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Ser-Prr 1-72.4tilluer. e) , I ___ 1 DIBBLE ENGINEERS,INC. PAYLESS SHOE SOURCE - STORE #4841 STRUCTURAL CALCULATIONS TIGARD, OREGON SECTION 2 STOREFRONT DESIGN & ICON WALL .: .- 7... fa . - —T (....!): . ____ . :._.q 1 -.. . ..1..• (D o . ". • - .Oa. --.• 3077.0 _ . ....__._30.0,. .. 3o:o. 30:0 30=0. 30' o I 25' - C9/4'= • • • • • • • O F..._,. 15 1 ■0. ° TYP UJ.W.6, !¢ O• - -, . l6=0 • k .. . . 1F SE V /C4r...4,04.&?? ... I.. . . q . _ 5 F /.(9. '..5 E... •. t w.g i /r - _._ -F� 1 • . I .. e r'—.. • ,A, y �1 ® t .2 O II ® ' . � , . �� ��' I o� Xs oursi Faces a • 1 . 1 _ _ -- - S � — - -• f DP WAIL[, I '� ` .,t, � d � ' - \ ; - " n y - -- -. � ,I, -.. J L ��, : rUBE cc's i j-- J ' 0 ._-7_-.-7._:.: U� _ r r �— _ ®$_9 r �_� — 'i —�9 r ll� . riA: . . " • L. I • :ICI , l' • • ,., . 0 yL . , '� 9 - � r - - i;, Pte . t�,� � ' I'' 027 • j m ' , , -y ' � i � . ® ^ �1 +p � ( `� { �G � }- 0� 1 / 4 � • • ® � I;t !1 �` �, . . b - - -- li • a /' 4' . yC• 55 • i �. ® r;4111. 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I " f " denotes stress controlled section, all other sections are deflection controlled See page 16 for Wall Height Table Notes 1R • iff SEAFE 0 General Product Information Steel Stud Manufacturing Co. .II Thickness - Steel Components Design Stiffening Lip Length I 1 � rr 1 441 i.7 IOL.. 17i' Q aoiii -I' ,! a'i, IA wr , (019111 - IDl !`Ilolo if lP . p,rwii . i .((4,01'• h�li :;ma,1,,.oA . Iufl1� c,, 1�; - :UJtlw,; 11$;:14*.; 'Alid,ti;i IIII 11i1i .' 18 0.0188 0.0843 25 S125 1 'Y:' 0.188 27 0.0283 0.0796 22 S137 1 %" 0.375 30 0.0312 0.0781 20 — Drywall S162 1 5 /8" 0.500 x:33•. ` .. • • '• 0.0346 •.0.0764 20 = Structural S200 2" 0.625 X43.• •• •'0.0451 0,0712 18 S250 2 Y2" 0.625 68 0.0713 0.1069 14 97 0.1017 0.1525 12 1 Minimum Thickness represents 95% of the design thickness and is the minimum acceptable thickness delivered to the job site based on Section A3.4 of the 1996 AISI Specification. General Notes for all tables 1. The strength increase due to cold work of forming was incorporated for flexural strength as applicable per AISI A7.2. 2. The moment of inertia for deflection is calculated at a stress which results in an effective section modulus such that the stress times that section modulus is equal to the allowable moment. This follows Procedure 1 of the AISI Specification. 3. The yield stress (33 ksi or 50 ksi) used to•calculate the tabulated values are indicated in the tables. 4. When provided, factory punch -outs will be located along the centering of the webs of the members and will have a minimum center -to- center spacing of 24 ". Punch -outs will have a maximum width = half the member depth (d /2) or 2'/2 ", whichever is less, and a maximum length = 4'/i'. The minimum distance between the end of the member and the near edge of the web punch -out = 10 ". 5. For those steels that have both 33 and 50 ksi listings, if the design is based upon 50 ksi, the 50 ksi steel needs to be specified by the contractor /purchasers. (i.e., 362S137 -54 (50 ksi)) . • Definitions of Structural Property Symbols Gross Properties lxx: Moment of inertia of the gross section about the X -X axis (strong axis). Y Rx: Radius of gyration of the gross section about the X -X axis. Iyy: Moment of inertia of the gross section about the Y -Y axis (weak axis). Ry: Radius of gyration of the gross section about the Y -Y axis. Effective Properties lxx: Moment of inertia for deflection calculations based on "Procedure 1 for Deflection Determination" of the 1996 AISI Specification. X — + — Sxx: Effective section modulus about the X -X axis (strong axis) Stress = FY. ., f Ma: Allowable Bending Moment – Based on the effective section modulus and the allowable stress including the strength increase from cold -work of forming (AISI 7.2) where applicable. Ycg: Maximum distance from the outside of the compression flange to the center of gravity of 9 the effective section. Y Torsional Properties J: St. Venant Torsional Constant 1 Cw: Torsional warping constant. Xo: Distance from the shear center to the centroid along the principal X -axis. Ro: Polar radius of gyration about the centroidal principal axis. R: 1 – (Xo /Ro) 5 3 J Kwik -Brid e Punch Steel Stud Manufacturing C a. The New Kwik - Bridge Punch • • • . Patent #5,943,838 What is a Kwik- Bridge Punch? e Punch is a unique hole punch design, which leaves a tab to fasten your lateral bridging to. Kwik - B rid g What does a Kwik- Bridge Punch do? Kwik- Bridge Punch allows you to secure lateral bridging in steel framing without the use of angle clips. Why should I use a Kwik- Bridge Punch? He Kwik- Bridge Punch should be used wherever lateral bridging is required, saving you time and material, which ring a real saving to the "bottom line ". /1 U- CHANNEL . CONT. 1 1/2" co 4 41 M ily —yam • 1 „ SCREW ATTACHMENT PUNCH DIMENSIONS CONNECT DETAIL • 4 S -STUD • KWIK BRIDGE PUNCH SYSTEM t THE NEW K1NIK- BR IDGE P UNCH PATTENT #5,943,838. Punch can be used in conjunction with the SSMA Technical Note # 1, "Single Deflection Track Selec- The Kwik dri�ge "Unsheathed Flange Gracing . 49 tion" and SSMA Industry Note # 2, I SCAFC® Steel Stud Manufacturing Co. . Typical Details 14) Cold Rolled lateral Bracing Wall Stud Web Stiffener Track Note: Stud depth 8" max. 414/ w' Web Stiffener r. Stud Clip Angle /� Length = Stud Depth — 1/2° 14k Flat Strap Lateral Bracing t ' a Track Blocking A 1 Wall Framing • . 4i 0 I 4 Flat Strap 1 Note: All connections to be designed. k_ . 53 • Project No. Sheet No. DIBBLE ENGINEERS, I NC. os-a v Project • S�Q� u Date 5 I' q Subject GC9rJ 14A B y TW • • A-2cek rte, a-- , HIGH GLOSS WHITE BRAKE METAL • HIGH 61-055 WHITE PROVIDE SHEET - PRIMED HIGH 6 1-055 WHITE BRAT . .77 BRAKE METAL WHITE AT AREAS OF ICON MET POSTERS 4 I - I . I 6Y /. BD. ON 2 -I/2' 20 VT 6Y /. BD. ON 4• 6A. METAL STUDS 9 Ib' OL. METAL STUDS PROVIDE 5HEET - PRIMED HIGH 61-055 WHITE BRAKE WHITE AT AREAS OF ICON METAL HIGH 6L055 WHITE POSTERS BRAKE METAL HIGH GLOSS WHITE NOTE. NO FIRE RETARDANT BRAKE WOOD /COMBUSTIBLE 10' 5'-0' 10' MATERJAL TO BE USED AS BACKIN6OR BLOCKING IN WALLS OR CEILING 1NALL DETAILS = I' -0' • • ✓ - 1•012) r 3s I C9 ‘/` / - I t "K., u 9 tRA �, c 5 S PS-7 I 1,L PLC I "Z S lCeZ �5 • it .: -tc,0 Sim, 6- L�-Z� O.qS (7 W Z`I 4x ` -3g (-T -r2-Au� L.)/ L?) / OLDY)50 — 59 -5)() t'-1 to.'S , I •0 I , ./evz -5 „Cnk ✓ �� = 2..33xZ V.0(.0 T 1,3 alL run� -tot t- /S 711‘ Z - 31, 4 ? S- �q. e4 1( Project No. Sheet No. D ENGINEERS, INC. 08. -m-3- Project Date L 1 •.9A LA-- 3)19 08 Subject By j $4-7 �,-0 e 14 - 4ew►.1 ea 5 7.-co -4 S lC _u. t....5-¢ - L) c. g oo s a 4 P1 C tom'` e/c, t34G (/ s- LoiN — Lc'- t , HetittHA L —seam n ) LI I dip- CD 19 a Li '-' C') — yL it`d' r /TLr -7V goi..4-4 -/v-P Les?v eJ - 0:3.0+4r •‘-r4044. c--4,A cT (...A OJT WV S 3L ■) t...) / '►et_._ N t:C — . s�+t7 e.,... / r—e., MI • . !.i • :Al OF DETAtt I L 3. 3. L 4 v 3 x `•• "'•• •• `"�-' • � I L4.3..q.L.cv � e6 , -6 - a 4 I 4 SAMB © AS I - i I - . CG G=B' .SAME AS L 4.4v4 .. • i • T / ON Q 5 ECT /OIl! 4 SEC T /ON Q • i • . • �• y I. OU J I i y2 tiI - I. � • .� _\ _ ' S IB 1 r c „ ci4i+r i • 1 TUBE B • 4 (FUT) „_.I 12. 7:16E5 6.6. ®-7;.4. (`. 1 " ' 1 ./ 6-3N) . • • • '' zi °� , I / I I I N I I I N N L� —I— _. __ — L� T(IDfI 6 a 4. (� I C 22�G -I I .I-----I— 1 � I-- 1........................„.. f [ ' ' ' ! 2 -TU8E3 6.6,.4 I = 7.30'•0-'. I :.3o' -o 7 .'20 %o'_ I 90' -O TYP/ CAL MALL CANOPY. STRUCTURAL. P.R A • M /NG t'flVAhL P FILAktll laCt • • - cow./ ds OOTT. . - _ 5 v � '- - -" PANEL Po/YT I . rr ' j ,� -- - Pc r -t- - • f 1 1104 V-4 -6 161 - - F ' . _ _ • .. . a r / fir - sa 5t C3 1 2.6 R 2 o I *'.1 . . .._ . . _ 1 .1 r . .______:_, 5 7 Jo/or ---. , • Tr p --- w10.8/.A.) MOOF / TAWS, • I P 1 7L 6' o.c. L5 .3 3 1 c CF 0.C. TUBE Eixa .4 TOEE Li .4.'9 . 7 , .-- ! / --/ ; 7 • 0E0 , /, • • 14.por ! • c i . x /0.5- - 5104.6 FODN ac III C. /0.5 € 7 / / ' / / cC • i 1: .9 . 2 . 44 LLV. COAR: C4 A 5.4 7:6 . . C4r 54 pew I e 7: G:ac. / / - r ,I , ' l I L. faRaFvezARF .11!9 Lx '/ rt ill N iffill I 1 i , , e al to, 1 / i -71105...6%G'i if ' ) I I 1 I .. •• _ L 3 . 3 . e; 1 I N . 1 _J A- 1 J.72;-A2..,;•. II - • on —.............72M 111F•!_.!Dlow, . ••°' — 7V3 4 3 x 4 (I comr , TOOC 8.4 .., coNr. 101 • S E CT /ON 4112k — . - w 1/2- /Lo- %EP G' MA SOA/RY WALL SEC ARCA" OAVG S. POR SPECIFICS. 1 2 OR 40. LicLTED CONN. 1 01# . Z . :L . 5 5 41 (LLV) DIAG. . , BRACH 40 A OOF $ 1 0 111 • • --- --.... N. I I I I \ . i I • T --- : - .., -- : IM"- - 1 ra■gi ::: i, .--. . 0 COM T 111 A. I 1 DO • 4 AT MAS. WALL. „ h _ C 0 AI ID L 7 / 0 N •AT. COLL/MN I . . , • C . 5.4..6 . . • _ Ei ----- - i w � - I ,i vve :'y r to: ...i Y•:•v... . • I w • , ..... -- _• ...� ���__.__� -._- f ' • _ _ ___ "� 14 rlwiui • .:l• - '•dawv� I I I 1 1 • _ •1! ofaY 2221 .' • la ° .o573a: • 13 ;• •\ . • • ina7 l.bi iv d.as; 1 - va - n, :./.....• I 7M.1 aL V]1t -L O:.71r1. I lanil ll . f .o..c ]ivaal• V,.1 '•1P! ODGIW. 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O.O•.5 ?Sae. 1 1.: • 'dADq .a]Ln Si C • ,y� T I I ' , g. a •On a cY �� S S co ° j aeoa •l16 rib •. pl 'I"— a Ta i3 . ng <y @ 'moron / Pd - roPhL� !•I. �: - • ?Oil 'LS y1 7W 1 / 1ib W r9 ,91s I I • sa . • L rye I nii +". _ . - — -•-- - > � -''- • • • • '��M' •IlH3 '�6'wa0l�nlLS • •o I alto ;a ax • �--- roanv • 9nvtaowri :wdan6 _ lybnlo ntlO22S. _ `. II \ 011// O y ONIaYLOI I / I _ l wanCntlLLOa C / - • o I ^ � DN1�vao l • pvJitNOO K77 n W I r ya i'LaVd 1 ! 3S .1..,,,,,,,, .1..,,,,,,,, .1..,,,,,,,, • I /, jp io no v�d� I • 1V1.W 1:3M6 i O L - I • < . / r dAO vo aaRa•rd 1 ? t O3.O n9./.1.W .. Ll . - — �Zhl o n ngN1 Otgta 'r • ,• :•1 --yq++ 4.`V.O Oooa an -i•Itn I �" . _ T I - • . •/ , T . • C;Oy ,O I _ luvnt7.0 , - b a • • • • r . , . r-- iti‘../ Q _ exa K'lerSTL.. e 5100 3TRt1 cr �0 ` " H+E ,r. �ru c s . , • z� o.t. Ica 11. Ck Ct �Yt OOO BOARDS I FlR�rR��t'Eo) 5FCURETO �/� CYF. 6 00°,140 vas r / ADHEStVE.CVT `o . . / , I • E X1ST !_, �IJ, ` .� LINE Y OFGp. . . S 4c)C.TUR.(- 5 aCEtL.3ENtND 1 I e ms— - --.a �• _ _ _ - • , I • � a { l � GYP. 5 D. I CME.T <AlioS = . I I -" ' P _ e u 2Qr'. 5t M STIWCT N A l WI. sLSP JWEO a''4 KU "5Tt_.Tv19r • - _. :E1LTt11C.7 /1.1.C• set STROCT 3Y.rEtiANr) . I. ' S i- Tb�� -to" - - _ '� t . 1 ! 2...... I � • ' t t' I Project No. Sheet No. DIBBLE ENGINEERS, INC. cog -cxo9 Project Date pAyi.cs5 SrioC 3,124.4 si „tee, Subject "7.0ti6 FR• @n.rr nuns ‘stswrtot J By - 5 (- Z corvkiiStot- S -0 I'M ace ok... , � r Low — 3 6) j Taw 3 N. r,s SC Fasteners (S and Welds) Steel Stud Manufacturing Ca. Screw Table Notes 1. Screw spacing and edge distance shall not be less than 3 x D. (D = Nominal screw diameter) 2. The allowable screw values are based on the steel properties of the members being connected, per AISI section E4. 3. When connecting materials of different metal thicknesses or yield strength, the lowest applicable values should be used. 4. The nominal strength of the screw must be at least 3.75 times the allowable loads. 5. Values include a 3.0 factor of safety. 6. Applied loads may be multiplied by 0.75 for seismic or wind loading, per AISI A 5.1.3. 7. Penetration of screws through joined materials should not be less than 3 exposed threads. Screws should be installed and tightened in accordance with screw manufacturer's recommendations. Allowable Loads for Screw Connections (lbs/screw) .....,. •. e - �µ,a- -,, oi1 i,1 I -,, {YV1 fm` II ,,I Ki:! iI V+ ;I If, Steel y Vrirtlek es§l r . pe Skis Pror le • ).- e - I 16 %(Int DIa 0190 (19) ,,,{{ I.ti ' iai 0164'(In =' �a S , DJa M (in) . `•MIli 1r•,Desl : in:..ffi "; ks :� Fu' ksl < S ea R out• Sheay r- 7610Viibut r :':S' - ' >..she:: ar ,'%Pullout.:, 18 0.0188 33 45 - : - - --- 77:77. --1- ; - .. . 60 33 27 0.0283 33 45 II • • 111 50 30 0.0312 33 45 151 76 129 55 33 0.0346 33 45 : - .: , I 177 84 164 ay 151 61 43 0.0451 33 45 280 124 263 109 224 79 54 0.0566 33 45 394 156 370 137 ; , _ y 68 0.0713 33 45 557 156 523 173 _ .. . ; Weld Table Notes 1. Weld capacities based on AISI, section E2. 2. When connecting materials of different metal thickness or tensile strength (Fu), the lowest applicable values • should be used. 3. Values include a 2.5 factor of safety. 4. Based on the minimum allowance load for fillet or flare groove welds, longitudinal or transverse loads. 5. Allowable loads based on E60xx electrodes 6. For material less than or equal to .1242" thick, drawings show nominal weld size. For such material, the effective • throat of the weld shall not be less than the thickness of the thinnest connected part. Allowable Loads For Fillet Welds And Flare Groove Welds ' rTi = „~ ` Ihl '1;Ieis - ' `Terlslle %;r 5 E60XX Electrodes ) rF:t'il : i �i ' „' 'MII .•liri.M.�':u',wr$k$li:- �ksh +�-•'.:•,':,�: ,Lt:::•Ibs11n; •�` 43 0.0451 33 45 609 54 0.0566 33 45 764 68 0.0713 33 45 963 97 0.1017 33 45 1373 118 0.1242 33 45 1677 54 0.0566 50 65 1104 68 0.0713 50 65 1390 ` 97 0.1017 50 65 1983 118 0.1242 50 65 2422 48 DIBBLE ENGINEERS,INC. PAYLESS SHOE SOURCE - STORE #4841 STRUCTURAL CALCULATIONS TIGARD, OREGON SECTION 3 HUNG CEILING SYSTEM - BRACING 1 1 1 Project No. Sheet No. DIBBLE ENGINEERS, INC. - l B y Project Date Subject ac:?/ �o .-J &i AGS5 / Con /izs 5, 0 ...N B lzn c.x _ .j ca., P TI -- f12-c vloS ll%hT (-ow; rx,Ft.St arm '+V ,E,YL- Tv As-,5 iST V a-r. GohlPo,- +s... of sue)sM1a -,:.jLC. S055 CL, i, Ja, 0. sI4 -' CIArEi -IA Z. oc'( SL3L) 7 L.VA V .4 P Pz - As cg • - oSs - nvra i'3e5 -' �OILGSS (_)E A sc.E . 4' -G�E c -1 . 1oe - (3. 3.1 r VV Sri c40.- c. fkir z.rst' , -)1.-`1 E = o. 2 5, D . ?� S,, S c I. 50 r /YJAX j Ev 2Psf1 . .0 0..)V6RT Yo Asa-- ST,2 DEs ii„. P - o - - - I . I f a D. Q.4 {;' sr=I / Dasm,J FaA- 12 x /2 ' 4,2,1,0 r AzsA '"- I41 4 F7 MA* /f_ /z./ / Project No. Sheet No. Date DIBBLE ENGINEERS INC. os -- .7 Pro Subject By 1: . Gor7-7PRa_ssi o,-.N 3sz-044" /ze2 -/e (l KI x - 1 I -P .,, R o,441 IA : L►+)ax = 2ac:' ,/ C+fEc Ic s772c. -39Th4 e 1 v - . A vgE /La tzs -!'e VP T ,, 7 o" SLF 1-rr = I.9 # For: Ca-1,i, vr 1 9kAg. C A P . = 0 1= " /? p CFS Version 4.14 Page 1 'L� Section: Section 5.sct Channel 1.625x1.25x0.25 -25 Gage ♦ - Section Inputs Material: A653 SS Grade 33 No strength increase from cold work of forming. Modulus of Elasticity, E 29500 ksi Yield Strength, Fy 33 ksi Tensile Strength, Fu 45 ksi Warping Constant Override, Cw 0 in ^6 Torsion Constant Override, J 0 in ^4 Stiffened Channel, Thickness 0.0188 in (25 Gage) Placement of Part from Origin: X to center of gravity 0 in Y to center of gravity 0 in Outside dimensions, Open shape Length Angle Radius Web k Hole Size Distance (in) (deg) (in) Coef. (in) (in) 1 0.2500 270.000 0.084300 None 0.000 0.0000 0.1250 2 1.2500 180.000 0.084300 Single 0.000 0.0000 0.6250 3 1.6250 90.000 0.084300 Cee 0.000 0.0000 0.8125 4 1.2500 0.000 0.084300 Single 0.000 0.0000 0.6250 5 0.2500 - 90.000 0.084300 None 0.000 0.0000 0.1250 CFS Version 4.14 Page 2 t+ Section: Section 5.sct Channel 1.625x1.25x0.25 -25 Gage Member Check - 2001 AISI Specification - US (ASD) Design Parameters: Lx 7.0000 ft Ly 7.0000 ft Lt 7.0000 ft Kr. 1.0000 Ky 1.0000 Kt 1.0000 Cbx 1.0000 Cby 1.0000 ex 0.0000 in Cmx 1.0000 Cmy 1.0000 ey 0.0000 in Braced Flange: None Moment Reduction, R: 0.0000 Loads: P Mx Vy My Vx (k) (k -in) (k) (k -in) (k) Entered 0.12100 0.00000 0.00000 0.00000 0.00000 Applied 0.12100 0.00000 0.00000 0.00000 0.00000 Strength • 0.12495 0.36060 0.30219 0.11509 0.48568 Effective section properties at applied loads: Ae 0.082512 in ^2 Ixe 0.038591 in ^9 Iye 0.017467 in ^9 Sxe(t) 0.047497 in ^3 Sye(1) 0.037385 in ^3 Sxe(b) 0.047497 in ^3 Sye(r) 0.022313 in ^3 Interaction Equations AISI Eq. C5.2.1 -1 (P, Mx, My) 0.968 + 0.000 + 0.000 = 0.968 <= 1.0 AISI Eq. C5.2.1 -2 (P, Mx, My) 0.118 + 0.000 + 0.000 = 0.118 <= 1.0 AISI Eq. C3.3.1 -1 (Mx, Vy) 0.000 + 0.000 = 0.000 <= 1.0 AISI Eq. C3.3.1 -1 (My, Vx) 0.000 + 0.000 = 0.000 <= 1.0 Full Section Properties Area 0.082512 in ^2 Wt. 0.00028054 k /ft Width 4.3889 in Ix 0.03859 in ^9 rx 0.6839 in Ixy 0.00000 in ^9 Sx(t) 0.047497 in ^3 y(t) 0.8125 in a 0.000 deg Sx(b) 0.047497 in ^3 y(b) 0.8125 in Height 1.6250 in Iy 0.01747 in ^9 ry 0.4601 in Xo - 1.0790 in Sy(1) 0.037385 in ^3 x(1) 0.4672 in Yo 0.0000 in Sy(r) 0.022313 in ^3 x(r) 0.7828 in jx 1.3187 in Width 1.2500 in jy 0.0000 in I1 0.03859 in ^9 r1 0.6839 in I2 0.01747 in ^9 r2 0.4601 in Ic 0.05606 in ^9 rc 0.8243 in Cw 0.010185 in ^6 Io 0.15212 in ^9 ro 1.3578 in J 9.7210e -06 in ^4 Project No. Sheet No. Date 1( DIBBLE ENGINEERS, INC. _ ai;: � Project Subject B y �(4 S r✓/71.4, - •02 B2Ac (pc-A7a1C) a /2 � pc- MAy_ 4ZGTI CPA(?) rv,JF /G,urLATlo MAX Lam►- 1 5 - 1 - 1 - I /_,,, / ,z5 /zS -/S E (1 's " „/''A' z `) ( lipzsl2s -le , 9,l &(2)/ ;) // k ' ` Z t) (z) ZS-05 /76-IS E 1 /6,- 10., C() V /Zux / i/It''K Z5 ) (2.. 3(ozsibt -33 E 1 z / - Z , (.6.7-) ).1c5)- D An M oc -rlPw M`m3Vs - foelz1+6Iz a ( W' 4 6x'/2 ” 5cf1■ws a 162110c Project No. Sheet No. DIBBLE ENGINEERS, INC. 6g ... 06 1 Project Date Ryti65 Subject B y Co.7-7PR &sry to .-J gR AGS" ,s ri o._l FR-o ✓IOS" 1/15:11-1 Gores a r-S M 6.N'J38 iST V O— Gcrrr(7dr-'s -rr of SVI SPA I a• 11:21re -s SVSP 0-£4,44G CfZ.IrEn.•.4A Zoe ' sLc- Mr. LoA l� 4 4 P4r A -ate s it --" �►.► ('✓- .5 Gti, l POn GSs OSE ASCE -o5 c:r7 13 I v..) c-7 E 0.2 SO5 7 ( , S 7- I. I MA>e D = 4Psf j Ev= 1.2 PsF .0 p,-)V50-1 T Au-.26- STIFf D r\ o -- .0s, 41 �c55l5.., op- 1 2. x /2 ' lvvL�v / flzsA /41 PIA )4 Project No. Sheet No. r DIBBLE ENGINEERS, INC Project Date P4Vif$? Subject B y Co m PR =s`a o�-► t3izaca (2 7 /19 2.5/25 /0 (0.-)/*k OA ZS ) _ #(o Scrr.Er,J _______...DE e gp "o c mix ° R = O. IpE5 Re.Fer ATT"cHt 2 L 0144e = 2'f L IV)A W : I O Cf Ec-4 Srx2-a■-b5 -rm c co '--c9 " of - /IL 1 417Ac.H &s U Z2) 1b2 /25 up -7-. lO/ -9 • Sei-FW7 =5'8 •= . 50,r 6 - rt.,/,, , 0,1(.7_,(.., 5,4,,,,,„r S cAP = Z�Ca - /ZZ ®� d� • CFS Version 4.14 Page 1 Section: Section 6.sct e • Double Channel 1.625x1.25x0.25 -25 Gage • n J Section Inputs Material: A653 SS Grade 33 No strength increase from cold work of forming. Modulus of Elasticity, E 29500 ksi Yield Strength, Fy 33 ksi Tensile Strength, Fu 45 ksi Warping Constant Override, Cw 0.045764 in ^6 Torsion Constant Override, J 0 in ^4 Connector Spacing 0 in Right Channel, Thickness 0.0188 in (25 Gage) Placement of Part from Origin: X to left edge 0 in Y to center of gravity 0 in Outside dimensions, Open shape Length Angle Radius Web k Hole Size Distance (in) (deg) (in) Coef. (in) (in) 1 0.2500 270.000 0.084300 None 0.000 0.0000 0.1250 2 1.2500 180.000 0.084300 Single 0.000 0.0000 0.6250 3 1.6250 90.000 0.084300 Double 0.000 0.0000 0.8125 4 1.2500 0.000 0.084300 Single 0.000 0.0000 0.6250 5 0.2500 - 90.000 0.084300 None 0.000 0.0000 0.1250 Left Channel, Thickness 0.0188 in (25 Gage) Placement of Part from Origin: X to right edge 0 in Y to center of gravity 0 in Outside dimensions, Open shape Length Angle Radius Web k Hole Size Distance (in) (deg) (in) Coef. (in) (in) 1 0.2500 - 90.000 0.084300 None 0.000 0.0000 0.1250 2 1.2500 0.000 0.084300 Single 0.000 0.0000 0.6250 3 1.6250 90.000 0.084300 Double 0.000 0.0000 0.8125 4 1.2500 180.000 0.084300 Single 0.000 0.0000 0.6250 5 0.2500 270.000 0.084300 None 0.000 0.0000 0.1250 CFS Version 4.14 Page 2 Section: Section 6.sct Double Channel 1.625x1.25x0.25 -25 Gage Member Check - 2001 AISI Specification - US (ASD) Design Parameters: Lx 10.750 ft Ly 10.750 ft Lt 10.750 ft Kx 1.0000 Ky 1.0000 Kt 1.0000 Cbx 1.0000 Cby 1.0000 ex 0.0000 in Cmx 1.0000 Cmy 1.0000 ey 0.0000 in Braced Flange: None Moment Reduction, R: 0.0000 Loads: P Mx Vy My Vx (k) (k -in) (k) (k -in) (k) Entered 0.06100 0.00000 0.00000 0.00000 0.00000 Applied 0.06100 0.00000 0.00000 0.00000 0.00000 Strength 0.55383 0.66221 0.60439 0.55172 0.97136 Effective section properties at applied loads: Ae 0.16502 in ^2 Ixe 0.077183 inA4 Iye 0.070955 inA4 Sxe(t) 0.094994 in ^3 Sye(1) 0.056764 in ^3 Sxe(b) 0.094994 in ^3 Sye(r) 0.056764 in ^3 Interaction Equations AISI Eq. C5.2.1 - 1 (P, Mx, My) 0.110 + 0.000 + 0.000 = 0.110 <= 1.0 AISI Eq. C5.2.1 -2 (P, Mx, My) 0.030 + 0.000 + 0.000 = 0.030 <= 1.0 AISI Eq. C3.3.1 - 1 (Mx, Vy) 0.000 + 0.000 = 0.000 <= 1.0 AISI Eq. C3.3.1 -1 (My, Vx) 0.000 + 0.000 = 0.000 <= 1.0 Full Section Properties Area 0.16502 in ^2 Wt. 0.00056108 k /ft Width 8.7779 in Ix 0.07718 inA4 rx, 0.6839 in Ixy 0.00000 inA4 Sx(t) 0.094994 in ^3 y(t) 0.8125 in a 0.000 deg Sx(b) 0.094994 in ^3 y(b) 0.8125 in Height 1.6250 in Iy 0.07095 inA4 ry 0.6557 in Xo 0.0000 in Sy(1) 0.056764 in ^3 x(1) 1.2500 in Yo 0.0000 in Sy(r) 0.056764 in ^3 x(r) 1.2500 in jx 0.0000 in Width 2.5000 in jy 0.0000 in Il 0.07718 inA4 rl 0.6839 in I2 0.07095 inA4 r2 0.6557 in Ic 0.14814 inA4 rc 0.9475 in Cw 0.045764 in ^6 Io 0.14814 inA4 ro 0.9475 in J 0.00001944 inA4 I Project No. Sheet No. • DIBBLE ENGINEERS, INC. ce.- Project Date Is 77= By -2-0) Subject y Gor�,o4�sro, -► t3 rz,a,Gx • S 4.411) 1 1A1? - 1 �_.� -- ..... 'FO/Z. 2Ac• 'L0:7O e /2 —o pt MAC_ E""r/ aA (' NiAX L== r -+4TF1 /62-5/Z5--/e I: „ ( 'vex I lY "u z - r---� Io/ -9" l�zslzs –iB (CZ) / " x II("xZSa) (z) 25b5/ZS -/S /L'- /o „ (C7)ar, ")-Ilis'Y Zs-� (2, 3(0ZSILDZ -33 7-4 -Z d v.1 c7rz ArrAc.fi Muc- 7"1Prrc, M GM - 1 - 04C - 1146 iL a t.O w' ' to K /2- " Sc-41-:WS a l(a « oL • Project No. Sheet No. • DIBBLE ENGINEERS, INC. -&,/ ri Date Project P ILS5 T� Subject By C.e3rr7PRGsb to .-1 13 ACE - G C7Mf , ? io 5/2-"C.2 - DES crz-IP �rZO Prt.rxst TEJ 124: (- vJ�7". Gm+1Po. -1 s a dF Ste? SPA I mazes S-' e-ElUh16 0syr4,-1 C II.I TE MA ooh =2.4 I4 ' LOA fOaLSS cuss P,sc.L �-s�r- sic,- rmo..► l: Ve.rm pv,143.r U..) E z 0.2 S D s r i , $ s - I.50 / MA)z D. 4psr j v = 1.2 Psr .Cc .Jysrr-7- ro A-- - ST #S DES Ili r �- O. +6 . O. 64 �5 fr DE's 4,- D 1 4 r...1 yO, r2 K !2 r•io / " A = I F PIA " / p: /z1 Project No. Sheet No. DIBBLE ENGINEERS, INC• / IL-- P roject Date . Subject By Go, P 11..sS sioJ Base \ 2) 2S-c7.5/ (2)Z1V).1y4-c h x Z57") }f 1 Rx _ I. of l ,.- (use 54. ftxe,) L.ikhc,r = Zoor C#L r-- S1123 7+1 t Jt.. I -ID Peg- ATTa c 46 . (..)g (2) 2505/25 -/Q vP 'v /La / 011 9/z- pkf-._.,rc -/---f /4i,-/ St/..r WT = // u40,,y5,0 fvG.-- ove.e.. = /2'• oK z,42 G,P = Z ze,/ _ CFS Version 4.14 Page 1 l3 Section: Section 4.sct Channel 2.5x1.25x0.25 -25 Gage ♦ IC I — J Section Inputs Material: A653 SS Grade 33 No strength increase from cold work of forming. Modulus of Elasticity, E 29500 ksi Yield Strength, Fy 33 ksi Tensile Strength, Fu 45 ksi Warping Constant Override, Cw 0 in ^6 Torsion Constant Override, J 0 in ^4 Stiffened Channel, Thickness 0.0188 in (25 Gage) Placement of Part from Origin: X to center of gravity 0 in Y to center of gravity 0 in Outside dimensions, Open shape Length Angle Radius Web k Hole Size Distance (in) (deg) (in) Coef. (in) (in) 1 0.2500 270.000 0.084300 None 0.000 0.0000 0.1250 2 1.2500 180.000 0.084300 Single 0.000 0.0000 0.6250 3 2.5000 90.000 0.084300 Cee 0.000 0.0000 1.2500 4 1.2500 0.000 0.084300 Single 0.000 0.0000 0.6250 5 0.2500 - 90.000 0.084300 None 0.000 0.0000 0.1250 CFS Version 4.14 Page 2 i Section: Section 4.sct Channel 2.5x1.25x0.25 -25 Gage Member Check - 2001 AISI Specification - US (ASD) Design Parameters: Lx 16.900 ft Ly 16.900 ft Lt 16.900 ft Kx 1.0000 Ky 1.0000 Kt 1.0000 Cbx 1.0000 Cby 1.0000 ex 0.0000 in Cmx 1.0000 Cmy 1.0000 ey 0.0000 in Braced Flange: None Moment Reduction, R: 0.0000 Loads: 2 Mr. Vy My Vx (k) -in) (k) (k -in) (k) Entered 06 000 .00000 0.00000 0.00000 0.00000 Applied .06000 0.00000 0.00000 0.00000 0.00000 Strength .0642 0.12601 0.25777 0.05836 0.48568 Effective section properties at applied loads: Ae 0.098962 in ^2 Ixe 0.10182 in ^4 Iye 0.02034 in ^4 Sxe(t) 0.081452 in ^3 Sye(1) 0.052010 in ^3 Sxe(b) 0.081452 in ^3 Sye(r) 0.023684 in ^3 Interaction Equations AISI Eq. C5.2.1 -1 (P, Mx, My) 0.935 + 0.000 + 0.000 = 0.935 <= 1.0 AISI Eq. C5.2.1 -2 (P, Mx, My) 0.057 + 0.000 + 0.000 = 0.057 <= 1.0 AISI Eq. C3.3.1 -1 (Mx, Vy) 0.000 + 0.000 = 0.000 <= 1.0 AISI Eq. C3.3.1 -1 (My, Vx) 0.000 + 0.000 = 0.000 <= 1.0 KL /r exceeds 200. Full Section Properties Area 0.098962 in ^2 Wt. 0.00033647 k /ft Width 5.2639 in Ix 0.10182 in ^4 rx 1.0143 in Ixy 0.00000 in ^4 Sx(t) 0.081452 in ^3 y(t) 1.2500 in a 0.000 deg Sx(b) 0.081452 in ^3 y(b) 1.2500 in Height 2.5000 in Iy 0.02034 in ^4 ry 0.4534 in Xo - 0.9479 in Sy(1) 0.052010 in ^3 x(1) 0.3911 in Yo 0.0000 in Sy(r) 0.023684 in ^3 x(r) 0.8589 in jx 1.5099 in Width 1.2500 in jy 0.0000 in I1 0.10182 in ^4 rl 1.0143 in I2 0.02034 in ^4 r2 0.4534 in Ic 0.12216 in ^4 rc 1.1110 in Cw 0.024828 in ^6 Io 0.21108 in ^4 ro 1.4604 in J 0.00001166 in ^4 • I Project No, Sheet No. DIBBLE ENGINEERS, INC. -c: .: Project Date Subject B y • S I - 7�0/L Pi2A« 6.s=•‘..-A71.0 e /2 —o pc_ MAX ECT/ a,�(s C O3-.1pi&ru 0-a,-rro, --+ MAX Lsr-+' rH IVe' "x ZStr: ( a,zs /zs -/8 ((2)17a "x / /'i )cZ5cr) 2St;051 5 lb'- o" £s/5t zsr) (9 36ZSIDZ - 33 1 C(2)3Velc 1 5 797"K?' � -- oTES V 47TAc H M u r_rr pc o 01 wML, ,s2‘ 1o',11 IL a (AD ee, w ) 4 6 K. " 5c4 Ew a /(A flat- Project No. Sheet No. DIBBLE ENGINEERS, INC. e8 _ e6 ,1 Project Date Plit/I-FS 77= Subject By T4 PREsS 10.-1 4SR ,4co� Dzsc2.�PTi�� {'R-o ✓iQS etz • s4 a rm /Y16- -7 EK- 7 j�SS P VJ 21 Gompo, -4 is- .-T dF SS/ sr.MG' l•):::./ S(.1SP C-E-IU4(o ass 4. an-IT-EA-4 A Z o o(p sly �- ASCL c PSF pc, • 13. I VEOn cap 'P0- E.-3T o..) -1 o. 2 S •r$ =1.50, MAC D J Ev = 1.2 PsF .a p d y6rr-7 - 7 - 0 A Ur" + STAZS 1)45".5 o. :'M i p o. Ps r' D0614,1 l Z/ K /2 ' 4tiro A zzp, HA/ F-r2- MA /pr. /Z/4. I INC Project No. Sheet No. 1( DIBBLE ENGINEERS, c - °� !7 Date Project Subject By /�i __ , (2 35/1Z- (Z 3g "xi *mK7_1(:) -. #(9 c-iz.so 1 ^ , — •F 1 X X °. i' fr'' ,ti (UV.. go< 5 S) �{.! ,' 2n1Au = 2 Z i CFFsatc- 5 -■57+1 74 2 PP.r_ PTTlc -t4Efl (J5E 6273Ut /L - ?3 ve Tv 2'' -2: *CP Sc r Q c lc s wT = 3 9' e u 1 dy5`"pf 3- P ?vt..-av ✓- c Iq/ Vey -. j ; f-,./U irzE.Par-o --.P.,(....ac( , R— 04P a Z.) /5Z, 3 CFS Version 4.14 Page 1 11' Section: Section 1.sct Channel 3.625x1.625x0.5 -20 Gage 1 ♦ --}-- J Section Inputs Material: A653 SS Grade 33 No strength increase from cold work of forming. Modulus of Elasticity, E 29500 ksi Yield Strength, Fy 33 ksi Tensile Strength, Fu 45 ksi Warping Constant Override, Cw 0 in ^6 Torsion Constant Override, J 0 in ^4 Stiffened Channel, Thickness 0.0346 in (20 Gage) Placement of Part from Origin: X to center of gravity 0 in Y to center of gravity 0 in Outside dimensions, Open shape Length Angle Radius Web k Hole Size Distance (in) (deg) (in) Coef. (in) (in) 1 0.5000 270.000 0.076400 None 0.000 0.0000 0.2500 2 1.6250 180.000 0.076400 Single 0.000 0.0000 0.8125 3 3.6250 90.000 0.076400 Cee 0.000 0.0000 1.8125 4 1.6250 0.000 0.076400 Single 0.000 0.0000 0.8125 5 0.5000 - 90.000 0.076400 None 0.000 0.0000 0.2500 CFS Version 4.14 Page 2 , . Section: Section 1.sct Channel 3.625x1.625x0.5 -20 Gage Member Check - 2001 AISI Specification - US (ASD) Design Parameters: Lx 24.170 ft Ly 24.170 ft Lt 24.170 ft Kx 1.0000 I <y 1.0000 Kt 1.0000 Cbx 1.0000 Cby 1.0000 ex 0.0000 in Cmx 1.0000 Cmy 1.0000 ey 0.0000 in Braced Flange: None Moment Reduction, R: 0.0000 Loads: ,' Mx Vy My Vx 4, (k) (k -in) (k) (k -in) (k) Entered 0.1210 0.00000 0.0000 0.00000 0.0000 Applied 0.1211 0.00000 0.0000 0.00000 0.0000 Strength 0.1 5 0.51678 1.0236 0.29448 1.2015 Effective section properties at applied loads: Ae 0.26212 in ^2 Ire 0.55125 in ^4 Iye 0.09936 in ^4 Sxe(t) 0.30414 in ^3 Sye(1) 0.18504 in ^3 Sxe(b) 0.30414 in ^3 Sye(r) 0.09132 in ^3 Interaction Equations AISI Eq. C5.2.1 - 1 (P, Mx, My) 0.722 + 0.000 + 0.000 = 0.722 <= 1.0 AISI Eq. C5.2.1 -2 (P, Mx, My) 0.034 + 0.000 + 0.000 = 0.034 <= 1.0 AISI Eq. C3.3.1 -1 (Mx, Vy) 0.000 + 0.000 = 0.000 <= 1.0 AISI Eq. C3.3.1 - 1 (My, Vx) 0.000 + 0.000 = 0.000 <= 1.0 KL /r exceeds 200. Full Section Properties Area 0.26212 in ^2 Wt. 0.00089121 k /ft Width 7.5757 in Ix 0.5512 in /4 rx 1.4502 in Ixy 0.0000 in ^4 Sx(t) 0.30414 in ^3 y(t) 1.8125 in a 0.000 deg Sx(b) 0.30414 in ^3 y(b) 1.8125 in Height 3.6250 in Iy 0.0994 in ^4 ry 0.6157 in Xo - 1.3066 in Sy(1) 0.18504 in ^3 x(1) 0.5370 in Yo 0.0000 in Sy(r) 0.09132 in ^3 x(r) 1.0880 in jx 2.0732 in Width 1.6250 in jy 0.0000 in I1 0.5512 in ^4 rl 1.4502 in 12 0.0994 in /4 r2 0.6157 in Ic 0.6506 in /4 rc 1.5755 in Cw 0.28429 in ^6 Io 1.0981 in /4 ro 2.0468 in J 0.00010460 in /4 Project No Sheet No. DIBBLE ENGINEERS, INC. z� Project Date Subject B y Gorr,? I U 17A.c -X S - 702 1p4P+7 e /2 1 -0 MAy =.r.1 r0,.►Flay MA (--)-' ) 6z5,z5-_,e (' VA?' Y-25 r-) ( ) Iroz sizs -fie ~ I0",I L ..J FelHg t k XZSg.) (z) Z5.05I75-/a /L'- /0" (cC)V/z "'/90XZ5 ) (2.) 3(ozSICcZ -33 I + 1 _ (.,z) 3 * _ xl o F} rrAG I j M o C -TIP-& M apleemS 'IOe.j$T446 IL e (AD Era w) K' /2 SGiZ S C. Ila II aL Project No. Sheet No. D ENGINEERS, INC. � 9 � Project Date FA 4 I s 7±- Subject ))4 3 By --� ° 17 (//vf . I p o ASScdu,la r • l c,I ) .&."' : lo k. L`Z7 57u. ) — 71 -,--- (zzot, 7- -6 5 : . ---- _ 6, Cac7 ca-- ) = 2'7 65 c fr. 1 r,Oi V Q -' — c . yr ry S v 1Aveix, o S 13 fs os r_ .4 ..i4 ) . g - - / e , , ,,– ----- -- i;.-.1 : o ;5. —.q. o1( - - -1 6 t_a6,, (7-16117) . 3‘,T4 ..366( p-i.r) -= avp,-,F --› El = - .q. oliti /..e. f 4 `"•-• 1( Project No. Sheet No. D ENGINEERS, INC. � Z_ Project Date P s z S u b j e c t b ) l t r /4L 2 / - By • i‘citte, IZI 0-1' c,O- ,mss ; /4 >, OclZ c = Z {. � rc, ‘. 30 , l il) . (.e)G o . c��i - 3 c-rvs / atom' c • MCE Ground Motion - Conterminous 48 States Zip Code - 97223 Central Latitude = 45.44033 • Central Longitude = - 122.776223 Period MCE Sa (sec) ( %g) 0.2 106.1 MCE Value of Ss, Site Class B 1.0 037.2 MCE Value of S1, Site Class B Spectral Parameters for Site Class D 0.2 114.6 Sa = FaSs, Fa = 1.08 1.0 061.7 Sa = FvS1, Fv = 1.66 Spectrum for Site Class D Period MCE Sa (sec) ( %g) 0.000 045.9 T = 0.0, Sa = 0.4FaSs 0.108 114.6 T = To, Sa = FaSs 0.200 114.6 T = 0.2, Sa = FaSs 0.538 114.6 T = Ts, Sa = FaSs 0.600 102.8 0.700 088.1 0.800 077.1 0.900 068.5 1.000 061.7 T = 1.0, Sa = FvS 1 1.100 056.1 1.200 051.4 1.300 047.5 1.400 044.1 1.500 041.1 1.600 038.6 1.700 036.3 1.800 034.3 1.900 032.5 2.000 030.8 c % 0&)(1. Ctd) o Will ' Period, sec MCE Sa, g 0.00 0.459 Maximum Considered Earthquake Ground Motion 0.11 1.146 Site Class D Fa = 1.08 Fv = 1.66 0.20 1.146 Zip Code = 97223 Central Lat. = 45.44033 deg Central Long. = - 122.776223 deg 0.54 1.146 0.60 1.028 1.6 0.70 0.881 0.80 0.771 d 1.4 0.90 0.685 : O r 1.2 1.00 0.617' ��� 1.10 0.561 1.20 0.514 1•) AMIN NMI ma. simm 1.30 0.475 Q 0.8 �� 1.40 0.441 ���� C �� = 1.50 0.411 t 0.6 = I j ID = =C kW.- 1.60 0.386 0 0.4 1.70 0.363 LIJ C1 ! I I 1.80 0.343 • 0.2 I I I - 1.90 0.325 , 0 ._..._ 0.308 0 0.5 1 1.5 2 Period, sec 1