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11101111`T11 <br /> Hilti PROFIS Engineering 3.0.40 <br /> Ovww.hlltf.com <br /> Company: Page: 5 <br /> Address: Specifier. <br /> Phone I Fax: I E-Mail: <br /> Design: 45-767 Date: 4/5/2019 <br /> Fastening point: <br /> 4.2 Pryout Strength <br /> V, =kg' [(es.) W ed.N No, ACI 318-14 Eq.(17.5.3.1a) <br /> ¢ Vq, 2 V ACI 318-14 Table 17.3.1.1 <br /> ANc see ACI 318-14,Section 17.4.2.1,Fig.R 17.4.2.1(b) <br /> Atka =9 h;t ACI 318-14 Eq.(17.4.2.1c) <br /> WedN =0.7+0.3ti5ht,51.0 ACI 318-14 Eq.(17.4.2.5b) <br /> W�N =MAX/cam,1.5hE!)s 1.0 ACI 318-14 Eq.(17.4.2.7b) <br /> ttlu Cu I <br /> Ne =kc X e Ytc h;‘" ACI 318-14 Eq.(17.4.2.2a) <br /> Variables <br /> kw her M-]. c„.Mn[in.] W 0, <br /> 2 4.000 12.000 1.000 <br /> c«[in.] i4 X a fc[psi] <br /> 6.750 17 1.000 4,000 <br /> faCalculations <br /> Aa[In.2] W ed.N Wcp.N Ny[lb] <br /> 144.00 144.00 1.000 - 1.000 8,601 <br /> Results <br /> V$nb] ¢canna +selvrk +rianducal• 4 V�[ib] Vt.[lb] <br /> 17,203 0.700 1,000 1.000 12,042 2,960 <br /> • <br /> Input data and results must be checked for confomdry with the existing condWons and for plausibility! <br /> PROFS Engineering(c)2003-2009 MtU AG,FL-9494 Schwan $HU is a registered Trademark of HiIU AG,Schwan <br /> 04/05/19 Boeing Flightline Stall 113 Page 117 <br />