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B16-1287 040-310-093
CRANDALL ENGINEERING LJ 5448 Merrill Mill Road Mariposa, CA 95338 Phone: 209-966-4844 SHEET OF JOB NO. I C—dp�I.- g2- /I DATE: z;:,/ / I L4. v oLn tO I "T; =4;1- :I-- epoi Lp s� It-, 0410 Ic / I�rrc- (;"::, Ib - I I N1 }.1 c _I- - ft -; I c— BUTrE COUNTY SEP.,O 2 2016 DEVELOPMENT SERVICES plan N�J.( c 1c) p Z)ro V:: i L, 1,::: - (f. > 802016 ) Design Maps Summary Report �l � S Design Maps Summary Report User -Specified Input Report Title Smuckers Electrical Room Tue August 2, 2016 17:47:22 UTC Building Code Reference Document ASCE 7-10 Standard (which utilizes USGS hazard data available in 2008) Site Coordinates 39.7060N, 121.8015°W Site Soil Classification Site Class D - "Stiff Soil" Risk Category I/II/III USGS-Provided Output Ss = 0.614 g SMs =. 0.803 g SDs = 0.536 g S1 = 0.272 g S,, = 0.504 g SDI = 0.336 g For information on how the SS and S1 values above have been calculated from probabilistic (risk -targeted) and deterministic ground motions in the direction of maximum horizontal response, please return to the application and select the "2009 NEHRV building code reference document. r MCE,R Response Spectrum ,Design Response Spectrum 0.90 + 0.81 0.54-- 0.72-- 0.43 0.63 0.42-- .054 0.36 Im CN 0'15 A .0.30 0.35 fA 0.24- 0.27, 0.12 0.09 0.06 0.00 - 0.00 0.00 0.20 040"0.60 .0.80 1.00 1.20 1.40 1.G0 1.90 2.00 0.00 0.20 0.40 0.50 0.90 1.00.1.20 1.40 1.60 1.80 2.60 - Period, T (sec) Period, T (sec) For PGA, T, CRS, and CR, values, please view the detailed report. Although this information is a product of the. U.S. Geological Survey, we provide no warranty, expressed or implied, as to the r accuracy of the data contained therein. This tool is not a substitute for technical subject -matter knowledge. http://ehp2-earthquake.wr.usgs.gov/designhiaps/us/sum mary.php?tem plate=mini mal&latitude=39.706&longitude=-121.8015&siteclass=3&riskcategory=0&ediba .. 1/1 I mat; r -A.- , 4 = I ss y CRANDALL ENGINEERING SHEET OF L -1i 5448 Merrill Mill Road JOB NO. Mariposa, CA 95338 Phone: 209-966-4844 DATE: I mat; r -A.- , 4 = I ss y Structural (S) Stud Section Properties _0 RON !RF"Z1.11 o 0 55 tAr uI 600S737-33 0.0346 33 0.464 1.548 0.455 8.98 8:19 638 638 0.127 0.500 .0.807 0.519 2.416 0.889 33.5 600SI37-43 0.0451 i.Af 21.042. . 0.681 2223 0.0.87 OAS 2.041 .0.645, .12.74 ..11.82 1416 . -1240 O,2:Bd 6.�13 - b .990 33.3', 5137-54 0.0566 33 0.574 1.75 2.518 0.839 2.213 0.105 0.452 2.518 0.832 16.44 46,95 2739 1890 0.549 0.769 .0.784 0.506 2.3911 0.893 33.0 600513744 0.0566- 50 _05 14 Mil. -'12_13' 0J6 OA52-" ,i.M- IJ.M 2316r_xo2124' 2823 .1947,•'0.546 :6766 4784:- 6M6 .INI 6'8§3 26.8 6005137-68 0.0713 33 0.640 2.18 3.094 1.031 2.i6Y OA25 0.443 3.094 1.031 24.05' 24.05 4347 2339 1.054 0.930 -0.768 OA97• 2.371 0.895 30.1 -60GS1370 0.0713- . 5T 0.640 i'l 8 3.094. . -031 , 2 .?00 .0 �125 .0.443 . I ':3-.OJU- - f.0-30:, 36��,� �JII.'89 - .. I _. . . SM � 28 79 1.6 Upp'. A368, 0.497, '2M.: - .. . _ - 019 , 15 26.5 6005137-97 0.1017 33 0.889 3.03 4.188 1.396 2A70 0.159 OA22 4.188 1.396 34.48, 34.49 6911 2512 3.066 1.216 -0.734 0.480 2.330 0.901 28.8 .600SI37-'97 'k� 0186 .03'. A.tp-- .4.,170, 4,459`e- OAU 4:188'..1:396 50.80'': .50:80:, 10472 3865 .3:066 q'A-8_0_ -.2-.33-0 ...23.6 600S162-33 0.0346 33 0.344 1.17 1.793 0.598 2.282 0.116 0.581 1.793 0.577 11.41 9.47 638 638 0.137 0.861 .1.072 0.677 2.587 0.68 41.1 60=62-43 0.0451 33 O:47 152 • 2.316 �O.T'h 2:276.* 0.1 48 .0.576 2.316:. . 0;767 16.68 14'.46 1416 . 1 1 1 2 . 40 0: . 303 . U95 . . .062. -1-0.670 1577 0 6005162-54 0D566 33 0.556 1.89 2.860 0.953 2.267 6.180 0.570 2.860 0.953 21.171 19.75 2739 1890 0.594 1.337 -1.049 0.663 2.562 0.832 38.4 6005162-54 0.0566 50 0.556 1,89 . 2,860 0.953 2.267 0.1 . 80 0.570 2,860 0.916 30.331 25.90" 2823 1947 0.594 1.337:.-1.049.. 06 .. 63 0.663 -2.562 .0132 t 31.4 600S162-68 0.0713 33 0.693 2.36 3.525 1,175 2.255 0.218 0,560 3.525 1.175 26.791 26.78 4347 2339 1.174 1.626 -1.032 0.655 2.543 0.835 37.7 6ODS162-68 OD713 50 0.693 2.36 3.525 1.175 2.255 0118 0560.'•3525 1.164 39.471 35.69 5350' .2879 1.174 162k., �'.-1:032 2:543. 0"" 30:8 600S162-97 0.1017 33 0.966 3.29 4.797 1.599 2.229 0.283 0,541 4.797 1.599 38.371 38.37 611 2512 3329 2.153 -0.997 0.636 2.501 0.841 36.4 6006167-970.1017 . 50 3.29 -4:797 1:599•: - 2229;_ - 0:283, 0;541 4.797 1599" 56.731 -56.72-', 10472 31305 3.329 .2153 . -0 997",0&l1.`''29.8 0.636: 2:501 600S762-118 0.1242 33 1.158 3.94 5.652 1.8114 2.209 0.321 0.526 5.652 1.884 46.821 46.82 8267 2391 5.956 2.487 -0.971 0.623 2.470 0M5 35.6 6005182-1186:1142' 56 7 3.14 '5.652:-11W_ -2.A•., 0.526 5.652 1.88W _88.40' •69.t -1'1'5i6 ',_36ff '5956",_,2487„»-0.971. .-0:6231.2470"__`_0,845 : '29.1r 6005200-33 0.63416 33 6.379 1.29 2.075 0.692 2.340 0.209 0.743 2.058 0.621 12.28 10.77 638 638 0.151 1.593 -1.457 0.961 2.855 0.740 51.6 6005200-03,,.0.64 `U 492 .'.M,;.I.'67. .1 1 1 ...- I.... . . ...- I _,0 739 _24: Q47�;�_ !j� .1 15:39 :4 033 �:i446 "".. ts. -'��5'1.4, .." 60OS200-54 0.0566 33 0.613 2.09 3.319 1.106 2.327 0.328 0.732 3.319 1.106 24.071 22.07 2739 1890 0.655 2.4m -1.432 0.887 2.829 0.744 ' 48.9 �OOKOD 00566 2.66 -3:319°-._ � - TIO ' ` �.'��7 -`Efi ' 1 .73 - 0 2 J '19' - -i'JD1 -5,' .. . `4U6. J�.i. - ' '`06��_2 2823'. 1947•' - _"*i'_jf ... _..,493. ' a - V 7 •0.746 t 60OS200-68 0.0713 33 0.764 2.60 4.101 667 2.316 0.400 0.723 4.101 U67 3OA2 - 29.97 4347 2339 1.295 3.047 -1.05 0.878 2.809 48.2 66OS200M 0.0713 60."..� 9.764:.047�* .60-, ..4101. 2.316, _-OAOO 0:723, 10 . 1.317 4311' :pj6'.'69 '13W V9 '-..1295.:" " 3 - 415 - '0.878,_:- 2: 809 F :0:746 ' ' - 739.3 60OS200-97 0.1017 33 1.067 363 5.612 1.871 2.293 0.530 0.705 5.612 1.871 43.491 43.49 6911 2512 3.679 4.080 .1.378 0.859 2.76 0.-752 46.9 6005200:97-- 0.1017 50 = 1.067 3.63 5.612 i'.ei' 2.29:4 0.536 5.*612, 1,671 6453 i 63.67 10472 1 3805. . 3:679'�7 - 4 .080. - 07� o: 0.859. "23R' _6.752 .38.3 60OS200-118 0.1242 33 1.283 4;36 6.641 2.214 2..275 0.611 0.690 6.641 2.214 53.05' 63.05 8267 23 91 6.5951 4.75 1 3 -1.35 . 1 0.845 2.735 0.756 46.1 6005200-118 0.1242 50 1.2133 .4,36 6.641 2.214 2.275 0.611 OA90 .'6.641 2.214. 78.40 78'.44 12526 3622 6:595 4.7W 1351 0" -2.735, 0.756, 37.6 6005255043 0.0451 33 0.537 1.83 3.082 1.027 2.396 0.458 0.923 3.62 0.918 18.14 16.21 1416 1240 0.364 3.411 -1.874 1.136 3.179 0.652 62.4 60OS25054 0.0566 33 0.6* 2.28 3.819 1.273 2.3138 0.562 0.917. 3.819 1.159. 22.90 21.90 2739 1890 O.rii5• _4,194.-.-1.960 1.12.9 3:163:0.654' 62.3 60OS250-54 0.0566 50 0.670 2.28 3.819 1.273 2.388 0.562 0.917 3.766 1.069 32.00 28.71 2823 447 0.715 4.194 A.860 1.129 3.163 0.654 50.5 . J00S250-68 0.07.13. 33. 0.11.36 2:84" 4.727. 1:57.6 2:378 0.688 0.908 A.727 1.508 32.827 31'.50- 4347. 2339 'tA16- 5:145- 4.84.2 3:142: 6.6016 .. 59..2 60OS250-68 0.0713 50 0.836 2.84 4.727 1.576 2.378 0.688 0.908 4.723 1.386 41.49 39.07 M 2879 1.416 5.145 -1.542 -1.1.1.9 1.119 3.142 0.656 50.4 0.1017 33 tlM 318 6.496 2_165 2357. 0.923 O'A9 6.'496 2.161 48.8 11 Q .91 6911 I 2512 4. OjO . 947 6:-.. - -.1'.803 1;100 3.098 0.661� 58.0... 6ODS250-97 0.1017 50 1.769168 6.496 2.15 2.357 OM3 0.889 6A96 2.063 6.381 Will 10472 3805 4.030 6.947 -1.803 1.100 3.098 0.661 - 47.3 6606250-118 0.1242 33 MOT" A.79 7313', 2571 2.342 . . 1,.07 . 5 0.874 T 3 71. 2.5711 59SBI 59.59, 8267 2391 7.234 8114 1.685 1 0 A65 57.3, 6005250-118 0.1242 50 1.407 4.79 7.713 2.571 2.342 1.075 0.874 7.713 2.498 85.921 86.83 12526 3622 7.234 8.142 775 1.085 3.066 0.665 46.6 •--60OS30054 0.0566 M- 025 2.47 4,319' 2439. 0.875 1.098- '4269 1.211 2323 2240 2739 1690 0.775' '6.452:- ;-2.299 1:372;'. 6005300-54 0.0566 50 0.726 2.47 4.319 1.440 2.439 0.875 1,098 4.014 1.106 33.13 29.62 2823 1947 0.775 6.452 -2.299 1.372 3.527 0.575 59.1 600530048 0.0713 33- 0.907 3.09 5.354 1".785 2.430 1.075 1.089 5.344 1.581. 31.23 30,88 _ 4347. '233.9. 15.37, .7-937 ,-2:280, 1.383 3.505 AM -72.8 60OS300-68 0.0713 50 0.907 3.09 5.354 1.785 2.430 1.075 1,089 5.221 1.44(i 43.30 46.53 5350 2879 1.537 7.937 -2. 1 280 1.36 .3.5-05- 0.577 5-9.0 600530097 0.1017 33'. 1.271 4.32 7.381.' 2.460 2410 1]454 ID70 7,3812.352' 52.07 kAOI '6911. BfZ' -4.21 11_0.-7.76. -2!241!,•• i _0Sk 66.8, 60OS300-97 0.1017 iO 1.271 4.32 7.381 2.460 2.410 1.454 1.070 7.280 2.247 67.28 64.67 10472 31305 4.381 10.776 -2.241 1.3433.461 0.581 58.8 60OS30011B 0.1242 33 1.531 5.21 8.785 2.928 2395 1.7134 1.055 8;785 2.840 64291. , 6628. 8267 -2391 71972 12.6E3* -2.212. 1,3.28. - 3.427. 0583....' 68.1 600S300-118 0.1242 50 1.531 5.21 8.795 2.928 2.395 1.704 1.055 8.713 2.797 94.241 90.37 12526 3622 7.872 12.683 -2.212 1.328 3.427 0.583 55.3 60OS356,54 0.0566 .33 0.825 2.81 5.022 1.674*. 2.467 1491. 1.344 4.911 1.452 28.70 27.98. 2739 .1890 0.881. 12.942-7.037 ' 1.787 .4.137 0.461 91.8. 6GOS350-54 0.0566 50 0.825 2.81 5.022 1.674 2.467 1.491 1.344 4.721 1.335 39.97 36.56 2823 1947 0.881 . .942 12.942 -3 .037 V87 4.1370.461 74.4 6006350-68 0.0713 33* 1.032 3.51 6.237' 2%(179,' 2.459 1.841 13M 6.237 1'.949 36.50. 4347" 2339 1.748"-i5� :9W 7.018 1'.777 4.05. 0.462 91.8 60OS350-68 0.0713 50 1.032 3.51 6.237 2.079 2.459 1.841 1.336 6.166 1.771 53.01 49.69 6350 2879 1.748 15.968 -3.018 1.777 4.115 0.462 74.4 600Si%97 OJOV 33 "-.1.449I: 4;93'. 8.631 2.877 -:2.441 . 2.518. 1318.. 8.631 .2.822 61:551 62:49 6611: '2 512 4;994 21.8it.. q, 17§7 4�1!71 87.5 6005350-97 0.1017 50 1.449 4.93 8.631 2.877 2.441 2.518 1.318 8:631 2.593 77.64 78.36 10472 3805 4.994. 21.811 -2.979 1.757 4.071 0.464 74.4 60OS350-118 0.1242 33- .1J48 5.95 10.304 3.435, 2.428 2.976 1-105 10:304 .3.435 76291. 76:40 820 .23 . 91 8 . .990- i25; . �§t ' 4.951', 1142 4.038 'OAA: 86.9 6005350118 0.1242 M 1.748 5.95 10.304 3.4353.4352.428 2.978 1.305 10.304 3.268 10841 107.66 12526 3622 8.990 25'.791 -2.951 1.742 4.038 0.466 70.6 8005137-33 0.0346 33 --0.388 132 3,198 0.799 2.873 0.073 0.435. 2.998 0.622' 1230.- 10.71' *474'• 474 0155 UP 4.696 0.460 2.987 :9.946 .32.5 BMS137-43 0.0451 33 0.503 1.711 4.134 1.033 2.866 0.093 0.430 4:001 0.896 17.70 15.78 105.1 1051 6341 1:214 -0.687 0.454 2.978 0.947 32.2 8005137-54 0.0566 33 0.627 2.13 5.110 1.277 2.855 0.112 0.423 5.077 1.179 23.29 .21.74 2091 2091 0.670 1.478 -0.676 ..0.448 2.964-• 0.948. 32.0 BOOS137-54 0.0566 so 0.627 2.13 5.110 1.277 2.855 0.112 0.423 4.974 1.083 32.42 28.47 2091 2091 0.670 1.478 -0.676 0.448 2.964 0.948 25.9 80OS137-68 0.0713 33 0.782 2.66 6.303 1.576 2839 0.434 0414 6.303 1;541 30.45 29.75 4221 3361 1.325 1,789 -0:661 0.440 2.94 0.950. 31.6 8005137-68 0.0713 50 0.782 2.66 6.303 1.576 2.839 0.134 OA14 6.285 1.468 43.96 39.57 4221 3367 1.325 1.789 .0.661 0.440 2.944 0.950 25.6 8005137-97 0.1017 33 1.093 3.72 8.597 2.149 2.805 0.169 0,394 8.597 2.149 53.091 53.09 8843 4824 3.767 2.349 -0.630 OA23 2.902 0.953 27.6 BOOS137-97 0.1017 so 1.093 3.72 8.597 2.149 2.805 0.169 0.394 8.597 2.149 64.35 63.91 10885 5938 3.767 2.349 -0.630 0.423 2.902 0.953 25.0 8COS162-33 0.0346. 33 0.413 1.41 '3.582 0.896 2.943 0.125' 0.550 3.384 0.710 14.03 12.61 474 474 0.165 1.6310 -0.936 0.607 3.137 0.911 40.1 BOOS16243 0.0451 33 0.537 1.83 4.633 1.158 2.937 0.160 0.546 4.500 1.019 20.14 18.33 1051 1051 0.364 2.076 -0.926 0.601 3.128 0.912 39.8 BODS162-54 0.0566 33 0.670. 2.28 5.736 -1 AN 2927 0.194 0.539 5.702 1.334 26.36 24.98 2091. 2091 0.715 2.639 ' 1L914 0.594 3.113- 0:914 39.6 BOGS162-54 0.0566 50 0.670 2.28 5.736 1.434 2.927 0.194 0.539 5.600 1.229 36.79 32.81 2091 2091 0.715 2.539 .0.914 0.594 3.113 0.914 32.1 800S162-68 0.0713 33 OMB 224 7.089, 1771 2.913 0.235 0.530 7.089 1.737 34.32 33.84 4221 3367 1A16 3.093 -0.899 OMB 3.094 0.916 39.3 8005162-68 0.0713 50 0.836 2.84 7.089 1.7'72 2.913 0.235 0,530 7.070, 1.663 49.80 45.111 4221 3367 1.416 3.093 .0.899 0.586 3.094 0.916 31.9 8005162-97 0.1017 33 1.169 3.98 9.713 2.428 2883 0.305 0510 9.71j 2.428 58.271 5817 8843 .4824 4.030 4.114 -.0.866 0568 3,053 0919 35.1 8005162-97 0.1017 50 1.169 3.98 9.70 2.428 2.883 0.305 0.510 9.711 • 2.428 72.70 71.93 108115 5938 4.030 4.114 -0.866 0.568 3.053 0.919 31.4 8006162-118 0.1242 33 1.407 4.79 11.504 2.876 2.860 0.345 OA96 11.504 2.876 71.472 7 ' 1.47 .11341 4971 7.234 '4:766. -0.642 0.556 3.022. U& 34.1 800S162-118 0.1242 50 1.407 4.79 11.504 2.876 2.860 0.345 0.496 11.504 2.876 105.231 105.23 16235 7115 7.234 4.766 -0.842 0.556 3.022 0.922 28.0' 80OS200-33 1 0.0346 33 0.448 1.52 4.095 1.024 3.023 0.227 0.712 4.096, 0.816 16:12, 1452 474* 474 0'.179 2.971-.� -1188- 0.817 3.363 *0.853 50.6' 8005200-43 0.0451 33 0.582 1.98 5.302 1.325 3.018 .0.292 0.708 5.302 1.293 25.54 20.99 1051 1051 0.395 3.797 .1.277 0.811 3.353 0.855 so BMS20054 0.0566 33 0.726 2,47 .6M 1.643 3.009 0.351.. 0.701. -6.573 1.643: .* 35.751 30.37 ..2091 2091 0.775 4.663 •'-1.265 0.804: 1338 0.956 47 BOOS200-54 0.0566 so 0.726 2.47 6.573 1.643 3.009 0.357 0.701 6.573 1.499 44.87 37.37 2091 2091 0.775 4.663 -1.265 0.804 3.338 0.856 40.1 ' Web -height to thickness ratio exceeds 200. Web stiffeners are required at all support points and concentrated loads. 2 Allowable moment includes cold work of forming. See Table Notes on page 6. Copyright @ 2011 by the Steel Stud Manufacturers Association CRANDALL ENGINEERING SHEET OF LJ 5448 Merrill Mill Road JOB NO. Marlposa, CA 95338 / Phone: 209-966-4844 DATE:L cp -,� 1 �v 0 Flet aq 3 si r ° 3 i �r" QiksF����� 43 54 68 .' s._97 z 54 `` :68..1.18 *..1. „5.18 . 12 2.19 3.38 4.56 7.04 3.07 7.00 11.01 14.09 4.14 7.42 9.99 15.70 20.19 8 16 2.09 3.29 4.48 6.97 2.95 5.06 6.89 10.91 14.00 4.00 7.28 9186 15.57 20.06 24 1.88 3.12 4.32 6.81 2.70 4.84 6.67 10.69 13.81 3.71 6.99 9.60 15.33 19.82 - 12 '210 _ ` 3.3L 6 4.49. •X6.98• -291,''. 508 6.90 •-,10.9'2 - 14:01 •4.02 ,730 ••` .:'9.88 4` ' 1559 .20.08 9 16 1.97 .320 X4.39 16.88' ;2.81 '+ .494 -•:6.76• '10.78 13:89 -,'3.84 `_711 '�971r : 1543 24 ,. , _ 1.71 ' - .298 -, , . 4.18 _. ; 6.68 :250. _ :. 4.65 6.48 - . 10.51 13.65 .' 3.47 ' j 6 75 '- 9 38 w .. 6 1511 i ; _• ,19.60., .. _ 12 2.01 322 4.42 6.90 2.85 4.97 6.86 10.81 13.92 3.88 7.15 9.75 15.46 19.95 10 16 1.84 3.09 4.29 6.78 2.65 4.79 6.62 10.64 13.76 3.65 6.92 9.54 15.26 19.75 24 1.52 2.83 4.03 6.54 227 4.43 627 10.29 13.46 3.20 6.47 9.12 14.85 19.35 12�r 178 3A3 423 672,• j257 471' 653., 10:55 .13.68355 '6.81 s '942 t 1514c ` 1962 12 16 154 �, 4: :>,284 404 654 t 229 444 ; 627;s 1029 v r13y45u� X322 647 ;911 x s1483 �* 1932 24 _'� 109 246• ;'c 367 ..,2 6-C,1� � J74.- 3.93': 5.76: -12.99 r •� - 2:57 ,+^ �•r3.11 : 581. _,L.,s; B49._.. a..�91422,�. ,, 1871,�� 12 1.51 2.80 4.00 6.50 224 4.38 6.20 10.20 13.37 6.28 8.94 14.71 19.18 14 16 1.19 2.54 3.74 6.25 1.86 4.02 5.84 9.84 13.04 2.67 5.82 850 14.27 18.74 24 059 2.02 3.24 5.76 1.14 3.32 5.14 9.12 12.40 1.83 4.94 7.66 13.41 17.87 • 12 '� 1.20:':' '- 253- �^ 373 - x{622-'�` 186 `- r'398- SE0, < 09.77 ..12.96 t - 2.59 i .:555 k `812 " 1378 r:1B35`•5, .-W 16 - y` O.BO s- 5.89 - " 1 38�". 3.52..•':1 _ 5:32" 19.27 IM -2.05 # 4:98, _;r , 7.57. ! . 13:207 `"'- 17 75-' ' 24:• .0.06E =:. : 1.53 if-_�..2.73'�---:.`524'." 0.49," .�.-;2.63 : -4.42 .. ,°8.33, - '.`.11:65 ::.-1.03 ..+".X391 •x -x...:;;.652. - 1 209 .., ,.1fi:58".; It no note, deflection meets L1720 Deflection meets 0120 a Deflection meets 0360 2 Deflection meets L1240 ° Deflection meets U600 See Table Notes on page 22. Copyright © 2011 by the Steel Stud Manufacturers Association f Structural (S) Stud Section Properties eco IBM Dei i es. r� eies. Areas VIe1gh ec.ar =PP ettres Iz ` " Sze al a>"a�let� rtslon I r"-er es d 1'OtfO °- 0F" kR4 .'ks1�: �. �- )��ll_,r���14.K)4�,�;Q�zk�"�b)b �6r � � )�5 ,,t., �x)a�'Up�)'•�'�� �l(!R���!7 , 25OS137-33 0.0346 33 0.197 0.67 0.203 0.163 1.015 0.052 0.515 0.203 0.158 3.11 3.10 975 399 0.079 0.076 -1.141 0.677 1.612 0.499 35.6 :2505137-0J.' .0.0451 33 0255 082 0261 O 208 1010 - 0067 0 511 0 261 0 205 4'53' 4 60 - X1265 394 .0:173 a 0098:: 1 129 . O 670 -: f599_ 0501- 33 6 2505137-54 0.0566 33 0.316 1.07 0.318 0.255 1.004 0.080 0.504 0.316 0.255 5.76' 5.75_ 1553 373 0.337 0.115 -1.115 0.663 1.583 0.504 33.4 2505137.54 0.0566 50 '0.316 • 1.97 .0318 .0.255 1004.."0.080 ' _ 0304OJ1B 0244- ' - 8:22'' ; 8.34 •'2353 ';' 565- : -0.337 0,115, 1115- 0663. 1583:,0:504 ';,27.17 2505737-68 0.0713 33 0.390 1.33 0.386 0.309 0.994 0.095 OA95 0.386 0.309 7.19' 7.19 1891 342 0.661 0.136 -1.096 0.653 1,561 0.507 33.1 250513768 0.0713 50 -0.390 1.33 0386 .. 0.369 6.994 •0.095 0.495 '.0:386' 0.308 ' 10.65' -' 10.67 2866 , 519 - ' 0.661' -' :0:138 .1096 ; ' ;0.653, ",1'561 -0.507 `.. 26 8 2505162-33 0.0346 33 0.223 0.76 0.235 0.188 1.027 0.087 0.624 0.235 0.180 3.55 3.56 975 399 0.089 0.146 -1.470 0.859 1.898 0.401 25OS162�3 0.0451 33, 0.289 , 0.98 0.302' 0.242 1.022 ..0:111' 0.620 :0.302. .0240 _5.22' 5.25: - ' 1265. 394 0:196.- 0184" f 457 0852 1.865 A402'. _44.1 dl' 250Si62-54 0.0566 33 0.358 1.22 0.370 0.296 1.016 0.135 0.613 0.370 0.296 6.571 6.57 1553 373 0.383 0.223 -1.443 0.845 1.868 0.403 41.8 250516234 0.0566 50 . '_=0358 .122 0,370 0:296. - 1,016 0:135 0.6131 0.370 0264'..,9.422 9:46' 2353.- 565 - '0.383 -0.223.` 1443 -: 0.845:_ _ "1.868' -.0.403 �339- 250S162S8 0.0713 33 0.443 1.51 0.450 0.360 1.007 0.162 0.605 0.450 0.360 8.21 8.21 1891 342 0.752 0.268 -1.424 0.835 1.846 0.405 417 250S162a 0.0713 50 4443` . 1'.51 0.450 0.360:. - 1.007 •0.162 0.605, ' 0.450 0.357 ` 12.11' 12.21. . *2866- 519-. ' +-0.952 - -0:268' 'A'A4' 0•SM 1S48 0.405 33.7' 350S162-33 0.0346 33 0.258 0.88 0.508 0.290 1.404 0.098 0.617 0.508 0.257 5.08 5.22 487 0.103 0.277 -1.324 0.796 2.026 0.573 427 350616213 0.0451 , 33 - -0.334.' .1.14 '0654 0.314 1.400 `. -0.-1 25 0.612 ' 0.654 • 0357 - -_705 :7.31 _1024 1739' -- 6310227 --0.443 0.350_. 1312 - - 89 ' -2,014 ~ 0575 `-42-6 - •42.7 3505162-54 0.0566 33 OA15 1.41 0.804 0.460 1.392 0.152 0.606 0.804 0.447 8.83 9.08 2253 633 0.426 -1.298 0.782 1.998 0.578 - 350516254 0.0566 ..: ; 50 OA 15.:: 1.4t -0.804 . '0;460 , 1392 - :0;152. ; 0.606 0 804' - :. 0.426•: 12.74 -• 13A5' -3372 ,• 947 , .0.443 0 426 t 298' , 067.82 _.. • 1.998 OS78' . 34.5 350516238 0.0713 33 0.515 1.75 0.985 0563 1.383 0.184 0597 0.985 OS51 14.56' 12.83 2774 592 0.872 0.514 .1.280 0.772 1.977 0.581 39.1 - 350S162a8 - - 0.07-13---.50--:1 0.515--1:75----0,985-0;563_ --4.383-= =0184--_ 0597-- - 0.985-_ -'-0.549. ;--16.44 -16.84 `--- 4202- - -- 897 _ - "0.872 - 0.514- 1280-,--0772 - _1:977- • - 0.581. - ._-345-% 350530054 0.0566 33 0.585 1.99 1.286 0.735 1.483 0.724 1.113 1.279 0.582 11.51 12.73 2253 633 0.624 2.166 -2.682 1.531 3.261 0.323 74.7 350530054: 0.0568; 50 - 0:585 .- 1.99='. :1286 0:735- --1483 :_ 0724;. .•1:,113 -.1'213r 0508:•. 1520 16.71 3372:'-,- 947 xd.-&24-'--_2166: - 2682_;-1531- 3261 ••3.238 0:323_' 60;4 350530068 0.0713 33 0.729 2.48 1.586 0.906 1.475 0.888 1.104 1.586 0.775 16.98 2774 592 1.235 2.649 -2.663 1.521 0.324 350530068 0.0713 ° 50- - . ',0.729 � � 2.48 � 1:586. ..AMB' ' 0.906 . 1.475• - -.1.10C..-. ... ',1:557-:. 0.887` -' _1531 2056 •:� �22'S4 4202 '. ' 897 �: -1235'' -%2:649'. =2.663 • _ f.! 21-" :3238'-. 0 324 �: _75.1 -60S 3625137-33 0.0346 33 0.236 0.80 0.479 0.264 1.424 0.059 0.501 0.479 0.232 4.59 4.73 1024 521 0.094 0.165 -1.003 0.615 1.813 0.694 34.7 362513713. -. 0.0451 : - _ 33 '_- 0306' • 1.04 - ' - 0.6 16- _- 0.340 .1:419-•._ 0 075 - 0.497. ; 0.816: - .0.321' . - '6.32' _' 6.65 1739. '• 676 0208;: --099.1,. 0608 1;601 - : 3415 3625737-54 0.0566 33 0.379 1.29 0.756 0.417 1.411 0.091 0.490 0.756 0.402 7.94 6.24 705 ,, .6.201_ 0.405 0.251 -0.978 0.601 1.785 _0697 0.700 345 1362S137S4-- 00566-; `50'-. 0.379 129-0756 X04171:411, -.0091,0;490, 0.756-• 0.381:11.42-'.11.91: _2341 - 3372•' -.1016 '_0:405 `0:251` 11978 _ ..0601 - -1,785 `.0.700° 362S137-68 0.0713 33 0.470 1.60 0.922 0.509 1.401 0.109 0.480 0.922 OA98 9.84 10.05 2884 662 0.797 0.302 -0.959 0.592 1.764 0.704 34.6 362S13738 - 0.0713 .5 - -0:470• -it60' 0922 .0:569. 1401' :0.109' 0:480. 0:922:• 0493`x,.-1477•., .15:24.. 4370: 1004 -�0.79Z - 0.302' -0.959 ":0592:.-•,1.764 0.704: -'278 3625162-33 0.0346 33 0.262 0.89 0.551 0.304 1.450 0.099 0.616 0.551 0.268 5.29 5.43 1024 521 0.105 0.297 -1.308 0.789 2.048 0.592 42.5 362516213 0.0451 33 = 0:340 - 1116-' 0.710: 0.392 1:445, ' 0.127 0:611' 0.7.10 0.372 -7.34 -' 7.62 -1739 • 676' .;4.230 0.376 --1:291' 0782 .x,2.036 ,0.:594 '.'42.5 3625762-54 0.0566 33 0.422 1.44 0.873 0.481 1.438. 0.154 0.604 0.873 0.466 9.22 9.51 2341 705 0.451 0.457 -1.283 0.774 2.020 0.597 42.5 3625162.54 0.0566 50- , 0.422 1.44 0.873: .0.481. 1.438 0.154 0.604- • 0.873 0.444 .'13.28 1359 3372 1016 -0.451 ,- 0.457 . -1283 0.774. `' 2.020' 0:597 34.4 362SI62-68 0.0713 33 0.524 1.78 1.069 0.590 1.429 0.186 0.596 1.069 0.579 11.43 11.65 2884 662 0.887 6.552 -1.264 0.765 1.998 0.600 42.7 3625162-68 0.0713 50 0.524 1'.78 1:069 0:590 1:429 0.186 0.596 1.069 0374 17.18 1X65. 4376 1004 ' 6.887 .'0.552 _ .1.998 -0.600' _ ; 34.3 3625200.33 0.0346 33 0.297 1.01 0.648 0.358 1.478 0.177 0.772 0.647 0.294 5.81 6.19 1024 521 0.116 0.577 _-1.264.0:765 -1.741 1.030 2.411 0.478 53:3 362S200-43 0.0451 33 0.385 1:31 0.836 0.461 1.474: 0227 0.767 0.836 0.427 8.43' 8.70 1739 676 0.261 '0:734' -1.729_ -1024 ;_;2.398 0.480':: 53.5 362520054 0.0566 33 0.479 1.63 1.030 0.568 1.467 0.277 0.761 1.030 O.W 10.93 11.23 2341 705 0,511 . 0.896 .1.715 1.015 2.382 0.482 53.3 362520054 0.0566 50 0.479 1.63 1.030 0.568 1:461 _ 0:277 0.761. 1.030 OA90 14.66 15.47 3372: 1616 < 0511 ' 0.896 •1.715 •1.016-':'2;-M- 0.482 •• 43.3 3625200.68 0.0713 33 0.595 2.02 1.265 0.698 1.458 0.337 0.753 1.265 0.687 15.29' 15.54 2884 662 1.006 1.089 -1.696 1.006 2.360 0.484 50.6 362S20058' 0.0713 50' 0.595 2.02 1265 0.698 1:458' 0.337 0:753 . 1265 0.666 19.95 _2051' 4370: 1004' - 1.008 1:089" -4.696. -f.Wd':'_-"2360 0:484? . 433 362530054 0.0566 33 0.592 2.01 1.390 0.767 1.533 0.734 1.114 1.383 0.607 11.99 13.22 2341 705 0.632 2.316 -2.659 1.522 3.265 0.337 74.5 362S30054'' :: 0.05W - '50. :-0.592' - - 2.Of 1390 -0787_.` 1.533.- .. -0734'; .. 14114: :, :11312 ' 0.529- ,15.83 -17.34• '. - 3372.- 1016.. - ;40.632 2.318; - 2659 -. -A 5 - 265..,,0.337 - --r 60:7 3625300-68 0.0713 33 0.738 2.51 1.716 0.947 1.525 0.900 1.105 1.716 0.811 16.02 17.65 2884 662 1.250 2.833 -2.640 • 1.512~ 3.243 0.337 74.9 362058" 630 0.0713 ' 501 0.738 "".2'.51 1.716 0:947 ' 1.525" 0.900 • 1:105. ' 1:684 0:716" 21'.44 -23.42' 4370 -1004; -1:20- ' 2.833 2.640 i =1.512. ' "314:f*, 0.337 60.4' 4005137-33 0.0346 33 0.249 0.85 0.603 0.301 1.556 0.061 0.496 0.603 0.259 5.12 5.29 976 595 0.099 0.204 -0.965 0.597 1.897 0.741 34.5 4005137130:045.1 33. 0:323 1:10 0.776 0388' ' 1.551' °-0.078' . OA91 0.776 0359 7.09. 7.47 - .1739`. 610 • :0219:: 0:257 -0.954' 0591. .1.885 0:744. 34:3 4005137-54 0.0566 33 0.401 _ 1.36 0.953 0.477 1.542 0.094 OA84 0.953 0.453 8.96 9.42 2603 944 0.428 0.311 -0.940 0.583 1.870 0.747 34.3 400S137S4' '0.0566 50 0: 401 1.36. 0.953 0.477 1.542 0.4. 09 0.484 0.953, OA28 1252 13.38- 3372 1223` : 0.428• _ M311 -0.940 _ -,OS83S` '-1'570 0.747 _27.7 4005137-68 0.0713 33 0.497 1.69 1.165 0.582 1.531 6.112 OA75 1.165 0.567 11.21 11.51 3215 895 6.842 0.375 -0.922 0.574 1.849 0.751 342 400513738 0.0713 50 0.497 1.69 • 1065 0.582 1:531 O.M.` OA75 -1;165 0.558' 16.70' 17.44 4871' . 1358 . 0.842... 0.375 -0.922 0.574 - "1.849. 0.751. 276 4005762-33 0.0346 33 0.275 0.94 0.692 0.346 1.586 0.103 0.611 0.692 0.299 5.91 6.07 976 595 0.110 0.363 -1.263 0.768 2.118 0.644 42.3 4COS162-43 0.0451 33 ' 0.357. 1:21 0S92 6446 14581. 0.131 0.606 . 0.892. 0417' 8.23. 8.54 1799 810 0.242 . 0:460 =1.252: 0:161• 2:106 0.64T 42.2 4005762-54 0.0566 33 0.443 1.51 1.098 0.549 1.574 0.159 0.600 1.098 0.526 10.39 16.84 2603 944 0.473 -1.238 0.754 2.090 0.649 42.2 400516234 . 0.0566 50 - 0:443: . 1.51 1.098 0349' 1.574. - - 0.159 0:600 -1.098 -. 0.498 14.90 1525, 3372 Q21- : 0.473. _0.560 0.560- -1.238. 0:764-.-- .2:090 0.649 34.1' 4005162-68 0.0713 33 0.550 1.87 1.346 0.673 1.564 0.192 0.591 1.346 0.658 13.00 13.30 3215 895 0.933 0.677 -1.220 0.745 2.069 0.653 42.2 400516258 0.0713 50 '0.550• 1.87'- •1.346- , 0.673' 1'.564 0.192 0S91, 1.346 0.648 19.41 20:15 4871 1356' 0.933 0:677 1:220' 0:745 .'2.069 ..0.653. 34.0 40OS20033 0.0346 33 0.310 1.05 0.812 0.406 1.619 0.183 0.769 0.812 0.328 6.49 6.90 976 595 0.124 0.697 -1.688 1.007 2.462 0.530 53.1 400520043... 0.9451 33 _ 0.402 ' 1.37 1:047 0.524' . • 1.615 :::0.235 0.764' 1.047 OA78 9.45 9.74 1739 810 •_ 0.272. .-0.88 6 -1,676 1.000 - 2.449 0.532 53.0 400520054 0.0566 33 0.500. 1.70- 1.292 0.646 1.608 0.287 0.758 1.292 0.623 12.30 12.77 2603 944 0.5341.083 -1.662 0.993 _ 2.433 0.534 53.0 40OS200S4 0.0566• 50 - 0.500 110 1292 0.646 1.608 0287 0.756 1.292 0.549 16.43 1731 3372' 1223 0.534 1.083 -1.662. 6.993 '2.433 0.534 42.£ 4WS200-68 0.0713 33 0.622 2.12 1.589 0.795 1.599 0.349 0.750 1.589 0.780 15.40 15.70 3215 895 1.054 1.318 -1.643 0.983 2.412 0.536 53.2 40OS20DS8 0.0713 50 0.622 2.12 1.589 0.795 1.599 0.349 0.750 1569 0.751 22.48 23.04 4871 1356 1:054 1:318 -1-.643 ' 0.983- 2.412' .0.536 42.9 400530054 0.0566 33 0.613 2.09 1.732 0.866 1.681 0.760 1.114 1.723 0.680 13.44 14.70 2603 944 0.655 2.802 -2.594 1.496 3.285 0.377 74.0 400S300-54 0.0566 50 0.613 2.09 1.732 0.866 1.681 0.760 1:114 1.637 0S92 17.72 19.25 3372 1223 0.655 2.802 -2.594 1.496 3.285 0.377 59.9 4005300-68 0.0713 33 0.764 2.60 2.139 1.070 1.673 0.933 1.105 2.139 0.914 18.06 19.68 3215 895 1.295 3.432 -2.574 1.486 3.263 0.378 74.3 40OS300S8 0.0713 50 0364 2.60 2.139 1.070 1.673 0.933 1.105 2.099 0.805 24.09 26.05 4871 1356' . 1.295 . 3.432. -2:574 1.486- 3.263 0.378 60.0 5505162-33 0.0346 33 0.327 1.11 1.458 0.530 2.112 0.113 0.589 1.458 0.512 10.11 8.63 699 699 0.130 0.713 -1.114 0.697 2.459 0.795 41.4 550516213 0.0451 33 0.424, 1.44 1.883 0.685 2.107 0.145 0.584 1.883 ' 0.661 14.79' 13:14 1550 1199. 0.288 0.905 -1:103 0S91 '2.448 0.797 392 5505162-54 0.0566 33 0.528 1.80 2.324 0.845 2.098 0.176 0.577 2.324 0.845 18.76' 17.87 2739 1666 0.564 1.105 -1.090 0.684 2.434 0.800 38.7 55OS162-54 0.0566 50 0.528 1.80 2.324 0.845' 2.098 0.176 0.577 2.324 0.611. 26.86'• 2352- 3093 188L. .0.564„ 1.105 -1.090 '0.684 2.434- 022 ..31.6 5505162-68 0.0713 33 0.657 2.24 2.861 1.040 2.086 0.212 0.568 2.861 1.040 23.72' 23.72 4347 2057 1.114 1.342 .1.072 0.675 2.414 0.803 38.0 55OS162-68' 0.0713 50 0:657 224 2261 1:040- 2.086, 0212 0S68 2.861 1.031' 34;94' 32.28 5350' 2532 1.114 • 1.342- -1A72` .'0.675 - 2.414. - 6.803.'-31.1 55OS300-54 0.0566 33 0.698 2.37 3.545 1.289 2.254 0.850 1.104 3.505 1.080 21.34 20.74 2739 1666 0.745 5.364 -2.365 1.401 3.449 0.530 73.0 55 M-54 •'-0.0566 50 --6.698- 2.37 3.545-- 1289, .2.254. 0.850 '1:104 3.295 0.983- 29.44 26.99' 3093' 1881: 045. 5.364 -2365 1.401 3.449 -- 0.530 59.2 55OS30068 0.0713 33 0.871 -•0.871 2.96 4.391 1.597 2.245 1.044 1.095 4.384 1.411 27.88 28.03 4347 2057 1.476 6.594 -2.346 _ 1.391 3.427 0.531 73.1 5505300-680.0713 50-- 2.96- 4391 1:597:-2.245 :1:044- 1.095 4285 ' 1287 -3853 36.85 _ 5350 2532.:'. 1.476• . 6.594 . -2:346- '1.391'.- _ 3:427.- .0.531-. 59:1 vveo-netgnr ro rntcxness rano exceeds luu, wed srtneners are required at all support points and concentrated loads. z Allowable moment includes cold work of forming. See Table Notes on page 6. CRANDALL ENGINEERING 5448 Merrill Mill Road Mariposa, CA 95338 Phone: 209-966-4844 \"�•�T� lEi� SHEET OF JOB NO. DATE: (T) Track Section Properties - es g>'* d_ Mess ��G><ossPCCoies� Area, IN gii Jx� Sx, 70Rx Effectnrero j3tcs" ijz I. Sze> [vta Vag if eP o� ltli Sxe. ag oaR , 0 w o i . o •� ti 1 ply, �t)fLn�}�"�-�17 �e L � �Jx , 1f:1 FI�L1t*'�1 -('n� . _,(. _.. ..t.rk),,�tu►'), bine 4WT150-N 0.0713 OA98• 1.69 ',.1.306- 0.615: 1:619'.0.102:- 0.453 -126. •0:548;,'10.82` 3435' -1'237;.0.513.'.-1535=;5205„,;0.844-,.;,0.320„_;[11.804_�.0_496-.1.864';0.814 400TXO -33 0.0346 0.2T7 0.94 0.768 0.371 1.665 0.113 0.639 0.561 0.220 4.341. 940 0.110 0.336 -1.229 0.737 2.166 0.678 4007200-03 0.0451 0360 - ` 1.23 1.002. 0.482 - 1.668. 0.148 0.637 0.811 0.3114 6.14 1739.0144 •0.46 0436_-w1224_a0.734 :2164 0.680 400720054 0.0566 0.452 1.54 1.268 0.604 1.675_ 0.182 0.635 1.093 0.426 8.42 2739 1.037 0.397 11.88 3372 3 0551 -1.217 0.730 2.165 0.684 40072008 8 0.07 13 `M69 1.94 1.617 0.761. -.1.685 ' 0.227_-0:632 " 1,485 0.591- -11.68 3435 1.412 0.549 ' 16.42'...7 •5205 '0.965 !'-0.702 'V66'0.689 55OT125-27 0.0283 0.226 0.77 0.948 0.336 2.046 0.027 0.348 0.786 0.192 3.79 372 0.060 0.160 -0.543 0.352 2.145 0.936 550T12540 0.6312-'0250 ._:0:85 1.045. �6.370�' 2,46 _ 0:030 '__0.347 • 0.897 0.226 4.47 499 : : 0.081 0,176: -0:542 0251„ 2145 0.936 55OT125-33 0.0346 0.277 0.94 1.159 0.410 2.046 0.033 0.346 1.029 0.270 5.33 680 0.110 0.195_ -0.541 0.350 2.145 0.936 55OT12543 0.0451 ` "0.360' -123 1510 0533 . 2.047 -0.043 0.344.' 1.428 0.416 8.23 1504• 0.244 _ ; 0.252 _ -0:537_ - 0.348-. '2,144' 0.937 55OT125-54 0.0566 OA52 1.54 1.903 0.668 2.052 0.053 0.342 1.862 0.597 11.80 2739 1.811 0.535 16.01 2980 0.483 0315 -0.532 0.345 2.147 0.939 55OT12588 0.0713 0569 1.94 2.412 0.839 2.058 0.066 0.339 2.412 0.807 15.95 4347 2,379 0.769 23.02 -5350 ' _0.965 0.397 -0.526 _--0.341 2.152 0.940 5507150.27 0.0283 0241 0.82 1.059 0.376 2.098 0.046 0.436 0.893 0.207 4.10 372 0.064 0.263 -0.716 0.456 2.259 0.900 550715030. 0:0312 0265 0.90 1.168 0.414 2.098 0.050 0.435 0.995 0251. 4:96 499 _ 0.086 _ 0289' ._ -0.715 ._ 0:455 _ ._ 2259 0.900 55OT150.33 0.0346 0.294 1.00 1.295 0.459 2.099 0.055 0.434 1.115 0.310 6.12 680 0.117 0320 -0.714 0.455 2.259 0.900 5507150-03 -0.0451 - OM&3 130. _1.688 0.596 2.099 OA72 0.432 1516 '0.468 9.25 - 1504 - - 0.260 b I -0709 '. 0;452 2258 0.901' 55OT150.54 0.0566 0.460 1.63 2.128 0.747 2.105 0.089 0.430 2.005 0.628 12.41 2739 1.928 0.595 17.81 2980 0.513 0.519 -0.704 0.449 2.261 0.903 550715088 0 0713 = ; 0.605:: 2.06, - 2 699<, 0.939 '. • 2112; 0:110 • -' 0:427 - _2.660 .-0.850- 16.80" 4347.... 2.569,• .0.804 24.07_ ` ' - 5350 •.' 1.025 4:655 -0:698 _- . 0.445. 2.265 ` 0.905 5507200.33 0.0346 0.329 1.12 1.567 0.555 2.184 0.1.123 0.613 1.246 0.307 6.06 680 0.131 0.694 4.088 0.674 2516 0.813 550r20D43 0.0451 -. ~0.0566 - • 0.428 ..1.46' - 2.043 _� 0.72 2 , _ 2.1851 _ 01160._ --0.6 11 x.1.690 _ 0.495 9.79 _.1504 - _ _ _ •18.86�_�_2980 .0.290 0.900 „ :1083 -:;60.671:._ 2514 , •' 0.8,14 55OT200-54 _ OS37 1.83 .2.578 0.905 2.191 0.199 0.609 2.253 0.669 13.21 2739 2.153- 0.630 0.573 1.133 -1.077 0.668 2.517 0.817 '5507200.68 0.0713 ` 'x :.0.676 "' �� 2:30`• �, � 3274 .. _ •1:139 - 2200' .. �.�-0.248 � ` .0.608 '` �3:07T 0.914 .18.06 - -4347 :- 2594: -- ". -0.857' _ 25.67 '- 5350 ^ ' ��1.146 r.+' -1 434 �"-. 1.070 .`;.0:663'.'__2.5'21',- 0.820 600T125-27' 0.0283 0.241 0.82 1.168 0.381 2.204 0.028 0.340 0.956 0.210 4.16 341 0.064 0.196 -0.519 0.339 2.290 0.949 600T125-30 _.;-00312 626.5_ - 0-94'_ .1286 4419 " 2.204'. `0.031' . ` 0'.340 - � 1.095. 6.249 4.92 456 - .. ` 0.086 0215' `° -0516 ':0.338 2289.1 .0.449 600T125-33 0.0346 0.294 1.00 1.428 0.465 2.204 0.034 0.339 1.258 0.297 5.87 622 0.117 0.238 -0.516 _ 0.337 2.289 0.949 6007125-43 0.0451 •0383 130 1.861 0.604 2.205 0.044 0:337 1.768 0.461 9.11 1377' _ 6:0.260 ,0.307, -0513 - 0:335. 2.289 0.950 60OT125-54 0.0566 0.480 1.63 2.344 0.756 2.209 0.054 0.335 2.299 0.666 13.15 2728 2.241 0.592 17.73 2728 0.513 0384 -0.508 0.332 2.291 0.951 600T125-68 0.0713 0.605 2.06 2.969 0.950 2.215 0.067 0.332 2.969 0.916 1809 4347 2.934 0.858 25.69 5350. .1.025 .0.483 - _ -0.503 -6.329. 2296 0.952 600T125-97 0.1017 0.862 2.93 4.281 1.347 2.228 0.092 0.326 4.281 1.347 30.43' 7359 4.281 1.347 40.33 10885 2.973 0.6&5 -0.491 0.321 2.305 0.955 600T15627'. 0.0283 0155` 0.87 1300 OA24 2.260 0.047 '0.427 1.011 0.214 4:23 341 0.668 :0320 -0.686 0:441 2400 0.918 600T150.30 0.0312. 0181 0.96 1.434 0.467 2.260 0.051 0.427 1.159 0.253 5.01 456 0.091 0352 -0.685 0.440 2.400 0.918 60OT15033 .0.0346 • 0.311 1.06 1.590 0.517 - 2.260 0.057 0.426 1.334 0:303 5.99 - 622 _ 0.124 0,390 ' - -0.684 0.439_ ,0.437 2.399 �y0:919 60OT15043 0.0451 OA05 1.38 2.072 0.673 2.261 0.073 0.424 1.890 0.474 9.36 1377 0.275 0.504 -0.680 2.398 0.920 600715054 40.0566 - 0.509 1.73 2.611 0.843 2266 0.091 0.422 2.473 0.689 13.62 2728 2.400 0.609 ' 1824 Z728 0.543 _ X6.632 - -0.675 -0.434 2:401-70.921 600T150-68 0.0713 0.641 2.18 3.309 1.059 2.273 0.113 0.419 3.262 0.963 19.03 4347 3.162 0.891 26.68 5350 1.086 0.797 -0.669 0.430 2.406 0.923 6007150-97 -6.1017- . 0913 3.11 4.778 1.504 2.288 0.156 0.413 '4.778 1.564 29.74. 7359 4378 1.444 4323 10885 3.148 1:138 -0.656,- 0.421 2:415 ^. 0:926 60OT200,33 0.0346 0346 1.18 1.913 0.622 2.352 0.126 0.604 1.542 0.333 6.59 622 0.138 0.847 -1.048 0.655 2.645) 0.843 60OT20D43 0:0451 0451 1.53 2.494 0.809 2.353 .- 0.163 0.602 • 2:076 0.565 11.16- 1377 .. ' 0.305 . - 1.098 _ =1.044 _ 0.652' '•'2.643';;, 0.944 60OT200-54 0.0566 0.565 1.92 3.145 1.015 2.359 0.203 0.600 2.759 0.759 15.00 2728 2.641 0.717 21.48 2728 0.604 1381 -1.038 0.649 2.646 0.846 60OT2008B *_0.0713 0.712 2.42 3.990 1.277 2.367 0254 -0.597 3.696 1.034 20:42 4347 3.540 0.973 29.12 5350 1.206' 1.746 -1.031 0.644 2.650 .0:649 60OT2D0.97 0.1017 1.015 3.45 5.773 1.816 2.385 0.354 0.591 5.758 1.667 32.95 7359 5.558 1.568 46.94 10885 3.499 2510 -1.016 0.635 2.659 0.854 80OT125.33` '0.0346 .03 63 1.24 2.895 0.711 2.824 0.036 0.313 2.441 0.407 8.03 465 _ 0.145 0.4 56-OA39 -.0.294•-2.875',:0.977 8DOT12543 0.0451 0.473 1.61 3.773 0.924 2.824 0.046 0.311 3.484 0.640 12.65 1030 0.321 0.589 -0.436 0.292 2.874 0.977 800712554 0.0566 0.594 2.02 4.745 058 2.827 0.057 0:309 4.666 0.940 18.58 2039,. 4.426 0.824 24.66- Z039 0.634- 0:735 -0.432' 0.289 2 8T ` 0.977 BOOT125-68 0.0713 0.748 2.54 5.998 1.454 2_.833 0.070 0.306 5.998 1.356 26.80 4087 5.956 1.216 36.39 4087 1.267 0.920 -0.427 0.286 2.861 0.978 800712597 0.1017 1.066 3.63- 8.613 � 2.082 2.843 0.096 0.301 , _8.613 2.062• 40.74 8843 8.613. • 2.062 61.72 10885 3.674 1.296 -OA17 _ 0179 2:889 0.979 BOOT15433' 0.0346 0,380 1.29 3.180 0.781 2.891 0.060• 0.397 2.569 0.414 8.18 465 0.152 0.751 -0.588 0.388 2.977 0.961 BOOT150-43, 0.0451 OA96 1.69 4.144. 1.015. 2.891 0.077 0:395 •3.689 0.655• . 12.95: 1030 0;336 0.972 0.564 -0.386 2.976 _0.961 800T150.54 0.0566 0.622 2.12 5.214 1.272 2.896 0.696 6.393 4.976 0.969 19.15 2039 4.692 0.844 25.27 2039 0.654 1.215 -0.580 0.383 2.979 0.962 800715088 0.0713 0.783 = 2.67 6594. - 1.599 2.962 _ 0.119- -0390 6.527 -1.412 27.91 4087- .6361 . 1.255. 37.58' 4087- - 1.327 1,525 -0575 0279 2.984 0:963 800T750.97 0.1017 1.116 3.80 9.479 2.269 2.914 0.165 0.384 9.479 2.269 44.83 8843 9.479 2.192 65.62 108.85 3.849 2.162 -0.564 0.372 2.993 0.965 800720033' 0.0346 OA15 1:41 3.749` 0.92'1 3.005. 6.135 -0.571 2.788 OA24 8.37 465 � � - 0.166 •1.638' -0.917 _ - 0.589.. 3.194 0.918 800720043 0.0451 0.541 1.84 4.887 1.197 3.006 0.175 0.569 4.043 0.676 13.35 1030 0.367 2.124 -0.913 0.587 3.193 0.918 BOOT20D54 0.0566 0.679 2.31 ' 6.152 1.501 3.011 0.218 0.567 . 5.505 1.009 19.93 2039 5.149 0.871 26.09 2039 0.725 2.664 -0.908 OSB4 3.196 0.919 BOOT20DM 0.0713 0.854 2.91 7.786 1.888 3.019 '0.272 0.564 7.306 1.490 29.45 4087 7.051 1.310 39.22 4087 1.448 3.357 -0.902 0.580 3.201 0.921 BOOT2DO-97 0.1017 1.218 4.15 11.212. 2.683 3.034 0.379 0:558 11.176 2.491 49.22 8843 10.833 2.347 7027 10885 .4.200 4.792 -0.889 -0.571 3.210 0.923 10007125.43' 0.0451 OS63 1.92 6.630 1.305 3.431 0.047 0.290 5.886 0.819 16.19 822 0382 0.973 -0.379 0.259 3.464 0.988 1000T125,% 0.0566 0.707 2.41 8333' 1.634' 3.434 0.059 0188 7.960 1.216 24.Q3 1628 7.479 1.055 3159' 1628 0:755 .1212 -0.376 0:256 3.466 '0.988 1000T125-68 0.6713 0.890 3.03 10.522 2.053 3.438 0.073 0.286 10.452 1.781 35.19 3261 10.155 1.575 47.15 3261 1.508 1.515 -0.372 0.253 3.470 0.989 1000T125-97 0.1017 1.269 4.32 15.077 2.912-_ 3.447 0.100 0.280 15.077 2.907 57.44 ' 8943 15.077 2.753 82.42 9507 4.375 .2.123 -0.363 0:247 3.477 0.989 1000T15043' 0.0451 0S86 1.99 7.207 1.419 3.507 0.080 0.370 6.195 0437 16.54 822 0.397 1.612 -0.513 0.345 3.564 0.979 1000T15054 0.0566 0.735 2.50 9461 1.777 3.511 0.100 0.368 8.430 1249 24.69 1628 7.880 1.079 32.29 1628 0.785 2.013 -0.509 0.342 3.567 0.980 1000T15088 0.0713 0.926 3.15 11.445 2.233 3.516 0.124 0.366 11.342 1.846 36.48 3261 10.774 1.621 48.53 3261 1.569 2.522 -0.505 0.339 3.571 0.980 1000T150.97 0.1017 1320 4.49 16.413 3.170 3.526 0.171. 0.360 1BA13 3.165 6254 8843 16.413 2.902 86.90 9507 4.550 3557 -0.495 0.332 • 3.579 0.981 1000T20D43' 0.0451 0.631 2.15 8361 1.646 3.640 0.183 0.539 6.722 0.861 17.01 822 0.428 3540 -0.813 0.534 3.769 0.953 10DOT20D54 0.0566 0.792 2.69 10.516 2.062 3.645 0.228 O.W. 9.231 1.295 25.60 1628 8,560 1.111 3326 1628 0.845 4.434 -0.809 0.531 3.772 0.954 1000T200M 0.0713 0.997 3.39 13.292 2.594 3.651 0.284 0.534 12.551 1.936 38.26 3261 11.820 1.684 50.42 3261 1.690 5.576 -0.603 0.527 3.776 0.955 1000T200-97 0.1017 1.422 4.84 19.087 1686 3.664 0:397 0.528 19.031 3.427 67.72 8843 18.583 3.081 92.25 9507 4.901 7.924 -0.791 0.519 3.786 0.956 1200T125-54' 0.0566 0.820 2.79 13.335 2.186 4.033 0.060 0.271 12.296 1.491 29.47 1354 11.460 1.286 38.51. 1354 0.876 1.820 -0.333 0.230 4.055 0.993 1200T125M 0.0713 1D33 3.51 16.826 2.747 4.036 0.074 0.268 16246 2.206 43.60 2713 15.686 1.934 57.90 2713 1.750 2270: -0.329 0227 4.059 0.993 1200T125-97 0.1017 1.472 5.01 24.078 3.897 4.644 0.102 0.263 24.078 3.690 72.92 - 7962 23.751 3.442 103.06 7902 5.076 3.171 -0.322 0.222 4.065 0.994 120OT15D54' 0.0566 020 2.8.9 14378- 2.357 4.117 0.103 0.348 12.962 1530 3013 1354 12.020 1.313 39.31 1354 0.9% - 3433. -0:454° 0.310 - 4.156 0.988 12DOT15048 0.0713 1.068 3.64 18.148 2.963 4.121 0.127 0.345 17.568 2.281 45.08 2713 16.566 1.987 59.48 2713 1.810 3.795 -0.450 0.307 4.160 0.988 120DT1%97 0.1017 1523- 5.18 25:987 4.206- 4.130, - 0.176 0340 25.987 3.996 78.97 7902 .25.719 -3.616 10827 7902 5.252 •5:335 0.301 4.168 0.989 120OT200-54' 0.0566 0.905 3.08 16.464 2.699 4.265 0.236 0.510 14.078 1.582 31.26 1354 12.962 1.350 40.41 1354 0.966 6.714 -0.730 _0.487 4.357 0.972 120OT20DM 0.0713 1.140 3.88 20.791 3.395 - 4.271.- 0.294 � 0.508 .19.277 2.383 47.09 2713 18.026 2.058 61.62_ 2713 1.931' `,BA31' -0.725 - 0.483 .. 4.362 0.972 12OOT200.97 0.1017 1 1.625 5.53 29.805 4.824 4.283 0.410 0.502 29.805 4.298 84.93 7902 28.959 3.819 114.35 7902 5.602 11.945 -0.714 0.476 4.371 0.973 ' Web -height to thickness ratio exceeds 200. Web stiffeners are required at all support points and concentrated loads. / 2 Allowable moment includes cold work of forming. VVV See Table Notes on page 12. Copyright O 2011 by the Steel Stud Manufacturers Association CRANDALL ENGINEERING 5448 Merrill Mill Road Marlposa, CA 95338 Phone: 209-966-4844 L SHEET OF JOB NO. DATE: Ing r- cnoz ?2- 0, SPG CRANDALL ENGINEERING 5448 Merrill Mill Road Mariposa, CA 95338 Phone: 209-966-4844 SHEET_ OF JOB NO. ILP OZd" DATE —SIT- / 14P 0 *', dv 'i — riL d (a, kv C -f I'2T '?-- kk-T Iz SECTION! I =�/ 8'/z" Zee Section D=8W B=2`�z' Ri =0.3125' j = 0.0" Fy = 60 ksi m = 0.0" F„ = 70 ksi xo = 0.0" Section Properties have been derived in accordance with AISI Standard "North American Specification for the Design of Cold -Formed Steel Structural Members" See DP 20.1 for definition of terms. When printed, this document becomes uncontrolled. Verify current revision number with controlled, on-line document. Author. Bob Hodges Full Properties Dimensions Axis x -x Axis y -y Critical Unbraced at f = 36 ksi Thick Len th Thick J CW re, 1, I, Fdgo.ol a, Thick Blank Area Lip, d Weight 1, Sx r■ ly Syd ry deg. in. in. int in. plf in' in' in. in' in in. 21.19 0.060 14.500 0.870 0.766 2.99 9.30 2.19 3.266 1.24 0.42 1.195 -15.76 0.068 14.500 0.986 0.782 3.38 10.52 2.48 3.263 1.42 0.47 1.198 -15.83 0.073 14.750 1.077 0.916 3.69 11.52 2.71 3.267 1.69 0.55 1.253 -16.60 0.079 14.750 1.165 0.928 3.99 12.45 2.93 3.264 1.84 0.60 1.255 -16.65 0.088 14.750 1.298 0.945 4.44 13.84 3.26 3.260 2.06 0.67 1.259 -16.72 0.098 14.750 1.446 0.964 4.94 15.37 3.62 3.256 2.31 0.75 1.263 -16.81 0.113 1 14.750 1 1.667 0.993 1 5.70 1 17.67 4.16 3.250 2.69 0.87 1.269 -16.93 When printed, this document becomes uncontrolled. Verify current revision number with controlled, on-line document. Author. Bob Hodges Distortional Buckling Deflection Properties Full Properties Critical Stress Critical Unbraced at f = 36 ksi Thick Len th Thick J CW re, 1, I, Fdgo.ol Fdb(2.4) Fdeio.oi Lod-0eed L .aebei in. in in' in. in in ksi ksi ksi in. in. 0.060 0.00105 15.749 3.478 0.622 2.470 31.22 180.14 14.36 21.19 23.43 0.068 0.00152 17.931 3.476 0.709 2.806 36.71 154.57 16.82 20.09 • 22.21 0.073 0.00192 21.538 3.499 0.847 3.214 42.66 155.67 20.52 21.48 23.75 0.079 0.00243 23.382 3.497 0.920 3.484 47.19 144.56 22.65 20.76 22.95 0.088 0.00336 26.172 3.495 1.031 3.889 54.26 133.81 25.96 19.83 21.92 0.098 0.00464 29.299 3.492 1.156 4.342 62.52 127.60 29.82 13.96 20.95 0.113 0.00712 34.050 3.489 1.347 5.024 75.68 125.69 35.95 17.89 19.76 When printed, this document becomes uncontrolled. Verify current revision number with controlled, on-line document. Author. Bob Hodges Effective Properties Evaluated at f = 60 ksi Deflection Properties Axis x -x Axis y -y at f = 36 ksi Thick lex Sex ' Mnxo le Se Meyo Ae col 1, ley in. in' k -in. ink ink k -in. int in n4 0.060 826 ' 1.$03 :• 108.18 1.00 0.322 19.29 0.447 9.07 1.24 0.068 9.66 2.164 129.84 1.21 0.396 23.75 0.538 10.48 1.42 0.073 10.92 2.486 149.16 1.67 0.543 32.59 0.639 11.52 1.69 0.079 1207 2.786 167.16 1.84 0.597 35.81 0.741 12.45 1.84 0.088 13.77 3.251 195.08 2.06 0.668 40.07 0.902 13.84 2.06 0.098 15.37 3.618 217.05 2.31 0.747 44.81 1.055 15.37 2.31 0.113 17.67 4.157 249.40 2.69 0.867 51.99 1.273 17.67 2.69 When printed, this document becomes uncontrolled. Verify current revision number with controlled, on-line document. Author. Bob Hodges GRANDALL ENGINEERING 5448 Merrill Mill Road Mariposa, CA 95338 Phone: 209-966-4844 ' SHEET_ OF JOB NO. l P � LA— DATE- 0j. 56 Z- \FP1 Screw Table Notes 1. Capacities based on section E4 of the AISI 2004 Specification. 2. When connecting materials of different steel thicknesses or tensile strengths, use the lowest values. Tabulated values assume two sheets of equal thickness are connected. 3. Capacities are based on Allowable Strength Design (ASD) and include safety factor of 3.0. 4. Where multiple fasteners are used, screws are assumed to have a center -to -center spacing of at least 3 times the nominal diameter (d) 5. Screws are assumed to have a center -of -screw to edge -of -steel dimension of at least 1.5 times the nominal diameter (d) of the screw. 6. Tension capacity is based on the lesser of pullout capacity in sheet closest to screw tip, or pullover capacity for sheet closest to screw head (based on head diameter shown) 7. Note that for all tension values shown in this table, pullover values have been reduced by 50% assuming eccentrically loaded connections that produce a non-uniform pull -over force on the fastener. 8. Values are for pure shear or tension loads. See AISI section E4.5 for combined shear and pull -over. 9. Higher values, especially for screw strength, may be obtained by specifying screws from a specific manufacturer. See manufacturer's data for specific allowable values and installation instructions. 10. Shear and tension data for screws was developed with the assistance of the Wei -Wen Yu Center for Cold -Formed Steel Structures (CCFSS), using manufacturers' data and evaluation reports available at the time of publication. Weld Table Notes 1. Capacities based on section E2.4 (for fillet welds) and E2.5 (for flare groove welds) of the AISI Specification. 2. When connecting materials of different steel thicknesses or tensile strengths, use the lowest values. 3. Capacities are based on Allowable Strength Design (ASD) and include appropriate safety factors. 4. Weld capacities are based on either 3/32" or 1/8" diameter E60 or E70 electrodes. For materials thinner than 68 mil, 0.030" to 0.035" diameter wire electrodes may provide best results. 5. Parallel capacity is considered to be loading in the direction of the length of the weld. 6. For flare groove welds, the effective throat of weld is conservatively assumed to be less than 2t. Allowable Screw Connection Capacity (Pounds Per Screw) for 1 " Long Welds "iarGra-al '�tF � �'-�v I ea ,0�• 9 di 4� ead �02�,�"&dfa�y�.�M_e�ad �. � 504d1a :�Q9°� d ,;•.._. Shears:,rnTension Shear4, ;Tension t, SheatzTensionTenswnR3 �tShear�,Tensionf: 18 0.0188 33 33 44 24 48 29 52 33 55 38 60 44 27 0.0283. 33 _ 33 ! 82 - T. 89 43 96- 50 `. 1&- _ 57. '110 .73 30 0.0312 33 33 _ 33 O.d346, 3-3 45 95 151 4U -61 103 164. -. 48 72. 111 177.- 55 (i4. 118 '- 188 63 95:_;UO.. 127 43 0.0451 33 45 214 79 244 94 263 1091 280 124 Note 3 14_4 64 0.0566 33 45 ' 214 84 361 118 310 r 137 394 156 -227 68 0.0713 33 45 214 84 363 118 406 ••159/ 525 196 6W 97 0-1017 33 45: 214' 84.. '. _ .303. 118 1406. -. _159 ' -525 205" -. ..704. 118 0.•1242 33 45 214 84 303 118 406 159 525 205 704 Z75 54 0.0566 .. 50 '...- 65' a 214 -.''BM1.... .303. .....- '118.406. i.. ...1�. • .. -.:_..... ,525'.205 ::: :_.613.. 68 0.0713 50 65 F 214 84 303 118 406 ' 159 205 704 97 0.1017 50 65 214 .. Elk. . 363 118 ` 406 _. 159 _525 525... 205. 118 0.1242 50 65 214 84 303 118 406 159 525 205 704 275 Weld Table Notes 1. Capacities based on section E2.4 (for fillet welds) and E2.5 (for flare groove welds) of the AISI Specification. 2. When connecting materials of different steel thicknesses or tensile strengths, use the lowest values. 3. Capacities are based on Allowable Strength Design (ASD) and include appropriate safety factors. 4. Weld capacities are based on either 3/32" or 1/8" diameter E60 or E70 electrodes. For materials thinner than 68 mil, 0.030" to 0.035" diameter wire electrodes may provide best results. 5. Parallel capacity is considered to be loading in the direction of the length of the weld. 6. For flare groove welds, the effective throat of weld is conservatively assumed to be less than 2t. i -or niter wetas, Hist 57uu equation t2.4-4 must be cnecked ror 118 mil material, or whenever the thickness of the thinnest part is greater than 0.10 inch. 2 For weld lengths greater than I", equations E2.4-1 and E2.4-2 must be checked. 3 For flare groove welds, AISI S100 equation E2.54 must be checked for 118 mil material, or whenever the thickness of the thinnest part is greater than 0.10 inch. Copyright O 2011 by the Steel Stud Manufacturers Association Allowable Welds Capacity (Pounds) for 1 " Long Welds "iarGra-al '�tF � �'-�v I - s .etpendicular.M .,Parallel:: Ni _a,r .. PORI _..... 43 54 0.0451 0.0566 33 45 33' 45 619 822 866 544 1,084 Paz 683 an 68 - 97' 0.0713 .0.1017 33 45 33` - 45 .- 1,082 .1 ,618 1,365 859 ' 1,947 - - 1',226. 1,048 118 0.1242 33 45 Note 1 I Note 1 Note 3 Note 3 54 0.0566:. 50. 65' :..1;188. . '. 1',566 .,. '985- 68 97. 0.0713 0:1017 50 65 50 1 65 1,563 2,337.. ' ' 1,972 2813'. 1,241 1771 1,514 zlsg 118 0.1242 50 65 Note 1 Note 1 No 3 Note 3 i -or niter wetas, Hist 57uu equation t2.4-4 must be cnecked ror 118 mil material, or whenever the thickness of the thinnest part is greater than 0.10 inch. 2 For weld lengths greater than I", equations E2.4-1 and E2.4-2 must be checked. 3 For flare groove welds, AISI S100 equation E2.54 must be checked for 118 mil material, or whenever the thickness of the thinnest part is greater than 0.10 inch. Copyright O 2011 by the Steel Stud Manufacturers Association Structural (S) Stud Section Properties 16�e�ross e on # �o es��� Afea; Wet�ftt _ Sxe ct�sRo Mal JkT00y Cw Xo t � �- '_> t /tri, y �J � �.a a9 #et �=� /in' rirrkr /trkk "`� /Ib�^ '0 3 I _ in "'�. ._\,__._,..1-'S4�_�rR��i.1.__._._.4.-/.1_.��'`__/3.'i".".Ll¢e- , Iblft/rin3in', Q in 1,,,yy iririn4 Y= tr1 in fns ,�c1._.,1.._��' /m 1n p .• BOOS200.68 "':0.0713 '33 "0.907. :3.09 ..8.140 ;2035 2996•',- 0_435-'. 0.692 :-8:140," .8:140'"., -2.035•_ . .45.29', 41:79: 4221.;`3367,,; '. '-11537 '4246. 0796 -{3!319 .-.:,02W -.,47.0, BOOS200.68 0.0713 50 0.907 3.09 8.140 2.035 2.996 0.435 0.692 8.140 1.964 65.21' 54.70 4221 3367 1.537 5.712 -1.248 0.796 3.319 0.859 38.4 8005200-97 0.1017 33 1.271 4.32_ 11203` '2.801 2.90 =`0.576.' 6.673'. 11.203-- 2.801' 65.12' 65.12: 8643- ,4824 4.381 .;7.884 1:214,.,'0777 .-3.278 0863 --_45.5 BOOS200-97 0.1017 50 1.271 4.32 11.203 2.801 2.969 0.576 0.673 11.203 2.801 96.63' 89.76 10885 5938 4.381 7.684 -1.214 0.777 0.862 37.2 800S200-118 0:1242 ' 33 7531 • ' 521 - 13.316- ' 3.329 2.`949• . 0.665 - -_ _ 0.659 . -.13:3116 •3329 ; 7978 ? 79:78'; 11341 :, 4971 - 7.873 .8 981 _- 1:188 ' -6.764 ' _3.278_ 3.247 O.Sfi6 . %id:6 BOOS200-118 0.1242 50 1.531 5.21 13.316 3.329 2.949 0.665 0.659 13.316 3.329 117.95 ' 117.55 16235 7115 7.872 8.981 -1.188 0.764 3.247 0.866 36.5 BOOSM5 43. '0.0451 .: 33. 0,62T,. 213- ; 6,015.-•.1;504,. 3097 `0.500- 0,8 -,;6.015 1313:.'.25.95. 2206 :105.:, 1051 ;_0.425 6.374..;-.1675: 1043' -3,632-.:0:787'- jl. 5 BOOS25054 0.0566 33 0.783 2.66 7.465 1.866 3.088 0.614 0.886 7.465 1.712 33.82 30.07 2091 2091 0,836-._7.850 -1.661 1.036 3.617 0.789- 61.4 800S250-54 "0.0556.6 50 ':'0.783 -0.978 .266:.--7.465_: 1.866".3.086.'-0.14.` 0.686. :7:378.`-<:I.iZ- 4566-, 39:13., 2091;,;;`-`2091 :0:836' 7.850'- X1661,',_1036 .3.617 - 0789' 49.8:': 8005250-68 0.0713 33 333 9.2§1 2.315 3.077 0.752 0.877 9.261 2.220 48.33' 43.63 4221 3367 1.658 9.652 -1.644 1.027 3.597 0.791 58.2 BOOS25058 0.0713 50 0.978. 3.33 9.261 . 2.315. 3.077 0:752 _ 0.877 9240 2.059: -`61:65 53:75 `4221 3367: ;1.656. 9.652 ' -1.644 `1.027 . ,3597 _ � 6.791. 49.6 800S25097 0.1017 33 1.372 4.67 12.789 3.197 3.053 1.069 0.857 12.789 3.191 72.07' 70.72 8843 4824 4.731 13.091 -1.607 ' 1.008 3.555 0.796 56.8- 800S25a97 0.1017. : 50 ;1:372--- =4.67. _ 12789 :3.197 3.053. 1.009- 0.857• 12.789 3.09- 102.70' -93.42 10885 'S93B _ ::4131: 13.091_ 1607 -,,1008_-. 3:555 -0:796.- � 46.4.- 8005250-116 0.1242 1.655 5.63 15.242 3.810 3.035 1.175 0.843 15.242 3.810 88.31' 88.31 11341 4971 8.511 15.395 -1.580 0.994 3.524 0.799 55.9 >-8005250.118•: 0.1242_,x. _33 ;. 50' ..1655`_ 5.63',45242 .. -_3.810 -3.035': 1175 ' ;0.843 - '15:242:_, 3707 .12731-' 12292- ..16235 -7115 -2091 X 8511 15:395.��1580- ,0994 ,3524_. 0799_.. '_45:6• 8005300-54 0.0566 33 0.839 2.86 8.358 2.090 3.156 0.960 1.069 8.249 1.795 31.13 2091 0.896 12.076 -2.0_73 1.271 3.924 0.721 72.2 8005300-54 , 0.0566'-' "50 : , ' 0.839 `2.86.. , 8.358 •, 2.090 . -3.156: 0.960 10069: _35.28 '7.862' - YS35',' 45.96 4022 ' 2091 ` . ' 2091: _ •;0:896- 12.076' •2.073 • =•1271 .: -3:924 - 0.721': •• 58.6 .. 800530058 0.0713 33 1.050 357 10.382 2.595 3.145 '145- 1.179 1.060 10.351 2.321 45.86 42.54 4221 3367 1.779 14.888 -2.055 1.262 3.903 0.72372.0 .800$300.68 0:0713' ' : 50- :.1:050 .:357 10382.: ;;2:595 1.174 1':060-' `.10.082-:.2.145 6421 55.47.-. '4221• 3367. .1,779`. 14,888:'-2.055: 1262, 0.723', 58.4. 8005300-91 0.1017 33 1.474 5.02 14.375 3.594 3.123 1.595 1.040 14.375 3.443 76.21' 73.25 9843 4824 5.082 20.304 -2.017 1243 ,3.9W- 3.860 0.727 67.7 800530091' 0.1017:' 50} .1:474: x'5:02 14375" 3:594 31231 . 1595, 1:040 '�'14.170 3:304",. 9892.,;.89.89 10885,,.'59381. ,5_082 20a04fi 2012 :(243.x3860 :0721; x_58:1':` 800S300-118 0.1242 331.779 6.05 1.767 4.292 3.106 1.871 1.025 17.167 4.168 94.33' 95.78 11341 4971 9.149MV 23.9790.1.989-1.229- 3.828 ~ 0.730 66.8 8005300118 .0:1242-_ 50'. 1:779' 605 -.17167'`4.292• ,3106 :-1;871_. 1.025 :17.022:'_4108-:138.41' 126.69 16235 -'71- -..9;-1- -•22.697 979,- 1`989 :1229h 3.828-:-0730 ;54:5_- BOOS350-54 0.0566 33 0.938 3.19 9.683 2.421 3.212 1.646 1.325 9.477 2.125 41.98 38.29 2091 2091• 1.002 v -2.766• 1.668 4.441 0.612 90.0 800S350-54 0.0566 50 0.938:... 3.19 "4.683:- 2:421 , 3.212: ,1:646, 1.325 8.191:;, 1:669; , 5596 �49:Z4:, , :2091 _ .°,2091 1002 22.897' 2766 r .1688_ , S. 0612 ',731:. BOOS350-68 0.0713 33 1.174 4.00 12.046 3.012 3.203 2.034 1.316 12.046 2.837 56.07 51.89 4221 3367 1.990 28.308y •2.748 1.658 4.421 0.614 89.9 .8005350-68 0.713' 50. - 1.174 4:00 12.46- 3.012 :3203 2034: 11316,- 11:909;i596' 77.73' .,68:05,- 4221-''•3367 '_ 4.990 X28.308; 2748;_ `1658 4:421 -0614'•- .''72:9:- SDOS350.97 0.1017 33 1.652 5.62 16.737 4.184 3.183 2.784 1.298 16.737 4.101 89.43' 87.25 8843 4824 5.696 38.834 -2.710 1.639 4.377 0.617 `BOOS95097 0:1017 '� 'SO. 1�.652, •,5:62'_167374:184 3:183`,2784:. 1298- 16.7373785;..:113.34 - -- 10867'� 10885 15938 _ 'M �, 5.696 38 834 2 710 `x'1'639 • -- 4:377 0 817 - _85.4 ^ 727 800S350-118 0.1242 33 1.997 6.79 20.041 5.010 3.168 3.295 1.285 20.041 5.010 111.44' 111.44 11341 - 4971 10.267 46.068 -2.682 4.345 0.619 84.6 8005350118 0.1242 50: 11997 ' 6:78 .20:041 '5.010 • '3:168`: 3.295" 1:285.' 20.Odf 4.762:' 158:02' 150:37- . .16235 . --7115--' _�10:26Z -46.066 X4345 -2:662 _1.624 4.624' - 0.619. 68:9. 10005162.43' 0.0451 33 0.627 2.13 8.025 1.605 3.577 0.168 0,518 7.523 1.302 25.74 22.49 836 836 0.425 3.430 -0.823 0.545 3.707 0.951 38.8 10DOS162-54-. 0.0566 33 -. 0.783 '2.66: 9.950 11990° -' 3:565 _ 0:204 .0511, . 9.627 1.722 - .34.02 .31.11- 7.166. 1661 ' s,0:B36-. 4:198> --0:812` `0538` -, 3;692 -;0:952 • 38:6 1000S162.54 0.0566 50 0.783 2.66 9.956 1.990 3.565 0.204 0.511 9.391 1.572 47.07 40.37 1661 1661 0.836 4.198 -0.812 0.538 3.692 0.952 31.3 1000S162-68 0:0713 33 0.978 333 12.325 - 2.465 3.550 0.246' 0:502- 12.256 2.276 44.98 42.91 3345 3345 ' 1:658- ' 5:121- -0.798 0:531' .33.673 0.953 '_ 38.2 1000S162-68 0.0713 50 0.978 3.33 12.325 2.465 3.550 0.246 0.502 11.978 2.154 64.51 56.35 3345 3345 1.658 5.121 -0.798 0.531 3.673 0.953 31.0 10005162-97 0.1017 33 1372 4:67 16.967 3.393-, 3.516. 0.320 0.483 . 16.967 3.393_ 67.06. 67.05 -, 8843.-. 6434' '4.731. -6.827; --0.768: - 0514 '3:631. 0955- 37.5 1000S162.97 0.1017 50 1.372 4.67 16.967 3.393 3.516 0.320 0.483 16.967 3.269 97.69 92.56 9864 7177 4.731 6.827 -0.768 0.514 3.631 0.955 30.4 -1000S162-118, 0:1242 - 33 : 1.655. _, 5.63 20.1.69- : 4.034'-. 3.491. 0,363 0.468 20:169' 4.034 .10014° -100.25•: 13189: 7747. : 8.511. - 7.924; -0.746 • 05023.600.- 0957;.: 32.9. 10005162-118 0.1242 50 1.655 5.63 4.034 3.491 0.363 0.468 20.169 4.034 120.77 120.34 16235 9536 8.511 7.924 -0.746 0.502 3.600 0.957 36.0 1000S20043'. ;0.0451' i3 ".0-67 229`. _20.169 _9CW, -1:817_ 3'd6-"'0369,'•0:671; :8:602- '1.470.,•;29.05, 26:14. '836:-- _ 836 -;0456- .6236-: 1.147 --0743 , 39:10-. 0.9,14, 49' 0.0566 33 0.839 2.86 11.278 2.256 3.666 0.378 0.671 10.953 1.984 39.20 35.86 1661 1661 0.896 7.665 .1.135 0.737 � 3.896 0.915 49.1 .0.0566 50 2.86.."11278..2:256 `3.666 0.378.: i0.671: '10.769��. 1705:'-51:05' 96.62 1661=:; 16611-;,0.8967:665 1135.i0737�--3:8960,915.-;.-39.8�: 10005200-M 0.0713 33 1.050 357 13.994 2.799 3.652 0.460 0.662 13.920 2.607 51.51 49.07 3345 3345 1.779 9.401 -1.120 0.729 3.876 0.917 48.8 f000S20058 -.' 0:0713 _ 50 1.050 _: 357 . •' 13 994 _. 2.799 3.652` ' 0.460' _ 0.662. 13.665 2.420 .: ,72.46 6450. ; 3345.. . 3345 • 1_779 9 401'' .1'.1.210 729 - 3'.876' 0,917. �., 39.6; 1000S200-97 0.1017 33 1.474 5.02 19.336 3.867 3.622 0.609 0.643 19.336 3.867 76.42 76.42 8843 6434 5.082 12.679 .1.088 _-.0 0.711 _ 3.836 0.920 48.2 1000S20097 '0.1011 50. 1.474 5.2 19.336.'.'3867 3,622. 0.609' 0.643' 191336. _3.741 .'112.00 104:7 .9864 _3- 77177-` '5:082_: 12.679 '.088- 0711- -39,0: 10DOS200-118 0.1242 33 1.779 6.05 23.052 4.610 3.599 0.703 0.629 23.052 4.610 110.50' 110.50 13189 7747 9.149 14.848 -1.064 - 0.699 _3.836_-,'0:920 3.805 0.922 43.3 10005200.118 0.1242 50' 1.779 "605 23.052' 4.610 3599 0.103 0.629. '23.052 4.610 138.04 135.74 ' 16235.. 9536 :'9.149 14:848 1.064 0:699 3.805,- 0:922, 38.7" - 1000S250-43' 0.0451 33 0.717 2.44 10.203 2.041 3.771 0.531 0.860 10.203 1.617 31.95 27.67 836 836 6.486 10.481 -1.518 0.965 4.155 0.867 60.7 1000825054 0.0566 33 0:896 3.05 12.677 2.535 3162 0.653 0.854. 12.677 2.277 44:99 38:62 1661 1661' -0:957 12.922 -1.505 0.958 41140 0.868. 605 1000525054 0.0566 50 0.896 3.05 12.677 2.535 3.762 0.653 0.854 12.660 1.879 56.26 49.16 1661 1661 0.957 12.922 -1.505 0.958 4.140 0.868 49.1 10DOS250.68 0.0713 33 1.121 3.81 15.751 3:150 3.749 0.799' 0.844 15.751 3.028 65.93' 55.62 3345 3345 - 1.899 15.909 -1.488'.0.950 4.121 .0.870 57.3 1000S250 -M 0.0713 50 1.121 3.81 15.751 3.150 3.749 6.799 0.844 15.741 2.768 82.89 68.13 3345 3345 1.899 15.909 -1.488 0.950 4.121 0.870 48.8 1000525097 0.1017.. 33 1.576' 538 21.827 4265. 3.722 1.072 - 0.825 21.827 4.357. 98.412 .91;77 8843 6434 ; 5.433. .21'.832 -.454.0.932, :4:080...0.873- 55,8 1000S25097 0.1017 50 1.576 5.36 21.827 4.365 3.722 1.072 0.825 21.827 4.181 140.63' 120.13 9864 7177 5.433 21.632 -1.454 0.932 4.080 0.873 45.6 10005250118 0.1242" 33 1'.904 6.48 26.080 5:216 -3.701. '1:249- 0,810- 26:080' 5.216, 120:89? 120.71 13189. .:7747' - 9788. '' 25.490. -1.428 0.918:' '4A49. �: 6.876 - 54:1 10005250118 0.1242 50 1.904 6.48 26.080 - 5.216 3.701 1.249 0.810 26.080 5.082 174.84' 159.80 16235 9536 9.786 25.490 4.428 0.918 4.049 0.876 44.8 t000S30054 0.0568 33- 0:95] '324. 14:076 2.815 1844' 1.024 ' 1.037 13.938 2312- 45.69"'99:41' 1661 1661 :' 1:017: 19.888- '-1:892'1.185-'•4.408` :0:816'- "71.5 10DOS300654 0.0566 50 0.953 3.24 14.076 2.815 3.844 1.024 1.037 13.440 1.962 56.96 50.69 1661 1661 1.017 19.888 -1.892 1.185 4.468 0.816 58.1 10DOS300-68 0.0713 33 1.192 4.06 17.509 3:502 3.832 1.258 1.027 '17.441 3.158 62.41 54.29 . 3345 3345 2.020 - 24551 -1.874: 1.176 4.388 0.818 - 71.3 10005300.8 0.0713 50 1.192 4.06 17.509 3.502 3.832 1.258 1.027 17.099 2.802 83.89 70.40 3345 3345 2.020 24.551 -1.874 1.176 4.388 0.818 57.8 1OWS300-97 0.1017 33 1:677 5.71 24:318 4.864 3.808 1.702 1.007 24.318 4.671 103392. 94.70 8843 -6434 5.783 33.570 . -1338 058 4.346 0.821 66.9 1000S30097 0.1017 50 1.677 5.71 24.318 4.864 3.808 1.702 1.007 23.970 4.499 134.69 115.62 9864 7177 5.783 33.570 •1.838 1.158 4.346 0.821 57.4 10005300-118 0.1242 33 2.028 6.90 29.109 5.822 3.789 1.997 0.992 29.109 5.662 128.16' 125.04 13189 7747 10.427 39.725 -1.811 .1..144 4.315 -0.824 65.8 1000S300-118 0.1242 50 2.028 6.90 29.109 5.822 3.769 1.997 0.992 28.861 5.586 188.23' 164.19 16235 9536 10.427 39.725 •1.811 1.144 4.315 0.824 518 1000535054 0.0566 33 1.052 3.58 16.220 3.244 3.927 1.768 1.297 15.942 2.772 54.77 48.69 1661 1661 1:123 36.575 -2.546 1.566 4.857 0.725 88.9 1000535054 0.0566 • 50 1.052 3.58 16.220 3.244 3.927 1.768 1.297 15.577 2.328 69.69 62.97 1661 1661 1.123 36.575 -2.546 1.566 4.857 0.725 72.2 1000S35058 0.0713 33 1.317 4.48 20204 4.041 3.917• 21&5 1188 20204 3.824 7557. 66,40 3345 3345 2.232 45.277 -2.529 1.657 4.837 0.727 88.7 10DOS350-8 0.0713 50 1.317 4.48 20.204 4.041 3.917 2.185 1.288 20.026 3.417 102.32 86.60 3345 3345 2.232 45.277 -2.529 1.557 4.837 0.727 72.0 1000535097 0:1017 33 - ..1.855 • :631 28.148: ;5.630 3.895 -: 2992 " 1270 28:148 5.517 .'-_12033' 112.86 8843 . 6434 _ 6:397 62.280- -2.492 ' 1.538: 4:795; . 0.730 84.1 1000535097 0.1017 50 1.855 631 28.148 5.630 3.895 2.992 1.270 28.148 5.118 153.25 139.74 9864 7177 6.397 62.280 -2.492 _- 1.538 4.795 0.730 71.6 1000S350118 0:1242: 33,.4 t 2245• 7.64 ' 33772 .6.754 3878 '' 9:543' 1256 '51.772 6.754 _I 23" 147:03' . 13189 :_.7747 11544 74;030': -2.465: 1524 "4:764 0.732 83:1 1060350118 0.1242 50 2.245 7.64 33.772 6.754 3.878 3.543 1.256 33.772 6.427 213.25' 194.46 16235 9536 11.544 74.030 .2.465 1.524 _' 4.764 0.732 67.8 ' web-nergnt to rnicKness ratio exceeds zuu. web stiffeners are required at all support points and concentrated loads. 2 Allowable moment includes cold work of forming. See Table Notes on page 6. / Table Notes 1. The centerline bend radius is based on inside corner radii shown in the steel thickness table on page 5. 2. Web depth for track sections is equal to the nominal height plus 2 times the design thickness plus the bend radius. 3. Hems on non-structural track sections are ignored. 4. Effective properties incorporate the strength increase from the cold work of forming as applicable per AISI A7.2. 5. For deflection calculations, use the effective moment of inertia. 6. 18, 27 and 30 mil track material considered non-structural, based on ASTM C645. (T) Track Section Properties Desg��C�ss Secboju �fi n oe[tPeSEiveP Area Welght : Rx :Ii o3 s�} 1xe� Sxex a V Eti�ropOKSj Ixex Sxe a Vague; llorllto"13i- !x1000 Fw� Xo: " m ;Ra y(xSx i �e 3 ,4 _ �f (n') `-®R r -Gn 177} ; (1!� blit (I _ (m.) �: :)_. (h). !�) . U�} f�') fn `..:(insk _ �!ti) . pa .( ) �) ry . On9:. ro f!�)t 1627125.19 0.0168 0.077 0.26 0.041 0.047 0.733 0.013 0.411 0.030 0.025 0.50 302 0.009 0.007 -0.878 0.503 1.215 0.478 1627125.27 0.0293 0.117 0.40.. 0.063 0.072 - 0.735 _.0.020' _':0.410 0.050 - ` 0.044 _ `. 0.87 - 541 - .... _ 0.03 1: - 0.010 -0.872. 0.51 1.211 0.482 1627125-30 0.0312 0.129 0.44 0,070 0.079 0.735 0.022 0.409 0.057 0.050 1.00 597 0.042 0.012 -0.870 0.500 1.210 0.483 .1627125.33. 0.0346 '. 0.143 0.49. : OA77: 0.087... 0.736_ :0.024 - .0.408' <0.066' 0.058' 1:15 x'.663.. :- - ,. - ; 0.057 ;. ' 0.013.. -0.868 X0.499 069, 0.484 250T125.18 0.0188 0.094 0.32 0.103 0.079 1.051 0.015 0.400 0.078 0.045 0.90 249 0.011 0.018 -0.769 0.4601.362 0.681 -250T12537------0.0283---0:141---0:48'-0:157-0:119-1:053---0:022---0:398- -0:-763=-0457.- .1 M, .0;685- -0:129'-0.079.-1:56-685- - =--0:038-0.027 250T125.30 0.0312 0.156 0.53 0.173 0.131 1.053 0.025 0.397 0.145 0.090 1.77 832 0.051 0.030 -0.762_ OA56 1.359 0.686 2507125-33 0.0346 0.173 OS9 0.192 0.145 •1:054 0.027 '0.397, :0.166.. 0.103.. 203 1024..E _ ,. _ 0.069.'0,033 -0760_, 0.456"_.1:356'0.687 2507125.43 0.0451 0.225 0.77 0250 0.188 1.055 0.035 0.395 0.231 0.147 2.91 1356 0.153 0.042 -0.755 0.453 1.356 0.690 250T12554 0.0566 0.282 0.96 0,318 0236 1.062 6.043 6.392 - 0.310 0203 4.01 1692. _ 0;297 0.186 5.64 2563- : 0.301'' "0,054.--0.749 ; _ 0349: -'i._357.'-0.696 2507725.68 0.0713 0.355 1.21 0.408 0.297 1.072 0.054 0.389 0.408 0.281 5.56 2111 0.402 0.262 7.85 3199 0.602 0.069 -0.740 0.444 1.360 0.704 2507150-27 0.0283 0.156 0.53 0.181 0.137 1.078 0.037 :.0.486 , 0.139 UN- 1.61 0.042.. ' 0.044', ` -0.976 X0.575 ,_ 1634:. 0.595 25OT150-30 0.0312 0.172 0.58 0.199 0.151 1.078 0.040 0.486 0.157 0.093 1.83 832 0.056 0.049 -0.975 0.574 1.533 0.595 25OT150-33 0.0346 - 0.190 0.65 0.221 .' 0.167 1.079 0.045 - 0.485 0.179 0.107 2.11 - 1024 - - 0.076:- .-0.054 ='-0.973 : _ 01573 1:532 `' 0.596 2507150.43 0.0451 0.248 0.84 0.289 0.217 1.080 0.058 0.483 0.252 0.154 3.03 1356 0.168 0.010 -0.968 0.570 1.529 0.599 250T15054 0.0566 0.311 1.06 0.368 0.273 1.088 0.072 0.481 0.342 0.213 422 1692 0.325 0.197 5.89 2563 0.332 0.089 -0.961 0.566 1.529 0.605 250TI50-68 0.0713 0.391 1.33 0.472 0.344 1.099 0.089 0.478 0.465 0.299 5.92 2111 0.445 0.276 8.27 3199 0.663 0.114 -0.953 0.561 1.531 0.613 2507200-33 0.0346 0.225 0.76 0280 0.212 1.117 0.097: 6.658.- 0.203' 0.112 2:22 1024 0.090 0.118 -1,418 0.813 1:921; 0.455 25OT200.43 0.0451 0.293 1.00 0.366 0.275 1.118 0.126 0.657 0.288 0.163 3.21 1356 0.198 0.153 -1.413 0.810 1.918 0.457 250720054 0.0566 0.367 1.25 OA66 0.346 1.127 0.157. 0.654' 0.396 0.228- . 4.51 1692 0.371 0209 6.25 2563 0.392 .0:195 -1.4051- 0.806 - 1.917:_ 0.462 25OT200-68 0.0713 OA62 1.57 0.600 0.437 1.139 0.196 0.652 0.548 0.324 6.41 2111 0.517 0.296 8.86 3199 0.787 0.251 .1.396 0.800 1.916 0.469 35OT125-18 0.0188 0.113 0.38 0219 0.121 1.394 0.016 0.383 0.174 0.063 1.25 175- 0.013 0.038' -0.675 - 0.418 '1.595. .0.821 35OT125-27 0.0283 0.170 0.58 0.331 0.182 1.396 0.025 0.381 0.277 0.128 2.53 590 0.045 0.057 -0.670 0.416 1.595 0.823 350T125-30 0.0312 0.187 0.64 0.365 0200 1.396 0.027 0.380. 0.312 0.145 2.86 790 0.061 0.063 -0.669. 0.415 1.594 0'.824 3507125.33 0.0346 0.207 0.71 0.405 0.222 1.397 0.030 0.379 0.354 0.165 3.27 1024 0.083 0.070 -0.668 0.414 1.594 0.824 35OT12543 0.0451 0.270 0.92 0b28 0.288 1.397 0.038 0:377 6.490 _-' 0233 4.61 1739 0.183 0.090 -0.663 _.0:412 1.592 0.826 3507725.54 0.0566 0.339 1.15 0.668 0.361 1.404 0.048 0.375 0.651 0.317 6.26 2392 0.626 0.297 8.89 3372 0.362 0.114 -0.658 0.408 1.595 0.830 350T125-68 0.0713 0477 1.45 0.851 0.454 1.412 0.059 *0372 ` 0.851 0.433 8.55 2994 - 0.839 0.407 12.18 4536 > 0.7M 0.144. -0.650 0:403 1:599_ - 0.935 350TI50.27 0.0283 0.184 0.63 0.377 0.207 1.431 0.041 0.470 0.298 0.132 2.62 590 0.049 0.094 -0.869 0.529 1.739 0.750 3507150-30 0.0312 0.203• 0.69 OA16.0.228 1:432 0.045` -'-0.469' ,0.336; 0.150 2.96 ' ;790'-" 0066 ' -0:867 0.526,- 1.739. 0.751 350T75433 0.0346 0225 0.76 0.461 0153 1.432 0.049 0.469 0.382 0.171 3.39 1024 0.090 _0:103,: 0.114 -0.866 0.527 1.738 0.752 350T150-43 0.0451 0.293 1.00 0.601 0.328 1.433 0.064 0.467 0.531 0.243 4.80 1739 - 0.198 0:148 ' -0.861 0.525 1.736 0.754 350T150.54 0.0566 0.367 1.25 0.761 OAl2 1.440 0.079 0.465 0.712 0.332 6.57 2392 0.679 0.310 9.28 3372 0.392 0.187 -0.855 0.521 1.738 0.758 35OT15488 0.0713 0.462 157 0.972 0.518 1.450 0.099 0.462 0.957 0:459 9.07 2994 0.919 0:428. 12.61 4536 0.783 0238 -0.847 0S15 1.741. 0.763 35OT200.33 0.0346 0.259 0.88 0574 0.315 1.487 0.108 0.647 0.428 0.181 3.57 1024 0.103 0.249 1.285 0.761 2.069 0.614 3507200-03 0.0451 0.338 1.15 0.749 0.409 1.489 0.140 0.645 0.600 - 0.257 5.09 1739 0.229 0.323 -1280- 0.758 - 2.066.- 0.616 35OT200-54 0.0566 0.424 1.44 0.949 0.513 1.496 0.175 0.642 0.814 0.355 7.01 2392 0.770 0.329 9.85 3372 0.453 0.409 -1.273 0.754 2.067 0.621 3507200.68 0.0713 0.534 1.82 1.213 0.647 1.508 0.218 0.639 1.112 0.496 9.80 -2994 1.054 0.458 13.71 - 4536 0.904 OS22 -1164 0.749 2.069 0.626 362T125-18 0.0188 0.115 0.39 0.237 0.126 1.435 0.017 0.380 0.189 0.065 1.29 169 0.014 0.042 -0.665 0.413 1.627 0.833 362T125-27 0.0283 0.173 0.59 0.358 0.191 1.438 0.025 0.378 0.301 0.135 2.66 569 .0.046 0.062 -0.661 OA11 1.627 0.835 362T125-30 0.0312 0.191 0.65 0.795 0.210 1.438 0.027 0.378 0.339 0.152 3.01 762 0.062 0.068 -0.659 0.410 1.626 0.836 362T125-33 0.0346 0.212 0.72 0438 0.232 1.438 0.030 0.377 0.384 0.174 3.44 1024 0.085- 0.676 -0.658 0:409 1.626 0.836 3627125.43 0.0451 0.276 0.94 0,571 0.302 1.439 0.039 0.375 0.531 0.245 4.84 1739 0.187 0.098 -0.654 0.407 1.625 0.838 362T12554 0.0566 0.346 1.18 0.723 0.378 1.445 0.048 0.373 ' 0.705 0.332 6.57 2480 0.678 0.312 9.34 3372 0.369 0.123- -0.648. _ 0.404 1.627 0.841 362712558 0.0713 0.436 1.48 0.921 0.475 1.454 0.060 0.370 0.921 0.453 8.95 3104 0.907 0.427 12.78 4703 0.738 0.156 -0.641 0.399 1.631 0.846 3627150.27 0.0283 0.187 0.64 0.408 0.217 1.475 0.041 0.468 0.323 0:140 2.76 569 .. 0.050 0.102 -0.857 0.524 1.769 0.765 362T150-30 0.0312 0.207 0.70 0.449 0.239 1.475 0.045 0.467 0.364 0.158 3.12 762 0.067 0.112 -0.856 0.523 1.768 0.766 362T150-33 0.0346 0229 0.78 OA99 0.264 1.475' 0.050 0.467 0.414 0.160 3.56 1024 0.091 0.124 -0.854 0S22 1.767 0.766 362TI50-43 0.0451 0.298 1.02 0.650 0.343 1.476 0.064 0.465 0.574 0.255 5.04 1739 0.202 0.160 -0.650 0.519 1.766 0.768 362T15054 0.0566 0274 1.27 0.823 - 0.431 1.483 0.080 OA62 0.769 0.349 6.89 2480 0.735 0.325 9.74 3372 0.400 0.202 -0.844 0.516 1.768 0.772 362T150-68 0.0713' 0.471 1.60 1.050 0.542 1.492 0.099• 0.459 1.034 0.480 9.49 3104 0.993 0.449 13.43 4703 0.799 0.257 -0.836 0511 1.771 0.777 362T200-33 0.0346 0.264 0.90 0.619 0.328 1.532 0:110 0.645 0.464 0.190 3.76 1024 0.105 0.269 .1.270 0.754 2.092 0.631 362T200-43 0.0451 0.343 1.17 0.808 0.427 1.534 0.142 0.643 0.649 0.270 5.34 1739 0.233 0.350 .1.265 0.752 2.090 0.633 362T20054 0.0566 0431 1.47 1.024 0S36 1.541 0.177 0.640 0.879 0.372 7.35 2480 0.832 0.345 10.34 3372 0.460 0.442 -1.259 0.748 2.091 0.637 362T20058 0.0713 0.543 1.85 1.307 0.675 1.552 0.221 0.638 1.199 0.519 10.26 3104 1.138 0.480 14.37 4703 0.919 0.564 -1.250 0.743 2.093 0.643 400T125-18' 0.0188 0.122 0.41 0.297 0.144 1.560 0.017 0.374 0.241 0.072 1.42 153 - 0.014 0.052 -0.637 OA00 1.726 0.864 400T125-27 0.0283 0.184 0.63 0.449 0.217 1.562 0.025 0.372 0.380 0.156 3.08 515 0.049 0.078 -0.633 0.398 1.726 0.866 40OT125-30 0.0312 0.203 0.69 OA95 0.239 1562 0.028 0.371 - 0.427 0.176 3.49 689 0.066 0.085 -0.632 0.397 1126 0.866 40OT125-33 0.0346 0.225 0.76 0S49 0.265 1.563 0.031 0.371 0.484 0.201 3.97 940 0.090 0.095 -0.630 0.396 1.725 0.867 40OT12543 0.0451 0.293 1.00 0.716 0.344 1.563 - 0.040 0.369 " '.0.666 0.282 5.57 1739 0.198 0.122 -0.626 0.394' 1.724 0.668 400T125-54 0.0566 0.367 1.25 0.904 0.431 1.569 6.049 0.366 0.882 0.381 7.53 2739 0.849 0.359 10.74 3372 0.392 0.154 -0.621 0.390 1.727 0.871 40OT12558 0.0713 0.462 157 1.150 0S41 1,577 0.061 0.363- 1.150:..OZ17 _ 1022 3435 1.134 0.486' 14.62 5205 0.763 0:194 -0.614. 0.386 1.731 0.874 400T150-27 0.0283 0.198 0.67 0.509 0.246 1.602 0.042 0.461 0.409 0.154 3.04 515 0.053 0.127 -0.8240.509 1.860 0.804 400T150-30 0.0312 0.218 0.74 0.561 0.271 1.603 0.046 0.461 0.458 0.183 3.61 689 0.071 0.140 -0.823 0.508 1.859 0.604 400T150-33 0.0346 0.242 0.82 0.622 0.300 1.603 0.051 0.460 0.519 0.208 4.12 940 0.097 0.155 -0.821 0.507 1.8590.805 40OT150-43 0.0451 0.315 1.07 0.811 0.390 1.604 0.066 0.458- 0.719 0293 5.80 1759 0.214 0200 -0:817 - 0.504'1.69. 0.807 400T15054 0.0566 0.396 1.35 1.025 0.489 1.610 0.082 0.456 0.960 0.399 7.89 2739 0.918 0.374 11.19 3372 0.422 0.252 -0.811 0.501 1.860 0.810 ' Web -height to thickness ratio exceeds 200. Web stiffeners are required at all support points and concentrated loads. 2 Allowable moment includes cold work of forming. 0 m o 40 N et ID JI CRANDALL ENGINEERING 5448 Merrill Mill Road Mariposa, CA 95338 Phone: 209-966-4844 ) cnw � c- 0—, -- T; — SHEET Iff OF JOB NO. DATE: IS"=, V.... 4-f�vv __gip �--��. ��,-- ��� �-.-- 54� t -S Data: 03 Aug 2016 Job: SMUCKERS ELECTRICAL Subject: BASE RUNNER GIVEN: Base Material Type: Normal Weight Concrete Base Material Mechanical Properties: rc - 2000 psi Base Material Temperature: NA S Minimum Base Malarial Thickness ss = 30 inches Applied Tension Load per Anchor. Tappked = 350 th. Applied Shear Load per Anchor. Vapplied - 0 Ib. Anchor Spacing: Anchor Edge Distance: Sl = NA C1 = 3.8 inches S2= NA C2= NA S3= NA C3= NA S4 = NA C4 = NA S5= NA CRUICAL G3 ANCHOR CQ Mom 1-118k ,,,� Rs—Sa - —431 4� 4116), CALCULATIONS: OPTION 1 Proposed Anchor System = Tden HD Anchor Diameter (in.) or Rebar Size - 3/8 Embedment Depth = 2 ' inches Temperature Sensitivty actor ftemp - 1.00 Short -Term Load Adjus ent Factor for Seismic fseismWWnd = Tension: 1.00 Shear: 1.00 -Where permitted by cope Al owable Tension: T- 1075 Ib. Reduced Efficiency Based on Spacing ISI =1 as S1 NA I fS2-1 as S2 NA (S3 =1 es S3 = NA FS4 = 1 as S4 = NA fS5=1_S5=NA ((Bitot. = 1.000 x 1.000 x 1.000 x 1.000 x 1.000 - 1.000 i Reduced Efficiency Based on Edge/End Distance: 1C1 = 0.83 +1(1 - 0.83)x(3.8 - 1.75y(3. 1.75)) 01, fC1 - 1.000 fC2 = 1 as C2 = NA (C3 = 1 as C3 = NA (C4- 1 as C4 = NA I (fC)toL - 1.000 x 1.000 x 1.000 x 1.000 - 1.000 Tdesign Is equal to: Tdesign - 1075 x 1.000 x 1.000 x 1.00 x 1.00 - 10751b. >=Tappked, OK AAowable Shear: V - 1585 lb. Reduced Efficiency Based on Spacing: fS1=1 as SI NA fS2 = 1 as S2.= NA IS3 = 1 as S3 = NA IS4 = 1 as S4 = NA fS5 = 1 as S5 = NA (IS)tot. - 1.000 x 1.000 x 1.000 x 1.000 x 1.000 = 1.000 Reduced Efficiency Based on Edge/End Distance: (C1=0.25+1(1.0.25)x(3.8-1.75u(4.5-1.75)) m1, ICI- 0.8091 IC2 -1 as C2 = NA fC3 = 1 as C3 = NA fC4 = 1 ea C4 = NA (fC)tot. - 0.8091 x 1.000 x 1.000 x 1.000 - 0.8091 Allowable Shear Value for Design: Vdwlgn Is equal to: Vdeslgn - 1585 x 1.000 x 0.8091 x 1.00 x 1.00 - 1282 m. �Vapplied, OK Check Combined Tension & Shear Interaction: (Tapplied/Tdesign)4n+(VappliedNdesign)"n <or=1.0 (350/1075)"1.666667 + (011282)M.666667 =: 0.154087 < or - 1.0 OK Where n - 513 for CarbonlStamless Steel Wedge-AII, Tden HD and Carbon/Stainless Steel Drop -In anchors installed In Normal Weight Concrete only. Otherwise, a - 1 for a0 other cases. - Table Notes 1. Properties based on the AISI S100-07. 2. Hems and offset in flange of non-structural channel sections are ignored. 3. For deflection calculations, use effective Ixx. Effective Ixx is based on Procedure 1 of the AISI S100-07. 4. Effective properties are given as the minimum value for positive or negative bending. r 1 n J �Rrea ini ht Iblft. ��I m m 1n �;o�l� ' �4Sx i luta Ib 087F125.18 33 0.0188 0.070 0.239 0.009 0.356 0.0354 0.710 0.0086 0.0160 26.41 087F125-27 33 OA283 0.105 - 0.356 - 0.013 . 0.353 0,6528 0.710 .0.0131 - 0.0272 44:78 _ 087F125-30 33 0.0312 0.115 0.391 0.014 0.353 0.0580 0.710 0.0143 0.0307 50.47 087F125-33 33 6.0346.. , 0.127. 6.432 .' 0.016 • . 0:351- 0.0641.. 0.710.. ': - 0.0157 0.0337 55;43. ~69.17 087F125-43 33 0.0451 0.162 0S50 0.020 0.348 0.0817 0.711 0.0196 0.0420 150F125-18. 33::. 0A188:. d' :,:0.094 O:320 :'T '; .Y 0.031.: -0 575 .,•. 00467 0.705,' ..'- 00299:• _. ,' 00344 _:a _°-'56.59_. 15OF125-27 33 0.0283 0.140 0.477 0.046 0.572 0.0697 0.705 0.0459 0.0569 93.74 150F125J0 33 0.0312;, 0;154; , ;_ 0525:,' 0.050 - -^ 0.571 - OD767 " 0:705: 00503 1 _ 00639 - 15OF125.33_ _- . 33- -_ . - 0.0346_ _ ..0.171 _ . _ 0,581 _._ _ . 0.055_ .- - - 0.570 .. _ - _0.0648-_ _ _ _ 0,705 _ 00554_ 0.0704 - _115.92 15OF125-43 33 - 6A451 0.219. •. 0.745 0.010 --'0.565 0.1087 -0:705 �. 0.0699 ' ' . ' .-0:0888 --_ .146.25 . r=VA7 Copyright O 2011 by the Steel Stud Manufacturers Association CRANDALL ENGINEERING SHEET 'ZZ OF 5448 Merrill Mill Road JOB NO. �e �Z►� Mariposa, CA 95338 / Phone: 209-966-4844 DATE: J ` f �� ��_ �.-gip -�� ��..`Y•.� V101I.Db = L- o ve = Iof0' - z3 G 2� ��- ESR -2089 I Most Widely Accepted and Trusted Page 8 of 46 Table 1.013 Hardy Frame® HFX/S-Series - Dimensions & Connectors Model Number Net Height (in) Width (in) Depth (In) HD Dla' (In) Top Screw Qty x' (ea) HFX/S-9)8 96 5/8 9 3 12 11/8 _ 5 HFX/S-12x8 12 6 HFX/S-15x8 15 8 HFX/S-1 &(8 18 12 HFX/S-21x8 21 18 HFX/S-24x8 24 22 HFX/S-32x8 32 7/f HFX/S44u8 44 16 HFX/S-12x9 1085/8 12 31/2 1 1/8 HFX/S-15x9 15 8 HFX/S-18x9 18 12 HFX/S-21x9 21 16 HFX/S-24x9 24 20 HFX/S-32x9 32 Ire 9 HFX/S-44x9 44 14 HFX/S-12x10 _ . 1205/8 _ .. 12 31/2 1 1/8 _ _ _ _ _ _ _ _ 6 HFX/S-15x10 15 8 HFX/S-18x10 18 10 HFX/S-21x10 21 14 HFX/S-24x10 24 18 HFXS-32x10 32 7/8 9 HFXS-44x10 44 12 HFXS-15x11 132 5/8 15 3 12 1 1/8 6 HFXS-18x11 18 10 HFXS-21x11 21 14 HFXS-24x11 24 16 HFXS-32x11 32 75 8 HFXS-44x11 44 11 HFXS-15x12 1445/8 15 31/2 1 1/8 6 HFXS-18x12 18 10 HFXS-21x12 21 12 HFXS-24x12 24 16 HFX/S-32x12 32 7/8 7 HFXS-44x12 44 11 HFXS-1503 1565/8 15 31/2 11/8 6 HFXS-18x13 18 10 HFXS-21x13 21 12 HFXS-24x13 24 14 HFXS-32(13 32 7/8 7 HFXS-44x13 44 11 For 51: 1 inch = 25.4 nYn, 1 Ibf = 4.45 N Notes 1) Hold Down rods can be Standard (STD) or High Strength (HS). STD indicates bolts complying with ASTM F1554 Grade 36. HS indicates bots complying with a high strength steel specification as set forth in Section 3.7.4 of this Report 2) The No. 14 metal screws nest be self -drilling tapping screwswith a minimum ASD design lateral load 302 bs excluding any duration of toad increase and is based on a connection consisting of a minimum 0.105 inch (No. 12 gage) base metal thickness steel in contact with Ila and a minimum 0.048 hch (Ne. 1 a gage) base metal thickness steel not in contact with the screw head. Screws must be referenced h a current ICC -ES Evaluation Rep and comply, with the requirements in Section 3.4.2 of this Report. ire ESR -2089 I Most Widely Accepted and Trusted Page 26 of 46 Table 2.1A Hardy Frame° HFX/S Installation - on 2500 psi Concrete''2 Net Seismic Wind Model Number Helght H HD Bolt Dia (in) Applied Axial Allowable In- Drill at U IIR at Allowable In- Drill at U IIR at (In) and Grade Load Plana Shear y e (lbs) V p. (lbs) Plane ee/Shear V ° flat) V P6 (lbs) HFX/S-W 965/8 1 1/8" STD 2,000 0.213 19,595 0 1,000 17,005 0 1 1/8" STD 3,500 6,500 HFX/S-12x8 965/8 0 0.198 1,000 3,500 0.177 14,3205 1 1/8" HS 0.330 21,615 ,45 6,500 21,380 1,900 0.320 1,000 2,305 0.388 1 1/8" STD 3,500 HFX/S-15x896 5/8 1,955 6,500 21,625 1,000 0.218 21,615 1 1/8" HS 3,500 21,615 2,625 0.218 6,500 3,570 0.298 39,500 1,000 0.283 33,70D 1 1/8" STD 3,500 6,500 HFX/S-111x8 96 518 21,090 ..---3,210..- 1,000 3,210 0.269 1 1/8" HS 3,500 0.423 43,265 4,875 6,500 41,070 4,595 0.391 1,000 3.420 0.151 --1.1/8"STD --- --3:500-- HFX/S-21x8 965/8 3,420 6,500 18,010 1,000 0.263 38,175 1 1/8" HS 3,500 6,500 5,910 0.263 38,175 2,265 0.133 8,540 1,000 0.126 8,130 1 1/8" STD 3,500 6,500 HFX/S-24x8 965/8 11,295 2,335 1,000 8,795 1,540 1 1/8" HS 3,500 6,500 0.090 7,270 2,816 0.090 7,270 2,080 1,000 5,365 4,510 7/8" STD 3,500 6,500 HFX/S-32(8 965/8 2,380 0.076 1,000 1,255 0.238 718" HS 3,500 6,500 17,005 1,035 0.196 14,325 1,255 0.240 1,400 . 1,155 0.221 7/8" STD 3,500 HFX/S-44x8 965/8 1,740 6,500 21,615 1,000_ 0.378 21,380 7/8" HS 3 500 20,560 2,050 0.449 6,500 1,920 0.421 26,150 1,000 0.381 21,625 1 1/8" STD 3,500 6,500 HFX/S-12)c9 1085/8 21,620 2,335 1,000 21,620 3,175 1 1/8" HS 3,500 3,015 0.318 33,700 6,500 0.295 28,745 2,925 1,000 21,545 2,915 1 1/8" STD 3,500 6,500 HFX/S-15x9 1085/8 4,305 0.475 1,000 4,305 0.475 1 1/8" HS 3,500 0.451 36,045 3,140 6,500 18,710 3,140 0.175 1,000 3,500 0.175 18,710 1 1/8" STD HFX/5-18:19 1085/8 5,230 6,500 1 37,830 1,000 0.294 1 37,830 1 1/8" HS 3,500 6,500 1,000 1 1/8" STD 3,500 6,500 HFX/S-21x9 108 5/8 1,000 3,500 1 1/8" HS 6,500 1,000 3,500 1 1/8" STD 6,500 HFX/S-24x9 108 518 1,000 1 1/8" HS 3,500 6,500 770 0.258 15,510 0 0.213 19,595 0 0.197 17,005 0 0.176 14,320 P770 0 0.214 19,595 0 0.198 17005 0 0.177 14,3205 1,955 0.330 21,615 ,45 0.327 21,380 1,900 0.320 20,560 2,305 0.388 31,340 2,160 0.364 26,150 1,955 0.330 21,625 2,625 0.218 21,615 2625 0.218 21,615 2,625 0.218 21,615 3,570 0.298 39,500 3,385 0.283 33,70D 3,135 0.262 28,745 3,210 0.272 21,090 ..---3,210..- - 0.-276---- 29.505-- 3,210 0.269 20,840 4,970 0.423 43,265 4,875 0.415 41,070 4,595 0.391 36,045 3.420 0.151 18,010 3,420 0.151 18,010 3,420 0.151 18,010 5,910 0.263 38,175 5,910 0.263 38,175 5,910 0.263 38,175 2,265 0.133 8,540 2,160 0.126 8,130 1,360 0.080 5,130 3,000 0.176 11,295 2,335 0.137 8,795 1,540 0.090 5,795 5 0.090 7,270 2,816 0.090 7,270 2,080 0.066 5,365 4,510 0.144 11,645 3,545 0.113 9,145 2,380 0.076 6,145 1,255 0.238 19,595 1,155 0.220 17,005 1,035 0.196 14,325 1,255 0.240 19,595 1,155 0.221 17,005 1,035 0.198 14,325 1,740 0.381 21,615 1,730 0.378 21,380 1,690 0.370 20,560 2,050 0.449 31,340 1,920 0.421 26,150 1,740 0.381 21,625 2,335 0.246 21,615 2,335 0.246 21,620 2,335 0.246 21,620 3,175 0.335 39,500 3,015 0.318 33,700 2,790 0.295 28,745 2,925 0.319 21,545 2,915 0.318 21,435 2,905 0.317 21,345 4,305 0.475 401285 4,305 0.475 40,285 4,085 0.451 36,045 3,140 0.175 18,710 3,140 0.175 18,710 3,140 0.175 18,710 5,230 0.294 37,830 5,230 0.294 1 37,830 5,230 0.294 1 37,830 770 0.258 15,510 1,410 0.213 19,595 1,300 0.197 17,005 1,160 0.176 14,320 1,410 0.214 19,595 1,300 0.198 17,005 1,160 0.177 14,320 1,955 0.327 21,615 1,945 0.325 21,380 1,900 1 0.318 20,560 0,388 31,340 0.364 26,150 0.330 21,625 02.,625 0.218 21,615 0.218 21,615 0.218 21,615 0.299 39,500 0.284 33,700 3,135 0.263 28.745 3,210 0.272 21,090 --3-210--- --0:276- - 21-505--- 3,210 0.269 20,840 5,030 0.428 44,825 4,875 0.415 41,070 4,595 0.391 36,045 3,730 0.165 20,005 730 0.168 20,465 730 0.171 20,890 450 0.288 45,290 360 0.284 43,925 210 N2.825 0.277 41,850 0.165 10,630 160 0.126 8,130 360 0.080 5,130 ,000 0.176 11,295 2,335 0.137 8,795 1,540 0.090 5,795 0.117 9,440 3 240 0.103 8,365 2,080 0.066 5,365 4,510 0.144 11,645 3,545 0.113 9,145 2,380 0.076 6,145 1,255 0.238 19,595 1,155 0.220 17,005 1,035 0.196 14,325 1,255 0.240 19,595 1,155 0.221 17,005 1.035 0.197 14,325 1,740 0.379 21,615 1,730 0.376 21,380 1,690 0.367 20,560 2,050 0.449 31,340 1,920 0.421 26,150 1,740 0.381 21,625 2,335 0.246 21,615 2,335 ,6203,175 ,5003,015 ,7002,790 M0.24621,620,6202,335 ,7452,925 5452,915 ,4352,905 ,345 4,475 0.494 44,825 4,340 0.479 41,070 4,085 0.451 36,045 3,385 0.191 20,745 3,385 0.195 21,245 3,385 0.189 20,500 5,775 0.325 45,935 5,675 0.319 44,165 5,525 1 0.311 41,850 .� • ,}, CRANDALL ENGINEERING 5448 Merrill Mill Road Mariposa, CA 95338 Phone: 209-966-4844 X� 1 SHEET 7 OF JOB NO. I (OO�ia- DATE: �1Gs91 LO, 7� 1 7f - �--Vie._.,. z@ CC, ` ®' Anchor Designer Company: CRANDALL ENGINEERING Date: 8/42016 Software Engineer. JAC Page:1/4 Project SMUCKERS ELECT - Version 2.3.5555.4 - ® Address: 5448 MERRILL MILL ROAD - Phone: 209-9664844 " - `- — E-mail: and @mndallengineedng.com 1I.Proloct Information Customer company: NVBS Project desuip0on: HARDIFRAME ANCHORS Customer contact name: BIN . Location: BUTTE CO, CA Customer e-ma0: _ Fastening description: Comment - - 2. Input Data B Anchor Parameters Gonoral - Baso Material Design method:ACI 318-11 Concrete: NomiW-eight . Units: Imperial units Concrete thickness, h (Inch): 30.00 State: Cracked Anchor Information: Compressive strength, r. (psi): 2500 Anchor type: Cast -in-place - `pkv: 1.0 Material: AB - - Reinforcement condition: A tension, A sheer Diameter Qnc): 0.875 Supplemental reinforcement: Not applicable Effective Embedment depth. he (inti: 12.000 Do not evaluate concrete breakout in tension: No Anchor category - Do not evaluele concrete breakout in shear. No Anchor ductility: Yes Ignore Edo requirement: No It : (inch): 14.25 Build-up grout part: No C— Qnch): 5.25 Sr, Qnct): 5.25 1 L., Load and Geometry Load faces source: ACI 318 Appendix C , \' Load combination: not set Seismic design: Yes Anchors subjected to sustained tension: Not applicable Ductility aedion for tension: not satisfied - DuWllty section for shear. not satisfied Ds factor: not set Z Appy dome shear Io; Anchors only resistin ,Figure 1> Input dere and rosuha must be checked for agreement with the adding cirwmntances, the standards and guidelines must be Necked for plausibility. Simpemi Stro ,O-Tte Company Inc. 5956 W. Loa Positaa 8W -1d Pte—cast, CA 94588 Ph— 925.560.9000 Fox: 925.847.3071 w 51 onglio.rom -Figure 2> Anchor Designer— Software Verslnn 2.3.5555.4 t 1 Recommended Anchor Anchor Name: PAB Pre -Assembled Anchor Bolt- PAB7 (718'8) Input data and msu04 must be chocked to Shcpsan Shnrhs`Ta Company Inc. 5859 W. Las ) existing drormstanres, the standards and gulden— must be checked for pleuslbillty. Ploeramon, CA 94588 Phone: 825.560.9000 Fac 925.1147.3971 a -v akongao.cmn TV Anchor DesignerTm CosAC CRANDALL E Software Engineer. : Project: SM: SMUCKERS 1 Version 2.3.5555.4 o Address: 5448 MERRIL Phone: 209-966-4844 3. Resulting Anchor Forces Anchor Tension load, Shear load x. Shear load y, Shear load combined, N,.. (b) V,,., (b) V.n (lo) 4(V...)1 -(V .)' (Ib) 1 11177.0 0.0 0.0 0.0 Sum 11177.0 0.0 0.0 0.0 Maximum concrete compression strain (%.): 0.00 Maximum concrete compression stress (psi): 0 Resultant tension force (Ib): 11177 Resultant compression force Ole): 0 Eccenbidty of resultant tension forces in x-axis, e'm (incl): 0.00 Eccentridy al resultant tension forces in yaxis, e'rm Cinch): 0.00 4. Stool Strenmh of Anchor in Tension(Soc. 0.5.11 N. @) 0 ON- (Ib) 26795 0.80 21435 S. Concrete Breakout Strenath of Anchor in Tension (Sec. D.5.21 Nn = 16.i.JPdhd° (Eq. D-7) .L r. (psi) hr On) N. (Ib) 1.00 2500 12.000 50318 0.750Nm - 0.750 (Am/A-) 944n vert w N. (Sec. D.4.1 8 Eq. D-3) A. (in-) A- Cnr Y e K. y'9,, N. (b) 0 0.750Nm (b) 649.19 1296.00 0.833 1.00 1.000 50318 0.85 13390 6. Pullout Strength of Anchor in Tension ISec. 0.5.31 0.75ONm = 0.75Ow vNo = 0.750P AAe f, (Sec. 0.4.1. Eq. D-13 & 0-14) W, A� (Inr) P. (psi) 0 0.750Na. (Ib) 1.0 4.46 2500 0.75 50189 Input date and resuhs mug be Nedtod far egroomenl with the existing drournwim es, the Vendems end guldellnes mug be Necked for plaugbtiity. 6lmpson 61-9-T,v Company 1- 5956 W. Les Poglas Boulevard! Pleasanton, CA 94588 Phone: 925.560.8800 Far. 925.847.3871 vnv Wongtie.conl t f Anchor Designer1m Software t 1 = Version 2.3.5555.4 r I 11, Reaults Tension Factored Load, N.. (Ib) Design Strength. oN. (Ib) Rego Status Steel 11177 1 21436 0.52 Pass Concrete breakout 11177 13390 0.83 Pass (Governs) Pullout 11177 50189 0.22 Pass I' PAB7 (718"0) with her= 12.000 Inch meets the selected design criteria. 12. Weminas i Bdtde failure govems for tension. Governing anchor (allure mode is bridle failure. Attachment shell be designed to satisfy the requirements of ACI 318-11 Section D.3.3.4.3 for structures assigned to Seismic Design Category C. D, E, or F when be component of the strength level earthquake force applied to anchors exceeds 20 percent of the total (adored anchor (orae associated with the same load combination. In case when ACI 313.11 Sections 0.3.3.4.3 (a)3 to 6,(b), (c), on (d) Is satisfied for tendon loading. select appropriate checkbox from Inputs tab to disable this message. Altemativey. DO factor can be entered to satisfy ACI 318-11 Section 0.3.3.4.3(d) to increase the earthquake portion of the loads as squired. - Designer must exercise own judgement to determine if thu design is suitable. Input date Ond Mulls mug be Narked far agreement with the existing dicumetsnees, the gandanls end guldegrim mug be Nck ood for plausibility. Oro- SbcngT:mnc. e C.:npy I 5956 W. Lu Pegtas Bod-aro Pleaesmon, CA 94588 Phone: 925.560.9000 Fax: 925.947.3871 www.rlrcngtio.rarn 1 <Figure 1> 21, Input data and Metals mug be che Med for agreement with the existing drounuu c- , the Standards and gulde in -s mug be chocked for plaudd8ty. Shapson St-ig-T-u Cuapm y IM. 5956 W. Las Pesiles Bmdevord Pieasartm, CA 94598 Phone: 925.560.8000 Fax 925.847.3871—strongtia.com Recommended Anchor j Anchor Name: PAB Pre -Assembled Anchor Bolt- PAB7 (7/6'0) I f Input data and results rtwSt be checked for agree.-. with me eW Ung drpr.gmces, the Standards and guidelines mug be thm"d res Plausibility. 6imraah SOahpT�a Cwlhpmy IM. 5956 W. Les for, asul.w. Pleasanton. CA 94588 Phone: 925.560.9000 Fax 925.947.3871—shongUe.com i "Co Anchor Designer"m EINGINEERING Pe9ee. an . CRANDALL EINGINEERING Date: 6/4/2016 � Anchor DBSlgnefTM Engineer. JAC Pa e: 114 Engineer. JARCANDALL 42016 _ .. r t ? Software Project: SMUCKERS ELECT � a r c Software I Project: SMUCKERS ELECT - - - - Version 2.3.5555.4 Address: 5448 MERRILL MILL ROAD - - . a Version 2.3.5555.4 Address: 5448 MERRILL MILL ROAD e Phone: 209-986844 I Phone: 209-966-0844 - - - E-mail: end Qtxandallengineering.cont �---� E+neil: and Qcrandallen ineerin .cam 1.Pralect Information —__--�---^-_--- - -Figure 2> Customer company: NVBS Project description: HARDIFRAME ANCHORS Customer contact name: BW Laced— BUTTE CO. CA 'r. Customer—all: - - Fastening description: - l Comment 2. Input Data A Anchor Parameters General - Base Material Design meWod:ACl 318-11 Comtrele: Normal -weight Units: Imperial units Concrete thickness, It (incl): 30.00 Slate: Cracked Anchor Information: .Compressive strength, P. (psi): 3000�� Anchor type: Cast -in-place "": 1.0 Material: AB �� Reinforcement condition: A tension, A shear��+ Diameter (in 0.875 Supplemental reinforcement: Not applicable Effective Embedment depth, hr (in :12.000 Anchor category: - Do not evaluate cancrele breakout In tension: No Do not evaluate concrete breakout in shear. Naj. I P 9^4 Anchor ductility: Yes Ignore ado requirement Yes h„a, (Inch): 14.25 - Build-up grout pad: Norig, to , C,m (Inch): 1.63 S„w (inch): 3.50 Load and Geometry Load factor source: ACI 316 Appendix C it }' Load combination: not set '-•- Seismic design: Yes ja r;4 Anchors subjected to sustained tension: Not applicable Ductility section for Tension: not satisfied Ducdiity section for shear. not satisfiedI Z ! 9 fw lr,l• II4 factor: nal set Apply entire shear load at front raw: No Anchors only resisting wind andlor seismic loads: Yes 0 Ib l t I <Figure 1> 21, Input data and Metals mug be che Med for agreement with the existing drounuu c- , the Standards and gulde in -s mug be chocked for plaudd8ty. Shapson St-ig-T-u Cuapm y IM. 5956 W. Las Pesiles Bmdevord Pieasartm, CA 94598 Phone: 925.560.8000 Fax 925.847.3871—strongtia.com Recommended Anchor j Anchor Name: PAB Pre -Assembled Anchor Bolt- PAB7 (7/6'0) I f Input data and results rtwSt be checked for agree.-. with me eW Ung drpr.gmces, the Standards and guidelines mug be thm"d res Plausibility. 6imraah SOahpT�a Cwlhpmy IM. 5956 W. Les for, asul.w. Pleasanton. CA 94588 Phone: 925.560.9000 Fax 925.947.3871—shongUe.com ®' Anchor DesignerTm Software s Version 2.3.5555.4 Company: CRANDAIL EINGINEERING I Date: 8/412016 Engineer. JAC Page: 1314 Project: SMUCKERS ELECT Address: 5448 MERRILL MILL ROAD Phone: 209.966.4844 Email_ _ Jend_ crandallengineering.cont 3. Resulting Anchor Forces Anclar Tension load, Shear load x. Shear load y. Shear load combined, NW (lb) V- M) v.., (to) 4(V_)4(Vu..)' (lo) 1 0.0 2164.0 0.0 2164.0 Sum 0.0 2164.0 0.0 2164.0 Maximum concrete compression strain (96): 0.00 Maximum concrete compression stress (psi): 0 Resultant tension force Qb): 0 ResuUsnt compression force Qb): 0 EccenWdty of resultant tension forces in x-axis, em (inch): 0.00 Eccentricity of resultant tension forces m y-axis. e',, (inch): 0.00 cen Ectricity of raw lard shear forces In x-axis, e'w (inch): 0.00 Eccentricity of resultant shear forces in y-axis, e'v. (inch): 0.00 8. Steel Strang of Anchor in Shear ISec. 13.6.11 V.. (lo) Ie=. 0 "OV.. (Ib) 16080 1.0 0.75 12060 S. Concrete Breakout Stron!h of Anchor In Shear (Sec. D.6.21 Shear perpendicular to edge in x -direction: V.. = min17(I./d.)'-4d.A.VJ` .....: 9A.Jr.c.h'-'I (Eq. D-33 8 Eq. D-34) V4r (to) 4 (in) d. (in) A. r. (psi) c.h (in) Ve. (lb) 7.00 0.88 1.00 3000 20.00 44091 OV- =0 (A.1 A-) (Sec 0.4.1 8 Eq. D-30) Ver (th) 0 OVm. (Ib) A. Qn') A- (In') W- Ysv Y>v V. (Ib) 0 OVm. (Ib) 384.00 1600.00 0.738 1.000 1.000 44091 0.85 5900 Shear parallel to edge In x -direction: V.r = min17(1./d.)'4d.A.4rx.i -5; 9 .Jf.c.i '1(Eq. D-33 8 Eq. 634) 1. (in) d. (in) A. r. (psi) u, (in) V4r (to) 7.00 0.88 1.00 3000 3.80 3652 OVm=0(2)(Aw/A-)1F i,VSvKWv (Sec. D.4.18 Eq. 0.30) A. CO) Aw Qn') YL4v Y4v Y'nv Ver (th) 0 OVm. (Ib) 64.98 64.98 1.000 1.000 1.000 3652 0.85 6208 10, Concrete Prvout Strength of Anchor In Shear (Sec. D.6.31 OV, • 01,.N. - Okm(As. / Ae.,,)Y:ye yhx Yy.,xN. (Eq. 0.4n) Iry Ax. (in') Ams Qn2) P.- Y<a Y1xx Nn (Ib) 0 011m (Ib) 2.0 488.80 1296.00 0.763 1.000 1.000 55121 0.75 23804 11. Results Interaction of Tensile and Shear Forces (Sec. 0.71 Shear Factored Load, V. (Ib) Design Strength. eV. Qb) Ratio Status Steel 2164 12060 0.18 Pass Input data end rasude must be Nedwd for egr---N adlh the edsOng d,cianKenwe, the elandaNs and Bhddellnas mud be Necked for plausibility. Shnpsun Shwhg-Ta Cwnpwhy Im 5956 W. Las Posims Boulevard Rosman, CA 94589 Phone: 925.560.9000 Fax: 925.647.3871 v stsong0e.cam i Anchor Design Software Version 2.3.5555.4 T Concrete breakout x+ 2164 11 Concrete breakout y- 2164 Pryout 2164 MILL ROAD I E-mail: 1 andy@cranda0enginewing.com I 5900 0.37 Pass (Governs) 6208 0.35 Pass (Governs) 23604 0.09 Pass PAB7 (7/8"121) with her= 12.000 Inch meets the selected design criteria. 12. Warnings - Minimum spacing and edge distance requirement of 6da per ACI 318 Sections D.B.1 and D.8.2 fair torqued castin-place anchor is waived per designer option. Brittle failure govems for shear. Governing anchor failure made Is brittle failure. Attachment shag be designed to satisfy the requirements of ACI 318.11 Section D.3.3.5.3 for structures assigned to Seismic Design Category C. D. E. or F when the component of the strength level earthquake force applied to anchors exceeds 20 percent lof the total factored anchor force associated with the same load combination. In was when ACI 31 &11 Sections 0.3.3.5.3(x), (b) or (c) Is satisfied for shear loading, select appropriate cleccbox from Inputs tab to disable this message. Alternatively, 00 factor can be entered to satisfy ACI 31 &11 Section D.3.3.5.3tc) to increase the earthquake portion of the loads as required. - Designer must exercise own judgement to determine if this design Is suitable I Input deta end rends must be d rocked fo tagrearrerd Wlh the i drting dramhdmms, the stendards and guido0nse mug be checked for plausibility. 6hnpum ShxrhSTn Canpery Inc. 5956 W. Les Posltes Bodeverd Reaeardon. CA 94588 Phone: 825.560.9000 Fex: 925.847.3871 nwa.dhong9o.can 1 I CRANDALL ENGINEERING SHEETtf� OF 5448 Merrill Mill Road JOB NO. Mariposa, CA 95338 Phone: 209-966-4844 DATE: A6 'tip AA 1-5 .. . .........