Text

Design Calculation, Qualification for Qai Duct Supports in Stress Rept 2848-1
	ML20069F162
Person / Time
Site:	Fermi
Issue date:	07/20/1984
From:	Chuang C, Raju Patel; HOPPER & ASSOCIATES, ENGINEERS
To:	;
Shared Package
ML20069F099	List: ML20069F095; ML20069F118; ML20069F135; ML20069F141; NRC-94-0050, Design Calculation, Qualification for Qai Duct Supports in Stress Rept 2848-1;
References
	CON-NRC-94-0050, CON-NRC-94-50 2806, NUDOCS 9406080155
	Download: ML20069F162 (191)
	v • d • e

{{#Wiki_filter:, 6 to r NRC-94-0050 [80& D.C. No. Page h t Table of Contents 1 Title Page No. L / Introduction 1 i Purpose Sumary of Results 1 Calculation References 3 e 0 General Nomenclature 7 Support Index Sheet Calculations: Support Load Determination h Part I lh Support Design Load Table Bounded Support Load Assessment 29 Part II Structural Support Calculations 2.1 Part III Other PAhT E-Ad+ Pxmv A%E%aEF bb k-i 7) List of Attachments 9406080155 940603 PDR ADOCK 05000341 P PDR e

T D.C. No. ill?O4. Page / Op b INTRODUCTION The responsibility for HVAC ductwork and associated support design was originally with the Fluor Pioneer Co. for all QA Level I/ Seismic Cat. I duct in the Reactor and Auxiliary Buildings, excluding the drywell. The original duct design was based upon a computer analysis of the systems between structural anchors to establish support system design loads and duct adequacy. This duct analysis was performed assuming the supports as being rigid attachments to the building. This assumption yields a high system frequency response and consequently artificially low support design loads. The support structures were designed using an established stan-dard and by Engineering judgement. The seismic support loads calculated by Fluor are based typically on zero period accele-ration ( 50 Hz response) for the OBE case at 2% damping. 1 l l 1 l

F i D.C. No. 28Cb Page

2. Of N 1!

i ~ PURPOSE This calculation establishes a conservative support design load by methods established in the reference design calculation 2935. The method provides increased loads to account for shifts in system frequencies due to support flexibility. Structural cal-l i culations of the subject supports noted on the index sheet for the Fluor Stress Report No.2649-/ are contained in this design calculation based on the newly established loads. l r E

SUMMARY

OF RESULTS ( All support calculations contained here comply with the govern-ing codes and standards addressed in reference design calcula-tion 2935. Member stresses are within limits expressed in the AISC Manual as established in Section 3.9.2.2.4.1 of the FSAR. i The support designs cre censidered adequate to resist the stated t design loads. i i i .k i ~. +.. c

D.C. No. E00b ?A his b Of HVAC DUCTWORK SUPPORTS CALCULATION REFERENCES Ref. No. TITLE 1 Design of Welded Structures, Blodgett-1972. 2 Manual of Steel Construction - AISC, Seventh Edition-1970, or 8th Edition as noted. 3 S6W Paper, EMTR-612, Design and Analysis of Base Plates. 4 S&L Report SL-2682, Seismic Analysis of the Reactor-Auxiliary Building Complex. 5 EF2-46,027 - Allowable Load for Phillips Flush Anchors. 6 Design Calculation 2935 , Design Methods - Standard Ductwork Supports. 7 Mechanical Engineering Design - Shigley, Second Edition. 8 Supplement No. 3 to the Specification for the Design, Fabrication & Erection of Structural Steel for Buildings - AISC, June 12, 1974. 9 EF2-19,726 - Load Carrying Capability Derating of Continuous (Gateway) Inserts. 10 ITT Phillips Drill Division - Spacing, Edge and End Distance Recommendations - Red Head Engineering Bulletin, 7/17/73. 11 Red Head Engineering Report No. 1372 - Minimum Embedment Depth. 12 Edison Specification 3071-226, Rev. D - Purchase & Installation of Concrete Anchors. 13 Formulas for Stress and Strain, Roark, Fourth Edition. I

1 D.C. No. 2 80$o fA 6s k of $ GENERAL NOMENCLATURE Term = Definition and Units a Acceleration (g) i i 2 A Cross Sectional Area of One Anchor Bolt (in ) 2 A, Total Area of Anchor Bolts in Tension (in ) B Length of Plate, (in) C Total Compressive Force in Concrete (Ib) e D Length of Base Plate (in) l d Distance from Extreme Concrete Compression Fiber to the Centroid j of the AnchorBolts in Tension, Diameter of Drilled Hole, (in) 6 E, Modulus of Elasticity of Steel (29 x 10 p, g). 6 E M d lus f Elasticity of Concrete (3.0 x 10 p,g) c Direct Force Eccentricity, (in) e fa Computed Axial Stress (psi) F, Axial Stress Allowed (psi) F Bending Stress Allowed (psi) b F Allowable Tensile Stress (psi) g F Allowable Shear Stress (psi) y L F Specified Minimum Yield Stress (psi) [ Y r FX,FY...MZ Forces and Moments Applied to the Base Plate and Reacted by I the Concrete and Anchor Bolts, Ib and in-lb. j j freq. Frequency (hz.) i I Moment.of Inertia of Section (in ) -l K Effective Length Factor K Fatigue Stress Concentration Factor j g L Span Length (ft) i M Moment (in-lb). i 1 g 3 j

D.C. No. 2806 ?A 6E S~ o f N GENERAL NOMENCLATURE (cont'd.) Term Definition and Units P Concentrated Load (1b) i R Reaction Applied to Beam (Ib) S Section Modulus (in ) S, Section Modulus of Weld Treated as a Line (Blodgett, page 7.4-7) T Anchor Bolt Tension i V, Shear Load at Weld Location V Shear Load (1b) W Width of Plate / C Distance from N.A. to the Point at which Stress is Desired (in) 1 d Nominal Bolt Diameter (in) I f Allowable Force on Fillet Weld (1b/in) f Force on Weld Due to Uniform Distribution of Load over Total I Weld Length (Ib/in) f Vertical Force on a Weld at a Specified Location Due to Moment (Ib/in) 2 f Horizontal Force on a Weld at a Specified Location Due to a Moment (Ib/in: 3 f Computed Bending Stress (psi) b f Compressive Stress in Concrete (psi) fI Compressive Strength of Concrete (psi = 3000) f Actual Bearing Pressure p f Computed Tensile Stress (psi) g f Computed Shear Stress (psi) l y k Distance from Extreme Concrete Compressive Fiber Stress to the Nuetral d Axis Location of the Base Plate, (in) I i 1 Length of Each Weld (in) Length of Vertical Weld (in) N Total Number of Anchor Bolts N Number of Fasteners in Tension g i

D.C. No. 7, dSO 6, F%s se 6 or 17:33 CENERAL NOMENCLATURE (cont'd.) Term Definition and Units n Ratio of Es/Ec - 9 r, Least Radius of Gyration with Respect to the Principal Axis (in) T, Total Tensile Force in Anchor Bolts, (Ib) t Thickness of Plate (in) p X, Y, Z Coordinate Axis 21 Perpendicular Deflection (in) O Leg Size of Fillet Weld (in) T Allowable Shear Stress on Throat of Weld (psi) l I 1

D.C. No. 2fCh Date 7 20-N Fermi 2 Power Plant Page

7 o f M

Subject:

Qualification for QAI Duct Supports in Stress Report No. 2 6 Y 7 f Computed By C. I. G//UA #G Checked By R. f. #A -7E (., SUPPORT INDEX Latest Su Design is: /pport Hanger Mark No. Type

Rev.

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D.C. No. $$d3Oba Page $.0 CF b-Part II - Bounded Support Load Assessment The structural calculation for supports within this calculation have been performed based on the design load determined within Part I of this design calculation. This load is based on calculation methods established in reference Design Calculation 2935 utilizing OBE and DBE spectra data. Subsequently, a duct capability evaluation was made by the Engineering consulting firm of Hopper & Associates. This analysis was necessary to assure the integrity of the ductwork itself, and was based on the site specific earthquake data. This duct assessment yielded bounded support loads based on duct size and support stiffness. Pertinent data from the analysis can be found attached to this design calculation. This part of the calculation is an evaluation of the subject duct sup-ports for the bounded load established by Hopper & Associates. The table found on the next page compares the design load used within the structural calculation and the bounded load. Conclusions relative to the adequacy of the support based on support member and weld stresses and anchor systems are stated in the table. OBE allowable stresses and allowable anchor bolt pullout have been maintained unless otherwise noted. Calculations required to substantiate these conclusions are referenced in the comment section of the table. For vertical system frequencies determined to be greater than or equal to 33 Hz, the ver-tical duct loading is the same as the values calculated within Part I. t h e

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O ACTIVE UNITS INCH LS DEG. F&MR SEC LeM O 'O ; INTERNAL MEMBER RESULTS O -= e y g MEMBER MAEIMun STRESS ---/ O STRESS - - -- ------=-_ f------- MEMBER MAN NORMAL AT SECTION LDAS MIM NORMAL AT SECTION LOAD gp 1 0.178972E*05 0.0 FR 2 .329477E*05 0.0 FR 2 0 2 0.571042E*05 0.0 FR 2 .ee4134Ee05 0.0 FR 2 3 0.214887E+05 1.000 FR 2 .248838E*05 1.000 FR 2 g 4 0.134940E*05 1.000 FR 2 .145072E*05 1.000 FR 2 I O 5 0.13679&E*05 0.0 FR 2 .148259E*05 0.0 .FR 2 r .I e 0.124442E*05 1.000 FR 2 .118311E*05 1.000 FR 2 gp 7 0.585450E*05 0.0 FR. 2 .551499E*03' O.0 FR 2 O 8 0.180821E*05 1.000 FR 2 .877289E*04 1.000 FR 2 9 0.724049E*05 1.000 FR 2 .573343E*05 1.000 FR 2 (p 10 0.450987E*05 0.0 FR 2 .443480E*05 0.0 FR 2 0 11 0.684125E*05 0.0 FR 2 .738401E*05 0.0 FR 2 12 0.712064E*05" 1.000 FR 2 .46022eE+05 1.000 FR 2 O Past - g O LIST FORCE REACTION ALL O PAGE - to 9 g O eseeeeeeeeeeeeeeeeeeeeeeeeen g mRESULTS OF LATEST ANALYSE $e g seeeeeeeeeeeeeeeeeeeeeeeeees O g PRotLEM - STIFFNES TITLE - MVAC SUPPORT en-2850-H-31 O ACTIVE UNITS INCH LS DEC. FAHR SEC LEM I g l LOAD 1NG - 1 O v MEMBER FORCES LOADING - 1 9f O

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4 g

MEMDER FORCE 8 LOASING - 1 8 - = ---- F O R C E - - - - - ---- --- --//- ---=-- MOMENT -~ --~~-~~--/ MEMBER JOINT - /- AxleL 8 HEAR Y 8 HEAR 2 TOR 810NAL SENSING Y DENDING 2 O 12 2 0.9627458 -0.5741635 -0.5474190 -0.243543 -5.2703448 5.0244983 G G SUPPORT JOINT RE4: TION LOADS LOABIMG - 8 O JOINT /-- - - - - - - - FORCE

//--------

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0.0 23351

499.528074 -0.1129905 4.8309488 0.0837718 0.4839281 10 CLP'4AL -0.0233511 500.471480 0.1429905 1.7748841 0.2431437 -0.4839281 9 S LOAF 4NG - 2 O 9 unsER FcaCES LOAs NG - 2 g g MEMBER JOINT /- - - ----- ------ FORCE --------------------//- - =------ MOMENT - - --- - ---- - ---/ AMIAL SHEAR V 8 HEAR 2 TOR 8IONAL SENDING V SENSING 2 g I 1 1 7068.08984 -124.575845 110.541752 54.4354964 -3064.40374 -3119.49219 1 2 -7068.08984 124.575145 -110.541752 -54.4354944 -1651.95947 -280.202437 2 2 4346.03514 -455.785645 422.502197 227.606552 -8967.15425 -10033.2447 O, g I 2 3 -4344.03516 455.785645 -422.502197 -227.604552 -8879.98437 -87e8.10937 O lt 3 3 1592.30835 -132.877594 129.539658 15.7872247 -2127.34717 -1955.8496 h 3 4 -1592.30835 132.877594 -129.539458 -15.7872267 -3400.11206 -3714.03906 j 4 4 381.353027 -377.112549 383.220215 -40.1948700 -8748.87207 -1534.93188 g 4 5 -381.353027 377.112549 -383.220215 40.1948700 -2083.33130 -2234.19434 Og I 5 5 537.634475 -2ee.403271 -272.711426 106.675459 2187.18530 -2130.34033 e 5 4 -537.634475 266.403271 272.731426 -106.475659 1630.77444 -1402.10791 [ le 23.559 -20.2699585 iS41.01001 1491.87280 t -23. 55,1734 20,.24995,85 - 1,7 7, 6,. 6 0,.18,.1 -1,8,8.54346 9 a 6 -388.353027 -29.ee70532 --.1736 --- -.70532 29.e4. -- 7 381.253027 1.4 7.,4

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FORCE - -

//------- -

M O M E NT -------------------/

O I G AX1AL SHEAR 1 SHEAR I' TORSI,0NAL BENDING'T BENSING 2 6 12 9 -2438.21631 991.559082 974.289795 -30.5180444 -9018.20312 8971.01953 O 12 2 2438.21631 -991.559002 -974.289795 30.5180444 -10271.7422 10440.8398 O e G SUPPORY JOINT REACTION LOADS LOADING - 2 g JOINT /-----*- -== *---- FORCE ---------~~--------//-----***----*- MO M E N T --~~~~---------*- # 3 x FORCE Y FORCE 2 FORCE M M0 MENT Y MONENT I M0 MENT g 1 GLOSAL -11.3231621 -7048.08984 147.481137 -5787.02734 -54.6354944

1453.02444 4D 10 GLOBAL 11.3231421 7068.08984 832.318848

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PAGE -

10 4 N \\ O '% O EXECUTE PROGRAM,*000LOBAL' q g V STRUDL ME99 AGE - MEMBER FORCES AND MOMENTS HAVE BEEN ROTATED TO THE OLODAL COURDINATE s BYSTEM FORALL ACTIVE MEMDERS AND LOAD 9. y 4 w a .f LIST FORCE REACTIDM PAGE - 11 M e e. m .,e.- ,n --e-m a-

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$80es000$$t9900000000000000s SRESULTS OF LATEST ANALYSESe secessettoestesesseesteetess PRODLEM - 2950-H-0 TITLE - NOME DIVEN ACTIVE UM1TS INCH LB DEO. FAHR BEC LBM o ~' ,5 MEMBER FORCES FORCES // ---MOMEN19 -/ MEMPER LOAD 1NO J01NT /==- AX14L SHEAR Y SHEAR Z TORSION MOMENT Y MOMENT 2 1 492.954249, 0.2695790 14.4592977 3 1 0.0401611 143.963373 -99.9939270 2 -0.0401764 -141.232193 99.0614166 210 339035 -0 2695790 -14 1770325 2 3 2 1.0176949 64.4114075 -51.7707672 227.912190 4.0769939 11 5396118 .3 -1.0176949 -42.6525979 49.0100555 276.092041 -6.0769939 -1 3629082 3 3 3 1.0174949 47.6525574 -49.0100709 -276.092041 4.0770111 1 3629235 4 -1 0176949 -43.1419679 45.6972046 -268.675293 6 1351624 -1 3629235 4 3 4 1.0176697 29.1419993 47 3027344 269.675293 -4 1351595 1 3429397 5 -1.0176949 -24.3931635 -50.0634413 219 155939 6 1351595 -11 5396271 5 l 3 5 0.0401411 94.6933594 100.095679 214.478409 -0.2124735 14.1770172 4 -0 0401459 -92.0621796 -102 019173 492.994766, 0.2124735 -14.4592925 6 3 5 0.9775239 -70 3101349 42.9777679 -432.633799 -S.9224379 -2.4374023 2 -0.9775239 74.9207245 -46 2906342 -439.150435 -5 9073120 2.4374025 ~ (j) Q Q ~ PAGE - 12 1 Jo O - t -4 lg l 1 Z P 0 SUPPORT J01NT REACTION LOAD 9 Q // MOMENT 9- -/ X FORCE Y FORCE Z FORCE X MOMENT T MOMENT Z NOMENT I g J01NT LOA 81NO /--- FORCES ~ ~ - - N D s O c-e 1 SLOoAL 3 0.0401709 143.963373 -99.9939423 492 954492 0 2495790 14.4592174 11 @ g e GLODAL \\ 3 -0.0401709 -92.0421794

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I l PAGE - 12 ^ ^ MEMBER FORCES MEMPER LOADINO JOINT /= FORCES // MOMENT 9------ -/ ^ AXIAL SHEAR Y SMEAR Z TORSION MOMENT Y MOMENT-Z 10 1 9622294 999.129639 119.541325 -1995 05542 -16.5160990 179.745341 g

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FAGE - 4 PEFORE RESEQUENCING NAx! MUM DANDWIDTH EDUALS 5 JOINTS PROFILE EDUALS 12 JOINTS ORIGINAL JOINT SEQUENCE ( FREE AND RELEASED JOINTS ) 2 3 4 5 6 PAGE - 5 AFTER RESE00ENCING MAXIMUM BANDWIDTH EDUALS 3 JOINTS PROFILE EDUALS 12 JOINTS JOINT ORDER AFTER RESEQUENCING ( FREE AND RELEASED JOINTS 1 2 e 3 5 4 PAGE - 4 LOAD LIST 3 4 OUT DY MEMBER LIST FORCE MEM 1 e B dd PAGE - 7 A JT1 Z t - o hl .g% Nw 4 o tRESULTS OF LATEST ANALYSES.e$ ,1I h sessettstesseepsestes****s L I, PROBLEM - 6M-2049-TITLE - MONE OIVEN a i b. ACTIVE UNITS INCH LB DEO. FAHR SEC LBM g 4

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NEMPER FORCES MEMPER LOADING JOINT /

FORCES----

//-

- -- MDME N T S ---------- -- - - ------ / AX1AL SHEAR Y SHEAR Z TORSION MOMENT Y MOMENT Z 1 3 1 -520.412354 -7.9913375 3 0755001 -3 4479971 -57.3129662 -189.665604 2 515.004766 23.2799693 19.6260034 3.4479971 306.122070 -311.515137 6 1 10.2955704 -9.1121157 2 0002317 -3.6771400 -41.2097779 -209.327699 2 -5.7679992 24.4107513 19.6213531 3.6771400 321.067676 -327.030006 6 ~ 3 6 -1047.96572 -17.6307220 -6.9107914 0.4995540 293.961094 -200.323792 7 1052.39331 39.3323212 22 2094269 -0.4995540 172.062103 -703 095449 6 6 -525.732422 -16.5941370 -6.0007734 0.2991624 290.299316 -193.230545 7 521.204034 30 2957209 21 2994000 -0 2991624 156.503464 -694.697256 9 3 5 1457.14160 13.6929196 12 7256460 -1.6624346 -168.019272 241.165344 9 -1491.49169 15.9149706 6 5951233 1 6624346 11.9616952 -295.196523 220.432175 4 5 1956.77002 10.5425673 9.5764799 -1.6910297 -149.014713, -251.471603' 9 -1491 29712 11 7619209 2 5409622 1 6918297 -29.2800903 s PAGE - 9 LIST MAX STRESS ALL SEC FR NS 2 0. 1. PAGE - 9 e3 t) seestesseestesseestessetteet eRESULTS OF LATEST ANALYSESe esseeeeeeeeeeeeeeeeeeeeeeeet .I PR09LEM - 6M-2949-TITLE - MONE 01VEN ACTIVE IMITS INCH LB DCO. FAHR SEC LDM V) O Q I>O d ~4FI Z O ')D), INTERMAL MEMKR RESULTS 4 a mN -~ I 4 O> s nN g MENKR MAXIMUM STRESS / STRESS - / MEMBER MAX NORMAL AT SECTION LOAD MIN WORMAL AT SECTION LOAD 'g 1

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PAGE - 10 EXECUTE PROGRAM '0GGLOPAL* ^ ~ STRUDL MESSADE - MEMDER FORCES AND NOMENTS HAVE BEEN ROTATED TC THE CLOBAL C00RDINATE SYSTEM FORALL ACTIVE MEMPERS AND LDADS. LIST FORCE REACTION PAGE - 11 setettetsteststeset**ttetste 9RESULTS OF LATEST ANALYSES $ 3 $$$tetts****S$$$$$$$$$ststet 3 PROPLEM - 6M-2949-TITLE - NONE O!VEN ACTIVE UNITS INCH LB DEO. FAHR SEC LBM MEMBER FORCES MEMPER LOADING JOINT / -FORCES -//J------- ---MOMENTS / AXIAL SHEAR Y SHEAR Z 70RS10N MOMENT Y MOMENT 2 / I 1 1 3 1 -7.9103699 -3.4699436 -520.412354 92.9903359 -173.933029 -3 4479971 l 2 3 2900001 29.6320343 515.904766 436.735352 -3 9135601 3.4479971 l 6 1 -7.9141046 -4.9722910 10.2955704 110.077274 -177 154738 -3.6771499 J l 2 3.3046139 31 1353912 -5.7679992 458.845459 -3 6561279 3.6771489 gg I# 3 2 -1 2119141 166.192932 -454.611572 -1350.02715 6.0279320 20.4411163_ _s d 3 -1.3349541 -151.476101 452.064697 -1500.19434 -4.9213n67 -20.4411163 2 a 2 -1.2249290 166.067591 63.0231629 -1352.95605 5.9757324 20.512:070 9 3 -1 3218231 -151.350815 -6Q.4763947 -1503.B0933 -5 0041504 -20.5122070 J 3 3 1.3340541 151.476212 -197.065040 1500.19430 4.9211397 20.4409190 Dh y I 4 -3.0016:23 -136.759460 194.519200 2016.0549.1 -4.9211397 26.5073242 s ( g l 6 3 1 3210231 151.350061 -194.523544 1503.00900 5.0039663 20.5122070 O~- t 4 -3.0605760 -136.634109 197.070312 2020.53491 -3 0039663 26.2011719 qg 4 J q 3 4 3.0816223 -336.240479 60.4816509 -2016.05519 4.9211426 -26.5072021 S -3.9624420 347.606760 -62.4624796 -2771.43604 -73 1293945 26.5072021 h l' '4 3.0605760 -336 365723 -452.070069 -2020.53491 5.0039062 -26.2012377 5 -5.0493005 347.012012 454.051025 -2760.71069 -73.0295410 26.2012177 5 g 3 5 6 5466309 669.450252 1106.02637 2432.09063 35 3000594 8.8903360 a 6 -7.1123047 -666.107744 -110%.59229 109.194672 -62 69n2269 -0.R903360 6 5 6.532714n 672 219402 506.100099 2506.90649 36.5249023 7.9112244 6 -7.0906329 -669.949463 -505.534100 175.432663 -63 7966050 -7.9112244 A 1 l l

PADE - 12 MEMPER FORCES MEMBER LOADING J01MT / -FORCES-- - --//---- -MOMENTS / Alt!AL SHEAR Y SHEAR Z TORSION MOMENT Y MOMENT 2 3 6 7 5001392 -17.3534546 1047.96572 -355 099145 60.4939325 -0.4995540 7 -12.1077175 43.5165710 -1052.39331 -619.922510 -375.490234 0.4995540 4 6 7.4935711 -15.9699402 525.732422 -334.935937 41 5669499 -0.2991624 7 -12.0111313 42.1330261 -521 204034 -594.011279 -373 492179 0.2991624 7 3 4 -0.4670650 210.541794 59.7263499 165.903939 2 2140627 9 3999926 2 -2.0799079 -195.925027 ~61.2731019 914.091309 -2 2140627 -23.9993602 '4 6 -0.3951013 211.919795 59.9019104 159.403595 2.2196274 9.2003794 2 -2.1616669 -197.203019 -37.2551575 994.110107 -2 2196274 -24 1992090 g n 3 5 -0.6930999 -1017.14502 -1043.54349 299.337159 37.7495909 -35.3975525 9 -4.5194244 1050.77051 1034.36035 -217.194509 -142.797949 140.436905 4 5 -0.6931303 -1020.03199 -1040.15112 241.903955 36 5050659 -34.1124725 8 -e.5202036 1081 65723 1047 35449 -157.113069 -141 572144 139 179535 9 SUPPORT JOINT REACTION LOADS / JOINT LOAD 1M9 /- FORCES

//- -

MOMENTS----+

=/ X FORCE Y FORCE Z FORCE X MOMENT T NOMENT - Z MOMENT (* 1 OLOBAL 3 -7.9193719 -3.4699436 -520.412354 92.9903711 -173.933014 -3.4479971 6 -7.9141945 -4.9722919 10.2955704 119.977274 -177.154709 -3.67714B9 7 OLOBAL -1052.39331 -619.922517 -375 490234 0.4995540 3 -12.1077347 43.5165963 6 -12,0111523 42.1330414 -521.204934 -594.911523 -373.492422 0.2991624 8 GLOBAL 3 -4 5194349 1059.77075 1034.3&O40 -217.196707 -142.799071 140.437042 6 -e.5202036 1061.65771 1047.35474 -157 113251 e141.572250 139 179657 / PAGE - 13

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._~ i D.C. Ms. Q2:cGo f Page No. bb af )) l e PART IV l ANCHOR BOLT ASSESSMENT AS-BUILT RECONCILIATION o r This section of the calculation addresses noted deficiencies in i the anchor system installation; see Non-Conformance Report 84-1606. i The following table identifies the supports affected, change documents, duct loading and reference derivation, and the anchor bolt margin of safety. The stated loading is the maximumL of the OBE or DBE load case. The allowable for the anchor bolts is limited to 25% of the avdrage ultimate espacities as determined by Pittsburgh Testing Laboratories as published in the Phillips Drill [ Company Catalog F-1000. I As an aid in determining the effect of misplacing the support attachment from the base plate mid point a study has been per-formed by Hopper & Associates. The resulta noted in correspondence BA-10/84-347 dated 10/4/84 state a maximum bolt load amplification [ of 4.5 and plate bending stress amplification of 1.1 due to support member ~ eccentricity. This study assumes that a standard base plate ( and bolting system has been used as well as a standard member size. Cases which cannot meet this 4.5 criteria or are odd cases have been justified by a specific calculation. This calculation can be found within this section, see the table for the specific page.

PART IV - ANCHOR BOLT ASSESSMENT TABLE

EN Duct Duct Loading Load As-Built Anchor Bolt dk i

Sup ort h.k 88 F (Lbs.) M (In.-Lbs.) Ref. See Change Margin * @ Calc. Cosaients i g, y,, Height Fx/Mx Fy/My Fz/Mz Legend Notice Ref. Load Fage # o - q P. O. >>an = 'Jo *1 '% < N E u 2o s d si toxico %6 1(o6 A Ben os54 4 i 344* = Auoo. cw- ? :: A 46m-cuer4 S, J S %$QQL ud649445 itox t'J. IS2 c: A 6 coM4649 4 44 Itaxt2 I62. 596 A 4EM-Oss7 9.6 (o c,M 2849 4 4s leo as 12. I 3 '2-S96 A '1BN 055+ e:> 7 5 % A T ia % ceo I wnb49 4 A1 sto x i?. Ib2 s96 A nm oxs+ 5.j b ocr u c4ea A m G ii'

34 l(o b A

A7N-055V l3 ~) ii! 'm N tS50 4 9 tox6 P4 O A 68V0s#4 7 $'EIMS$ F' W 1650-411 LOX (o 1"l 1 coo n a tb'L (o O b ABN0354-b y l k'j' y G y Y A tb50-4 % l1

b

[ GH-2650 4 Tl 118 8 ISS (o o b BBM-4559 S,o) olTro (4m 4 %) { j p h a. n M 2850 5 30 11x6 13 3 (o o D //BM-#554-8,10 onto (We W 2G) = w W 1650-d bl 1186 8,10 Dirro(We 4 10) II 1S4 '(o O D //dh 055f-9N* i 2

: 7

% = b 3 (P N O h n I i A o a' e h ,D E t i' <k

Anchor bolt margins assuming plate attachment @ baseplate ( is allowable bolt pull-out/ actual calc. value.

h

Forni 2 Fowsr F1cnt D.C. N >. 7 6 0 45 A D2to to '5c>- 8 4 F:s2 bd # U

Subject:

_ Qualification for QAI Duct Supports in Stress Report No. 'Z. 6 48). ] t FART IV I ANCHOR BOLT ASSESSMENT AS-BUILT RECONCILIATION i ASSESSMENT TABLE LEGEND FCR LOAD DERIVATION REFERENCES i t Designation Description l ) A Feak bounded lateral support loads by Hopper & Associates per HA-10/84-351. B Reduced bounded lateral support loads by Hopper & Associates. C Specific anchor loads supplied by Hopper & Associates due f to duct system flexibility. ( ~ D-H Dynamic analysis results supplied by Hopper & Associates. D-D , Dynamic analysis results by Edison. f E Fluor loads modified by a system frequency factor - Maximums of OBE/DBE load case. F Fluor analysis loads used directly for OBE load case and modified to DBE case @ ZFA. t G Static analysis by Edison at system frequencies derived by computer analysis. E i I

oc de- ?.6oe A to '2.9 84 E.FE?vA1 E (ksE % og 75 Adc M6 bolt ASSEssu sr4T Ch @cd eLTeh R. S. Purc L Mt->A M-51 occ7 LDb 05Eo tW coM FoTEh Ard AL.YSIS - PA AT E : t. F = 8460 Fs= blo* y bocWDEo Doc T LOS A F7 E : F = 29b N i F, = l co b

y co815EF,VATIVE LY PAoP, ATE 6 ALE R. P,5 ACTierdS 6Y A

FecTo h oP (796 /9 4,) =. b 4 C6 tTic A L. 6ASE R 6EAGTioWS - PsoA ATEC - AF15 ' 4 F.

105 5'/ 64 )

b8 5 D r 52c/'f JT 7, LDc, 5 k= (o 19 ( V >' = 3 9 u f ) = b l (o " T i .A, L / +g= cd /.e2S" = >.6 >8 2 c =g.-<>--- c ,w i G q' E HTh. c, .. L. P. = l. S (54 1PLIF IED McMoD ) = P'o4 1

e _,#

U ~ ~ ~ ~ Foh *b" P4tLLIF5 ArJcM AS OSED'- ~ l'

3" Rc. Actoc = 1 S44 gg

. b' (@ JT.7 ) ___ _ F.o._ ASS + g,3)+y3)ble 3764 S20 sm 4 EFF. MAX R C). D'lO [ I, b) = SG7 154M,*. C)h Mcdos co. T eo. e onJ 6 use e5, ' A' 4 'c.' e Ju I 6 6 E f1ESPECTivELY A6E LESS Nr4 @ f:ASE Ft 'Ed, JT.7 6Y IN'5fECT-tord oF AS-boiLT5 d ST60DL. o L>T pot. l

o c. ed 2. 7. S o e A 10 10).84 a Feh Al H PL, H oF 73 AtJcdon e:ot T ASSE55u EdT A5A b lEL.T % RA.MTEb F4c,h A 4 2, Ab i 4b n4sse >Jc>AS AAs toEtJTical. 9/ 3 Is. s e < e s o orJ o s. o L os,. ords Ardat.vs ts alt L cousA T>Ise alt. boodoEO ocx T LoS A AE: Fx = l b 2.bi F = 59b

y occ.T L.oS o s so ar4 c.ou P. AW AL.. - fb67 E - ML0.6 51 A6E' Y

F = 94c/ 4 F,g.= Sto y cow 5 E6vATivE LY' FAo AATE 6ASE R_ 6E ACTio45 6Y P FAc.To6 oF ( 5% /9 4 La ) =.co b '2. c6TicAL BASE R. 6E ACTier45 - PAomATso - A hs.: P, = to sB(.c,32 3 = eee * )= 2 5 6" + J T. 7,, LCr.o 3 4= Sw( ) = b => \\ " h m,= st9 ( acne: c,w as eoiuvs ros e.1c'(ears)asne Nioso FoA MESE bh5 30dlCd P(M MAD 4 g's 4/td dE bolt ibTrkhd. DOE To IM ACCE55Abit. TTY Wo AS 60tL"C wese woeo sx e.> wiVcsaTs to msfECTiVELY)/.ME P.o, AMAt.ysts IS bAMC l OA de ATIKE>AEh oF% To 4.oF ff. PER 09. WETCdE%. of 4 3 " + rMass (m = 1s AA% bxse n. s"<5"nc" s 5 = + ( 2 bb + 3871 ) S

'D 1 4 t.1/te=.ffs= b 4 66-Max Po,

4 gg y ...L.F.= 1,o A1T O uawa = (S4 4 /'2. ll = 5,7 > 4. .,OK 48 Adcdos dour

Ct IdGL 2.8 o(o d t o 2.0) b 4 F FEhM \\ 1T. Pe to8 0F

E ArJcdon e= c.r ASSE.S$ ugd T oc h Sed eers.h R.s.eere.A d L,h d 44 d

bo0MDED DOCT LDb ,e F = 6 >bE 4 f-i = 1 b 2.8 1 _ c,e4 7 co BEAcricWS @ JTl 5 1" 16' tod IN LIEO oF STA.) o - i Adat.Y$15; OSE WE py ,w S::o* bco* Fattooisit uoo E L. 1 To DEustoF JT l me xTioWS 5 h= ee4 sw 754 w % ec-wsw) u = 'xo(z Xio) 66+ 20) = 5 ISO $N5 _ Ul r 2.(2ot sm bscis [E.ZU, au" i e ^ n oinow y

i4 Ro.= [ +

= gg4 4 5 uA >t 3 '><o D/<Fl6 # b

- LF* !* O (SIMPL1FIED HETMoo)

EM T8bi L/*t # 2 P6 4 hEACTioWS @ JT. b i h = 60 sw M= S co"* 4 Ro. = Y + % = 1564 c6 mat g o, Max ut.t.o.a. e.o. ( s ' + nacdas) = 1 s 4 4 0 e A4c4# eat.T u+neid = i S44 / 156 = o).6 > 4 eud. 4 g c3 is <diW eocr earrena eos mJis re ..on 4 6

O c rd e 7. b o ro A to - 2.9 b4 E FEhMI E. Pa se 69or 73 Ark. dom bot.T A55s55usr4T Ch $cMELTEh R - S - P AT U.. IMCoh N-9 00CT Los osso i9 coMPoTEh Ar4 ALY SIS - PAhT E F : So* 6 P.g = 18e8 y l D o vedo E D D0C.T LDS

F=

34 E F, = l (o6 - E y Gord5EhvATiv e tY. 05s t4od pac:> HATED DASE fE. 6 E - ACTiordS F = 14 4 E M x = 46 5'* H = 14"* - JT.1 (c A men t.) y g lM Asc + n A = ile + L /+.g= b/ss=6.'. LF = l wax Fo.=. 4 sc3) + t ALloc Po. ( b"& Adcdoec) = IS44 E i A Wcelon bour Maat,tra = 15244 = 15 7 4 t ..Oh Appsce j ,,q

6 Oco n N - 1').

pao-hATeo 6 Ass ft. hs Ac.Tiot45 To. 6EFLECT bourJOED LD5 AhE -PEh b 19 CALCS "- P= 17 4 4 4 84 t= lo '2.co *

y Ro. allee (Foh '
-

--4>-- Lz / t g = 7,5 / G Z 5 = l '2. .- L P = 1. 5 L_A e l'2 " J '1' Ma P.o,= 174 /'2. + lo 2(o /4.S = SIS 4 EFF.' M Ax P.O. = 315(l,S) = 47 2.5 < '2.61 ..oh uggg',,$ F;W g, ^

oc do 2boe, A so. 2nb4 e FEhui E. P6 '2D op '/.3 A WcJo n eau.T Assessusa r oh fedeuveh R.s.eArct i dt,h d '2. ro,1 1, So 6 Sl occr Los oseD IW Cou PoTEh ANALYS]S - PAAT E E l'y = l lo F, = (oro d i hE FINED booMDED LOAD PEh MoPPEh 6 assoc, exI 4 7 i Fy=lbA4 6 P =.<o(tooN)= took %1 g t TdESE VALoEs AS E APPhak.. EctOn t. 4 SidcE A dohlt. ML,b iWEhTIA LOAD toAS iMPoTTED 4W THE ST600L Rod i I TdE 6ASE it., AEACTioWS SWootD ACTO ALLY BE SLic::>dTLY dord5ERVAT1VE 714EhE FohE 05E TN E. 6 ASE ft. h E AC.TioWS Phovtoso oW P6 4ci oF PA6T E. l AWcdos eo. = Sa 2.4 (Pt, w ce PAAT m.) AMcdca bou-r ua66tW = 1544/58,2.

2.,(o b codsAs Attoo P.o, FoA A. g'96 ArdcdoA : 1544k de,h d -2(o it.As DOitT AdaL.Y5tS (beso a 4 c.g.)

N o srd !? ~ T= 'k =. l') l 8= =,54S l heob A. 6. A.MPLIFlcATiod t-f. <. 7.. to 5 /. o h i .8 42 soot 14 ft. - Y = 992. =. b x = 1 =. 4 21 Arrac4 2.

b Pe.so A.D. AMPLIFicATiod t

2. l 4. 1. (o S.. o h 61

{ i Mc h M-27 ft.AS botLT AWALYstS Wasn4 e: Y = S BS =.8c) x = $6=.62e l l 65C D A, b. AMPLIFlcATioW t 'l. 6 > 2,(o S .*. W. L,. i l t

D C. rdo 2.606 A 11-1 5 - 8 4 5 FEhMI E S rne 7I of 73 Adcdo6 A5tessueWT Ch ScdE LTE h R.5 P ArE.t M6h M 26, 7.~7, do 4 S } (cod T.)

1. C.53

.76S_ 'dA scand E : Y=2 .85 x= = 1 P,asa A.b. e M PttFic ATio W 't 7. 6 ') 2. 6 5 . W.6. er iw sPecTiW6 As-bOi tT5., e_ ' A' APFeAns Tc) Eb e. c AiTic e t. 4 o t. t be AW e, t i seo Foh ACTOF_ P. O. PEfm A b - BOI LT D 1Mb. Il' of 4 . 50) '), 4 l$% E b 4

2. e-ne wi

>y' y 4 l.b'o' + S. 2 + e 4 p.oF bout _i bA'os E AE NTio45 F=6664 W = 196.5* M = 1 19 8 y g cr-se I - A.e.'l' het:575 ALL oF Mg L. !t : 2.IS 379:~).6<Ot.LF=l 2 P - 800 (I-IP 1R.f5N<lS4M..oh g,0, = hk+4,d 2.,, + IDSI ( 7.7 6 ) + 1 (1. 6 1 $) = gg i c ASE E - 6.b. '1' 4 ' b' e>EttSTS 4 L./tL: 5.16/375 =b.(/7)bt.LF=l.5 i t 00D b R#S M14 -t =- P.o. = k nick + 2('s.23) 20.cou e2 i A 2 er go. = sn (i.e) = es v < ie w..on

DG de 2600 A 1 0 0 *; o b4 E FEhMI I. P4 m 7 2,:gy 73. l AMCdoh tbtT A SSES$MEWT' Oh idELTEh R. S. P ATE L. idcoh d - 2.(o, 2. 7, bo 4. S 1 Cot 4T' Id t, P, d - bo FE. A 5 bon LT A r4 ALY Slb SitJ45 bot 1J I* W ave nde L2.x2.xQ MeMSEA f VIATo* LLY CEtJ7E6eo ord ME 6ASE ft. ME A 6. ATracd A MFt. I Flc ATaos! < 2. to 5 6Y i r45P E cT to M. . o h 46 Pt, 2 dt,h id -b l FE. A5' B olLT ArJALY6tb i r WohTd D Y= " 19e x = kDD =.2(47 heQt) A. 6, AMPLIFicATiod

2.0

< '2..co b ..c> h sound it.: Y: 1.59 2.=,'796 ,o92. =,oS 1 > <. = 7, i .. oh hEQD A, 6. A M PLlFicpTioW e 2.2.4.

2. e 5 h

i i i

D.6. 2 & c 6 10 8 4-Feami 2 Pount /21sr % Tb e 7.3 G%uncwon ;& Q4.I Dxr Svers. InSker&n zm l Soens-reo-r

n. s. es,et I

ATT AC HMsWT Lis T I. FLO OR'4 S TI= E S 5 R e f o R. T 2-4%ETdHLS OF dhtdfj&R.. e V pc f d o. T 4 t o 2 - M o I 4. PGR de. bl6 R&V & t 77 C f tj o. T 4to ?- M o Z im NOPPGK bovNO6O lcAo5 lLe r-re12 lc,as e H 7. McFFEh BE F1WE D E:o0N DE D LOADS / LETT6 h O-I-!oPPEh Adcdoh bot.T LOAD AMPLIFlGATiord d FAc.Toh cde, AT / LET766

9. As Satur, Asm-oss 4 Res4 i

i 1 l l ,,.s.a.a...

.,m.m,,3 ""-".a-_, ---_.m,, m 3 h $ ~- .. _[;f -{. .= e xmn.. a,.3'.'I& ~, i d;ts. $..

x..

' - <f ..'p. ~~

4.,.

s. 1,3 m

-(w. 5..,,,..

,W, s,9./r. 2 . r '. -~ i pl'f l l %-i'j:Q ,.. V Q N. g " u Y Z' bl ~*2/J f i 4,- f.. %b - t'. k

A ADA..

Yh ? Q g 'f.' -24' '.l-

' l 3

^-* v 4 '*w& 4 g ..,.9-.- sy. ,h,s.. '.,C% j' ) v ec + p, y. e, $m.>: %,.,y&i *./ u_.. al.,?V,'y~ . J IIi 7) 5@ is;y.;%_ 9 1, ,_ g m 3 .) y ~- - ..\\ A m, e $5 e :j$5.J (m,. g

$ e f+

.i, . ~.. s ) y t j f:..t .s k"' el ~ x D.,\\. g - g.I i 3 f,. T g,. 9 =...... - = .3 h ~ g acemamy. k [= #'" ,r ) y .s mamw& -- $. g

7)4 y =y ~~

~. a..r - :3.;,-,3;g4 -. - y. ^ ^h qt ~~ +- n.- ,..2.. l .fS ' Y[0fYiy +~ ~ ~ . y.. _ t j o,. c / f. r l. 0 9e e.,._ _ _ _ _ .4 P%f. c :s m.,' ^$*, a .1 ,$ } ,n E g 4 I 6 I W:n l l. - l 2e v. 3 k i r ?i i

0. =.*

up t o p ?. ; 3 e, -. v. . e4 1 y p p< py., v s.... _;.:y:z

f..

y ? ..g,. e .U f i

s. :

1 ....c l }l .J fgyy7ygjy

,..: 3y p/ frg c h a '374 y --

g--.y j ; ygig m.s g.M r w r f e ~a t e n p a R ; Q $r p r : -daj:a k;;p.f'e,. z~~-@Wt. kr wor u ~ a w d u k ey.ggm.. m.. g iy ng

~ ~~~l.f& :, )'[ _. - _ p. f g.;2 * ',, 1 ~ '. J ;

3n g^y:{ff

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Tr!.l.

S p C c 'I 17. - t-7 .1 ~-MM', ~ ?..

$t;. m,

[ .t, N,' T, Y. DOCT SUPPORT DESibt SHEET b A ,r J oS- .a ;; 3-9-11 Analysis Pt.*No. Date ^ The Robert'Irsay Co. _ Hanger Mk. Ilo. [N-Uf0"N-9 Client Project Enrico Feral Atomic Power Plant #2 Hanger Deg. No.h-'/tr8-MO '#-h -9 1D-4221 Duet sire- /0N ~ ~ ~ ~ Project No. CCWW {6NE$. WG. Computed by D* MADN$ 5ystem E r

1..

'( y -~ .-....ay, 1 --.s k , 7 i.- Support Type Eang'cr ~ LaGral'-~~ ~~ Axial ~ ...):k"a +.a a Direction VEE.T-N,9 - ~ =~-_:--- / Coordinate Axis [ f., 3 :g=. g u.. p n - O y L Force Weight Setemic lead (f): z,y.s, Dir. Cobained Max. yy.quiv. Cylinder ' lead (1bs.) load Ixx Equiv.. Cylinder l E F x 18 ,o r, gj o j ' 'J r ~ ,'k ;. ; Of.+

t. -

~ T x 3 The m.aximum load is^ weight load plus seismic load. is used. iU The larger sciente load from eithey fxx or tyy.. 3' --c .s l' 7 Af ~ *a+.* . g"? : 'o / r,.

.g N

v'm*- .k.i. al.. ' ' '. ~., ' k.

i

n g -3 E gRemark: support design drawing is ' included in this report. c .. a 't '. O support ta for.uittple ducts, ts. deide desvios is v.m includedin"reht566 'h b ,l. /.ddMfM$$h$$NT N @ $ h !f M df N N I l

[-_-_-__--_-__-__ ,,.,.s-_._.. l ~D C,. _(P3.. IM DU d '. f 6P - - _ - _ - - .,s..f@:4/..w}1J). Cj Vh.V %

c. Q?

f I. ~ S. !-,,$ ~7. f :$.e - 9mu s ~ Q .< (? OF_ %k-l, -1 '

g..

i - ~ W t t [m,. J.. ~ t A-SHT; 1..

f l >y.. ' '. }4..<^. y !y

* *,t.,f.3

[ bh '. h I,l.1 - r'8 bk, * ?g k*a' 7 ' f. g. d. 4. k. u ary[., ...e + e,.. M E4C, g a.- .p p -.- g. ~: 1-mq - 'P.,T. SUPPORT DESIGN SHF.ET gp ~ 4.- - DUC - s i.% o r r

,, y..: ;

(. - ~ - .. g. y y.- . a. m .u...~. 2 Analysis Pt. No,. r Date HanaerMk.No.[M-2ffC-8-N The Robert Irsay b[' Clicat Hanger Dwn. No./04221-N-M-4_@_-M

2 Project _ _ Enrico Termi Atoute Power Plant-.___._ __. _

.../U8 $, _, 10-4221 Duet size Project No. System [o_NIEtt CEMit1JVAC. ____ computed by T) map 4 M w-.... wa..:;2.,a... .:e-:- ~.. ;,c, i ~ C;i ;. (( ;,Qi_.ld;;.-_.:, .. ~.. _ - ~ _.. ~ _..---,.m_ Support Type,* m '

Manger IAteret-Axial.

i .t:;._ _. D_irection_. _ _. _ _ _ __ V. ETT1 E-N ~~ Coordinate Axis , g... y..,, _ X-

.. 7 i.

3,. u~_ < .,.g e* . ~.. I Torce Weight Selenic load (i): n.y s. Dir. Codined Max. 'h.5 (1bs.) load las Equiv. Cylinder 1 Equiv. Cyli,oder 14ed 77 o 7 7 a. /,. - r, p: o 's7 4y.. r 97 o. i.- r -"'O. 1

r,

p A[

The maximum load'is weight load plus seismic load., The Israer seismic load from either las or tyy is used. f,.,, p 'i. ' ' J." - L . 3, .. -.fi.. -l >s c.r, ..,:g t , v.5-4 P, g. t.' 5*,-

8 e

I ? % 7 r F A f',hRemarks Support design drawing is included in thin report. . 2c : O support i. ror. Itiet.' e ct., th. de.i.n dr i i.- '.- .42, g.;t.. m. included is;t. port.50.f'M... t.s,.. m.: s.c.m v n e c,',e n :,. y :s.v~C " c.< W 'g, !)i.e. Li.a N :.A*A... 'ye-ps;;+p,jj p,*. 4 ,hp f* )

~ lN[f,. Wi&SW ' f y Y

] JJ f f.,6 4 ' f[1--

__k,_f y n.:'.,'~'f. f. f.., +. p.'g s += g _.9 gy.;;, gL'.$'( ( f".ll,[*~,.y,. R; y,a,..,.y..,.' ii. 4, 4

3.,,;. ' l..i,

~> s .'s',. 1 7 :. s .,c,c . j, s,a +,.. y, n. as.. 3 -.,'t .,= . s. + -. ;..w, ,,x

f M M y@C, N'f.o..

w;- (.. e. w <. y,. -. 1 {,..

n... *

. y.. t. ., t v

3.,,

. :,r 7, 9 ..o.7 _ y ,7, >,",d ' if.; i. _ oc. -,2 . DUCT SUPPORT DESIQI SHF.ET ,>, ;.?. f. * ; *4 c .v.7;M. s .s. .,... ' j.' -; - 1 f- ,g 27'- ,, 3 D Analysis Pt'. No, b80 _ b-h~f*7 bE E ^ I., .Date ~, .m... y Client The Robert Irsa'y'Co. J k '. Hanger Mk. No. [N-2I N 2S Project Enrico Fermi Atomic ower Plant #2 _HangerDwA.No.!O 22#" W O' M " O'2S n, e Project No. --- 422f ~ - Duet Size -- - - [2A 8 - System 00MRol Ce' meg. WAc computca by - D.MADA3/ . L. '.:.: w 4' d-blu,.r:. <.r..: -w ~. : h.. i.

. * -.,,.. c. -

...:. n.,.a.,.,. : a. n,,..a...,.,..,-. .~ , w n.. ,n. L.:--%. stDJMii. Ems =. Gm.ni.%+%.;= =.: - - -.. - - -i.- - ~* c -.: w m ;. e.q v.._.a. > : uy ;c .~==.mo-. =.. . ~ - -, ~. - l Support Typ... Hanger-- -1.ateral -. - Axi al - ----- e n,. 1. Direction,$[." Mf~ jf '.' - 7' ". b .r..r. ~ Coordinate ~ Axis = -'7 i Y ' ' ~2:: - ' .T' - . c _ & = x, w m t.,. ~..,. ~t -.u. e.,...,_.,. v.:g,., m.m 3._, -., _.r._.,. ~-,:.,.. .n,, o r. . e.m s .3 a --.- ,n.. . ~,.. 2 - -Q 2 :. _.. '~}".- Force Weight selspie load (i): w y,z. Dir. Coniped Max. (1bs.) load Igx Equiv., Cylinder 1 Equiv. Cylinder Imad 77 l r, I Z-r, - 82. i9 x f,- ;., f z.._ ~f . ~... - - - T.. .... ~. _. . :a - x, . x. r.. ., The maximum load is weight load alus seismie load. or t y.is used.. The larger seismic load froe either !xx y .d..^ ~N. . [, ,- jgM ( [, j, ", b Ij U' , ".w*- (. ..-.wv 3 /.- -y ,,, =. 3( 8 ~' p-

p.,.>4--3,

,+f... ? ...r t pw m, e e ._,g*j 4' *;.*.*. m, l~~ e _ ~l 's { 7 c. w :: Z O. , ; g,,,,,a E support desian arawlos is incioded in thi. r., ore. ' a.. sopport s. rse.ulti,1 4.c'es, the.4. sten ar i W.r q 4't$...?:.. h ^ . M n ltsej& ' Y r & So $ & S $} W Y &. $ $ % 5 i s ) g.. 4 48 m; * .p' gs. g,' g= f y n.., , 9g.< ' ^ * ,,.,, 6 t".' 4 f La g w.e e, gy q.n,.'

W ; eg,

6 .. :.m .g .+ .( q ;e:.$ h. h .y? ^

7 - c.t' 3.. y,_ ,c g,.,. 2.,.3 ... g u.c u,. ,,t.>, ~

s.

.**-[.~,.-4...,}..., gg 2

..'r}/ d aj.

,'f a .]# ,. L., . e.. T =* },(/9] [,. y. ..s v '.O5 A3 ~~-*~~". i !, ~' v l 1 a 'l .,. t;: -,.5, *...; 7, .g . / ?.m.,.. g.,., 9.j.

. j c i,.,

e p j.;. 1.ppro 'a rt. - 'y ...4 24 ; i 4;^i .m.s yp.. s, , z. -u .c p '4 's ,' ~-," is t Q Y U. DICT SUPP, ORT DESICH SHEET ,1 . e $, 11,. .L 3. 9.-77 --4

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$ * ~5 ,'5.- .[ ^ t .i.. ,, a g, to,1,,1,,,,,,, 57o p Cilent Tbe Robert Irsay Co.' Hanger Mk. No. [Ilf-2870-N-27 Project Enrico Teral Atomic Power Plant #2 Hanger tw. No./O-422/-tm /M-283 -27 t k Pro, ject No.2-- 4221 ~ - Duet Size ~~ f2 I~~ --~~~~~ ~ ~ - ' Systen QJ)] el C6NTtd /h/NC ' ' ~ 9 AIND.IM Computed by .:.a. a u.1:_.: m:2m: .. ; u.

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...._.._-..,,J._ ...w = :.- .a j Support Type - -; - - Hanger - - Lateral - - Axial ~~- ' ~ Dir'ection't ' ' NRi ' W.,. 9 i _. ~ - hdime Axis ~ -h-- "~$~'~~ ~~~ ~~ ~' ~" - ~ ~' I i I '* n'. Q : %: 4%.;i.i.,~ ?l \\ %V k..::.. = - - i.. P l Torce Weight Seisnie Load (f): z,y,s, Dir. Cob &tned Max. i (1bs.) load, Ixx Equiv. Cylinder 1 Equiv. Cylinder Imad 77 F, ~. r 83 et t.. 10 lof r a . }....,. F s ~. . ' 6 ~ \\ . I', ~ [ c: i .. e ,f..,... i .The maxisca load is weight load plus seienic load. n. the larger seismic load from either fxx or t is used. yy ,h. ~ t .,q N. sg:c f e v.. n.9.-....f. 4 .p; ..j , 4, .g.. ..j., r.- y -g.- ,s a. .+ Remark: Support design drawing is included in this report. O Support is for multiple ducts, the design draw'r.g is i ^ 4 ; lre.W. -. ?? ..s f'.::t ~ ...c.. . a.. included in report 30.1( **'

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~ DUCT SUPPORT DESIGN SilEET '.~ { 5., ' j'_ -, 1 3"<f~7) ^ AnalysisP'b.No. f85' _ Date Client The Robert Irsay'Co. Hanger Mk. No. f Af Wo -h-30 'l ~ Froject. Enrico Fermi Atomic Power Plant #2 Hanger. Dwn.' Mo./04271-OOO -/./5f. 2851c-3(* Project No. - -.- 10-4221...- - Duet S' ire - ID0 4 OOMik'st. CEM{CC. SV4C Computed by .D. AlijpA A/ Systen L ~- 3.._ - _ ....2. _. ... ~.. u,. g,. _., Sup po r t Type._.-. -.- - f : ~ ~~~'.a*.-1 t e ral'?.'Z'. '.~T Axial. '_'.*_~' ' Z Z". !.'"T._"'* *", : ... Hanger. ~ - -,.U. in 3 9 ' Direction gf, N.' . Coordinate Axis - T . +,l.: - .m.. x r. ;.f - - m. r m..~.........-- y.

i. e.:...;,.

l m,a. _,a,, . u._ Force Weight Scismic lead (f): x.y,s Dir. Cobained

Mez, (1bs.)

Ioad Ixx Equiv. Cylinder l Equiv. Cylinder Load yy F, T 83 03 ),l l06 y E l 6. q ~ 7.. .c a s. .P e. The maximum load is weight load plus seismic load. The larger seismic load from either Ixx or tyy,1s used.- ,~ ? ., p, .x. gf. . :g:g; s; . v. 3 -.,. ? l ~+ .u l -.h. .r. .b i i /Y 4 'r ~ hg,,g, Support design draying is included in'this report. C Support is for multiple ducts, the design dra'ving is .. G ly.s.*. Q n p.e.;.;.,% 2 N 9 -@ y ~inc1'uded in report No.:.'..,.6. - N ". r, .7 -M .,:..,, ?... - n., p.. w..a irr

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t.

.r. c.. ,9 77 [O;. m 'W $' ' .2 W: Date Analysis Pt. No.~ -.. _ ' _ ' ~ a Hange' Mk. No [N-288'd-3/AS/ T i~'T ~ The' Robert Iraay Co. ~ ~~ Cliens r Enrico retal Atomic Power Plant #2 Hanger fug. No./O 3/22/*CDO-0N-28, *3I ~ , Project ~ u Project No. 10-4221 Duct Sire -- NX0 -..s;.7 O

N/lD.4 N t

System OMTfDL bd7tI N V C. ' Computed by ']* i .]+j_,-i.g-; h r .c'

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v ,...._..__.~.u.. ..e... L ,.ss

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j /. ,f. --. -.v, .,et, .t.,...,;: c A. . 1 21 Support Type. _ _ ,._ j!angt r. _ L.ateral. ... Axial,,.. _...a v-Q -kWJvM 4 Direction pg72T". g,y ~ e--u ce. % w-. sa,/ow. %4% Coordinate Axis _3_..,.... _' . 1.%;.......... - a .n .~-.7._q.,.._..- g,

.; 7

,,,, 3 u,,,.;;,.,,g.g, .., m... .y .r:? m t%=,,,- r,,.,..;1.ur:n,.1. n-a,, r V force Weigh"t Seisste toad (i): r,y,s, Dir. Cobained - Mas. lead (1bs.). Icad Ixx Equiv. Cylinder lyy Equiv. Cylinder u r, .z: Sc/ - S$ 31 lib ** l Fy f ,. u - j y g-4y x.m ; The maximum load is weight load plus' seismic load.., f ~; '.n'yjl }f 5 3 s Thelargerscissteloadfromeither*Ixx or tyy is used..',. ..T.,1 'f1i.,f./3 \\ i .c f .,n c: ... ; :.~x ~ nlQ j Q ...o y N, 5 _. 's 's g ., l J;v 9; . a x- - vy ,g,ue. T f.H y@j.p... n.s u n. s:

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.m> ..a.,. t C' 4 gg,,,,g, ' Support design drawing is included in this report. f,. [p C Support is for multiple ducts, the design drawing is y_ . bNk -ha b'kN included La report No.', I [ ' mw%Li.w$ - ,w v.:. -,w w - s.I.3 < sc:... i .i,..

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l g i.. uGNuggpf1 .n.; DATE DATE,k7//.g. Vi l ' -($1 l LEHT'. SHTs 012aop/pg ' L I ,,.9.5 i l y,]t.I - d, I*.hs, 8"g,,,g ',y,':;,., pp '..{,Js, t [g p,4.@ t'- , e, i j y g;,y,,*; j .g '.di '. ~ .. n.,. ~ 8% o . k Pil)OR WC. U. . s. .s / f DUCT SUPPORT DES!Cil SIIEET c, i Date Analysis

t. No.

MM- ,,. MJ Client The Robert Irsay Co. Ilanger Hk. No bi-28(/9-N-41 Project _ Enrico Fermi A'tomic Power Plant #2 Hanger Dwg. No.h *il72/-4'b /M-7F<N (/2 2 i =,. Project No. 10-4221 Duet Site - l(-K if. 31 System I_ CUT Ctf CENR$ #VAC. computed b' D M404/ r.r- -.Y.>; ..t f.;.u.. :,.a, .e

..:.7 3,,,

Support Type.. - Hanger 4teral.<.. .~ Axial...,h w-, .. ~ v _ _ _... _. C I :- Direction - $f g f. . E IV.. ~,~"w' - ; m, w t Coordinate Axis y_ )( r l {_- , g: :z.~..; g%g;,3.p' ~ ~.*~ c 4k 4 - ) ~ rorce Weight Setssic Load (tit z,y,s, Dir. Cobalnad Man.~ (1bs.) load Irx Equiv. Cylinder l Equiv. Cylinder , lead yy F, g .y fg 4 Y 19 7 'll lY ZIS r. ~ F, 7 wr o. - \\ r; the maxleum load is weight load plus seisale lead.... ..,L. -. l .,4 The 1stger seismic load from either fra or f is used. '..h37] yy s,

Ny p

r. t: j [ i '3 y dj - . }l, s. 'ef j :- ').*. *y '. :?.g,':: -fg^ .1 ; g ,. qp (C-5 ~ 7.,. s. E'.?.? ' $.,i h . w e,t,y 4,T i g ~ g.' Rema rk t Support design drawing is includedi in tkis' report $ ' i N 4.' ~ p C Support is for multiple ducts, the design drawing to included ik reporh [lo. kkh.k3 .i $ N b'eb fh:*i M.-;y.y ;7766-{;{ y h N W

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Date Analysis Pt. 380. . MJO . m <;,-L Client The Robert Irsay Co. Hanger Mk. No. [N-2ft/9'-//-MJ Project _ Enrico Fermi Atomic Power Plant #2 Hanger Dwg. No./O-t/tti-O@ -6Af.7]</9./j se 3, - Project No. 10-4221 Duct Size /6A l f --- - -- - ~-~h System CUTDt CEWd pVAC Computed by D.M/ID.N 5 ...i. t . naz..u nq -......~^L...,.-,...-..l',.T..~. n.. :.,..w.~.., 4...s.h % M &i2.YLM.Ii.A :EdE5 __.x ......_.-.-.._.s+ w~.-....c.... .m .l,. Support Type. _ _.. Hanger.- -. t.ateral _,.. _ Axia Direc tion' - gy. '< - - -E-W ~= + ",. A" * *W..... n#.~.' ' .s . w Coordinate Axis- -T -g...- .f-; -J :. y.. s .. :., gp:.3.t:;qq1g'i j.;7. ';ggy.;ql,:h.,gQ p; hh O

*.. T

. ~.1.:: 2,1., p - . e., -~ g Torce Weight Seismic toad (i); x.y s$ Dir. Cobalmed' ' > Max. .i[ (Ibs.) load Ixx F,quiv. Cylinder, 177 Equiv. Cylinder load y 4 33 y*- 33- } r, r, So6 'f4 ItfL % S20 r 0; ~ , h(b

g.. e.s..y-

.w. 'l ..**"dr.,,s. a.... EA.', <r A a .e, i . ". j d'. ? 3 s : 's t m- ...?

"% -';;,i...: C L f...

_l.' The maximum load is weight load plus seismic load."'C.'i'iW J.E' C. % j A ^, '? g 3 isused.yff'sf2"i The larger seismie load from either Ixx or 1.. J'!& kWh;.. gf W.'. N;d 77 . W.. 'y-q.j' Mlk,)f:.f. K;, L-2. ; 4.'*-; c.l- ... qfF .s ,-s.;y;,~t .& D,};$)@i?rh..SIilA&5?'.h s

c. a& h 6,....aj}.d.1Q(

.y.. Q .u "1 ^ 4.* d,.:j,7 'l y . sp.4% 3 :,p;; w... : 4.,..~.s v .;.w n,.- J >,;fc".. &gcy : ..p ,g 1 . a,.,.y.. :.u... p.,, o.,.,.,- s u. -

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gRemarb Support design drawing is included in this re'hrt'.

p Q Support is for multiple ducts, the design' drew'ing is r* - '\\ ' ~includedlareporYNo.'lRN. Nh 'D-; j,g.::q M " M U M & W if

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, ITjp ' . 1 s. .a. - ,, e:j_t'y yk (h..,y.. l l. t;PLUOft M NC. t -g r DUCT SUPPORT DESIGN SHEET 'i - {, 31-7 7.. _, )_., i._ ,,,,,,, (, Client The Robert Irsay Co. Ranger Hk. No.6M-2.#44-/f-# Project Enrico Teral Atomic Power Plant #2 Hanger Dws. No./C-#f 21-M bM 28Q t(( =,, Project No. 10-4221'~ Duet Size ~ ~ I6A l2, ' _. ~ ~ ~ ~ ' ' ~ ~ ~ ~ ' ~ ' ' ~ ~ Systenff&1l?tt CENTER }lVAC Computed by .D Af A r>t d ..6.'A. . s . - p M...-.4.,:./ N.i d. $ z u ; f,a.!d-.h ; ~.s+ ;.',;', ^- - - r .. ~..

- : a r-

...a-Support Type Hanger ^~ 1.ateral~~~' ~TAxial ~ ~ ~ ~ ~ ~ ~ ~ ~ ~ ' " ~ ' Direction ' MD. E-W" E' ~ Coordinate Axis T: ' )( - - - ~^ .? .. :v s

.. e..e

.,..-:=.n: 9 I .m j e

_. -.s Force Weight Setssic toad (i): z,y,s. Dir. Cobained Max.

(1bs.) load Ixx Equiv. Cylinder 1 Equiv. Cylinder lead 77 r, I g 23

7 T

jjf, jf,

r: l.T - 4 2N y --- r - r, . S ',.s.r* d The maximon load is weight load plus seismic load. 't r f. yy isused{^. The larger seismic 16ad from either,1xx or l k ? ~ 5;.. -y: f 3: ; 2f ~, ; y 4.;,j. 4.: b W.'.

s

^ ~. , ;, ~.r s' ~ ? hRewrh E support design drawing is focluded in th1s report'l' ~ e O' support is for tittile' ducts;.th. dess n ar rio i. #.... imeluded'in$ehrt Ididh ~ b 'b ~ $g,..a. 3,..

v... -.,

m ~... f's p4 b4.. t j u '; C,

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l'- t S H T.__ 1 $ D JO F _.1 1 }. 3, f. ".Ig M ?hM,.i.,iik V -. ;Ty3*f.3 g g,('.4-j,,9..p. 4 , q. % x,p,*) - a w m.c ....e ..i..A Q.?, * ',1., 7 : k M. M.. E ~ i 1 DUCT SUPPORT DESICH SHEET s MO V' 3-9-17 Analysis Pt. No. Date Client The Robert Irsay Co. Hanger Mk. No.(>Al-2N9-//-Yi" Project,,, Enjco retai Atomic Power Plant f2 Hanger Dwg. No./O-922I"@ IM 2M/-Y.7 I Project No. _ 10-4221 " ~ ~~~~ ~~~ Duet Size /6Kl[ i Syatcm .M[ot. k&JQfl}/A C.. ~ Cosiputed by J). AMDh/

.a. 3::w.

.a. L ":0?*ii _. ' = ?M.5 ~ '- - " .m-.. Support Type ~ 11an ge r--' - 1.ateral ~ Axial -- Direction -~ VERT^ E-W Coordinati~ Ails ~ ~ f ~ ~' - ;"J ~ ~ '-- ~~- - ~ ~ ~ ^ - -- ~ v.e r-m. . s..:. x, - r.;.a.. :..~,.... O rorce Weight Seismic load (t) z,y I, Dir. Cobained Max.- ~~ (Ibs.) load Ixx Equiv. Cylinder 1 Equiv. Cylinder Iesd 77 r, j9 2.2. 29 r, ASo to. I7 950 a r, - . _:..:. ( The maximum load is weight load plus seismic load.' ~ 1he large'r _ seismic load from either 1xx,or t y is used. y a y'I.r:., ,.1, ., v i : r 40,.. '.3 -*~ N ,8 % m ;r - ~ v. .;, ' % s ;. .y 3 , n. c. - ,e-v,. g .c. 3 . 'n, ~ Remark t h Support desig drawing is included in this report. 5 O ' 5=rPore 'is'ror.uiti,i. ducts.. ts. 4..is. 4ravi 1. 1.e1.d.4 L re w e % W ri; A $ M....... W.....% eh & W W & W ~. v.. ~ akikNkbh$$$?bhhh hkN'Y ^. UAQhh

g. ~ h 0f5E...1 HON ' NO7 4 .-r------- '.', S' H T.l'.'g f ~ d p?? } y.~- ....,_.e~..-_. .. - g.,-... y.r.?.3 e ".31 J; ?.; .,.y ~ ..' ? l . 6. 3- ,g' - ~. ,,._ :3 y _, ~,

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50 DUCT SUFFORT DESIGN SHEET 3

.L*.1"Y.-

Date Analysis Pt. No. M Client The Robert Irsay Co. Manger Mk. No.SM-7I8/9 -#- % Project _ Enrico Fermi Atomic Power Plant #2 Hanger !%,g. No. h-V221-O@-SN f8W.8/6 e. Project No. '10-4221 ~ k (f. _ Duet sire systemh07Rct. OEsprR, M4C computed by D AfADAM .l 4.:v r s - i e.. w, - ~.. _. .. - - - ~ ~...- ~~ Support TYPE Hanger Lateral Axial 1 . Direction __ __. . Mf; _. E-W.. l3 -l----- Coordinate Axis, f,- @ q _...,-)("" ~~ ~ ~ ~V O ~ i l r. ..;. k-Force ' Weight Seissie lead (2): x.y,s. Dir. Cobained Max. (1bs.) load Ixx Equiv. Cylinder I Equiv. Cylinder 14ad > ['. N yy i r, 4D S3 53 -~ i ~ T, ,936' $3 )t; 'A. y, 9,d. The maximum load is weight load plus seismic load. 2 The larger seismic load from either Ix, or lyy is used. A

.p'

+ .r 1 1 ..e .~ t4 Z hFemark: Support design drawing la included in this report. i C Support is for multiple' ducts, the design dreving is.- .-*'9-g, included in report No.' 1:y;f:,.; tsS'f. :%4$%'.yW [..i.Q. r...h * - w *.W.sr i t4..r .f; i.i:i.. 4 % 9.. h' "i - - ~ t< _~.

.. y ' h" ; i k< *"," ;. _, _., & Q } N. &p >.,,_~ V- , - ',j., j l

l. W:$ '

, Y7*0)7-Y OkT% aAl 7 se_ _p ... a, _mem z i T- ? f ' '. f'-J'[;;$ %f1'6uI'$x,%'h'$iI..*diaT'[/*'j[E. i: i. 4 !.3 3 ' ~~* S, T , p.[ & y f ~ W- }g ~' f,,.. a gc t . v-s. ~ 3 e DUCT SUPPORT DESICN SHEET y h d'.. .. :E. ~ 880 $" #I* 7 7 Analysis Pt. No. Date i Client The Robert Irsay Co. Hanger Mk. No.0 M'lI O */f-9 7 i l Project Enrico Fermi Atomic Power Plant #2 Hanger Dwg. No.h.V22f.000 4M 2JW 8// -- Project No. 10-4221 Duet Site /0El6 5ystes h lylftsL (CAJTf_L' //t 40. Computed by D IIII)D4A/ / 1 ,J.,. m ee e<>...-...~._..--=-.~.~*~=--.=~-*~~~~.-----.-------J. - - ~ - -*---~--Am.- - - - + - + - 4,,, Support Type'- ~ Hanger t.ateral Axial - Direction - -ygRT - L.bl p*. Coordinate Axis f g i Porce Weigh.: Selenic toad (i); x,y,s, Dir. Cobained Max. (1bs.) load Iza Equiv. Cylinder 1 E.quiv. Cylinder toad 77 s 50 52 El T F. M'l to Sa* 'i.*ll y i. F,., r The maximus loa'd is weight load',plus seismic load. The larger seismie load from either 1xx or Iyy is used.

~ r

{[,, N 9-2' er Remarkt Support design drawing' is included in this report. ~ Q Support.is for multiple ducts, the design drewing is N ' e .-!.*.,'. : L f;pi'..~' *jz.q-A / ai] - included la. <k.c. - <.4, - :.:ts .t e $ '...-t_ 5 ", +: L : report No P- .U.; 'W **' ? % '** M *.., ,t b .. :t p.:,'.5:.6#4{ ' ~ ~, ..a__,___.._ 4' C.. - it @,,', .4 t 4. m g 4_ %.. y . ?. -- -, d;,,.- 4- - -, --e. -y

i ' '

N/ {yif f.NO_gO $ ' - ~ lf MTr -Tf

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t gh, 3.u.c r.gl. f M M NC. r-1 i,, ,'l,.. <W ,, y DOCT SUPPORT DESlQt SHEET we. 3}~l) Analyste Pt. No. 8l[O e', Date . Hanger Mk. No./M 2$'U/f-8" /8 Client The Robert Irssy Co. Project Enrlco Fermi Atomic Power Plant #2 Hanger Dwg. No.h-Y22/'8V' *dN'78'/7"f8 ~ e. Project No. 10-4221 Duct Size /SX16 Systea Oh)1998. (UnstrID }WAC. _ _. Computed by j). tllAp4N 5- =. 6.~ 6___...._ Support Type Hanger t.ateral ' Axial Direction yg?r. N,# ,ry-Coordinate Axis [ ~d:: t Q.7 rorce Weight Seissie lead (i): x,y.s. Dir. Cobaloed Max. (1bs.) load Ixx Equiv.' Cylinder 1 Equiv. Cylinder lead 77 g.: r, r 96 16 87 l13 R.. y 6,.. ITS l82. 185 r l s T (3 *. The maximum load is weight load plus seirsic load. 1

g.

The larger seismic load from either fxx or l is used. yy 4..c ( llJ N &. - 1 a .i. Remarkt Support design drawing is included in this report. 4[; .y. .O Support is 'for smaltiple ducts, the design' d swing is 'i. 3 I IIbI $E H-rk? ' jfegg y d.,"eport ho 'M ??M$'SkCb$kYh 5h hh k $h:-

W. N $ 9 $.3 6 '=.1 fk$ , /" T/7/ 7 ONd//.k ~ l - ~' . 8Hk)h._;_QF__j.%-s:m ~f l I I .. r' ..t. ,q1y p} p g a.,,, ,,*]7 ^' ;~ ~ ,o., .' . ? J f;... y".p e *fm;'a ,,3 s - ~. .y o y rx, '$ @'.t @.p',: $[

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, y j-y. . 7t.* ..; ') [ .$j DUCT SUPPORT DESIGI $HEET '" ~- 4 ~ .w. Date Analysis Pt. No. 380 ..e.. CIlent The Robert Iraay Co. Ranger Mk. No.[N 2FC/9-//-l/9 7 Froject Enrico Termi Atomic Power Plant #2 Nanger Dwg. No./tF-Vl#-Cet' -MNWf. i Froject No. 10-4221 Doct Site /dXila System b0lVII'I-[GUR/d/IVAC. Computed by h M494d m, g.. ,.., _,y , -. ~. ..__,,,.,.m__;__ .,,4 i j Support Type Hanger Lateral Antall - ^

d..

I Direction y0,ET.._. g.,g. l Coordinate Axis 7 A . ',. d. n'=- w -.s s, -c Force Wet ht Setsaic toad (+): x.y s, Dir. Cobained Max. S (Ibs.) load Ixx Equiv. Cylinder 1 Equiv. Cylinder , teed 77 4 ~. y, 1.03 - F j& ' )4 fl + y ts' Is. JW s.i r, 7.3 ' (( %2. ',.. [. p'..

n.. g :.1

'l -,r The marious load is weight load plus seismic load.',, r e e n. " - d -{f"- [ & .f i h. The larger seismic load from either fxx or t y is used.,.4 y . ry.. :.. , ky .,p,., Q ^ * ^ y. +q sp.f, ?,. ir,9; ....h. '...; ; l ',. l

,s.

.q. .7- ~,r I hy,,,,g Support design drawing is included in this report. [ l C Support is, for multiple ducts, the design dravias is. a' N fka ~~ " - inelhed[idrehrt ebNU' r-n. :. s L. ,. J',;@n..x:.ni - x v

' ((

k .;4d , [..\\ ;

.....g - ~ ~ n ;.y..,,,_ ~ ~,,. . ~_.. DCi % _'l.82P6._JJ$ ll. ? hT7MT Yl L . hkTGC 2fts/s4..n. G': f { l - g g l I r ,.' - }J - g,.4J J 'd 5.q. % ' '. y v.a... ,J... .1.. F /I';h . "f Y. s ~ g - e-p. o, ......... g.t.c;.... n.),. t, g.:e ' ' '9 'J ~ j DUCT SUPPORT DESIQl' SHEET i. ., _., :. a. , ~... - 7 Date Analysis Pt. No. i i Client The Robert Irsay Co. Ranger Mk. No.d M.)$ @. N f0 t Project Enrico Fermi Atoute Power Plant #2 Hanger Dwg. No. M N " M M ' N I 88 __ =. Froject No. 10-4221 Duct Sise fSXEe i l System [CNJRrl. l'GLik"fi NVAC. Computed by D.MAMd l -.-L. 9., 5.+..h..,;.J. g-LEH r. 7y.. ..~.n l -1 i Support TyP' Ranger Lateral - Axial,s.y' 3.. ; A ;A. .w.-_. o ) 7 Direction. /66.__. _ Af,5. i Coordinste Axis Y: g .e. +# m w ? - ~.__. \\ 5' .s a .~ 1 Force Weight Seisele Load u): x.y,s, Dir. Cobained Man'. i X (ibs.). Ioad Izz Equiv. Cylinder I Equiv. Cy11aser imod yy F, ..y. .g ;* Y $90 b k' 5. ~ y , 8, .3 O' ~ ' U Ui/1 bl=I fb 'h [,,;. F s-s -d .~ t e: O c E.. ~ !? The maximum toed is weight load plus seismic loed. .-T W,, I T.e,a ;,f. ' 3 J. or t yy is used. P.1 It P : #.n/.$...'. :,... y The larger seismic load from either tax .... = e.n. y, w &y..-. , <.. ^ ' fE . L,k.. Q+ : } x : Np*..f.,... ?

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.r. .e 1 s. -? Remarks Support design drawing is included in this Ireport. .- ;/.y '. O s., port i. c., It1,1e 4uete, in. destoo dr.y;;. c..,- -. svies i.x WD e

~n g,:- :.~

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.;;_ :. g 2.u._.; A* 3 " 9 'II Analysis Pt. No. '3F# Date Client The Robert Irssy Cs. ~ ~ Hanger Mk. No.[W-2fM9-N*[I Froject Enrico Fermi Atomic Power Plant #2 Hanger Dwg. No./0 4/111-000 M28V9 4'/_ s Project No. 10-4221 Duct Site NX16 biRol. CEMTcR #dC Computed by . FAN A AA Il Syaten .,. -.... :.... w..., g.1 - -. ..g .yg .s. ..o. +, _ w... %. 4. C's Hauger1 1.ateral-

Axial l' N Support Type Direction

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m. ; m,._. v.

s e 4 Z

9 Remarks Support design drawing is ine'luded in this report.

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/ of 4 ~~. '.~ I T4tc2, m ENkICO DESIGN CHANGE PACKAGE DCP NO. M M $'ERMI COVER SHEET =2, CONSTRUCTION STARTUP SYSTEM / SUBSYSTEM NO. T4102-SYSTEM NAME Control Center A/C System BASIS FOR DCP: The addition of a Halon System in the Computer Room requires new supply and return air shut off dampers for room isolation Ref. EF2-58,172. CHANGE MUST BE ACCOMPLISHED: ,8 PRIOR W SYSTEM OPERATION YES NO PRIOR M FUEL 14AD YES NO (Portion of duct with new I shut off dampers down TASK 10. QA LEVEL graced to QA III) ALL ENGINEERING INPUT COMPLETED NIPO ITEM NO. None ll~/2-92 y SCHEDULE REQUIREMENTS: ENGINEERING 7- /- [ 2 c+- # CONSTRUCTION Si C N- ~ FINISH DATE PROJECTED RELEASE DATE ONO IS FSAR CHANGE REQUIRED? YES IF YES, DATE LICENSING NOTIFIED IF CONTROL CENTER AFFECTED, FMR NO. FOR CONTROL CENTER MODIFICATION IF GE AFFECTED BY FDDR AND/OR FDI, DiR NO. FOR MODIFICATION DESCRIPTION OF CHANGE - REFERENCES E BASE CDNFIGURATION DRAWINGS, PURCHASE REQUISITION. OTHER DOCUMENTS RELATED M THE DCP BUT WERE RELEASED PRIOR M IEE DESIGN FREEZE DATE. 'nlE PHYSICAL LOCATION OF MAJOR (DMP0hT.NTS AND ITEMS REQUIRING SPECIAL ATTENTION ARE TO BE INCLUDED. 6M721-2851 Add new supply air shut off damper in vertical section of 16"x20". Zone 4 duct. Add QA III Seismic II Class brake to both sides of new damper T4100F174. ~ 21-2849 Add new rtn. air shut off damper to part plan _(20"x16" duct) & Section El-El(16"x20" Add QA III, Seismic II Class brake to both sides of new darper T4100F175. Det 6M721-2751 Diagram - Add new dampers & note to declassify affected duct wor _k at both sides of new shut of f dampers T4100FI74 and T4100F175. 6M721-4500 Schedule - Add (2) new shut of f dampers No.s T4100F174 & F175 (OA III. Seismie II) NOTE: I 6 C_ portion to be completed _ under DCP P80002101 RELEASED W CONSTRUCIION S E C M '- ., r1 DATE X ORIGINATING DISCIPLINE CONSTRUCTION COMPLETED BY d.LO DATE fc fale,c't O OTHER INVOLVED DISCIPLINE (S) 8 ' (C T J/_j CONTINUATION SHEET ATTACHED VERIFICATION OF COMPLETION _ MAMi. DATE /p[5[$3_ (CON ~ DCP COORD) X0 X0 DCP W ENGINEERING DESIGN 'GE OFFICE DATE () ELEC. (X ) MECH. DCP M ORIGINATING ENGINEERING DISCIPLINE DATE () ARCH. () INST. & () CIVIL CONTL WORK ORIG. DISC. EDCP CDCP PROJ. START-CONSTR. DATE , I!ESCRIPTION LDR. SUP.ENG. C0pR, / COOR CONTROL UP SUPT. _ _ _ A 7;< g,@ COPE l'.fl. M&f7/8E //////////))] M. ~ % 44 _ /////// /,l//// /////// r.tc.n fi' REVIEWM(f b-'7/n/62 //////////IM iD%iufMti&5thM UM,verMI U /7, acevinntsa e/,.;n n. n i, n ::' n -o -+ist r+ CONSTRUCTION L.rfr(fte9(qw gg.npLiye::. :L:a:T:'*' /

G _";"

T" 4 _ 16 APPR. FOR CONSTRUCTION: DIR., PROJ. DES.MhPf/XQ EX kgW I//.% b " Revised 4-26-82 [ } GED/67/15. ]V A [ ^ 'i.": t."f f r 3jV h b[ [, b Q [y[ % r c..p a a g.)f r i i higtri Date C00rdinat d III

~ ^ wm:mm ~'Y W/WV $ l __ _ .w_v -~~. ?- c " W -~ " w w ^ / A b GY hWh "aAI "T 4 I c 3. W I

NkICO' DESIGN CHANGE PACKACitgIS IS AN IFITIAL mm DCP NO. 3440G-eG5 STARTUP SYSTEM / SUBSYSTEM NO. T4107-SYSTEM NAME Control Center A/C System

! ASIS FOR DCP: The addition of a Halon System in the Computer Room requires new supply and return air shut of f dampers for room isolation Ref. EF2-58,172.

MANGE MUST BF, ACCOMPLISHED:

PRIOR TO SYSTEM OPERATION YES NO PRIOR TO WEL IDAD YES NO (Portion of duct with new QA LEVEL I shut of f dampers down TASK 10. graced to QA III) iLL ENGINEERING INPUT COMPLETED NIPO ITEM NO. None l/~/2-92 y,y

CHEDULE REQUIREMENTS: ENGINEERING 7- /- M ce r CONSTRUCTION dC-h FINISH DATE PROJECTED RELEASE DATE ONO

.S FSAR CHANGE REQUIPID? YES .F YES, DATE LICENSING NOTIFIED .F CONTROL CENTER AFFECTED, FMR :.0. FOR CONTROL CENIER MODIFICATION .F CE AFFECTED BY FDDR AND/OR FDI, TMR NO. FOR HODIFICATION PESCRIP 10N OF CHANGE - REFi.FINCES TO BASE CDNFIGURATION DRAWINGS, PURCHASE REQUISITION. >THER DOCUMENTS RELATED E THE DCP BUT WERE RELEASED PRIOR TD THE DESIGN IIEEZE DATE. THE 'HYSICAL LOCATION OF MAJOR COMPONENTS AND ITEMS REQUIRING SPECIAL ATTENTION ARE TO BE INCLUDED. 6M721-2851 Add new supply air shut of f damper in vertical section of 16"x20". Zone 4 duct. Acd Q.~.111 Scismie 11 Class brake to both sides of new damper T4100F174 jM/21-2549 Add n.-w rtn. air shut of f damper to part plan (20"x16" duct) & Sect ion El-El(16"x20y Add Ql. Ill. Scismic 11 Class brake to both sides of new damper T4100F175. 65721-2751 JQrp. - Add new dampers 6 note to declassify af fected duct work at both sides o f ns.t stut of f dampers T4100F174 and T4100F175. 6M721 -50J Schedule - /.dd (2) new shut of f dampers No.s T4100F174 & F175 (QA 111. Seismic II) NOTE: I 6 C _ port io, t o be co pleted, ufnd. er DCP PB0002101 ELEASED TU CONSTRLCTION GEWt-DATE X ORIGINATING DISCIPLIhT,

0NSTRUCTION COMPLETED BY DATE O OTHER INVOLVED DISCIPLINE (S)

(CONTRACTOR) CONTINUATION SHEET ATTACHED /ERIFICATION OF COMPLETION DATE (CONST DCP (DORD) X0 X0 .iCP TO ENGINEERING DESIGN CHANGE OFFICE DATE () ELEC. (X ) MECH. )CP 10 ORIGINATING ENGINEERING DISCIPLINE DATE () ARCH. () INST. & () CIVIL CONTL WORK ORIG. DISC. EDCP CDCP PROJ. START-CONSTR. DATE , !!ESCRIPTION LDR. SUP.ENG. C0pR, f COOR CONTROL UP SUPT. 1 KM /udSCOPE ri. N+hlet ///////////// 7-4 Lillfill JJilli II/II/I Qd' hr 7/d8_t /////////// 2"* /GMynJK,.re%#nwrh 4 to.n (L ' REv1D:~ V /7.. Aj / ~ -,, n '[ M t H CONSTRUCTION L}W(fyffqW y.2.?L. Hj[1Q f s ] APPR. FOR CONSTRUCTION: DIR., PROJ. DES.-/77M M,}AM/ F075 MF0tCTdl6P0ih GED/67/15.1 042782

POR: DCP NO. T4 tot Mol ENRICO DESIGN CHANGE PACKACE.THIS IS AN INITIAI; TERMI INDEX SHEET ISSUE AND APPROYAI,., SHEET DISCIPLINE l M C N A hllC 4 l REVISION 8 NEW ATTACHMENT SHEET NO. INDEX DOCUMENT SATELLITE MYLAR NO. AFFECTED BASE ITEM f ADDED TO OR CR-7s CONTIGURATION . NO. REV. DCP-REV. SHEET DOCUMENT NO./PIV. 001 futeMASE lre.>t s t 5 231-120 O C.'l M -l 1,M '1,31-2 151/C. 003 se.I. tori aI-1g St /D 0 04 M.3 L M nl-2f'}4 { sf ++s A i;ct,'eQVo n b 3 006 R tnen th _ _135r spot s irre * * *t ) (USE ADDITIONAL SHEETS AS REOUTRED) MAT. RIALS & EQUIPMENT REQUIRED OU~M"oodeont vias uced fFr efAEWru INDEX MBER ITEM # ITEM d ool fo'x/t/ AB. Ar44 (fp ggrther Edison approvals are9 227 42o d W Meott. yc 30 rRutira. oot AcTvAToFi. EbwERS (O EA. 7 F-1 f 7-41o MoDEL 33)-2193 DEt"- Engineering be Oni lbS4TIO*4 SwTCH (?.) Eh. Y S-tt1= 4% o A/AMco EA700 Sorco Coordin0, tor L (USE ADDITIONAL SHEETS S REQUIRED) 7 ti!#l PREPAREDBY8/(/G#0V[49 h DATE / ASK ADER/ WORK LEADER Q /fAf/4 DATE 7 23 % APPROVED BY / SUPykVISING ENGINEERING _REV. DATE DIR. PROJ. DES. DATE _ _f DCP, COO). FOR REVIEW ///////l/////// 7-M71-FOR CONSTRUCTION />7 f/e/A/ //-I.f-ft. H:5~e-LV Ie n_J s A 2 N A.$ 2 -st& 4 3 % N A .f. - s7 - 3 3 6 r 3 @ .y Y tf u CED/67/15.2 1 041582 j

_ _ f y ri n 7 43 km 4 or 9 " ^^ MIIIAL EDIam'ED FOR: DCP NO. T4/02 Mc/ DESIGN CRANGE PACg""7E AND ATPROYAL. INDEX ITEM NO. 004 ENRICO ATTACHMENT REVISION FERMI fA

'T 2 SHEET OF DESCRIPTION OF ATTACHMENT SHEET M-S AFFECTED BASE CONFIGURATION DOC. REV.

GM 7212849 REV. Al - m. p DRAWN /4tcW sCEECKED[gfjM SUPERVISO f0TRER DISC.f 5 " /t004 OTHER DIS. EA-I&C/ ELECT. EL. 4,7 7' 6" SYST. ENG. l l l. 7 l l 4 1 I 76 "r 34 ' UP 70 AfruAAI FAhl //6A. SI PActt/DE NEW AcrESS D00A Wx.50 " /W 2'0" 2 '-// " y n, 4 7y *,p ~ l ~ Y M O- , q., s 4 72'0 " l s a \\ /- l S,' 2 l n,i to v

j.

9 N j-i I 2120 CFM y-g ,j 4 ~ A.O. ~ V.u, ; f l NEW 5 Wor 04*i i b., DAMPEA f lT4/coFt75l GA-Z _,L QA-Z MISMll'.1 ', V$f15*1tc -I /8"n it ' & 0.O. G(o7 '-O " f GA 12T STO Cfht Scistnec.2{/z ~7\\ MEN AETUAM AIR.$ NUT-Off DAbfftA ENGA&l2ED CLOSED, FAIL OPEN SCAL.E: Y2"* l'0" CED/67/25.3 041582

W YA&L4 l df Y ec'&rd.nees ros m, MTAOf M N - 8 k PROCEDURE a m:21.am a a

D,wTEnu (DcP ieTNt01 % 8 ENRICO FERMI UNIT 2 TYPE (1 OR !!) 3 DEScNCHANGt DESON CHANGE n nELD SCDF D(RECORDAS SulLT)

REQUEST (F4 ELD) DCTICE (DESJGN) LJ REQUEST (DESON) DATE REDO a OR SCHD SAPACT EST COST (IF K)CWN) toCAnoN a oR systrk m. GLEd. (e 7 7 *-O NO. 6 ) (o REV. O ContpE11ee DOCUMENT TOgE REVISED:(No. arid Rev.) 9 Tsifd3 SHEET l . or. 9 ra - a n '? G-v Ja. - Ic k s a rm un-o v'i p DESCRIPTlON i% A ss s l-o c L-T s e u, of S U J -r o f'F-M m,o tM Donan=syy-op CHANGE: REASON FOR A M)^ 8 2 E S Pb t G DsD &T Auow Cen s,C,o,s o n o r) CHANGE: AC OLNb&oa n ( [ (1) CONCURRENCE (2) APPROVAL (3) AUTHORJ.ATION wRmEN ar T 7A DATE __4 -B - 03 RESPONSIBLE DSCtPUNE ENGR (1) DATE

- / C
b AUTHORrTY FOR WORK TO PROCEED (1)

DATE EO9tPutNT OVALIFICATON ALITHOR12ATION (3) DATE-EDtSON VERBAL CONCURRENCE i DATE

~

~O EDSON RESJDENT ENGINEE DATE EDtSON ASST DR.. PROJ F1 eld ENGR (2) h DATE: d-d b EDtSON SUPERVISING ENGINEER (2) DATE: ~ EDISON DRECTOR PRDJ DESGN (2) DATE. su.ETCN ANDom ADomoNAL woReTiON der ARMS DOEXED f DTC: TC.bte k ~ t D (q" DSN: 8 5 y. tO U>

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Engr D P Coord
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Al 1/M M C 4 } y'fq tse / OP / JS g y ISSUED FOR: DCP NO. 74101 H02 ENRICO DESIGN CHANGE F M'D Ap g,D # INDEX ITEM NO. 037 REVISION FERMI ATTACEMENT M Itw!T 2 SHEET 9F *) 0 $

2.0 DESCRIPTION

OF ATTACMMENT SHEET C-6

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REV. hlO ME h% r W

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DRAWNI,. h w.- CHECKED JJ. N,.., A SUPERVISORg4 THER DISQ[/ 4 '\\ OTHER DIS -I&C/ ELECT.thya/s #/f/g f i k ^/ 51 ga SYST. ENG. f \\ Al , Ref-t.w! P LUO f~ f(OTE F~ RC(C-f.T q.o% s?. y /' 9, we. Rrce 2.t 49-1 c Nh' ( kEUlsE 0 Eic w Q~ I c,y ISOMET RIC wn ? 3 j S 4 3}0 2 49 g [ 45A ~ T.O. D. M 1 e T 2849 EL G~l3' 4 Y p N N 4gs b W '<j/ v T 2649 .g C> kX '[41M \\ 2 c Z M g, C' inlN s d 'a,- H i ~N t.'4 y',f " NOTES:

f. ALL SUPPORTS ARE QA LEVEL I

2. DUCT 15 G A LEVEL I,22 GAGE. GALV.

dA

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i JolNTS AT 4' MAX. WITH 3a" DIA. BOLTS s/, \\ 'T f ,? / s i / AT G' MAX. SPACING. PROVIDE L lle vlI2x 8 STIFFENERS FOR DUCTS EYCEEDING 14" O'/ N /49 2549 (MAY. CROSS-SECTION). Q g'b, e A ^ t, 3 ALL DUCT LINES SHOWN ARE /' CE.NTER LINE OF DUCT. Qq's / INFORMATION gyg EVSD SOV B C 3Ar

284c

7l ) oni a ISSUED FOR: DCP NO. T410'2. M07. INDEX ITEM NO. 034

NRICO DESIGN CHANGE PSC7fCg D REVISION Dygg ATTACKKENTSS0y D Appggyjs,,

f ERMI SHEET 8F 6 CF JNIT 2 DESCRIPTION OF ATTACHMENT SHEET QA LEVEL I c-7 AFFECTED BASE CONFIGURATION DOC. REV. goyc x,,..,.. DRAWN Id 06 _. CHECKED 9 r., L..., SUPERVISORev joTHERDISC[ftf' H oTHtR DISC. tA-isC/ ELECT.c g,4 of,t SYST. ENG. T Ct.E F w t.u o CL 9ioggs R G.Y.EcRT f40 OC o 7 94,-l s I l1 (TYP.) T' 2 ~ = .O T.O.D. EL G'l2' O" 7 __i:. ; 1_ _ _" j f. - DUCT B ol 2 '- 'r-- ALL MLMBERS

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7W-ISSUED FOR: DCP NO. T4101 M0'l g INDEX ITEM NO. 039 U IFITIgg g DESIGN CHANGE PA g AMnyj g,, REVISION f NRICO ATTACHMENT TA gggy SHEET W 9 #F 1.0 gt-2 DESCRIPTION OF ATTACHMENT SHEET ~~ c.- s GA LEVEL I AFFECTED BASE CONFIGURATION DOC. REV. noog a.. o... DRAWN /A06dee CHECKED '/p (_.' O. SUPERVISOR THER DISC [/fff 7 I OTHER D15 -16C/ ELECT.a* An ur /a SYST. ENC. R.ET- -T Lu c5t. V* ion EE R. R.E Pc' 9.T Mo R. t c. o - 2.S4 9 .I c ~ \\.'.-)r i ;.

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W norw. -r m i W S Is gy ISSUED FOR: DCP NO.T+102-H02 DESIGN CHANCE PACMUf A1;n gy IIAL ED INDEX ITEM NO. 043 REVISION ENRICO Ala.

ATTACHMENT SHEET w 10 0F 1.0 g/A FERMI JNIT 2 DESCRIPTION OF ATTACMMENT SHEET

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c. 9 AFFECTED RASE CONFIGURATION DOC. REV.

N C h) E M.,. ? DRAWN F. 6G CHECKED. '. i-1. N.r'; - SUPERVISORW THER DIS @ ' OTHER DI -I&C/ ELECT.c'La #/r/,,. SYST. ENG. ILE F K Lu oR., P i o N gi p g Rypo gy MD Il%C O ~ ~1 iE 4 'l - I O \\ly/*/. ;. .\\ / \\ l/ ,,' c ...o.,., s c CEllt!4G d I If OfSE$'(PE E L. GlG'-G" s s ?!.Q'JAL { h j f 4-- / l'2" (T't'P) p 't T.O. D.

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HOPPEH ANI) AssorlATES E NGWE E R1, 249 AVENDIA DEL NORTE REDONDO DE ACH. CA 90277 21>316-0835 October 4, 1984 HA-10/84-347 Contract #84895A Task B5 Detroit Edison Company ) 3331 W. Big Beaver Road Troy, MI 48084 Attention: Y.N. Anand, Contract Adminh trator

Subject:

Safety-Related Duct Evaluation - Status Summary Gentlemen: As per your request, we will take this opportunity to sumarize the status of the subject activities and formally provide you with some of the ducting hanger and anchor load infomation which we have generated. Exhibit 1 provides a summary of our initial categorization of the vari-ous HVAC ducting systems. We have identified those systems which we con-i sider to be rigid, those systems with apparent flexibility, those systems for which recent design changes necessitate reevaluation, and those systems which we now understand to be categorized as II/1. The systems which we identify as rigid were so established by approxi-mate frequency evaluation showing the response to be in the ZPA' range. For these systems, the original Fluor analyses loads may be used directly for OBE hanger and anchor evaluation purposes. It must be noted, however, that the Fluor analysis did not incorporate any support weight whatsoever. Femi hanger qualification loads must include a consideration of the support self-weight as it responds to the applicable building location ear +hquake exci-tation. The effective dynamic mass of the supports should be detemined using dynamic equivalency factors less than unity. j The hangers in those systems which have not been identified to be rigid { should not be evaluated using the Fluor analysis it, ads. Support loads for these hangers may come from detailed dynamic response analyses. In the ab-sence of such dynamic analyses, the bounded horizontal load infomation which we have infomally transmitted to you nay be used for support accept-ability verification purposes. l The bounded horizontal load information provided to Fdison was generated using envelope facility earthquake response spectra associated with the Femi site specific earthquake event. We understead the hanger structural evalua-tion is completed using AISC allowable working stresses. For this reason, th? bounded site specific earthquake loads may be reduced by a factor for co6;patibility with the original Fluor design basis and current Edison allow-able working stress assumptions. The derivation of these bounded load re-i duction factors follows: krrm7 A6 g45g 2-w 13 l = = = _ - _ _ _ _ _ _ ____-_____-_-_-__L

j HOPPEH ANI) ASSOCIATES HA-10/B4-347 t euc* Page Two 1 k Site specific earthquake effective load reduction factor I f.6F { =.6 ~,' i 1 1 4 Design basis earthquake effective load reduction factor b C6FT a}y.'If=.35 ' X ^ * ' Operating basis earthquake effective load reduction factor l et - 18 g =.33 ' l Exhibit 2 sumarizes the bounded load infonnation provided to Edison as a function of duct width. Included in Exhibit 2 are curves which show the initial bounded support and anchor loads transmitted to Edison in mid l September and recent bounded load data adjusted to compatible acceleration l 1evels for the various. Fermi earthquake events._ It is our opinion that the original bounded load data is satisfactory for necessary hanter and anchor . verification purposes, exclusive of the round ducting syster for which i higher bounded load magnitudes are justifyable. 1 In our walkdown of the HVAC system above the Fermi control center, we observed that some hanger angles were not welded to the supporting plates i at.the midpoint location. The maximum effect of such support member eccen-1 tricity has been established. ~ i Bolt Load Plate Bending Configuration Amplification Amplification l As-built 4.5 1.1 y1 Under member 2.6 3.3 bolt removed 1 i l l Pass 3 of 13 l I

E ] l HOPPER AND ASSOCIATEg HA-10/84-347 tuome rca, Page Three We are continuing to complete specific anchor and hanger evaluations on a case-by-case basis. Exhibit 3 provides documentation of our detailed dynamic response analysis results for systems 2850-1 and 2850-4. Other specific load infomation will be transmitted as it becomes available. If questions arise, please contact the undersigne. Very ply yours, ,i ~ avid M. Hopper Professional Engineer l cc: D. Schweikhart R. Moore b.N""'D 7g DMH:ekr [M6 - OF I3

HOPPER AND ASSOCIATES HA-10/84-347 - 1 suciuter.s APPARENT APPARENT DCP II/I RIGIDITY FLEXIBILITY EFFECT NO SYSTEM EXISTING EVALUATION EVALUATION EVALUATION EVALUATION NECESSARY NECESSARY NECESSARY 2251-1A X 2251-1B X 2251-1C X 2251-10 X 2255-1A* X X 2255-1B* X X 2255-1C* X X 2255-1D* X X 2255-1E* X X 2255-1F* X X 2255-1G* X X 2255-1H* X X 2255-1-1 A X 2255-2 X 2255-3 X 2255-4 X 2255-5 X 2255-6 X 2255-7 X 2255-8 X 2268-1A X 2268-1B X 2268-2A X 2268-2B X 2268-2C X 2268-2D X 2268-3A*** X 2268-3B*** X 2268-3C*** X 2268-3D*** X 2268-4A X 2268-4B X 2848-1 X 2848-1-1 A X 2848-1-1B X 2848-1 -1 C X 2848-1-2A 2848-1-2B 2848-1-2C 2848-1-2D X 2848-2A X 2848-3 X i !!'i:3 An#4 x 2848-4C X ?M,ef xB 2848-5** X 2849-1 X 2849-2 X 2849-3 X

HOPPER AND ASSOCIATES HA-10/84-347 I E NGIN E E 4 APPARENT APPARENT DCP II/1 SYSTEM RIGIDITY FLEXIBILITY EFFECT NO EXISTING EVALUATION EVALUATION EVALUATION EVALUATION NECESSARY NECESSARY_ NECESSARY i 2849-4 X 2849-6 X 2849-5 X 2849-7 X 2849-8 X 2849-9 X 2849-10 X r 2850-1**** X 2850-2 X 2850-3 X 2850-4**** X 2850-5 X 2850-6 X 2850-8 X 2850-9 X 2850-10 X 2853-1 X 2853-2 X 2853-3 X t 2854-1 X 2854-2 X 2854-3 X 2854-4 X 4126-1*** X 4148-1A X 4148-1B X 4316-1 X 4316-2 X 4316-3 X 4316-4 X 4316-5 X 4316-6 X 4316-7 X 4355-1A X 4355-1B X 4355-2A X 4355-28 X

Erroneous 11/1 designation will necessitate DCP effect evaluation.

'i

- Insufficient data for rigidity assessment.
  - Detailed dynamic analysis underway.

\\ Detailed dynamic analysis complete. TTE)/, gg DUCTING SYSTEM CATEGORIZATION

SUMMARY

g g h pp g EXHIBIT 1 g

~ HOPI'I'.R Axl AssoclATE5 l'l-I!'4-387 tuwnete 800 b j

00 r

sp g c#* s# E C S t /,

00

~ LOADS s / ANCHOR w LOADS BASIS ANCHOR DESIGNBASIS y LOADS OPERATING HANGER 0A0S l ~ L BANGEE GINAL m O~1 C C *i IF SPE E00 TE r LOADS SI HANGER Sigy 481S LOADS / HANGER s IING g4SJS / i J t i i 1 1 1 I 10 20 30 40 50 60 70 g :d g DUCT WIDTH (IN) -j REPRESENTATIVE ANCHOR AND HANGER LOADS [ggg. 9 SE /3 EXHlBIT 2

HOPI'Elt Anis ASSOCIATES HA-10/M-347 ss unu ANALYSIS NODE HANGER LOAD (LBS) System 2850-1 4 2849-H58 42 7 2849-H57-118 10 2850-H84 47 17 2850-H73 111 26 2849-H61 15 31 2849-H62 38 36 2850-H74 248 39 2850-H75 106 42 2850-H76 38 2850-1-H3 73 47 51 2850-H85 35 58 2850-H77 250 63 2850-H78 41 66 2850-H79 130 70 2850-H80 36 73 2850-H81 280 76 2850-H82 133 79 2850-H83 13 84 2850-1-H3 150 _ System 2850-4 7 2850-H49 321 12 2850-H50 74 17 2850-H51 159 22 2850-H52 24 26 2850-H53 55 28 2850-H28 184 35 2849-H4 53 39 2849-H3 94 42 2849-H6 107 45 2849-H7 27 IU SPECIFIC EVALUATION RESULTS h/P66

F M Exa18n 3

T-HOPPER AND ASSOCIATES ENGINEERS 249 AVENDIA DEL NORTE REDONDO BEACH CA 90277 213-3164835 ^ October 9, 1984 HA-10/84-351 Contract #84895A Task B5 PIS fT41-00 Detroit Edison Company 3331 W. Big Beaver Road Troy, MI 48084 Attention: Y.N. Anand, Contract Administrator

Subject:

Load EstablishmentSafety-Related Duct Evaluation - Bounded Hanger Gentlemen: for all Fermi safety-related duct sizes as a function of ha This infomation is presented by the enclosed curves, a family of which h been plotted for each duct width. as vided to you in the same fomat.The data hereby transmitted reaffirms the inf Documentation which proves that these generic bounded loads are the largest loads that a hanger with a given stiff ness will feel, exists and will be fomally provided at If questions arise, please contact the undersig ur request. Very r ly o ,/ avid M. opper Professional Engineer cc: D. Schweikhart R. Moore R. Kennedy NOC Approval DMH:ekr g fnc,s

)

OP 13

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' ~ ATl'AC.M Er47" E7 PCo l 01: S) HOPPER AND ASSOCIATES ENGINEEfts 249 AVENDIA DEL NORTE REDONDO BEACH.CA 90277 213-31W35 October 8,1984 HA-10/84-349 Contract #84895A Task B5 PIS #T41-00 Detroit Edison Company 3331 W. Big Beaver Road Troy, MI 48084 Attention: Y.N. Anand, Contract Administrator

Subject:

Safety-Related Duct Evaluation - Hanger Load Establishment

Reference:

1) EF2-69,989; Peak Bounded Duct Support Load Assessment; October 1,1984.

2) Our Letter HA-10/84,-347; Safety-Related Duct Evaluation -

Status Summary; October 4,1984. Gentlemen: As per your request, we have established a refined bounded support load magnitude for those hangers described in Reference 1. Exhibit 1 is attached summarizing these loads for your use. The tabulated load magnitudes represent full site specific earthquake bounded load limits. Bounded load reduction factors roay be applied as ae-Jired in accordance with Reference 2. If questions arise, please contact the undersigned. Very uly David M. Hopper Professional Engineer cc: D. Schweikhart R. Moore R. Kennedy NOC Approval DMH:ekr l

ATTAc.Megr 4 7 P6 '2. O F S HOPPER AND ASSOCIATES HA-10/84-349 E NG'NE E RS p899 l Of 4 REFINED B0UNDED SUPPORT NUMBER LOAD STRESS REPORT MAGNITUDE 1. 6M-2268-H-6 200 2268-2A.C 2. 6M-2268-H-11 5 2268-3C 3. 6M-2268-H-12 15 2268-3C 4. 6M-2268-H-13 50 2268-3C 5. 6M-2268-H-14 10 2268-3C 6. 6M-2268-H-15 20 2268-3C 7. 6M-2268-H-16 35 2268-3C 8. 6M-2268-H-24 5 2268-3C 9. 6M-2268-H-25 15 2268-3C

10. 6M-2268-H-26 50 2268-3C

11. 6M-2268-H-27 20 2268-3C

12. 6M-2268-H-28 35 2268-3C

13. 6M-2850-H-26 100 2849-1 14-6M-2850-H-27 100 2849-1

15. 6M-2850-H-30

100 4849-1

16. 6M-2850-H-31 100 4849-1

17. 6M-2854-H-17 150 2854-1

18. 6M-2854-H-21 190 2854-1

19. 6M-2854-H-5 140 2854-2

20. 6M-2854-H-6 200 2854-2

21. 6M-2854-H-7 180 2854-2 22, 6M-2854-H-8 180 2854-2

23. 6M-2854-H-9 200 2854-2

24. 6M-2854-H-13 160 2854-2

25. 6M-2854-H-35 320 2854-3

26. 6M-2854-H-36 190 2854-3

27. 6M-2854-H-37 240 2854-3

28. 6M-2854-H-38 290 2854-3 EXHIBIT 1

~ AWACNust4T I'7 % b oF 6 HOPPER AND ASSOCIATES HA-10/84-349 t~cmet s Page 2 of 4 REFINED I BOUNDED SUPPORT NUMBER 1.0AD STRESS REPORT MAGNITUDE ? 29. 6M-2854-H-40 170 2854-4 30. 6M-2854-H-41 170 2854-4 31. 6M-2854-H-42 170 2854-4 32. 6M-2854-H-43 200 2854-4 33. 6M-2854-H-46 170 2854-4 34. 6M-2854-H-47 170 2854-4 35. 6M-2854-H-49 180 2854-4 { 36. 6M-4316-H-18 150 4316-2 + 200 37. 6M-4316-H-8 300 4316-4 38. 6M-4316-H-9 300 4316-4 39. 6M-4316-H-12 120 4316-6 41. 6M-4316-H-33 120 4316-6 42. 6M-4316-H-35 120 4316-6 43. 6M-2849-H-53 210* 2849-3 250* e 44. 6M-2849-H-54 300* 2849-3 480* l 45. 6M-2849-H-55 260* 2849-3 480* 46. 6M-2849-H-60 370* 2849-3 47. 6M-2849-H-63 170* 2849-3 48. 6M-2849-H-64 170*- '2849-3 49. 6M-2849-H-2 200* 2849-5 50. 6M-2849-H-69 600* 2849-5 51. 6M-2849-H-15 500* 2849-5 52. 6M-2849-H-16 650* 2849-5 I

If this system has had the anchors removed per DCP, it requires

-detailed dynamic evaluation. EXHIBIT 1 (Con't.)

A TTAcW ME.M W '7 Pe:,4 oF 5 HOPPER AND ASSOCIATES HA-10/84-349 r~omtp:s Page 3 of 4 REFINED BOUNDED SUPPORT NUMBER LOAD STRESS REPORT MAGNITUDE 53. 6M-2849-H-23 200* 2849-5 54. 6M-2849-H-12 600* 2849-5 55. 6M-2849-H-24 200* 2849-5 56. 6M-2849-H-13 250* 2849-5 150* 57. 6M-2849-H-14 250* 2849-5 150* 58. 6M-2849-H-33 100 2849-6 100 59. 6M-2849-H-66 70 2849-6 60. 6M-2849-H-31 140 2849-7,8 61. 6M-2849-H-38 140 2849-7,8 62. SM-2849-H-9 240 2849-9 63. 6M-2849-H-27 350 2849-9 64. 6M-2849-H-28 350 2849-9 65. 6M-2850-1-H-2 90 2850-3 66. 6M-2850-1-H-4 90 2850-3 67. 6M-2850-1 -H-5 90 2850-3 68. 6M-2850-H-49 321 2850-4 240 69. 6M-2850-H-50 74 2850-4 70. 6M-2850-H-51 159 2850-4 71. SM-2850-H-52 24 2850-4 72. 6M-2850-H-53 55 2850-4 73. 6M-2850-H-19 50 2850-5 74. 6M-2850-H-24 140 2850-6 110 75. 6M-2850-H-38 220 2850-9 150

If this system has had the anchors removed per DCP, it requires detailed dynamic evaluation.

EXHIBIT 1 (Con't.)

.. i, A*TTA4.4ME AT 7 Pc3-5 o F S i HOPPER AND ASSOCIATES HA-10/84-349 ENGINEERS page 4 Of 4 REFINED BOUNDEO SUPPORT NUMBER ' LOA 0 STRESS REPORT MAGNITUDE i 76. 6M-2850-H-37 220 2850-9 150 77. 6M-2850-H-36 220 2850-9 150 78. 6M-2850-H-35 220 2850-9 220 79. 6M-2850-H-34 220 2850-9 150 80. 6M-2850-H-33 220 2850-9 220 81. 6M-2849-H-8 200 2850-9 { 40 30 r 30 82. 6M-2849-H-7 200 2850-9 l 40 30 30 i 83. 6M-2268-H-5' 200 2268-2A' l 84. 6M-2268-H-7 180 2268-2A 85. 6M-2263-H-8 150 2268-2A 86. 6M-2268-H-9 200 2268-2A 87. 6M-226B-H-10 200 2268-2A 88. 6M-2849-H-30 140 2849-7,8 89. 6M-2847-H-26 110 2840-10 ~ EXHIBIT 1 (Con't.) . - ~ _

ATrAc h s,Jr

6 Pc> l oF 2.

HOPPER AND ASSOCIATES ENGINEERS a40 AVENDIA DEL NoRTE nEooNoo sEAcH. cA soarr 213-316-0636 October 26, 1984 HA-10/84-359 ) Contract #84895A l t* Task B5 l PIS fT41-00 Detroit Edison Company 3331 W. Big Beaver Road Troy, MI 48084 Attention: Y.N. Anand, Contract Administrator

Subject:

Safety-Related Duct Evaluation - Hanger Angle / Supporting Plate Eccentricity Effects

Reference:

Our Letter HA-10/84-355; Safety-Related Duct Evaluation - Hanger Angle / Supporting Plate Eccentricity Effects; October 23,1984. Gentlemen: As per your request, we have amplified the information transmitted by the reference to illustrate the relative effects of eccentricity in the two orthogonal directions. A revised Exhibit 1 is enclosed to document the results of our evalua-tion. Anchor bolt load amplification factors are documented for the situa-tion where all four anchor bolts secure the plate. If questions arise, please contact the undersigned. Ver uly y David . Hopper Professional Engineer l cc: D. Schweikhart ' t R. Moore R. Kennedy NOC Approval DfH:ekr l [

~ HOPPER Ai.s ASSOCIATES ENG8MEERS O N <! PLATE 1 BOLTS 4.o l // 1 i W.' 3.0 -J/ 9 a n 5 o / s. t 8 // g /. 9 /- e3l 8 2 2.0 / 4 1 4 / i,.# y (l EXISTING b ANGLE y 1.0 o O _X m 2 ^ 0 .2 .4 .6 .8 1.0 X AMCHOR BOLT LOAD AMPLIFICATION FACTOR N ANCHOR BOLT LOAD AMPLIFICATION FACTOR I 4, O I EXHIBIT 1

AC, 2M. /77924/44r AA T PROCEDURE sio. s.ri. 3:e & 32: j . as anom m ercs os m ENRICO FERMI UNii 2 ' O wTERm (DCP wo. ) DOCUMENT CONTROL 8ITE "" I' 0" ") No...I.N.T..S M..-'..Q.... RECORD DESIGN CHANGE DESIGN CHANGE FIELD MODIF.

(AS sulLT)

REQUEST (FIELD) NOTICE (DESIGN) REQUEST (DESIGN) { g jg DATE REOD & OR SCHD NPACT EST. COST (IF KNOWN) LOCATION S OR SYSTEM - HVAC-Res_gj;or/ Aux. B1de. Stres s Report 2849-1 (RICO) NO. ABM-0554 REY. 6 SHEET 1 OF 38 _ DOCUMENT TO BE REVISED:(No. and Rev.) As Noted Below. Documentation i DESCRIPTION d OF CHANGE: To doeuroent walkdown per FEWF-9 REASON FOR CHANGE: (1 NCURRENCE (2) APPROVAL (3) g MM*M WRITTEN SY; M-ATE:

D N ~I"'8 V RESPONSIBLE DISCIPLINE ENGR. (1)
AUTHORITY FOR WORK TO PROCEED (1)

> DA IG DA EOutPMENT OUALIFICATION AUTHORIZATION (3) EDtSON VERBAL CONCURRENCE (1) D DATE I _f .rM L EDISON RESIDENT ENGINEER (2) k .O DA EDISON ASST. DIR., PROJ FIELD ENGR. (2) _ e EDISON SUPERVISING ENGINEER (2)._3 l-MF E: / ~2 "'8~"N EDISON DIRECTOR. PROI DESIGN (2) ATE: /2.ddI SKETCH AND/OR ADDITIONAL INFORMATION ARMS INDEXED For NCR 84-1606 DTC: [C A.'TA The following documents are enclosed: SN M /// ' 8 6'#'#/ J Walkdown Sheets for Walkdown Sheets for Vendor Drawing D.E. File No. Vendor Drawing D.E. File No. Fluor Pioneer 6M-2849-H-50 B9-962 Fluor Pioneer 6M-2849-H-43* B9-962 6M-2849-H-42* i 6M-2849-H-49 6M-2850-H-12 B9'-10H T01 6M-2849-H-48 6M-2850-H-9* B9-70679d4 6M-2850-H-26 B9-1936T(oA 6M-2849-H-51 39-962 6M-2850-H-27 6M-2849-H-47 6M-2850-H-30 B9-itM #8 6M-2849-H-45* 6M-2850-H-31 6M-2849-H-44* 6M-2849-H-46 B9-962 [ If

Some or all of the plates for these supports are inaccessible, therefore no data is r

available from walkdown. NOTE: FOR APPROVAL. REQUIREMENTS, SEE BACK OF THIS FORM L--

yg$)N CRAM,1 $DCUPe a AFTE0?A1/TRAJtDff77Al LIFT ~ l'E7f EnciattrR!sc 48N OST4 si p Casage Doco.est: &&m heeisaen 31C Piggs-2. o M Type: 1 I&see Date /.3 74-

Date, Arch / Civil Eagineerlag = SG-14 To Centrols Engineerias - 8G-33 (Imad Discipliae)

(14ad Discipline) hechaalce) Engineerlag - 3rde er E{C-45 Electrical Engineerlag - EG-44 (Land Disciplina) g (Land Discipliae) Free: Change control Group, 241 ECT The design change document listed above is being transmitted to you for your review andF1sase approval in accordance with Frn 3.3 (Design verification). signatures by checking the appropriste bones as listed below. Please return the Trans*itta! List, along with the Change Documen as indicated below. The reviews /spprovsts of this design change document abould be expedited to permit the final disposition of this document by (Date) Routits Sirnature Date order _ Rovre to INM /E"4"8/- h Imad Discipliae Originator I mM / 2 " I-d r' Q Lead Discipline Tarifier 2 /7 f"-f/ h h taad Disciplias Dork lander 3 ] Controls Engineerlag 50-53 ] Electrical Eagineerias, EG-64 5 0 = ' < 2 5 5 = 5 4 =a-a 5 6 ] uschanical Engineering BG-45 7 ] Arch / Civil Engineering 50-14 8 ] f;41saic Qualification Eagineer 9 O a 25'i >< r >< '. sa 54 10 ] Other (specify) 11 ] Eag(meeting Aasurasce 12 O esei tai e- (o**> t 13 Supervising Eagineet (land Discipline)

9. [.

A __ /2 -fW 14 N7AA /puh4A/ /A-/# */'/ h Directer, Projvet Design V / t/ 15 h Change Control Croup, 241 SCT* 16 Coseests:

Denotes receipt of the design change docuernt by the Chasse Costrel Croup for flaal retanties.

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&A ' A IN Mart-I p,,p, poor >i w 4x i isenrisy wird cp.src. Rm 8 in KsN-t i > Ju>xmc Down istgecoc7,ug - s\\o f~ 4 2 %,^2 $,. e d e t.. s o w s %. a / x 'NW c. pposing JDJJccar mW bi O kwe maso N#!a7N (l /N IS/M171/5 ,n + ,_ _j p Q w 4. f %'0 VI D E N A TE -4 7 h G Q t% k PIM(NS/pWS M 4 g o W 5 Sk'E7:M ATrAcyn', R'. 4 s F kcA1svs To 80v l ^>H 5 " *_ : LocAfioNS. I c m n = = u i u P2pA7 boxjNG G. PR' oviDC DisrAuc. l e A pog FROM A AGic/ -S, AUGtZ TO Ep&S GOp 0 'q Of %ATC i o o <r y runt of Para strovo. k }

in w y ~ cs% 2-m 7, PA6V 18 op Jg ' GA I //VAC,..- REAc rO/7 //WXlllMf Bull.p/N6 NM W ) N)N462 K 'd U TATCufM pas m is T ON h yll lh@M INsixxrious : /. /MNf/// //ANACE 5g A80Vf. A y MET /t/C E. C/XClf hi, Af/N6 CWEC#fD /4 MAN b' } 3 /NOMATC A7 a A 1 0._A $ ) Af/IT 0/vf of // THteC ARC Moff ^ '}K M,,,'f t; TMr fotcowtN6 TMAM 2/tss crirep A IN MAM-Appponsat 4xsriop fQA[k l /N $N / GENTW{ 8 in M48-g ~ wird e,p.sre. /NiccocTIN6 det. Apw$ /- I C - pro /tof b JDJ/ccar Y h h YW Gj!g'l O O-g,g g,,,,; m } N M /M iffic c q3fg tt L.'lp g 'L (pcK@T

4. PRoviot Matt u

/ / ggo O -- pietrusions O ip 5 SVGTcH ATrAcyn REUTIVS 70 80, ">N (," LocAfioNS = G. PRovtOC ptsrsw I cm u j u ]G [ {$a rm) Il F120M is AcIc/ \\ a l ', / ~ z,,% we O k lAV, le ChT' O O ~ iL SAMNf of PATA Nf1019. g. 9 m w u-

~~~ -n._ T PAbe 19 w 38 1 //wittMy Bwt.ptgs GAI //VAC. - Rucro/r,Il44 MA9 //)N662 ?<h'TCLIFft pirs lO-l1-84 pm t A l M9.H43 /NSTKVCT/ OMS : y' %l pt @M H4 h lj, 'k"[? I ~ /SGMET/t/C l/AClf 8. Af/NG J ~ C//tC,K10 /N MAN 1 3 /NO/M ff A7 z /fMr CNr of P. jf T//teC ARC Morr 5 TMF /pttouMN6 T/JAN 2 fts, crtics JPPRonornr 4xsrio'd kb A IN PL4M-Ato/27)/ in )Gy / etursy 6 * /N AAN-2 RAM wirit c,p.nc. /NicGSCT/N6

1. '- d'""5

\\ 076; f! 64 C doerg C - PRovior 4 AhCf2Z5V6 # scaccur g,g,;O y,ggg agg O 1 p J N IS/Mrffti gqy2} / e /_ ss k, PA0 VIDE YAft i O 9y " -O piMrNS/QNS g 5 S WGTc H ATrAc1ln ht.47:Vs ro 80 =yH (p l 0CA TIONS = a ,o G. F/20V!OC ptsTAu s A 1 Fl20M S AGW./ I l ', 9 3 ft

Y b

N6fA TO SDS O Op Of ~dATC lb1 k, O O aL CAMNf of PATA Nidorp. g. j

^ ^ HlWI ~ 0554-Ke v. @ ~

fnse Zd a 38

~ GAI //VACs. REAcroi7 //wiCtAey Bw&.ptNc //pgga *. 'l849 d443 lb Il-8& IX UCC P- (<'ArcuFrs as sw f sf /NSTKKTMN6 : l' t /. /MNfiff llAN6CK h M bl fl -} Aeovs. ,>g. '/soMrraie i i 2. Cacs's Al Rains c Wec,x f o 14 AtA N % b / f 'WV 3 /NOlddff A7 l (. i i /. // Lestr civt of lF 7//tec ppc Morr TMf fettowiN6 YMAN 2. A a, c es rei! A A IN PLAN-APPRow1c twrioH Ato/27)/ ix 4x / etursy RAW 6 - in MAN - 2 wire t,p.sre. /Nir4CdCT/N6 det. A'ows . <>.h k' D c - PRovior L. P f,'fy } hf U, / N M4Mf7fti O O-g. J p YL!}.10-

4. PROVIDE Fl' ATE O

~O ' p>McNSloWS u 5 SKETCH ATr4cyn ' kl.A7 ivc' w 80.; h L0cAfioNS -4H G 0 yat 1

4. PR Ovic t pis rx y.

1 Q g (f8 y) e A p p p y a A c g.,e s AUGt C To Ept; ho, $'",yy y % r o OF 447s ~ q o o JL SAMNf of PATA NifDip. g<

~ - Brse zl se 39 GA 7 //VAC. - REscrott //wittAey BwLDIN6 12S 4 0) d M G ms16-IlR6-ypwea e 92tkk G. k'ATCL PFt &w t l /NSTKLA 7"/0NS : @f f i. iwurity saue u pp, l ASovc. Y p ' l -l j ' /soMeraic / 2. Cac16 A BrinS iy y' $Sc}\\ 0 h. % > u Gf c N w f o !^t A M (YlO 3 /NQ/CAff AT l /cstr ont of If THNC ARC Mar ([t Tpr fottowiN6 i T//AH 2 As,crirck ( A

lN (MH -

APPA0Mornic L K JTio'$/ N0/2TM f. ( iN #sa / privrity RAM ' 8-lN MAN-2 WiTH e, D. frc. INifb^tcT/N4 det.. Rows F-i \\( C

PAOVfD6 JDJ/ccar O

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Q:-

/

4. PROVIDE 7t'A16 O

O piMrivstous u 5 SKGTcH ATrAcyx fit A7IV6 To 80 LocApoNS -*>N f,) Oo o 0 'I G. PROVIOC DISTAN Q f Ff2OH 15 AGIc/ A 9 6 e / - S,' &LEM LNq' f,}\\c$ AUGtZ.To ED6 Gop o Of % ATti 'm ~ O O L SAMMf of PATA NffDip. g* 1 b.

_, ~ _,_ _ fs gg 22. or.3 8 GA.T //VAC,. - RKAc ro!! //cixit&Aey Brai&.ati/6, //)N6gg ' # /b-ftt/ 6477)-295O W S2Nr. *A* jykut & vns-S M/JEd Ds1C )$*//~8f N%ct, l i.. /NSTAMCT/ OMS: ,/ /r' %l .A s l. /MNfff' //AN6C& Aeovs. fli..- g i .\\ l' y. /, V /SoMff/ TIC 2. C/AClf A Af/NS l C//1C#10 /4 NAN l s y 3 /ND/CAff A7 Afstr'O/vf of ff Thief ARC Mort fPf fottowsN$ THAM 2 A b, trift*H N A' A IN f3AN- ] APPfonpre1C 4xstio'M $0 1 I po/2TN w 4N / eturity 6-in Men-e .AAu wire cp.src. flooxinc -fP ,,,,e;,ey,ug i l._gs u,,, voe.. #aws i 1 e - PRovior ,l [ JDJsccar' D O O HAu & NVM,f L JN /HMiffM K ,1 (p g m

4. 9 tov 10s it'nt Li l

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i JN,fdf.s.SAZ y

FROM 15 Acv,./ e / AUGL.C TO 6p Z 'lop or ma o q o]2L o. reior om suoso. J g i . ~ K N:, -- _. ' .n.,,,,

ABM~03r4 Z a v. # R46e 23

n. 38 j

GA J //VACs. - AC4croir t'Jwit'tMy lBuit.p/N6 /o - 905$ LN727-2I56 12 /hCr 8 * //pH662

Cluor sesulic pirs so-/>-no pms t.

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.e.. m.-JAAL -

8 In /Een-t UNIWEP /NTf4CdCT/N6 .w, /$,, c o s.. R o w s ,~ $

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x & "8, -

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j..

y

/H6M-eM4 Ke J- @ i PA6C 24 ef J8 GAI //VAC,. - Rtscroft //usittAey Bil/4-DIN 6 ///N654 # E f So - 26 Kc P/ re pirs tornitt m t I i.. j - A /NSTAkt"7"/ONS : v' Ml i l* /MNflff //AN6CC ,/ l ll} l/SGMET/EIC I E ^80V' l 'E. C/Xcif A Bf/NS ) C/VEC,kfD /4 RAN 3 /NOKAff A7 I ff//f ONf of ff T//tel ARC McPC fff f04LoanN4 TMAM 2 fts i critc// JPPRosistni l-xn;o's ILS &A A IN R AN - NoorN in 4x / ornwy RAM -N = 6-/N R$N-2 wiTH c,0.tre. /NTt4~9CT/N4 ft 6 "x 6'k &g det.. Aows C - PEO//DC ~ JDJ/ccur O O ,4,u,,,,e g a g /N ll/A'rrfic r' L 2x Z l 6 ~ ^

4. PRovlDE It' ATE O

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4. PROvtOC DistAn FROM S Ace /

/

Y bNhY $0 $Of t

O O of M.ATC 'm o o .__.1. SDsNf of PATA Nfforp. g. k

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r, t NIFON3 .147 4'/F"t r 's 3 St,e. 2 7 or= 3 8 I. b df kl ~ zik y G3 i I t PLAHt)l t 2850- H-26 ? E I i i 5 5 h I I ) i .7 i i I -l I a ..,..m.i

+ -. " - * '

' ' ~ ~ ~ ,wr-w i

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h. PROYIOC DtsTAW.

FROM A AGE / / / 3 ( SEE s! E e A /Q AAMlf TO Eps

S o

Gop bETArL) of "R(ATC 'm o o < r CAMNt of PATA Nffoto. g ~- e.~.=.sw%<e .#r

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r momrnabwru m pgr/nis ~ m ' YA4G' $ 0 h p' ]$ GA7 J/VAC. - REscrott //wittAey DtAiLDIN6 //pH462 6 '2 R CO '2 *? Jc c /A ~1 d= L. Daft /O ll!If 4. y I l /NSTKucrioNs : I 'A c / /. /AfNT/ff //ANACE l li - '[ ASovt.

j

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ix 4x / eturity 6-IniMAN-2 RAM N=

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4. PRov>0E )R' Arc O

O-- pikirNSloNS y 5 Sk'GTcH ATr4co, ~ fravvs To BC LOCATIONS - */H g" r-i n e k

4. FRoyIOC PtsTAn e

t_; (le,x.,9 p) u A FROM A Acic/ l' Y' fSEE l} M & PAf> E A l)G L C T C G D ic o Op or tire k ro x no, e..,,,, m_ ~ bc raig O O q CAMNr of PATA NE90tp. g. (

~ -w h kr.3/ of 38 Y GAI //VAG. - REscro/7 /AfwittMy Dwt. DIN 6 ///N4SR '2 BSD - 30 kc PA1ee psis lo /n i ec ms t 1 i.. I /NSTAtACT/ OMS : y' %l A /. /AfNflff //AN4re l l / o l ', {. _ _ / j/ aSovr. l-n. / /soMEr/ttc 2. C/xcif Al Af/N6 ) cac.aro in sus i x-3 /NO/MTC AT lest7 oivt of ~ If THtet MtC piors TPr fotccanN6 TMAM 2 11s, ch'; rat APMonenc 4xnio'd A6 LA A IN PLArt-f/0/27)/ lN 4N / /prur/7 RAM - N : 8 - /N A AM - 2 Wirit e,D. src. /NTitC&CT/W6 It G"x Gx 3/s dog.. / % s 1 7 1 C - pro /106 /DJ/ccx7 O D-g,ggg g,,g l j J N MdMf7fti + 6 u

4. AeovIDE R'A16 j

O O pikirnstous / 5 SVGTcM ATr4citM g ig' r L 2"x 2"' kuisv6 70 80 LOcATsoNS \\ - */H g, " ~ O 8 G. FRoyIOC Disrau /,, (%4 y) FROM (s AGIc/ \\ 0 A v $.t AUGLC TO Epc' o (Su hAuc OF ~447s ,q y al) g o r SkfMi 0F DATA NitpfD. g* s ~

f InA0A M pe D R.S1W7/ \\ Le .32. or 18 O l GD "/ J E 1 TC ', ' j 4 i )., \\ H s e <. s+- g 2E50-3o I 7. 2eso-a-so puu 8 e 6 i 1 1 J 9 e 4 ^--'-

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4. provide It'Are e-+L W

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4. PRoyIOC ptstss.

i&u {% u a /,, FROM A AGE - i t bNS A TO NOf Y d.e-fn ') L'u. O Of sw n pep p t/<1 V)O' N " t O O <r. SkfMi of PATA Nif0fp. g* ______:_=_- =_: = _ = - = _.

x 2* %,f@>'i43 O .s 'kh l'*46, A 'W IMAGE EVALUATION v [<fjY4gf j // jff TEST TARGET (MT-3) / s (S, 47

4pff, j

+ + ,.o -2" c w llg = = lt 23 b it l[012 l.l

== 1.8 1.25 1.4 1.6 4--- 150mm 4 6" A. > s//( 4% " / s /,o8s e> ;y' )>,y,,,,, f7 ,,p g////4 ~*3

$3?tp

+ 4 ~ ns.92 bhi$bN ,3

i 1 <t ),+ to .& 44 g. $14 1*',, IMAGE EVALUATION ///j/ 4 Qf g,g , y;, ,EE,, -,< + l.0 li "* M u t" u e, pm Y T L. ('=12 1.1 e = l=1.8 l \\, = 1.25 1.4 1.6 4 -- 150mm 4-6" Al*%/ a$ s.. ? ." '*;l# T j O-44 4 / 4 ..i L'

h A t 4 // O.A Q l MAGE EVALUATION Y// 'f# TEST TARGET (MT-3) N / ,8. 4 # 49

, f,

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i.6 i.4 4-~-~-

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<e ev, @, 9 IMAGE EVALUATION N

A4Q,

\\//o//'h[ %f# TEST TARGET (MT-3) [ :fe g, / )W' k's $'7)/ +4y,, + l.0 [:aa c m p== tm E EL lllll=3S ii 4 .= 1.25 1.4 1.6 4 150mm 4_ 6" p+>% +++//A e,g+ e;,K:og )V <43 g, ////s\\ m 7p j +pp. g, x r 40 - : 3, .,.., ?llV; &i?!.S y ["

3 f PA6e .34-oP .5 8 GA.I h'. AG.

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12. 6 "x s "x &g

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4. FRovtOE Msic O

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4. Fnovioc pisun L.J j LJ e

s.,_ m'. H2on is Actc/ N ?" " S 'L'L 04 % bMi E TO EDt; <GOf Of %ATC o EG Py & ddw*/. O O 'r $YNY hh hkN Nhhh$o=

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c'Jto1MmakpTto (25VFM ,e PAbs st, oc 38 GA.T //VAC,. - Rescroir /Juxit&Aey BtdiL.DiH6 mph 6fa # 2250-31 K c PA -re t pits to / tt /K4-pm t. I i.. A s l /NSTRxr/ONS

j 5'

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4. provide It' ATE O

QW O - pikirnstous 3 5 SKETCH ATr4cyn. g r,go Rru7avs 70 80 ~ LocArtoNS - =7N g i' n m Y

b. PROVIOC DISTAW l 6

E#0N M0EI de,/a.,'/ de_a_ lo d O', o bU6LE TO SDS f } Of et me /~ i'id ' A '), or ure O y O O l <r SAMNf of PATA NL1069. g.

~.-~ .A55 05iI E5V $ %e 39 or 38 GA7 //VAC,. - REscro/r //wittMy Buit.p/N6 yp/6gg et /d -422/- &N2 6'49-A'N A, 747, A w eLyos sAwoks Arts /oA7/8f , /QYll D NSTAsMT/pHS : A g 1/' ptfy, P'f ' g,, / / /. /xurity i/xasce l 1 /

y;

!.-li A80vt. f po ) '~ / /soMEritic 2. C/ Acts A Af/NG i cA/cc,xfD IN MAN h 3 /ND/CAff AT ff T//tec ARC Mort listi civt of '~ r$AW 2 5si critcp h fMf follow /N6 ,I APMowrc 4xnioH A6 UP &A A IN PLAM-in 4N /irrurg No/2rH wit // C D. fre. RAM 8 - /N RAN - 2 LUW?N4 @ EAsr MA N ,,,,,,,,,,4 gWhlbf ? y ^ det.. Rows c - PRovior 4 4 "i l g, ' )DJsccur a l '( 2hg ') YAN6(A NWf.! >~ A + } N /Sik rTrii -o _O O-n- $g ' V' sm

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NRC-94-0050, Design Calculation, Qualification for Qai Duct Supports in Stress Rept 2848-1

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