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111111 . I -\tic. To c011CV-- <br /> Hiiti PROFIS Engineering 3.0.40 <br /> hilti.corn <br /> ompany: Page' 1 <br /> Address Specifier <br /> Phone I Fax: G E-Mail: <br /> Design: 45-767 Date: 4/5/2019 <br /> Fastening point: <br /> Speci ier's comments: <br /> 1 Input data <br /> Anchor type and diameter: Kwik Boit TZ-CS 5/8(4) ., <br /> item number not available <br /> Effective embedment depth he.,=4.000 in., h =4 438 in, <br /> Material: Carbon Steel <br /> Evaluation Service Report. ESR-1917 <br /> Issued I Valid: 4/1/2018 15/1/2019 <br /> Proof: Design Method ACI 318-14/Mech. <br /> Stand-off installation: eb=0 000 in.(no stand-off):t;0.250 in. <br /> Anchor platen: I.x I.x t=3.000 in x 2.063 in.x 0.250 in.;(Recommended plate thickness:not calculated) <br /> Profile: no profile '-) &cr.u'-\ /1/43o e- `' 1v r On 4to-cA <br /> Base material- cracked concrete,4000,fc'=4,000 psi;h=8.000 in. 1510 ` 3.00 <br /> r % Mf7• Fail 6(AA <br /> • <br /> Reinforcement:Installation: hammer drilled hole,Installation condition:Dry <br /> tension:condition B,shear condition B;no supplemental splitting reinforcement present <br /> edge reinforcement:none or<No.4 bar <br /> Seismic loads(cat.C,D,E,or F) Tension load:yes(17.2.3.4.3(d)) <br /> Shear load:yes(17.2.3.5.3(c)) <br /> n- The anchor calculation is based on a rigid anchor plate assumption. <br /> Geometry[in.]&Loading[lb,'nib] <br /> R <br /> r <br /> rs" lJ <br /> r i. <br /> Y <br /> \ 61,3 <br /> 11111 x <br /> N <br /> Input date end es Ai <br /> muff be cf•ecked for conformity with the axLsUn t conditions and for plaus bdliyl <br /> PROFIS Engineering(c)2003.2009 Hith AG.FL-9494 Sdraan Ktis a registered Trademark of MS AG,Schaan <br /> 04/05/19 Boeing Flightline Stall 113 Page 113 <br />