONVAi.VES 4 c00c PAaAnnArn Sema 'n. e l 9 lable he-4622.1 1 Table H8 4622.1 1 Table NB.4622.1 1 p4vlu as follow s he effM. t I Decrease la Temperature Mlalaum geeldlag slee Decrease la Temperature Mlaismas teeldlag time 1. For P.aumber 6.' change alahman temperature at telen Mlaleum Specified Secreased Temperature at teles Mlaleian Spectfled secreased iesperature from 1400 to 1250. I Iseverature leeurs Per Inch of Temperature leeurs Per Ingh of Degrees f Weld Thie'. ness Deerees F Weld iniciness 2. Add a seu Note 1,A.(4) te nad I I I I (4)Postueldheattreatmentismelther 50 2 50 Il 100f 3f 100f 3 required or prehlbited for hard surfaclag en -t 150 S 150 S be n estal has papwted carte centeet H 2 g 2 g a 200 le 200 10 not more than 0. 'ihese,esiusi. hesi i, eat. eat i m,eniures 2-aa a ~ '" a aa' i ihese,estueid oat t,ea. i niu,es and times are applicable only t
~~1. P.3 and lleet are applicable only te P.I. P.3 Note 4. P a m r 4 esterial say he cooled P.12A and P.128.~~
P. IIA and P.128. pgum,'a "dt sold heat treatment heldlag Se air from the pe d 'a aa"a' a*'r=" - r %se,estueu eat tre.amarte,aiores ikese,esiseu heat iresi.e. ie.,eraiures and ii.es a,,i, sei,i P.i. P-3. PirA Se i. and it.es a,,i,eni,is P.i. P 3. Pi a Se i. Plte and PltC. Pl!8 and F1tc. ne 5120 TIME OF EIAMINATION of WELOS M j g. TIME of IIAninATI(se Of M LD5 as.$170fb]sevisethread no effect. g esaminettonssbartl'cleerliquidpenetreet Acceptance esamlastlens of melds shall be Acceptance esamisellens of welds s' hall te (b) Magnetic li be performed after any erformed at the times stipulated la the performed at the times stipulated la thq fellemlag subparagraphs durlag fabrication. fellemlag subparagraphs durlag fa6cicatles regelred postield heat treatment eecept that and lastalletten, escept as otherutse specified and lasta11stlea, escept as otheralse speelfled melds in P.umsber Itaaterials may be esamined la me.5200 and 110 5400. la at.5200 and at.5400. either before or after postield heat treatment. 11 eld surfaces that )re covered alth meld setal th) Magnetic particle er liquid penetreet (b) Magneticparticleorligelipenetr&st claddlag shall be esamlaed before the meld. esaminations shall be perfereed after any esamlastions shall be performed after any metal claddlag is applied. Deld surfaces uhtch reentred postueld heat treatment escept for regelred postuele heat treatment escept for are set accessible jefter a postueld heat j P. number 1 asterials. P.ilumber 1 materials. treatment shall be psamlaed prior to the opers. tleas d ich caused his laeccessibility. ns.5410. EsAMINATION AffER Nf0A05fAllC f(5T 90-5419. (IAMINAll0N Aff!E Mv000llAllC it.T M i}g Sevise to ryad: g3 5400 applied te vessels. Subsequest.te the hydrostatic or pneumatic test Subsequent to the bedrostatic or paeimatic test After the hydrosta[lc or pneumatic test of a of a vessel, all selds and heat.affected of a vessel, all molds and heat.af facted wasel, all i=14 Jelets and heat effected senes surfaces Jelalag ferritic meterials, lectedlag surfaces Jelalag ferritic meterials. Idcluelog of Categories A.B.C and B used to Jelet ferritic lelats and selds used to repair ferritic meter. Jotats and melds used to repair fertitic meter. .asterial-andmelds>sedtorepaleferritic tal shall. when physically accessible. he sal shall, whea yhysically accessible. be meterial,shell. d en physipily accessible, esamined by the sognetic particle or ligold esaetaed by the m. gaelic particle er liquid be ensalmed by the' tic particle er liguld. penetreet erthed. All austentic stataless steel penetrant method. 811 austentic stateless steel penetreat mothed. Al of the jelett la and menferrous weld surfaces, lacludlag the and esaferrous w Is surfaces, lacludlag the sostealtic stainless steel and eenferrous 4 heat affected tone, shall be esamlaed by the heat affected vene, shall be esamlaed by the materials shall be3esamlaed by the liquid Ilquid penetreet method subsequent to en later. Ilquidpenetraatmethodsubsequesttoselater. penetreet meths4 after se latermediate er flaal i sediate er final postueld heat treatment, if any aestate er final postield heat treatment, if any pestield heat trealaeat, if any is performeds is performed. Ihis esamination may be perfereed is performed. Ints enastaation may be performed thisesaminetleaa(ybeperformedbeforeer lefore or af ter hydrostatic or pneumatic test. hetere er after hydrostellt er poeisestic test. after hydrostatic t e pneumatic testleg. steld ' ot accessible.la the i lag, weld surfaces d ich are met accessible tag. IIsid serfaces elch are met accessible surfaces d ich ere m i* la the completed vessel, i.e., these covered la the completed vessel, i.e., these c6,ered cespleted vessel, i.e.,tasse covered by t.y laternal or esternal parts of these faside DF laternal er esternal parts of these laside laternal or enternal parts of these leside l chambers are met designed for laternal access, chambers are met designed for laternal eccess, chambers met desig6ed for laternet access. shall i shall be esamlaed prior to the operatless he esamined prior to the aperstles d ich caused 4 shall be esentmed prior to the operetless this inaccessibill leelds that are covered ulthmeld-setalcle$y.ddlagisapplied. These elch result la this leaccesslbility. leelds dich result la this fasccessibility. 11eldt that are covered ulth meld-setel claddlag shall that are covered ulth eeld-setal' claddlag shall . se esamined before the meld-setal cladelag is be esamland before the meld-metal cladelag.ls. . requirements de me4 apply to tute.te. tube. sheet a 11ed irements de met apply to tutec applied. These regelresents de met apply to Jelets. ty.tute These rgets, tube.te.tute. sheet jeless. sheet je i ) ..h..... ..g .. - = = C a. 4 _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ - _ _ _ _ _ _ _ _ _ _ _. _ _ _ _ ~. _ _ _ _ _ _ _ _.. _ - - ~ _., _.. _ - _. _. _ _ _ - _. - _ _, _ _ _.. .._,__.,,,,m__
A,., q = . (. 1 s a s Coot pAnu.narn Sumin'n wician on IMPACT OtHVALVES ~ t f a The Equipment Specificatlop,does not ristric! ns.6111,1. HTDA0iitilC if5flNG No.6111.1 - MTOR0$fAllC illilNG 118-6111.1 Revise as fellows:
~~l the valves on the balls of site from inspect All components and apportenances constructed All components and appurtenances constructed I.~~
Designate first paragraph (a) witness potat, and/or installed under the rules of this and/or installed under the rules of this t Section of the Code shall be hydrostatically Sectles of the Code shall be hydrostatically 2. Add new paragr,ap (t)and(c)asfollows: tested, in the presence of the Inspector, tested, in the presence of the Inspector. Nuts, bolts, studs and gestets are eneset Nuts, belts, studs and gastets are enes9t (b) The hydrost tic test of each line from hydrostatic testing. from hydrostatic testing. valveandpumpalthJeletconnectlensever 4.In. nominal pipe s se shall be witnessed by the Autherlied Inspe 'ter and a data report completed for each., seellA-8400). (c) A hydrostat 'c test of each line valve and puur witn inlet biplag connectless of 4.In. 4 nominal pipe stre and smaller must be performed by the Manufacturer had se noted on the data report form (see R4-0400): bewever, this ] bydrostatic tatt nee'd not be tillnessed b{s the Authortred laspector. The inspector l review of the Manufacturer's test records will be his authority to ' sign the report. (this talesprecedenceeye,rNA.$200). i Nt.3352.4 has ne tapact en control valves as the valves furnishe.d are not fabr8cated. a' I + I i e t l l l 4
210.7J In FSAR Table 5.2-1, identify the code edition and addenda of ASME Section III, Class 1 interconnecting piping to the reactor coolant system and a part of the reactor coolant pressure boundary, as defined'in 10CFR Part 50.2(V) of the Commission's regulations.
~~RESPONSE~~
Large bore interconnecting piping is fabricated to the. requirements of ASME III,1974 Edition and addenda up to and including the 1' amer, 1974 addenda. FSAR Table 5.2-1.has been revised in Amendment 46 to incorporate this information. l I I r l i l l
-210.74 In FSAR Table 5.2-1, identify the code edition and addenda of ASME ~ Section III, Class 1 valves in interconnecting lines to the reactor coolant system and a part of the reactor coolant pressure boundary as noted in the previous question. i
~~RESPONSE~~
Small bore (2" nominal diameter or less) manual valves are fabricated to the requirements of ASME III, 1974 Edition and addenda up'to and including Summer, 1975' Edition, FSAR Table 5.2-1 has been revised to incorporate this information. 9 t b I s s b 7 P 9 L r y,-,,
. TABLE 5.2-1 APPLICABLE' CODE ADDENDA FOR REACTOR COOLANT SYSTEM COMPONENTS -Reactor, Vessel ASME III, 1971 Edition, through Winter 72 Steam Generator ASME III, 1971 Edition, through Summer.73 Pressurize'r ASME III, 1971 Edition, through Summer 73 CRDM Housing ASME III, 1974 Edition, through Summer 74 Full Length L CRDM Head Adapter ASME III, 1971 Edition, through Winter 72 Reactor Coolant Pump ASME III, 1971 Edition, through Summer 73-Reactor Coolant Pipe ASME.III, 1974 Edition, through Summer 75 Class 1 Interconnecting Piping ASME III, 1974 Edition, through Summer 74 to the RCS Surge Lines ASME III, 1974 Edition, through Summer 75 Valves Pressurizer Safety ASME III, 1971 Edition, through Winter 72 Motor Operated ASME III, 1974 Edition, through Summer 74 Manual (3" and larger) ASME III, 1974 Editir/ through Summer 74 (2" and smaller) ASME III, 1974 Edition, through Summer 75 Control ASME III, 1974 Edition, through Summer 75 4 Pressurizer Spray ASME III, 1971 Edition, through Summer 72 t = e en> --..-y 4we A g-9 g3m gh se
-e- ~. e. . e 's . up i ! 210.75[ E LVerify that'a11 components within the reactor coolant pressure r boundary'as defined in 10CFR Part 50.2(V) are classified as j Quality. Group A and constructed to Section III,. Class 1, of the? ASME iBoiler and Pressure ; Vessel Code in compliance with the Codes - e and Standards-Rule Section 50 55a of 10CFR Part 50,' or as a . minimum are classified Quality Group _B and constructed to Section III,DClass 2,lof the code if components meet the conclusion t requirements. of.the rule. .j 'RESPOSE:' BOP All components within the reactor coolant pressure boundary, as idefined in 10CFR Part 50.2(V), are classified as either Saf ety Class 1 or Safety Class 2, as defined in ANSI N18.2a-1975~. All i Safety Class 1 components are fabricated in accordance' with ASME i Section III, Class 1, of the issue in effect at the time of~ award of the purchase order for that' component. Changes of safety class from Class 1 to Class 2 occur beyond the' second isolation valve or downstream of a= flow restricting orifice in interconnecting ^11nes that form a part'of the reactor coolant pressure boundary. For line classifications, see FSAR Figures j 5.1-1, 5.4-10, 6.3-1 and 9.3-13. NSSS j Components within the reactor coolant pressure boundary (RCPB), as [ defined in 10 CFR 50.2(V), are classified as Safety Class 1 except those components exempted by Footnote 2 of 10 CFR 50.55a. = The .l exempted components, in most cases, are classified as Safety Class l 2. In some cases, appropriate safety class interfaces permit the classification of exempted components within the RCPB (as defined in 10 CFR 50.2(V) to be less than Safety Class 2; for example, the f SIS (accumulator) test line includes non-nuclear s'afety piping. In all cases, the equipment classifications are in compliance with 1 10 CFR 50.55a. The respective industry codes used in the construction of equipment of various safety classification are identified in Table 3.2-2. Westinghouse utilizes safety class terminology, as.definedJin ANSI N18.2a-1975, for classification of components rather than the ' Regulatory Guide 1.26 recommendations for quality group j classification (refer to Section 1.8). i 'h I t I k ~! ? + n
m --[: -210.76 I , In addition.to Code Case 1528 ident'ified in Section 5.2.1.2 of the -FSAR, identify all other ASME Code Cases (including those that are listed as acceptable in Regulatory. Guide 1.84 and 1.85) that were used in the construction of each Quality Group A component within the reactor coolant pressure-boundary. These Code Cases should be identified by the Code Case Number. revision and title for each component to which the Code Case has been applied. = RESPONSE:- BOP In addition to' Code Case 1528, the following Code Cases have been used in construction of Quality Group A components: a. Piping Code Case N-218, Testing Lots of Carbon Steel Solid, Bare Welding Electrode or Wire. Code Case N-228, Alternative Rules for Sequence of Completion of Code Data Report Forms and Stamping for Section III, t Classes 1, 2, 3 and MC Construction. I 1 Code Case N-237, Hydrostatic Testing of Internal Piping, Section III, Division 1. b. Small Bore Valves Code Case 1621, Line Valve Internal and External Items, Section III, Classes 1, 2 and 3, April 29,1974. i NSSS The ASME Code Cases utilized for Class 1 components are given below: Component Code Case Title. CRDM N-228: Alternate Rules for Sequence of Completion of Code Data Report. Forms and Stamping for Section III, Classes.1, 2, 3 acd MC Construction Steam Generator 1528-3: High Strength Steel SA-508,. i Class'2, and SA-541, Class 2 Forgings, Section III, Class ~1 Components 1484.3: SB-163 Nickel-Chromium Iron Tubing (Alloy 600 and 690) and l. Nickel-Iron-Chromium Alloy 800 at a Specified Minimum Yield ! ~ Strength of 40.0 Ksi, Section-III, Division 1, Class 1 L I L i r L-
m RC Pipe 1423-2: Wrought Type 304 and 316 with Nitrogen Added Valves 1553-1: Upset Heading and Roll Threading of SA-453 for High-Temperature. Bolting, Section III. Classes 1, 2, 3 and MC Construction 1649: Modified SA-453 - Cr 660 for Classes _l, 2, 3 and CS Construction The reactor coolant pumps for Seabrook Station will be ASME certified following the cold hydrotest at the site. Following the testing, pumps will be N-stamped, ASME Code Data Forms will be signed and appropriate Code Cases, if any, will be noted. 4 1 4 ) e f 1
'210.77 The_ sample ~1ines from the steam and liquid sections.of the pressurizer as shown as FSAR Piping and Instrumentation Diagram 9.3-5,' of the Nuclear Sampling System are incorrectly classified ' Safety Class NNS and are unacceptable. These lines are part of the reactor coolant-pressure _ boundary as defined-in 10CFR Part 50.2(V) of the Commissions' regulations. Since'the lines meet the exclusion requirements'of footnote 2 of 10CFR Part 50,-Section 50.55a,.the lines may be classified Quality Group B (Safety Class
~~2) in accordance with the guidance provided in Regulatory Guide 1.26.~~
1
~~RESPONSE~~
-TheIsample. lines from the steam and liquid sections of the pressurizer are part of the reactor coolant pressure boundary and are classified Quality Group B (Safety Class 2) in_accordance with Regulatory Guide 1.26. This classification applies up. to and - t including the first_ isolation valve outside the containment. The classification, Safety Class NNS, pertains. to the line' from the - t-relief _ valve discharge to a drain, both of which'are inside the containment. [ l 9 4 h f i b 1 a l' ] _- d F -me ~_y ,,,,e y.,- t
-210.78 Verify that the delay coils in the sample lines from reactor coolant system loops 1 and 3, as shown on FSAR Piping and Instrumentation Diagram 9.3-5 of the Nuclear Sampling System, are classified Quality Group B (Safety Class 2).
~~RESPONSE~~
The sample lines, including their delay coils, from reactor coolant system loops 1 and 3, as shown on FSAR Piping and Instrumentation Diagram 9.3-5, are classified-Quality Group B (Safety Class 2) in accordance with Regulatory Guide 1.26. This classification applies up to, and including, the first isolation valve outside the containment. 7 F b i 5 e a b 9
210.79 The Quality Group C (Safety Class 3)' piping and valves associated , with the recirculation pumps and surge tank should be identified -on Sheet 6 of Table 3.2-2. The component code should be ASME e Section III, Class 3. These items.should also be classified seismic Category.1. ~ RESPONSE: Table 3.2-2 (Page 6 of 31) has been revised to show the code e i classification for the recirculation pump and surge tank piping. t i r ' I; )' I .o i 6 8 6 b ,a: i t I ( f r D } ) x f >i i 1 4 r [
q ( fil., 2#.7#7) b TABLE 3.2-2 U (Shact 6 of 31) u ANS Principal G FSAR Safe ty Design /Const. Code Seismic g Section Systems and Components class Codes /Stds. Class Category Building (ll) Supplier Notes 9 ~ 6.3 Emergency Core Cooling System Accumula tor 2
~~ASE III 2~~
I FA E $a Boron Injection Tank 2 ASE III 2 I PA y See Note Ib $2 Baron Injection Surge Tank 3 AS E III 3 I PA y See Nota Ib E High Head SIS Pump 2 ASME III 2 I FA 3 See Notes la, j ic & 2 a I PA 3 See Note Ib Baron Injection Tank 3 ASME III 3 Recirculation Pump g' Boron Injection Flush Orifice 3 ASME III 3 PA E See Note 6 ~ ' Piping Reactor Coolant Pressure 1 ASM3 III 1 I CS/PA y ~ Boundary Sample / drain, vent and NNS ANSI 331.1 FA AE test lines beyond the first pressure boundary isolation valve. acnep rMder.se A ctntM - 3 j.* & 94~ f 3 [ PA 48 I 4, e,u /*[es M/' A#7 8 #/'"1 2 ASME III 2 I PA AE Valves 2 ASME III 2 I FA/CS AE and ANSI B16.5 6.5.1 Engineered Safety Feature i Filter Systems contaittaent Enclosure Emergency Cleanup System k a
i - 210.80 Why is the hydrogen analyzer on Sheet 5 of FSAR Table 3.2-2 not classified Safety Class 2 as are the other major components of the Combustible Gas Control System? The hydrogen analyzer should also be subject to a Quality Assurance Program that is in conformance with 10CFR Part 50, Appendix B.
~~RESPONSE~~
The redundant hydrogen analyzers are considered class,1 E instruments.. They meet al,l'the requirements for a lE instrument including 10CFR Part 50, Appendix B. The hydrogen analyzer will be removed from Table 3.2-2 as they are classified as instruments and instruments' are not included in this table. The hydrogen analyzers are on the lE Equipment List, Appendix 3H. I r 1 + b b t i Y b r o V bf-m
w.-,-, -,. --v-i- 210.81 To assure cons'iotency in the classification of fluid system components, the chiller pumps of the Boron Thermal Regeneration System shown on Page 16 of FSAR Table 3.2-2 should be classified Safety Class NNS. These components'are currently unclassified.
~~RESPONSE~~
Table.3.2-2, page 16, has been modified to show NNS classification for the chiller pumps. s e __l
^- n, .s TABLE 3.2-2 (Sheet 5 of 31) ANS Principal FSAR Safety Design /Const. Code Seismic Section Systema and Components Class Codes /Stds. Class Category Building (II) Supplier Notes 6.2.5 - Combustible cas control in Containment Hydrogen Recombiner Package 2 ASME III 2 I CS W Piping and Valves 2 ASME III 2 I CS AE (pressurized) Containment Recirculating Filter System Fans 3 MFRS. STDS. I CS AE g Filter Unit [ MFRS. STDS. CS AE Ductwork and Dampers 3 MFRS. STDS. I CS AE Containment Purge System All' pressurized components 2 ASME III 2 I CS/CE AE upstream of emergency ex-hatist filters (flow meter, throttle valve, piping) Containment Atmosphere Sample System m -h $i My4?;-- ^--lyrrr "C """ C. STOS. C:: A:: 44 c$ S( Supply and Exhaust Piping 2 ASME III 2 I CS/CE AE " a Supply and Exhaust Valves 2 ASME III 2 I CS/CE AE G" E$ 9 w-,,,- g ,,,p ~, -, -.,
I."21#. TABLE 3.2-2 kg (Sh:sst 16 ef 31) 7., ANS Principal f FSAR Safety Design /Const. Code Seismic . _Sec tion Systems and Components Class _ Codes /Stds. Class Category Building (II) Supplier Notes Y Reactor Coolant Pump NNS ASM VIII ~ CS W I f Standpipe 9 Reactor Coolant Puup MS CS W ~ Standpipe Orifice a Piping 'C ASM III 2 I CS/PA W/AE See Note 3. C x AS M III 3 I PA W/AE 2 n mas ANSI B31.1 [ FA e.2 valves 2 ASME III 2 I CS/FA W/AE See Note 3.
~~v. "~~
3 ASME III 3 I CS/PA W/AE E" ~ We NNS AR$1 B31.1 ~ CS/PA AE !9.3.4 Boron Thermal Regeneration i Subsystem chiller Pump-V5 No Code FA W See Note 6. Chiller Surge, Tank NNS ASME VIII FA W See Note 6. Moderating Heat Exchanger PA-W i, Tube Side 3 ASME III 3 t See Note 6. Shell Side 3 ASME III 3 See Note 6. j Letdown Chiller Heat Exchanger PA W Tube Side 3 ASME III' 3 See Note 6. h ~ l Shell Side NES ASME VIII See Note 6*. DRAFT e
~~1.....-~~
-... _,.. _ _ _.. ~. _ -... _ _. _,.. _, -.. ~.. -. _. _ _.. _ _. - _ _......... -. _ _,., - -. - _....
210.82 The isolation dampers and duct work passing through the containment enclosure of the Primary AuxiliaryLBuilding Ventilation System on Sheet 21 of FSAR Table 3.2-2 is incorrectly classified as not designed to Seismic Category I Requirements. These components should be classified as Seismic Category I. Revise Table 3.2-2 accordingly.
~~RESPONSE~~
FSAR Table 3.2-2, Sheet 2 is being revised in Amendment 46 to -correct the classification to Seismic Category I for isolation dampers and ductwork passing through the containment enclosure. i e d E
I TABl.E 3.2-2 (Sheet 21 of 31) I.1) 1 ANS Principal s -FSAR VQ Sa fe ty Design /Const. Code Seiamic b-Sec tion, Systems and Components Class Codes /Stds. Class Category BuQding(II) Supplier Notes 9.4.2 Fuel Storage Building Ventila-tion System Ventilation Fans W RS. STDS. FS AE Dampers 3 NFRS. STDS. 1 FS AE Doctwork NFRS. STDS. I PS AE 9.4.3 Primary Auxiliary Building Ventilation System Ventilation Fans W RS. STDS. PA AE 5-N e-PCCW and 81 Pump Area Wall 3 MFRS. STOS. 1 PA AE w Fans and Dampers i Normal Cleanup Exhaust Fans NFRS. STDS. PA AE Normal Cleanup Filters WAS. STDS. PA AE Duc'twork and Dampers Isolation Dampers and Doctwork Passing through CE 2 NFRS. STDS. I PA/S AE l Other NNS,. MFRS. STDS. PA AE 9.4.4 Waste Processing Building i Ventilation System t M yana WRS. STDS. W AE g O.< A5
210.86 The staff has reviewed the report, " Stress An_ lysis for Nuclear Valves, FP-91924-07 (Fisher Controls Co. Report) Rev. 2, dated 8/18/80. Page 6 (and other pages) of this document lists, under design conditions, " Maximum Torque Required". This torque is used later (e.g., on P. 13) to calculate Shear Stresses in the shaft. If the " Maximum Torque Required" is substantially less than the torque capacity of the actuator (stall torque), please indicate what checks are made with the actuator stall torque.
~~RESPONSE~~
Fisher Controls Company (through their representative C. B. Ives Company, Inc.) has advised there is no problem in this regard because there are travel stops provided in the actuator to limit travel. Two travel stops are provided 'n the Limitorque Gear Units mounted on the valve shaft. The mechanical travel stops are set for twe (2) positions, one at the fully closed position (00) and one at the full opened position (900) adjusted to prevent damage to the valve. Limit switches in the Limitorque Operator are set to control the limits of travel and the seating of the valve disc in the rubber seat. In Limitorque Operators, this is referred to as " position seating" as opposed to " torque seating". Torque switches are provided in the limitorque actuator to shut off the power to the motor if torque becomes excessive, which would happen if the limit switch should fail. In view of these precautions, transmittal of the maximum possible operator torque to the valve shaft is not considered to be a credible event, and checks of valve shaft stress with maximum operator torque are not considered to be necessary. i-
.s; I-210.87 ' Class 2'or 3 Piping, 1-factors' At the 5/13/82 meeting held at United Engineers & Constructors, i ~the applicant stated that presently-completed calculations.for ~ stresses at branch connections do not include the stress intensification 1-factors as defined in the Code. If.our understanding is correct, then the applicant should describe how the applicant can' assure that piping systems are in compliance with Code requirements.
~~RESPONSE~~
The final' documen' ation for the as-built piping systems,- including l both run and branch piping, will include the proper 1-factors for all branches and tee connections required for full code compliance. i L P
z_ 7-
~~f. \\~~
1210.88 Bending Moment Checks on Flanged Joints At the 5/13/82 meeting held at UE&C, the applicant stated that Code-required checks of bending moment capacity of flanged joints have been made. The applicant must provide a commitment to-perform the Code-required checks of bending moment capacity of flanged joints-in order to assure proper compliance, with Code requirements.
~~RESPONSE~~
As part of the as-built documentation for the Seabrook Plant, all flanged joints will be subjected to bending moment capacity checks I to ensure compliance with the ASME Code requirements. I t I h I 9 t I i W ~ gr g-- e p-- y-r+--~ W}}

ML20065H646

Contents

Text

SUMMARY

SUMMARY

Dear Branko:

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

Navigation menu

ML20065H646

Text

SUMMARY

SUMMARY

Dear Branko:

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

RESPONSE

Navigation menu

Search