200 W MARINE VIEW DR ON TRAC LOGISTICS 2025-09-16

LAI AS SHUTLER CONSULTING ENGINEERS, INC. Job Name : Baywood Industrial Structural Engineers Job No. : 20-33 12503 Bel-Red Road, Suite 100 Engr: : CT Bellevue, washington 98005 Date: : 10-20-2020 (425) 450-4075 Sheet No.: Description: Panel 73 - 62" leg Page 2 4 Number 5 Bars Results shown are for 62.00 inch wide section. CASE 1 @ Roof, U = 1.4D ( M = P*e -- No P * Deflection. ) Service Load = 1.0D Service Defl. = N.A. in. Mu 8.24 in-k Ultimate Defl.= N.A. in. Phi * Mn = 333.66 in-k CASE 1 @ Mid-ht., U = 1.4D ( M = .5*P*e + P * Deflection. ) Service Load = 1.0D Service Defl. = 0.01 in. Mu = 5.48 in-k Ultimate Defl.= 0.09 in. Phi * Mn = 365.02 in-k CASE 2 @ Roof, U = 1.2D + 1.6 (Lr or S or R) + 1.0L (M=P*e, No P*Delta) Service Load = 1.0D + 1.0(Lr or S or R) Service Defl. = N.A. in. Mu = 22.78 in-k Ultimate Defl.= N.A. in. Phi * Mn = 353.65 in-k CASE 2 @ Mid-ht, U = 1.2D + 1.6(Lx or S or R) + 1.0L (M=.5*P*e + P*Delta.) Service Load = 1.OD + 1.0(Lr or S or R) Service Defl. = 0.01 in. Mu = 16.88 in-k Ultimate Defl.= 0.26 in. Phi * Mn = 380.44 in-k CASE 3 U = 1.2D + 1.6 ( Lr or S or R ) + 0.5W Service load = 1.OD + 0.75L + 0.75*0.6W + 0.75(Lr or S or R) Service Defl. = 0.19 in. Mu = 172.83 in-k Ultimate Defl.= 2.66 in. Phi * Mn = 380.44 in-k CASE 4 U = 1.2D + 1.0W + 1.01, + 0.5 (Lr or S or R) Service load = 1.0D + 0.75L + 0.75*0.6W + 0.75(Lr or S or R) Service Defl. = 0.19 in. Mu = 288.89 in-k Ultimate Defl.= 4.60 in. Phi * Mn = 365.67 in-k CASE 5 U = (1.2 + 0.2 Sds)D + 1.0E + 1.0L + 0.2S Service load = (1.0 + 0.1 Sds)D + 0.75L + 0.525E + 0.75(Lr or S or R) Service Defl. = 0.23 in. Mu = 296.62 in-k Ultimate Defl.= 4.71 in. Phi * Mn = 366.71 in-k CASE 6 U = 1.2D + l.OW Service load = 1.0D + 0.6W Service Defl. = 0.24 in. Mu = 272.60 in-k Ultimate Defl.= 4.41 in. Phi * Mn = 358.94 in-k CASE 7 U = (1.2 + 0.2 Sds)D + 1.0E Service load = (1 + 0.14Sds)D + 0.7E Service Defl. = 0.36 in. Mu = 289.85 in-k Ultimate Defl.= 4.63 in. Phi * Mn = 364.02 in-k CASE 8 U = 0.9D + 1.0W Service load = 0.6D + 0.6W Service Defl. = 0.24 in. Mu = 255.24 in-k Ultimate Defl.= 4.23 in. Phi * Mn = 349.80 in-k CASE 9 U = (0.9 - 0.2 Sds)D + 1.0E Service load = (0.6 - 0.14 Sds)D + 0.7E Service Defl. = 0.28 in. Mu = 252.10 in-k _ Ultimate Defl.- 4.23 in. Phi * Mn = 344.70 in-k