Laserfiche WebLink
project Boeing NIL 737 Engine by MAZ <br />lqpff <br />location Everett, WA date02/07/2024 <br />client Boeing <br />3C+Oi Stll AVl'1lUC Suitr ifi[1!) <br />5 VfG, WA 99101 206 6z2-;8zz Fp <br />SEISMIC DEMAND FOR NONSTRUCTURAL COMPONENTS <br />Calculations are based upon IBC 2018 and ASCE 7-16, unless noted otherwise. <br />SEISMIC DEMAND (ASCE 7-16 Ch. 13) Code Check <br />Design Spectral Acceleration (Short Period) SIDS = 0.924 g Eq. 11.4-3 <br />sheet no <br />job ms <br />2300208 <br />Component Importance Factor <br />Ip = <br />1.0 <br />Section 13.1.3 <br />Amplification Factor <br />ap = <br />1 <br />Table 13.5-1, 13.6-1 <br />Response Modification Factor <br />Rp a = <br />1 1/2 <br />Table 13.5-1, 13.6-1 <br />Overstrength Factor <br />Qo3= <br />2 <br />Table 13.5-1, 13.6-1 <br />Average Roof Height <br />h = <br />112 ft <br />Height at Point of Attachment <br />z s = <br />20 ft <br />Horizontal Seismic Design Force <br />Fp = <br />0.34Wp <br />Eq. 13.3-1, 13.3-2, 13.3-3 <br />Seismic Design Uplift <br />0.2*Sd5*Wp = <br />0.18Wp <br />Section 13.3-1 <br />NOTES: <br />1. Fp is calculated as a function of component weight, Wp. <br />2. Fp acts as a horizontal force at component center of mass. <br />3. Values of DO are provided for engineer reference only. DO is not included in the tabulated values and must be <br />used when required by code for nonductile anchors. <br />4. Rp shall be limited to a maximum of 6 for anchorage, per section 13.4.1. <br />5. Value of z/h need not exceed 1.0 per section 13.3.1.1. <br />A04 <br />