Laserfiche WebLink
Check Top Chord of Existing Truss <br />Dec. 7, 2022 14:22 <br />Design Check Calculation Sheet <br />WoodWorks Sizer 2019 (Update 4) <br />Loads: <br />Load Type Distribution Pat- Location [ft] Magnitude Unit <br /> tern Start End Start End <br />Roof-DL Dead Full Area No 10.00(24.0") psf <br />Roof-LLR Roof constr. Full Area Yes 20.00(24.0") psf <br />PV1 Dead Point No 1.00 32 lbs <br />PV2 Dead Point No 6.00 32 lbs <br />PV3 Dead Point No 7.50 32 lbs <br />PV4 Dead Point No 12.50 32 lbs <br />Self-weight Dead Full UDL No 1.2 plf <br />Maximum Reactions (lbs) and Bearing Lengths (in) : <br />1.5' 8.5' <br />16.74' <br />15.5' <br />Unfactored: <br /> Dead 145 262 76 <br /> Roof Live 192 340 127 <br />Factored: <br /> Total 337 602 204 <br />Bearing: <br /> Length 0.50* 0.51 0.50* <br /> Min req'd 0.50* 0.51** 0.50* <br />*Minimum bearing length setting used: 1/2" for end supports and 1/2" for interior supports <br />**Minimum bearing length governed by the required width of the supporting member. <br /> Lumber-soft, D.Fir-L, No.2, 2x4 (1-1/2"x3-1/2") <br />Supports: All - Timber-soft Beam, D.Fir-L No.2 <br />Roof joist spaced at 24.0" c/c; Total length: 16.88'; Clear span(horz): 1.5', 6.938', 6.938'; Volume = 0.6 cu.ft.; Slope: 22.0 deg <br />Lateral support: top = continuous, bottom = 2'-0 (in); Repetitive factor: applied where permitted (refer to online help); <br />This section PASSES the design code check. <br />Analysis vs. Allowable Stress and Deflection using NDS 2018 : <br /> Criterion Analysis Value Design Value Unit Analysis/Design <br /> Shear fv = 81 Fv' = 225 psi fv/Fv' = 0.36 <br /> Bending(+) fb = 1199 Fb' = 1941 psi fb/Fb' = 0.62 <br /> Bending(-) fb = 1678 Fb' = 1916 psi fb/Fb' = 0.88 <br />Deflection: <br /> Interior Dead 0.09 = L/991 <br /> Live 0.21 = L/423 0.50 = L/180 in 0.42 <br /> Total 0.31 = L/297 0.75 = L/120 in 0.40 <br /> Cantil. Dead -0.04 = L/456 <br /> Live -0.15 = L/128 0.22 = L/90 in 0.70 <br /> Total -0.19 = L/100 0.32 = L/60 in 0.60 <br />5024 1%2 W 6th St <br />01/23/23