ML20203P344

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Forwards Responses to NRC 860321 Request for Addl Info Re Drawings & Weld Dimensions.W/Three Oversize Drawings
ML20203P344
Person / Time
Site: 07105942
Issue date: 04/01/1986
From: Schwoerer F
NEUTRON PRODUCTS, INC.
To: Macdonald C
NRC OFFICE OF NUCLEAR MATERIAL SAFETY & SAFEGUARDS (NMSS)
Shared Package
ML20203P345 List:
References
26741, NUDOCS 8605070015
Download: ML20203P344 (19)
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Text

{{#Wiki_filter:7/- 59%2 RETURN TU 193_gg DOUTROn PRODUCTS inc 22301 Aft. Ephraim Road, P.O. Box 68 Dickerson, Afaryland20842 USA 301/349-5001 TWX: 710-828-0342 April 1, 1986 Mr. Charles E. MacDonald, Chief Transportation Branch Office of Nuclear Material Safety and Safeguards U.S. Nuclear Regulatory Commission Washington, D.C. 20555 Ref: (1) Certificate of Compliance"No.~5942 (2) NRC letter to Neutron, Pro. ducts., dated March 21, 1986

Dear Mr. MacDonald:

-~' Responses to the requests for'addiEiona'1' information transmitted by reference 2 are enclosed. Also enclosed are eight copies of Neutron Products drawing 240139, Rev. E (3 sheets), containing revised notes and weld dimensions, in response to reference 2. Very truly yours, NEUTRON PRODUCTS, INC. g P pg 1 Frank Schwoerer, Vice President p gc (( 4pg 4$60(, ~g _ ' - ~ _ _ FS:mvc ~ Enclosures t;uss \\ yytSECRE -._ pocKgt CLER1 f) 4r EE NOT iE0J RE) =

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8605070015 860401 DR ADOCK 0710 9 2 [

E i. DOCKET NO. /- CONTROL IR).__ [h/ DATE OF DQC. 0W/)/fSh DATE RCVD._ 0W8W$b FCUF PDR FCAF LPDR k?! I&E REF. hTIUR SAFEGUARDS FCTC __ OTHER 'aCRIPTION: k, W Ae' %~u . _Ww& f a to u d i z 1 4, 1~ - A3/H76 /VA#% mmt NGL '/ (

s April 1, 1980 RESPONSE TO REQUESTS FOR INFORMATION IN NRC LETTER OF MARCH. 21, 1986 DRAVINGS 1. The portions of ASME Section III, Subsection NB that pertain to welding are NB-4300, Velding Qualification, and NB-4400, Rules 0taerning Making, Examining, and Repairihg Velds. These articles in turn refer to ASME Section IX for weld qualification and welder qualification. c 4 The welding on the liner meets the requirements of articles 6B-4300 and NB-4400. The welding records, however, are in accordance with Sections VIII and IX. Because of the small size of the liner, welding r ecords are fully traceable to specific welds and meet the intent of Section III, Subsection NB. 2. The typographical error ("AMSE") in Notes 1.B and 1.C has been corrected to "ASME". 3. The drawing has been modified to show the size of each fillet weld. 4. Note 3 has been deleted. STRUCTURAL 1. The valve body 'a attached to-the base plate (item 27) by two screws and a valve ca,ture plate (item 47). The base plate is welded to the cover plate. The structural adequacy of these attachments is demonstrated by the enclosed revision to Fnclosure 3D, originally submitted by our letter of February 28 1986. Two insert pages contain calculations of the stresses in the we.us that attach the base ple.te to the cover plate. 2. The i 0.5 in. tolerance is not applicable to the cavity dimensions. Note 3 pertains to the cavity and states that, "The tolerances do not infer variations which affect the proper fit or function of components". This conclusion has been confirmed by: A telephone conversation with General Electric on 3/26/86; and Measurement of the cask cavity of one of two GE 700 shipping packages while on lease to Neutron Products in the Fall of 1985. Prior to the first shipment using the liner and sleeve in the GE Model 700 shipping package, a trial assembly will be made of the cask, sleeve and liner, and dimensions and assembly clearances will be checked to verify that adequate clearances exist to accomodate the differential thermal expansions discussed in responses #3 and #4, below, without closing any gap between the cask cavity, sleeve and liner. l 1 / NEUTRON 3RODUCTS inc 1 a

RESPONSE TO REQUESTS FOR INFORMATION April 1, 1986 Page No. 2 3. The average coefficients of linear thermal expansion over the temperature range of 70 to 3500F of austenitic stainless steel and aluminum are 9.4x10-6 oF and 14.4x10-6 oF, respectively. The thermal analysis, f f submitted with Neutron Products letter of February 28, 1986, gives temperatures of 3030F for the inside surface of the cask cavity. 3380F for the aluminum sleeve, and 3600F for the liner outside diameter. Thermal expansions have been calculated as the product of the average coefficient of expansion, the temperature change from 700F, and the linear dimension. This shows that the sleeve will expand axially 0.124".. the liner will expand 0.095", and the cavity will expand 0.072". As stated in response #2, above, a trial assembly will be made to verify that clearances are adequate to accomodate these expansions. 4. Thermal expansions in the radial direction have been calculated by the method outlined in the response #3. The nominal radial clearance at room temperature between the cask cavity and the outside of the sleeve is 0.0625". At the temperatures stated in response #3, this clearance is reduced to 0.050", which is acceptable. The nominal radial clearance at room temperature between the inside of the sleeve and the liner is 0.0625". At the temperatures stated in response

  1. 3, this clearance is increased to 0.067", which is acceptable.

The nominal radial clearance at room temperature between the flange of the liner and the cask cavity is 0.0625". At the temperatures stated in response #3, this clearance is reduced to 0.057", which is acceptable. NEUTRON )RODUCTS inc

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g .._.57Acss -_UAllt96. Ut'sM__lowd. /W4cr = ..37, L = 17f fst _-_._- _. -. -. - - %W STXeu % 7ao_f.L .- S E ? 2 fa. = ~ d '~~~ ' ^ ~ * ~ ~ - " .m.-., _m. e,_ e m oue e-egF v.-h_ _ +. e em w_.- g e. e_. m s ~ ' ._.-...._..__".".....-.._~_._._L_ t l ....--.___ 2 1 ...__.__.._...___..._._..__.______.__,._..L m f . _ _,.._.._._ _.__ L. 1 _.__ l } l .f._.._.___..*..__,_.____,_ l .2 ...-..._.._._.-....._........_.._1 1 ) l n' i i J

EX/CLoSvM Sb ... a [ o l~. I'f.. - fot A So m -Dou)Al t u Pact-Tite-Beubi^14 Srtesse Ist 79hir tk3b (Lib) Alf EEE hi1&L'f A 09, ?JecAUTE 7N6' OHL-Y' .Loeb is. 7?fe s/S7GVr* 0F. 7?f6 Lib frSEZ.F,. (//r/ps),... W144 15 MdGl 1GTS TAH9H TW6' 20 4 % IMt'oSeb is/ A-

  • Ta/~30u/I lHP&cn THt=tafofE,

/ T' is OBVoods w irifo/r-A bottV4 ExPu ct r A-A44Y'.5GS ~7?f47~ "TetG .BeX)h rDr STASTM Adb y ..- - bEREC TroNS & A-CCEPTAbts.. SifL. Yoam hpd / ERhM t AIE StfEhlt. Lokhirlf itJ L.iMe-A d4-s4. R&laa FtAdqE. ~1 l Ml= /80 (CesInvart) +- loo (LikR. ,14rJ 11111 & i Santo A.4etse -O

  • 2to 24r ii 6*.% 284 : 2707. e 2.fr/. /gfoo g

. _ Sec2ht. M e t =./G r *7 /0 5 7 s [ +1 tu. . '.Soless = IS,773 ja ._....... -.t.. W fb $ YfNE $ l$ NlNSb$ $ flMk i Wif L- )$lG 7" WW SS Of / WON W Of',$t h e Mex. 7ExKrt2 Srfe O Coo 'f *G foo (,AsM6 E C4916EIr5.f) f .- p. sae =. m a n a= se,fo. 2F v,m% - z:fo..- 33 I.. f 4 = -... <w , - ~ ~.. _. ..-.--.__..-.4. ......~.4 ,4-- .7 4 m ( + 4 -p._ e . _.. g. .._. g. . i.. t ( 4 h O l f .-.-.....:...-.--.....~--.-......-.....-,......+.- i t I

EllclosaM Sb la cP /f EkdMoArc w suPAokT" oP 7W ISotATrosi s/Atass. osert;rupai9 HoAeur /t AS 2615LotMb PRD td. ..{ ..7 l l ~ + 4SSJpg V/41.VF PJV073 W .O gg, 3,is m .%Ik --( f.W. ~ . -__._.] .. _ p,g , p t,s. g .. W,ugur = /.33 la 14 @ /) = S~1t s. tis & ~270}....-. T.esisridq HoNeur-n P90drDc~b 8l/ ~2.*/O -3L SthWS Y CM . T.. citu4,- w,ru 'f % t < M. WerAs + e g 'SW .s 9 w ~ b--i.o -,i%Mm ~ ', ~ ~ ~ ~ kssons TvRc5 'is Phr%wnonhu ro "berstrrod (fr4rb B@f RiorgeD) ~~ festsr7d4 poa.mtr = F*{t.o + 'h +.*,/N) =./ '{51F = 3r8[t5 '~ F ' 24C'7 AL ~. 29.x*7 f*L 55 '{tGLb.51gets @ yeo *F_ 3rfe3G'. ord..tJEtM u ,,,,j * [iA slas ) t u.mlo7so =//ys/ .SF.i %~1.. .I:I srue i,s fse .scpeJ dh't* Wf1 = 12 i YSb.Crkss = 2 760 Y. .* */"....-.....,. /ZGjt 9 = Sf...s. I.]. (.. otoa. + B. 2. HyArwrite. ner evswMn-hfMedrW-77te0.xAs GRPAd*AI Be7tdas ont-is 6hitine.) .. AJb.1 r b (Aastelo ne.) FpeM fic M 7df /.rb fie*4 "kV.. *A ~% Y. ~ ~ t5tmKN~i ~ caen or planst-ewsa< s - ase-rs d J-4 7 57

  • to u A. *p

).5-=. . 3 6 e." . _..' 3 6 mro.- .Ar-yk *F .l ' & e. h o f r~ >1y$c/oJ 'tkn=/f*= OV$ E _ [ s s,. s. w..,o y.,:y A..ya..e-9 i

_._ Ehla.o30/.E 3b.- /o W M If .e ._a-o.~~ 3.,- w. ,s ..m- ." * ~* ~ vv ~ TAISM.T' oW JME' to th17.ER. SoPhtr of 1soM7m) MA t-M 'l ..Ex4inide SitesSL._ts1 WEl.hs 7fh W. kvTn W v'Atvr.50Phk' PaHE' .Pe +Tr ht-I'). (Pkb-Nos. AS -. ..C a A-2-)J 7b Gofer aid.o x1. hm19 No..:140157.) r-5 m m J 4 = ".. y _ , a y_ __ __. M .,j 1 lieMeAt 2,70.y4.2/42.y.0Kr.f.lGy./441.'3A3._ ._ / Wt /37*.100 3. 07 (,a = ezay TesrSridGj Roner!T IS f /7.o Vi D & D )' Y(o Nidth Alt.- }}hdAlb -. _ _ SilP/blT fL4rer :.. - _.. _1_ _sih s :_- d M2..2 *[l d =._.2.S.'. t* wk: -_t y a .I u d.. -. K= 0.5y. O.$ _ M _ Ib dMhb_. K5o W._ 6hsb) -. _... ~. (T; = .._.. S/~, fi. LYiet.b-_ _.-...__ .// 58 e.. Vao *F )- G .= .1. lf ___._. _ _.1 .-.__ Sin /L =_ signg -__ _ _.._ _u W7^ oL. VAuf.h_S'uflUtr fL4rtC =.-/.05' tl ........ -. Le 4-b. M. 2 7 o y

. J. o S V 2 9 0 ? '22 5 S~24

..m _.s. b ...y _'p. rp //, '3h~g 5'E = /C... g .aw -..*4 ,w&de.. m. 6 ,m...w, ..,ya_%,,,_ + 1

s5W<S'M%ef'"'zu ~ // of /Y TAIT.c X.-FDtUI,Ae Fo2 PI.AT Pl.ATES Notation: W = total applied load (lb.); ta = unit applied load Ob. per eq. in.);i = thickness of plata (in.); a.= cnit stress et otif;ca . -of phte_(Ib. per sq. in.);r y - vertical deflection of plate irom origin d position (in.); O = alope of plate measured from horizontal (rad); 5 s B = modulus of elasticity; m = reciprocalof r, Poisson's ratio. g denotes any given point on the surface of plate; r denotes the distance of g from the cen ter of a circular plate. Other dimensions and corresponding symbols are indicated on figures. Positive sign for e indicates tension at upper surface and equal compression at lower surface; negative sign indicates reverse condition. Positive sign for y indicates, upward deflection, negative sign downward deflection. Subscripts r, f, a, and b used with a denote respectively radial direction, tangential direction, direction of dimension a, and direction of dimension b. All dimensions are in inches. All logarithms are to the base e, g Gog.: = 2.3026 logi.2). - (See pp. 215,216 and 218 for stress and deflection coefficients.) g T*"'*'*"***d*A**" f M',*',"c# '$** , am Cirsulat sad sorul [' h ~ l ' 5D~.E"-'

  • "[on+u( -5)] n--5[on+n-($'+o;]

{ gio a.- 3F( *-!) r* (3= + Or8 w.

== - ..=tne [(3n + I)atx wr+sa =-i-i3 W_!!!!!!. al.,,t.,3u..-,, .*.*,.on o M..-*""..","=",+"' = y . = >c,'- . ~... ata ) .. e, m d ut r <r.) --g[n +(n + u w;-(n - us-on + ns] --n[= 4 (n + n w;-(n - us-m4] = .r >mm -nr W mt.a . - IG Env L. -,, + e. - o,...,,,, w xa - n+ - m + - - e 1 >= r# re (n + 1)# =+ J f(n f 1) log *-(n-1) + (n - O se== 2 (* ~ t) + C* + t) t 8 ( ~ lI' ~I" ~ I (Al g. r > ra) ar = - 3 F(st - 8)[(12m + 4)(at - r9,2(as - 1)r#(at - r$ _ g,, gg g ]J-8 a per.sesg y - -- lerEnv L si + 1 (n + 1)v r ggggg Mas er = se = -fa + (n + 1)los*-. -(n - 1) Muy= 3,"g - dre !as *- - M (At eenter) 8 For te very aman (concentrateillona) Mas y qIE ~ff[# L gi a,,) , *wr i-na 3 wKrir r-g. .Q,:. m. s. .' ~... Q. ^ .c r. g . ~. ,/ affE"W es (At e r < r.) M. a, - a, - -h (n - 3) + ( + 1)los *,-(n - 1 3, ofra&us - -. 3 U,,"i',,,,1)[(3m + 1)(d - r9-v + r.9,w,; + e -,.9 - (n - 1)r#(a - e )] a s s x=.,. o ,n,,,, I y (Al f. r > rn) a, s.,- -~ (n + 1) log

  • 4 (n 1) -(n:I se -.

(as - 1) -l- (n + 1) log * - (n - 1) (n I g g ,,,,,,3 F(m' - !)f (3n + 1)(e8 - t'),g g, (n - 1)re*(o' - r$ 1 E g 2*E=P L 2(= + 1) 2(= + 1)e .] g M- - *'7 ;,"[o +';',y,p o-,#(w;+i)] q. ,,. -,,,( aiaa.r) f

4.,N,.a.orm*Y..,,,

. (n + 1)Ica *".! .(n + 1)losi+ (n - 1)' .,1 3 # [= + (n + 1) log * ~.L. (n - 3)[u.'#,)-)] (At point elIml.f) Mu a, - se - r. s m ~*d"**6" M,f4 (At g)#~ ar = (Mas a.) = - plas n) _i+(n + n w E _ -+ (n + n w { .. - r.(v - r e +.m, e. iae + n.w, # + xe. - 5,.e + men 9 g; x ( ,, x-+ n m -i r +no),,, mn + nwr s.e no,},, n= + n>m,.-a.ag +,, g 09= t OKre 3(9s + 1)Kes* (in + 1)(5= + 1)K,em ~ Mm a 8 I' " sun + D: 6 f($n + 1); n 2(= + 2)'" " 2pn + 1}'" " 4., + 3 E " 12(n* - 4'I' " 3f2= + 0 n'Ett 4e + I en + 1 en + t N R3= + D 4, + 3 f eest ett 2(n + 0 %.2, - ~ ~; u n h, s.MEdd ai r - r.) M- - &[i + ("l') w 'e;p] .ta x c,,'.,*,$','j (trunnica loa &es) g

  • M I?

7. (See else p. 216) !l \\ 1 . * ~ s'd.m (At d a, - [pn + hh-(n + U] ag,[(n + 3)j-(n +1)] y-3F n;_],p[(a -,33] 3 s . s. / (At ds.),Mu= 8d:e.-$ 'lIIIIIi!! pg,g,,),,., __3 mn + n y,,, ~* 3 m in - De g w s,w= n rav c,, I a..?. 1

MM&M M -p g ~ ~ LISTING OF BASIC PROGRAM TO CALCULATE BENDING STRESSES IN LINER LID 100 REM GE700 LINER, STRESSES IN TOP PLATE 110 CLEAR-12D DIM R(7),SR(7),ST(7),Y(7) 130 DEFINT I 140 FOR I=1 TO 7 150 READ ' R'(I) ~ ~'~ ~-- 160 DATA 0,2.65,5.3,5.71,6.688,7.038,7.44 170 NEXT I 180 M=1!/.27 : T=1.5 : E=3E+07 : A=R(7) 19D SF=-3/(6.28*M*T^2) 200 YF3=-3*(M^2-1)/(6.28*E*M^2*T^3) 210 YF2=YF3/8! 220 LPRINT "R(IN)","SR(PSI)","ST(PSI)","Y(IN)" 230 LPRINT 240 REM BOLTUP LOADS 250 LPRINT " STRESSES AND DEFLECTIONS FROM BOLTUP" 260 REM LOAD COMBINATION 1 270 R0=13.375/2! : W=106800! 280 FOR I=1 TO 7 290 GOSUB 3000 300 NEXT I 310 REM LOAD COMBINATION 2 320 R0=11.414/2! : W=-106800! 3 330 FOR I=1 TO 7 340 GOSUB 3000 '350 LPRINT R (I), SR (I), ST (I), Y.(I) 360 NEXT I 370 LPRINT ~ 380 REM ADD PRESSURE LOADS 390 LPRINT." STRESSES AND DEFLECTIONS FROM DOLTUP PLUS PRESSURE" 400 REM LOAD COMBINATION 1 410 R0=13.375/2! : W=2300! 420 FOR I=1 TO 7 430 GOSUB 3000 440 NEXT I 'l 450 REM LOAD COMBINATION 2 460 R0=10.62/2! : W=-2300! 470 FOR I=1 TO 7 480 GOSUB 2000 '. ' - 490 LPRINT R(I),SR(I),ST(I),Y(I) 500 NEXT I 510 LPRINT 520 REM ADD LOADS FROM TOP DOWN IMPACT 530 LPRINT "STGESSES AND DEFLECTIONS WITH TOP-DOWN IMPACT" 540 REM LOAD COMBINATION 1 550 R0=10.59/2 : W=114258!+60048! 560 FOR I=1 TO 7 570 GOSUD 3000 580 NEXT I 8; \\ ~ 590 REM LOAD COMBINATION 2 6CO R0=14.13/2 : W=-114258! _ 1 S

M* 15 of N- ~ 6.10.FOR,I=1 TO 7-623 GOSUB 3000 633 NEXT I 643 REM LOAD COMBINATION 3 653 R0=10.42/2 : W=-60048! 66D FOR I=1 TO 7 670 GOSUB 2000 683.LPRINT_ RII), SRII), ST (I )., Y ( I ) _. 690 NEXT I 7EO END 2003 REM CASE 2, ROARK TABLE X 2010'IF R(I))RO.THEN 2200 202D Pi=M+(M+1)* LOG (A/RO)-(M-1)*RO^2/(4*A^2) 203D P2=-(3*M+1)*R(I)^2/(4*RO^2) 2'43 P3=-(M+3) *R (I) ^2/ (4*RO^2) 2 50 SR (I) =SR (I) +W*SF* (Pi+P2) 2069 ST(I)=ST(I)+W*SF*(Pi+P3) 2G70 Pi=4*A^2-5*RO^2+R(I)^4/RO^2-(8*R(I)^2+4*RO^2)* LOG (A/RO) 2083 P2=-2*(M-1)*RO^2*(A^2-R(I)^2)/((M+1)*A^2) -2090 P3=8*M*(A^2-R(I)^2)/(M+1) 2100 Y (I) =Y (I) +W*YF2* (Pi+P2+P3) 2110 GOTO 2400 2200 Pi=(M+1)* LOG (A/R(I))-(M-1)*RO^2/(4*A^2) 2210 P2=(M-1)*RO^2/(4*R(I)^2) 2223 SR(I)=SR(I)+W*SF*(Pi+P2) 2230 ST (I) =ST (I) +W*SF* ( (M-1) +P1-P2) i 2240 Pi=(12*M+4)*(A^2-R(I)^2)/(M+1) _2253 P2=-2*(M-1)*RO^2*(A^2-R(I)^2)/((M+1)*A^2) 2260 P3=~(8*R(I)^2+4*RO^2)* LOG (A/R(I)) 2270 Y(I)=Y(I)+W*YF2*(P1+P2+P3) 2400 RETURN / 3000 REM CASE 3, ROARK TABLE X 3310 IF R(I))RO THEN 3200 ~ 3020 Pl=(M-1)/2+(M+1)* LOG (A/RO) 3030 P2=-(M-1)*RO^2/(2*A^2) 3040 SR(I)=SR(I)+W*SF*(Pi+P2) 3050 ST(I)=ST(I)+W*SF*(Pl+P2) l = "7

  • 3E60 Pi= (3*M+1) * ( A^2-R (I) ^2) / (2* (M+1) ).

3370 P2=-(R(I)^2+RO^2)* LOG (A/RO) + (R(I)^2-RO^2) 3080 P3=~(M-1) *RO^2* ( A^2-R ( I ) ^2) / (2* (M+1)

  • A^2) 3090 Y (I) =Y (I) +W*YF3* (Pl+Pa+P3) 3100 GOTO 3400 3200 Pl= (M+1)
  • LOG ( A/ R (1) )

3210 P2=(M-1)*RO^2/(2*R(I)^2) i 3223 P3=-(M-1)*RO^2/(2*A^2) 3230'SR(I)=SR(I)+W*SF*(Pi+P2+P3) 324D ST(I)=ST(I)=W*SF*((M-1)+P1-P2+P3) 3250 P1=(3*M+1)*(A^2-R(I)^2)/(2*(M+1))-(R(I)^2+RO^2)* LOG (A/R(I)) 3260 P2=-(M-1) *RO^2* ( A^2-R (I) ^2) / (2* (M+1 )

  • A^2) 0270 Y(I)=Y(I)+W*YF3*(Pl+P2)

\\ '3400 RETURN- \\- --...,----:'._7-~ l A e . 0 L

e#ctose#2Xb' f./f lY c ANALYSIS OF GE700 CASK WITH NEUTRON PRODUCTS LINER R(INi SR(PSI) ST(PSI) Y(IN) STRESSES AND DEFLECTIONS.FROM BOLTUP 2.65' " ~ 6382.82 6382.82 5.501994E-03 O .. ~ ' f82.'82~~~ 6382.82 4.774858E-03 6

5. 3 6382.82 6382.82 2.593454E-03

~ 5.71 6358.99 0 2.126049E-03 6.688f -431.5991 0 9.181204E-04 7.038 -213.5056-0 4.869167E-04 7.44 0 0 0 STRESSES AND DEFLECTIONS FROM BOLTUP PLUS PRESSURE O-6934.557 6934.557 5.863322E-03 2.65 6835.131 6879.523 5.075533E-03

5. 3 6536.855 6714.422 2.738558E-03 5.71 6454.433 297.7783 2.242967E-03 6.688

-455.0215 320.9848 9.679457E-04 7.038 -225.0923 294.7991 5.133411E-04 7.44 0 265.6846 0 STRESSES AND DEFLECTIONS WITH TOP-DOWN IMPACT 0 4123.919 4123.919 4.972629E-@4'. 2.65 1328.11 2576.392 8.931384E-05 , _ 5. 3 -6981.948 13872.42 -3.923448E-04 5.71 -3213.401 12977.26 -3.575273E-04 6.688 -2628.494 10942.58 -1.832279E-04 7.038 -142.8217, 10253.62 -9.854301E-05 7.44 0 7024.885 0 e S e.. e. .O N i .+ ..J -.. l i O j i ~, s 4

OVERSIZE DOCUMENT PAGE PULLED SEE APERTURE CARDS NUMBER OF PAGES: ACCESSION NUMBER (S): R(oO 50700 / fo /9 i (S "O APERTURE CARD /HARD COPY AVAILABLE FROM RECORD SERVM:ES BRANCH,TIDC - FTS 492-3939 1 wmw -w.pw m mwwm ae -ww wemy- ___._.w--w,-.,_,..,__-,-- -}}

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