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Plans (98) \�.3 \k C perlo OFFICE���� ���� CONSTRUCTION JAGUAR LAND ROVER OF Subcontractor: ProSteel Inc. PORTLAND Submittal#: 106 Rev#: ,... ED Specification Section: 05 21 00 MAa'i 0 G NIB - C ARD Perlo Job Number: 1368 Date Submitted: 4/29/19 DiNG DiVi310t Submittal Item: Joist Calculations Please Respond By: 5/2/19 PROJECT SITE: PERLO CONSTRUCTION HAS REVIEWED THIS SUBMITTAL DATE 4/29/19 SIGNED Jake Jensen Jaguar Land Rover of Portland 10125 SW Washington Square Road REVIEW BY CONTRACTOR IS UNDERTAKEN SOLELY TO g a SATISFY ANY OBLIGATIONS OF CONTRACTOR TO OWNER Tigard, Oregon 97223 AND DOES NOT IN ANY WAY RELIEVE SUBCONTRACTOR FROM HIS OBLIGATION FULLY TO PERFORM ALL SUBCONTRACT REQUIREMENTS, NOR SHALL SUCH REVIEW APPROVER: GIVE RISE TO ANY RIGHT OF ACTION OR SUIT IN FAVOR OF SUBCONTRACTOR OR THIRD PERSONS AGAINST CONTRACTOR. REVIEW DOES NOT EXTEND TO Mildren Design Group CONSIDERATION FOR STRUCTURAL INTEGRITY,SAFETY, DETAILED COMPLIANCE WITH CONTRACT REQUIREMENTS Attention: Curt Trolan OR ANY OTHER OBLIGATION OF THE SUBCONTRACTOR. 7650 SW Beveland Street, Suite 120 SUBCONTRACTOR IS FULLY RESPONSIBLE FOR CONFIRMING AND CORRELATING ALL DIMENSIONS; Tigard, Oregon 97223 FABRICATING AND CONSTRUCTION TECHNIQUES; COORDINATING HIS WORK WITH THAT OF ALL OTHER TRADES;AND THE SATISFACTORY PERFORMANCE OF HIS GENERAL CONTRACTOR ENTIRE WORK IN STRICT ACCORDANCE WITH THE CONTRACT DOCUMENTS. Approver's Stamp: Perlo Construction City of Tigard Attention: Jake Jensen Approved Plans 11450 SW Amu Street Tualatin, Oregon 97062 By 9Date 3--- �- REVISION OR CCS 189243 1 LICENSED THROUGHOUT THE WESTERN UNITED STATES t--AZ ROC 293181 NEW MILLENNIUM BUILDING SYSTEMS April 29, 2019 To: Greg Hasenoehrl Prosteel,Inc. Project: Jaguar Land Rover Portland,OR NMBS Job#5618-0088 Re: Joist Calculations This letter is to certify that the steel joists and bridging supplied by New Millennium Building Systems,LLC for the above-mentioned project have been designed and manufactured in accordance with the current Steel Joist Institute standards and specifications, as well as with the specified design and loading information provided in the Contract Documents. New Millennium Building Systems,LLC is a fully approved member company of the Steel Joist Institute. Respectfully,StPROF�c ,�S �,r,l N E F '/� jt' 92304 Scott MortonA—M11 NMBS Design Engineer II\ Nc REGON,� cZ O RY N � Exp. 12/31/ 20 4---2J- 20!9 8200 Woolery Way Fallon,Nevada 89406 Phone:775-867-2130 Fax:775-867-2169;www.newmill.com Building a better steel experience. 4.1 NEW MILLENNIUM BUILDING SYSTEMS JOIST CALCULATION DEFINITION SHEET Load Types: (Figure 1) Uniform Uniform line load applied to TC or BC Net Uplift Uniform line load applied to TC(not concurrent w/uniform dead or live loading) Gross Uplift Uniform line load applied to TC(concurrently w/factored dead loads per Code requirements) Axial Compressive/Tensile(+/-)forces applied to TC or BC Concentrated Load Vertical load applied at given location Conc @ any pp Vertical load applied at any panel point(local panel bending not applied to chords) Conc anywhere Vertical load applied at any location along chord (local panel bending applied to chords) Conc w/bending Vertical load applied at given location (local panel bending applied to chords) Category: (Figure 1) DL Dead Load LL Live Load TL Total Load (DL+ LL) IP Inward Pressure WL Wind Load SM Seismic Load CL Collateral Load SL Snow Load (1), (2), (3), etc. Individual Separate Design Load Cases Position: (Figure 1) TC Top Chord BC Bottom Chord Load Combinations: (Figure 2) All shown load combinations are ran for each Load Case (1, 2, 3, etc.) Loads Load Type Category Loadt Load2 Position Direction Leo/Begin Sp/End Uniform(plf) DL(1) 9647 96.47 IC + 0-0 30-5 5/8 Figure 1 Uniform(pit) LL(1) 234.22 234.22 TC + 0-0 30-55/8 (Example only) Net Uplift(plf) WL(1) 67.00 67.00 TC - 0-0 30.8 6/8 Uniform(plf) TL(2) 319.00 319.00 TC + 0-0 30-5 5/8 Axial(lbs) SM(2) 300.00 0.00 IC + 0-0 0-0 Conc Load(ba) DL(2) 1,700.00 0.00 TC + 13-01/4 13.01/4 Cone Load(lbs) DL(2) 1,700.00 0.00 IC + 26-6 1/4 26-61/4 Load Combinations Case 1:Di. Case 8a:DL+CL+0.85(TL)+WL+AX Case 2a:LL Case 6b:DL+CL+0.85(71)+WL-AX Figure 2 Case 2b:SL Case 8c:DL+CL+0.85(TL)+WL+AX+1P Case 3a:DL+CL+TL+LL Case 6d:DL+CL+0.85(TL)+WL-AX+IP Case 3b:DL+CL+TL+SL Case 6e:DL+CL+0.85(TL)+SM+AX Case 3c:DL+CL+TL+LL+FEM Case 6f:DIACL+0.85(TL)+SM-AX Case 3d:DL+CL+TL+SL+FEM Case 7a:DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 30:DL+CL+TL+LL Case 7b:DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 31:DL+CL+TL+SL Case 7c:DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4a:DL+WL+AX Case 7d:DL+CL+0.85(1L)+0.75(WL-AX+LL+IP) Case 4b:DL+WL-AX Case 7e:DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4c:DL+WL+AX+1P Case 71:DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4d:DL+WL-AX+IP Case 8a:DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4e:DL+SM+AX Case 8b:DL+CL+0.85(IL)+0.75(WL-AX+SL) Case 41:0L+SM-AX Case 8c:DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5a:0.61DL)+WL+AX Case 8d:0L+CL+0.85(TL)+0.75(W L.AX+SL+1P) Case 5b:0,8(DL)+WL-AX Case 8e:DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5e:0.6(DL)+WL+AX+IP Case 8f:DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 5d:0.6(DL)+WL-AX+IP Case 9a:I.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 5e:0.8(DL)+WL+AX+SM Case 9b:1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 51:0.6(D1)+WL-AX+SM 8200 Woolery Way Fallon,Nevada 89406 I Phone:775-867-2130 I Fax:775-867-2169 www.newmill.com Building a better steel experience. Interior Dimensions: TC PANEL '114 Vsi BC PANEL — Left End Dimensions: OVERALL LENGTH • FBASELENGTH —r TCX - FIRST DIAGONAL j F-, TO PANEL I W2 V1 S W3 W4 `.'-2 1 3C PANEL • - - FIRST HALF • 3CX - - Right End Dimensions: I FIRST DIAGONAL TCX F-.--- TC PANEL =ja L72 4 W3 1S 2 BCX FIRST HALF - - BC PANEL Notes&Abbreviations: TCX-Top Chord Extension BCX-Bottom Chord Extension BPL-Base Plate Length V1S-First Vertical Web Member V2-Standard Vertical Web Member W2-First Diagonal Web Member TC/BC-Top Chord/Bottom Chord All vertical and diagonal web members are ordered numerically progressive toward interior 8200 Woolery Way!Fallon,Nevada 89406!Phone:775-867-2130 Fax:775-867-2169 www.newmill.com Building a better steel experience. STRESS ANALYSIS- PAGE 1 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:47:51 AM NEW NI i L L E N N I U M Location: Joist Description: Mark: SLIMMING SYSTEMS PORTLAND,OR Short Span Crimp 28K350/200 J1 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 42-31/4 41-11 1/4 28.00 28.84 9 @ 4-0 Parallel Chords ------------------ -------- -- _____ Variable Left End Right End BC Panel 3-1 3-2 1/4 TC Panel 1-7 2-0 (1117TTTrri l 1ET1 I r r,r,�. , ----- .r . First Half 2-0 2-0 First Diag. 5-1 5-2 1/4 Depth 28.00 28.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 42-3 1/4 L-BL Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 42-3 1/4 L-BL Uniform (plf) LL(1) 360.00 0.00 TC + 0-0 16-2 L-OAL Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Conc @ any pp (lbs) CL(1) 350.00 0.00 TC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 42-3 1/4 L-BL Axial (lbs) WL(1) 412.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere (lbs) CL(1) 300.00 0.00 BC + Conc Load (lbs) DL(1) 1,440.00 0.00 TC + 1-1 1-1 L-OAL Conc Load (lbs) WL(1) 412.00 0.00 TC + 34-0 40-0 L-OAL Gross Uplift(plf) WL(2) 105.00 105.00 TC - 0-0 42-3 1/4 L-BL Conc Load (lbs) WL(2) 412.00 0.00 TC - 34-0 40-0 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 12,376.81 8,781.20 3,094.20 42,782.40 43,038.86 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 2,879.30 14,053.65 0.00 0.00 18,512.25 3,630.06 44.11 0-2 V1S 2,706.18 12,549.38 0.00 0.00 422.96 4,245.03 32.32 1-7 W3 2,706.18 12,549.38 19,825.37 4,449.74 2,953.52 11,646.91 36.01 3-1 W4 5,935.10 25,745.29 19,825.37 4,449.74 9,384.21 2,588.17 36.01 5-1 W5 5,935.10 25,745.29 30,658.69 7,232.68 2,043.78 7,746.45 36.01 7-1 W6 8,342.48 34,641.68 30,658.69 7,232.68 6,787.42 1,666.26 36.01 9-1 W7 8,342.48 34,641.68 37,770.39 9,264.49 1,384.55 5,728.60 36.01 11-1 W8 9,998.73 40,120.91 37,770.39 9,264.49 4,789.56 1,102.83 36.01 13-1 W9 9,998.73 40,120.91 41,769.38 10,545.18 849.52 4,150.84 36.01 15-1 W10 10,903.85 42,782.40 41,769.38 10,545.18 4,150.84 849.52 36.01 17-1 W11 10,903.85 42,782.40 43,038.86 11,074.74 4,150.84 4,150.84 36.01 19-1 W11 11,057.84 42,059.73 43,038.86 11,074.74 4,150.84 4,150.84 36.01 21-1 W10 11,057.84 42,059.73 40,300.73 10,853.17 4,150.84 849.52 36.01 23-1 W9 10,460.71 37,915.80 40,300.73 10,853.17 849.52 4,150.84 36.01 25-1 W8 10,460.71 37,915.80 34,904.93 9,880.48 4,789.56 1,102.83 36.01 27-1 W7 9,112.46 31,268.13 34,904.93 9,880.48 1,384.55 5,728.60 36.01 29-1 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: �Ii/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 10:47:51 AM NEW MILLENNIUM Location: Joist Description: Mark: aLM.nwc SYSTEr.A9 PORTLAND,OR Short Span Crimp 28K350/200 J1 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W6 9,112.46 31,268.13 27,005.38 8,156.66 6,787.42 1,666.26 36.01 31-1 W5 6,794.33 22,116.70 27,005.38 8,156.66 2,043.78 7,746.45 36.01 33-1 W4 6,794.33 22,116.70 16,602.07 5,094.56 9,384.21 2,588.17 36.01 35-1 W3 3,151.26 11,145.28 16,602.07 5,094.56 2,953.52 11,646.91 36.01 37-1 V1S 3,151.26 11,145.28 0.00 0.00 1,043.80 2,177.34 30.39 40-3 1/4 W2 3,291.21 11,545.13 0.00 0.00 14,196.41 4,188.27 45.10 39-1 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 1,112.00 2,246.61 26.84 STRESS ANALYSIS- PAGE 2 0 Job Number: 5618-0088 Job Name: Date Run: JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:47:51 AM NEW MILLENNIUM Location: Joist Description: Mark: wuu.ninrr SYSTEM% PORTLAND,OR Short Span Crimp 28K350/200 J1 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 584.54 296.08 444.12 17-6 3/8 15-11 1/2 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 17.00 42.00 24.00 38.25 22.00 1.1250 Bending Load 694.93 642.61 350.00 350.00 350.00 Min Weld Len 2X: Axial Load 14,053.65 12,549.38 42,782.40 11,145.28 11,545.13 Max Load Fillers TC: fa 4,265.92 6,743.36 22,988.93 5,988.87 3,504.47 49,625.71 Maximum K L/r 43.46 107.36 46.01 97.78 56.24 Max Load no Fillers TC: 45 Fcr 43,551.60 21,525.32 42,829.38 24,853.79 39,677.35 ,547.55 TC Fa 26,130.96 12,915.19 25,697.63 14,912.27 23,806.41 OAL/3885.795.79Ryy: Fe 808,645.63 60,216.98 327,847.97 72,603.02 482,848.31 BCOAL/Ryy: Cm 0.9974 0.9440 0.9530 0.9588 0.9964 390.38 Panel Point Moment 9331.44 10364.17 2644.44 5161.40 6566.53 BC Stress: Mid Panel Moment 704.48 6572.02 1750.00 3956.03 3682.04 1.00 Panel Point fb 4600.32 21145.55 5395.34 10530.57 3237.24 121..8888 1293 Mid Panel fb 307.45 5624.19 1497.61 3385.48 1815.22 TC Shear Stress: Fillers 0 0 0 0 0 12,022.29 Panel Point Stress 8,866.24 27,888.91 28,384.27 16,519.44 6,741.72 BC Shear Stress: Mid Panel Stress 0.0919 0.7156 0.9425 0.5131 0.1346 15,832.39 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 18,512.25 26,972.16 3,630.06 9,555.41 3.60 x 0.245 1 R112= round 1 1/8 W3 2,953.52 28,624.38 11,646.91 12,786.97 4.18 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 9,384.21 10,742.43 2,588.17 5,330.90 4.90 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 2,043.78 18,714.09 7,746.45 8,898.52 2.96 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 6,787.42 7,826.93 1,666.26 3,564.90 4.48 x 0.102 1 Cl6BB= 1.125 x 1.025 x.102 W7 1,384.55 14,381.54 5,728.60 6,928.23 2.57 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 4,789.56 5,758.64 1,102.83 2,157.24 3.58 x 0.090 1 Cl2BB= 1.125 x 0.799 x.090 W9 849.52 8,984.69 4,150.84 4,326.22 2.37 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 4,150.84 4,802.89 849.52 1,636.66 3.63 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 W11 4,150.84 8,984.69 4,150.84 4,326.22 2.37 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W11 4,150.84 8,984.69 4,150.84 4,326.22 2.37 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 4,150.84 4,802.89 849.52 1,636.66 3.63 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 849.52 8,984.69 4,150.84 4,326.22 2.37 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 4,789.56 5,758.64 1,102.83 2,157.24 3.58 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 1,384.55 14,381.54 5,728.60 6,928.23 2.57 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 6,787.42 7,826.93 1,666.26 3,564.90 4.48 x 0.102 1 Cl 6BB= 1.125 x 1.025 x.102 W5 2,043.78 18,714.09 7,746.45 8,898.52 2.96 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W4 9,384.21 10,742.43 2,588.17 5,330.90 4.90 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 2,953.52 28,624.38 11,646.91 12,786.97 4.18 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: i/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 10:47:51 AM N E V V MILLENNIUM Location: Joist Description: Mark: pL"Ln'^'G SVSTF�s PORTLAND,OR Short Span Crimp 28K350/200 J1 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 14,196.41 21,311.81 4,188.27 5,706.40 2.94 x 0.230 1 R100= round 1 V1 1,043.80 8,984.69 4,245.03 4,736.99 2.42 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V2 1,112.00 4,802.89 2,246.61 2,577.11 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 401 Job Number: Job Name: Date Run: �/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:47:51 AM NEW MILLENNIUM Location: Joist Description: Mark: RIMMING 8LY,RTF_i.AS PORTLAND,OR Short Span Crimp 28K350/200 J1 TCX Design TCX Left TCX Right TCX Length 0-1 1/4 TCX Length 0-5 1/4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-1 1/8 BPL Length 2-9 3/4 Clear Bearing 0-5 1/4 Clear Bearing 0-9 3/8 BPL Material:2018=2 X 2 X.188 BPL Material: 2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.02 Reqd TL Def L/80 0.07 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.01 Reqd LL Def L/120 0.04 Section Modulus 2.0284 Section Modulus 2.0284 Reqd SM 0.0051 Reqd SM 0.2189 Mom of Inertia 2.6899 Mom of Inertia 2.6899 Reqd MI 0.0003 Reqd MI 0.0425 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) N N \ i EVAN ;%� Concentrated Loads Conc @ 0-5 1/4 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b:DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case Gc:DL+CLt0.85(TL)*WL+C+AX+f-' STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: �/�,! 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:01:00 PM NEW MILLENNIUM Location: Joist Description: Mark: ®IJILOIN6 SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J10 Geometry Base Length: Working Length: !Joist Depth: Effective Depth: BC Panel Length: Shape: 46-101/2 46-61/230.00 28.65 10 @ 4-0 Parallel Chords L Variable Left End Right End BC Panel 3-5 1/2 3-5 111111111 1111111111111111111111111111/1111 11L111111111I11111111111111i1 SIL - 111111 ] TC Panel 1-8 1/2 1-8 First Half 2-0 2-0 N lr lr, ,r,, ,,,,r,,,,liv First Diag. 5-5 1/2 5-5 Depth 30.00 30.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 46-10 1/2 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 46-10 1/2 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Axial(lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere (lbs) CL(1) 300.00 0.00 BC + Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 46-10 1/2 L-BL Conc @ any pp (lbs) CL(1) 1,800.00 0.00 TC + Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 46-10 1/2 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 10,926.44 10,929.74 2,732.43 53,329.51 51,892.70 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,356.15 12,887.02 0.00 0.00 18,130.79 1,675.28 48.80 0-2 V 1 S 1,192.40 12,305.19 0.00 0.00 3,419.70 4,674.16 35.52 1-8 1/2 W3 1,192.40 12,305.19 19,103.57 1,874.34 1,064.14 12,324.46 37.37 3-5 1/2 W4 2,457.53 25,254.83 19,103.57 1,874.34 11,011.77 910.37 37.37 5-51/2 W5 2,457.53 25,254.83 30,819.68 2,972.02 803.40 9,784.39 37.37 7-51/2 W6 3,417.82 35,798.11 30,819.68 2,972.02 8,871.22 696.43 37.37 9-5 1/2 W7 3,417.82 35,798.11 40,190.11 3,794.92 589.46 7,643.83 37.37 11-51/2 W8 4,103.33 43,995.71 40,190.11 3,794.92 6,730.66 482.49 37.37 13-51/2 W9 4,103.33 43,995.71 47,214.89 4,343.05 375.52 5,503.28 37.37 15-51/2 W10 4,514.07 49,847.66 47,214.89 4,343.05 4,590.11 380.71 37.37 17-51/2 W11 4,514.07 49,847.66 51,892.70 4,616.39 1,086.28 3,564.55 37.37 19-5 1/2 W12 4,650.02 53,329.51 51,892.70 4,616.39 3,564.55 1,477.64 37.37 21-5 1/2 ,,y 1 W12 4,650.02 53,329.51 51,857.35 4,614.96 3,564.55 1,477.64 37.37 23-5 1/2 W11 4,511.20 49,798.79 51,857.35 4,614.96 1,086.28 3,564.55 37.37 25-5 1/2 W10 4,511.20 49,798.79 47,153.80 4,338.75 4,590.11 380.71 37.37 27-5 1/2 W9 4,097.61 43,922.41 47,153.80 4,338.75 375.52 5,503.28 37.37 29-5 1/2 W8 4,097.61 43,922.41 40,104.60 3,787.77 6,730.66 482.49 37.37 31-51/2 W7 3,409.23 35,700.37 40,104.60 3,787.77 589.46 7,643.83 37.37 33-5 1/2 W6 3,409.23 35,700.37 30,709.72 2,962.00 8,871.22 696.43 37.37 35-5 1/2 W5 2,446.08 25,132.66 30,709.72 2,962.00 803.40 9,784.39 37.37 37-5 1/2 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 �,/� Job Number: Job Name: Date Run: �// 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:01:00 PM NEW M I L L EN N I U M Location: Joist Description: Mark: RUIL.nIN[S SVSTERA9 PORTLAND,OR Short Span Crimp 30K350/200 J10 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. ___ W4 2,446.08 25,132.66 18,969.19 1,861.46 11,011.77 910.37 37.37 39-51/2 W3 1,178.09 12,176.04 18,969.19 1,861.46 1,064.14 12,324.46 37.37 41-5 1/2 V 1 S 1,178.09 12,176.04 0.00 0.00 3,419.70 4,674.16 35.52 45-2 1/2 W2 1,256.98 12,753.29 0.00 0.00 18,018.48 1,559.68 48.39 43-5 1/2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 2,500.00 3,698.48 28.65 STRESS ANALYSIS- PAGE 2 l/� Job Number: Job Name: Date Run: ��/�i/// 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:01:00 PM NEW MILLENNIUM Location: Joist Description: Mark: RIM ninon sysTEMS PORTLAND,OR Short Span Crimp 30K350/200 J10 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 1.0162 0.8183 0.4925-.. 1.5555 0.7604 0.6804 0.9652 A42A=2.6250 x.209 -- BC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 799.37 296.23 444.34 21-0 26-11/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 18.50 45.00 24.00 45.00 18.00 1.1250 Min Weld Len 2X: Bending Load 350.00 350.00 350.00 350.00 350.00 0.5000 Axial Load 12,887.02 12,305.19 53,329.51 12,176.04 12,753.29 Max Load Fillers TC: fa 3,718.34 6,054.51 26,239.67 5,990.96 3,679.75 54,747.40 Maximum K L/r 37.56 91.37 24.37 91.37 36.55 Max Load no Fillers TC: Fcr 43,685.70 26,773.67 46,279.65 26,773.67 43,918.29 51,956.74 Fa 26,211.42 16,064.20 27,767.79 16,064.20 26,350.97 359.05 5Ryy: 9.05 F'e 737,895.13 94,645.03 591,531.44 94,645.03 779,458.63 BC OAL/Ryy: Cm 0.9975 0.9680 0.9703 0.9684 0.9976 428.14 Panel Point Moment 6566.53 6542.98 2644.44 7142.57 6021.64 BC Stress: Mid Panel Moment 4354.17 5216.06 1750.00 5019.13 2255.56 0.93 Panel Point fb 2696.11 8965.34 3623.48 9786.91 2472.39 BC L/Rz: 122.6994 Mid Panel fb 1787.75 2914.68 977.88 2804.64 926.09 TC Shear Stress: Fillers 0 0 2 0 0 12,647.09 Panel Point Stress 6,414.45 15,019.85 29,863.15 15,777.88 6,152.14 BC Shear Stress: Mid Panel Stress 0.1330 0.4739 0.9764 0.4662 0.1020 11,439.18 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 18,130.79 23,679.79 1,675.28 4,875.81 3.75 x 0.230 1 R100= round 1 W3 1,064.14 28,624.38 12,324.46 12,325.55 4.43 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 11,011.77 14,381.54 910.37 6,696.07 4.94 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 803.40 24,373.24 9,784.39 10,696.87 3.51 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 8,871.22 10,742.43 696.43 5,154.62 4.63 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W7 589.46 18,714.09 7,643.83 8,594.42 2.92 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W8 6,730.66 7,826.93 482.49 3,438.59 4.44 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 375.52 14,381.54 5,503.28 6,696.07 2.47 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W10 4,590.11 4,802.89 380.71 1,519.05 4.01 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 1,086.28 8,984.69 3,564.55 4,175.69 2.03 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W12 3,564.55 4,802.89 1,477.64 1,519.05 3.12 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 W12 3,564.55 4,802.89 1,477.64 1,519.05 3.12 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 1,086.28 8,984.69 3,564.55 4,175.69 2.03 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W 10 4,590.11 4,802.89 380.71 1,519.05 4.01 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 375.52 14,381.54 5,503.28 6,696.07 2.47 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 6,730.66 7,826.93 482.49 3,438.59 4.44 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 589.46 18,714.09 7,643.83 8,594.42 2.92 x 0.176 1 C34AA= 1.125 x 1.549 x.176 1 W6 8,871.22 10,742.43 696.43 5,154.62 4.63 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 803.40 24,373.24 9,784.39 10,696.87 3.51 x 0.188 1 C38BA= 1.125 x 1.845 x.199 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:01:00 PM NEW MILLENNIUM Location: Joist Description: Mark: ouiLniNr., SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J10 Web Design,Continued... Member Web Tension Allow Tension Web Comp .Allow Comp Weld Qty Material W4 11,011.77 14,381.54 910.37 6,696.07 4.94 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 1,064.14 28,624.38 12,324.46 12,325.55 4.43 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W2 18,018.48 23,679.79 1,559.68 4,957.54 3.73 x 0.230 1 R100=round 1 V1 3,419.70 10,742.43 4,674.16 5,393.48 2.44 x 0.129 1 C22BB= 1.125 x 1.110 x.129 V2 2,500.00 7,826.93 3,698.48 4,277.76 2.38 x 0.102 1 C16BB= 1.125 x 1.025 x.102 STRESS ANALYSIS- PAGE 3 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:01:00 PM NEW MILLENNIUM Location: Joist Description: Mark: HUM miNf.. SVSTBMS PORTLAND,OR Short Span Crimp 30K350/200 J10 TCX Design TCX Left TCX Right TCX Length 0-5 1/4 TCX Length 0-0 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-6 3/4 BPL Length 2-1 Clear Bearing 0-9 1/8 Clear Bearing 0-3 7/8 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.07 Reqd TL Def L/80 0.00 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.04 Reqd LL Def L/120 0.00 Section Modulus 2.4356 Section Modulus 2.4356 Reqd SM 0.2189 Reqd SM 0.0000 Mom of Inertia 3.0580 Mom of Inertia 3.0580 Reqd MI 0.0425 Reqd MI 0.0000 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) ,/ N'N j ��\ �� 7/7 77 Concentrated Loads Conc @ 0-5 1/4 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) ase 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM ac- r// STRESS ANALYSIS- PAGE 1 ✓? Job Number: Job Name: Date Run: ✓ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 11:57:00 AM NEW MILLENNIUM Location: Joist Description: Mark: ®uiLowc SYSTEMS PORTLAND,OR Short Span Round 10K350/200 J13 Geometry Base Length: Working Length: Joist Depth: Effective Depth: I BC Panel Length: Shape: 14-61/4 14-21/4 10.00 9.10 17 @ 1-8 Parallel Chords Variable Left End Right End BC Panel 1-5 1/8 1-51/8 NFITT1 T I T1TC I EMT l IT I 11 11 TC Panel 0 10 0 10 First Half 0-10 0-10 First Diag. 2-3 1/8 2-3 1/8 Depth 10.00 10.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 14-6 1/4 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 14-6 1/4 L-BL Conc @ any pp (lbs) CL(1) 350.00 0.00 TC + Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 14-6 1/4 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 14-6 1/4 L-BL Stress Analysis Summary Inl.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 20.00 20.00 3,447.72 3,465.27 866.32 15,473.68 16,130.46 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,188.38 5,853.40 0.00 0.00 6,497.00 537.78 17.65 0-2 V1S 1,262.17 5,607.41 0.00 0.00 1,070.75 1,755.31 11.56 0-10 W3 1,262.17 5,607.41 7,226.33 684.74 348.12 4,223.18 13.52 1-51/8 W4 872.54 9,965.01 7,226.33 684.74 3,418.61 253.87 13.52 2-31/8 W5 872.54 9,965.01 11,531.82 1,060.33 253.87 3,262.19 13.52 3-1 1/8 W6 1,173.00 13,262.83 11,531.82 1,060.33 2,395.31 152.32 13.52 3-11 1/8 W7 1,173.00 13,262.83 14,554.83 1,285.68 152.32 2,212.81 13.52 4-9 1/8 W8 1,323.24 15,473.68 14,554.83 1,285.68 1,345.94 387.81 13.52 5-7 1/8 W9 1,323.24 15,473.68 16,130.46 1,360.80 544.24 1,287.41 13.52 6-5 1/8 W9 1,323.24 15,473.68 16,130.46 1,360.80 544.24 1,287.41 13.52 7-3 1/8 W8 1,323.24 15,473.68 14,554.83 1,285.68 1,345.94 387.81 13.52 8-1 1/8 W7 1,173.00 13,262.84 14,554.83 1,285.68 152.32 2,212.81 13.52 8-11 1/8 W6 1,173.00 13,262.84 11,531.83 1,060.33 2,395.31 152.32 13.52 9-9 1/8 W5 872.54 9,965.01 11,531.83 1,060.33 253.87 3,262.19 13.52 10-7 1/8 W4 872.54 9,965.01 7,226.33 684.74 3,418.61 253.87 13.52 11-51/8 W3 1,262.17 5,607.41 7,226.33 684.74 348.12 4,223.18 13.52 12-3 1/8 V1S 1,262.17 5,607.41 0.00 0.00 1,070.75 1,755.31 11.56 13-8 1/4 W2 1,188.38 5,853.40 0.00 0.00 6,497.00 537.78 17.65 13-1 1/8 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �// 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201911:57:00 AM NEW MILLENNIUM Location: Joist Description: Mark: FILM rIWG gY%7E1,4% PORTLAND,OR Short Span Round 10K350/200 J13 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.4306 0.5149 0.3062 0.8995 0.4877 0.1141 1.0000 A26B= 1.6560 x 0.142 BC 0.3151 0.4675 0.2972 0.8133 0.4154 0.0689 0.9057 1510= 1 1/2 x 1 1/2 x.109 Axial and Bendin Analysis K: y: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 30.48 398.75 598.13 11-2 7/8 16-3 1/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 8.00 17.13 20.00 17.13 8.00 0.5000 Bending Load 350.00 350.00 350.00 350.00 350.00 Min Weld Len 2X: 0.5000 Axial Load 5,853.40 5,607.41 15,473.68 5,607.41 5,853.40 fa Max Load Fillers TC: 2,550.95 6,511.16 17,967.58 6,511.16 2,550.95 21,036.77 Maximum K Ur 37.62 55.93 48.99 55.93 37.62 Max Load no Fillers TC: Fcr 45,084.93 39,778.26 41,953.31 39,778.26 45,084.93 19,582.83 Fa 27,050.96 23,866.96 25,171.98 23,866.96 27,050.96 TCOAURyy: 189.26 F'e 3,692,184.25 258,751.22 337,257.06 258,751.22 3,692,184.25 BCOAL/Ryy: Cm 0.9997 0.9874 0.9643 _ 0.9874 0.9997 209.34 Panel Point Moment 1153.00 1755.19 2009.26 1755.19 1153.00 BC Stress: Mid Panel Moment 514.37 1077.73 1361.11 1077.73 514.37 0.85 Panel Point fb 676.12 8985.92 10286.67 8985.92 676.12 BC Mid Panel fb 67.229494 8 377.17 2303.27 2908.91 2303.27 377.17 Fillers 0 TC Shear Stress: 0 0 0 0 9,872.39 Panel Point Stress 3,227.07 15,497.08 28,254.25 15,497.08 3,227.07 BC Shear Stress: Mid Panel Stress 0.0597 0.3432 0.8050 0.3432 0.0597 11,152.48 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 6,497.00 6,743.04 537.78 3,583.90 2.00 x 0.177 1 R056= round 9/16 V1S 1,070.75 7,492.27 1,755.31 5,022.13 2.00 x 0.177 1 R056= round 9/16 W3 348.12 7,492.27 4,223.18 4,333.39 2.00 x 0.177 1 R056=round 9/16 W4 3,418.61 7,492.27 253.87 4,333.39 2.00 x 0.177 1 R056=round 9/16 W5 253.87 7,492.27 3,262.19 4,333.39 2.00 x 0.177 1 R056= round 9/16 W6 2,395.31 5,918.44 152.32 2,960.52 2.00 x 0.170 1 R050= round 1/2 W7 152.32 5,918.44 2,212.81 2,960.52 2.00 x 0.170 1 R050=round 1/2 W8 1,345.94 5,918.44 387.81 2,960.52 2.00 x 0.170 1 R050=round 1/2 W9 544.24 5,918.44 1,287.41 2,960.52 2.00 x 0.170 1 R050=round 1/2 W9 544.24 5,918.44 1,287.41 2,960.52 2.00 x 0.170 1 R050= round 1/2 W8 1,345.94 5,918.44 387.81 2,960.52 2.00 x 0.170 1 R050= round 1/2 W7 152.32 5,918.44 2,212.81 2,960.52 2.00 x 0.170 1 R050= round 1/2 W6 2,395.31 5,918.44 152.32 2,960.52 2.00 x 0.170 1 R050=round 1/2 W5 253.87 7,492.27 3,262.19 4,333.39 2.00 x 0.177 1 R056=round 9/16 W4 3,418.61 7,492.27 253.87 4,333.39 2.00 x 0.177 1 R056= round 9/16 W3 348.12 7,492.27 4,223.18 4,333.39 2.00 x 0.177 1 R056= round 9/16 V1S 1,070.75 7,492.27 1,755.31 5,022.13 2.00 x 0.177 1 R056= round 9/16 W2 6,497.00 6,743.04 537.78 3,583.90 2.00 x 0.177 1 R056= round 9/16 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201911:57:00 AM NEW NI I L L E N N I U NI Location: Joist Description: Mark: RLHLMINr SYSTEM% PORTLAND,OR Short Span Round 10K350/200 J13 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 0-0 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 1-2 7/8 BPL Length 1-2 7/8 Clear Bearing 0-4 3/4 Clear Bearing 0-4 3/4 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.00 Reqd TL Def L/80 0.00 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.00 Reqd LL Def L/120 0.00 Section Modulus 1.3637 Section Modulus 1.3637 Reqd SM 0.0000 Reqd SM 0.0000 Mom of Inertia 1.8944 Mom of Inertia 1.8944 Reqd MI 0.0000 Reqd MI 0.0000 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) `‘ \\ / ' \ // .`- // / '''', Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(W L+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP_ __ STRESS ANALYSIS- PAGE 1 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:16:09 PM NEW /VII L L E N N I U/M Location: Joist Description: Mark: ®V1LOING SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J16 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 46-101/8 46-61/8 30.00 28.83 10 @ 40 Parallel Chords Variable Left End Right End BC Panel 3-5 3-5 1/8 111111111111111111 -11 11- HI -1 1 II 11I 1111 1111' TC Panel 1-8 1-8 1/8 `���AAAAVAVAALW& P. First Half 2-0 2-0 First Diag. 5-5 5-5 1/8 Depth 30.00 30.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 46-10 1/8 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 46-10 1/8 L-BL Axial (lbs) SM(1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 46-10 1/8 L-BL Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 46-10 1/8 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 9,128.57 9,146.39 2,286.60 44,234.29 43,528.20 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,248.23 11,459.77 0.00 0.00 14,952.00 1,697.77 48.50 0-2 V1S 1,169.83 10,886.14 0.00 0.00 1,223.32 2,429.52 35.67 1-8 W3 1,169.83 10,886.14 16,871.47 1,848.38 1,060.56 10,212.30 37.51 3-5 W4 2,428.80 22,242.49 16,871.47 1,848.38 8,903.00 907.19 37.51 5-5 W5 2,428.80 22,242.49 27,030.77 2,940.95 800.49 7,887.26 37.51 7-5 W6 3,384.84 31,236.32 27,030.77 2,940.95 6,976.44 693.80 37.51 9-5 W7 3,384.84 31,236.32 34,859.13 3,760.47 587.10 5,953.70 37.51 11-5 W8 4,067.83 37,899.19 34,859.13 3,760.47 5,042.89 480.41 37.51 13-5 W9 4,067.83 37,899.19 40,356.53 4,306.93 373.71 4,020.15 37.51 15-5 W10 4,477.76 42,231.13 40,356.53 4,306.93 3,109.33 310.15 37.51 17-5 W11 4,477.76 42,231.13 43,523.32 4,580.34 310.15 2,975.24 37.51 19-5 W12 4,614.65 44,234.29 43,523.32 4,580.34 2,975.24 414.62 37.51 21-5 W12 4,614.65 44,234.29 43,528.20 4,580.69 2,975.24 414.62 37.51 23-5 W11 4,478.48 42,239.37 43,528.20 4,580.69 310.15 2,975.24 37.51 25-5 W10 4,478.48 42,239.37 40,367.81 4,307.99 3,109.33 310.15 37.51 27-5 W9 4,069.25 37,913.50 40,367.81 4,307.99 373.71 4,020.15 37.51 29-5 W8 4,069.25 37,913.50 34,876.47 3,762.24 5,042.89 480.41 37.51 31-5 W7 3,386.97 31,256.69 34,876.47 3,762.24 587.10 5,953.70 37.51 33-5 W6 3,386.97 31,256.69 27,054.19 2,943.44 6,976.44 693.80 37.51 35-5 W5 2,431.64 22,268.94 27,054.19 2,943.44 800.49 7,887.26 37.51 37-5 W4 2,431.64 22,268.94 16,900.96 1,851.58 8,903.00 907.19 37.51 39-5 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 l/� Job Number: Job Name: Date Run: �/// 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:16:09 PM NEW MILLENNIUM Location: Joist Description: Mark: auiLninir.. SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J16 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W3 1,173.39 10,914.33 16,900.96 1,851.58 1,060.56 10,212.30 37.51 41-5 V1S 1,173.39 10,914.33 0.00 0.00 1,223.32 2,429.52 35.67 45-2 W2 1,366.79 11,489.10 0.00 0.00 14,952.00 1,697.77 48.60 43-5 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 700.00 1,896.97 28.83 6 44i- 41410404.soWot- STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:16:09 PM NEW M I L LEN N I U M Location: Joist Description: Mark: RI.21L.1711Nr %Y%TEMS PORTLAND,OR Short Span Crimp 30K350/200 J16 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.8173 0.6134 0.3924 1.2964 0.5795 0.3076 1.0000 2021 =2 x 2 x.216 Axial and Bending Analysis 0.75 50,000.00 30,000.00 724.591nertia: 269.06 403.58 17-7 3/8 0: Max BridgTC 25-11Maxri1/g 88C: Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 18.00 45.00 24.00 45.00 18.13 1.1250 Bending Load 350.00 350.00 350.00 350.00 350.00 0.5Len 2X: 00000 Axial Load 0.5 11,459.77 10,886.14 44,234.29 10,914.33 11,489.10 Max Load F fa 3,478.56 5,849.62 23,769.10 5,864.76 3,487.46 49,625.71i/lers TC: Maximum K L/r 46.01 115.03 46.01 115.03 46.33 Max Load no Fillers TC: Fcr 42,829.38 18,970.12 42,829.38 18,970.12 42,737.08 45,547.55 Fa 25,697.63 11,382.07 25,697.63 11,382.07 25,642.25 TC OAL/Ryy: F'e 427.85 721,291.88 52,455.68 327,847.97 52,455.68 711,377.38 BC OAL/Ryy: Cm 0.9976 0.9442 0.9514 0.9441 0.9975 430.54 Panel Point Moment 6315.03 7435.96 2644.44 7049.28 6947.87 BC Stress: Mid Panel Moment 2500.05 4922.77 1750.00 5049.77 4806.99 0.89 Panel Point fb 3113.26 15171.26 5395.34 14382.32 3425.24 122.3242 Mid Panel fb 1232.51 4212.80 1497.61 4321.48 2369.81 TC Shear Stress: Fillers 0 0 0 0 0 9,508.06 Panel Point Stress 6,591.82 21,020.88 29,164.44 20,247.08 6,912.71 BC Shear Stress: Mid Panel Stress 0.1090 0.6588 0.9730 0.6639 0.1475 10,906.10 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 14,952.00 21,311.81 1,697.77 4,935.62 3.10 x 0.230 1 R100= round 1 W3 1,060.56 24,373.24 10,212.30 10,657.42 3.67 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 8,903.00 10,742.43 907.19 5,136.77 4.65 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 800.49 18,714.09 7,887.26 8,563.68 3.02 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 6,976.44 8,984.69 693.80 4,160.47 3.98 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 587.10 14,381.54 5,953.70 6,672.60 2.67 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 5,042.89 5,758.64 480.41 1,989.00 3.77 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W9 373.71 8,984.69 4,020.15 4,160.47 2.29 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 3,109.33 4,802.89 310.15 1,507.82 2.72 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 310.15 7,826.93 2,975.24 3,425.87 2.00 x 0.102 1 Cl6BB= 1.125 x 1.025 x.102 W12 2,975.24 4,802.89 414.62 1,507.82 2.60 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W12 2,975.24 4,802.89 414.62 1,507.82 2.60 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 310.15 7,826.93 2,975.24 3,425.87 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W10 3,109.33 4,802.89 310.15 1,507.82 2.72 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 373.71 8,984.69 4,020.15 4,160.47 2.29 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 5,042.89 5,758.64 480.41 1,989.00 3.77 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 587.10 14,381.54 5,953.70 6,672.60 2.67 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 6,976.44 8,984.69 693.80 4,160.47 3.98 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 800.49 18,714.09 7,887.26 8,563.68 3.02 x 0.176 1 C34AA= 1.125 x 1.549 x.176 *Continued on Next Page... - STRESS ANALYSIS- PAGE 2 G, Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 1:16:09 PM NEW MILLENNIUM Location: Joist Description: Mark: auiLninic SYeFTEAA9 PORTLAND,OR Short Span Crimp 30K350/200 J16 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W4 8,903.00 10,742.43 907.19 5,136.77 4.65 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 1,060.56 24,373.24 10,212.30 10,657.42 3.67 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 14,952.00 21,311.81 1,697.77 4,915.22 3.10 x 0.230 1 R100= round 1 V1 1,223.32 7,826.93 2,429.52 3,596.39 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V2 700.00 4,802.89 1,896.97 2,362.58 2.00 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 1:16:09 PM NEW MILLENNIUM Location: Joist Description: Mark: BUIL.own %iYSTEt.A5 PORTLAND,OR Short Span Crimp 30K350/200 J16 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 0-5 5/8 . TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-1 BPL Length 2-6 3/4 Clear Bearing 0-4 Clear Bearing 0-9 3/4 BPL Material:2018=2 X 2 X.188 BPL Material: 2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.00 Reqd TL Def L/80 0.07 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.00 Reqd LL Def L/120 0.05 Section Modulus 2.0284 Section Modulus 2.0284 Reqd SM 0.0000 Reqd SM 0.2316 Mom of Inertia 2.6899 Mom of Inertia 2.6899 Reqd MI 0.0000 Reqd MI 0.0472 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) ' 72 A V ,% \N // Concentrated Loads Conc @ 0-5 5/8 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DLICL*O.65(TL)+WL+C+AX+IP STRESS ANALYSIS- PAGE 1 ,, Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:30:52 PM NEW !MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J18 Geometry Base Length: Working Length: Joist Depth: Effective Depth: IBC Panel Length: Shape: 46-10 1/2 46-6 1/2 30.00 28.66 110 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-5 3-5 1/2 1111111 11 111 1 1111111 -1111111 - 11111111 --_ 11111 11111111111111=1 TC Panel 1-8 1-8 1/2 \1 _IF_______I/* First Half 2-0 2-0 First Diag. 5-5 5-5 1/2 Depth 30.00 30.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 46-10 1/2 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 46-10 1/2 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) SM(1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Conc @ any pp (lbs) CL(1) 350.00 0.00 TC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 46-10 1/2 L-BL Conc @ any pp (lbs) CL(1) 950.00 0.00 TC + Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 46-10 1/2 L-BL Stress Analysis Summary lnt.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 10,073.82 10,096.07 2,524.02 49,170.82 48,083.07 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,256.48 12,170.50 0.00 0.00 16,568.40 1,559.27 48.40 0-2 V1S 1,177.62 11,593.48 0.00 0.00 2,365.46 3,619.73 35.53 1-8 W3 1,177.62 11,593.48 18,027.35 1,860.71 1,063.97 11,325.24 37.38 3-5 W4 2,445.10 23,832.46 18,027.35 1,860.71 10,012.77 910.22 37.38 5-5 W5 2,445.10 23,832.46 29,051.38 2,960.81 803.27 8,880.96 37.38 7-5 W6 3,407.86 33,684.13 29,051.38 2,960.81 7,967.94 696.31 37.38 9-5 W7 3,407.86 33,684.13 37,730.70 3,786.25 589.36 6,846.12 37.38 11-5 W8 4,095.96 41,191.08 37,730.70 3,786.25 5,933.10 482.41 37.38 13-5 W9 4,095.96 41,191.08 44,065.30 4,337.01 375.45 4,801.29 37.38 15-5 W10 4,509.39 46,353.32 44,065.30 4,337.01 3,888.27 311.11 37.38 17-5 W11 4,509.39 46,353.32 48,055.16 4,613.11 586.63 3,292.12 37.38 19-5 W12 4,648.16 49,170.82 48,055.16 4,613.11 3,292.12 977.93 37.38 21-5 W12 4,648.16 49,170.82 48,083.07 4,614.54 3,292.12 977.93 37.38 23-5 W11 4,512.26 46,394.76 48,083.07 4,614.54 586.63 3,292.12 37.38 25-5 W10 4,512.26 46,394.76 44,118.93 4,341.30 3,888.27 311.11 37.38 27-5 W9 4,101.69 41,256.95 44,118.93 4,341.30 375.45 4,801.29 37.38 29-5 W8 4,101.69 41,256.95 37,808.77 3,793.40 5,933.10 482.41 37.38 31-5 W7 3,416.45 33,774.42 37,808.77 3,793.40 589.36 6,846.12 37.38 33-5 W6 3,416.45 33,774.42 29,153.88 2,970.83 7,967.94 696.31 37.38 35-5 W5 2,456.54 23,947.17 29,153.88 2,970.83 803.27 8,880.96 37.38 37-5 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 GJob Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201 9 1:30:52 PM N E V V NII L L E N N I UNI Location: Joist Description: Mark: R"""'^'r SY51-614A5 PORTLAND,OR Short Span Crimp 30K350/200 J18 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W4 2,456.54 23,947.17 18,154.27 1,873.59 10,012.77 910.22 37.38 39-5 ' W3 1,191.93 11,715.17 18,154.27 1,873.59 1,063.97 11,325.24 37.38 41-5 V1S 1,191.93 11,715.17 0.00 0.00 2,365.46 3,619.73 35.53 45-2 W2 1,355.60 12,296.77 0.00 0.00 16,712.07 1,674.84 48.80 43-5 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 1,650.00 2,848.40 28.66 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: 5618 0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:30:52 PM NEW M I L L E N NI UN' Location: Joist Description: Mark: aLM_.niNn SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J18 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.0162 0.8183 0.4925 1.5555 0.7604 0.6804 0.9652 A42A=2.6250 x.209 BC 0.8173 0.6134 0.3924 1.2964 0.5795 0.3076 1.0000 2021 =2 x 2 x.216 Axial and Bendin Analysis K: Fr Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 746.13 276.50 414.75 21-0 25-111/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 18.00 45.00 24.00 45.00 18.50 1.1250 Bending Load 350.00 350.00 350.00 350.00 350.00 M0.500000 Len 2X: 0.5 Axial Load 12,170.50 11,593.48 49,170.82 11,715.17 12,296.77 fa Max Load Fillers TC: 3,511.60 5,704.33 24,193.48 5,764.20 3,548.03 54,747.40 Maximum K L/r 36.55 91.37 36.55 91.37 37.56 Max Load no Fillers TC: Fcr 43,918.29 26,773.67 43,918.29 26,773.67 43,685.70 51,956.74 TC Fa 26,350.97 16,064.20 26,350.97 16,064.20 26,211.42 OAL3559.059.05 Ryy: F'e 779,458.63 94,645.03 591,531.44 94,645.03 737,895.13 BCOAL/Ryy: Cm 0.9977 0.9699 0.9726 0.9695 0.9976 430.82 Panel Point Moment 6021.64 7142.57 2644.44 6542.98 6566.53 BC Stress: Mid Panel Moment 2255.56 5019.13 1750.00 5216.06 4354.17 0.98 Panel Point fb 2472.39 9786.91 3623.48 8965.34 2696.11 122.3242 . Mid Panel fb 1232 926.09 2804.64 977.88 2914.68 1787.75 Fillers 0 0 0 0 TC Shear Stress: 0 11,647.69 Panel Point Stress 5,983.99 15,491.24 27,816.96 14,729.55 6,244.14 BC Shear Stress: Mid Panel Stress 0.0988 0.4479 0.9495 0.4554 0.1298 12,089.48 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 16,568.40 23,679.79 1,559.27 4,956.14 3.43 x 0.230 1 R100= round 1 W3 1,063.97 28,624.38 11,325.24 12,322.60 4.07 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 10,012.77 10,742.43 910.22 5,153.48 5.23 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 803.27 24,373.24 8,880.96 10,694.36 3.19 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 7,967.94 8,984.69 696.31 4,174.72 4.55 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 589.36 16,730.22 6,846.12 7,461.23 2.92 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W8 5,933.10 7,826.93 482.41 3,437.78 3.92 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 375.45 10,742.43 4,801.29 5,153.48 2.51 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W10 3,888.27 4,802.89 311.11 1,518.33 3.40 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 586.63 7,826.93 3,292.12 3,437.78 2.17 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W12 3,292.12 4,802.89 977.93 1,518.33 2.88 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W12 3,292.12 4,802.89 977.93 1,518.33 2.88 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 586.63 7,826.93 3,292.12 3,437.78 2.17 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W10 3,888.27 4,802.89 311.11 1,518.33 3.40 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 375.45 10,742.43 4,801.29 5,153.48 2.51 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 5,933.10 7,826.93 482.41 3,437.78 3.92 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 589.36 16,730.22 6,846.12 7,461.23 2.92 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W6 7,967.94 8,984.69 696.31 4,174.72 4.55 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 803.27 24,373.24 8,880.96 10,694.36 3.19 x 0.188 1 C38BA= 1.125 x 1.845 x.199 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �Ii/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:30:52 PM NEW NI I L L E N N I U NI Location: Joist Description: Mark: aLm.nmic %V T6/.1S PORTLAND,OR Short Span Crimp 30K350/200 J18 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W4 10,012.77 10,742.43 910.22 5,153.48 5.23 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 1,063.97 28,624.38 11,325.24 12,322.60 4.07 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W2 16,712.07 23,679.79 1,674.84 4,874.47 3.46 x 0.230 1 R100=round 1 V1 2,365.46 8,984.69 3,619.73 4,378.72 2.07 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V2 1,650.00 5,758.64 2,848.40 3,026.99 2.06 x 0.090 1 C12BB= 1.125 x 0.799 x.090 STRESS ANALYSIS- PAGE 3 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 1:30:52 PM NEW N%ILLENNIUM Location: Joist Description: Mark: RIM.OWG SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J18 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 0-5 1/4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-0 7/8 BPL Length 2-6 5/8 Clear Bearing 0-3 7/8 Clear Bearing 0-9 1/8 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.00 Reqd TL Def L/80 0.07 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.00 Reqd LL Def L/120 0.04 Section Modulus 2.4356 Section Modulus 2.4356 Reqd SM 0.0000 Reqd SM 0.2189 Mom of Inertia 3.0580 Mom of Inertia 3.0580 Reqd MI 0.0000 Reqd MI 0.0425 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) // \\ `,,,N� /\ \ /, \ Concentrated Loads Conc @ 0-5 1/4 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a:LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b:DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM STRESS ANALYSIS- PAGE 1 ' Job Number: Job Name: Date Run: �+'/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:29:48 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J19 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 46-10 1/2 46-6 1/2 30.00 28.66 10 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-5 3-51/2 TC Panel 1-8 1-8 1/2 jel"1 ITT iffillIF iii ill[Ti 1 1111 1117ill l i i 1 IT First Half 2-0 2-0 First Diag. 5-5 5-5 1/2 Depth 30.00 30.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 46-10 1/2 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 46-10 1/2 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) SM(1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 46-10 1/2 L-BL Conc @ any pp(lbs) CL(1) 1,050.00 0.00 TC + Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 46-10 1/2 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 10,172.75 10,195.53 2,548.88 49,657.56 48,528.81 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,256.48 12,238.54 0.00 0.00 16,735.45 1,559.27 48.40 0-2 V 1 S 1,177.62 11,661.52 0.00 0.00 2,489.43 3,743.70 35.53 1-8 W3 1,177.62 11,661.52 18,137.26 1,860.71 1,063.97 11,440.25 37.38 3-5 W4 2,445.10 23,984.24 18,137.26 1,860.71 10,127.78 910.22 37.38 5-5 W5 2,445.10 23,984.24 29,245.03 2,960.81 803.27 8,984.75 37.38 7-5 W6 3,407.86 33,919.65 29,245.03 2,960.81 8,071.73 696.31 37.38 9-5 W7 3,407.86 33,919.65 38,008.09 3,786.25 589.36 6,939.39 37.38 11-5 W8 4,095.96 41,510.34 38,008.09 3,786.25 6,026.37 482.41 37.38 13-5 W9 4,095.96 41,510.34 44,426.43 4,337.01 375.45 4,883.34 37.38 15-5 W10 4,509.39 46,756.32 44,426.43 4,337.01 3,970.32 311.11 37.38 17-5 W11 4,509.39 46,756.32 48,500.03 4,613.11 646.24 3,324.55 37.38 19-5 W12 4,648.16 49,657.56 48,500.03 4,613.11 3,324.55 1,037.53 37.38 21-5 W12 4,648.16 49,657.56 48,528.81 4,614.54 3,324.55 1,037.53 37.38 23-5 W11 4,512.26 46,798.63 48,528.81 4,614.54 646.24 3,324.55 37.38 25-5 W10 4,512.26 46,798.63 44,480.94 4,341.30 3,970.32 311.11 37.38 27-5 W9 4,101.69 41,577.08 44,480.94 4,341.30 375.45 4,883.34 37.38 29-5 W8 4,101.69 41,577.08 38,087.04 3,793.40 6,026.37 482.41 37.38 31-5 W7 3,416.45 34,010.81 38,087.04 3,793.40 589.36 6,939.39 37.38 33-5 W6 3,416.45 34,010.81 29,348.40 2,970.83 8,071.73 696.31 37.38 35-5 W5 2,456.54 24,099.82 29,348.40 2,970.83 803.27 8,984.75 37.38 37-5 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:29:48 PM NEW NI I L L E N N I U M Location: Joist Description: Mark: eU,LOINo SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J19 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W4 2,456.54 24,099.82 18,265.05 1,873.59 10,127.78 910.22 37.38 39-5 W3 1,191.93 11,784.08 18,265.05 1,873.59 1,063.97 11,440.25 37.38 41-5 V1S 1,191.93 11,784.08 0.00 0.00 2,489.43 3,743.70 35.53 45-2 W2 1,355.60 12,365.68 0.00 0.00 16,881.44 1,674.84 48.80 43-5 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 1,750.00 2,948.40 28.66 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: i/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:29:48 PM NEW NI I L L E N N I U M Location: Joist Description: Mark: auILIIINUr.. SV97EMS PORTLAND,OR Short Span Crimp 30K350/200 J19 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 1.0162 0.8183 0.4925 1.5555 0.7604 0.6804 0.9652 A42A=2.6250 x.209 BC 0.8173 0.6134 0.3924 1.2964 0.5795 0.3076 1.0000 2021 =2 x 2 x.216 Axial and Bendin Analysis K: Y: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 746.13 276.50 414.75 21-0 25-111/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 18.00 45.00 24.00 45.00 18.50 1.1250 Bending Load 350.00 350.00 350.00 350.00 350.00 0.5 0..500000 Len 2X: Axial Load 12,238.54 11,661.52 49,657.56 11,784.08 12,365.68 fa Max Load Fillers TC: 3,531.23 5,737.81 24,432.97 5,798.11 3,567.92 54,747.40 Maximum K L/r 36.55 91.37 36.55 91.37 37.56 Max Load no Fillers TC: Fcr 43,918.29 26,773.67 43,918.29 26,773.67 43,685.70 51,956.74 Fa 26,350.97 16,064.20 26,350.97 16,064.20 26,211.42 TC OAL/Ryy: 359.05 F'e 779,458.63 94,645.03 591,531.44 94,645.03 737,895.13 BC OAURyy: Cm 0.9977 0.9697 0.9723 0.9694 0.9976 430.82 Panel Point Moment 6021.64 7142.57 2644.44 6542.98 6566.53 BC Stress: Mid Panel Moment 2255.56 5019.13 1750.00 5216.06 4354.17 0.99 Panel Point fb 2472.39 9786.91 3623.48 8965.34 2696.11 122.3242 . Mid Panel fb 1232 926.09 2804.64 977.88 2914.68 1787.75 Fillers 0 0 0 0 TC Shear Stress: 0 11,765.73 Panel Point Stress 6,003.62 15,524.72 28,056.45 14,763.45 6,264.02 BC Shear Stress: Mid Panel Stress 0.0992 0.4501 0.9586 0.4576 0.1302 12,212.00 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 16,735.45 23,679.79 1,559.27 4,956.14 3.46 x 0.230 1 R100= round 1 W3 1,063.97 28,624.38 11,440.25 12,322.60 4.11 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 10,127.78 10,742.43 910.22 5,153.48 5.29 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 803.27 24,373.24 8,984.75 10,694.36 3.23 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 8,071.73 8,984.69 696.31 4,174.72 4.61 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 589.36 16,730.22 6,939.39 7,461.23 2.96 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W8 6,026.37 7,826.93 482.41 3,437.78 3.98 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 375.45 10,742.43 4,883.34 5,153.48 2.55 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W10 3,970.32 4,802.89 311.11 1,518.33 3.47 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 646.24 7,826.93 3,324.55 3,437.78 2.19 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W12 3,324.55 4,802.89 1,037.53 1,518.33 2.91 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W12 3,324.55 4,802.89 1,037.53 1,518.33 2.91 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 646.24 7,826.93 3,324.55 3,437.78 2.19 x 0.102 1 Cl 6BB= 1.125 x 1.025 x.102 W10 3,970.32 4,802.89 311.11 1,518.33 3.47 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 W9 375.45 10,742.43 4,883.34 5,153.48 2.55 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 6,026.37 7,826.93 482.41 3,437.78 3.98 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 589.36 16,730.22 6,939.39 7,461.23 2.96 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W6 8,071.73 8,984.69 696.31 4,174.72 4.61 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 803.27 24,373.24 8,984.75 10,694.36 3.23 x 0.188 1 C38BA= 1.125 x 1.845 x.199 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:29:48 PM NEW MILLENNIUM Location: Joist Description: Mark: auu.nwr.. SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J19 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W4 10,127.78 10,742.43 910.22 5,153.48 5.29 x 0.129 1 C22BB= 1.125 x 1.110 x.129 ' W3 1,063.97 28,624.38 11,440.25 12,322.60 4.11 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W2 16,881.44 23,679.79 1,674.84 4,874.47 3.50 x 0.230 1 R100= round 1 V1 2,489.43 8,984.69 3,743.70 4,378.72 2.14 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V2 1,750.00 5,758.64 2,948.40 3,026.99 2.14 x 0.090 1 C12BB= 1.125 x 0.799 x.090 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: r// 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:29:48 PM NEW M I L L E N NI UNI Location: Joist Description: Mark: BUIL.niNr., SY%-l-FMs PORTLAND,OR Short Span Crimp 30K350/200 J19 TCX Design TCX Left TCX Right TCX Length 0-0 TCX Length 0-5 1/4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-0 7/8 BPL Length 2-6 5/8 Clear Bearing 0-3 7/8 Clear Bearing 0-g 1/8 BPL Material:2018=2 X 2 X.188 BPL Material: 2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.00 Reqd TL Def L/80 0.07 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.00 Reqd LL Def L/120 0.04 Section Modulus 2.4356 Section Modulus 2.4356 Reqd SM 0.0000 Reqd SM 0.2189 Mom of Inertia 3.0580 Mom of Inertia 3.0580 Reqd MI 0.0000 Reqd MI 0.0425 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) Concentrated Loads Conc @ 0-5 1/4 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) 1 Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) - Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) - -- - Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case Gc: DL+CL+ . STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: �/�/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:34:52 PM NEW MILLENNIUM Location: Joist Description: Mark: ELIILDIN6 SYSTEMS PORTLAND,OR Short Span Crimp 28K350/200 J2 Geometry Base Length: Working Length: I Joist Depth: I Effective Depth: BC Panel Length: Shape: 42-2 41-10 1 28.00 j 26.84 9 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-0 7/8 3-1 1/8 Ti� 1 T17TFTI---FTr-rrt-r, ...,n ._ L TC Panel 1-7 2-0 First Half 2-0 2-0 r First Diag. 5-0 7/8 5-1 1/8 Depth 28.00 28.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 42-2 L-BL Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 42-2 L-BL Uniform (plf) LL(1) 360.00 0.00 TC + 0-0 16-2 L-OAL Axial (lbs) WL(1) 412.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 42-2 L-BL Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere (lbs) CL(1) 350.00 0.00 TC + Conc Load (lbs) DL(1) 1,440.00 0.00 TC + 1-1 1-1 L-OAL Conc Load (lbs) WL(1) 412.00 0.00 TC + 34-0 40-0 L-OAL Gross Uplift(plf) WL(2) 105.00 105.00 TC - 0-0 42-2 L-BL Conc Load (lbs) WL(2) 412.00 0.00 TC - 34-0 40-0 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 12,354.97 8,766.48 3,088.74 42,621.41 42,860.53 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 2,860.43 14,016.45 0.00 0.00 18,486.92 3,611.09 44.01 0-2 V1S 2,688.89 12,513.16 0.00 0.00 419.99 4,269.95 32.25 1-7 W3 2,688.89 12,513.16 19,764.37 4,427.03 2,957.84 11,621.28 36.01 3-0 7/8 W4 5,907.47 25,670.48 19,764.37 4,427.03 9,362.47 2,599.09 36.01 5-0 7/8 W5 5,907.47 25,670.48 30,569.83 7,200.12 2,039.65 7,757.04 36.01 7-0 7/8 W6 8,304.99 34,538.58 30,569.83 7,200.12 6,818.00 1,658.88 36.01 9-0 7/8 W7 8,304.99 34,538.58 37,652.90 9,222.08 1,377.17 5,750.43 36.01 11-0 7/8 W8 9,951.39 39,988.96 37,652.90 9,222.08 4,811.39 1,095.46 36.01 13-0 7/8 W9 9,951.39 39,988.96 41,622.91 10,492.92 848.07 4,143.51 36.01 15-0 7/8 W10 10,846.66 42,621.41 41,622.91 10,492.92 4,143.51 848.07 36.01 17-0 7/8 W11 10,846.66 42,621.41 42,860.53 11,012.63 4,143.51 4,143.51 36.01 19-0 7/8 W11 10,990.81 41,851.04 42,860.53 11,012.63 4,143.51 4,143.51 36.01 21-0 7/8 W10 10,990.81 41,851.04 40,077.53 10,781.21 4,143.51 848.07 36.01 23-0 7/8 W9 10,383.83 37,678.07 40,077.53 10,781.21 848.07 4,143.51 36.01 25-0 7/8 W8 10,383.83 37,678.07 34,652.68 9,798.67 4,811.39 1,095.46 36.01 27-0 7/8 W7 9,025.72 31,001.35 34,652.68 9,798.67 1,377.17 5,750.43 36.01 29-0 7/8 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 G, Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:34:52 PM NEW MILLENNIUM Location: Joist Description: Mark: RUiLOWG SYSTEMA% PORTLAND,OR Short Span Crimp 28K350/200 J2 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W6 9,025.72 31,001.35 26,724.08 8,065.00 6,818.00 1,658.88 36.01 31-0 7/8 W5 6,705.42 21,820.87 26,724.08 8,065.00 2,039.65 7,757.04 36.01 33-0 7/8 W4 6,705.42 21,820.87 16,291.72 5,000.72 9,362.47 2,599.09 36.01 35-0 7/8 W3 3,056.90 10,868.89 16,291.72 5,000.72 2,957.84 11,621.28 36.01 37-0 7/8 V1S 3,056.90 10,868.89 0.00 0.00 1,079.42 2,121.64 29.88 40-2 W2 3,183.39 11,230.30 0.00 0.00 13,886.08 4,098.18 44.21 39-0 7/8 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 1,112.00 2,246.51 26.84 STRESS ANALYSIS- PAGE 2 lid Job Number: Job Name: Date Run: �i/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 1:34:52 PM NEW MILLENNIUM Location: Joist Description: Mark: RUILninir.. SYSTELAS PORTLAND,OR Short Span Crimp 28K350/200 J2 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024 a 2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 584.54 298.29 447.44 17-6 1/2 16-0 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 17.00 41.88 24.00 37.13 22.00 1.1250 Min Weld Len 2X: Bending Load 694.92 642.68 350.00 350.00 350.00 0.5000 Axial Load 14,016.45 12,513.16 42,621.41 10,868.89 11,230.30 Max Load Fillers TC: fa 4,254.63 6,723.89 22,902.42 5,840.35 3,408.91 49,625.71 Maximum K L/r 43.46 107.04 46.01 94.90 56.24 Max Load no Fillers TC: Fcr 43,551.60 21,633.42 42,829.38 25,881.38 39,677.35 45,547.55 TC Fa 26,130.96 12,980.05 25,697.63 15,528.83 23,806.41 3884.83 yy: 4.83OAL F'e 808,645.63 60,577.02 327,847.97 77,069.87 482,848.31 BC OAL/Ryy: Cm 0.9974 0.9445 0.9532 0.9621 0.9965 389.41 Panel Point Moment 9284.12 10310.37 2644.44 4809.62 7462.72 BC Stress: Mid Panel Moment 740.27 6538.12 1750.00 3804.63 4379.96 1.00 Panel Point fb 4576.99 21035.77 5395.34 9812.85 3679.06 BC 121..8888 93 Mid Panel fb 323.06 5595.18 1497.61 3255.92 2159.29 TC Shear Stress: Fillers 0 0 0 0 0 12,028.26 Panel Point Stress 8,831.62 27,759.66 28,297.76 15,653.20 7,087.97 BC Shear Stress: Mid Panel Stress 0.0922 0.7102 0.9391 0.4824 0.1442 15,840.42 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 18,486.92 26,972.16 3,611.09 9,598.50 3.59 x 0.245 1 R112=round 1 1/8 W3 2,957.84 28,624.38 11,621.28 12,786.97 4.17 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 9,362.47 10,742.43 2,599.09 5,330.90 4.89 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 2,039.65 18,714.09 7,757.04 8,898.52 2.97 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 6,818.00 7,826.93 1,658.88 3,564.90 4.50 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 1,377.17 14,381.54 5,750.43 6,928.23 2.58 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 4,811.39 5,758.64 1,095.46 2,157.24 3.60 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W9 848.07 8,984.69 4,143.51 4,326.22 2.36 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 4,143.51 4,802.89 848.07 1,636.66 3.62 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 W11 4,143.51 8,984.69 4,143.51 4,326.22 2.36 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W11 4,143.51 8,984.69 4,143.51 4,326.22 2.36 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 4,143.51 4,802.89 848.07 1,636.66 3.62 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 848.07 8,984.69 4,143.51 4,326.22 2.36 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 4,811.39 5,758.64 1,095.46 2,157.24 3.60 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 1,377.17 14,381.54 5,750.43 6,928.23 2.58 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 6,818.00 7,826.93 1,658.88 3,564.90 4.50 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W5 2,039.65 18,714.09 7,757.04 8,898.52 2.97 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W4 9,362.47 10,742.43 2,599.09 5,330.90 4.89 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 2,957.84 28,624.38 11,621.28 12,786.97 4.17 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 GJob Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:34:52 PM NEW MILLENNIUM Location: Joist Description: Mark: BUIL.p WC. SYSTEI.AS PORTLAND,OR Short Span Crimp 28K350/200 J2 Web Design Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 13,886.08 21,311.81 4,098.18 5,940.88 2.87 x 0.230 1 R100=round 1 V1 1,079.42 8,984.69 4,269.95 4,744.79 2.44 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V2 1,112.00 4,802.89 2,246.51 2,577.11 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 r/A Job Number: Job Name: Date Run- 1/9/2019 un: �/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:34:52 PM NEW MILLENNIUM Location: Joist Description: Mark: a�.in.nwr.. SY5TEM5 PORTLAND,OR Short Span Crimp 28K3501200 J2 TCX Design TCX Left TCX Right TCX Length 0-0 7/8 TCX Length 0-6 1/8 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-0 3/4 BPL Length 2-10 1/2 Clear Bearing 0-4 7/8 Clear Bearing 0-10 1/4 BPL Material:2018=2 X 2 X.188 BPL Material: 2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.01 Reqd TL Def L/80 0.08 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.01 Reqd LL Def L/120 0.05 Section Modulus 2.0284 Section Modulus 2.0284 Reqd SM 0.0040 Reqd SM 0.2488 Mom of Inertia 2.6899 Mom of Inertia 2.6899 Reqd MI 0.0002 Reqd MI 0.0540 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) `��, /2 N \ % Concentrated Loads Conc @ 0-6 1/8 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL im, Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) ' Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM ase C: I + t•.. +TT + +• •- - STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: ice/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:28:53 PM NEW MILLENNIUM Location: Joist Description: Mark: HUILOING SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J20 Geometry Base Length: Working Length: 1 Joist Depth: Effective Depth: BC Panel Length: Shape: 46-101/2 46.61/2 30.00 28.65 10 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-5 3-5 1/2 TC Panel 1-8 1_81/2 -I. 11111E111111 _Hi__ .. .1 1111 Ill 11 111111111111!111111 1 111111111111 I I First Half 2-0 2-0 First Diag. 5-5 5-5 1/2 Depth 30.00 30.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 46-10 1/2 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 46-10 1/2 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) SM(1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Uniform (plf) SM(1) 16.00 16.00 TC + 0-0 46-10 1/2 L-BL Conc @ any pp(lbs) CL(1) 1,900.00 0.00 TC + Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 46-10 1/2 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 11,013.61 11,040.96 2,760.24 53,816.44 52,338.62 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,256.98 12,821.36 0.00 0.00 18,160.15 1,559.68 48.39 0-2 V1S 1,178.09 12,244.10 0.00 0.00 3,543.69 4,798.15 35.52 1-8 W3 1,178.09 12,244.10 19,079.13 1,861.46 1,064.14 12,419.84 37.37 3-5 W4 2,446.08 25,284.50 19,079.13 1,861.46 11,107.15 910.37 37.37 5-5 W5 2,446.08 25,284.50 30,903.45 2,962.00 803.40 9,868.55 37.37 7-5 W6 3,409.23 35,935.98 30,903.45 2,962.00 8,955.38 696.43 37.37 9-5 W7 3,409.23 35,935.98 40,382.10 3,787.77 589.46 7,733.43 37.37 11-5 W8 4,097.61 44,241.80 40,382.10 3,787.77 6,820.26 482.49 37.37 13-5 W9 4,097.61 44,241.80 47,515.08 4,338.75 375.51 5,581.65 37.37 15-5 W10 4,511.20 50,201.95 47,515.08 4,338.75 4,668.48 436.29 37.37 17-5 W11 4,511.20 50,201.95 52,302.40 4,614.96 1,153.08 3,600.82 37.37 19-5 W12 4,650.02 53,816.44 52,302.40 4,614.96 3,600.82 1,544.44 37.37 21-5 W12 4,650.02 53,816.44 52,338.62 4,616.39 3,600.82 1,544.44 37.37 23-5 W11 4,514.07 50,251.69 52,338.62 4,616.39 1,153.08 3,600.82 37.37 25-5 W10 4,514.07 50,251.69 47,577.04 4,343.05 4,668.48 436.29 37.37 27-5 W9 4,103.33 44,315.97 47,577.04 4,343.05 375.51 5,581.65 37.37 29-5 W8 4,103.33 44,315.97 40,468.50 3,794.92 6,820.26 482.49 37.37 31-5 W7 3,417.82 36,034.59 40,468.50 3,794.92 589.46 7,733.43 37.37 33-5 W6 3,417.82 36,034.59 31,014.28 2,972.02 8,955.38 696.43 37.37 35-5 W5 2,457.53 25,407.54 31,014.28 2,972.02 803.40 9,868.55 37.37 37-5 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: �/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:28:53 PM NEW MILLENNIUM Location: Joist Description: Mark: MUM 171ING SV%1-F AS PORTLAND,OR Short Span Crimp 30K350/200 J20 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W4 2,457.53 25,407.54 19,214.40 1,874.34 11,107.15 910.37 37.37 39-5 W3 1,192.40 12,374.13 19,214.40 1,874.34 1,064.14 12,419.84 37.37 41-5 V1S 1,192.40 12,374.13 0.00 0.00 3,543.69 4,798.15 35.52 45-2 W2 1,356.15 12,955.96 0.00 0.00 18,325.85 1,675.28 48.80 43-5 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 2,600.00 3,798.48 28.65 , STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: moi/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:28:53 PM NEW MILLENNIUM Location: Joist Description: Mark: BUIL.RLNC 'S'V TEM5 PORTLAND,OR Short Span Crimp 30K350/200 J20 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.0162 0.8183 0.4925 1.5555 0.7604 0.6804 0.9652 A42A=2.6250 x.209 BC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 799.37 296.23 444.34 21-0 26-11/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 18.00 45.00 24.00 45.00 18.50 1.1250 Bending Load 350.00 350.00 350.00 350.00 350.00 Min Weld Len 2X. 0.5000 Axial Load 12,821.36 12,244.10 53,816.44 12,374.13 12,955.96 fa Max Load Fillers TC: 3,699.39 6,024.46 26,479.26 6,088.43 3,738.23 54,747.40 Maximum K L/r 36.55 91.37 24.37 91.37 37.56 Max Load no Fillers TC: Fcr 43,918.29 26,773.67 46,279.65 26,773.67 43,685.70 51,956.74 TC Fa 26,350.97 16,064.20 27,767.79 16,064.20 26,211.42 OAL3559.059.05 yy: Fe 779,458.63 94,645.03 591,531.44 94,645.03 737,895.13 BC OAL/Ryy: Cm 0.9976 0.9682 0.9700 0.9678 0.9975 428.14 Panel Point Moment 6021.64 7142.57 2644.44 6542.98 6566.53 BC Stress: Mid Panel Moment 2255.56 5019.13 1750.00 5216.06 4354.17 0.94 Panel Point fb 2472.39 9786.91 3623.48 8965.34 2696.11 1BC L/Rz : 22.69 Mid Panel fb 122.6994 926.09 2804.64 977.88 2914.68 1787.75 Fillers 0 0 2 0 0 TC Shear Stress: 12,769.49 Panel Point Stress 6,171.78 15,811.37 30,102.74 15,053.77 6,434.34 BC Shear Stress: Mid Panel Stress 0.1024 0.4683 0.9851 0.4760 0.1334 11,555.32 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 18,160.15 23,679.79 1,559.68 4,957.54 3.76 x 0.230 1 R100= round 1 W3 1,064.14 28,624.38 12,419.84 16,326.31 4.46 x 0.188 1 CW4OBA= 1.5 x 1.926 x.218 W4 11,107.15 14,381.54 910.37 6,696.07 4.99 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 803.40 24,373.24 9,868.55 10,696.87 3.54 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 8,955.38 10,742.43 696.43 5,154.62 4.68 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W7 589.46 18,714.09 7,733.43 8,594.42 2.96 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W8 6,820.26 7,826.93 482.49 3,438.59 4.50 x 0.102 1 Cl6BB= 1.125 x 1.025 x.102 W9 375.51 14,381.54 5,581.65 6,696.07 2.51 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W10 4,668.48 4,802.89 436.29 1,519.05 4.08 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 1,153.08 8,984.69 3,600.82 4,175.69 2.06 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W12 3,600.82 5,758.64 1,544.44 2,003.81 2.69 x 0.090 1 Cl2BB= 1.125 x 0.799 x.090 W12 3,600.82 5,758.64 1,544.44 2,003.81 2.69 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W11 1,153.08 8,984.69 3,600.82 4,175.69 2.06 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 4,668.48 4,802.89 436.29 1,519.05 4.08 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 375.51 14,381.54 5,581.65 6,696.07 2.51 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 6,820.26 7,826.93 482.49 3,438.59 4.50 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 589.46 18,714.09 7,733.43 8,594.42 2.96 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 8,955.38 10,742.43 696.43 5,154.62 4.68 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 803.40 24,373.24 9,868.55 10,696.87 3.54 x 0.188 1 C38BA= 1.125 x 1.845 x.199 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 f/rl Job Number: Job Name: Date Run: moi/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 1:28:53 PM NEW MILLENNIUM Location: Joist Description: Mark: 91.1I1..O1NC %Y97E�A9 PORTLAND,OR Short Span Crimp 30K350/200 J20 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W4 11,107.15 14,381.54 910.37 6,696.07 4.99 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 1,064.14 28,624.38 12,419.84 16,326.31 4.46 x 0.188 1 CW40BA= 1.5 x 1.926 x.218 W2 18,325.85 23,679.79 1,675.28 4,875.81 3.79 x 0.230 1 R100= round 1 V1 3,543.69 10,742.43 4,798.15 5,393.48 2.50 x 0.129 1 C22BB= 1.125 x 1.110 x.129 V2 2,600.00 7,826.93 3,798.48 4,277.76 2.45 x 0.102 1 C16BB= 1.125 x 1.025 x.102 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: �/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:28:53 PM NEW NI I L L E N N I UN% Location: Joist Description: Mark: wUIi.niNc SV WTIE nAs PORTLAND,OR Short Span Crimp 30K350/200 J20 TCX Design TCX Left TCX Right TCX Length 0-0 _ TCX Length 0-5 1/4 --. --.- -- TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-1 BPL Length 2-6 3/4 Clear Bearing 0-3 7/8 Clear Bearing 0-9 1/8 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.00 Reqd TL Def L/80 0.07 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.00 Reqd LL Def L/120 0.04 Section Modulus 2.4356 Section Modulus 2.4356 Reqd SM 0.0000 Reqd SM 0.2189 Mom of Inertia 3.0580 Mom of Inertia 3.0580 Reqd MI 0.0000 Reqd MI 0.0425 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) � > N` /'''Y Concentrated Loads Conc @ 0-5 1/4 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b: 0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM - Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) - - Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM aoe . . -- ..-- 'FLfG ,. A-' / STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:26:45 AM NEW M I L L E N N I U M Location: Joist Description: Mark: B"""'^'° SYSTEMS PORTLAND,OR Short Span Round 12K300/162 J23 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 20-0 1/2 19-8 1/2 12.00 11.05 10 @ 1-8 Parallel Chords Variable Left End Right End BC Panel 1-8 1/4 1-8 1/4 1 TC Panel 0-10 1/4 0-101/4 T� � I IIII�, i�11� � _.11 _ ,.- I 111 =u 111 ; 1 First Half 0-10 0-10 �IIlli �� �� '' ' First Diag. 2-6 1/4 2-6 1/4 Depth 12.00 12.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 138.00 138.00 TC + 0-0 20-0 1/2 L-BL Uniform (plf) LL(1) 162.00 162.00 TC + 0-0 20-0 1/2 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) WL(1) 412.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) SM(1) 14.00 14.00 TC + 0-0 20-0 1/2 L-BL Axial (lbs) SM(1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Conc Load (lbs) WL(1) 412.00 0.00 TC + 3-0 9-0 L-OAL Conc Load (lbs) WL(1) 412.00 0.00 TC + 14-0 20-0 L-OAL Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 20-0 1/2 L-BL Conc Load (lbs) WL(2) 412.00 0.00 TC - 3-0 9-0 L-OAL Conc Load (lbs) WL(2) 412.00 0.00 TC - 14-0 20-0 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 20.00 20.00 3,932.38 3,943.59 985.90 23,054.58 20,960.66 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 3,934.89 7,371.90 0.00 0.00 7,440.85 4,778.12 21.33 0-2 V1S 2,289.66 7,095.35 0.00 0.00 3,962.77 1,848.88 14.90 0-10 1/4 W3 2,289.66 7,095.35 7,936.78 2,800.53 1,154.52 4,615.56 14.90 1-8 1/4 W4 3,265.01 12,082.62 7,936.78 2,800.53 4,032.13 1,062.34 14.90 2-61/4 W5 3,265.01 12,082.62 12,463.63 3,729.48 1,013.10 3,875.67 14.90 3-41/4 W6 4,147.55 16,286.74 12,463.63 3,729.48 3,292.24 920.92 14.90 4-2 1/4 W7 4,147.55 16,286.74 16,234.02 4,565.63 878.71 3,158.13 14.90 5-01/4 W8 4,937.30 19,707.72 16,234.02 4,565.63 2,574.71 786.53 14.90 5-10 1/4 W9 4,937.30 19,707.72 19,263.42 5,308.97 738.37 2,418.24 14.90 6-81/4 W10 5,372.60 22,071.04 19,263.42 5,308.97 1,834.82 645.11 14.90 7-61/4 W11 5,372.60 22,071.04 20,960.66 5,440.28 509.30 1,471.31 14.90 8-4 1/4 W12 5,439.10 23,054.58 20,960.66 5,440.28 1,165.59 1,329.94 14.90 9-2 1/4 W12 5,439.10 23,054.58 20,958.88 5,437.91 1,165.59 1,329.94 14.90 10-0 1/4 W11 5,374.86 22,072.74 20,958.88 5,437.91 509.30 1,471.31 14.90 10-10 1/4 W10 5,374.86 22,072.74 19,268.59 5,314.14 1,834.82 645.11 14.90 11-8 1/4 W9 4,945.94 19,716.36 19,268.59 5,314.14 738.37 2,418.24 14.90 12-61/4 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: i/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 10:26:45 AM NEW MILLENNIUM Location: Joist Description: Mark: auILniNr SY57ELA9 PORTLAND,OR Short Span Round 12K300/162 J23 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W8 4,945.94 19,716.36 16,246.13 4,577.74 2,574.71 786.53 14.90 13-41/4 W7 4,157.89 16,297.08 16,246.13 4,577.74 878.71 3,158.13 14.90 14-21/4 W6 4,157.89 16,297.08 12,463.63 3,738.04 3,292.24 920.92 14.90 15-01/4 W5 3,271.79 12,089.40 12,463.63 3,738.04 1,013.10 3,875.67 14.90 15-101/4 W4 3,271.79 12,089.40 7,936.78 2,805.55 4,032.13 1,062.34 14.90 16-81/4 W3 2,292.90 7,098.58 7,936.78 2,805.55 1,154.52 4,615.56 14.90 17-61/4 V1S 2,292.90 7,098.58 0.00 0.00 3,962.77 1,848.88 14.90 19-2 1/4 W2 3,938.13 7,375.13 0.00 0.00 7,440.85 4,778.12 21.33 18-41/4 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:26:45 AM NEW MI L L E N N IUM Location: Joist Description: Mark: BUIL river. SY%T6M5 PORTLAND,OR Short Span Round 12K300/162 J23 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.5206 0.5580 0.3331 0.9584 0.5292 0.1621 1.0000 A30B= 1.7970 x 0.158 BC 0.3922 0.4635 0.2955 0.8194 0.4256 0.0843 0.9945 1513= 1 1/2 x 1 1/2 x.137 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 55.07 268.76 403.14 11-10 5/8 10-81/2 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 8.25 20.00 20.00 20.00 8.25 0.5000 Bending Load 300.00 300.00 300.00 300.00 300.00 0.5 0..500000 Len 2x. Axial Load 7,371.90 7,095.35 23,054.58 7,098.59 7,375.13 fa Max Load Fillers TC: 2,979.03 6,814.59 22,142.31 6,817.70 2,980.33 26,560.31 Maximum K L/r 35.31 60.04 45.03 60.04 35.31 Max Load no Fillers TC: Fcr 45,643.72 38,414.38 43,109.91 38,414.38 45,643.72 25,090.48 TC Fa 27,386.23 23,048.63 25,865.95 23,048.63 27,386.23 246.77 46.77OALyy: Fe 3,491,891.25 222,795.39 396,080.69 222,795.39 3,491,891.25 BCOAL/Ryy: Cm 0.9996 0.9847 0.9625 0.9847 0.9996 288.63 Panel Point Moment 17286.08 2044.82 1870.37 2044.82 17286.08 BC Stress: Mid Panel Moment 13815.52 1528.42 1291.67 1528.42 13815.52 0.89 Panel Point fb 9749.88 7996.37 7314.18 7996.37 9749.88 6BC L/Rz : 7.681 Mid Panel fb 7792.38 2494.88 2108.42 2494.88 7792.38 67.6819 Fillers 0 0 TC Shear Stress: 0 9,294.63 Panel Point Stress 12,728.91 14,810.95 29,456.49 14,814.06 12,730.22 BC Shear Stress: Mid Panel Stress 0.3144 0.3724 0.9224 0.37250.3144 10,214.46 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 7,440.85 10,072.50 4,778.12 5,444.11 2.00 x 0.192 1 R068= round 11/16 V1S 3,962.77 9,250.01 1,848.88 5,396.49 2.00 x 0.185 1 R062= round 5/8 W3 1,154.52 9,250.01 4,615.56 5,396.49 2.00 x 0.185 1 R062= round 5/8 W4 4,032.13 9,250.01 1,062.34 5,396.49 2.00 x 0.185 1 R062= round 5/8 W5 1,013.10 9,250.01 3,875.67 5,396.49 2.00 x 0.185 1 R062= round 5/8 W6 3,292.24 9,250.01 920.92 5,396.49 2.00 x 0.185 1 R062=round 5/8 W7 878.71 9,250.01 3,158.13 5,396.49 2.00 x 0.185 1 R062=round 5/8 W8 2,574.71 5,918.44 786.53 2,551.34 2.00 x 0.170 1 R050= round 1/2 W9 738.37 5,918.44 2,418.24 2,551.34 2.00 x 0.170 1 R050= round 1/2 W10 1,834.82 5,918.44 645.11 2,551.34 2.00 x 0.170 1 R050= round 1/2 W11 509.30 5,918.44 1,471.31 2,551.34 2.00 x 0.170 1 R050= round 1/2 W12 1,165.59 5,918.44 1,329.94 2,551.34 2.00 x 0.170 1 R050=round 1/2 W12 1,165.59 5,918.44 1,329.94 2,551.34 2.00 x 0.170 1 R050=round 1/2 W11 509.30 5,918.44 1,471.31 2,551.34 2.00 x 0.170 1 R050= round 1/2 W10 1,834.82 5,918.44 645.11 2,551.34 2.00 x 0.170 1 R050= round 1/2 W9 738.37 5,918.44 2,418.24 2,551.34 2.00 x 0.170 1 R050= round 1/2 W8 2,574.71 5,918.44 786.53 2,551.34 2.00 x 0.170 1 R050= round 1/2 W7 878.71 9,250.01 3,158.13 5,396.49 2.00 x 0.185 1 R062=round 5/8 W6 3,292.24 9,250.01 920.92 5,396.49 2.00 x 0.185 1 R062= round 5/8 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 /�� Job Number: Job Name: Date Run: �j/if 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 10:26:45 AM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEM% PORTLAND,OR Short Span Round 12K300/162 J23 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W5 1,013.10 9,250.01 3,875.67 5,396.49 2.00 x 0.185 1 R062=round 5/8 W4 4,032.13 9,250.01 1,062.34 5,396.49 2.00 x 0.185 1 R062=round 5/8 W3 1,154.52 9,250.01 4,615.56 5,396.49 2.00 x 0.185 1 R062= round 5/8 V1S 3,962.77 9,250.01 1,848.88 5,396.49 2.00 x 0.185 1 R062= round 5/8 W2 7,440.85 10,072.50 4,778.12 5,444.11 2.00 x 0.192 1 R068=round 11/16 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: f/�/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:26:45 AM NEW MILLENNIUM Location: Joist Description: Mark: euILninir.. SYSTEMS PORTLAND,OR Short Span Round 12K300/162 J23 TCX Design TCX Left TCX Right TCX Length 1-5 3/8 TCX Length 1-5 3/8 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-8 7/8 BPL Length 2-8 7/8 Clear Bearing 1-10 Clear Bearing 1-10 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 300.00 Total Load 300.00 Reqd TL Def L/80 0.22 Reqd TL Def L/80 0.22 Live Load 162.00 Live Load 162.00 Reqd LL Def L/120 0.14 Reqd LL Def L/120 0.14 Section Modulus 1.5323 Section Modulus 1.5323 Reqd SM 0.5762 Reqd SM 0.5762 Mom of Inertia 2.0548 Mom of Inertia 2.0548 Reqd MI 0.2871 Reqd MI 0.2871 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) `\ /> I /% // Concentrated Loads Concentrated Loads Conc @ 1-5 3/8 650.00 Conc @ 1-5 3/8 650.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) - Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case Cc: DL+CL+0.05(TL)+WL+C+AX*IP STRESS ANALYSIS- PAGE 1 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:26:59 AM NEW MILLENNIUM Location: Joist Description: Mark: BLIILCNN❑ SYSTEMS PORTLAND,OR Short Span Round 14K300/162 J24 Geometry Base Length: Working Length: I Joist Depth: Effective Depth: BC Panel Length: Shape: 20-01/4 19-81/4 L 14.00 j 13.07 10 @ 1-8 Parallel Chords Variable Left End Right End BC Panel 1-8 1/8 1-8 1/8 111 1 11 1 TIT "IF 111I 11 ' 1TfT 11111TC Panel 0-10 0-10111 � First Half 0-10 0-10 First Diag. 2-6 1/8 2-6 1/8 Depth 14.00 14.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 138.00 138.00 TC + 0-0 20-0 1/4 L-BL Uniform (plf) LL(1) 162.00 162.00 TC + 0-0 20-0 1/4 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Uniform (plf) SM(1) 14.00 14.00 TC + 0-0 20-0 1/4 L-BL Axial (lbs) WL(1) 412.00 0.00 TC + 0-0 0-0 L-BL Conc Load (lbs) WL(1) 412.00 0.00 TC + 3-0 9-0 L-OAL Conc Load (lbs) WL(1) 412.00 0.00 TC + 14-0 20-0 L-OAL Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 20-0 1/4 L-BL Conc Load (lbs) WL(2) 412.00 0.00 TC - 3-0 9-0 L-OAL Conc Load (lbs) WL(2) 412.00 0.00 TC - 14-0 20-0 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 20.00 20.00 3,929.78 3,940.47 985.12 19,748.83 17,675.85 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 3,399.58 6,500.61 0.00 0.00 6,585.47 4,350.04 22.35 0-2 V1S 2,050.84 6,265.10 0.00 0.00 3,821.69 1,729.25 16.54 0-10 W3 2,050.84 6,265.10 6,672.13 2,369.34 1,077.62 4,309.27 16.46 1-8 1/8 W4 2,761.74 10,479.49 6,672.13 2,369.34 3,763.06 991.32 16.46 2-61/8 W5 2,761.74 10,479.49 10,496.52 3,154.13 951.93 3,637.89 16.46 3-4 1/8 W6 3,507.33 14,031.22 10,496.52 3,154.13 3,093.38 865.90 16.46 4-2 1/8 W7 3,507.33 14,031.22 13,682.68 3,860.53 819.94 2,947.36 16.46 5-0 1/8 W8 4,174.52 16,921.34 13,682.68 3,860.53 2,402.85 733.91 16.46 5-10 1/8 W9 4,174.52 16,921.34 16,241.99 4,488.52 689.11 2,256.82 16.46 6-8 1/8 W10 4,531.40 18,917.92 16,241.99 4,488.52 1,712.31 601.92 16.46 7-6 1/8 W11 4,531.40 18,917.92 17,675.85 4,588.27 475.10 1,373.00 16.46 8-4 1/8 W12 4,587.27 19,748.83 17,675.85 4,588.27 1,086.86 1,240.24 16.46 9-2 1/8 W12 4,587.27 19,748.83 17,674.35 4,586.27 1,086.86 1,240.24 16.46 10-0 1/8 W11 4,533.00 18,919.35 17,674.35 4,586.27 475.10 1,373.00 16.46 10-10 1/8 W10 4,533.00 18,919.35 16,246.35 4,492.88 1,712.31 601.92 16.46 11-8 1/8 W9 4,181.81 16,928.63 16,246.35 4,492.88 689.11 2,256.82 16.46 12-61/8 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 /�/� Job Number: Job Name: Date Run: �/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:26:59 AM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYBTELA9 PORTLAND,OR Short Span Round 14K300/162 J24 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W8 4,181.81 16,928.63 13,692.91 3,870.75 2,402.85 733.91 16.46 13-41/8 W7 3,516.05 14,039.94 13,692.91 3,870.75 819.94 2,947.36 16.46 14-2 1/8 W6 3,516.05 14,039.94 10,496.51 3,161.35 3,093.38 865.90 16.46 15-01/8 W5 2,767.46 10,485.21 10,496.51 3,161.35 951.93 3,637.89 16.46 15-101/8 W4 2,767.46 10,485.21 6,672.13 2,373.56 3,763.06 991.32 16.46 16-81/8 W3 2,050.84 6,267.82 6,672.13 2,373.56 1,077.62 4,309.27 16.46 17-61/8 V1S 2,050.84 6,267.82 0.00 0.00 3,821.69 1,729.25 16.54 19-2 1/4 W2 3,402.30 6,503.33 0.00 0.00 6,585.47 4,350.04 22.35 18-41/8 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 10:26:59 AM NEW MILLENNIUM Location: Joist Description: Mark: AUILrIING • YSTEBAA PORTLAND,OR Short Span Round 14K300/162 J24 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.4771 0.5392 0.3214 0.9323 0.5106 0.1387 1.0000 A28B= 1.7350 x 0.150 BC 0.3151 0.4675 0.2972 0.8133 0.4154 0.0689 0.9057 1510= 1 1/2 x 1 1/2 x.109 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 65.29 319.65 479.47 11-10 5/8 10-4 3/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 8.00 20.13 20.00 20.13 8.00 0.5000 Bending Load 300.00 300.00 300.00 300.00 300.00 Min Weld Len 2X: 0.5000 Axial Load 6,500.61 6,265.10 19,748.83 6,267.82 6,503.33 fa Max Load Fillers TC: 2,722.65 6,565.81 20,696.74 6,568.67 2,723.79 23,966.52 Maximum K L/r 36.30 62.62 46.67 62.62 36.30 Max Load no Fillers TC: Fcr 45,408.36 37,537.53 42,638.66 37,537.53 45,408.36 22,510.16 TC Fa 27,245.01 22,522.52 25,583.20 22,522.52 27,245.01 OAL2553.40 Ryy: 3.40 F'e 3,706,204.25 205,459.27 369,840.97 205,459.27 3,706,204.25 BC OAL/R Cm yy� 0.9996 0.9840 0.9625 0.9840 0.9996 290.49 Panel Point Moment 17428.07 2034.72 1870.37 2034.72 17428.07 BC Stress: Mid Panel Moment 13971.88 1510.55 1291.67 1510.55 13971.88 0.93 Panel Point fb 10013.26 8980.95 8255.52 8980.95 10013.26 6BC L/Rz : 7.294 Mid Panel fb 67.2948 8027.52 2780.41 2377.52 2780.41 8027.52 TC Shear Stress: Fillers 0 0 0 10,018.28 Panel Point Stress 12,735.91 15,546.76 28,952.26 15,549.61 12,737.05 BC Shear Stress: Mid Panel Stress 0.3178 0.3772 0.8838 0.3773 0.3178 12,520.48 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 6,585.47 10,072.50 4,350.04 5,074.58 2.00 x 0.192 1 R068= round 11/16 V1S 3,821.69 9,250.01 1,729.25 4,762.92 2.00 x 0.185 1 R062= round 5/8 W3 1,077.62 9,250.01 4,309.27 4,792.10 2.00 x 0.185 1 R062=round 5/8 W4 3,763.06 9,250.01 991.32 4,792.10 2.00 x 0.185 1 R062=round 5/8 W5 951.93 9,250.01 3,637.89 4,792.10 2.00 x 0.185 1 R062=round 5/8 W6 3,093.38 9,250.01 865.90 4,792.10 2.00 x 0.185 1 R062= round 5/8 W7 819.94 9,250.01 2,947.36 4,792.10 2.00 x 0.185 1 R062= round 5/8 W8 2,402.85 9,250.01 733.91 4,792.10 2.00 x 0.185 1 R062= round 5/8 W9 689.11 9,250.01 2,256.82 4,792.10 2.00 x 0.185 1 R062= round 5/8 W10 1,712.31 5,918.44 601.92 2,115.50 2.00 x 0.170 1 R050=round 1/2 W11 475.10 5,918.44 1,373.00 2,115.50 2.00 x 0.170 1 R050=round 1/2 W12 1,086.86 5,918.44 1,240.24 2,115.50 2.00 x 0.170 1 R050=round 1/2 W12 1,086.86 5,918.44 1,240.24 2,115.50 2.00 x 0.170 1 R050=round 1/2 W11 475.10 5,918.44 1,373.00 2,115.50 2.00 x 0.170 1 R050= round 1/2 W10 1,712.31 5,918.44 601.92 2,115.50 2.00 x 0.170 1 R050= round 1/2 W9 689.11 9,250.01 2,256.82 4,792.10 2.00 x 0.185 1 R062= round 5/8 W8 2,402.85 9,250.01 733.91 4,792.10 2.00 x 0.185 1 R062= round 5/8 W7 819.94 9,250.01 2,947.36 4,792.10 2.00 x 0.185 1 R062=round 5/8 W6 3,093.38 9,250.01 865.90 4,792.10 2.00 x 0.185 1 R062= round 5/8 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 (f Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 10:26:59 AM NEW MILLENNIUM Location: Joist Description: Mark: RimniNo <..Y%-rFAAS PORTLAND,OR Short Span Round 14K300/162 J24 Web Design Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W5 951.93 9,250.01 3,637.89 4,792.10 2.00 x 0.185 1 R062= round 5/8 W4 3,763.06 9,250.01 991.32 4,792.10 2.00 x 0.185 1 R062=round 5/8 W3 1,077.62 9,250.01 4,309.27 4,792.10 2.00 x 0.185 1 R062=round 5/8 V1S 3,821.69 9,250.01 1,729.25 4,762.92 2.00 x 0.185 1 R062=round 5/8 W2 6,585.47 10,072.50 4,350.04 5,074.58 2.00 x 0.192 1 R068= round 11/16 STRESS ANALYSIS- PAGE 3 r Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:26:59 AM NEW NII L L E N NI UN% Location: Joist Description: Mark: BUIL.nING SYSTEMS PORTLAND,OR Short Span Round 14K300/162 J24 TCX Design TCX Left TCX Right TCX Length 1-5 1/2 TCX Length 1-5 1/2 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-8 3/8 BPL Length 2-8 3/8 Clear Bearing 1-9 5/8 Clear Bearing 1-9 5/8 BPL Material:2018=2 X 2 X.188 BPL Material: 2018=2 X 2 X.188 Total Load 300.00 Total Load 300.00 Reqd TL Def L/80 0.22 Reqd TL Def L/80 0.22 Live Load 162.00 Live Load 162.00 Reqd LL Def L/120 0.15 Reqd LL Def L/120 0.15 Section Modulus 1.4515 Section Modulus 1.4515 Reqd SM 0.5809 Reqd SM 0.5809 Mom of Inertia 1.9787 Mom of Inertia 1.9787 Reqd MI 0.2912 Reqd MI 0.2912 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) ,\ ; / ii' � // 'NN A, // , Concentrated Loads Concentrated Loads Conc @ 1-5 1/2 650.00 Conc @ 1-5 1/2 650.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TLj0.75(WL-AX+SL+-SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case Cc: DL+CL+0.85(iL)-WL*C+AX+FP // STRESS ANALYSIS- PAGE 1 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:49:37 AM NEW MILLENNIUM Location: Joist Description: Mark: BLLLOWG SYSTEMS PORTLAND,OR Short Span Crimp 28K350/200 J5 Geometry Base Length: Working Length: !Joist Depth: Effective Depth: BC Panel Length: Shape: 42-2 7/8 41-10 7/8 28.00 26.84 9 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-0 5/8 3-2 1/4 7 7� 7 TC Panel 1 7 2 0 �iiinIAIII.5 T 1 113.: in,-S.._._.. i_ '.............'`'' a.- ......_ems --' tr ,�,_-..,.. •. . First Half 2-0 2-0 First Diag. 5-0 5/8 5-2 1/4 Depth 28.00 28.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 42-2 7/8 L-BL Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 42-2 7/8 L-BL Uniform (plf) LL(1) 360.00 0.00 TC + 0-0 16-2 L-OAL Axial (lbs) WL(1) 412.00 0.00 TC + 0-0 0-0 L-BL Axial(lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 42-2 7/8 L-BL Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Conc Load (lbs) DL(1) 1,440.00 0.00 TC + 1-1 1-1 L-OAL Conc Load (lbs) WL(1) 412.00 0.00 TC + 34-0 40-0 L-OAL Gross Uplift(plf) WL(2) 105.00 105.00 TC - 0-0 42-2 7/8 L-BL Conc Load (lbs) WL(2) 412.00 0.00 TC - 34-0 40-0 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 12,364.67 8,777.57 3,091.17 42,729.22 42,990.73 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 2,845.22 13,969.47 0.00 0.00 18,471.48 3,601.54 43.81 0-2 V1S 2,676.79 12,482.22 0.00 0.00 417.19 4,281.61 32.11 1-7 W3 2,676.79 12,482.22 19,739.05 4,419.58 2,952.70 11,643.44 36.01 3-0 5/8 W4 5,905.64 25,665.12 19,739.05 4,419.58 9,392.42 2,587.36 36.01 5-0 5/8 W5 5,905.64 25,665.12 30,583.96 7,203.91 2,016.83 7,752.84 36.01 7-0 5/8 W6 8,314.40 34,571.82 30,583.96 7,203.91 6,788.86 1,667.31 36.01 9-0 5/8 W7 8,314.40 34,571.82 37,704.98 9,237.12 1,385.60 5,721.29 36.01 11-0 5/8 W8 9,972.04 40,059.68 37,704.98 9,237.12 4,782.25 1,103.89 36.01 13-0 5/8 W9 9,972.04 40,059.68 41,712.18 10,519.19 849.26 4,146.76 36.01 15-05/8 W10 10,878.56 42,729.22 41,712.18 10,519.19 4,146.76 849.26 36.01 17-05/8 W11 10,878.56 42,729.22 42,990.73 11,050.15 4,146.76 4,146.76 36.01 19-05/8 W11 11,033.95 42,021.55 42,990.73 11,050.15 4,146.76 4,146.76 36.01 21-0 5/8 W10 11,033.95 42,021.55 40,266.57 10,829.97 4,146.76 849.26 36.01 23-0 5/8 W9 10,438.21 37,885.66 40,266.57 10,829.97 849.26 4,146.76 36.01 25-0 5/8 W8 10,438.21 37,885.66 34,878.80 9,858.67 4,782.25 1,103.89 36.01 27-0 5/8 W7 9,091.35 31,246.01 34,878.80 9,858.67 1,385.60 5,721.29 36.01 29-0 5/8 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 /�/� Job Number: Job Name: Date Run. �/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:49:37 AM NEW MILLENNIUM Location: Joist Description: Mark: RUIL.minrr.. SYSTEMA PORTLAND,OR Short Span Crimp 28K350/200 J5 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W6 9,091.35 31,246.01 26,987.28 8,136.25 6,788.86 1,667.31 36.01 31-0 5/8 W5 6,791.89 22,102.61 26,987.28 8,136.25 2,016.83 7,752.84 36.01 33-0 5/8 W4 6,791.89 22,102.61 16,592.00 5,092.81 9,392.42 2,587.36 36.01 35-0 5/8 W3 3,150.21 11,141.55 16,592.00 5,092.81 2,952.70 11,643.44 36.01 37-0 5/8 V 1 S 3,150.21 11,141.55 0.00 0.00 1,063.42 2,177.31 30.39 40-2 7/8 W2 3,290.16 11,541.40 0.00 0.00 14,188.81 4,187.52 45.10 39-0 5/8 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 1,112.00 2,247.03 26.84 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: /� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:49:37 AM NEW MILLENNIUM Location: Joist Description: Mark: FILM.oinro %V%TE�+s PORTLAND,OR Short Span Crimp 28K350/200 J5 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 584.54 296.74 445.11 17-61/2 15-113/4 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 17.00 41.63 24.00 38.25 22.00 1.1250 BendingLoad Min Weld Len 2X: 694.90 642.82 350.00 350.00 350.00 0.5000 Axial Load 13,969.47 12,482.22 42,729.22 11,141.55 11,541.40 Max Load Fillers TC: fa 4,240.37 6,707.26 22,960.36 5,986.86 3,503.34 49,625.71 Maximum K L/r 43.46 106.40 46.01 97.78 56.24 MaxLoadnoFillersTC: Fcr 43,551.60 21,850.26 42,829.38 24,853.79 39,677.35 45,547.55 TC Fa 26,130.96 13,110.16 25,697.63 14,912.27 23,806.41 OAL3885.50 Ryy: 5.50 F'e 808,645.63 61,306.86 327,847.97 72,603.02 482,848.31 BC OAL/Ryy: Cm 0.9974 0.9453 0.9531 0.9588 0.9964 390.09 Panel Point Moment 9187.80 10201.08 2644.44 5132.82 6947.88 BC Stress: Mid Panel Moment 780.79 6471.22 1750.00 3965.67 3995.07 1.00 Panel Point fb 4529.51 20812.81 5395.34 10472.26 3425.25 BC 121..8888 93 Mid Panel fb 340.75 5537.92 1497.61 3393.73 1969.54 Fillers TC Shear Stress: 0 0 0 0 0 12,063.26 Panel Point Stress 8,769.88 27,520.08 28,355.70 16,459.12 6,928.59 BC Shear Stress: Mid Panel Stress 0.0926 0.7014 0.9414 0.5133 0.1398 15,886.85 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 18,471.48 26,972.16 3,601.54 9,685.40 3.59 x 0.245 1 R112= round 1 1/8 W3 2,952.70 28,624.38 11,643.44 12,786.97 4.18 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 9,392.42 10,742.43 2,587.36 5,330.90 4.90 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 2,016.83 18,714.09 7,752.84 8,898.52 2.97 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 6,788.86 7,826.93 1,667.31 3,564.90 4.48 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 1,385.60 14,381.54 5,721.29 6,928.23 2.57 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 4,782.25 5,758.64 1,103.89 2,157.24 3.58 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W9 849.26 8,984.69 4,146.76 4,326.22 2.37 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 4,146.76 4,802.89 849.26 1,636.66 3.63 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 4,146.76 8,984.69 4,146.76 4,326.22 2.37 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W11 4,146.76 8,984.69 4,146.76 4,326.22 2.37 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 4,146.76 4,802.89 849.26 1,636.66 3.63 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 849.26 8,984.69 4,146.76 4,326.22 2.37 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 4,782.25 5,758.64 1,103.89 2,157.24 3.58 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 1,385.60 14,381.54 5,721.29 6,928.23 2.57 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 6,788.86 7,826.93 1,667.31 3,564.90 4.48 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W5 2,016.83 18,714.09 7,752.84 8,898.52 2.97 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W4 9,392.42 10,742.43 2,587.36 5,330.90 4.90 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 2,952.70 28,624.38 11,643.44 12,786.97 4.18 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 10:49:37 AM NEW MILLENNIUM Location: Joist Description: Mark: FILM OWG SYSTEMS PORTLAND,OR Short Span Crimp 28K350/200 J5 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 14,188.81 21,311.81 4,187.52 5,706.40 2.94 x 0.230 1 R100=round 1 V1 1,063.42 8,984.69 4,281.61 4,760.28 2.44 x 0.118 1 Cl 8BB= 1.125 x 1.035 x.118 V2 1,112.00 4,802.89 2,247.03 2,577.11 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:49:37 AM NEW MILLENNIUM Location: Joist Description: Mark: RuILniNn SYSTEMS PORTLAND,OR Short Span Crimp 28K350/200 J5 TCX Design TCX Left TCX Right TCX Length 0-0 1/2 TCX Length 0-5 5/8 1 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-0 3/8 BPL Length 2-10 1/8 Clear Bearing 0-4 1/2 Clear Bearing 0-9 3/4 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.01 Reqd TL Def L/80 0.07 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.00 Reqd LL Def L/120 0.05 Section Modulus 2.0284 Section Modulus 2.0284 Reqd SM 0.0030 Reqd SM 0.2316 Mom of Inertia 2.6899 Mom of Inertia 2.6899 Reqd MI 0.000.2 Reqd MI 0.0472 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) vSv ` �5 '/ f' V, ,% \ •.,•„,`� \A /1/ / „,V \ / \ ` /// \ \ 7 Concentrated Loads Conc @ 0-5 5/8 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL MNIPWRIE7. Case 6h: DL+CL+0.85(TL)+SM-AX IiiiiiiiiiiiiiWiiiiii Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) 1 Case 5f:0.6(DL)+WL-AX+SM Case 8h:DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM 1 Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case Gc: DL-rCL-r0.85(TL)+WL+C+AX+IP STRESS ANALYSIS- PAGE 1 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:57:44 AM N E W M I L L E N N I U NI Location: Joist Description: Mark: a1JILnINC SYSTEMS PORTLAND,OR Short Span Crimp 28K350/200 J6 Geometry Base Length: Working Length: I Joist Depth: Effective Depth: BC Panel Length: Shape: 42-2 7/8 41-10 7/8 j 28.00 26.83 9 @ 4-0 Parallel Chords Left End Right End ------------Variable ---- --- BC Panel 3-0 5/8 3-2 1/4 TC Panel 1 7 2 0 (l(.1111...1.T.-.IU]::uaIrL:.,..r. -:,... : -.......... -- .- ..__,_,..,... _ �...-......:...-- - First Half 2-0 2-0 First Diag. 5-0 5/8 5-2 1/4 Depth 28.00 28.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 42-2 7/8 L-BL Uniform (pif) DL(1) 150.00 150.00 TC + 0-0 42-2 7/8 L-BL Uniform (plf) LL(1) 360.00 0.00 TC + 0-0 16-2 L-OAL Conc @ any pp (lbs) CL(1) 420.00 0.00 TC + Uniform (plf) SM(1) 16.00 16.00 TC + 0-0 42-2 7/8 L-BL Axial (lbs) WL(1) 412.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Conc Load (lbs) DL(1) 1,440.00 0.00 TC + 1-1 1-1 L-OAL Conc Load (lbs) WL(1) 412.00 0.00 TC + 34-0 40-0 L-OAL Gross Uplift(plf) WL(2) 105.00 105.00 TC - 0-0 42-2 7/8 L-BL Conc Load (lbs) WL(2) 412.00 0.00 TC - 34-0 40-0 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 12,779.64 9,195.05 3,194.91 44,519.30 44,968.77 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 2,846.30 14,245.80 0.00 0.00 19,153.37 3,602.40 43.80 0-2 V1S 2,677.81 12,757.23 0.00 0.00 417.24 4,784.63 32.10 1-7 W3 2,677.81 12,757.23 20,205.42 4,421.26 2,953.20 12,138.07 36.00 3-0 5/8 W4 5,907.88 26,321.59 20,205.42 4,421.26 9,886.66 2,587.79 36.00 5-0 5/8 V2 5,907.88 26,321.59 20,205.42 4,421.26 1,120.00 2,667.08 26.83 7-0 5/8 W5 5,907.88 26,321.59 31,430.16 7,206.65 2,017.17 8,192.81 36.00 7-0 5/8 W6 8,317.56 35,607.39 31,430.16 7,206.65 7,232.05 1,667.59 36.00 9-0 5/8 V3 8,317.56 35,607.39 31,430.16 7,206.65 1,120.00 2,536.59 26.83 11-0 5/8 W7 8,317.56 35,607.39 38,929.59 9,240.63 1,385.83 6,110.31 36.00 11-0 5/8 W8 9,975.83 41,473.04 38,929.59 9,240.63 5,171.11 1,104.07 36.00 13-05/8 V4 9,975.83 41,473.04 38,929.59 9,240.63 1,120.00 2,389.01 26.83 15-0 5/8 W9 9,975.83 41,473.04 43,314.02 10,523.19 849.41 4,286.66 36.00 15-0 5/8 W10 10,882.69 44,519.30 43,314.02 10,523.19 4,286.66 849.41 36.00 17-0 5/8 V5 10,882.69 44,519.30 43,314.02 10,523.19 1,120.00 2,312.61 26.83 19-0 5/8 W11 10,882.69 44,519.30 44,968.77 11,054.34 4,286.66 4,286.66 36.00 19-0 5/8 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 /�i/� Job Number: Job Name: Date Run: �/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 10:57:44 AM NEW /MILLENNIUM Location: Joist Description: Mark: BULL minim SYSTEMS PORTLAND,OR Short Span Crimp 28K350/200 J6 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W11 11,038.14 43,824.08 44,968.77 11,054.34 4,286.66 4,286.66 36.00 21-0 5/8 V6 11,038.14 43,824.08 44,968.77 11,054.34 1,120.00 2,308.92 26.83 23-0 5/8 W10 11,038.14 43,824.08 41,880.58 10,834.09 4,286.66 849.41 36.00 23-0 5/8 W9 10,442.18 39,310.91 41,880.58 10,834.09 849.41 4,286.66 36.00 25-05/8 V7 10,442.18 39,310.91 41,880.58 10,834.09 1,120.00 2,292.70 26.83 27-0 5/8 W8 10,442.18 39,310.91 36,115.06 9,862.42 5,171.11 1,104.07 36.00 27-05/8 W7 9,094.81 32,293.03 36,115.06 9,862.42 1,385.83 6,110.31 36.00 29-0 5/8 V8 9,094.81 32,293.03 36,115.06 9,862.42 1,120.00 2,263.97 26.83 31-0 5/8 W6 9,094.81 32,293.03 27,844.83 8,139.34 7,232.05 1,667.59 36.00 31-0 5/8 W5 6,794.47 22,770.45 27,844.83 8,139.34 2,017.17 8,192.81 36.00 33-0 5/8 V9 6,794.47 22,770.45 27,844.83 8,139.34 1,532.00 2,426.21 26.83 35-0 5/8 W4 6,794.47 22,770.45 17,069.89 5,094.75 9,886.66 2,587.79 36.00 35-0 5/8 W3 3,151.40 11,428.77 17,069.89 5,094.75 2,953.20 12,138.07 36.00 37-0 5/8 V1S 3,151.40 11,428.77 0.00 0.00 1,539.08 2,653.08 30.38 40-2 7/8 W2 3,291.41 11,828.78 0.00 0.00 14,894.06 4,188.54 45.10 39-0 5/8 STRESS ANALYSIS- PAGE 2 /�� Job Number: Job Name: Date Run: /�/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:57:44 AM NEW MILLENNIUM Location: Joist Description: Mark: 9i.tM.ninus SYSTEMS PORTLAND,OR Short Span Crimp 28K350/200 J6 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.8173 0.6134 0.3924 1.2964 0.5795 0.3076 1.0000 2021 =2 x 2 x.216 Axial and Bendin Analysis K: Fr Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 627.72 318.66 477.99 17-61/2 17-13/4 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 17.00 41.63 24.00 38.25 22.00 1.1250 Min Weld Len 2X: Bending Load 694.90 642.82 350.00 350.00 350.00 0.5000 Axial Load 14,245.80 12,757.23 44,519.30 11,428.77 11,828.78 Max Load Fillers TC: fa 4,324.25 6,855.04 23,922.25 6,141.20 3,590.57 49,625.71 Maximum K L/r 43.46 106.40 46.01 97.78 56.24 Max Load no Fillers TC: Fcr 43,551.60 21,850.26 42,829.38 24,853.79 39,677.35 45,547.55 TC OAL/ Fa 26,130.96 13,110.16 25,697.63 14,912.27 23,806.41 3885.505.50Ryy: F'e 808,645.63 61,306.86 327,847.97 72,603.02 482,848.31 BC OAL/Ryy: Cm 0.9973 0.9441 0.9511 0.9577 0.9963 387.92 Panel Point Moment 9187.80 10201.08 2644.44 5132.82 6947.88 BC Stress: Mid Panel Moment 780.79 6471.22 1750.00 3965.67 3995.07 0.92 Panel Point fb 4529.51 20812.81 5395.34 10472.26 3425.25 BC Linz: 122.3242 Mid Panel fb 340.75 5537.92 1497.61 3393.73 1969.54 TC Shear Stress: Fillers 0 0 0 0 0 12,506.12 Panel Point Stress 8,853.76 27,667.85 29,317.59 16,613.46 7,015.82 BC Shear Stress: Mid Panel Stress 0.0942 0.7134 0.9790 0.5240 0.1416 14,346.16 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 19,153.37 25,761.95 3,602.40 15,682.31 5.92 x 0.218 1 CW4OBA= 1.5 x 1.926 x.218 V1 S 417.24 10,742.43 4,784.63 5,837.66 2.50 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 2,953.20 28,624.38 12,138.07 12,789.55 4.36 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 9,886.66 14,381.54 2,587.79 6,929.53 4.44 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V2 1,120.00 5,758.64 2,667.08 3,254.42 2.00 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W5 2,017.17 18,714.09 8,192.81 8,900.22 3.13 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 7,232.05 8,984.69 1,667.59 4,327.06 4.13 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V3 1,120.00 4,802.89 2,536.59 2,578.21 2.22 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 W7 1,385.83 14,381.54 6,110.31 6,929.53 2.74 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 5,171.11 5,758.64 1,104.07 2,158.09 3.87 x 0.090 1 C12BB= 1.125 x 0.799 x.090 V4 1,120.00 4,802.89 2,389.01 2,578.21 2.09 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 849.41 8,984.69 4,286.66 4,327.06 2.45 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 4,286.66 4,802.89 849.41 1,637.35 3.75 x 0.077 1 C10AB= 1.125 x 0.756 x.077 V5 1,120.00 4,802.89 2,312.61 2,578.21 2.02 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 W11 4,286.66 8,984.69 4,286.66 4,327.06 2.45 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W11 4,286.66 8,984.69 4,286.66 4,327.06 2.45 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V6 1,120.00 4,802.89 2,308.92 2,578.21 2.02 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W10 4,286.66 4,802.89 849.41 1,637.35 3.75 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 849.41 8,984.69 4,286.66 4,327.06 2.45 x 0.118 1 C18BB= 1.125 x 1.035 x.118 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 Job Number: Job Name: Date Run: 5618 0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:57:44 AM NEW MI L L E N N I UM Location: Joist Description: Mark: MllL.dWG SY%TEMS PORTLAND,OR Short Span Crimp 28K350/200 J6 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material V7 1,120.00 4,802.89 2,292.70 2,578.21 2.01 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W8 5,171.11 5,758.64 1,104.07 2,158.09 3.87 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 1,385.83 14,381.54 6,110.31 6,929.53 2.74 x 0.150 1 C28BB= 1.125 x 1.344 x.150 V8 1,120.00 4,802.89 2,263.97 2,578.21 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W6 7,232.05 8,984.69 1,667.59 4,327.06 4.13 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 2,017.17 18,714.09 8,192.81 8,900.22 3.13 x 0.176 1 C34AA= 1.125 x 1.549 x.176 V9 1,532.00 4,802.89 2,426.21 2,578.21 2.12 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W4 9,886.66 14,381.54 2,587.79 6,929.53 4.44 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 2,953.20 28,624.38 12,138.07 12,789.55 4.36 x 0.188 1 C40BA= 1.125 x 2.014 x.218 V1 S 1,539.08 5,758.64 2,653.08 2,815.65 2.00 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W2 14,894.06 21,311.81 4,188.54 5,707.93 3.08 x 0.230 1 R100= round 1 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: �/i/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:57:44 AM NEW MILLENNIUM Location: Joist Description: Mark: BUIL niNIG SYSTEMS PORTLAND,OR Short Span Crimp 28K350/200 J6 TCX Design TCX Left TCX Right TCX Length 0-0 1/2 TCX Length 0-5 5/8 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-0 3/8 BPL Length 2-10 1/8 Clear Bearing 0-3 3/4 Clear Bearing 0-9 3/4 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.01 Reqd TL Def L/80 0.07 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.00 Reqd LL Def L/120 0.05 Section Modulus 2.0284 Section Modulus 2.0284 Reqd SM 0.0030 Reqd SM 0.2316 Mom of Inertia 2.6899 Mom of Inertia 2.6899 Reqd MI 0.0002 Reqd MI 0.0472 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) /'V` ,, \ ; �7 \\ \ \\ G/ N,� i � �`� N -i ''',, A Concentrated Loads Cone @ 0-5 5/8 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+I13) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM ase c: • + *i.I i-r+ + +• * - STRESS ANALYSIS- PAGE 1 f, Job Number: Job Name: Date Run: ✓ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201911:46:47 AM NEW Nil L L E N NI UN% Location: Joist Description: Mark: SUILO1WG SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J7 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 46-10 1/8 46-6 1/8 30.00 28.83 10 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-5 1/8 3-5 l Tin III II 1 ITT i T T Fir t Half 2-0 1/8 1-8 ��� First Half 2-0 2-0 First Diag. 5-5 1/8 5-5 Depth 30.00 30.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 46-10 1/8 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 46-10 1/8 L-BL Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Uniform (plf) SM(1) 16.00 16.00 TC + 0-0 46-10 1/8 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 46-10 1/8 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 9,141.02 9,133.95 2,285.25 44,232.11 43,527.87 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,366.79 11,489.10 0.00 0.00 14,942.94 1,697.77 48.60 0-2 V 1 S 1,173.39 10,914.33 0.00 0.00 1,223.32 2,429.52 35.67 1-8 1/8 W3 1,173.39 10,914.33 16,900.96 1,851.58 1,060.56 10,205.30 37.51 3-5 1/8 W4 2,431.64 22,268.94 16,900.96 1,851.58 8,896.01 907.19 37.51 5-5 1/8 W5 2,431.64 22,268.94 27,054.19 2,943.44 800.49 7,880.26 37.51 7-51/8 W6 3,386.97 31,256.69 27,054.19 2,943.44 6,969.45 693.80 37.51 9-51/8 W7 3,386.97 31,256.69 34,876.47 3,762.24 587.10 5,946.71 37.51 11-5 1/8 W8 4,069.25 37,913.50 34,876.47 3,762.24 5,035.89 480.41 37.51 13-51/8 W9 4,069.25 37,913.50 40,367.80 4,308.00 373.71 4,013.15 37.51 15-51/8 W10 4,478.48 42,239.36 40,367.80 4,308.00 3,102.34 310.15 37.51 17-51/8 W11 4,478.48 42,239.36 43,527.87 4,580.69 310.15 2,973.49 37.51 19-5 1/8 W12 4,614.65 44,232.11 43,527.87 4,580.69 2,973.49 407.63 37.51 21-5 1/8 W12 4,614.65 44,232.11 43,522.99 4,580.34 2,973,49, 407.63 37.51 23-51/8 W11 4,477.76 42,231.13 43,522.99 4,580.34 310.15 2,973.49 37.51 25-5 1/8 W10 4,477.76 42,231.13 40,356.53 4,306.93 3,102.34 310.15 37.51 27-5 1/8 W9 4,067.83 37,899.20 40,356.53 4,306.93 373.71 4,013.15 37.51 29-51/8 W8 4,067.83 37,899.20 34,859.12 3,760.47 5,035.89 480.41 37.51 31-5 1/8 W7 3,384.84 31,236.32 34,859.12 3,760.47 587.10 5,946.71 37.51 33-5 1/8 W6 3,384.84 31,236.32 27,030.77 2,940.95 6,969.45 693.80 37.51 35-5 1/8 W5 2,428.80 22,242.49 27,030.77 2,940.95 800.49 7,880.26 37.51 37-51/8 W4 2,428.80 22,242.49 16,871.47 1,848.38 8,896.01 907.19 37.51 39-51/8 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 ,# Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201911:46:47 AM NEW Nt 1 L L E N N t U M Location: Joist Description: Mark: ROIL.Rln1G sv5�en.4s PORTLAND,OR Short Span Crimp 30K350/200 J7 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W3 1,169.83 10,886.14 16,871.47 1,848.38 1,060.56 10,205.30 37.51 41-5 1/8 V 1 S 1,169.83 10,886.14 0.00 0.00 1,223.32 2,429.52 35.67 45-2 1/8 W2 1,248.23 11,459.78 0.00 0.00 14,942.94 1,697.77 48.50 43-5 1/8 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 700.00 1,896.97 28.83 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201911:46:47 AM NEW MILLENNIUM Location: Joist Description: Mark: RUI DWG SYSTEAAS PORTLAND,OR Short Span Crimp 30K350/200 J7 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.8173 0.6134 0.3924 1.2964 0.5795 0.3076 1.0000 2021 =2 x 2 x.216 Axial and Bendin Analysis K: y: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 724.59 269.06 403.58 17-73/8 25-111/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 18.13 45.00 24.00 45.00 18.00 1.1250 Min Weld Len 2X: Bending Load 350.00 350.00 350.00 350.00 350.00 0.5000 Axial Load 11,489.10 10,914.33 44,232.11 10,886.14 11,459.78 Max Load Fillers TC: fa 3,487.46 5,864.77 23,767.93 5,849.62 3,478.56 49,625.71 Maximum K L/r 46.33 115.03 46.01 115.03 46.01 Max Load no Fillers TC: Fcr 42,737.08 18,970.12 42,829.38 18,970.12 42,829.38 45,547.55 TC Fa 25,642.25 11,382.07 25,697.63 11,382.07 25,697.63 27.85 yy: 427.85 Fe 711,377.38 52,455.68 327,847.97 52,455.68 721,291.88 BC OAL/Ryy: Cm 0.9975 0.9441 0.9514 0.9442 0.9976 430.54 Panel Point Moment 6947.87 7049.28 2644.44 7435.96 6315.03 BC Stress: Mid Panel Moment 4806.99 5049.77 1750.00 4922.77 2500.05 0.89 Panel Point fb 3425.24 14382.32 5395.34 15171.26 3113.26 BC 122..3232 42 Mid Panel fb 2369.81 4321.48 1497.61 4212.80 1232.51 TC Shear Stress: Fillers 0 0 0 0 0 9,506.51 Panel Point Stress 6,912.71 20,247.09 29,163.27 21,020.88 6,591.82 BC Shear Stress: Mid Panel Stress 0.1475 0.6639 0.9729 0.6588 0.1090 10,904.37 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 14,942.94 21,311.81 1,697.77 4,915.22 3.09 x 0.230 1 R100= round 1 W3 1,060.56 24,373.24 10,205.30 10,657.42 3.67 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 8,896.01 10,742.43 907.19 5,136.77 4.64 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 800.49 18,714.09 7,880.26 8,563.68 3.02 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 6,969.45 8,984.69 693.80 4,160.47 3.98 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 587.10 14,381.54 5,946.71 6,672.60 2.67 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 5,035.89 5,758.64 480.41 1,989.00 3.77 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W9 373.71 8,984.69 4,013.15 4,160.47 2.29 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 3,102.34 4,802.89 310.15 1,507.82 2.71 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 310.15 7,826.93 2,973.49 3,425.87 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W12 2,973.49 4,802.89 407.63 1,507.82 2.60 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W12 2,973.49 4,802.89 407.63 1,507.82 2.60 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 310.15 7,826.93 2,973.49 3,425.87 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W10 3,102.34 4,802.89 310.15 1,507.82 2.71 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 373.71 8,984.69 4,013.15 4,160.47 2.29 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 5,035.89 5,758.64 480.41 1,989.00 3.77 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 587.10 14,381.54 5,946.71 6,672.60 2.67 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 6,969.45 8,984.69 693.80 4,160.47 3.98 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 800.49 18,714.09 7,880.26 8,563.68 3.02 x 0.176 1 C34AA= 1.125 x 1.549 x.176 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 , Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201911:46:47 AM NEW MILLENNIUM Location: Joist Description: Mark: BIEL.nING SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J7 Web Design Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W4 8,896.01 10,742.43 907.19 5,136.77 4.64 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 1,060.56 24,373.24 10,205.30 10,657.42 3.67 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 14,942.94 21,311.81 1,697.77 4,935.62 3.09 x 0.230 1 R100= round 1 V1 1,223.32 7,826.93 2,429.52 3,596.39 2.00 x 0.102 1 Cl6BB= 1.125 x 1.025 x.102 V2 700.00 4,802.89 1,896.97 2,362.58 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: i/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 11:46:47 AM NEW NI I L L E N N I UNI Location: Joist Description: Mark: w1.1ii.nINr, SVSTF_I,A9 PORTLAND,OR Short Span Crimp 30K3501200 J7 TCX Design TCX Left TCX Right TCX Length 0-5 5/8 TCX Length 0-0 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-6 3/4 BPL Length 2-1 Clear Bearing 0-9 5/8 Clear Bearing 0-4 1/8 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.07 Reqd TL Def L/80 0.00 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.05 Reqd LL Def L/120 0.00 Section Modulus 2.0284 Section Modulus 2.0284 Reqd SM 0.2316 Reqd SM 0.0000 Mom of Inertia 2.6899 Mom of Inertia 2.6899 Reqd MI 0.0472 Reqd MI 0.0000 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) ,� /, / / �� ',‘/., ` \ /�� // 'f Concentrated Loads Conc @ 0-5 5/8 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(W L+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM , Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case Gc: DL+CL+0. T1 )--WL+r.+AX+IP STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:01:48 PM NEW MILLENNIUM Location: Joist Description: Mark: BLE"o'"'° SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J9 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 46-101/2 46-61/2 30.00 28.66 10 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-5 1/2 3-5 TC Panel 1-8 1/2 1-8 1111111 =1 1111111111111 11. 11111 111_ 11/11/11 II I'11111111111' 11111//1 ' - I_ First Half 2-0 2-0 \w____Irv____IV First Diag. 5-5 1/2 5-5 Depth 30.00 30.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 46-10 1/2 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 46-10 1/2 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 46-10 1/2 L-BL Conc @ any pp(lbs) CL(1) 950.00 0.00 TC + Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 46-10 1/2 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 10,085.58 10,084.31 2,521.39 49,170.82 48,083.07 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,355.60 12,296.77 0.00 0.00 16,694.22 1,674.84 48.80 0-2 V1S 1,191.93 11,715.17 0.00 0.00 2,365.46 3,619.73 35.53 1-81/2 W3 1,191.93 11,715.17 18,154.27 1,873.59 1,063.97 11,338.92 37.38 3-5 1/2 W4 2,456.54 23,947.17 18,154.27 1,873.59 10,026.45 910.22 37.38 5-51/2 W5 2,456.54 23,947.17 29,153.88 2,970.83 803.27 8,894.64 37.38 7-51/2 W6 3,416.45 33,774.41 29,153.88 2,970.83 7,981.62 696.31 37.38 9-5 1/2 W7 3,416.45 33,774.41 37,808.77 3,793.40 589.36 6,849.81 37.38 11-5 1/2 W8 4,101.68 41,256.95 37,808.77 3,793.40 5,936.79 482.41 37.38 13-51/2 W9 4,101.68 41,256.95 44,118.94 4,341.30 375.45 4,804.98 37.38 15-5 1/2 W10 4,512.26 46,394.75 44,118.94 4,341.30 3,891.96 311.11 37.38 17-51/2 W11 4,512.26 46,394.75 48,083.07 4,614.54 579.45 3,288.70 37.38 19-51/2 W12 4,648.16 49,170.82 48,083.07 4,614.54 3,288.70 970.74 37.38 21-51/2 W12 4,648.16 49,170.82 48,055.16 4,613.11 3,288.70 970.74 37.38 23-51/2 W11 4,509.39 46,353.31 48,055.16 4,613.11 579.45 3,288.70 37.38 25-51/2 W10 4,509.39 46,353.31 44,065.30 4,337.01 3,891.96 311.11 37.38 27-5 1/2 W9 4,095.96 41,191.09 44,065.30 4,337.01 375.45 4,804.98 37.38 29-51/2 W8 4,095.96 41,191.09 37,730.71 3,786.25 5,936.79 482.41 37.38 31-5 1/2 W7 3,407.86 33,684.13 37,730.71 3,786.25 589.36 6,849.81 37.38 33-5 1/2 W6 3,407.86 33,684.13 29,051.39 2,960.81 7,981.62 696.31 37.38 35-51/2 W5 2,445.10 23,832.46 29,051.39 2,960.81 803.27 8,894.64 37.38 37-51/2 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 `, Job Number: Job Name: Date Run: ✓ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:01:48 PM NEW MILLENNIUM Location: Joist Description: Mark: A1111-r„Nr sys renes PORTLAND,OR Short Span Crimp 30K350/200 J9 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W4 2,445.10 23,832.46 18,027.35 1,860.71 10,026.45 910.22 37.38 39-51/2 W3 1,177.62 11,593.48 18,027.35 1,860.71 1,063.97 11,338.92 37.38 41-5 1/2 V1S 1,177.62 11,593.48 0.00 0.00 2,365.46 3,619.73 35.53 45-21/2 W2 1,256.48 12,170.50 0.00 0.00 16,586.11 1,559.27 48.40 43-51/2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 1,650.00 2,848.40 28.66 STRESS ANALYSIS- PAGE 2 0 Job Number: 5618-0088 Job Name: Date Run: JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:01:48 PM NEW NI I L L E N N I U NI Location: Joist Description: Mark: wi.m.nwc fi.YSTEiAS PORTLAND,OR Short Span Crimp 30K350/200 J9 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 1.0162 0.8183 0.4925 1.5555 0.7604 0.6804 0.9652 .A42A=2.6250 x.209 BC 0.8173 0.6134 0.3924 1.2964 0.5795 0.3076 1.0000 2021 =2 x 2 x.216 Axial and Bendin Analysis K: Fr Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 746.13 276.50 414.75 21-0 25-111/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 18.50 45.00 24.00 45.00 18.00 1.1250 Min Weld Len 2X: Bending Load 350.00 350.00 350.00 350.00 350.00 0.5000 Axial Load 12,296.77 11,715.17 49,170.82 11,593.48 12,170.50 Max Load Fillers TC: fa 3,548.03 5,764.21 24,193.48 5,704.33 3,511.60 54,747.40 Maximum K L/r 37.56 91.37 36.55 91.37 36.55 Max Load no Fillers TC: Fcr 43,685.70 26,773.67 43,918.29 26,773.67 43,918.29 51,956.74 Fa 26,211.42 16,064.20 26,350.97 16,064.20 26,350.97 TC OAL/Ryy: 359.05 F'e 737,895.13 94,645.03 591,531.44 94,645.03 779,458.63 BCOAL/Ryy: Cm 0.9976 0.9695 0.9726 0.9699 0.9977 430.82 Panel Point Moment 6566.53 6542.98 2644.44 7142.57 6021.64 BC Stress: Mid Panel Moment 4354.17 5216.06 1750.00 5019.13 2255.56 0.98 Panel Point fb 2696.11 8965.34 3623.48 9786.91 2472.39 122.3322 12242 Mid Panel fb 1787.75 2914.68 977.88 2804.64 926.09 TC Shear Stress: Fillers 0 0 0 0 0 11,644.37 Panel Point Stress 6,244.14 14,729.55 27,816.96 15,491.24 5,983.99 BC Shear Stress: Mid Panel Stress 0.1298 0.45541 0.9495 0.4479 0.0988 12,080.62 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 16,694.22 23,679.79 1,674.84 4,874.47 3.46 x 0.230 1 R100= round 1 W3 1,063.97 28,624.38 11,338.92 12,322.60 4.07 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 10,026.45 10,742.43 910.22 5,153.48 5.23 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 803.27 24,373.24 8,894.64 10,694.36 3.19 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 7,981.62 8,984.69 696.31 4,174.72 4.56 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 589.36 16,730.22 6,849.81 7,461.23 2.92 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W8 5,936.79 7,826.93 482.41 3,437.78 3.92 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 375.45 10,742.43 4,804.98 5,153.48 2.51 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W10 3,891.96 4,802.89 311.11 1,518.33 3.40 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 579.45 7,826.93 3,288.70 3,437.78 2.17 x 0.102 1 Cl 6BB= 1.125 x 1.025 x.102 W12 3,288.70 4,802.89 970.74 1,518.33 2.88 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W12 3,288.70 4,802.89 970.74 1,518.33 2.88 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 W11 579.45 7,826.93 3,288.70 3,437.78 2.17 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W10 3,891.96 4,802.89 311.11 1,518.33 3.40 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 375.45 10,742.43 4,804.98 5,153.48 2.51 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 5,936.79 7,826.93 482.41 3,437.78 3.92 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 589.36 16,730.22 6,849.81 7,461.23 2.92 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W6 7,981.62 8,984.69 696.31 4,174.72 4.56 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 803.27 24,373.24 8,894.64 10,694.36 3.19 x 0.188 1 C38BA= 1.125 x 1.845 x.199 *Continued on Next Page... v STRESS ANALYSIS- PAGE 2 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:01:48 PM NEW N11 LLE N N 1 UM Location: Joist Description: Mark: RULL.bwG SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 J9 Web Design Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W4 10,026.45 10,742.43 910.22 5,153.48 5.23 x 0.129 1 C22BB- 1.125 x 1.110 x.129 W3 1,063.97 28,624.38 11,338.92 12,322.60 4.07 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W2 16,586.11 23,679.79 1,559.27 4,956.14 3.43 x 0.230 1 R100= round 1 V1 2,365.46 8,984.69 3,619.73 4,378.72 2.07 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V2 1,650.00 5,758.64 2,848.40 3,026.99 2.06 x 0.090 1 C12BB= 1.125 x 0.799 x.090 STRESS ANALYSIS- PAGE 3 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:01:48 PM NEW MILLENNIUM Location: Joist Description: Mark: nu1LtLNG BYSTEAAS PORTLAND,OR Short Span Crimp 30K350/200 J9 TCX Design TCX Left TCX Right TCX Length 0-5 1/4 TCX Length 0-0 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-6 5/8 BPL Length 2-0 7/8 Clear Bearing 0-9 1/8 Clear Bearing 0-3 7/8 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.07 Reqd TL Def L/80 0.00 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.04 Reqd LL Def L/120 0.00 Section Modulus 2.4356 Section Modulus 2.4356 Reqd SM 0.2189 Reqd SM 0.0000 Mom of Inertia 3.0580 Mom of Inertia 3.0580 Reqd MI 0.0425 Reqd MI 0.0000 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) /'/ / .A / ,'� Concentrated Loads Conc @ 0-5 1/4 800.00 Load Combinations Case 1: DL • Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case Gc: DL+CLt-0.854T1)+WL+C+-AXi4P STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: �/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:59:39 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILOING SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 TJ11 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 46-5 1/2 46-1 1/2 30.00 28.66 10 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-2 3/4 3-2 3/4 1-5 3/4 1-6 3/4 -\ TTS T T T 1Ff(TT i Ti Ill T TC Panel � First Half 2-0 2-0 First Diag. 5-2 3/4 5-2 3/4 Depth 30.00 30.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 46-5 1/2 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 46-5 1/2 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere (lbs) CL(1) 350.00 0.00 TC + Axial(lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 46-5 1/2 L-BL Conc @ any pp(lbs) CL(1) 1,300.00 0.00 TC + Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 46-5 1/2 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 10,363.49 10,359.37 2,590.87 50,076.88 48,820.79 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,519.90 11,743.88 0.00 0.00 16,451.61 1,927.46 46.60 0-2 V 1 S 1,101.92 11,187.46 0.00 0.00 3,143.73 3,999.93 35.53 1-5 3/4 W3 1,101.92 11,187.46 17,669.46 1,784.30 1,062.85 11,736.06 37.38 3-2 3/4 W4 2,367.97 23,615.00 17,669.46 1,784.30 10,423.59 909.11 37.38 5-23/4 W5 2,367.97 23,615.00 28,974.38 2,882.97 802.15 9,249.71 37.38 7-2 3/4 W6 3,329.31 33,747.56 28,974.38 2,882.97 8,336.68 695.20 37.38 9-2 3/4 W7 3,329.31 33,747.56 37,934.57 3,706.97 588.25 7,179.10 37.38 11-2 3/4 W8 4,015.97 41,535.39 37,934.57 3,706.97 6,266.08 481.29 37.38 13-2 3/4 W9 4,015.97 41,535.39 44,550.04 4,256.31 374.34 5,092.20 37.38 15-23/4 W10 4,427.98 46,978.50 44,550.04 4,256.31 4,179.17 308.33 37.38 17-23/4 W11 4,427.98 46,978.50 48,820.78 4,530.98 787.95 3,379.32 37.38 19-2 3/4 W12 4,565.31 50,076.88 48,820.78 4,530.98 3,379.32 1,179.25 37.38 21-2 3/4 W12 4,565.31 50,076.88 48,820.79 4,530.98 3,379.32 1,179.25 37.38 23-2 3/4 W11 4,427.98 46,978.50 48,820.79 4,530.98 787.95 3,379.32 37.38 25-2 3/4 W10 4,427.98 46,978.50 44,550.04 4,256.31 4,179.17 308.33 37.38 27-2 3/4 W9 4,015.97 41,535.39 44,550.04 4,256.31 374.34 5,092.20 37.38 29-2 3/4 W8 4,015.97 41,535.39 37,934.56 3,706.97 6,266.08 481.29 37.38 31-2 3/4 W7 3,329.31 33,747.56 37,934.56 3,706.97 588.25 7,179.10 37.38 33-2 3/4 W6 3,329.31 33,747.56 28,974.37 2,882.97 8,336.68 695.20 37.38 35-2 3/4 W5 2,367.97 23,615.00 28,974.37 2,882.97 802.15 9,249.71 37.38 37-2 3/4 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:59:39 PM NEW MILLENNIUM Location: Joist Description: Mark: muiL.oiNG %YSTE+.A9 PORTLAND,OR Short Span Crimp 30K350/200 TJ11 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W4 2,367.97 23,615.00 17,669.45 1,784.30 10,423.59 909.11 37.38 39-2 3/4 W3 1,103.35 11,197.93 17,669.45 1,784.30 1,062.85 11,736.06 37.38 41-2 3/4 V1S 1,103.35 11,197.93 0.00 0.00 2,360.83 3,935.17 34.95 44-103/4 W2 1,175.78 11,727.84 0.00 0.00 16,451.61 1,927.46 46.60 43-2 3/4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 2,000.00 3,194.86 28.66 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:59:39 PM NEW MILLENNIUM Location: Joist Description: Mark: NUM nWn 5Y5TEM5 PORTLAND,OR Short Span Crimp 30K350/200 TJ11 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material __. TC 1.0162 0.8183 0.4925 1.5555 0.7604 0.6804 0.9652 A42A=2.6250 x.209 BC 0.8173 0.6134 0.3924 1.2964 0.5795 0.3076 1.0000 2021 =2 x 2 x.216 Axial and Bendin Analysis K: y: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 746.13 284.06 426.09 21-01/4 25-111/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 15.75 45.00 24.00 44.00 16.75 1.1250 Min Weld Len 2X: Bending Load 350.00 350.00 350.00 350.00 350.00 0.5000 Axial Load 11,743.88 11,187.46 50,076.88 11,197.93 11,727.84 Max Load Fillers TC: fa 3,388.50 5,504.56 24,639.29 5,509.71 3,383.88 54,747.40 Maximum K Ur 31.98 91.37 36.55 89.34 34.01 Max Load no Fillers TC: Fcr 44,899.43 26,773.67 43,918.29 27,476.03 44,476.86 51,956.74 Fa 26,939.66 16,064.20 26,350.97 16,485.62 26,686.12 TC 3AURyy. 355.83 F'e 1,018,068.44 94,645.03 591,531.44 98,995.97 900,136.69 BC OAURyy: Cm 0.9983 0.9709 0.9721 0.9722 0.9981 426.97 Panel Point Moment 9458.32 6432.65 2644.44 6867.32 5714.05 BC Stress: Mid Panel Moment 7103.77 5252.38 1750.00 4843.79 604.24 1.00 Panel Point fb 3883.43 8814.17 3623.48 9409.76 2346.09 122.3242 Mid Panel fb 2916.69 2934.97 977.88 2706.66 245.89 TC Shear Stress: Fillers 0 0 0 0 0 11,940.86 Panel Point Stress 7,271.94 14,318.73 28,262.77 14,919.47 5,729.97 BC Shear Stress: Mid Panel Stress 0.1640 0.4395 0.9664 0.4233 0.0719 12,363.83 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 16,451.61 23,679.79 1,927.46 5,345.06 3.41 x 0.230 1 R100= round 1 W3 1,062.85 28,624.38 11,736.06 12,322.60 4.22 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 10,423.59 14,381.54 909.11 6,694.58 4.68 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 802.15 24,373.24 9,249.71 10,694.36 3.32 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 8,336.68 8,984.69 695.20 4,174.72 4.76 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 588.25 16,730.22 7,179.10 7,461.23 3.06 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W8 6,266.08 7,826.93 481.29 3,437.78 4.14 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 374.34 10,742.43 5,092.20 5,153.48 2.66 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W10 4,179.17 4,802.89 308.33 1,518.33 3.66 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 787.95 7,826.93 3,379.32 3,437.78 2.23 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W12 3,379.32 4,802.89 1,179.25 1,518.33 2.96 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 W12 3,379.32 4,802.89 1,179.25 1,518.33 2.96 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 787.95 7,826.93 3,379.32 3,437.78 2.23 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W10 4,179.17 4,802.89 308.33 1,518.33 3.66 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 374.34 10,742.43 5,092.20 5,153.48 2.66 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 6,266.08 7,826.93 481.29 3,437.78 4.14 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 588.25 16,730.22 7,179.10 7,461.23 3.06 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W6 8,336.68 8,984.69 695.20 4,174.72 4.76 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 802.15 24,373.24 9,249.71 10,694.36 3.32 x 0.188 1 C38BA= 1.125 x 1.845 x.199 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:59:39 PM NEW AA1 L L E N N t U Nt Location: Joist Description: Mark: 0uiLoiNr SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 TJ11 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W4 10,423.59 14,381.54. 909.11 6,694.58 4.68 x 0.150 1 C28BB= 1.125 x 1.344 x.150 . W3 1,062.85 28,624.38 11,736.06 12,322.60 4.22 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W2 16,451.61 23,679.79 1,927.46 5,345.06 3.41 x 0.230 1 R100= round 1 V1 3,143.73 8,984.69 3,999.93 4,378.72 2.28 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V2 2,000.00 7,826.93 3,194.86 4,276.59 2.05 x 0.102 1 C16BB= 1.125 x 1.025 x.102 STRESS ANALYSIS- PAGE 3 l/� Job Number: Job Name: Date Run: �r// 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:59:39 PM NEW MILLENNIUM Location: Joist Description: Mark: RUlL I lnIc SYSTer,es PORTLAND,OR Short Span Crimp 30K350/200 TJ11 TCX Design TCX Left TCX Right TCX Length 0-8 TCX Length 0-2 1/4 - TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-6 5/8 BPL Length 2-1 7/8 Clear Bearing 0-11 7/8 Clear Bearing 0-6 1/8 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.10 Reqd TL Def L/80 0.03 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.07 Reqd LL Def L/120 0.02 Section Modulus 2.4356 Section Modulus 2.4356 Reqd SM 0.3153 Reqd SM 0.0088 Mom of Inertia 3.0580 Mom of Inertia 3.0580 Reqd MI 0.0836 Reqd MI 0.0008 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) NN � ;. / > v ' /// ///i/ ��AV / ///,// � N , ;,/ , \ // ////// i \\\ // Concentrated Loads Conc @ 0-8 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP j Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c: 0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case Cc: DI +Ct+0.85(TI )4-WI J+AX+lP STRESS ANALYSIS- PAGE 1 /%� Job Number: Job Name: Date Run: �/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 1:43:23 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 TJ12 Geometry Base Length: Working Length: Joist Depth: Effective Depth: IBC Panel Length: Shape: 46-51/2 46-1 1/2 30.00 1 28.84 110 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-2 7/8 3-2 5/8 11111 11111111.11111111111/1 1 I 11111 11 I Ili111111111111111111111111111/11 111111 I' TC Panel 1-6 7/8 1-6 5/8 '-111111111111111111111111111111111111 �_ -_�_�_' __i First Half 2-0 2-0 First Diag. 5-2 7/8 5-2 5/8 Depth 30.00 30.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 46-5 1/2 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 46-5 1/2 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Uniform (plf) SM(1) 16.00 16.00 TC + 0-0 46-5 1/2 L-BL Axial (lbs) SM(1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 46-5 1/2 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 9,077.62 9,066.44 2,269.40 43,525.35 42,824.71 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,470.22 10,866.05 0.00 0.00 14,308.61 1,866.47 46.81 0-2 V1S 1,100.04 10,338.35 0.00 0.00 1,454.60 2,347.31 35.10 1-6 7/8 W3 1,100.04 10,338.35 16,219.67 1,776.39 1,058.46 10,193.22 37.52 3-2 7/8 W4 2,356.06 21,584.24 16,219.67 1,776.39 8,903.09 907.33 37.52 5-2 7/8 W5 2,356.06 21,584.24 26,366.28 2,867.50 800.65 7,879.28 37.52 7-2 7/8 W6 3,310.70 30,565.78 26,366.28 2,867.50 6,968.60 693.97 37.52 9-2 7/8 W7 3,310.70 30,565.78 34,182.76 3,685.66 587.29 5,951.86 37.52 11-2 7/8 W8 3,992.39 37,217.20 34,182.76 3,685.66 5,041.17 480.62 37.52 13-2 7/8 W9 3,992.39 37,217.20 39,669.12 4,230.87 373.94 4,017.36 37.52 15-2 7/8 W10 4,401.11 41,538.50 39,669.12 4,230.87 3,106.68 307.54 37.52 17-2 7/8 W11 4,401.11 41,538.50 42,824.71 4,503.11 307.54 2,952.44 37.52 19-2 7/8 W12 4,536.88 43,525.35 42,824.71 4,503.11 2,952.44 411.29 37.52 21-2 7/8 W12 4,536.88 43,525.35 42,814.96 4,502.40 2,952.44 411.29 37.52 23-2 7/8 W11 4,399.69 41,522.03 42,814.96 4,502.40 307.54 2,952.44 37.52 25-2 7/8 W10 4,399.69 41,522.03 39,646.58 4,228.73 3,106.68 307.54 37.52 27-2 7/8 W9 3,989.54 37,188.59 39,646.58 4,228.73 373.94 4,017.36 37.52 29-2 7/8 W8 3,989.54 37,188.59 34,148.08 3,682.11 5,041.17 480.62 37.52 31-2 7/8 W7 3,306.44 30,525.04 34,148.08 3,682.11 587.29 5,951.86 37.52 33-2 7/8 W6 3,306.44 30,525.04 26,319.46 2,862.53 6,968.60 693.97 37.52 35-2 7/8 W5 2,350.38 21,531.36 26,319.46 2,862.53 800.65 7,879.28 37.52 37-2 7/8 W4 2,350.38 21,531.36 16,160.72 1,769.99 8,903.09 907.33 37.52 39-2 7/8 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 0 Job Number: 5618-0088 Job Name: Date Run: JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:43:23 PM NEW MILLENNIUM Location: Joist Description: Mark: aun.owc f`,Y57P A% PORTLAND,OR Short Span Crimp 30K350/200 TJ12 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W3 1,092.93 10,282.00 16,160.72 1,769.99 1,058.46 10,193.22 37.52 41-2 7/8 V1S 1,092.93 10,282.00 0.00 0.00 1,454.60 2,347.31 35.10 44-10 7/8 W2 1,164.75 10,807.54 0.00 0.00 14,263.17 1,482.51 46.62 43-2 7/8 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 700.00 1,893.65 28.84 STRESS ANALYSIS- PAGE 2 /�i� Job Number: Job Name: Date Run: moi// 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:43:23 PM NEW MILLENNIUM Location: Joist Description: Mark: HUM mime SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 TJ12 Chord Properties Chord Area Rx Rz Ryy Y Ix 0 Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 674.71 256.87 385.30 17-71/2 25-01/4 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 16.88 44.00 24.00 44.00 16.63 1.1250 Min Weld Len 2X: Bending Load 350.00 350.00 350.00 350.00 350.00 0.5000 Axial Load 10,866.05 10,338.35 43,525.35 10,282.00 10,807.54 Max Load Fillers TC: fa 3,298.34 5,555.26 23,388.15 5,524.99 3,280.58 49,625.71 Maximum K Ur 43.14 112.47 46.01 112.47 42.50 Max Load no Fillers TC: Fcr 43,639.80 19,827.17 42,829.38 19,827.17 43,814.76 45,547.55 Fa 26,183.88 11,896.30 25,697.63 11,896.30 26,288.86 TC OAURyy: 424.31 Fe 820,669.88 54,867.12 327,847.97 54,867.12 845,537.25 BCOAURyy: Cm 0.9980 0.9494 0.9522 0.9497 0.9981 429.36 Panel Point Moment 9458.32 6663.57 2644.44 7154.36 5992.67 BC Stress: Mid Panel Moment 7008.11 4910.96 1750.00 4749.17 540.34 1.00 BC Panel Point fb 4662.87 13595.38 5395.34 14596.73 2954.34 121.88 121.8893 Mid Panel fb 3454.94 4202.69 1497.61 4064.23 235.81 TC Shear Stress: Fillers 0 0 0 0 0 9,390.87 Panel Point Stress 7,961.21 19,150.64 28,783.49 20,121.72 6,234.92 BC Shear Stress: Mid Panel Stress 0.1787 0.6093 0.9581 0.6019 0.0703 12,367.98 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 14,308.61 21,311.81 1,866.47 5,297.42 2.96 x 0.230 1 R100= round 1 W3 1,058.46 24,373.24 10,193.22 10,655.20 3.66 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 8,903.09 10,742.43 907.33 5,135.76 4.65 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 800.65 18,714.09 7,879.28 8,561.94 3.01 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 6,968.60 8,984.69 693.97 4,159.61 3.98 x 0.118 1 Cl 8BB= 1.125 x 1.035 x.118 W7 587.29 14,381.54 5,951.86 6,671.28 2.67 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 5,041.17 5,758.64 480.62 1,988.17 3.77 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W9 373.94 8,984.69 4,017.36 4,159.61 2.29 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 3,106.68 4,802.89 307.54 1,507.19 2.72 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 307.54 7,826.93 2,952.44 3,425.15 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W12 2,952.44 4,802.89 411.29 1,507.19 2.58 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W12 2,952.44 4,802.89 411.29 1,507.19 2.58 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 307.54 7,826.93 2,952.44 3,425.15 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W10 3,106.68 4,802.89 307.54 1,507.19 2.72 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 373.94 8,984.69 4,017.36 4,159.61 2.29 x 0.118 1 Cl8BB= 1.125 x 1.035 x.118 W8 5,041.17 5,758.64 480.62 1,988.17 3.77 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 587.29 14,381.54 5,951.86 6,671.28 2.67 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 6,968.60 8,984.69 693.97 4,159.61 3.98 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 800.65 18,714.09 7,879.28 8,561.94 3.01 x 0.176 1 C34AA= 1.125 x 1.549 x.176 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 0 Job Number: 5618-0088 Job Name: Date Run: JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 1:43:23 PM NEW MILLENNIUM Location: Joist Description: Mark: wuti.ntNr.. SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 TJ12 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W4 8,903.09 10,742.43 907.33 5,135.76 4.65 x 0.129 1 C22BB= 1.125x 1.110 x.129 W3 1,058.46 24,373.24 10,193.22 10,655.20 3.66 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 14,263.17 21,311.81 1,482.51 5,342.22 2.95 x 0.230 1 R100= round 1 V1 1,454.60 7,826.93 2,347.31 3,649.83 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V2 700.00 4,802.89 1,893.65 2,361.49 2.00 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: ri;, eRun: �/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS /9/2019 1:43:23 PM NEW MILLENNIUM Location: Joist Description: Mark: aiiu.owr., %YSTEiUS PORTLAND,OR Short Span Crimp 30K350/200 TJ12 TCX Design TCX Left TCX Right TCX Length 0-8 TCX Length 0-2 1/4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-7 7/8 BPL Length 2-1 7/8 Clear Bearing 1-0 Clear Bearing 0-6 1/4 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.10 Reqd TL Def L/80 0.03 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.07 Reqd LL Def L/120 0.02 Section Modulus 2.0284 Section Modulus 2.0284 Reqd SM 0.3153 Reqd SM 0.0088 Mom of Inertia 2.6899 Mom of Inertia 2.6899 Reqd MI 0.0836 Reqd MI 0.0008 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) �` // i/ \..\.N‘,,,,,,,,\ /f, //i xA % /i \ /\ / i i Concentrated Loads Conc @ 0-8 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Ca asec CL-+-0 ��� ��-r STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: /�// 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201912:01:08 PM NEW M I L L E N N I U M Location: Joist Description: Mark: BIDE-CENG SYSTEMS PORTLAND,OR Short Span Round 10K350/200 TJ14 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 14-3 3/4 113-11 3/4 10.00 9.10 6 @ 1-8 Parallel Chords Variable Left End Right End BC Panel 2-1 7/8 2-1 7/8 1 III TC Panel 1-3 7/8 1-3 7/8 First Half 0-10 0-10 w___ '1V - First Diag. 2-11 7/8 2-11 7/8 Depth 10.00 10.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 14-3 3/4 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 14-3 3/4 L-BL Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Conc anywhere (lbs) CL(1) 300.00 0.00 BC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 14-3 3/4 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) SM(1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 14-3 3/4 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 20.00 20.00 3,410.64 3,428.50 857.12 15,410.88 15,178.04 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 689.91 8,010.36 0.00 0.00 9,060.90 738.29 25.55 0-2 V1S 825.21 7,544.88 0.00 0.00 1,187.94 2,249.65 13.52 1-3 7/8 W3 825.21 7,544.88 9,132.03 851.64 304.64 3,768.25 13.52 2-1 7/8 W4 1,001.88 11,392.35 9,132.03 851.64 2,901.38 203.10 13.52 2-11 7/8 W5 1,001.88 11,392.35 12,796.28 1,152.11 203.10 2,742.15 13.52 3-9 7/8 W6 1,227.23 14,140.54 12,796.28 1,152.11 1,875.28 106.47 13.52 4-7 7/8 W7 1,227.23 14,140.54 15,178.04 1,302.35 291.91 1,689.52 13.52 5-5 7/8 W8 1,302.35 15,410.88 15,178.04 1,302.35 1,094.62 1,273.75 13.52 6-3 7/8 W8 1,302.35 15,410.88 15,178.04 1,302.35 1,094.62 1,273.75 13.52 7-1 7/8 W7 1,227.23 14,140.54 15,178.04 1,302.35 291.91 1,689.52 13.52 7-11 7/8 W6 1,227.23 14,140.54 12,796.28 1,152.11 1,875.28 106.47 13.52 8-9 7/8 W5 1,001.88 11,392.35 12,796.28 1,152.11 203.10 2,742.15 13.52 9-7 7/8 W4 1,001.88 11,392.35 9,132.03 851.64 2,901.38 203.10 13.52 10-5 7/8 W3 825.21 7,544.89 9,132.03 851.64 304.64 3,768.25 13.52 11-3 7/8 V1S 825.21 7,544.89 0.00 0.00 1,187.94 2,249.65 13.52 12-117/8 W2 689.91 8,010.36 0.00 0.00 9,060.90 738.29 25.55 12-17/8 STRESS ANALYSIS- PAGE 2 01 Job Number: 5618-0088 Job Name: Date Run: JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 12:01:08 PM NEW NI I L L E N N I U N% Location: Joist Description: Mark: BUIL nINr SYSTEMS PORTLAND,OR Short Span Round 10K350/200 TJ14 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.4306 0.5149 0.3062 0.8995 0.4877 0.1141 1.0000 A26B= 1.6560 x 0.142 BC 0.3151 0.4675 0.2972 0.8133 0.4154 0.0689 0.9057 1510= 1 1/2 x 1 1/2 x.109 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 30.48 416.85 625.27 11-3 1/8 16-3 1/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 13.88 20.00 20.00 20.00 13.88 0.5000 Min Weld Len 2X:: Bending Load 350.00 350.00 350.00 350.00 350.00 0.5000 Axial Load 8,010.36 7,544.88 15,410.88 7,544.89 8,010.36 Max Load Fillers TC: fa 3,490.96 8,760.90 17,894.66 8,760.90 3,490.96 21,036.77 Maximum K L/r 45.31 65.32 48.99 65.32 45.31 Max Load no Fillers TC: Fcr 43,029.68 36,601.31 41,953.31 36,601.31 43,029.68 19,582.83 TC Fa 25,817.81 21,960.79 25,171.98 21,960.79 25,817.81 186.48 86.48 yy: F'e 1,227,431.75 189,707.09 337,257.06 189,707.09 1,227,431.75 BC OAL/Ryy: Cm 0.9986 0.9769 0.9645 0.9769 0.9986 206.26 Panel Point Moment 1876.20 2017.49 2009.26 2017.49 1876.20 BC Stress: Mid Panel Moment 1052.09 1372.29 1361.11 1372.29 1052.09 0.80 Panel Point fb 1100.20 10328.83 10286.67 10328.83 1100.20 BC 67.229494 8 Mid Panel fb 771.47 2932.80 2908.91 2932.80 771.47 TC Shear Stress: Fillers 0 0 0 0 0 10,243.72 Panel Point Stress 4,591.16 19,089.73 28,181.33 19,089.73 4,591.16 BC Shear Stress: Mid Panel Stress 0.0934 0.4909 0.8021 0.4909 0.0934 11,935.87 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 9,060.90 10,072.50 738.29 3,974.06 2.31 x 0.192 1 R068= round 11/16 V1 S 1,187.94 7,492.27 2,249.65 4,333.39 2.00 x 0.177 1 R056= round 9/16 W3 304.64 7,492.27 3,768.25 4,333.39 2.00 x 0.177 1 R056= round 9/16 W4 2,901.38 5,918.44 203.10 2,960.52 2.00 x 0.170 1 R050=round 1/2 W5 203.10 5,918.44 2,742.15 2,960.52 2.00 x 0.170 1 R050=round 1/2 W6 1,875.28 5,918.44 106.47 2,960.52 2.00 x 0.170 1 R050= round 1/2 W7 291.91 5,918.44 1,689.52 2,960.52 2.00 x 0.170 1 R050= round 1/2 W8 1,094.62 5,918.44 1,273.75 2,960.52 2.00 x 0.170 1 R050= round 1/2 W8 1,094.62 5,918.44 1,273.75 2,960.52 2.00 x 0.170 1 R050= round 1/2 W7 291.91 5,918.44 1,689.52 2,960.52 2.00 x 0.170 1 R050=round 1/2 W6 1,875.28 5,918.44 106.47 2,960.52 2.00 x 0.170 1 R050=round 1/2 W5 203.10 5,918.44 2,742.15 2,960.52 2.00 x 0.170 1 R050= round 1/2 W4 2,901.38 5,918.44 203.10 2,960.52 2.00 x 0.170 1 R050= round 1/2 W3 304.64 7,492.27 3,768.25 4,333.39 2.00 x 0.177 1 R056= round 9/16 V1S 1,187.94 7,492.27 2,249.65 4,333.39 2.00 x 0.177 1 R056= round 9/16 W2 9,060.90 10,072.50 738.29 3,974.06 2.31 x 0.192 1 R068=round 11/16 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201912:01:08 PM NEW MILLENNIUM Location: Joist Description: Mark: euILDINc sVI;TPAas PORTLAND,OR Short Span Round 10K350/200 TJ14 TCX Design TCX Left TCX Right TCX Length 0-1 1/4 TCX Length 0-1 1/4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 1-10 3/4 BPL Length 1-10 3/4 Clear Bearing 0-7 5/8 Clear Bearing 0-7 5/8 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.02 Reqd TL Def L/80 0.02 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.01 Reqd LL Def L/120 0.01 Section Modulus 1.3637 Section Modulus 1.3637 Reqd SM 0.0051 Reqd SM 0.0051 Mom of Inertia 1.8944 Mom of Inertia 1.8944 Reqd MI 0.0003 Reqd MI 0.0003 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) V /> \ /// ���. \\ \\ /%/ Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a:LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP STRESS ANALYSIS- PAGE 1 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:06:18 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS PORTLAND,OR Short Span Round 10K350/200 TJ15 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 14-1 3/4 13-9 3/4 1 10.00 9.10 6 @ 1-8 Parallel Chords Variable Left End Right End BC Panel 2-0 7/8 2-0 7/8 TC Panel 1-2 7/8 1-27/8 - ��_____i 1 First Half 0-2 0-10 iLA_�A First Diag. 2-10 7/8 2-10 7/8 Depth 10.00 10.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 14-1 3/4 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 14-1 3/4 L-BL Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Uniform (plf) SM(1) 16.00 16.00 TC + 0-0 14-1 3/4 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 14-1 3/4 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 20.00 20.00 3,380.82 3,399.01 849.75 15,120.61 14,855.76 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 758.43 7,712.53 0.00 0.00 8,690.07 706.74 24.62 0-2 V1S 893.95 7,260.79 0.00 0.00 1,211.13 2,226.56 13.52 1-2 7/8 W3 893.95 7,260.79 8,809.74 820.33 304.64 3,789.48 13.52 2-0 7/8 W4 970.56 11,108.26 8,809.74 820.33 2,922.61 203.10 13.52 2-10 7/8 W5 970.56 11,108.26 12,474.00 1,120.80 203.10 2,733.47 13.52 3-8 7/8 W6 1,195.91 13,856.44 12,474.00 1,120.80 1,866.59 114.83 13.52 4-6 7/8 W7 1,195.91 13,856.44 14,855.76 1,271.03 276.95 1,704.48 13.52 5-4 7/8 W8 1,271.03 15,120.61 14,855.76 1,271.03 1,083.79 1,262.79 13.52 6-2 7/8 W8 1,271.03 15,120.61 14,855.76 1,271.03 1,083.79 1,262.79 13.52 7-0 7/8 W7 1,195.92 13,856.44 14,855.76 1,271.03 276.95 1,704.48 13.52 7-10 7/8 W6 1,195.92 13,856.44 12,474.00 1,120.80 1,866.59 114.83 13.52 8-8 7/8 W5 970.56 11,108.26 12,474.00 1,120.80 203.10 2,733.47 13.52 9-6 7/8 W4 970.56 11,108.26 8,809.74 820.33 2,922.61 203.10_ 13.52 10-4 7/8 W3 893.95 7,260.79 8,809.74 820.33 304.64 3,789.48 13.52 11-2 7/8 V1S 893.95 7,260.79 0.00 0.00 1,211.13 2,226.56 13.52 12-10 7/8 W2 758.43 7,712.52 0.00 0.00 8,690.07 706.74 24.62 12-0 7/8 STRESS ANALYSIS- PAGE 2 ', Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:06:18 PM NEW MILLENNIUM Location: Joist Description: Mark: RIM.ninic SV5TF.M9 PORTLAND,OR Short Span Round 10K350/200 TJ15 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.4306 0.5149 0.3062 0.8995 0.4877 0.1141 1.0000 A26B= 1.6560 x 0.142 BC 0.3151 0.4675 0.2972 0.8133 0.4154 0.0689 0.9057 1510= 1 1/2 x 1 1/2 x .109 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 30.48 432.12 648.18 11-3 3/8 16-31/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 12.88 20.00 20.00 20.00 12.88 0.5000 Min Weld Len 2X:: Bending Load 350.00 350.00 350.00 350.00 350.00 0.5000 Axial Load 7,712.53 7,260.79 15,120.61 7,260.79 7,712.53 Max Load Fitters TC: fa 3,361.16 8,431.02 17,557.61 8,431.02 3,361.16 21,036.77 Maximum K L/r 42.05 65.32 48.99 65.32 42.05 Max Load no Fillers TC: Fcr 43,936.75 36,601.31 41,953.31 36,601.31 43,936.75 19,582.83 Fa 26,362.05 21,960.79 25,171.98 21,960.79 26,362.05 TCOAL/Ryy: 184.26 Fe' 1,425,505.38 189,707.09 337,257.06 189,707.09 1,425,505.38 BC OAL/Ryy: Cm 0.9988 0.9778 0.9651 0.9778 0.9988 203.81 Panel Point Moment 1798.34 2020.32 2009.26 2020.32 1798.34 BC Stress: Mid Panel Moment 835.11 1376.12 1361.11 1376.12 835.11 0.79 Panel Point fb 1054.55 10343.29 10286.67 10343.29 1054.55 BC 67.229494 8 Mid Panel fb 612.37 2940.99 2908.91 2940.99 612.37 Fillers 0 0 0 0 0 TC Shear Stress: 10,099.63 Panel Point Stress 4,415.72 18,774.31 27,844.27 18,774.31 4,415.72 BC Shear Stress: Mid Panel Stress 0.0842 0.4759 0.7886 0.4759 0.0842 11,725.37 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 8,690.07 10,072.50 706.74 4,280.63 2.21 x 0.192 1 R068= round 11/16 V1 S 1,211.13 7,492.27 2,226.56 4,333.39 2.00 x 0.177 1 R056= round 9/16 W3 304.64 7,492.27 3,789.48 4,333.39 2.00 x 0.177 1 R056=round 9/16 W4 2,922.61 5,918.44 203.10 2,960.52 2.00 x 0.170 1 R050= round 1/2 W5 203.10 5,918.44 2,733.47 2,960.52 2.00 x 0.170 1 R050= round 1/2 W6 1,866.59 5,918.44 114.83 2,960.52 2.00 x 0.170 1 R050= round 1/2 W7 276.95 5,918.44 1,704.48 2,960.52 2.00 x 0.170 1 R050= round 1/2 W8 1,083.79 5,918.44 1,262.79 2,960.52 2.00 x 0.170 1 R050= round 1/2 W8 1,083.79 5,918.44 1,262.79 2,960.52 2.00 x 0.170 1 R050= round 1/2 W7 276.95 5,918.44 1,704.48 2,960.52 2.00 x 0.170 1 R050=round 1/2 1 W6 1,866.59 5,918.44 114.83 2,960.52 2.00 x 0.170 1 R050= round 1/2 W5 203.10 5,918.44 2,733.47 2,960.52 2.00 x 0.170 1 R050= round 1/2 W4 2,922.61 5,918.44 203.10 2,960.52 2.00 x 0.170 1 R050= round 1/2 W3 304.64 7,492.27 3,789.48 4,333.39 2.00 x 0.177 1 R056= round 9/16 V1 S 1,211.13 7,492.27 2,226.56 4,333.39 2.00 x 0.177 1 R056= round 9/16 W2 8,690.07 10,072.50 706.74 4,280.63 2.21 x 0.192 1 R068=round 11/16 . STRESS ANALYSIS- PAGE 3 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/20191:06:18 PM NEW M I L LEN N I UM Location: Joist Description: Mark: eun..mimr., %,/STEM% PORTLAND,OR Short Span Round 10K350/200 TJ15 TCX Design TCX Left TCX Right TCX Length 0-2 1/4 TCX Length 0-2 1/4 _. TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 1-10 3/4 BPL Length 1-10 3/4 Clear Bearing 0-8 3/8 Clear Bearing 0-8 3/8 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.03 Reqd TL Def L/80 0.03 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.02 Reqd LL Def L/120 0.02 Section Modulus 1.3637 Section Modulus 1.3637 Reqd SM 0.0088 Reqd SM 0.0088 Mom of Inertia 1.8944 Mom of Inertia 1.8944 Reqd MI 0.0008 Reqd MI 0.0008 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) \\\\ /// \\\ Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6 DL +WL-AX+SM ( ) Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case 6c: DL+CL+0.85(TL)+WL+C+AX+IP - STRESS ANALYSIS- PAGE 1 �/' Job Number: Job Name: Date Run: ��/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 1:41:42 PM NEW MILLENNIUM Location: Joist Description: Mark: , ®""-x'^16 SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 TJ17 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 46-7 46-3 30.00 28.84 10 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-3 3/4 3-3 1/4FT ' I ' , TC Panel 1-7 3/4 1-7 1/4 • �� VW ' �� V Y, First Half 2-0 2-0 First Diag. 5-3 3/4 5-3 1/4 Depth 30.00 30.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 46-7 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 46-7 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 46-7 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 46-7 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 9,082.94 9,104.13 2,276.03 43,746.36 43,052.44 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,201.37 11,094.96 0.00 0.00 14,535.32 1,511.83 47.51 0-2 V1S 1,128.21 10,559.67 0.00 0.00 1,399.02 2,364.08 35.10 1-7 3/4 W3 1,128.21 10,559.67 16,472.32 1,804.21 1,059.02 10,214.25 37.52 3-3 3/4 W4 2,383.53 21,833.86 16,472.32 1,804.21 8,924.12 907.89 37.52 5-3 3/4 W5 2,383.53 21,833.86 26,612.86 2,894.61 801.21 7,900.92 37.52 7-3 3/4 W6 3,337.46 30,809.33 26,612.86 2,894.61 6,990.24 694.53 37.52 9-3 3/4 W7 3,337.46 30,809.33 34,423.28 3,712.06 587.85 5,967.04 37.52 11-3 3/4 W8 4,018.43 37,454.68 34,423.28 3,712.06 5,056.36 481.17 37.52 13-3 3/4 W9 4,018.43 37,454.68 39,903.57 4,256.55 374.49 4,033.16 37.52 15-3 3/4 W10 4,426.44 41,769.92 39,903.57 4,256.55 3,122.48 308.37 37.52 17-3 3/4 W11 4,426.44 41,769.92 43,052.44 4,528.09 308.37 2,961.06 37.52 19-3 3/4 W12 4,561.50 43,746.36 43,052.44 4,528.09 2,961.06 427.20 37.52 21-3 3/4 W12 4,561.50 43,746.36 43,032.93 4,526.67 2,961.06 427.20 37.52 23-3 3/4 W11 4,423.60 41,736.98 43,032.93 4,526.67 308.37 2,961.06 37.52 25-3 3/4 W10 4,423.60 41,736.98 39,858.49 4,252.29 3,122.48 308.37 37.52 27-3 3/4 W9 4,012.74 37,397.47 39,858.49 4,252.29 374.49 4,033.16 37.52 29-3 3/4 W8 4,012.74 37,397.47 34,353.93 3,704.95 5,056.36 481.17 37.52 31-3 3/4 W7 3,328.93 30,727.85 34,353.93 3,704.95 587.85 5,967.04 37.52 33-3 3/4 W6 3,328.93 30,727.85 26,519.24 2,884.66 6,990.24 694.53 37.52 35-3 3/4 W5 2,372.16 21,728.10 26,519.24 2,884.66 801.21 7,900.92 37.52 37-33/4 W4 2,372.16 21,728.10 16,354.43 1,791.41 8,924.12 907.89 37.52 39-3 3/4 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 �/� Job Number: Job Name: Date Run: �! 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 1:41:42 PM NEW M I L L E N N I U IV1 Location: Joist Description: Mark: nuu.nwr SY5T5M9 PORTLAND,OR Short Span Crimp 30K350/200 TJ17 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W3 1,113.99 10,446.98 16,354.43 1,791.41 1,059.02 10,214.25 37.52 41-3 3/4 V1S 1,113.99 10,446.98 0.00 0.00 1,399.02 2,364.08 35.10 44-11 3/4 W2 1,440.05 10,977.93 0.00 0.00 14,434.79 1,821.21 47.11 43-3 3/4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 700.00 1,894.70 28.84 AWIttialn 4 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �// 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:41:42 PM NEW MILLENNIUM Location: Joist Description: Mark: RUM miNG SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 TJ17 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 - BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 674.71 254.79 382.18 17-71/2 24-111/2 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 17.75 44.00 24.00 44.00 17.25 1.1250 Min Weld Len 2X: Bending Load 350.00 350.00 350.00 350.00 350.00 0.5000 Axial Load 11,094.96 10,559.67 43,746.36 10,446.98 10,977.93 Max Load Fillers TC: fa 3,367.82 5,674.19 23,506.91 5,613.64 3,332.30 49,625.71 Maximum K L/r 45.37 112.47 46.01 112.47 44.10 Max Load no Fillers TC: Fcr 43,012.66 19,827.17 42,829.38 19,827.17 43,373.79 45,547.55 TC Fa 25,807.59 11,896.30 25,697.63 11,896.30 26,024.28 OAL425.46 25.46 Ryy. F'e 741,753.06 54,867.12 327,847.97 54,867.12 785,376.44 BC OAURyy: Cm 0.9977 0.9483 0.9520 0.9488 0.9979 430.52 Panel Point Moment 6062.05 7147.97 2644.44 6678.96 8916.13 BC Stress: Mid Panel Moment 779.38 4751.28 1750.00 4905.88 6510.10 1.00 Panel Point fb 2988.54 14583.67 5395.34 13626.78 4395.58 121..8888 1293 Mid Panel fb 340.13 4066.04 1497.61 4198.35 3209.42 TC Shear Stress: Fillers 0 0 0 0 0 9,421.10 Panel Point Stress 6,356.37 20,257.87 28,902.25 19,240.42 7,727.88 BC Shear Stress: Mid Panel Stress 0.0766 0.6151 0.9627 0.6142 0.1715 12,407.18 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 14,535.32 21,311.81 1,511.83 5,144.15 3.01 x 0.230 1 R100=round 1 W3 1,059.02 24,373.24 10,214.25 10,655.20 3.67 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 8,924.12 10,742.43 907.89 5,135.76 4.66 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 801.21 18,714.09 7,900.92 8,561.94 3.02 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 6,990.24 8,984.69 694.53 4,159.61 3.99 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 587.85 14,381.54 5,967.04 6,671.28 2.68 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 5,056.36 5,758.64 481.17 1,988.17 3.78 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W9 374.49 8,984.69 4,033.16 4,159.61 2.30 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 3,122.48 4,802.89 308.37 1,507.19 2.73 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 308.37 7,826.93 2,961.06 3,425.15 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W12 2,961.06 4,802.89 427.20 1,507.19 2.59 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W12 2,961.06 4,802.89 427.20 1,507.19 2.59 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 308.37 7,826.93 2,961.06 3,425.15 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W10 3,122.48 4,802.89 308.37 1,507.19 2.73 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 374.49 8,984.69 4,033.16 4,159.61 2.30 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 5,056.36 5,758.64 481.17 1,988.17 3.78 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 587.85 14,381.54 5,967.04 6,671.28 2.68 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 6,990.24 8,984.69 694.53 4,159.61 3.99 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 801.21 18,714.09 7,900.92 8,561.94 3.02 x 0.176 1 C34AA= 1.125 x 1.549 x.176 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: i/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:41:42 PM NEW MILLENNIUM Location: Joist Description: Mark: BUIL CIING %V6TEM% PORTLAND,OR Short Span Crimp 30K3501200 TJ17 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W4 8,924.12 10,742.43 907.89 5,135.76 4.66 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 1,059.02 24,373.24 10,214.25 10,655.20 3.67 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 14,434.79 21,311.81 1,821.21 5,231.07 2.99 x 0.230 1 R100=round 1 V1 1,399.02 7,826.93 2,364.08 3,649.83 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V2 700.00 4,802.89 1,894.70 2,361.49 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: ij�//// 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:41:42 PM NEW MILLENNIUM Location: Joist Description: Mark: euiLniNc SYSTBM9 PORTLAND,OR Short Span Crimp 30K350/200 TJ17 TCX Design TCX Left TCX Right __ TCX Length '0-1 1/4 TCX Length 0-7 1/2 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-2 BPL Length 2-7 3/4 Clear Bearing 0-5 1/4 Clear Bearing 0-11 5/8 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.02 Reqd TL Def L/80 , 0.09 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.01 Reqd LL Def L/120 0.06 Section Modulus 2.0284 Section Modulus 2.0284 Reqd SM 0.0051 Reqd SM 0.2972 Mom of Inertia 2.6899 Mom of Inertia 2.6899 Reqd MI 0.0003 Reqd MI 0.0750 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) i, 'N`, �v'' '/ y A // NN i ,NNN ii // i „//' / i Concentrated Loads Conc @ 0-7 1/2 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM - Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case Gc: DL+CL+0.0.5(TLI.-WL--C+AX*IP STRESS ANALYSIS- PAGE 1 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:03:02 PM NEW NI I L L E N N I U NI Location: Joist Description: Mark: B LOLMING SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 TJ21 Geometry Base Length: Working Length: Joist Depth: !Effective Depth: BC Panel Length: Shape: 46-6 46-2 30.00 1 28.66 10 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-2 3/4 3-3 1/4 TT1TT rr i rr r...rrrrrrlllTI 111111111_. _r ITT 1fF TC Panel 1-6 3/4 1-7 1/4 � , First Half 2-0 2-0 First Diag. 5-2 3/4 5-3 1/4 Depth 30.00 30.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 46-6 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 46-6 L-BL Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 46-6 L-BL Conc @ any pp(lbs) CL(1) 1,300.00 0.00 TC + Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere (lbs) CL(1) 350.00 0.00 TC + Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 46-6 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 10,354.30 10,382.35 2,595.59 50,147.29 48,916.05 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,176.87 11,735.86 0.00 0.00 16,439.97 1,492.44 46.60 0-2 V1S 1,104.45 11,205.94 0.00 0.00 2,987.15 3,944.74 34.95 1-6 3/4 W3 1,104.45 11,205.94 17,684.91 1,786.11 1,061.74 11,724.38 37.38 3-2 3/4 W4 2,370.49 23,636.57 17,684.91 1,786.11 10,430.93 910.22 37.38 5-2 3/4 W5 2,370.49 23,636.57 29,002.04 2,886.21 803.27 9,258.46 37.38 7-2 3/4 W6 3,333.26 33,781.34 29,002.04 2,886.21 8,345.44 696.31 37.38 9-2 3/4 W7 3,333.26 33,781.34 37,974.45 3,711.65 589.36 7,172.97 37.38 11-2 3/4 W8 4,021.36 41,581.38 37,974.45 3,711.65 6,259.94 482.41 37.38 13-2 3/4 W9 4,021.36 41,581.38 44,602.13 4,262.41 375.45 5,087.47 37.38 15-2 3/4 W10 4,434.79 47,036.70 44,602.13 4,262.41 4,174.45 308.61 37.38 17-2 3/4 W11 4,434.79 47,036.70 48,885.09 4,538.51 791.48 3,385.47 37.38 19-2 3/4 W12 4,573.56 50,147.29 48,885.09 4,538.51 3,385.47 1,182.78 37.38 21-23/4 W12 4,573.56 50,147.29 48,916.05 4,539.94 3,385.47 1,182.78 37.38 23-2 3/4 W11 4,437.65 47,081.18 48,916.05 4,539.94 791.48 3,385.47 37.38 25-2 3/4 W10 4,437.65 47,081.18 44,658.82 4,266.70 4,174.45 308.61 37.38 27-2 3/4 W9 4,027.08 41,650.28 44,658.82 4,266.70 375.45 5,087.47 37.38 29-2 3/4 W8 4,027.08 41,650.28 38,055.57 3,718.80 6,259.94 482.41 37.38 31-23/4 W7 3,341.85 33,874.66 38,055.57 3,718.80 589.36 7,172.97 37.38 33-2 3/4 W6 3,341.85 33,874.66 29,107.59 2,896.23 8,345.44 696.31 37.38 35-2 3/4 W5 2,381.94 23,754.32 29,107.59 2,896.23 803.27 9,258.46 37.38 37-2 3/4 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 0Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:03:02 PM NEW MILLENNIUM Location: Joist Description: Mark: BULL.OWG SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 TJ21 Stress Anal sis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W4 2,381.94 23,754.32 17,814.88 1,798.99 10,430.93 910.22 37.38 39-23/4 W3 1,118.75 11,330.68 17,814.88 1,798.99 1,061.74 11,724.38 37.38 41-2 3/4 V 1 S 1,118.75 11,330.68 0.00 0.00 2,987.15 3,944.74 34.95 44-10 3/4 W2 1,447.60 11,864.96 0.00 0.00 16,587.84 1,826.49 47.00 43-2 3/4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 2,000.00 3,195.21 28.66 STRESS ANALYSIS- PAGE 2 /�,/'� Job Number: Job Name: Date Run: �i/f 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:03:02 PM NEW MILLENNIUM Location: Joist Description: Mark: EI.lIL.CENG SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 TJ21 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 1.0162 0.8183 0.4925 1.5555 0.7604 0.6804 0.9652 A42A-2.6250 x.209 BC 0.8173 0.6134 0.3924 1.2964 0.5795 0.3076 1.0000 2021 =2 x 2 x.216 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 746.13 283.29 424.94 21-01/4 25-111/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 16.75 44.00 24.00 44.00 17.25 1.1250 Min Weld Len 2X: Bending Load 350.00 350.00 350.00 350.00 350.00 0.5000 Axial Load 11,735.86 11,205.94 50,147.29 11,330.68 11,864.96 Max Load Fillers TC: fa 3,386.19 5,513.65 24,673.93 5,575.02 3,423.44 54,747.40 Maximum K Lir 34.01 89.34 36.55 89.34 35.03 Max Load no Fillers TC: Fcr 44,476.86 27,476.03 43,918.29 27,476.03 44,257.41 51,956.74 Fa 26,686.12 16,485.62 26,350.97 16,485.62 26,554.45 TC OAURyi. 356.15 Fe 900,136.69 98,995.97 591,531.44 98,995.97 848,711.13 BC OAURyy: Cm 0.9981 0.9722 0.9721 0.9718 0.9980 427.35 Panel Point Moment 5714.05 6867.32 2644.44 6233.50 8916.14 BC Stress: Mid Panel Moment 604.24 4843.79 1750.00 5094.16 6414.91 1.00 Panel Point fb 2346.09 9409.76 3623.48 8541.29 3660.82 BC 122..3232 42 Mid Panel fb 245.89 2706.66 977.88 2846.56 2633.85 TC Shear Stress: Fillers 0 0 0 0 0 11,950.15 Panel Point Stress 5,732.28 14,923.41 28,297.41 14,116.32 7,084.26 BC Shear Stress: Mid Panel Stress 0.0720 0.4235 0.9677 0.4319 0.1559 12,378.79 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 16,439.97 23,679.79 1,492.44 5,345.06 3.40 x 0.230 1 R100= round 1 W3 1,061.74 28,624.38 11,724.38 12,322.60 4.21 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 10,430.93 14,381.54 910.22 6,694.58 4.68 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 803.27 24,373.24 9,258.46 10,694.36 3.33 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W6 8,345.44 8,984.69 696.31 4,174.72 4.76 x 0.118 1 Cl 8BB= 1.125 x 1.035 x.118 W7 589.36 16,730.22 7,172.97 7,461.23 3.06 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W8 6,259.94 7,826.93 482.41 3,437.78 4.13 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W9 375.45 10,742.43 5,087.47 5,153.48 2.66 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W10 4,174.45 4,802.89 308.61 1,518.33 3.65 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 791.48 7,826.93 3,385.47 3,437.78 2.24 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W12 3,385.47 4,802.89 1,182.78 1,518.33 2.96 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W12 3,385.47 4,802.89 1,182.78 1,518.33 2.96 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 791.48 7,826.93 3,385.47 3,437.78 2.24 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W10 4,174.45 4,802.89 308.61 1,518.33 3.65 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 375.45 10,742.43 5,087.47 5,153.48 2.66 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W8 6,259.94 7,826.93 482.41 3,437.78 4.13 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 589.36 16,730.22 7,172.97 7,461.23 3.06 x 0.158 1 C32BA= 1.125 x 1.520 x.158 W6 8,345.44 8,984.69 696.31 4,174.72 4.76 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 803.27 24,373.24 9,258.46 10,694.36 3.33 x 0.188 1 C38BA= 1.125 x 1.845 x.199 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 0/�i/� Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:03:02 PM NEW MILLENNIUM Location: Joist Description: Mark: FILM ming.. SY%TEr.A% PORTLAND,OR Short Span Crimp 30K350/200 TJ21 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W4-- - 40,430.93- 14,381.54 910.22 6,694.58 4.68 x 0.150 . 1 C28BB= 1.125 x 1.344 x.150 W3 1,061.74 28,624.38 11,724.38 12,322.60 4.21 x 0.188 1 C40BA= 1.125 x 2.014 x.218 W2 16,587.84 23,679.79 1,826.49 5,255.53 3.43 x 0.230 1 R100=round 1 V1 2,987.15 8,984.69 3,944.74 4,443.20 2.25 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V2 2,000.00 7,826.93 3,195.21 4,276.59 2.05 x 0.102 1 C16BB= 1.125 x 1.025 x.102 STRESS ANALYSIS- PAGE 3 I�/� Job Number: Job Name: Date Run: /�/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 2:03:02 PM NEW INA I L LEN N I UNI Location: Joist Description: Mark: RUM ninon SYSTEMA. PORTLAND,OR Short Span Crimp 30K350/200 TJ21 TCX Design TCX Left TCX Right TCX Length 0-2 1/4 TCX Length 0-7 1/2 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-1 7/8 BPL Length 2-7 5/8 Clear Bearing 0-6 1/8 Clear Bearing 0-11 3/8 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.03 Reqd TL Def L/80 0.09 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.02 Reqd LL Def L/120 0.06 Section Modulus 2.4356 Section Modulus 2.4356 Reqd SM 0.0088 Reqd SM 0.2972 Mom of Inertia 3.0580 Mom of Inertia 3.0580 Reqd MI 0.0008 Reqd MI 0.0750 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) „ , „ ,, -,. \.\\ i '-,N \ ' j 47i i Concentrated Loads Conc @ 0-7 1/2 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f:0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case Gc: DL*CL+0.85f i Li*WL+C+AX+IP - STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: �/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:40:46 PM NEW MILLENNIUM Location: Joist Description: Mark: REALIZING SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 TJ22 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 46-6 46-2 30.00 28.84 10 @ 4-0 Parallel Chords T Variable Left End Right End BC Panel 323/4 331/4 1111111111111111111111111111111111 i _ TC Panel 1-6 3/4 1-7114 _II 11111111111111111111111111 111111111111 111111"11r IIPP First Half 2-0 2-0 First Diag. 5-2 3/4 5-3 1/4 Depth 30.00 30.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 46-6 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 46-6 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Uniform (plf) SM(1) 16.00 16.00 TC + 0-0 46-6 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) SM(1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 46-6 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 9,068.36 9,089.38 2,272.34 43,597.50 42,903.57 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,169.54 10,844.76 0.00 0.00 14,293.39 1,486.67 46.71 0-2 V1S 1,097.57 10,318.15 0.00 0.00 1,398.97 2,354.48 35.10 1-6 3/4 W3 1,097.57 10,318.15 16,205.57 1,774.99 1,059.02 10,195.06 37.52 3-2 3/4 W4 2,355.73 21,579.23 16,205.57 1,774.99 8,904.92 907.89 37.52 5-2 3/4 W5 2,355.73 21,579.23 26,370.37 2,868.24 801.21 7,881.73 37.52 7-2 3/4 W6 3,312.50 30,578.98 26,370.37 2,868.24 6,971.04 694.53 37.52 9-2 3/4 W7 3,312.50 30,578.98 34,205.06 3,688.53 587.85 5,947.84 37.52 11-2 3/4 W8 3,996.32 37,248.61 34,205.06 3,688.53 5,037.16 481.17 37.52 13-2 3/4 W9 3,996.32 37,248.61 39,709.62 4,235.87 374.49 4,013.97 37.52 15-2 3/4 W10 4,407.18 41,588.11 39,709.62 4,235.87 3,103.28 307.82 37.52 17-2 3/4 W11 4,407.18 41,588.11 42,884.07 4,510.24 307.82 2,956.26 37.52 19-2 3/4 W12 4,545.08 43,597.50 42,884.07 4,510.24 2,956.26 411.82 37.52 21-2 3/4 W12 4,545.08 43,597.50 42,903.57 4,511.67 2,956.26 411.82 37.52 23-2 3/4 W11 4,410.02 41,621.05 42,903.57 4,511.67 307.82 2,956.26 37.52 25-2 3/4 W10 4,410.02 41,621.05 39,754.71 4,240.13 3,103.28 307.82 37.52 27-2 3/4 W9 4,002.00 37,305.82 39,754.71 4,240.13 374.49 4,013.97 37.52 29-2 3/4 W8 4,002.00 37,305.82 34,274.41 3,695.64 5,037.16 481.17 37.52 31-2 3/4 W7 3,321.03 30,660.47 34,274.41 3,695.64 587.85 5,947.84 37.52 33-2 3/4 W6 3,321.03 30,660.47 26,464.00 2,878.19 6,971.04 694.53 37.52 35-2 3/4 W5 2,367.11 21,684.99 26,464.00 2,878.19 801.21 7,881.73 37.52 37-23/4 W4 2,367.11 21,684.99 16,323.46 1,787.78 8,904.92 907.89 37.52 39-2 3/4 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 G, Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:40:46 PM NEW MILLENNIUM Location: Joist Description: Mark: RULL.OING SYS,EM4 PORTLAND,OR Short Span Crimp 30K350/200 TJ22 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W3 1,111.79 10,430.84 16,323.46 1,787.78 1,059.02 10,195.06 37.52 41-2 3/4 V1S 1,111.79 10,430.84 0.00 0.00 1,398.97 2,354.48 35.10 44-10 3/4 W2 1,438.58 10,961.79 0.00 0.00 14,410.97 1,819.35 47.11 43-2 3/4 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 700.00 1,894.00 28.84 STRESS ANALYSIS- PAGE 2 0 Job Number: 5618-0088 Job Name: Date Run: JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:40:46 PM NEW MILLENNIUM Location: Joist Description: Mark: RUIL.OING %Y%TF.MS PORTLAND,OR Short Span Crimp 30K350/200 TJ22 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x .248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 674.71 256.17 384.26 17-71/2 25-0 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 16.75 44.00 24.00 44.00 17.25 1.1250 Min Weld Len 2X:: Bending Load 350.00 350.00 350.00 350.00 350.00 0.5000 Axial Load 10,844.76 10,318.15 43,597.50 10,430.84 10,961.79 Max Load Fillers TC: fa 3,291.88 5,544.41 23,426.92 5,604.96 3,327.40 49,625.71 Maximum K L/r 42.82 112.47 46.01 112.47 44.10 Max Load no Fillers TC: Fcr 43,727.52 19,827.17 42,829.38 19,827.17 43,373.79 45,547.55 Fa 26,236.51 11,896.30 25,697.63 11,896.30 26,024.28 TC OAURyy: 424.69 F'e 832,964.44 54,867.12 327,847.97 54,867.12 785,376.44 BC OAL/Ryy: Cm 0.9980 0.9495 0.9521 0.9489 0.9979 429.74 Panel Point Moment 5999.55 7152.82 2644.44 6678.96 8916.13 BC Stress: Mid Panel Moment 556.66 4749.67 1750.00 4905.88 6510.10 1.00 BC L/Rz Panel Point fb 2957.73 14593.58 5395.34 13626.78 4395.58 121.88: 121.8893 Mid Panel fb 242.93 4064.67 1497.61 4198.35 3209.42 TC Shear Stress: Fillers 0 0 0 0 0 9,405.55 Panel Point Stress 6,249.61 20,137.99 28,822.26 19,231.74 7,722.98 BC Shear Stress: Mid Panel Stress 0.0709 0.6036 0.9596 0.6135 0.1714 12,386.71 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 14,293.39 21,311.81 1,486.67 5,319.77 2.96 x 0.230 1 R100=round 1 W3 1,059.02 24,373.24 10,195.06 10,655.20 3.66 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 8,904.92 10,742.43 907.89 5,135.76 4.65 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 801.21 18,714.09 7,881.73 8,561.94 3.02 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 6,971.04 8,984.69 694.53 4,159.61 3.98 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 587.85 14,381.54 5,947.84 6,671.28 2.67 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 5,037.16 5,758.64 481.17 1,988.17 3.77 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W9 374.49 8,984.69 4,013.97 4,159.61 2.29 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 3,103.28 4,802.89 307.82 1,507.19 2.71 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 307.82 7,826.93 2,956.26 3,425.15 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W12 2,956.26 4,802.89 411.82 1,507.19 2.59 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W12 2,956.26 4,802.89 411.82 1,507.19 2.59 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 307.82 7,826.93 2,956.26 3,425.15 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W10 3,103.28 4,802.89 307.82 1,507.19 2.71 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 374.49 8,984.69 4,013.97 4,159.61 2.29 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 5,037.16 5,758.64 481.17 1,988.17 3.77 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 587.85 14,381.54 5,947.84 6,671.28 2.67 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 6,971.04 8,984.69 694.53 4,159.61 3.98 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 801.21 18,714.09 7,881.73 8,561.94 3.02 x 0.176 1 C34AA= 1.125 x 1.549 x.176 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 ', Job Number: 5618-0088 Job Name: Date Run: JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 1:40:46 PM NEW NI I L L E N N t U Nt Location: Joist Description: Mark: BUIL OWG SYSTEMS PORTLAND,OR Short Span Crimp 30K3501200 TJ22 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material — W4 8,904.92 10,742.43 907.89 5,135.76 4.65 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 1,059.02 24,373.24 10,195.06 10,655.20 3.66 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 14,410.97 21,311.81 1,819.35 5,231.07 2.98 x 0.230 1 R100=round 1 V1 1,398.97 7,826.93 2,354.48 3,649.83 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V2 700.00 4,802.89 1,894.00 2,361.49 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 1:40:46 PM NEW MILLENNIUM Location: Joist Description: Mark: wuu.nwr SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200TJ22 J TCX Design TCX Left TCX Right TCX Length 0-2 1/4 TCX Length 0-7 1/2 - TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-2 BPL Length 2-7 3/4 Clear Bearing 0-6 1/4 Clear Bearing 0-11 5/8 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.03 Reqd TL Def L/80 0.09 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.02 Reqd LL Def L/120 0.06 Section Modulus 2.0284 Section Modulus 2.0284 Reqd SM 0.0088 Reqd SM 0.2972 Mom of Inertia 2.6899 Mom of Inertia 2.6899 Reqd MI 0.0008 Reqd MI 0.0750 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) c‘ `� / ,Z;. .\\ , N N �,, /�/ ���� ;f / j Nv v / / /////////2/ \ \ \NNNv N //'/X i� / / N /r Concentrated Loads Conc @ 0-7 1/2 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d: 0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case Gc: DL+CL+0.057 i L)--WL*C*AX+IP STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 10:27:14 AM NEW MILLENNIUM Location: Joist Description: Mark: BUILDING SYSTEMS PORTLAND,OR Short Span Round 14K300/162 TJ25 Geometry Base Length: Working Length: I Joist Depth: Effective Depth: BC Panel Length: Shape: 19-10 1/4 19-6 1/4 1 14.00 13.07 10 @ 1-8 Parallel Chords Variable Left End Right End BC Panel 1-7 1/8 1-7 1/8 TC Panel 0-10 0-10 .` .I_.1.=VI/ IrlIVIIIIIIIIIPPA 1 __ . _..:_. _ p .. ..I. . . .. . ...I_.L . . L . I First Half 0-10 0-10 First Diag. 2-5 1/8 2-5 1/8 Depth 14.00 14.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 138.00 138.00 TC + 0-0 19-10 1/4 L-BL Uniform (plf) LL(1) 162.00 162.00 TC + 0-0 19-10 1/4 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Conc @ any pp (lbs) CL(1) 350.00 0.00 TC + Axial (lbs) WL(1) 412.00 0.00 TC + 0-0 0-0 L-BL Uniform (plf) SM(1) 14.00 14.00 TC + 0-0 19-10 1/4 L-BL Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Conc Load (lbs) WL(1) 412.00 0.00 TC + 3-0 9-0 L-OAL Conc Load (lbs) WL(1) 412.00 0.00 TC + 14-0 20-0 L-OAL Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 19-10 1/4 L-BL Conc Load(lbs) WL(2) 412.00 0.00 TC - 3-0 9-0 L-OAL Conc Load (lbs) WL(2) 412.00 0.00 TC - 14-0 20-0 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 20.00 20.00 3,908.60 3,918.83 979.71 19,492.40 17,419.42 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 3,493.51 6,221.70 0.00 0.00 6,315.46 4,392.12 21.55 0-2 V1S 2,224.67 6,017.00 0.00 0.00 3,867.93 1,651.48 15.94 0-10 W3 2,224.67 6,017.00 6,408.97 2,397.48 1,071.15 4,290.37 16.46 1-7 1/8 W4 2,789.87 10,223.10 6,408.97 2,397.48 3,757.77 987.00 16.46 2-51/8 W5 2,789.87 10,223.10 10,233.35 3,182.26 947.10 3,631.01 16.46 3-3 1/8 W6 3,535.45 13,774.83 10,233.35 3,182.26 3,086.50 861.07 16.46 4-1 1/8 W7 3,535.45 13,774.83 13,426.28 3,888.64 814.52 2,938.60 16.46 4-11 1/8 W8 4,202.63 16,664.93 13,426.28 3,888.64 2,394.09 728.49 16.46 5-9 1/8 W9 4,202.63 16,664.93 15,985.58 4,516.62 689.10 2,267.32 16.46 6-71/8 W10 4,559.49 18,661.50 15,985.58 4,516.62 1,722.81 602.56 16.46 7-5 1/8 W11 4,559.49 18,661.50 17,419.42 4,602.37 482.55 1,365.71 16.46 8-3 1/8 W12 4,601.61 19,492.40 17,419.42 4,602.37 1,078.99 1,233.43 16.46 9-1 1/8 W12 4,601.61 19,492.40 17,417.91 4,600.85 1,078.99 1,233.43 16.46 9-11 1/8 W11 4,560.90 18,662.90 17,417.91 4,600.85 482.55 1,365.71 16.46 10-9 1/8 W10 4,560.90 18,662.90 15,989.90 4,520.94 1,722.81 602.56 16.46 11-7 1/8 W9 4,209.87 16,672.17 15,989.90 4,520.94 689.10 2,267.32 16.46 12-51/8 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 �/� Job Number: Job Name: Date Run: fir/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/2019 10:27:14 AM NEW MILLENNIUM Location: Joist Description: Mark: wi.M.oinic SYS.TEM% PORTLAND,OR Short Span Round 14K300/162 TJ25 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W8 4,209.87, 16,672.17 13,436.44 3,898.79 2,394.09 728.49 16.46 13-31/8 W7 3,544.09 13,783.47 13,436.44 3,898.79 814.52 2,938.60 16.46 14-1 1/8 W6 3,544.09 13,783.47 10,233.35 3,189.39 3,086.50 861.07 16.46 14-111/8 W5 2,795.48 10,228.72 10,233.35 3,189.39 947.10 3,631.01 16.46 15-91/8 W4 2,795.48 10,228.72 6,408.96 2,401.58 3,757.77 987.00 16.46 16-71/8 W3 2,224.67 6,019.59 6,408.96 2,401.58 1,071.15 4,290.37 16.46 17-51/8 V1S 2,224.67 6,019.59 0.00 0.00 3,867.93 1,651.48 15.94 19-01/4 W2 3,493.51 6,224.29 0.00 0.00 6,315.46 4,392.12 21.55 18-31/8 1 STRESS ANALYSIS- PAGE 2 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:27:14 AM NEW MILLENNIUM Location: Joist Description: Mark: 9LLLOING SYSTEM% PORTLAND,OR Short Span Round 14K300/162 TJ25 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.4771 0.5392 0.3214 0.9323 0.5106 0.1387 1.0000 A28B= 1.7350 x 0.150 BC 0.3151 0.4675 0.2972 0.8133 0.4154 0.0689 0.9057 1510= 1 1/2 x 1 1/2 x.109 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 65.29 327.90 491.85 11-10 3/4 10-41/4 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 8.00 19.13 20.00 19.13 8.00 0.5000 Bending Load 300.00 300.00 300.00 300.00 300.00 0.5000Md Len 2X: Axial Load 6,221.70 6,017.00 19,492.40 6,019.59 6,224.29 Max Load Fillers TC: fa 2,605.84 6,305.81 20,428.00 6,308.52 2,606.92 23,966.52 Maximum K L/r 36.30 59.51 46.67 59.51 36.30 Max Load no Fillers TC: Fcr 45,408.36 38,595.03 42,638.66 38,595.03 45,408.36 22,510.16 Fa 27,245.01 23,157.02 25,583.20 23,157.02 27,245.01 TCO2L/Ryy: 251.25 F'e 3,706,204.25 227,506.94 369,840.97 227,506.94 3,706,204.25 BC OAL/Ryy: Cm 0.9996 0.9861 0.9630 0.9861 0.9996 288.03 Panel Point Moment 18578.06 1956.53 1870.37 1956.53 18578.06 BC Stress: Mid Panel Moment 14903.63 1450.78 1291.67 1450.78 14903.63 0.92 Panel Point fb 10673.99 8635.83 8255.52 8635.83 10673.99 BC 67.229494 8 Mid Panel fb 8562.85 2670.39 2377.52 2670.39 8562.85 Fillers 0 0 0 0 TC Shear Stress: 0 9,923.81 Panel Point Stress 13,279.83 14,941.63 28,683.52 14,944.35 13,280.91 BC Shear stress: Mid Panel Stress 0.3335 0.3541 0.8732 0.3542 0.3335 12,377.90 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 6,315.46 10,072.50 4,392.12 5,365.91 2.00 x 0.192 1 R068= round 11/16 V1S 3,867.93 9,250.01 1,651.48 4,990.77 2.00 x 0.185 1 R062= round 5/8 W3 1,071.15 9,250.01 4,290.37 4,792.10 2.00 x 0.185 1 R062= round 5/8 W4 3,757.77 9,250.01 987.00 4,792.10 2.00 x 0.185 1 R062= round 5/8 W5 947.10 9,250.01 3,631.01 4,792.10 2.00 x 0.185 1 R062= round 5/8 W6 3,086.50 9,250.01 861.07 4,792.10 2.00 x 0.185 1 R062=round 5/8 W7 814.52 9,250.01 2,938.60 4,792.10 2.00 x 0.185 1 R062= round 5/8 W8 2,394.09 9,250.01 728.49 4,792.10 2.00 x 0.185 1 R062= round 5/8 W9 689.10 9,250.01 2,267.32 4,792.10 2.00 x 0.185 1 R062= round 5/8 W10 1,722.81 5,918.44 602.56 2,115.50 2.00 x 0.170 1 R050= round 1/2 W11 482.55 5,918.44 1,365.71 2,115.50 2.00 x 0.170 1 R050=round 1/2 W12 1,078.99 5,918.44 1,233.43 2,115.50 2.00 x 0.170 1 R050= round 1/2 W12 1,078.99 5,918.44 1,233.43 2,115.50 2.00 x 0.170 1 R050= round 1/2 W11 482.55 5,918.44 1,365.71 2,115.50 2.00 x 0.170 1 R050=round 1/2 W10 1,722.81 5,918.44 602.56 2,115.50 2.00 x 0.170 1 R050= round 1/2 W9 689.10 9,250.01 2,267.32 4,792.10 2.00 x 0.185 1 R062= round 5/8 W8 2,394.09 9,250.01 728.49 4,792.10 2.00 x 0.185 1 R062=round 5/8 W7 814.52 9,250.01 2,938.60 4,792.10 2.00 x 0.185 1 R062= round 5/8 W6 3,086.50 9,250.01 861.07 4,792.10 2.00 x 0.185 1 R062= round 5/8 *Continued on Next Page... H- STRESS ANALYSIS- PAGE 2 �/� Job Number: Job Name: Date Run: �j 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:27:14 AM NEW MILLENNIUM Location: Joist Description: Mark: wIin.niNr.. SYSTEMS PORTLAND,OR Short Span Round 14K300/162 TJ25 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W5 947.10 9,250.01 3,631.01 4,792.10 2.00 x 0.185 1 R062=round 5/8 W4 3,757.77 9,250.01 987.00 4,792.10 2.00 x 0.185 1 R062= round 5/8 W3 1,071.15 9,250.01 4,290.37 4,792.10 2.00 x 0.185 1 R062= round 5/8 V1 S 3,867.93 9,250.01 1,651.48 4,990.77 2.00 x 0.185 1 R062= round 5/8 W2 6,315.46 10,072.50 4,392.12 5,365.91 2.00 x 0.192 1 R068= round 11/16 STRESS ANALYSIS- PAGE 3 0 Job Number: Job Name: Date Run: �/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/8/201910:27:14 AM NEW M I L L E N N I U VI Location: Joist Description: Mark: eI.m.nwr.. SY8IiTE1.4% PORTLAND,OR Short Span Round 14K300/162 TJ25 TCX Design TCX Left TCX Right TCX Length 1-6 1/2 TCX Length 1-6 1/2 -------._ TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-9 1/4 BPL Length 2-9 1/4 Clear Bearing 1-10 1/2 Clear Bearing 1-10 1/2 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 300.00 Total Load 300.00 Reqd TL Def L/80 0.23 Reqd TL Def L/80 0.23 Live Load 162.00 Live Load 162.00 Reqd LL Def L/120 0.15 Reqd LL Def L/120 0.15 Section Modulus 1.4515 Section Modulus 1.4515 Reqd SM 0.6193 Reqd SM 0.6193 Mom of Inertia 1.9787 Mom of Inertia 1.9787 Reqd MI 0.3255 Reqd MI 0.3255 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) %! S ;j ' Concentrated Loads Concentrated Loads Conc @ 1-6 1/2 650.00 Conc @ 1-6 1/2 650.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e: 0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM ase C: ■ t +1.. +" t +' P+ - STRESS ANALYSIS- PAGE 1 �/�' Job Number: Job Name: Date Run: �+�� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:35:09 PM N E VN M I L L EN NI U M Location: Joist Description: Mark: ®WLt3WG SYSTEMS PORTLAND,OR Short Span Crimp 28K350/200 TJ3 Geometry Base Length: Working Length: Joist Depth: Effective Depth: BC Panel Length: Shape: 41-7 5/8 41-3 5/8 28.00 26.84 9 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 2-6 1/2 3-1 1/8 TC Panel 1-7 2-0 \fir �_�_��__� First Half 2-0 2-0 __ -' First Diag. 4-6 1/2 5-1 1/8 Depth 28.00 28.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 41-7 5/8 L-BL Uniform (pif) DL(1) 150.00 150.00 TC + 0-0 41-7 5/8 L-BL Uniform (plf) LL(1) 360.00 0.00 TC + 0-0 16-2 L-OAL Uniform (pif) SM(1) 16.00 16.00 TC + 0-0 41-7 5/8 L-BL Axial (lbs) WL(1) 412.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Conc L7a any pp (lbs) CL(1) 350.00 0.00 TC + Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Conc Load (lbs) DL(1) 1,440.00 0.00 TC + 1-1 1-1 L-OAL Conc Load (lbs) WL(1) 412.00 0.00 TC + 34-0 40-0 L-OAL Gross Uplift(plf) WL(2) 105.00 105.00 TC - 0-0 41-7 5/8 L-BL Conc Load (lbs) WL(2) 412.00 0.00 TC - 34-0 40-0 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 12,183.45 8,656.65 3,045.86 41,373.15 41,728.62 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 2,302.63 11,697.46 0.00 0.00 16,304.09 3,164.51 39.15 0-2 V1S 2,204.21 10,791.83 0.00 0.00 343.20 3,751.12 29.20 1-7 W3 2,204.21 10,791.83 17,738.08 3,937.88 2,917.54 11,639.50 36.01 2-61/2 W4 5,438.78 23,780.09 17,738.08 3,937.88 9,580.57 2,558.79 36.01 4-61/2 W5 5,438.78 23,780.09 28,802.97 6,751.90 1,971.37 7,921.60 36.01 6-6 1/2 W6 7,877.24 32,885.39 28,802.97 6,751.90 6,667.26 1,689.66 36.01 8-61/2 W7 7,877.24 32,885.39 36,105.97 8,814.79 1,407.94 5,598.13 36.01 10-61/2 W8 9,564.57 38,543.33 36,105.97 8,814.79 4,659.09 1,126.23, 36.01 12-6.x/2 W9 9,564.57 38,543.33 40,276.13 10,126.56 844.52 4,085.99 36.01 14-61/2 W10 10,500.77 41,373.15 40,276.13 10,126.56 4,085.99 840.39 36.01 16-6 1/2 W11 10,500.77 41,373.15 41,728.62 10,687.20 2,243.60 4,085.99 36.01 18-61/2 W11 10,685.85 40,918.61 41,728.62 10,687.20 2,243.60 4,085.99 36.01 20-6 1/2 W10 10,685.85 40,918.61 39,243.62 10,496.71 4,085.99 840.39 36.01 22-61/2 W9 10,119.79 36,942.69 39,243.62 10,496.71 844.52 4,085.99 36.01 24-61/2 W8 10,119.79 36,942.69 34,015.83 9,555.10 4,659.09 1,126.23 36.01 26-61/2 W7 8,802.62 30,463.03 34,015.83 9,555.10 1,407.94 5,598.13 36.01 28-6 1/2 *Continued on Next Page... r STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 1:35:09 PM NEW M I L L E N N I UM Location: Joist Description: Mark: BUIL.DINO 5V%TEMS PORTLAND,OR Short Span Crimp 28K350/200 TJ3 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W6 8,802.62 30,463.03 26,284.29 7,862.36 6,667.26 1,689.66 36.01 30-61/2 W5 6,634.54 21,479.61 26,284.29 7,862.36 1,971.37 7,921.60 36.01 32-61/2 W4 6,634.54 21,479.61 16,048.99 4,950.31 9,580.57 2,558.79 36.01 34-61/2 W3 3,026.95 10,753.57 16,048.99 4,950.31 2,917.54 11,639.50 36.01 36-61/2 V1S 3,026.95 10,753.57 0.00 0.00 1,481.40 2,330.48 29.88 39-7 5/8 W2 3,153.44 11,114.98 0.00 0.00 13,704.48 4,061.53 44.21 38-6 1/2 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 1,112.00 2,251.47 26.84 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �/i/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:35:09 PM NEW MILLENNIUM Location: Joist Description: Mark: Alla now.; 'SY%TEikA% PORTLAND,OR Short Span Crimp 28K350/200 TJ3 Chord Properties Chord Area Rx Rz Ryy Y Ix Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 584.54 309.95 464.93 17-6 3/4 16-2 7/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 17.00 35.50 24.00 37.13 22.00 1.1250 Bending Load 694.43 646.34 350.00 350.00 350.00 Min Weld Len 2X: 0.5000 Axial Load 11,697.46 10,791.83 41,373.15 10,753.57 11,114.98 Max Load Fillers TC: fa 3,550.71 5,798.94 22,231.68 5,778.38 3,373.90 49,625.71 Maximum K L/r 43.46 90.75 46.01 94.90 56.24 Max Load no Fillers TC: Fcr 43,551.60 27,382.63 42,829.38 25,881.38 39,677.35 45,547.55 TC Fa 26,130.96 16,429.57 25,697.63 15,528.83 23,806.41 3779.949.94Ryy: Fe 808,645.63 84,287.05 327,847.97 77,069.87 482,848.31 BCOAL/Ryy: Cm 0.9978 0.9656 0.9546 0.9625 0.9965 384.46 Panel Point Moment 6964.24 7659.93 2644.44 4809.62 7462.72 BC Stress: Mid Panel Moment 2652.92 4921.14 1750.00 3804.63 4379.96 0.97 Panel Point fb 3433.31 15628.21 5395.34 9812.85 3679.06 121..8888 1293 Mid Panel fb 1307.87 4211.40 1497.61 3255.92 2159.29 Fillers 0 0 0 0 0 TC Shear Stress: 11,710.52 Panel Point Stress 6,984.02 21,427.15 27,627.02 15,591.23 7,052.96 BC Shear Stress: Mid Panel Stress 0.1118 0.4891 0.9129 0.4783 0.1434 15,429.96 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 16,304.09 25,761.95 3,164.51 16,757.23 5.04 x 0.218 1 CW4OBA= 1.5 x 1.926 x.218 W3 2,917.54 28,624.38 11,639.50 12,786.97 4.18 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 9,580.57 14,381.54 2,558.79 6,928.23 4.30 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W5 1,971.37 18,714.09 7,921.60 8,898.52 3.03 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 6,667.26 7,826.93 1,689.66 3,564.90 4.40 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 1,407.94 14,381.54 5,598.13 6,928.23 2.51 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 4,659.09 4,802.89 1,126.23 1,636.66 4.07 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 W9 844.52 8,984.69 4,085.99 4,326.22 2.33 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 4,085.99 4,802.89 840.39 1,636.66 3.57 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 2,243.60 8,984.69 4,085.99 4,326.22 2.33 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W11 2,243.60 8,984.69 4,085.99 4,326.22 2.33 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 4,085.99 4,802.89 840.39 1,636.66 3.57 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 844.52 8,984.69 4,085.99 4,326.22 2.33 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 4,659.09 4,802.89 1,126.23 1,636.66 4.07 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 W7 1,407.94 14,381.54 5,598.13 6,928.23 2.51 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 6,667.26 7,826.93 1,689.66 3,564.90 4.40 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W5 1,971.37 18,714.09 7,921.60 8,898.52 3.03 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W4 9,580.57 14,381.54 2,558.79 6,928.23 4.30 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W3 2,917.54 28,624.38 11,639.50 12,786.97 4.18 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 /�i� Job Number: Job Name: Date Run: �i/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 1:35:09 PM NEW M I L L E N N I U M Location: Joist Description: Mark: euiLnmir.. SYSTEMS PORTLAND,OR ' Short Span Crimp 28K350/200 TJ3 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 13,704.48 21,311.81 4,061.53 5,940.88 2.84 x 0.230 1 R100=round 1 V1 1,481.40 7,826.93 3,751.12 4,222.09 2.48 x 0.102 1 Cl 6BB= 1.125 x 1.025 x.102 V2 1,112.00 4,802.89 2,251.47 2,577.11 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:35:09 PM NEW MILLENNIUM Location: Joist Description: Mark: AUIL.r]INr., SYSTEM% PORTLAND,OR Short Span Crimp 28K350/200 TJ3 TCX Design TCX Left TCX Right - TCX Length .0-0 TCX Length .0-6 1/8 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 1-11 3/8 BPL Length 2-10 1/2 Clear Bearing 0-3 Clear Bearing 0-10 1/4 BPL Material:2018=2 X 2 X.188 BPL Material: 2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.00 Reqd TL Def U80 0.08 Live Load 200.00 Live Load 200.00 Reqd LL Def U120 0.00 Reqd LL Def L/120 0.05 Section Modulus 2.0284 Section Modulus 2.0284 Reqd SM 0.0000 Reqd SM 0.2488, Mom of Inertia 2.6899 Mom of Inertia 2.6899 Reqd MI 0.0000 Reqd MI 0.0540 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) • it Concentrated Loads Conc @a 0-6 1/8 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL IRNOWINN " Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+I13) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case Gc: DL+CL+0.85(TL),-WL+C+AX+iP / STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run: �/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:36:06 PM NEW /VII L L E N N I UNI Location. Joist Description: Mark: BUIlO1NG SYSTEMS PORTLAND,OR Short Span Crimp 28K350/200 TJ4 Geometry Base Length: Working Length: !Joist Depth: Effective Depth: BC Panel Length: Shape: 42-2 41-10 i 28.00 26.84 9 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-0 7/8 3-1 1/8 TC Panel 1-7 2-0 .l t1TTTr{-itr--iT1 ri-r,---.-.- ...._ . First Half 2-0 2-0 IF_w First Diag. 5-0 7/8 5-1 1/8 Depth 28.00 28.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 42-2 L-BL Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 42-2 L-BL Uniform (plf) LL(1) 360.00 0.00 TC + 0-0 16-2 L-OAL Axial (lbs) WL(1) 412.00 0.00 TC + 0-0 0-0 L-BL Axial(lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 42-2 L-BL Conc @ any pp(lbs) CL(1) 350.00 0.00 TC + Axial (lbs) SM (1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 350.00 0.00 TC + Conc Load (lbs) DL(1) 1,440.00 0.00 TC + 1-1 1-1 L-OAL Conc Load (lbs) WL(1) 412.00 0.00 TC + 34-0 40-0 L-OAL Gross Uplift(plf) WL(2) 105.00 105.00 TC - 0-0 42-2 L-BL Conc Load (lbs) WL(2) 412.00 0.00 TC - 34-0 40-0 L-OAL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 12,354.97 8,766.48 3,088.74 42,621.41 42,860.53 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 2,860.43 14,016.45 0.00 0.00 18,486.92 3,611.09 44.01 0-2 V1S 2,688.89 12,513.16 0.00 0.00 419.99 4,269.95 32.25 1-7 W3 2,688.89 12,513.16 19,764.37 4,427.03 2,957.84 11,621.28 36.01 3-0 7/8 W4 5,907.47 25,670.48 19,764.37 4,427.03 9,362.47 2,599.09 36.01 5-0 7/8 W5 5,907.47 25,670.48 30,569.83 7,200.12 2,039.65 7,757.04 36.01 7-0 7/8 W6 8,304.99 34,538.58 30,569.83 7,200.12 6,818.00 1,658.88 36.01 9-0 7/8 W7 8,304.99 34,538.58 37,652.90 9,222.08 1,377.17 5,750.43 36.01 11-0 7/8 W8 9,951.39 39,988.96 37,652.90 9,222.08 4,811.39 1,095.46 36.01 13-0 7/8 A. W9 9,951.39 39,988.96 41,622.91 10,492.92 848.07 4,143.51 36.01 15-0 7/8 W10 10,846.66 42,621.41 41,622.91 10,492.92 4,143.51 848.07 36.01 17-0 7/8 W11 10,846.66 42,621.41 42,860.53 11,012.63 4,143.51 4,143.51 36.01 19-0 7/8 W11 10,990.81 41,851.04 42,860.53 11,012.63 4,143.51 4,143.51 36.01 21-0 7/8 W10 10,990.81 41,851.04 40,077.53 10,781.21 4,143.51 848.07 36.01 23-0 7/8 W9 10,383.83 37,678.07 40,077.53 10,781.21 848.07 4,143.51 36.01 25-0 7/8 W8 10,383.83 37,678.07 34,652.68 9,798.67 4,811.39 1,095.46 36.01 27-0 7/8 W7 9,025.72 31,001.35 34,652.68 9,798.67 1,377.17 5,750.43 36.01 29-0 7/8 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 /ice Job Number: Job Name: Date Run: moi// 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:36:06 PM NEW MILLENNIUM Location: Joist Description: Mark: AU/LriINC. SYSTFAAS PORTLAND,OR Short Span Crimp 28K350/200 TJ4 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W6 9,025.72 31,001.35 26,724.08 8,065.00 6,818.00 1,658.88 36.01 31-0 7/8 W5 6,705.42 21,820.87 26,724.08 8,065.00 2,039.65 7,757.04 36.01 33-0 7/8 W4 6,705.42 21,820.87 16,291.72 5,000.72 9,362.47 2,599.09 36.01 35-0 7/8 W3 3,056.90 10,868.89 16,291.72 5,000.72 2,957.84 11,621.28 36.01 37-0 7/8 V1S 3,056.90 10,868.89 0.00 0.00 1,079.42 2,121.64 29.88 40-2 W2 3,183.39 11,230.30 0.00 0.00 13,886.08 4,098.18 44.21 39-0 7/8 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 1,112.00 2,246.51 26.84 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: i/�/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:36:06 PM NEW MILLENNIUM Location: Joist Description: Mark: BUILMINO SYSTl7A4s PORTLAND,OR Short Span Crimp 28K350/200 TJ4 Chord Properties Chord Area Rx Rz Ryy Y lx Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bending Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 584.54 298.29 447.44 17-61/2 16-0 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 17.00 41.88 24.00 37.13 22.00 1.1250 Bending Load 694.92 642.68 350.00 350.00 350.00 0.5 0..500000 Len 2X: Axial Load 14,016.45 12,513.16 42,621.41 10,868.89 11,230.30 fa Max Load Fillers TC: 4,254.63 6,723.89 22,902.42 5,840.35 3,408.91 49,625.71 Maximum K L/r 43.46 107.04 46.01 94.90 56.24 Max Load no Fillers TC: Fcr 43,551.60 21,633.42 42,829.38 25,881.38 39,677.35 45,547.55 TC OAL/ Fa 26,130.96 12,980.05 25,697.63 15,528.83 23,806.41 Rri' 384.83 F'e 808,645.63 60,577.02 327,847.97 77,069.87 482,848.31 BCOAL/Ryy: Cm 0.9974 0.9445 0.9532 0.9621 0.9965 389.41 Panel Point Moment 9284.12 10310.37 2644.44 4809.62 7462.72 BC Stress: Mid Panel Moment 740.27 6538.12 1750.00 3804.63 4379.96 1.00 Panel Point fb 4576.99 21035.77 5395.34 9812.85 3679.06 BC L/Rz: 121.8893 Mid Panel fb 323.06 5595.18 1497.61 3255.92 2159.29 FillersTC Shear Stress: 0 0 0 0 0 12,028.26 Panel Point Stress 8,831.62 27,759.66 28,297.76 15,653.20 7,087.97 BC Shear Stress: Mid Panel Stress 0.0922 0.7102 0.9391 0.48240.1442 15,840.42 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 18,486.92 26,972.16 3,611.09 9,598.50 3.59 x 0.245 1 R112=round 1 1/8 W3 2,957.84 28,624.38 11,621.28 12,786.97 4.17 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 W4 9,362.47 10,742.43 2,599.09 5,330.90 4.89 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 2,039.65 18,714.09 7,757.04 8,898.52 2.97 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 6,818.00 7,826.93 1,658.88 3,564.90 4.50 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W7 1,377.17 14,381.54 5,750.43 6,928.23 2.58 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 4,811.39 5,758.64 1,095.46 2,157.24 3.60 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W9 848.07 8,984.69 4,143.51 4,326.22 2.36 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 4,143.51 4,802.89 848.07 1,636.66 3.62 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 4,143.51 8,984.69 4,143.51 4,326.22 2.36 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W11 4,143.51 8,984.69 4,143.51 4,326.22 2.36 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 4,143.51 4,802.89 848.07 1,636.66 3.62 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 848.07 8,984.69 4,143.51 4,326.22 2.36 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 4,811.39 5,758.64 1,095.46 2,157.24 3.60 x 0.090 1 C12BB= 1.125 x 0.799 x.090 W7 1,377.17 14,381.54 5,750.43 6,928.23 2.58 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 6,818.00 7,826.93 1,658.88 3,564.90 4.50 x 0.102 1 C16BB= 1.125 x 1.025 x.102 W5 2,039.65 18,714.09 7,757.04 8,898.52 2.97 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W4 9,362.47 10,742.43 2,599.09 5,330.90 4.89 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 2,957.84 28,624.38 11,621.28 12,786.97 4.17 x 0.188 1 C4OBA= 1.125 x 2.014 x.218 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: �/ 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:36:06 PM NEW MILLENNIUM Location: Joist Description: Mark: RIM rum"; SY9TF..M9 PORTLAND,OR Short Span Crimp 28K350/200 TJ4 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 13,886.08 21,311.81 4,098.18 5,940.88 2.87 x 0.230 1 R100=round 1 V1 1,079.42 8,984.69 4,269.95 4,744.79 2.44 x 0.118 1 C18BB= 1.125 x 1.035 x.118 V2 1,112.00 4,802.89 2,246.51 2,577.11 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 G, Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 1:36:06 PM NEW MILLENNIUM Location: Joist Description: Mark: RUM.niNr.. SYSTERAS PORTLAND,OR Short Span Crimp 28K350/200 TJ4 TCX Design TCX Left TCX Right TCX Length 0-0 7/8 TCX Length 0-6 1/8 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-0 3/4 BPL Length 2-10 1/2 Clear Bearing 0-4 7/8 Clear Bearing 0-10 1/4 BPL Material:2018=2 X 2 X.188 BPL Material: 2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.01 Reqd TL Def L/80 0.08 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.01 Reqd LL Def L/120 0.05 Section Modulus 2.0284 Section Modulus 2.0284 Reqd SM 0.0040 Reqd SM 0.2488 Mom of Inertia 2.6899 Mom of Inertia 2.6899 Reqd MI 0.0002 Reqd MI 0.0540 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) \, / -‘,„x'N 'N Concentrated Loads Conc @ 0-6 1/8 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b: SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a: 0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM - Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM Case Gc: DL+CL--0.85(f L)+W L.0*AX+IN STRESS ANALYSIS- PAGE 1 �,/'� Job Number: Job Name: Date Run: �/� 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:44:18 PM NEW MILLENNIUM Location: Joist Description: Mark: euiLoInic SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 TJ8 Geometry Base Length: Working Length: Joist Depth: Effective Depth: (BC Panel Length: Shape: 46-7 46-3 30.00 28.84 10 @ 4-0 Parallel Chords Variable Left End Right End BC Panel 3-3 7/8 3-3 1/8 QIIIllWill I_I I I I TC Panel 1-6 7/8 1-6 1/8 � �• First Half 2-0 2-0 First Diag. 5-3 7/8 5-3 1/8 Depth 30.00 30.00 Loads Load Type Category Load1 Load2 Position Direction Loc/Begin Sp/End Reference Uniform (plf) DL(1) 150.00 150.00 TC + 0-0 46-7 L-BL Uniform (plf) LL(1) 200.00 200.00 TC + 0-0 46-7 L-BL Conc anywhere (lbs) CL(1) 350.00 0.00 TC + Uniform (plf) SM (1) 16.00 16.00 TC + 0-0 46-7 L-BL Axial (lbs) SM(1) 1,700.00 0.00 TC + 0-0 0-0 L-BL Axial (lbs) WL(1) 2,200.00 0.00 TC + 0-0 0-0 L-BL Conc anywhere(lbs) CL(1) 300.00 0.00 BC + Conc @ any pp (lbs) CL(1) 350.00 0.00 TC + Gross Uplift(plf) WL(2) 41.00 41.00 TC - 0-0 46-7 L-BL Stress Analysis Summary Int.Panel TC: Max Panel BC: Reaction LE: Reaction RE: Minimum Shear: Max TC Comp.: Max BC Tension 24.00 48.00 9,098.73 9,088.34 2,274.68 43,744.15 43,056.95 Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W2 1,477.67 11,140.60 0.00 0.00 14,586.80 1,857.28 47.61 0-2 V1S 1,130.34 10,577.41 0.00 0.00 1,431.47 2,404.77 35.68 1-6 7/8 W3 1,130.34 10,577.41 16,501.76 1,807.40 1,061.80 10,217.42 37.52 3-3 7/8 W4 2,386.37 21,860.27 16,501.76 1,807.40 8,908.32 908.45 37.52 5-3 7/8 W5 2,386.37 21,860.27 26,636.23 2,897.10 801.77 7,885.12 37.52 7-3 7/8 W6 3,339.58 30,829.67 26,636.23 2,897.10 6,974.44 695.09 37.52 9-3 7/8 W7 3,339.58 30,829.67 34,440.57 3,713.83 588.41 5,951.24 37.52 11-3 7/8 W8 4,019.84 37,468.95 34,440.57 3,713.83 5,040.56 481.73 37.52 13-3 7/8 W9 4,019.84 37,468.95 39,914.80 4,257.62 375.05 4,017.36 37.52 15-3 7/8 W10 4,427.15 41,778.11 39,914.80 4,257.62 3,106.68 308.37 37.52 17-3 7/8 W11 4,427.15 41,778.11 43,056.95 4,528.44 308.37 2,959.30 37.52 19-3 7/8 W12 4,561.49 43,744.15 43,056.95 4,528.44 2,959.30 408.70 37.52 21-3 7/8 W12 4,561.49 43,744.15 43,027.70 4,526.31 2,959.30 408.70 37.52 23-3 7/8 W11 4,422.88 41,728.70 43,027.70 4,526.31 308.37 2,959.30 37.52 25-3 7/8 W10 4,422.88 41,728.70 39,847.19 4,251.22 3,106.68 308.37 37.52 27-3 7/8 W9 4,011.31 37,383.13 39,847.19 4,251.22 375.05 4,017.36 37.52 29-3 7/8 W8 4,011.31 37,383.13 34,336.55 3,703.17 5,040.56 481.73 37.52 31-3 7/8 W7 3,326.79 30,707.44 34,336.55 3,703.17 588.41 5,951.24 37.52 33-3 7/8 W6 3,326.79 30,707.44 26,495.79 2,882.17 6,974.44 695.09 37.52 35-3 7/8 W5 2,369.31 21,701.62 26,495.79 2,882.17 801.77 7,885.12 37.52 37-3 7/8 W4 2,369.31 21,701.62 16,324.92 1,788.21 8,908.32 908.45 37.52 39-3 7/8 *Continued on Next Page... STRESS ANALYSIS- PAGE 1 0 Job Number: Job Name: Date Run. 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:44:18 PM NEW MILLENNIUM Location: Joist Description: Mark: ei.���.ninir.. RYSTEras PORTLAND,OR Short Span Crimp 30K350/200 TJ8 Stress Analysis Summary,Continued... Member TC Tension TC Compresion BC Tension BC Compresion Web Tension Web Comp. Web Length PP Dist. W3 1,109.01 10,408.37 16,324.92 1,788.21 1,061.80 10,217.42 37.52 41-3 7/8 V1S 1,109.01 10,408.37 0.00 0.00 1,431.47 2,404.77 35.68 45-0 7/8 W2 1,185.05 10,964.74 0.00 0.00 14,431.26 1,500.60 47.01 43-3 7/8 Standard Verticals Member Position Max Tension Max Comp. Length V2 Interior 700.00 1,894.70 28.84 STRESS ANALYSIS- PAGE 2 0 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 1:44:18 PM NEW MILLENNIUM Location: Joist Description: Mark: ElulLniNn 9YSTENAS PORTLAND,OR Short Span Crimp 30K350/200 TJ8 Chord Properties Chord Area Fix Rz Ryy Y Ix Q Material TC 0.9305 0.6092 0.3912 1.3045 0.5910 0.3453 1.0000 2024=2 x 2 x.248 BC 0.7167 0.6172 0.3938 1.2891 0.5693 0.2730 1.0000 2018=2 X 2 X.188 Axial and Bendin Analysis K: Fy: Fb: Mom of Inertia: LL 360: LL 240: Max Bridg TC: Max Bridg BC: 0.75 50,000.00 30,000.00 674.71 254.79 382.18 17-71/2 24-113/8 Top Chord Check End Panel LE First Panel LE Interior Panel First Panel RE End Panel RE Gap Between Chords: Length 16.88 45.00 24.00 45.00 16.13 1.1250 Min Weld Len 2X: Bending Load 350.00 350.00 350.00 350.00 350.00 0.5000 Axial Load 11,140.60 10,577.41 43,744.15 10,408.37 10,964.74 Max Load Fillers TC: fa 3,381.68 5,683.73 23,505.72 5,592.89 3,328.30 49,625.71 Maximum K L/r 43.14 115.03 46.01 115.03 41.22 Max Load no Fillers TC: Fcr 43,639.80 18,970.12 42,829.38 18,970.12 44,158.89 45,547.55 TC OAU Fa 26,183.88 11,382.07 25,697.63 11,382.07 26,495.34 4225.465.46Ryy: F'e 820,669.88 52,455.68 327,847.97 52,455.68 898,786.69 BC OAURyy: Cm 0.9979 0.9458 0.9520 0.9467 0.9981 430.52 Panel Point Moment 8916.13 6984.13 2644.44 7450.52 6203.30 BC Stress: Mid Panel Moment 6601.07 5071.17 1750.00 4917.99 527.16 1.00 BCUPanel Point fb 4395.58 14249.41 5395.34 15200.97 3058.18 121.88 88 1293 Mid Panel fb 3254.27 4339.79 1497.61 4208.71 230.06 TC Shear Stress: Fillers 0 0 0 0 0 9,438.04 Panel Point Stress 7,777.26 19,933.13 28,901.06 20,793.86 6,386.47 BC Shear Stress: Mid Panel Stress 0.1736 0.64781 0.9627 0.6350 0.0705 12,428.87 Web Design Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W2 14,586.80 21,311.81 1,857.28 5,122.69 3.02 x 0.230 1 R100= round 1 W3 1,061.80 24,373.24 10,217.42 10,655.20 3.67 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W4 8,908.32 10,742.43 908.45 5,135.76 4.65 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W5 801.77 18,714.09 7,885.12 8,561.94 3.02 x 0.176 1 C34AA= 1.125 x 1.549 x.176 W6 6,974.44 8,984.69 695.09 4,159.61 3.98 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W7 588.41 14,381.54 5,951.24 6,671.28 2.67 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W8 5,040.56 5,758.64 481.73 1,988.17 3.77 x 0.090 1 Cl 2BB= 1.125 x 0.799 x.090 W9 375.05 8,984.69 4,017.36 4,159.61 2.29 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W10 3,106.68 4,802.89 308.37 1,507.19 2.72 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 W11 308.37 7,826.93 2,959.30 3,425.15 2.00 x 0.102 1 Cl 6BB= 1.125 x 1.025 x.102 W12 2,959.30 4,802.89 408.70 1,507.19 2.59 x 0.077 1 Cl OAB= 1.125 x 0.756 x.077 W12 2,959.30 4,802.89 408.70 1,507.19 2.59 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W11 308.37 7,826.93 2,959.30 3,425.15 2.00 x 0.102 1 Cl 6BB= 1.125 x 1.025 x.102 W10 3,106.68 4,802.89 308.37 1,507.19 2.72 x 0.077 1 C10AB= 1.125 x 0.756 x.077 W9 375.05 8,984.69 4,017.36 4,159.61 2.29 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W8 5,040.56 5,758.64 481.73 1,988.17 3.77 x 0.090 1 Cl 2BB= 1.125 x 0.799 x.090 W7 588.41 14,381.54 5,951.24 6,671.28 2.67 x 0.150 1 C28BB= 1.125 x 1.344 x.150 W6 6,974.44 8,984.69 695.09 4,159.61 3.98 x 0.118 1 C18BB= 1.125 x 1.035 x.118 W5 801.77 18,714.09 7,885.12 8,561.94 3.02 x 0.176 1 C34AA= 1.125 x 1.549 x.176 *Continued on Next Page... STRESS ANALYSIS- PAGE 2 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/20191:44:18 PM NEW NI I L L E N NI UN% Location: Joist Description: Mark: wutLninir.. SVSTF..MS PORTLAND,OR Short Span Crimp 30K350/200 TJ8 Web Design,Continued... Member Web Tension Allow Tension Web Comp Allow Comp Weld Qty Material W4 - 8,908.32 10,742.43 908.45 5,135.76 4.65 x 0.129 1 C22BB= 1.125 x 1.110 x.129 W3 1,061.80 24,373.24 10,217.42 10,655.20 3.67 x 0.188 1 C38BA= 1.125 x 1.845 x.199 W2 14,431.26 21,311.81 1,500.60 5,253.08 2.99 x 0.230 1 R100= round 1 V1 1,431.47 7,826.93 2,404.77 3,595.62 2.00 x 0.102 1 C16BB= 1.125 x 1.025 x.102 V2 700.00 4,802.89 1,894.70 2,361.49 2.00 x 0.077 1 C10AB= 1.125 x 0.756 x.077 STRESS ANALYSIS- PAGE 3 Job Number: Job Name: Date Run: 5618-0088 JAGUAR LAND ROVER-SHOPORDERS 1/9/2019 1:44:18 PM NEW NI ILL EN N I UNI Location: Joist Description: Mark: ei.Ju.nmic SYSTEMS PORTLAND,OR Short Span Crimp 30K350/200 TJ8 TCX Design TCX Left TCX Right TCX Length 0-7 1/2 TCX Length 0-1 1/4 TCX Type R, Rnfd. TCX Type R, Rnfd. TCX Depth 2 1/2 TCX Depth 2 1/2 BPL Length 2-7 3/8 BPL Length 2-0 3/8 Clear Bearing 0-11 1/2 Clear Bearing 0-5 1/4 BPL Material:2018=2 X 2 X.188 BPL Material:2018=2 X 2 X.188 Total Load 350.00 Total Load 350.00 Reqd TL Def L/80 0.09 Reqd TL Def L/80 0.02 Live Load 200.00 Live Load 200.00 Reqd LL Def L/120 0.06 Reqd LL Def L/120 0.01 Section Modulus 2.0284 Section Modulus 2.0284 Reqd SM 0.2972 Reqd SM 0.0051 Mom of Inertia 2.6899 Mom of Inertia 2.6899 Reqd MI 0.0750 Reqd MI 0.0003 Seat Type:Lapped(Reinforced) Seat Type:Lapped(Reinforced) C-. < , VA i i' ////// i / NNNN ,, Concentrated Loads Conc @ 0-7 1/2 800.00 Load Combinations Case 1: DL Case 6d: DL+CL+0.85(TL)+WL+C-AX+IP Case 2a: LL Case 6e: DL+CL+0.85(TL)+WL+AX+IP Case 2b:SL Case 6f: DL+CL+0.85(TL)+WL-AX+IP Case 3a: DL+CL+TL+LL Case 6g: DL+CL+0.85(TL)+SM+AX Case 3b: DL+CL+TL+SL Case 6h: DL+CL+0.85(TL)+SM-AX • Case 3c: DL+CL+TL+LL+FEM Case 7a: DL+CL+0.85(TL)+0.75(WL+AX+LL) Case 3d: DL+CL+TL+SL+FEM Case 7b: DL+CL+0.85(TL)+0.75(WL-AX+LL) Case 3e: DL+CL+TL+LL Case 7c: DL+CL+0.85(TL)+0.75(WL+C+AX+LL+IP) Case 3f: DL+CL+TL+SL Case 7d: DL+CL+0.85(TL)+0.75(WL+C-AX+LL+IP) Case 4a: DL+WL+AX Case 7e: DL+CL+0.85(TL)+0.75(WL+AX+LL+IP) Case 4b: DL+WL-AX Case 7f: DL+CL+0.85(TL)+0.75(WL-AX+LL+IP) Case 4c: DL+WL+AX+IP Case 7g: DL+CL+0.85(TL)+0.75(SM+AX+LL) Case 4d: DL+WL-AX+IP Case 7h: DL+CL+0.85(TL)+0.75(SM-AX+LL) Case 4e: DL+SM+AX Case 8a: DL+CL+0.85(TL)+0.75(WL+AX+SL) Case 4f: DL+SM-AX Case 8b: DL+CL+0.85(TL)+0.75(WL-AX+SL) Case 5a:0.6(DL)+WL+AX Case 8c: DL+CL+0.85(TL)+0.75(WL+C+AX+SL+IP) Case 5b:0.6(DL)+WL-AX Case 8d: DL+CL+0.85(TL)+0.75(WL+C-AX+SL+IP) Case 5c:0.6(DL)+WL+AX+IP Case 8e: DL+CL+0.85(TL)+0.75(WL+AX+SL+IP) Case 5d:0.6(DL)+WL-AX+IP Case 8f: DL+CL+0.85(TL)+0.75(WL-AX+SL+IP) Case 5e:0.6(DL)+WL+AX+SM Case 8g: DL+CL+0.85(TL)+0.75(WL+AX+SL+SM) Case 5f: 0.6(DL)+WL-AX+SM Case 8h: DL+CL+0.85(TL)+0.75(WL-AX+SL+SM) Case 6a: DL+CL+0.85(TL)+WL+AX - Case 9a: 1.2(DL)+0.5(LL)+0.8(TL)+SM+AX+FEM Case 6b: DL+CL+0.85(TL)+WL-AX Case 9b: 1.2(DL)+0.5(LL)+0.8(TL)+SM-AX+FEM FOR OFFICE USE ONLY-SITE ADDRESS: This form is recognized by most building departments in the Tri-County area for transmitting information. Please complete this form when submitting information for plan review responses and revisions. This form and the information it provides helps the review process and response to your project. City of Tigard • COMMUNITY DEVELOPMENT DEPARTMENT N . Transmittal Letter T I G A R D 13125 SW Hall Blvd. • Tigard, Oregon 97223 • 503.718.2439 • www.tigard-or.gov TO: )044 i71-0C-1-171;TE2 DATE RECEIVED: DEPT: BUILDING DIVISION R EC VED FROM: 3-t-A2-2-► sE ( S- r---14 MAY I 2039 COMPANY: ?r C o 5;.Iz-Lk---7-1 vLJ c'_ .- 2- 4 /25 g La:I(-; �6 , PHONE: (CO3) gy:` I RE: ICE 2-3- 5‘k1 WPCs(-15O. IZ . L.)? 20/o _. ( t�l6 (Site Address) (Permit Number) A u 17_, L 1 ?`11� 2-oV"E i2 j+— 1 1\7 b (Project name or subdivision name and lot number) ATTACHED ARE THE FOLLOWING ITEMS: Copies: Description: C;' 'es. Description: Additional set(s) of plans. .r �U Revisions: Cross section(s)and details. Wall bracing and/or lateral analysis. Floor/roof framing. \� Basement and retaining walls. Beam calculations. Engineer's calculations. Other(explain): t-E 2 �� 5v,�r✓! 'tt P REMARKS: (i ) 1��i= 'i-' 4- ("10-E--I> s r s,—S r- (L> ,e j b,Z Ai1/5 C2) ?Le sr-e&-z_ T 5/ <i Com,t be-72be-72 CALC-A.A., io r(S FOR OFFICE USE ONLY Routed to Permit Tech ian: Date: , Initials: Fees Due Yes No Fee Description: Amount Due: 'L 1-) P) r $ __ Special Instructions: Reprint Permit(per PE): ❑ Yes No ❑ Done Applicant Notified: T ;,,, Date: 1;5-/. Initials: / "'"; I:\Building\Forms\TransmittalLetter-Revisions.doc 05/25/2012