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200 W MARINE VIEW DR ON TRAC LOGISTICS 2025-09-16
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200 W MARINE VIEW DR ON TRAC LOGISTICS 2025-09-16
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9/16/2025 8:53:18 AM
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5/30/2025 2:26:43 PM
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Address Document
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W MARINE VIEW DR
Street Number
200
Tenant Name
ON TRAC LOGISTICS
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SHUTLER CONSULTING ENGINEERS, INC. Job Name : Baywood Industrial <br /> Structural Engineers Job No. : 20-33 <br /> 12503 Bel-Red Road, Suite 100 Engr: : CT <br /> Bellevue, washington 98005 Date: : 10-20-2020 <br /> (425) 450-4075 Sheet No.: <br /> Description: Panel 95 - 26" leg Page 2 <br /> 5 Number 7 Bars <br /> Results shown are for 26,00 inch wide section. <br /> CASE 1 @ Roof, U = 1.4D ( M = P*e -- No P * Deflection. ) <br /> Service Load = 1.0D <br /> Service Defl. = N.A. in. Mu = 11.14 in-k <br /> Ultimate Defl.= N.A. in. Phi * Mn = 996.00 in-k <br /> CASE 1 @ Mid-ht., U = 1.4D ( M = .5*P*e + P * Deflection. ) <br /> Service Load - 1.OD <br /> Service Defl. = 0.01 in. Mu = 7.27 in-k <br /> Ultimate Defl.= 0.05 in. Phi * Mn = 1,094.38 in-k <br /> CASE 2 @ Roof, U = 1.2D + 1.6 (Lr or S or R) + 1.0L (M=P*e, No P*Delta) <br /> Service Load = 1.0D + 1.0(Lr or S or R) <br /> is <br /> Service Defi. = N.A. in. Mu = 30.77 in-k <br /> Ultimate Defl.= N.A. in. Phi * Mn = 1,002.43 in-k <br /> CASE 2 @ Mid-ht, U = 1.2D + 1.6(Lx or S or R) + 1.OL (M=.5*P*e + P*Delta.) <br /> Service Load = 1.OD + 1.0(Lr or S or R) <br /> Service Defl. = 0.03 in. Mu = 19.64 in-k <br /> Ultimate Deft.= 0.13 in. Phi * Mn = 1,086.79 in-k <br /> CASE 3 U = 1.2D + 1.6 ( Lr or S or R ) + 0.5W <br /> k Service load = 1.0D + 0.751 + 0.75*0.6W + 0.75(Lr or S or R) <br /> Service Defl. = 0.92 in. Mu = 307.13 in-k <br /> Ultimate Defl.- 2.03 in. Phi * Mn = 1,086.79 in-k <br /> CASE 4 U = 1.2D + 1.0W + 1.0L + 0.5 (Lr or S or R) <br /> Service load = 1.OD + 0.75L + 0.75*0.6W + 0.75(Lr or S or R) <br /> Service Defl. = 0.92 in. Mu = 577.74 in-k <br /> Ultimate Defl.= 3.63 in. Phi * Mn = 1,082.15 in-k <br /> CASE 5 U = (1.2 + 0.2 Sds)D + 1.0E + 1.0L + 0.2S <br /> Service load = (1.0 + 0.1 Sds)D + 0.75L + 0.525E + 0.75(Lr or S or R) <br /> Service Defl. = 1.58 in. Mu = 773.82 in-k <br /> Ultimate Defl.= 5.10 in. Phi * Mn = 1,092.88 in-k <br /> CASE 6 U = 1.2D + 1.OW= <br /> Service load = 1.OD + 0.6W <br /> Service Defl. = 1.29 in. Mu = 570.20 in-k <br /> Ultimate De£l.= 3.78 in. Phi * Mn = 1,080.04 in-k <br /> CASE 7 U = (1.2 + 0.2 Sds)D + 1,0E <br /> Service load = (1 + 0.14Sds)D + 0.7E <br /> Service Defl. = 2.18 in. Mu = 770.23 in-k <br /> Ultimate Defl.= 5.08 in. Phi * Mn = 1,092.04 in-k <br /> CASE 8 U = 0.9D + 1.0W <br /> Service load = 0.6D + 0.6W <br /> Service Defl. = 1,22 in. Mu = 536.11 in-k <br /> Ultimate Defl.= 3.60 in. Phi * Mn = 1,058.38 in-k <br /> CASE 9 U = (0.9 - 0.2 Sds)D + 1.0E <br /> Service load = (0.6 - 0.14 Sds)D + 0.7E <br /> Service Defl. = 2,02 in. Mu = 676.48 in-k <br /> Ultimate Defl.= 4.57 in. Phi * Mn = 1,046.23 in-k <br />
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