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PAGE NO. 1 **************************************************** * * * STAAD.Pro * * Version 2006 Bld 1002.US * * Proprietary Program of * * Research Engineers, Intl. * * Date= F EB 6, 2011 * * Time= 11:27: 2 * * * * USER ID: ME * **************************************************** 1. STAAD SPACE DXF IMPORT OF TOWER.DXF INPUT FILE: Jhapa DD HT 132KVA line.STD 2. START JOB INFORMATION 3. JOB NAME DD TYPE 132KVA HT TRANSMISSION LINE 4. JOB CLIENT  MUDBURY AND JOSHI CO. 5. JOB NO 1 6. JOB REV 1 7. JOB PART 1 8. JOB COMMENT 132KVA HT TRANSMISSION LINE TO JHAPA SUBSTATION  9. ENGINEER NAME PRAKASH 10. ENGI NEER DATE 23 -JAN-11 11. END JOB INFORMATION 12. INPUT WIDTH 79 13. UNIT METER KN 14. JOINT COORDINATES 15. 79 0.25 1.46875 6.3125; 80 1.625 1.46875 6.3125; 81 1.5 7.85938 5.07813 16. 82 5.0625 7.85938 5.07813; 83 2.0625 10.7969 4.51563; 84 4.5 10.7969 4.51563 17. 85 2.4375 20.4688 4.14063; 86 4.125 20.4688 4.14063; 87 2.4375 16 .9688 4.14063 18. 88 4.125 16.9688 4.14063; 89 2.4375 13.4688 4.14063; 90 4.125 13.4688 4.14063 19. 91 0.8125 0.734375 6.45313; 92 0.125 0.734375 6.45313 20. 93 0.375 2.20313 6.17188; 94 1.9375 3.92188 5.84375; 95 0.75 3.92188 5.84375 21. 96 0.9375 4.90625 5.65625; 97 2.5625 10.2813 4.625; 98 1.9375 10.2813 4.625 22. 99 2.5625 8.92188 4.875; 100 1.8125 9.60938 4.75; 101 2.75 11.1094 4.45313 23. 102 2.1875 11.3438 4.42188; 103 2.75 11.5625 4.375; 104 1.6875 8.92188 4.875 24. 105 2.125 8.5 4.96875; 106 2.875 12.125 4.26563; 107 2.375 12.3281 4.21875 25. 108 2.875 12.5313 4.1875; 109 3.8125 11.1094 4.45313 26. 110 4.375 11.3438 4.42188; 111 3.8125 11.5625 4.375; 112 3.6875 12.125 4.26563 27. 113 4.1875 12.3281 4.21875; 11 4 3.6875 12.5313 4.1875 28. 115 4.125 12.7656 4.14063; 116 2.4375 12.7656 4.14063 29. 117 4.125 16.2656 4.14063; 118 2.4375 16.2656 4.14063 30. 119 4.125 19.7656 4.14063; 120 2.4375 19.7656 4.14063 31. 121 2.4375 14.8594 4.14063; 122 4.125 14.8594 4.14063 32. 123 2.4375 18.3594 4.14063; 124 4.125 18.3594 4.14063 33. 125 2.4375 2.20313 6.17188; 126 0.5625 2.95313 6.03125 34. 127 2.4375 2.95313 6.03125; 128 3.0625 25.5625 3.5; 129 3.5 25.5625 3.5 35. 130 4.0625 21 .1563 4.04688; 131 2.625 21.8438 3.96875; 132 3.875 22.5313 3.875 36. 133 2.8125 23.2344 3.79687; 134 3.6875 23.9219 3.70312 37. 135 2.9375 24.6094 3.60937; 136 3.625 24.6094 3.60937 38. 137 2.8 75 23.92 19 3.70 312; 138 3. 75 23.23 44 3.796 87; 139 2.6 875 22.5 313 3.87 5 39. 140 3.9375 21.8438 3.96875; 141 2.5 21.1563 4.04688; 142 6.3125 1.46875 6.3125 40. 143 4.9375 1.46875 6.3125; 144 5.75 0.734375 6.45313 41. 145 6.4375 0.734375 6.45313; 146 6.125 2.20313 6.17188 42. 147 4.125 2.2 0313 6.17188; 148 6 2.95313 6.03125 ; 149 4.125 2.9531 3 6.03125 43. 150 4.625 3.92188 5.84375; 151 5.8125 3.92188 5.84375 44. 152 5.625 4.90625 5.65625; 153 4.1875 7.23438 5.20313 45. 154 4.1875 5.9375 5.45313; 155 5.3125 6.57813 5.32813; 156 5.5 5.5 5.53125 46. 157 5.25 5.15625 5.60938; 158 5.1875 7.23438 5.20313 47. 159 5.4375 5.9375 5.45313; 160 4.8125 5.5 5.53125; 163 0 0 6.59375 48. 164 3.25 2.95313 6.03125; 165 6.5625 0 6.59375; 166 3.25 4.90625 5.65625 49. 167 4 10.2813 4.625; 168 4.625 10. 2813 4.625; 169 4 8.92188 4.875 50. 170 4.75 9.60938 4.75; 171 4.875 8.92188 4.875; 172 4.4375 8.5 4.96875 51. 173 2.375 7.23438 5.20313; 174 2.375 5.9375 5.45313; 175 1.25 6.57813 5.32813

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PAGE NO. 1

***************************************************** ** STAAD.Pro ** Version 2006 Bld 1002.US ** Proprietary Program of ** Research Engineers, Intl. ** Date= F EB 6, 2011 *

* Time= 11:27: 2 ** ** USER ID: ME *****************************************************

1. STAAD SPACE DXF IMPORT OF TOWER.DXFINPUT FILE: Jhapa DD HT 132KVA line.STD

2. START JOB INFORMATION3. JOB NAME DD TYPE 132KVA HT TRANSMISSION LINE4. JOB CLIENT MUDBURY AND JOSHI CO.5. JOB NO 16. JOB REV 17. JOB PART 18. JOB COMMENT 132KVA HT TRANSMISSION LINE TO JHAPA SUBSTATION  9. ENGINEER NAME PRAKASH10. ENGINEER DATE 23-JAN-11

11. END JOB INFORMATION12. INPUT WIDTH 7913. UNIT METER KN14. JOINT COORDINATES15. 79 0.25 1.46875 6.3125; 80 1.625 1.46875 6.3125; 81 1.5 7.85938 5.0781316. 82 5.0625 7.85938 5.07813; 83 2.0625 10.7969 4.51563; 84 4.5 10.7969 4.5156317. 85 2.4375 20.4688 4.14063; 86 4.125 20.4688 4.14063; 87 2.4375 16 .9688 4.1406318. 88 4.125 16.9688 4.14063; 89 2.4375 13.4688 4.14063; 90 4.125 13.4688 4.1406319. 91 0.8125 0.734375 6.45313; 92 0.125 0.734375 6.4531320. 93 0.375 2.20313 6.17188; 94 1.9375 3.92188 5.84375; 95 0.75 3.92188 5.8437521. 96 0.9375 4.90625 5.65625; 97 2.5625 10.2813 4.625; 98 1.9375 10.2813 4.62522. 99 2.5625 8.92188 4.875; 100 1.8125 9.60938 4.75; 101 2.75 11.1094 4.4531323. 102 2.1875 11.3438 4.42188; 103 2.75 11.5625 4.375; 104 1.6875 8.92188 4.87524. 105 2.125 8.5 4.96875; 106 2.875 12.125 4.26563; 107 2.375 12.3281 4.21875

25. 108 2.875 12.5313 4.1875; 109 3.8125 11.1094 4.4531326. 110 4.375 11.3438 4.42188; 111 3.8125 11.5625 4.375; 112 3.6875 12.125 4.2656327. 113 4.1875 12.3281 4.21875; 11 4 3.6875 12.5313 4.187528. 115 4.125 12.7656 4.14063; 116 2.4375 12.7656 4.1406329. 117 4.125 16.2656 4.14063; 118 2.4375 16.2656 4.1406330. 119 4.125 19.7656 4.14063; 120 2.4375 19.7656 4.1406331. 121 2.4375 14.8594 4.14063; 122 4.125 14.8594 4.1406332. 123 2.4375 18.3594 4.14063; 124 4.125 18.3594 4.1406333. 125 2.4375 2.20313 6.17188; 126 0.5625 2.95313 6.0312534. 127 2.4375 2.95313 6.03125; 128 3.0625 25.5625 3.5; 129 3.5 25.5625 3.535. 130 4.0625 21.1563 4.04688; 131 2.625 21.8438 3.96875; 132 3.875 22.5313 3.87536. 133 2.8125 23.2344 3.79687; 134 3.6875 23.9219 3.7031237. 135 2.9375 24.6094 3.60937; 136 3.625 24.6094 3.6093738. 137 2.875 23.9219 3.70312; 138 3.75 23.2344 3.79687; 139 2.6875 22.5313 3.875

39. 140 3.9375 21.8438 3.96875; 141 2.5 21.1563 4.04688; 142 6.3125 1.46875 6.312540. 143 4.9375 1.46875 6.3125; 144 5.75 0.734375 6.4531341. 145 6.4375 0.734375 6.45313; 146 6.125 2.20313 6.1718842. 147 4.125 2.20313 6.17188; 148 6 2.95313 6.03125; 149 4.125 2.95313 6.0312543. 150 4.625 3.92188 5.84375; 151 5.8125 3.92188 5.8437544. 152 5.625 4.90625 5.65625; 153 4.1875 7.23438 5.2031345. 154 4.1875 5.9375 5.45313; 155 5.3125 6.57813 5.32813; 156 5.5 5.5 5.5312546. 157 5.25 5.15625 5.60938; 158 5.1875 7.23438 5.2031347. 159 5.4375 5.9375 5.45313; 160 4.8125 5.5 5.53125; 163 0 0 6.5937548. 164 3.25 2.95313 6.03125; 165 6.5625 0 6.59375; 166 3.25 4.90625 5.6562549. 167 4 10.2813 4.625; 168 4.625 10. 2813 4.625; 169 4 8.92188 4.87550. 170 4.75 9.60938 4.75; 171 4.875 8.92188 4.875; 172 4.4375 8.5 4.9687551. 173 2.375 7.23438 5.20313; 174 2.375 5.9375 5.45313; 175 1.25 6.57813 5.32813

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52. 176 1.0625 5.5 5.53125; 177 1.25 5.15625 5.60938; 1 78 1.375 7.23438 5.2031353. 179 1.125 5.9375 5.45313; 180 1.75 5.5 5.53125; 181 4.3125 11.7813 4.3281354. 182 2.25 11.7813 4.32813; 183 3.25 6.57813 5.32813; 184 3.25 9.60938 4.7555. 185 3.25 11.3281 4.42188; 186 3.25 12.3281 4.21875; 187 3. 0625 25.5625 3.0937556. 188 3.5 25.5625 3.09375; 189 0.25 1.46875 0.28125; 190 1.625 1.46875 0.2812557. 191 1.5 7.85938 1.5; 192 5.0625 7.85938 1.5; 193 2.0625 10.7969 2.0781358. 194 4.5 10.7969 2.07813; 195 2.4375 20.4688 2.45312; 196 4.125 20.4688 2.4531259. 197 2.4375 16.9688 2.45312; 198 4.125 16.9688 2.4531260. 199 2.4375 13.4688 2.45312; 200 4.125 13.4688 2.45312

61. 201 0.8125 0.734375 0.140625; 202 0.125 0.734375 0.14062562. 203 0.375 2.20313 0.421875; 204 1.9375 3. 92188 0.75; 205 0.75 3.92188 0.7563. 206 0.9375 4.90625 0.9375; 207 2.5625 10.2813 1.9687564. 208 1.9375 10.2813 1.96875; 209 2.5625 8.92188 1.7187565. 210 1.8125 9.60938 1.84375; 211 2.75 11.1094 2.125; 212 2.1875 11.3438 2.1718866. 213 2.75 11.5625 2.21875; 214 1.6875 8.92188 1.71875; 215 2.125 8.5 1.62567. 216 2.875 12.125 2.32813; 217 2.375 12.3281 2.35938; 218 2.875 12.5313 2.4062568. 219 3.8125 11.1094 2.125; 220 4.375 11.3438 2.1718869. 221 3.8125 11.5625 2.21875; 2 22 3.6875 12.125 2.3281370. 223 4.1875 12.3281 2.35938; 224 3.6875 12.5313 2.4062571. 225 4.125 12.7656 2.45312; 226 2.4375 12.7656 2.4531272. 227 4.125 16.2656 2.45312; 228 2.4375 16.2656 2.4531273. 229 4.125 19.7656 2.45312; 230 2.437 5 19.7656 2.4531274. 231 2.4375 14.8594 2.45312; 232 4.125 14.8594 2.4531275. 233 2.4375 18.3594 2.45312; 234 4.125 18.3594 2.45312

76. 235 2.4375 2.20313 0.421875; 236 0.5625 2.95313 0.562577. 237 2.4375 2.95313 0.5625; 238 4.0625 21.15 63 2.53125; 239 2.625 21.8438 2.62578. 240 3.875 22.5313 2.71875; 241 2.8125 23.2344 2.7968779. 242 3.6875 23.9219 2.89062; 243 2.9375 24.6094 2.9687580. 244 3.625 24.6094 2.96875; 245 2.875 23.9219 2.89062; 246 3.75 23.2344 2.7968781. 247 2.6875 22.5313 2.71875; 248 3.9375 21.8438 2.625; 249 2.5 21.1563 2.5312582. 250 6.3125 1.46875 0.28125; 251 4.9375 1.46875 0.2812583. 252 5.75 0.734375 0.140625; 253 6.4375 0.734375 0.14062584. 254 6.125 2.20313 0.421875; 255 4.125 2.20 313 0.421875; 256 6 2.95313 0.562585. 257 4.125 2.95313 0.5625; 258 4.625 3.92188 0.75; 259 5.8125 3.92188 0.7586. 260 5.625 4.90625 0.9375; 261 4.1875 7.23438 1.3906387. 262 4.1875 5.9375 1.14063; 263 5.3125 6.57813 1.26563; 264 5.5 5.5 1.0 468888. 265 5.25 5.15625 0.984375; 266 5.1875 7.23438 1.3906389. 267 5.4375 5.9375 1.14063; 268 4.8125 5.5 1.04688; 271 0 0 0

90. 272 3.25 2.95313 0.5625; 273 6.5625 0 0; 274 3.25 4.90625 0.937591. 275 4 10.2813 1.96875; 276 4.625 10.281 3 1.96875; 277 4 8.92188 1.7187592. 278 4.75 9.60938 1.84375; 279 4.875 8.92188 1.71875; 280 4.4375 8.5 1.62593. 281 2.375 7.23438 1.39063; 282 2.375 5.9375 1.14063; 283 1.25 6.57813 1.2656394. 284 1.0625 5.5 1.04688; 285 1.25 5.15625 0.9843 75; 286 1.375 7.23438 1.3906395. 287 1.125 5.9375 1.14063; 288 1.75 5.5 1.04688; 289 4.3125 11.7813 2.2656396. 290 2.25 11.7813 2.26563; 291 3.25 6.57813 1.26563; 292 3.25 9.60938 1.8437597. 293 3.25 11.3281 2.17188; 294 3.25 12.3281 2.35938 ; 295 6.3125 1.46875 4.9531398. 296 6.4375 0.734375 5.76563; 297 5.8125 3.92188 4.6562599. 298 4.625 10.2813 3.98437; 299 4.875 8.92188 3.98437

100. 300 4.4375 11.1094 3.8125; 301 4.375 11.5625 3.8125; 302 4.9375 8.5 4.42188101. 303 4.25 1 2.125 3.67187; 304 4.1875 12.5313 3.6875; 305 4.4375 11.1094 2.78125102. 306 4.375 11.5625 2.78125; 307 4.25 12.125 2.90625; 308 4.1875 12.5313 2.90625103. 309 6.125 2.20313 4.125; 310 6 2.95313 4.125; 311 6.3125 1.46875 1.64063

104. 312 6.4375 0.734375 0.828125; 313 6.125 2.20313 2.46875; 314 6 2.95313 2.46875105. 315 5.8125 3.92188 1.92188; 316 5.1875 7.23438 2.39062106. 317 5.4375 5.9375 2.39062; 318 5.5625 5.15625 1.29688; 319 5.5 5.5 1.76563107. 320 6 2.95313 3.29687; 321 5.625 4 .90625 3.29687; 322 4.625 10.2813 2.60937108. 323 4.875 8.92188 2.60937; 324 4.9375 8.5 2.15625; 325 5.1875 7.23438 4.20313109. 326 5.4375 5.9375 4.20313; 327 5.5625 5.15625 5.29688; 328 5.5 5.5 4.82813110. 329 5.3125 6.57813 3.29687; 330 4.75 9.60938 3.29687111. 331 4.375 11.3281 3.29687; 332 4.1875 12.3281 3.29687112. 333 0.25 1.46875 4.95313; 334 0.125 0.734375 5.76563; 335 0.75 3.92188 4.65625113. 336 1.9375 10.2813 3.98437; 337 1.6875 8.92188 3.98437114. 338 2.125 11.1094 3. 8125; 339 2.1875 11.5625 3.8125; 340 1.625 8.5 4.42188115. 341 2.3125 12.125 3.67187; 342 2.375 12.5313 3.6875; 343 2.125 11.1094 2.78125116. 344 2.1875 11.5625 2.78125; 345 2.3125 12.125 2.90625

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117. 346 2.375 12.5313 2.90625; 347 0.375 2.20313 4.125; 348 0.5625 2.95313 4.125118. 349 0.25 1.46875 1.64063; 350 0.125 0.734375 0.828125119. 351 0.375 2.20313 2.46875; 352 0.5625 2.95313 2.46875120. 353 0.75 3.92188 1.92188; 354 1.375 7.23438 2.39062; 355 1.125 5.9375 2.39062121. 356 1 5.15625 1.29688; 357 1.0625 5.5 1.76563; 358 0.5625 2.95313 3.29687122. 359 0.9375 4.90625 3.29687; 360 1.9375 10.2813 2.60937123. 361 1.6875 8.92188 2.60937; 362 1.625 8.5 2.15625; 363 1.375 7.23438 4.20313124. 364 1.125 5.9375 4.20313; 365 1 5.15625 5.29688; 366 1.0625 5.5 4.82813125. 367 1.25 6.57813 3.29687; 368 1.8125 9.60938 3.29687

126. 369 2.1875 11.3281 3.29687; 370 2.375 12.3281 3.29687127. 371 3.28125 7.85938 5.07813; 372 3.28125 7.85938 1.5128. 373 5.0625 7.85938 3.28 906; 374 1.5 7.85938 3.28906129. 375 3.28125 10.7969 4.51563; 376 3.28125 10.7969 2.07813130. 377 4.5 10.7969 3.29688; 378 2.0625 10.7969 3.29688131. 379 3.28125 12.7656 4.14063; 380 3.28125 12.7656 2.45312132. 381 2.4375 12.7656 3.25; 382 4.125 12.7656 3.25; 383 3.28125 13.4688 4.14063133. 384 3.28125 13.4688 2.45312; 385 2.4375 13.4688 3.25; 386 4.125 13.4688 3.25134. 387 3.28125 16.2656 4.14063; 388 3.28125 16.2656 2.45312135. 389 2.4375 16.2656 3.25; 390 4.125 16.2656 3.25; 3 91 3.28125 16.9688 4.14063136. 392 3.28125 16.9688 2.45312; 393 2.4375 16.9688 3.25; 394 4.125 16.9688 3.25137. 395 3.28125 20.4688 4.14063; 396 3.28125 19.7656 4.14063138. 397 3.28125 20.4688 2.45312; 398 3.28125 19.7656 2.45312139. 399 2.4375 19.7656 3.25; 400 4.125 19.7656 3.25; 401 2.4375 20.4688 3.25140. 402 4.125 20.4688 3.25; 403 3.28125 25.5625 3.5; 404 3.0625 25.5625 3.29688

141. 405 3.28125 25.5625 3.09375; 406 3.5 25.5625 3.29688142. 407 3.28125 25.5625 3.29688; 408 1.5 16.7571 2.73438; 409 1.5 16.2656 2.73438143. 410 0.75 16.5802 2.96875; 411 0.75 16.2656 2.96875; 416 2.4375 13.4623 2.45313144. 417 2.4375 13.4623 4.14063; 418 4.125 13.4623 2.45313145. 419 4.125 13.4623 4.14063; 424 2.4375 16.9623 2.45313146. 425 2.4375 16.9623 4.14063; 426 4.125 16.9623 2.45313147. 427 4.125 16.9623 4.14063; 432 2.4375 20.4623 2.45313148. 433 2.4375 20.4623 4.14063; 434 4.125 20.4623 2.45313149. 435 4.125 20.4623 4.14063; 436 -0.1875 16.3817 3.25; 437 -0.1875 16.2656 3.25150. 438 -0.1875 16.3817 3.34375; 439 -0.1875 16.2656 3.34375151. 440 0.75 16.2656 3.60938; 441 1.5 16.2656 3.85938; 442 1.5 16.7571 3.85938152. 443 0.75 16.5802 3.60938; 444 1.5 20.2572 2.73438; 445 1.5 19.7658 2.73438153. 446 0.75 20.0803 2.96875; 447 0.75 19.7658 2.96875; 448 -0.1875 19.8819 3.25154. 449 -0.1875 19.7658 3.25; 450 -0.1875 19.8819 3.34375

155. 451 -0.1875 19.7658 3.34375; 452 0.75 19.7658 3.60938; 453 1.5 19.7658 3.85938156. 454 1.5 20.2572 3.85938; 4 55 0.75 20.0803 3.60938; 456 1.5 13.2572 2.73438157. 457 1.5 12.7658 2.73438; 458 0.75 13.0803 2.96875; 459 0.75 12.7658 2.96875158. 460 -0.1875 12.8819 3.25; 461 -0.1875 12.7658 3.25159. 462 -0.1875 12.8819 3.34375; 463 -0.1875 12.7658 3.34375160. 464 0.75 12.7658 3.60938; 465 1.5 12.7658 3.85938; 466 1.5 13.2572 3.85938161. 467 0.75 13.0803 3.60938; 468 5.0625 16.7571 2.73438162. 469 5.0625 16.2656 2.73438; 470 5.8125 16.5802 2.96875163. 471 5.8125 16.2656 2.96875; 472 6.75 16. 3817 3.25; 473 6.75 16.2656 3.25164. 474 6.75 16.3817 3.34375; 475 6.75 16.2656 3.34375; 476 5.8125 16.2656 3.60938165. 477 5.0625 16.2656 3.85938; 478 5.0625 16.7571 3.85938166. 479 5.8125 16.5802 3.60938; 480 5.0625 20.2572 2.73438167. 481 5.0625 19.7658 2.73438; 482 5.8125 20.0803 2.96875168. 483 5.8125 19.7658 2.96875; 484 6.75 19.8819 3.25; 485 6.75 19.7658 3.25

169. 486 6.75 19.8819 3.34375; 487 6.75 19.7658 3.34375; 488 5.8125 19.7658 3.60938170. 489 5.0625 19.7658 3.85938; 490 5.0625 20.2572 3.85938171. 491 5.8125 20.0803 3.60938; 492 5.0625 13.2572 2.73438172. 493 5.0625 12.7658 2.73438; 494 5.8125 13.0803 2.96875173. 495 5.8125 12.7658 2.96875; 496 6.75 12.8819 3.25; 497 6.75 12.7658 3.25174. 498 6.75 12.8819 3.34375; 499 6.75 12.7658 3.34375; 500 5.8125 12.7658 3.60938175. 501 5.0625 12.7658 3.85938; 502 5.0625 13.2572 3.85938176. 503 5.8125 13.0803 3.60938; 504 -0.1875 16.3817 3.29688177. 505 -0.1875 16.2656 3.29688; 506 -0.1875 19.8819 3.2968 8178. 507 -0.1875 19.7658 3.29688; 508 -0.1875 12.8819 3.29688179. 509 -0.1875 12.7658 3.29688; 510 6.75 16.3817 3.29688180. 511 6.75 16.2656 3.29688; 512 6.75 19.8819 3.29688; 513 6.75 19.7658 3.29688181. 514 6.75 12.8819 3.29688; 515 6.75 12.7658 3.29688

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182. MEMBER INCIDENCES183. 1 202 271; 2 92 163; 3 189 202; 4 79 92; 5 203 189; 6 93 79; 7 236 203184. 8 126 93; 9 205 236; 10 95 126; 11 206 205; 12 96 95; 13 284 206; 14 176 96185. 15 264 260; 16 156 152; 17 260 259; 18 152 151; 19 259 256; 20 151 148186. 21 256 254; 22 148 146; 23 254 250; 24 146 142; 25 250 253; 26 142 145187. 27 253 273; 28 145 165; 29 287 284; 30 179 176; 31 283 287; 32 175 179188. 33 286 283; 34 178 175; 35 191 286; 36 81 178; 37 214 191; 38 104 81189. 39 210 214; 40 100 104; 41 208 210; 42 98 100; 43 193 208; 44 83 98190. 45 212 193; 46 102 83; 47 220 194; 48 110 84; 49 194 276; 50 84 168

191. 51 276 278; 52 168 170; 53 278 279; 54 170 171; 55 279 192; 56 171 82192. 57 192 266; 58 82 158; 59 266 263; 60 158 155; 61 263 267; 62 155 159193. 63 267 264; 64 159 156; 65 290 212; 66 182 102; 67 217 290; 68 107 182194. 69 226 217; 70 116 107; 71 226 199; 72 199 231; 73 231 228; 74 228 197195. 75 116 89; 76 89 121; 77 121 1 18; 78 118 87; 79 225 200; 80 200 232196. 81 232 227; 82 227 198; 83 115 90; 84 90 122; 85 122 117; 86 117 88197. 87 225 223; 88 115 113; 89 223 289; 90 113 181; 91 289 220; 92 181 110198. 93 197 233; 94 233 230; 95 230 195; 96 87 123; 97 123 1 20; 98 120 85199. 99 195 249; 100 85 141; 101 249 239; 102 141 131; 103 238 248; 104 130 140200. 105 196 238; 106 86 130; 107 198 234; 108 234 229; 109 229 196; 110 88 124201. 111 124 119; 112 119 86; 113 239 247; 114 131 139; 115 247 241; 116 139 133202. 117 241 245; 118 133 137; 119 245 243; 120 137 135; 121 243 187; 122 135 128203. 123 244 188; 124 136 129; 125 242 244; 126 134 136; 127 246 242; 128 138 134204. 129 240 246; 130 132 138; 131 248 240; 132 140 132; 133 352 236; 134 3 58 352205. 135 348 358; 136 126 348; 137 359 206; 138 96 359; 139 236 237; 140 374 191

206. 141 81 374; 142 126 127; 143 358 272; 144 358 164; 145 378 193; 146 83 378207. 147 206 274; 148 359 274; 149 359 166; 150 96 166; 151 191 372; 152 374 37 2208. 153 374 371; 154 81 371; 155 199 385; 156 228 389; 157 197 393; 158 230 399209. 159 195 401; 160 226 381; 161 116 381; 162 89 385; 163 389 118; 164 393 425210. 165 399 120; 166 401 433; 167 193 376; 168 378 376; 169 378 375; 170 83 375211. 171 237 272; 172 127 164; 173 226 380; 174 199 384; 175 228 388; 176 197 392212. 177 230 398; 178 195 397; 179 381 380; 180 385 384; 181 389 388; 182 393 392213. 183 399 398; 184 401 397; 185 381 379; 186 385 383; 187 389 387; 188 393 391214. 189 399 396; 190 401 395; 191 116 379; 192 89 383; 193 118 387; 194 87 391215. 195 120 396; 196 85 395; 197 404 187; 198 128 404; 199 187 405; 200 128 403216. 201 405 188; 202 403 129; 203 188 406; 204 406 129; 205 272 257; 206 164 149217. 207 380 225; 208 384 200; 209 388 227; 210 392 198; 211 398 229; 212 397 196218. 213 380 382; 214 384 386; 215 388 390; 216 392 394; 217 398 400; 218 397 402219. 219 379 382; 220 383 386; 221 387 390; 222 391 394; 223 396 400; 224 395 402

220. 225 379 115; 226 383 90; 227 387 117; 228 391 88; 229 396 119; 230 395 86221. 231 376 194; 232 376 377; 233 375 377; 234 375 84; 235 225 382; 236 227 390222. 237 198 394; 238 229 400; 239 196 402; 240 200 386; 241 386 90; 242 382 115223. 243 390 117; 244 394 427; 245 400 119; 246 402 435; 247 372 192; 248 372 373224. 249 371 373; 250 371 82; 251 274 260; 252 274 321; 253 166 321; 254 166 152225. 255 377 194; 256 84 377; 257 272 320; 258 164 320; 259 257 256; 260 373 192226. 261 82 373; 262 149 148; 263 321 260; 264 152 321; 265 314 256; 266 320 314227. 267 310 320; 268 148 310; 269 350 271; 270 163 334; 271 349 350; 272 334 333228. 273 351 349; 274 333 347; 275 271 201; 276 163 91; 277 358 351; 278 347 358229. 279 353 236; 280 126 335; 281 359 353; 282 335 359; 283 201 190; 284 91 80230. 285 236 204; 286 126 94; 287 190 235; 288 80 125; 289 204 274; 290 94 166231. 291 235 272; 292 125 164; 293 272 255; 294 164 147; 295 274 258; 296 166 150232. 297 255 251; 298 1 47 143; 299 258 256; 300 150 148; 301 251 252; 302 143 144233. 303 321 315; 304 297 321; 305 315 256; 306 148 297; 307 320 313; 308 309 320

234. 309 252 273; 310 144 165; 311 313 311; 312 295 309; 313 311 312; 314 296 295235. 315 312 273; 316 16 5 296; 317 206 356; 318 96 365; 319 356 357; 320 365 366236. 321 206 285; 322 357 355; 323 366 364; 324 96 177; 325 355 367; 326 364 367237. 327 367 354; 328 367 363; 329 354 191; 330 363 81; 331 285 288; 332 177 180238. 333 191 362; 334 81 340 ; 335 362 361; 336 340 337; 337 361 368; 338 337 368239. 339 191 215; 340 81 105; 341 368 360; 342 368 336; 343 281 191; 344 173 81240. 345 360 193; 346 336 83; 347 288 282; 348 180 174; 349 207 193; 350 97 83241. 351 215 209; 352 105 99; 353 2 82 291; 354 291 281; 355 183 173; 356 174 183242. 357 209 292; 358 292 207; 359 184 97; 360 99 184; 361 277 292; 362 292 275243. 363 184 167; 364 169 184; 365 262 291; 366 291 261; 367 183 153; 368 154 183244. 369 280 277; 370 172 169; 371 275 194; 372 167 84; 373 268 262; 374 160 154245. 375 322 194; 376 298 84; 377 261 192; 378 153 82; 379 330 322; 380 330 298246. 381 192 280; 382 82 172; 383 323 330; 384 299 330; 385 324 323; 386 302 299

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247. 387 192 324; 388 82 302; 389 265 268; 3 90 157 160; 391 316 192; 392 325 82248. 393 329 316; 394 329 325; 395 317 329; 396 326 329; 397 260 265; 398 152 157249. 399 319 317; 400 328 326; 401 318 319; 402 327 328; 403 260 318; 404 152 327250. 405 193 343; 406 83 338; 407 343 369; 408 338 369; 409 369 344; 410 369 339251. 411 344 290; 412 339 182; 413 290 345; 414 182 341; 415 345 370; 416 341 370252. 417 370 346; 418 370 342; 419 193 211; 420 346 226; 421 342 116; 422 83 101253. 423 213 290; 424 103 182; 425 290 216; 426 18 2 106; 427 218 226; 428 108 116254. 429 211 293; 430 293 213; 431 185 103; 432 101 185; 433 216 294; 434 294 218255. 435 186 108; 436 106 186; 437 222 294; 438 294 224; 439 186 114; 440 112 186

256. 441 219 293; 442 293 221; 443 185 111; 444 109 185; 445 224 225; 446 114 115257. 447 289 222; 448 181 112; 449 221 289; 450 111 181; 451 194 219; 452 225 308258. 453 84 109; 454 332 308; 455 332 304; 456 307 332; 457 303 332; 458 289 307259. 459 181 303; 460 306 289; 461 301 181; 462 331 3 06; 463 331 301; 464 305 331260. 465 300 331; 466 194 305; 467 84 300; 468 226 89; 469 116 199; 470 199 121261. 471 89 231; 472 121 228; 473 231 118; 474 228 87; 475 118 197; 476 197 123262. 477 87 233; 478 123 230; 479 233 120; 480 230 85; 481 120 195; 482 85 249263. 483 195 238; 484 85 130; 485 225 199; 486 226 200; 487 231 200; 488 232 199264. 489 228 232; 490 227 231; 491 227 197; 492 228 198; 493 233 198; 494 234 197265. 495 230 234; 496 229 233; 497 229 195; 498 230 196; 499 11 5 89; 500 116 90266. 501 121 90; 502 122 89; 503 118 122; 504 117 121; 505 117 87; 506 118 88267. 507 123 88; 508 124 87; 509 120 124; 510 119 123; 511 119 85; 512 120 86268. 513 249 196; 514 141 86; 515 130 196; 516 225 90; 517 115 200; 518 20 0 122269. 519 90 232; 520 122 227; 521 232 117; 522 227 88; 523 117 198; 524 198 124270. 525 88 234; 526 124 229; 527 234 119; 528 229 86; 529 119 196; 530 249 131

271. 531 239 141; 532 139 239; 533 131 247; 534 247 133; 535 241 139; 536 137 241272. 537 133 245; 538 245 135; 539 243 137; 540 128 243; 541 135 187; 542 248 249273. 543 246 247; 544 243 188; 545 135 129; 546 138 139; 547 140 141; 548 239 240274. 549 241 242; 550 244 245; 551 136 137; 552 133 134; 553 131 132; 554 247 248275. 555 245 246; 556 242 243; 557 134 135; 558 137 138; 559 139 140; 560 238 239276. 561 240 241; 562 187 244; 563 128 136; 564 132 133; 565 130 131; 566 129 244277. 567 136 188; 568 242 136; 569 244 134; 570 134 246; 571 138 242; 572 240 138278. 573 246 132; 574 132 248; 575 140 240; 576 238 140; 577 248 130; 1001 350 202279. 1002 334 92; 1003 350 189; 1004 334 79; 1005 189 349; 1006 79 333280. 1007 349 203; 1008 333 93; 1009 203 351; 1010 93 347; 1011 201 202281. 1012 351 236; 1013 351 352; 1014 347 348; 1015 347 126; 1016 91 92282. 1017 201 189; 1018 91 79; 1019 353 205; 1020 335 95; 1021 353 206; 1022 335 96283. 1023 189 190; 1024 79 80; 1025 190 203; 1026 80 93; 1027 204 205; 1028 94 95284. 1029 203 235; 1030 93 1 25; 1031 204 206; 1032 94 96; 1033 235 236

285. 1034 125 126; 1035 235 237; 1036 125 127; 1037 255 257; 1038 147 149286. 1039 255 256; 1040 147 148; 1041 254 255; 1042 258 260; 1043 150 152287. 1044 146 147; 1045 258 259; 1046 150 151; 1047 251 254; 1048 143 146288. 1049 250 251; 1050 142 143; 1051 315 260; 1052 297 152; 1053 315 259289. 1054 297 151; 1055 252 250; 1056 144 142; 1057 313 256; 1058 313 314290. 1059 309 310; 1060 309 148; 1061 252 253; 1062 144 145; 1063 254 313291. 1064 146 309; 1065 311 254; 1066 295 146; 1067 250 311; 1068 142 295292. 1069 312 250; 1070 296 142; 1071 312 253; 1072 296 145; 1501 284 356293. 1502 176 365; 1503 284 357; 1504 176 366; 1505 357 287; 1506 366 179294. 1507 355 287; 1508 364 1 79; 1509 284 285; 1510 176 177; 1511 283 355295. 1512 175 364; 1513 354 355; 1514 363 364; 1515 283 354; 1516 175 363296. 1517 354 286; 1518 363 178; 1519 284 288; 1520 176 180; 1521 288 287297. 1522 180 179; 1523 214 362; 1524 104 340; 1525 36 1 214; 1526 337 104298. 1527 282 287; 1528 361 210; 1529 337 100; 1530 174 179; 1531 283 282

299. 1532 283 281; 1533 360 361; 1534 336 337; 1535 175 173; 1536 175 174300. 1537 281 286; 1538 210 360; 1539 100 336; 1540 173 178; 1541 214 215301. 1542 104 105; 1543 360 208; 1544 336 98; 1545 209 214; 1546 99 104302. 1547 209 210; 1548 210 207; 1549 100 97; 1550 99 100; 1551 207 208; 1552 97 98303. 1553 281 282; 1554 173 174; 1555 207 209; 1556 97 99; 1557 275 277304. 1558 167 169; 15 59 261 262; 1560 153 154; 1561 275 276; 1562 167 168305. 1563 277 278; 1564 278 275; 1565 170 167; 1566 169 170; 1567 277 279306. 1568 169 171; 1569 322 276; 1570 298 168; 1571 279 280; 1572 171 172307. 1573 261 266; 1574 278 322; 1575 170 298; 1576 153 158; 1577 263 262308. 1578 263 261; 1579 322 323; 1580 298 299; 1581 155 153; 1582 155 154309. 1583 262 267; 1584 323 278; 1585 299 170; 1586 154 159; 1587 323 279310. 1588 299 171; 1589 279 324; 1590 171 302; 1591 268 267; 1592 160 1 59311. 1593 264 268; 1594 156 160; 1595 316 266; 1596 325 158; 1597 263 316

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312. 1598 155 325; 1599 316 317; 1600 325 326; 1601 264 265; 1602 263 317313. 1603 155 326; 1604 156 157; 1605 317 267; 1606 326 159; 1607 319 267314. 1608 328 159; 1609 264 319; 1610 156 328; 1611 264 318; 1612 156 327315. 2001 343 212; 2002 338 102; 2003 212 344; 2004 102 339; 2005 345 217316. 2006 341 107; 2007 217 346; 2008 107 342; 2009 211 212; 2010 212 213317. 2011 102 103; 2012 101 102; 2013 216 21 7; 2014 217 218; 2015 107 108318. 2016 106 107; 2017 222 223; 2018 223 224; 2019 113 114; 2020 112 113319. 2021 219 220; 2022 220 221; 2023 110 111; 2024 109 110; 2025 113 304320. 2026 307 223; 2027 303 113; 2028 220 306; 2029 110 301; 2030 305 220

321. 2031 300 110; 3001 460 461; 3002 461 509; 3003 460 508; 3004 509 463322. 3005 508 462; 3006 462 463; 3007 461 459; 3008 460 458; 3009 463 464323. 3010 462 467; 3011 458 459; 3012 459 464; 3013 458 467; 3014 467 464324. 3015 459 457; 3016 458 457; 3017 458 456; 3018 464 456; 3019 459 466325. 3020 464 465; 3021 467 465; 3022 467 466; 3023 456 457; 3024 457 465326. 3025 456 466; 3026 466 465; 3027 457 226; 3028 456 226; 3029 456 416327. 3030 465 416; 3031 457 417; 3032 465 116; 3033 466 116; 3034 466 417328. 3035 493 225; 3036 492 225; 3037 418 492; 3038 501 418; 3039 493 419329. 3040 501 115; 3041 502 115; 3042 419 502; 3043 492 493; 3044 493 501330. 3045 492 502; 3046 502 501; 3047 493 495; 3048 494 493; 3049 4 92 494331. 3050 500 492; 3051 495 502; 3052 501 500; 3053 503 501; 3054 502 503332. 3055 494 495; 3056 495 500; 3057 494 503; 3058 503 500; 3059 495 497333. 3060 494 496; 3061 500 499; 3062 503 498; 3063 496 497; 3064 497 515334. 3065 496 514; 3066 515 499; 3067 514 498; 3068 498 499; 4001 436 437335. 4002 437 505; 4003 436 504; 4004 505 439; 4005 504 438; 4006 438 439

336. 4007 437 411; 4008 436 410; 4009 439 440; 4010 438 443; 4011 410 411337. 4012 411 440; 4013 410 443; 4014 44 3 440; 4015 411 409; 4016 410 409338. 4017 410 408; 4018 440 408; 4019 411 442; 4020 440 441; 4021 443 441339. 4022 443 442; 4023 408 409; 4024 409 441; 4025 408 442; 4026 442 441340. 4027 409 228; 4028 408 228; 4029 408 424; 4030 441 424; 4031 409 425341. 4032 441 118; 4033 442 118; 4034 442 425; 4035 469 227; 4036 468 227342. 4037 426 468; 4038 477 426; 4039 469 427; 4040 477 117; 4041 478 117343. 4042 427 478; 4043 468 469; 4044 469 477; 4045 468 478; 4046 478 477344. 4047 469 471; 4048 470 469; 4049 468 470; 4050 476 468; 4051 471 478345. 4052 477 476; 4053 479 477; 4054 478 479; 4055 470 471; 4056 471 476346. 4057 470 479; 4058 479 476; 4059 471 473; 4060 470 472; 4061 476 475347. 4062 479 474; 4063 472 473; 4064 473 511; 4065 472 510; 4066 511 475348. 4067 510 474; 4068 474 475; 5001 448 449; 5002 449 507; 5003 448 506349. 5004 507 451; 5005 506 450; 5006 450 451; 5007 449 447; 5008 448 446

350. 5009 451 452; 5010 450 455; 5011 446 447; 5012 447 452; 50 13 446 455351. 5014 455 452; 5015 447 445; 5016 446 445; 5017 446 444; 5018 452 444352. 5019 447 454; 5020 452 453; 5021 455 453; 5022 455 454; 5023 444 445353. 5024 445 453; 5025 444 454; 5026 454 453; 5027 445 230; 5028 444 230354. 5029 444 432; 5030 453 432; 5031 445 433; 5032 453 120; 5033 454 120355. 5034 454 433; 5035 481 229; 5036 480 229; 5037 434 480; 5038 489 434356. 5039 481 435; 5040 489 119; 5041 490 119; 5042 435 490; 5043 480 481357. 5044 481 489; 5045 480 490; 504 6 490 489; 5047 481 483; 5048 482 481358. 5049 480 482; 5050 488 480; 5051 483 490; 5052 489 488; 5053 491 489359. 5054 490 491; 5055 482 483; 5056 483 488; 5057 482 491; 5058 491 488360. 5059 483 485; 5060 482 484; 5061 488 487; 5062 491 486; 5063 484 485361. 5064 485 513; 5065 484 512; 5066 513 487; 5067 512 486; 5068 486 487362. 10476 404 407; 10520 405 407; 10521 407 403; 10537 407 406363. START GROUP DEFINITION

364. MEMBER365. _LEG1 1 TO 28366. _LEG2 29 TO 64367. _LEG3 65 TO 92368. _LEG4 93 TO 112369. _LEG5 113 TO 132370. _PLAT_BRA1 197 TO 204371. _PLAT_BRA2 155 TO 166 173 TO 196 207 TO 230 235 TO 246372. _PLAT_BRA3 140 141 145 146 151 TO 154 167 TO 170 231 TO 234 247 TO 250 255 -373. 256 260 261374. _PLAT_BRA4 133 TO 139 142 TO 144 147 TO 150 171 172 205 206 251 TO 254 257 -375. 258 TO 259 262 TO 268376. _DIA_BRA1 269 TO 316

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377. _DIA_BRA2 317 TO 404378. _DIA_BRA3 405 TO 467379. _DIA_BRA4 468 TO 529380. _DIA_BRA5 530 TO 577381. _REDUND1 1001 TO 1072382. _REDUND2 1501 TO 1612383. _REDUND3 2001 TO 2031384. _CROSSARM 3001 TO 3068 4001 TO 4068 5001 TO 5068385. END GROUP DEFINITION

386. DEFINE MATERIAL START387. ISOTROPIC STEEL388. E 2.05E+008389. POISSON 0.3390. DENSITY 76.8195391. ALPHA 1.2E-005392. DAMP 0.03393. END DEFINE MATERIAL394. MEMBER PROPERTY INDIAN395. *************LEG1***************396. 1 TO 28 TABLE ST ISA200X200X25397. *************LEG2*** ************398. 29 TO 64 TABLE ST ISA150X150X15399. *************LEG3***************400. 65 TO 92 TABLE ST ISA110X110X12

401. *************LEG4***************402. 93 TO 112 TABLE ST ISA100X100X12403. *************LEG5***************404. 113 TO 132 TABLE ST ISA75X75X8405. *******************************PLATFORM BRACING1******************************406. 197 TO 204 10476 10520 10521 10537 TABLE ST ISA60X60X10407. ****************************PLATFORM BRACING2************ *********************408. 155 TO 166 173 TO 196 207 TO 230 235 TO 246 3018 3019 3030 3031 3038 3039 -409. 3050 3051 4018 4019 4030 4031 4038 4039 4050 4051 5018 5019 5030 5031 5038 -410. 5039 5050 5051 TABLE ST ISA75X75X10411. ************* ******************PLATFORM BRACING3******************************412. 140 141 145 146 151 TO 154 167 TO 170 231 TO 234 247 TO 250 255 256 260 -413. 261 TABLE ST ISA100X100X8414. *******************************PLATFORM BRACING4****************** ************

415. 133 TO 139 142 TO 144 147 TO 150 171 172 205 206 251 TO 254 257 TO 259 262 -416. 263 TO 268 TABLE ST ISA130X130X8417. **************************CROSSARM BRACING ***********************************418. 3001 TO 3006 3011 TO 3 014 3016 3021 3023 TO 3026 3028 3033 3036 3041 3043 -419. 3044 TO 3046 3048 3053 3055 TO 3058 3063 TO 3068 4001 TO 4006 4011 TO 4014 -420. 4016 4021 4023 TO 4026 4028 4033 4036 4041 4043 TO 4046 4048 4053 -421. 4055 TO 4058 4063 TO 4068 5001 TO 5006 5011 TO 5014 5016 5021 5023 TO 5026 -422. 5028 5033 5036 5041 5043 TO 5046 5048 5053 5055 TO 5058 5063 TO 5067 -423. 5068 TABLE ST ISA75X75X10424. ***********************************CROSSARM************************************425. 3007 TO 3010 3015 3017 3020 3022 3027 3029 3032 3034 3035 3037 3040 3042 3047 -426. 3049 3052 3054 3059 TO 3062 4007 TO 4010 4015 4017 4020 4022 4027 4029 4032 -427. 4034 4035 4037 4040 4042 4047 4049 4052 4054 4059 TO 4062 5007 TO 5010 5015 -428. 5017 5020 5022 5027 5029 5032 5034 5035 5037 5040 5042 5047 5049 5052 5054 -

429. 5059 TO 5062 TABLE ST ISA130X130X12430. ******DIAGONAL BRACING1***********431. 269 TO 316 TABLE ST ISA150X150X12432. ******DIAGONAL BRACING2***********433. 317 TO 404 TABLE ST ISA130X130X12434. ******DIAGONAL BRACING3***********435. 405 TO 467 TABLE ST ISA100X100X10436. ******DIAGONAL BRACING4***********437. 468 TO 529 TABLE ST ISA75X75X10438. ******DIAGONAL BRACING5***********439. 530 TO 577 TABLE ST ISA65X65X10440. ***********REDUNDANTS1************441. 1001 TO 1072 TABLE ST ISA100X100X8

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442. ***********REDUNDANTS2************443. 1501 TO 1612 TABLE ST ISA80X80X8444. ***********REDUNDANTS3************445. 2001 TO 2031 TABLE ST ISA60X60X10446. CONSTANTS447. MATERIAL STEEL ALL448. SUPPORTS449. 163 165 271 273 FIXED450. DEFINE WIND LOAD

451. TYPE 1452. <! STAAD PRO GENERATED DATA DO NOT MODIFY !!!453. ASCE-7-2002:PARAMS 172.200 KMPH 5 3 3 0 0.000 FT 0.000 FT 0.000 FT 1 -454. 1 26.100 M 6.560 M 60.000 2.000 0.010 -455. 0 0 0 0 1.393 1.000 1.150 0.850 0 -456. 0 0 0 0.647 1.900 0.550457. !> END GENERATED DATA BLOCK458. INT 1.73749 1.73749 1.82663 1.89891 1.96008 2.013 34 2.06065 2.10329 2.14219 -459. 2.17799 2.2112 2.24219 2.27128 2.2987 2.32464 2.34928 2.56693 HEIG 0 4.572 -460. 6.096 7.62 9.144 10.668 12.192 13.716 15.24 16.764 18.288 19.812 -461. 21.336 22.86 24.384 25.908 25.908462. EXP 1 JOINT 79 TO 160 163 TO 268 271 TO 402

463. LOAD 1 LOADTYPE WIND TITLE WIND+X 464. WIND LOAD X 1 TYPE 1 XR 0 2.438 YR 0 12.766 ZR 0 6.594 OPEN465. WIND LOAD X 1 TYPE 1 XR 2.438 2.438 YR 12.766 20.469 ZR 2.453 4.141 OPEN466. WIND LOAD X 1 TYPE 1 XR 2.438 3.063 YR 20.469 25.563 ZR 2.453 4.141 OPEN467. WIND LOAD X 1 TYPE 1 XR -0.188 2.438 YR 12.766 20.469 ZR 2.906 3.594 OPEN

468. LOAD 2 LOADTYPE DEAD TITLE SELFWEIGHT OF STRUCTURE  469. SELFWEIGHT Y -1

470. LOAD 3 LOADTYPE NONE TITLE 1A. NC -5D, 75KG/M2 471. JOINT LOAD472. 407 FX 31.94 FY -5.15473. 505 507 509 511 513 515 FX 69.32 FY -11.48

474. LOAD 4 LOADTYPE NONE TITLE 1B. NC (SC STRUNG 1) -5D, 75KG/M2475. JOINT LOAD476. 407 FX 31.94 FY -5.15477. 505 507 513 FX 69.32 FY -11.48

478. LOAD 5 LOADTYPE NONE TITLE 1C. NC (SS STRUNG 2) -5D, 75KGM2 

479. JOINT LOAD480. 407 FX 31.94 FY -5.15481. 505 507 509 FX 69.32 FY -11.48

482. LOAD 6 LOADTYPE NONE TITLE 2A. EW + TC BROKEN WIRE COND 5D, 75KG /M483. JOINT LOAD484. 407 FX 10.46 FY -3.72 FZ 8.71485. 507 FX 22.87 FY -7.91 FZ 18.89486. 505 509 511 513 515 FX 69.32 FY -11.48

487. LOAD 7 LOADTYPE NONE TITLE 2B. EW+MC BROKEN WIRE COND -5D, 75KG/M2488. JOINT LOAD489. 407 FX 10.46 FY -3.72 FZ 11.48490. 507 509 511 513 515 FX 69.32 FY -11.48491. 505 FX 22.87 FY -7.91 FZ 18.89

492. LOAD 8 LOADTYPE NONE TITLE 2C. EW+BC BROKEN WIRE COND -5D,

75KG/M2LOAD CASE 8 493. JOINT LOAD494. 407 FX 10.46 FY -3.72 FZ 8.71495. 507 509 511 513 515 FX 69.32 FY -11.48496. 505 FX 22.87 FY -7.91 FZ 18.89

497. LOAD 9 LOADTYPE NONE TITLE 2D. TC+MC BROKEN WIRE COND -5D,75KG/M2498. JOINT LOAD499. 407 FX 31.94 FY -5.15500. 507 FX 22.87 FY -7.91 FZ 18.89501. 505 509 511 513 515 FX 69.32 FY -11.48

502. LOAD 10 LOADTYPE NONE TITLE 2E. TC+BC BROLEN WIRE COND -5D,75KG/M2503. JOINT LOAD

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566. ELA 5 MEMB 140 141 145 146 151 TO 154 167 TO 170 231 TO 234 247 TO 250 255 -567. 256 260 261 133 TO 139 142 TO 144 147 TO 150 171 172 205 206 251 TO 254 -568. 257 TO 259 262 263 TO 268 3001 TO 3006 3011 TO 3014 3016 3021 3023 TO 3026 -569. 3028 3033 3036 3041 3043 3044 TO 3046 3048 3053 3055 TO 3058 3063 TO 3068 -570. 4001 TO 4006 4011 TO 4014 4016 4021 4023 TO 4026 4028 4033 4036 4041 -571. 4043 TO 4046 4048 4053 4055 TO 4058 4063 TO 4068 5001 TO 5006 5011 TO 5014 -572. 5016 5021 5023 TO 5026 5028 5033 5036 5041 5043 TO 5046 5048 5053 -573. 5055 TO 5058 50 63 TO 5067 5068574. ELA 5 MEMB 3007 TO 3010 3015 3017 3020 3022 3027 3029 3032 3034 3035 3037 -

575. 3040 3042 3047 3049 3052 3054 3059 TO 3062 4007 TO 4010 4015 4017 4020 4022 -576. 4027 4029 4032 4034 4035 4037 4040 4042 4047 4049 4052 4054 40 59 TO 4062 -577. 5007 TO 5010 5015 5017 5020 5022 5027 5029 5032 5034 5035 5037 5040 5042 -578. 5047 5049 5052 5054 5059 TO 5062579. ELA 7 MEMB 1001 TO 1072 1501 TO 1612 2001 TO 2031580. CNSF 1 MEMB 1 TO 132581. CNSF 1 MEMB 269 TO 577582. CNSF 1 MEMB 1001 TO 1072 1501 TO 1612 2001 TO 2031583. CNSF 1 MEMB 197 TO 204 10476 10520 10521 10537 155 TO 166 173 TO 196 -584. 207 TO 230 235 TO 246 3018 3019 3030 3031 3038 3039 3050 3051 4018 4019 -585. 4030 4031 4038 4039 4050 4051 5018 5019 5030 5031 5038 5039 5050 5051586. CNSF 1 MEMB 140 141 145 146 151 TO 154 167 TO 170 231 TO 234 247 TO 250 255 -587. 256 260 261 133 TO 139 142 TO 144 147 TO 150 171 172 205 206 251 TO 254 -588. 257 TO 259 262 263 TO 268 3001 TO 3006 3011 TO 3014 3016 3021 3023 TO 3026 -589. 3028 3033 3036 3041 3043 3044 TO 3046 3048 3053 3055 TO 3058 3063 TO 3068 -

590. 4001 TO 4006 4011 TO 4014 4016 4021 4023 TO 4026 4028 4033 4036 4041 -591. 4043 TO 4046 4048 4053 4055 TO 4058 4063 TO 406 8 5001 TO 5006 5011 TO 5014 -592. 5016 5021 5023 TO 5026 5028 5033 5036 5041 5043 TO 5046 5048 5053 -593. 5055 TO 5058 5063 TO 5067 5068594. CNSF 1 MEMB 3007 TO 3010 3015 3017 3020 3022 3027 3029 3032 3034 3035 3037 -595. 3040 3042 3047 304 9 3052 3054 3059 TO 3062 4007 TO 4010 4015 4017 4020 4022 -596. 4027 4029 4032 4034 4035 4037 4040 4042 4047 4049 4052 4054 4059 TO 4062 -597. 5007 TO 5010 5015 5017 5020 5022 5027 5029 5032 5034 5035 5037 5040 5042 -598. 5047 5049 5052 5054 50 59 TO 5062599. DBL 0.016 MEMB 1 TO 132600. DBL 0.016 MEMB 269 TO 577601. DBL 0.016 MEMB 1001 TO 1072 1501 TO 1612 2001 TO 2031602. DBL 0.012 MEMB 197 TO 204 10476 10520 10521 10537 155 TO 166 173 TO 196 -603. 207 TO 230 235 TO 246 3018 3019 3030 3031 3038 3039 3050 3051 4018 4019 -

604. 4030 4031 4038 4039 4050 4051 5018 5019 5030 5031 5038 5039 5050 5051605. DBL 0.012 MEMB 140 141 145 146 151 TO 154 167 TO 170 231 TO 234 247 TO 250 -606. 255 256 260 261 133 TO 139 142 TO 144 147 TO 150 171 172 205 206 251 TO 254 -607. 257 TO 259 262 263 TO 268 3001 TO 3006 3011 TO 3014 3016 3021 3023 TO 3026 -608. 3028 3033 3036 3041 3043 3044 TO 3046 3048 3053 3055 TO 3058 3063 TO 3068 -609. 4001 TO 4006 4011 TO 4014 4016 4021 402 3 TO 4026 4028 4033 4036 4041 -610. 4043 TO 4046 4048 4053 4055 TO 4058 4063 TO 4068 5001 TO 5006 5011 TO 5014 -611. 5016 5021 5023 TO 5026 5028 5033 5036 5041 5043 TO 5046 5048 5053 -612. 5055 TO 5058 5063 TO 5067 5068613. DBL 0.012 MEMB 3 007 TO 3010 3015 3017 3020 3022 3027 3029 3032 3034 3035 3037 -614. 3040 3042 3047 3049 3052 3054 3059 TO 3062 4007 TO 4010 4015 4017 4020 4022 -615. 4027 4029 4032 4034 4035 4037 4040 4042 4047 4049 4052 4054 4059 TO 4062 -616. 5007 TO 5010 50 15 5017 5020 5022 5027 5029 5032 5034 5035 5037 5040 5042 -617. 5047 5049 5052 5054 5059 TO 5062

618. GALVA 0 MEMB 1 TO 132619. GALVA 0 MEMB 269 TO 577620. GALVA 0 MEMB 1001 TO 1072 1501 TO 1612 2001 TO 2031621. GALVA 0 MEMB 197 TO 204 1 0476 10520 10521 10537 155 TO 166 173 TO 196 -622. 207 TO 230 235 TO 246 3018 3019 3030 3031 3038 3039 3050 3051 4018 4019 -623. 4030 4031 4038 4039 4050 4051 5018 5019 5030 5031 5038 5039 5050 5051624. GALVA 0 MEMB 140 141 145 146 151 TO 154 1 67 TO 170 231 TO 234 247 TO 250 255 -625. 256 260 261 133 TO 139 142 TO 144 147 TO 150 171 172 205 206 251 TO 254 -626. 257 TO 259 262 263 TO 268 3001 TO 3006 3011 TO 3014 3016 3021 3023 TO 3026 -627. 3028 3033 3036 3041 3043 3044 TO 3046 3048 3053 3055 TO 3058 3063 TO 3068 -628. 4001 TO 4006 4011 TO 4014 4016 4021 4023 TO 4026 4028 4033 4036 4041 -629. 4043 TO 4046 4048 4053 4055 TO 4058 4063 TO 4068 5001 TO 5006 5011 TO 5014 -630. 5016 5021 5023 TO 5026 5028 5033 5036 5041 5043 TO 5046 5048 5053 -

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631. 5055 TO 5058 5063 TO 5067 5068632. GALVA 0 MEMB 3007 TO 3010 3015 3017 3020 3022 3027 3029 3032 3034 3035 3037 -633. 3040 3042 3047 3049 3052 3054 3059 TO 3062 4007 TO 4010 4015 4017 4020 4022 -634. 4027 4029 4032 4034 4035 4037 4040 4042 4047 4049 4052 4054 4059 TO 4062 -635. 5007 TO 5010 5015 5017 5020 5022 5027 5029 5032 5034 5035 5037 5040 5042 -636. 5047 5049 5052 5054 5059 TO 5062637. GUSSET 0.01 MEMB 1 TO 132638. GUSSET 0.01 MEMB 269 TO 577639. GUSSET 0.01 MEMB 1001 TO 1072 1501 TO 1612 2001 TO 2031

640. GUSSET 0.006 MEMB 197 TO 204 10476 10520 10521 10537 155 TO 166 173 TO 196 -641. 207 TO 230 235 TO 246 3018 3019 3030 3031 3038 3039 3050 3051 4018 4019 -642. 4030 4031 4038 4039 4050 4051 5018 5019 5030 5031 5038 5039 5050 5051643. GUSSET 0.006 MEMB 140 141 145 146 151 TO 154 167 TO 170 231 TO 234 247 TO 250 -644. 255 256 260 261 133 TO 139 142 TO 144 147 TO 150 171 172 205 206 251 TO 254 -645. 257 TO 259 262 263 TO 268 30 01 TO 3006 3011 TO 3014 3016 3021 3023 TO 3026 -646. 3028 3033 3036 3041 3043 3044 TO 3046 3048 3053 3055 TO 3058 3063 TO 3068 -647. 4001 TO 4006 4011 TO 4014 4016 4021 4023 TO 4026 4028 4033 4036 4041 -648. 4043 TO 4046 4048 4053 4055 TO 4058 4063 TO 4068 5001 TO 5006 5011 TO 5014 -649. 5016 5021 5023 TO 5026 5028 5033 5036 5041 5043 TO 5046 5048 5053 -650. 5055 TO 5058 5063 TO 5067 5068651. GUSSET 0.006 MEMB 3007 TO 3010 3015 3017 3020 3022 3027 3029 3032 3034 3035 -652. 3037 3040 3042 3047 3049 3052 3054 3059 TO 3062 4007 TO 4010 4015 4017 4020 -653. 4022 4027 4029 4032 4034 4035 4037 4040 4042 4047 4049 4052 4054 4059 TO 4062 -654. 5007 TO 5010 5015 5017 5020 5022 5027 5029 5032 5034 5035 5037 5040 5042 -

655. 5047 5049 5052 5054 5059 TO 5062656. TRACK 9 MEMB 1 TO 132657. TRACK 9 MEMB 269 TO 577658. TRACK 9 MEMB 1001 TO 1072 1501 TO 1612 2001 TO 2031659. TRACK 9 MEMB 197 TO 204 10476 10520 10521 10537 155 TO 166 173 TO 196 -660. 207 TO 230 235 TO 246 3018 3019 3030 3031 3038 3039 3050 3051 4018 4019 -661. 4030 4031 4038 4039 4050 4051 5018 5019 5030 5031 5038 5039 5050 5051662. TRACK 9 MEMB 140 141 145 146 151 TO 154 167 TO 170 231 TO 234 247 TO 250 255 -663. 256 260 261 133 TO 139 142 TO 144 147 TO 150 171 172 205 206 251 TO 254 -664. 257 TO 259 262 263 TO 268 3001 TO 3006 3011 TO 3014 3016 3021 3023 TO 3026 -665. 3028 3033 3036 3041 3043 3044 TO 3046 3048 3053 3055 TO 3058 3063 TO 3068 -666. 4001 TO 4006 4011 TO 4014 4016 4 021 4023 TO 4026 4028 4033 4036 4041 -667. 4043 TO 4046 4048 4053 4055 TO 4058 4063 TO 4068 5001 TO 5006 5011 TO 5014 -668. 5016 5021 5023 TO 5026 5028 5033 5036 5041 5043 TO 5046 5048 5053 -

669. 5055 TO 5058 5063 TO 5067 5068670. TRACK 9 MEMB 3007 TO 3010 3015 3017 3020 3022 3027 3029 3032 3034 3035 3037 -671. 3040 3042 3047 3049 3052 3054 3059 TO 3062 4007 TO 4010 4015 4017 4020 4022 -672. 4027 4029 4032 4034 4035 4037 4040 4042 4047 4049 4052 4054 4059 TO 4062 -673. 5007 TO 5010 5015 5017 5020 5022 5027 5029 5032 5034 5035 5037 5040 5042 -674. 5047 5049 5052 5054 5059 TO 5062675. *****LEG MEMBER STEEL DESIGN*****676. CHECK CODE MEMB 1 TO 132

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 1 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 1 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 |

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| * |< ---LENGTH (ME= 0.76 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.6 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 19.4 BOLT CAP = 43.8 3 KN fa = 234.0 |

| KL/R = 19.4 # BOLT = 26 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION |

| ==================================================== == || PASS TENSION 0.936 13 || 1108.85 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWE R.DXF -- PAGE NO. 2647

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 19.39

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 19.39

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

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ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1108853.38 N

ACTUAL AXIAL TENSILE STRESS :1108853.38 / ( 5780.0*0.820 ) : 234.04 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 2 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT |

| * |=============================| ------------ ||MEMBER 2 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.76 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.6 BOLT DIA = 16 MM FA = 249.9 |

| L/R-Z = 19.4 BOLT CAP = 43.83 KN fa = 239.7 || KL/R = 19.4 # BOLT = 26 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *|

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|* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.959 13 || 1135.66 T 0.0 0.0 0.00 ||* *||**************************************************************************|| |

|-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2649

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKN ESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 19.39

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 19.39

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1135655.88 N

ACTUAL AXIAL TENSILE STRESS :1135655.88 / ( 5780.0*0.820 ) : 239.70 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

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 BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26DXF IMPORT OF TOWER.DXF -- PAGE NO. 2650

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 3 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|--------------------------------------------- ----------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 3 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 |

| IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.76 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.6 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 19.4 BOLT CAP = 43.83 KN fa = 235.5 || KL/R = 19.4 # BOLT = 26 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 |

| C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||*************************************** ***********************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.942 13 |

| 1115.63 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||------------------------------------ -------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2651

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

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TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO

---------------------------

VALUE OF L/r : 19.39

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 19.39

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1115632.12 N

ACTUAL AXIAL TENSILE STRESS :1115632.12 / ( 5780.0*0.820 ) : 235.47 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26DXF IMPORT OF TOWER.DXF -- PAGE NO. 2652

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 4 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- |

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| Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 4 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.76 --->| RY = 7.9 |

|************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.6 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 19.4 BOLT CAP = 43.83 KN fa = 241.2 || KL/R = 19.4 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 |

| ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ============================================== ======== || PASS TENSION 0.965 13 || 1142.66 T 0.0 0.0 0.00 ||* *||**************************************************************************|| |

|-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2653

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 19.39

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 19.39

ALLOWABLE KL/r : 400.00

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 RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1142660.88 N

ACTUAL AXIAL TENSILE STRESS :1142660.88 / ( 5780.0*0.820 ) : 241.18 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2654

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 5 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 5 * | INDIAN SECTIONS | AX = 57.8 || * | S T ISA200X200X15 | --Z AY = 20.0 |

|DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.76 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.6 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 19.4 BOLT CAP = 43.83 KN fa = 240.1 || KL/R = 19.4 # BOLT = 26 FYB = 436.0 |

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| FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *|

|* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.960 13 || 1137.36 T 0.0 0.0 0.00 ||* *||************************************************** ************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2655

DETAILS OF CALCULATION

----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERN ESS RATIO

---------------------------

VALUE OF L/r : 19.39

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 19.39

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS----------------------------- ----

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1137364.00 N

ACTUAL AXIAL TENSILE STRES S :1137364.00 / ( 5780.0*0.820 ) : 240.06 MPA

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 RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26DXF IMPORT OF TOWER.DXF -- PAGE NO. 2656

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 6 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN D ESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 6 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |<---LENGTH (ME= 0.76 --->| RY = 7.9 |

|************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.6 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 19.4 BOLT CAP = 43.83 KN fa = 246.0 || KL/R = 19.4 # BOLT = 27 FYB = 436 .0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 |

| NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.984 13 || 1165.52 T 0.0 0.0 0.00 ||* *|

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|**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2657

DETAILS OF CALCULATION-------------------- --

CHECK FOR MINIMUM THICKNESS

---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 19.39

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 19.39

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1165523.75 N

ACTUAL AXIAL TENSILE STRESS :1165523.75 / ( 5780.0*0.820 ) : 246.00 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2658

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STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 7 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |================ =============| ------------ ||MEMBER 7 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.79 --->| RY = 7 .9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES |

|IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 10.0 B OLT DIA = 16 MM FA = 249.9 || L/R-Z = 20.1 BOLT CAP = 43.83 KN fa = 244.9 || KL/R = 20.1 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *|

|* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.980 13 || 1160.31 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2659

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS----------------- ----------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

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 CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 20.10

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 20.10

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERM ISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1160308.25 N

ACTUAL AXIAL TENSILE STRESS :1160308.25 / ( 5780.0*0.820 ) : 244.90 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2660

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 8 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|--------------------------------------------------------------------- -----|| Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 8 * | INDIAN SECTIONS | AX = 68.8 || * | ST ISA200X200X18 | --Z AY = 24.0 ||DESIGN CODE * | | AZ = 24.0 || IS-802 * ============= ================== SY = 297.8 |

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| * SZ = 130.7 || * |< ---LENGTH (ME= 0.79 --->| RY = 7.8 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRES SES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 10.0 BOLT DIA = 16 MM FA = 249.9 |

| L/R-Z = 20.1 BOLT CAP = 43.83 KN fa = 210.8 || KL/R = 20.1 # BOLT = 28 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||*************************************************************** ***********||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|

| FX MY MZ LOCATION || ============== ======================================== || PASS TENSION 0.843 13 || 1188.37 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||------------------------------------------------------------ --------------|DXF IMPORT OF TOWER.DXF -- PAGE NO. 2661

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS

---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICK NESS : 6.0 MM

ACTUAL THICKNESS : 18.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 20.15

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 20.15

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

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 ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1188375.38 N

ACTUAL AXIAL TENSILE STRESS :1188375.38 / ( 6881.0*0.819 ) : 210.78 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 28DXF IMPORT OF TOWER.DXF -- PAGE NO. 2662

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 9 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 9 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 1.00 --->| RY = 7.9 ||************* RZ = 3.9 || || |

|PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 12.7 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 25.7 BOLT CAP = 43.83 KN f a = 244.3 || KL/R = 25.7 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || |

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|**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.977 13 |

| 1157.28 T 0.0 0.0 0.00 ||* *||****************** ********************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2663

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 25.69

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 25.69

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1157275.88 N

ACTUAL AXIAL TENSILE STRESS :1157275.88 / ( 5780.0*0.820 ) : 244.26 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

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 SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2664

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 10 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT |

| * |=============================| ------------ ||MEMBER 10 * | INDIAN SECTIONS | AX = 68.8 || * | ST ISA200X200X18 | --Z AY = 24.0 ||DESIGN CODE * | | AZ = 24.0 || IS-802 * =============================== SY = 297.8 || * SZ = 130.7 || * |< ---LENGTH (ME= 1.00 --->| RY = 7.8 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 12.8 BOLT DIA = 16 MM FA = 249.9 |

| L/R-Z = 25.8 BOLT CAP = 43.83 KN fa = 210.3 || KL/R = 25.8 # BOLT = 28 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *|

|* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.841 13 || 1185.41 T 0.0 0.0 0.00 ||* *||************************************************************************** || ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2665

DETAILS OF CALCULATION----------------------

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 CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 18.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 25.75

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 25.75

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1185413.12 N

ACTUAL AXIAL TENSILE STRESS :1185413.12 / ( 6881.0 *0.819 ) : 210.25 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 28DXF IMPORT OF TOWER.DXF -- PAGE NO. 2666

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 11 IS NOT A TRUSS MEMBER.

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THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIA L FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 11 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 |

|DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 1. 02 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 12.9 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 26.1 BOLT CAP = 43.83 KN fa = 245.6 || KL/R = 26.1 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 |

| C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.982 13 |

| 1163.42 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2667

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 26.07

EQN. USED TO FIND KL/r : K*L/r

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 ACTUAL VALUE OF KL/r : 26.07

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 24 9.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1163424.38 N

ACTUAL AXIAL TENSILE STRESS :1163424.38 / ( 5780.0*0.820 ) : 245.56 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2668

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 12 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|------------------------------------- ------------------------------------- || Y PROPERTIES |

|************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 12 * | INDIAN SECTIONS | AX = 68.8 || * | ST ISA200X200X18 | --Z AY = 24.0 ||DESIGN CODE * | | AZ = 24.0 || IS-802 * =============================== SY = 297.8 || * SZ = 130.7 || * |< ---LENGTH (ME= 1.02 --->| RY = 7.8 ||************* RZ = 3.9 || || ||PARAMETER BOLTIN G STRESSES ||IN NEWT MM IN NEWT MM|

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|--------------- ------------- -------------|| L/R-Y = 13.0 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 26.1 BOLT CAP = 43.83 KN fa = 211.4 || KL/R = 26.1 # BOLT = 28 FYB = 436.0 || FYLD = 250.0 FVB = 218. 0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 |

| NSF = 0.8 || ||******************************* *******************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.846 13 || 1191.84 T 0.0 0.0 0.00 ||* *||**************************************************************************|| |

|---------------------------- ---------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2669

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 18.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 26.14

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 26. 14

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

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 DESIGN AXIAL FORCE : 1191836.88 N

ACTUAL AXIAL TENSILE STRESS :1191836.88 / ( 6881.0*0.819 ) : 211.39 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43. 83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 28DXF IMPORT OF TOWER.DXF -- PAGE NO. 2670

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 13 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 13 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 |

|DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.62 --->| RY = 7.9 ||************* RZ = 3. 9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 7.8 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 15.8 BO LT CAP = 43.83 KN fa = 234.6 || KL/R = 15.8 # BOLT = 26 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 |

| GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION |

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| ====================================== ================ || PASS TENSION 0.938 13 || 1111.29 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2671

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO

---------------------------

VALUE OF L/r : 15.77

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 15.77

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1111287.50 N

ACTUAL AXIAL TENSILE STRESS :1111287.50 / ( 5780.0*0.820 ) : 234.56 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

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NO. OF BOLTS REQD. : 26DXF IMPORT OF TOWER.DXF -- PAGE NO. 2672

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 14 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIE S ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 14 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.62 --->| RY = 7.9 |

|************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN N EWT MM||--------------- ------------- -------------|| L/R-Y = 7.9 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 15.8 BOLT CAP = 43.83 KN fa = 244.7 || KL/R = 15.8 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 |

| NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS T ENSION 0.979 13 || 1159.38 T 0.0 0.0 0.00 ||* *||****************************************** ********************************|

| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2673

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

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 ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 15.84

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 15.84

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS--------------------- ------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1159384.75 N

ACTUAL AXIAL TENSI LE STRESS :1159384.75 / ( 5780.0*0.820 ) : 244.71 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOW ER.DXF -- PAGE NO. 2674

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 15 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ |

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|MEMBER 15 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |<---LENGTH (ME= 0.62 --->| RY = 7.9 ||************* RZ = 3.9 || || |

|PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 7.8 BOLT DIA = 16 MM FA = 248.0 || L/R-Z = 15.8 BOLT CAP = 43.83 KN fa = 219.1 || KL/R = 15.8 # BOLT = 29 FY B = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *|

|* DESIGN SUMMARY ( KN-METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADIN G/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.883 13 || 1266.19 C 0.0 0.0 0.62 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2675

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 15.77

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 15.77

ALLOWABLE KL/r : 120.00

RESULT : PASS

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CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 248.02 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1266191.00 N

ACTUAL AXIAL COMP. STRESS :1266191.00 / 5780.0 : 219.06 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2676

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 29DXF IMPORT OF TOWER.DXF -- PAGE NO. 2677

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 16 IS NOT A TRU SS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 16 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X 200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 |

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| * |< ---LENGTH (ME= 0.62 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 7.9 BOLT DIA = 16 MM FA = 248.0 || L/R-Z = 15.8 BOLT CAP = 43.83 KN fa = 226.4 |

| KL/R = 15.8 # BOLT = 30 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CR ITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION |

| ====================================================== || PASS COMPRESSION 0. 913 13 || 1308.38 C 0.0 0.0 0.62 ||* *||************************************************************ **************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2678

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 15.84

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 15.84

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

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Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 248.00 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1308378.62 N

ACTUAL AXIAL COMP. STRESS :1308378.62 / 5780.0 : 226.36 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2679

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2680

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 17 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- |

| Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 17 * | INDIAN SECTIONS | AX = 5 7.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 1.02 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES |

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|IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 12.9 BOLT DIA = 16 MM FA = 244.7 || L/R-Z = 26.1 BOLT CAP = 43.83 KN fa = 227.8 || KL/R = 26.1 # BOLT = 31 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 |

| ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.931 13 || 1316.68 C 0.0 0.0 1.02 ||* *||********************** ****************************************************|

| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2681

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 26.07

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 26.07

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

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(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 244.69 MPA

CHECK AGAINST PERMISSIBLE STRESS

--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1316679.50 N

ACTUAL AXIAL COMP. STRESS :1316679.50 / 5780.0 : 227.80 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2682

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 4 3.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 31DXF IMPORT OF TOWER.DXF -- PAGE NO. 2683

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 18 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 18 * | INDIAN SECTIO NS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 |

|DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 1.02 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 12.9 BOLT DIA = 16 MM FA = 244.7 || L/R-Z = 26.1 BOLT CAP = 43.83 KN fa = 232.7 || KL/R = 26.1 # BOLT = 31 FYB = 436.0 |

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| FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *|

|* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ==================================== ================== || PASS COMPRESSION 0.951 13 || 1344.96 C 0.0 0.0 1.02 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2684

DETAILS OF CALCULATION

----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO

---------------------------

VALUE OF L/r : 26.07

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 26.07

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

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 ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 244.69 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1344960.50 N

ACTUAL AXIAL COMP. STRESS :1344960.50 / 5780.0 : 232.69 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2685

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 31DXF IMPORT OF TOWER.DXF -- PAGE NO. 2686

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 19 IS NOT A TRUSS MEMBER.

THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|----------------------------------------------------- --------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 19 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 1.00 --->| RY = 7.9 ||************* RZ = 3.9 |

| || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 12.7 BOLT DIA = 16 MM FA = 2 44.8 || L/R-Z = 25.7 BOLT CAP = 43.83 KN fa = 226.9 || KL/R = 25.7 # BOLT = 30 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 |

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| NSF = 1.0 || ||*********************************************** ***************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION |

| ====================================================== || PASS COMPRESSION 0.927 13 || 1311.29 C 0.0 0.0 1.00 ||* *||**************************************************************************|| ||-------------------------------------------- ------------------------------ |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2687

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 25.69

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 25.69

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 244.85 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

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 LOAD NO. : 13

DESIGN AXIAL FORCE : 1311286.88 N

ACTUAL AXIAL COMP. STRESS :1311286.88 / 5780.0 : 226.87 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2688

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30DXF IMPORT OF TOWER.DXF -- PAGE NO. 2689

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 20 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES |

|************* | IN CM UNIT || * |================== ===========| ------------ ||MEMBER 20 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 1.00 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|

| L/R-Y = 12.7 BOL T DIA = 16 MM FA = 244.8 || L/R-Z = 25.7 BOLT CAP = 43.83 KN fa = 231.5 || KL/R = 25.7 # BOLT = 31 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *|

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|* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.946 13 || 1338.19 C 0.0 0.0 1.00 ||* *||**************************************************************************|

| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2690

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS------------------- --------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 25.69

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 25.69

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 244.85 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1338194.62 N

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ACTUAL AXIAL COMP. STRESS :1338194.62 / 5780.0 : 231.52 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2691

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 31DXF IMPORT OF TOWER.DXF -- PAGE NO. 2692

STAAD.Pro MEMBER SELECTION - (I802)

**************************

WARNING : THE MEMBER 21 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 21 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 |

| IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.77 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.8 BOLT DIA = 16 MM FA = 246.9 || L/R-Z = 19.8 BOLT CAP = 43.83 KN fa = 232.1 || KL/R = 19.8 # BOLT = 31 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 |

| C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== |

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| PASS COMPRESSION 0.940 13 || 1341.53 C 0 .0 0.0 0.77 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2693

DETAILS OF CALCULATION

----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 19.78

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 19.78

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159 265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 246.92 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1341532.88 N

ACTUAL AXIAL COMP. STRESS :1341532.88 / 5780.0 : 232.10 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2694

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 BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 31DXF IMPORT OF TOWER.DXF -- PAGE NO. 2695

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 22 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 22 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.77 --->| RY = 7.9 ||************* RZ = 3.9 || |

| ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.8 BOLT DIA = 16 MM FA = 246.9 || L/R-Z = 19.8 BOLT CAP = 43.83 KN fa = 237.0 || KL/R = 19.8 # BOLT = 32 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || |

|**************************************************************************||* *||* DESIG N SUMMARY ( KN-METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.960 13 || 1370.01 C 0.0 0.0 0.77 ||* *||**************************************************************************|| |

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|-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2696

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO------------------------- --

VALUE OF L/r : 19.78

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 19.78

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSI ON

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS

: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 246.92 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1370014.50 N

ACTUAL AXIAL COMP. STRESS :1370014.50 / 5780.0 : 237.03 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2697

BOLTING-------

BOLT DIA : 16 MM

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 SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 32DXF IMPORT OF TOWER.DXF -- PAGE NO. 2698

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 23 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT |

| * |=============================| ------------ ||MEMBER 23 * | INDIAN SECTIONS | AX = 57.8 || * | S T ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.77 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.8 BOLT DIA = 16 MM FA = 246.9 |

| L/R-Z = 19.7 BOLT CAP = 43.83 KN fa = 228.6 || KL/R = 19.7 # BOLT = 31 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *|

|* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSI ON 0.926 13 || 1321.35 C 0.0 0.0 0.77 ||* *||************************************************** ************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2699

DETAILS OF CALCULATION----------------------

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 CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERN ESS RATIO---------------------------

VALUE OF L/r : 19.72

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 19.72

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS------------------------------- --

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 246.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1321347.12 N

ACTUAL AXIAL COMP. STRESS :1321347.12 / 5780.0 : 228.61 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2700

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

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BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 31DXF IMPORT OF TOWER.DXF -- PAGE NO. 2701

STAAD.Pro MEMBER SELECTION - (I802)

************************* *

WARNING : THE MEMBER 24 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 24 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 |

| * SZ = 112.6 || * |< ---LENGTH (ME= 0.77 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.8 BOLT DIA = 16 MM FA = 246.9 || L/R-Z = 19.7 BOLT CAP = 43.83 KN fa = 233.4 || KL/R = 19.7 # BOLT = 31 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 |

| LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.945 13 || 1349.32 C 0.0 0.0 0.77 |

|* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2702

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

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 MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 19.72

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 19.72

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STR ESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 246.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1349325.62 N

ACTUAL AXIAL COMP. STRESS :1349325.62 / 5780.0 : 233.45 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2703

BOLTING

-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 31DXF IMPORT OF TOWER.DXF -- PAGE NO. 2704

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STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 25 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 25 * | IND IAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * ========================= ====== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.76 --->| RY = 7.9 ||************* RZ = 3.9 || || |

|PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.6 BOLT DIA = 16 MM FA = 247.0 || L/R-Z = 19.4 BOLT CAP = 43.83 KN fa = 220.7 || KL/R = 19.4 # BOLT = 30 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************|

|* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ========================== ============================ || PASS COMPRESSION 0.893 13 || 1275.68 C 0.0 0.0 0.76 ||* *||**************************************************************************|| ||------------------------------------------------------------------------ --|DXF IMPORT OF TOWER.DXF -- PAGE NO. 2705

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 M M

ACTUAL THICKNESS : 15.0 MM

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RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 19.39

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 19.39

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 247.04 MPA

CHECK AGAINST PERMISSIBLE STRESS------------------------ --------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1275680.50 N

ACTUAL AXIAL COMP. STRESS :1275680.50 / 5780.0 : 220.71 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2706

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30DXF IMPORT OF TOWER.DXF -- PAGE NO. 2707

STAAD.Pro MEMBER SELECTION - (I802)**************************

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WARNING : THE MEMBER 26 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|------------------------------------------- ------------------------------- || Y PROPERTIES ||************* | IN CM UNIT |

| * |=============================| ------------ ||MEMBER 26 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.76 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.6 BOLT DIA = 16 MM FA = 247.0 || L/R-Z = 19.4 BOLT CAP = 43.83 KN fa = 225.3 |

| KL/R = 19.4 # BOLT = 30 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||************************************* *************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|

| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.912 13 || 1302.45 C 0.0 0.0 0.76 ||* *||**************************************************************************|| ||---------------------------------- ---------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2708

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS

---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

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VALUE OF L/r : 19.39

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 19.39

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 247.04 MPA

CHECK AGAINST PERMISSI BLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1302450.00 N

ACTUAL AXIAL COMP. STRESS :1302450.00 / 5780.0 : 225.34 MPA

RESULT : PASS

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2709

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30DXF IMPORT OF TOWER.DXF -- PAGE NO. 2710

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 27 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

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 |-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |======== =====================| ------------ ||MEMBER 27 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 |

| * SZ = 112.6 || * |< ---LENGTH (ME= 0.76 --->| R Y = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.6 BOLT DIA = 16 MM FA = 247.0 || L/R-Z = 19.4 BOLT CAP = 43.83 KN fa = 219.1 || KL/R = 19.4 # BOLT = 29 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 |

| ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.887 13 || 1266.20 C 0.0 0.0 0.76 ||* *|

|**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2711

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 19.39

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 19.39

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 ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 247.04 MPA

CHECK AGAINST PERMISSIBLE STRESS

--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1266199.88 N

ACTUAL AXIAL COMP. STRESS :1266199.88 / 5780.0 : 219.07 MPA

RESULT : PASSDXF IMPORT OF TOWER .DXF -- PAGE NO. 2712

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 29DXF IMPORT OF TOWER.DXF -- PAGE NO. 2713

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 28 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CO NSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ |

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|MEMBER 28 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.76 --->| RY = 7.9 ||************* RZ = 3.9 || || |

|PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.6 BOLT DIA = 16 MM FA = 247.0 || L/R-Z = 19.4 BOLT CAP = 43.83 KN fa = 223.7 || KL/R = 19.4 # BOLT = 30 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *|

|* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.905 13 || 1292.79 C 0.0 0.0 0.76 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2714

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 19.3 9

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 19.39

ALLOWABLE KL/r : 120.00

RESULT : PASS

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CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1-0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 247.04 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1292795.38 N

ACTUAL AXIAL COMP. STRESS :1292795.38 / 5780.0 : 223.67 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2715

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30DXF IMPORT OF TOWER.DXF -- PAGE NO. 2716

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 29 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 29 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 |

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| * |< ---LENGTH (ME= 0.45 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 5.7 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 11.6 BOLT CAP = 43.83 KN fa = 237.4 |

| KL/R = 11.6 # BOLT = 26 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ R ATIO/ LOADING/ *|| FX MY MZ LOCATION |

| ====================================================== || PASS TENSION 0.950 13 || 1124.69 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2717

DETAILS OF CALCULA TION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 11.55

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 11.55

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

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ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1124693.50 N

ACTUAL AXIAL TENSILE STRESS :1124693.50 / ( 5780.0*0.8 20 ) : 237.39 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26DXF IMPORT OF TOWER.DXF -- PAGE NO. 2718

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 30 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FO RCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 30 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.45 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES |

|IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 5.7 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 11.5 BOLT CAP = 43.83 KN fa = 245.6 || KL/R = 11.5 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************|

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|* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.983 13 || 1163.54 T 0.0 0.0 0.00 |

|* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2719

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM TH ICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 11.48

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 11.48

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1163536.62 N

ACTUAL AXIAL TENSILE STRESS :1163536.62 / ( 5780.0*0.820 ) : 245.59 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

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SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2720

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 31 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|----------------------------------------- --------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ |

|MEMBER 31 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.66 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 8.4 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 17.0 BOLT CAP = 43.83 KN fa = 239.9 |

| KL/R = 17.0 # BOLT = 26 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||*********************************** ***************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|

| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.960 13 || 1136.72 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------- ------------------------------------------ |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2721

DETAILS OF CALCULATION----------------------

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CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 17.00

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 17.00

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1136717.00 N

ACTUAL AXIAL TENSILE STRESS :1136717.00 / ( 5780.0*0.820 ) : 239.92 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 K N

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26DXF IMPORT OF TOWER.DXF -- PAGE NO. 2722

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 32 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

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|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 32 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 |

| IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.66 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 8.4 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 17.0 BOLT C AP = 43.83 KN fa = 245.2 || KL/R = 17.0 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 |

| LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ========================================== ============ || PASS TENSION 0.981 13 || 1161.89 T 0.0 0.0 0.00 |

|* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2723

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 17.00

EQN. USED TO FIND KL/r : K*L/r

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ACTUAL VALUE OF KL/r : 17.00

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1161891.75 N

ACTUAL AXIAL TENSILE STRESS :1161891.75 / ( 5780.0*0.820 ) : 245.24 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2724

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 3 3 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT |

| * |=============================| ------------ ||MEMBER 33 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.68 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|

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| L/R-Y = 8.6 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 17.4 BOLT CAP = 43.83 KN fa = 239.2 || KL/R = 17.4 # BOLT = 26 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 |

| ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSI ON 0.957 13 || 1133.19 T 0.0 0.0 0.00 ||* *||********************************************** ****************************|| ||-------------------------------------------------------------------------- |

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2725

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 17.38

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 17.38

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS------------------------- --------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

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DESIGN AXIAL FORCE : 1133186.88 N

ACTUAL AXIAL TENSILE S TRESS :1133186.88 / ( 5780.0*0.820 ) : 239.18 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26DXF IMPORT OF TOWER.D XF -- PAGE NO. 2726

STAAD.Pro MEMBER SELECTION - (I802)

**************************

WARNING : THE MEMBER 34 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 34 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 |

| IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |<---LENGTH (ME= 0.68 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 8.6 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 17.4 BOLT CAP = 43.83 KN fa = 243.2 || KL/R = 17.4 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 |

| C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== |

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DXF IMPORT OF TOWER.DXF -- PAGE NO. 2728

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 35 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |============ =================| ------------ ||MEMBER 35 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.65 --->| RY = 7.9 ||************* RZ = 3.9 |

| || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 8.2 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 16.5 BOLT CAP = 43.83 KN fa = 240.5 || KL/R = 16.5 # BOLT = 26 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 |

| ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY M Z LOCATION || ====================================================== || PASS TENSION 0.962 13 || 1139.42 T 0.0 0.0 0.00 ||* *||**************************************************************************|| |

|-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2729

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

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ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 16.54

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 16.54

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1139417.62 N

ACTUAL AXIAL TENSILE STRESS :1139417.62 / ( 5780.0*0.820 ) : 240.49 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26DXF IMPORT OF TOWER.DXF -- PAGE NO. 2730

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 36 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|----------------------------------------------------------------- ---------|| Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 36 * | INDIAN SECTIONS | AX = 57.8 |

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| * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.65 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING S TRESSES |

|IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 8.2 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 16.6 BOLT CAP = 43.83 KN fa = 245.3 || KL/R = 16.6 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||*********************************************************** ***************||* *||* DESIGN SUMMARY ( KN -METR) *|

|* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.981 13 || 1162.02 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------- ------------------|DXF IMPORT OF TOWER.DXF -- PAGE NO. 2731

DETAILS OF CALCULATION

----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO

---------------------------

VALUE OF L/r : 16.61

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 16.61

ALLOWABLE KL/r : 400 .00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS

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---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1162016.38 N

ACTUAL AXIAL TENSILE STRESS :1162016.38 / ( 5780.0*0.820 ) : 245.26 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69 .76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2732

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 37 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 37 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 1.10 --->| RY = 7.9 |

|************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 14.0 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 28.2 BOLT CAP = 43.83 KN fa = 227.0 || KL/R = 28.2 # BOLT = 25 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 |

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| ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|

| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.908 13 || 1075.39 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2733

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 28.16

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 28.16

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STR ESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1075389. 12 N

ACTUAL AXIAL TENSILE STRESS :1075389.12 / ( 5780.0*0.820 ) : 226.98 MPA

RESULT : PASS

BOLTING

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-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 25DXF IMPORT OF TOWER.DXF -- PAGE NO. 2734

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 38 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 38 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 1.10 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES |

|IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 13.9 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 28.1 BOLT CAP = 43.83 KN fa = 229.4 || KL/R = 28.1 # BOLT = 25 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *|

|* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL CON D/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.918 13 || 1086.90 T 0.0 0.0 0.00 ||* *||********************************************************************** ****|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2735

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 DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 28.08

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 28.08

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1086899.75 N

ACTUAL AXIAL TENSILE STRESS :1086899.75 / ( 57 80.0*0.820 ) : 229.41 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 25DXF IMPORT OF TOWER.DXF -- PAGE NO. 2736

STAAD.Pro MEMBER SELECTION - (I802)**************************

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WARNING : THE MEMBER 39 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT |

| * |=============================| ------------ ||MEMBER 39 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.71 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.0 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 18.2 BOLT CAP = 43.83 KN fa = 228.4 |

| KL/R = 18.2 # BOLT = 25 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|

| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.914 13 || 1082.16 T 0 .0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2737

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS

---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

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VALUE OF L/r : 18.16

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 18.16

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1082159.25 N

ACTUAL AXIAL TENSILE STRESS :1082159.25 / ( 5780.0*0.820 ) : 228.41 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 25DXF IMPORT OF TOWER.DXF -- PAGE NO. 2738

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 40 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|--------------------------------- ----------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 40 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20. 0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.71 --->| RY = 7.9 ||************* RZ = 3.9 || |

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| ||PARAMETER BO LTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.0 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 18.2 BOLT CAP = 43.83 KN fa = 231.1 || KL/R = 18.2 # BOLT = 25 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 |

| C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||*************************** ***********************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.925 13 || 1095.05 T 0.0 0.0 0.00 |

|* *||**************************************************************************|| ||------------------------ -------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2739

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 18.16

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 18.16

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS

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--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1095055.12 N

ACTUAL AXIAL TENSILE STRESS :1095055.12 / ( 5780.0*0.820 ) : 231.13 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 25DXF IMPORT OF TOWER.DXF -- PAGE NO. 2740

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 41 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT |

| * |=============================| ------------ ||MEMBER 41 * | INDIAN SECT IONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.69 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 8.8 BOLT DIA = 16 MM FA = 249.9 |

| L/R-Z = 17.8 BOLT CAP = 43.83 KN fa = 217.5 || KL/R = 17.8 # BOLT = 24 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *|

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|* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ================================== ==================== || PASS TENSION 0.870 13 || 1030.29 T 0.0 0.0 0.00 ||* *||**************************************************************************|| |

|-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2741

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 17.77

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 17.77

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1030285.69 N

ACTUAL AXIAL TENSILE STRESS :1030285.69 / ( 5780.0*0.820 ) : 217.46 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

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 BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 24DXF IMPORT OF TOWER.DXF -- PAGE NO. 2742

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMB ER 42 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPE RTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 42 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 |

| IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.69 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 8.8 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 17.8 BOLT CAP = 43.83 KN fa = 222.2 || KL/R = 17.8 # BOLT = 25 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 |

| C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.889 13 |

| 1052.87 T 0.0 0.0 0.00 ||* *||************************************** ************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2743

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

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TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO

---------------------------

VALUE OF L/r : 17.77

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 17.77

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS----------------- ----------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1052869.88 N

ACTUAL AXIAL TENSILE STRESS :1052869.88 / ( 5780.0*0.820 ) : 222.23 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 25DXF IMPORT OF TOWER.DXF -- PAGE NO. 2744

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 43 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- |

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| Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 43 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |<---LENGTH (ME= 0.54 --->| RY = 7.9 |

|************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 6.9 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 13.9 BOLT CAP = 43.83 KN fa = 222.2 || KL/R = 13.9 # BOLT = 25 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 |

| ||**************************************************************************||* *||* DESIGN SUMM ARY ( KN-METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LO ADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.889 13 || 1052.67 T 0.0 0.0 0.00 ||* *||**************************************************************************|| |

|-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2745

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 13.85

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 13.85

ALLOWABLE KL/r : 400.00

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 RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1052672.75 N

ACTUAL AXIAL TENSILE STRESS :1052672.75 / ( 5780.0*0.820 ) : 222.19 M PA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 25DXF IMPORT OF TOWER.DXF -- PAGE NO. 2746

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 44 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |==== =========================| ------------ ||MEMBER 44 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 |

|DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.54 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 6.9 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 13.9 BOLT CAP = 43.83 KN fa = 226.8 || KL/R = 13.9 # BOLT = 25 FYB = 436.0 |

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| FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *|

|* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.907 13 || 1074.37 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2747

DETAILS OF CALCULATION

----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO

---------------------------

VALUE OF L/r : 13.85

EQN. USED TO FIND KL/r : K* L/r

ACTUAL VALUE OF KL/r : 13.85

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1074365.88 N

ACTUAL AXIAL TENSILE STRESS :1074365.88 / ( 5780.0*0.820 ) : 226.76 MPA

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 RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 25DXF IMPORT OF TOWER.DXF -- PAGE NO. 2748

STAAD.Pro MEMBER SELEC TION - (I802)**************************

WARNING : THE MEMBER 45 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|--------------------------------------------------------- -----------------|| Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 45 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.57 --->| RY = 7.9 |

|************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 7.2 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 14.5 BOLT CAP = 43.83 KN fa = 247.2 || KL/R = 14.5 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 |

| NSF = 0.8 || ||*************************************************** ***********************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.989 13 || 1171.00 T 0.0 0.0 0.00 ||* *|

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|**************************************************************************|| ||------------------------------------------------ -------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2749

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS

---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 14.55

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 14.55

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS-------------------------- ------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1171003.00 N

ACTUAL AXIAL TENSILE STRESS :1171003.00 / ( 5780.0*0.820 ) : 247.16 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2750

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STAAD.Pro MEMBER SELECTION - (I802)******************* *******

WARNING : THE MEMBER 46 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 46 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.57 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES |

|IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 7.2 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 14.5 BOLT CAP = 43.83 KN fa = 249.7 || KL/R = 14.5 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *|

|* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.999 13 || 1182.98 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2751

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 M M

RESULT : PASS

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 CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 14.55

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 14.55

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1182982.50 N

ACTUAL AXIAL TENSILE STRESS :1182982.50 / ( 5780.0*0.820 ) : 249.69 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2752

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 47 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 47 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X20 0X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 |

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| * SZ = 112.6 || * |< ---LENGTH (ME= 0.57 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 7.2 BOLT DIA = 16 MM FA = 248.3 |

| L/R-Z = 14.5 BOLT CAP = 43.83 KN fa = 222.3 || KL/R = 14.5 # BOLT = 30 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRIT ICAL COND/ RATIO/ LOADING/ *|

| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.89 5 13 || 1284.63 C 0.0 0.0 0.57 ||* *||************************************************************** ************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2753

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS

---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 14.55

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 14.55

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

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 Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 248.31 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1284630.38 N

ACTUAL AXIAL COMP. STRESS :1284630.38 / 5780.0 : 222.25 MPA

RESULT : PASS

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2754

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30DXF IMPORT OF TOWER.DXF -- PAGE NO. 2755

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 48 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 48 * | INDIAN SECTIONS | AX = 57. 8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.57 --->| RY = 7.9 ||************* RZ = 3.9 || || |

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|PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 7.2 BOLT DIA = 16 MM FA = 248.3 || L/R-Z = 14.5 BOLT CAP = 43.83 KN fa = 224.8 || KL/R = 14.5 # BOLT = 30 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 |

| LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.905 13 || 1299.59 C 0.0 0.0 0.57 ||* *|

|************************ **************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2756

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 14.55

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 14.55

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

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 (b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 248.31 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1299590.12 N

ACTUAL AXIAL COMP. STRESS :1299590.12 / 5780.0 : 224.84 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2757

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43. 83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30DXF IMPORT OF TOWER.DXF -- PAGE NO. 2758

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 49 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 49 * | INDIAN SECTIONS | AX = 50.2 |

| * | ST ISA200X150X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 15.0 || IS-802 * =============================== SY = 181.9 || * SZ = 76.0 || * |< ---LENGTH (ME= 0.54 --->| RY = 7.1 ||************* RZ = 3. 2 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 7.7 BOLT DIA = 16 MM FA = 247.7 || L/R-Z = 16.9 BO LT CAP = 43.83 KN fa = 231.1 |

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| KL/R = 16.9 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************|

|* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================== ================ || PASS COMPRESSION 0.933 13 || 1161.31 C 0.0 0.0 0.45 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2759

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 16.93

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 16.93

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS

---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 13.5 : 171.5 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.43

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(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 247.73 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1161306.88 N

ACTUAL AXIAL COMP. STRESS :1161306.88 / 5025.0 : 231.11 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2760

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2761

STAAD.Pro MEMBER SEL ECTION - (I802)**************************

WARNING : THE MEMBER 50 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|------------------------------------------------------- ------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 50 * | INDIAN SECTIONS | AX = 50.2 || * | ST ISA200X150X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 15.0 || IS-802 * =============================== SY = 181.9 || * SZ = 76.0 || * |< ---LENGTH (ME= 0.54 --->| RY = 7.1 |

|************* RZ = 3.2 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 7.7 BOLT DIA = 16 MM FA = 247 .7 || L/R-Z = 16.9 BOLT CAP = 43.83 KN fa = 234.8 || KL/R = 16.9 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 |

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| ELA = 1.0 || NSF = 1.0 || ||************************************************* *************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|

| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.948 13 || 1179.81 C 0.0 0.0 0.45 ||* *||**************************************************************************|| ||---------------------------------------------- ---------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2762

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 16.93

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 16.93

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 13.5 : 171.5 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.43

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 247.73 MPA

CHECK AGAINST PERMISSIBLE STRESS

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--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1179814.50 N

ACTUAL AXIAL COMP. STRESS :1179814.50 / 5025.0 : 234.79 MPA

RESULT : PASS

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2763

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2764

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 51 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- |

| Y PROPERTIES ||************* | IN CM UNIT || * |==================== =========| ------------ ||MEMBER 51 * | INDIAN SECTIONS | AX = 50.2 || * | ST ISA200X150X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 15.0 || IS-802 * =============================== SY = 181.9 || * SZ = 76.0 || * |< ---LENGTH (ME= 0.69 --->| RY = 7.1 ||************* RZ = 3.2 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM|

|--------------- ------------- -------------|| L/R-Y = 9.8 BOLT DIA = 16 MM FA = 246.3 || L/R-Z = 21.7 BOLT CAP = 43.83 KN fa = 226.2 || KL/R = 21.7 # BOLT = 26 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *|

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|* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.918 13 || 1136.75 C 0.0 0.0 0.69 ||* *|

|**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2765

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS--------------------- ------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 21.71

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 21.71

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 13.5 : 171.5 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.43

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 246.30 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1136746.12 N

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 ACTUAL AXIAL COMP. STRESS :1136746.12 / 5025.0 : 226.22 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2766

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26DXF IMPORT OF TOWER.DXF -- PAGE NO. 2767

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 52 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AX IAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 52 * | INDIAN SECTIONS | AX = 50.2 || * | ST ISA200X150X15 | --Z AY = 20.0 |

|DESIGN CODE * | | AZ = 15.0 || IS-802 * =============================== SY = 181.9 || * SZ = 76.0 || * |< ---LENGTH (ME= 0.69 --->| RY = 7.1 ||************* RZ = 3.2 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.8 BOLT DIA = 16 MM FA = 246.3 || L/R-Z = 21.7 BOLT CAP = 43.83 KN fa = 229.9 || KL/R = 21.7 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 |

| GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION |

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| ====================================================== || PASS COMPRESSION 0.933 13 || 1155.16 C 0.0 0.0 0.69 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2768

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO

---------------------------

VALUE OF L/r : 21.71

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 21.71

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.1415926 5*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 13.5 : 171.5 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.43

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 246.30 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1155161.12 N

ACTUAL AXIAL COMP. STRESS :1155161.12 / 5025.0 : 229.88 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2769

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BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2770

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 53 IS NOT A TRUSS MEMBER.

THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 53 * | INDIAN SECTIONS | AX = 50.2 || * | ST ISA200X150X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 15.0 || IS-802 * =============================== SY = 181.9 || * SZ = 76.0 || * |< ---LENGTH (ME= 0.71 --->| RY = 7.1 ||************* RZ = 3.2 |

| || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 10.0 BOLT DIA = 16 MM FA = 246.1 || L/R-Z = 22.2 BOLT CAP = 43.83 KN fa = 238.7 || KL/R = 22.2 # BOLT = 28 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 |

| ||**************************************************************************||* *||* DESIGN SUMMARY ( KN-METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.970 13 || 1199.63 C 0.0 0.0 0.71 ||* *||**************************************************************************|

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| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2771

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 22.18

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 22.18

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 13.5 : 171.5 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.43

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 246.14 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1199634.75 N

ACTUAL AXIAL COMP. STRESS :1199634.75 / 5025.0 : 238.73 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2772

BOLTING-------

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BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 28

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2773

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 54 IS N OT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES |

|************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 54 * | INDIAN SECTIONS | AX = 50.2 || * | ST ISA200X150X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 15.0 || IS-802 * =============================== SY = 181.9 || * SZ = 76.0 || * |< ---LENGTH (ME= 0.71 --->| RY = 7.1 ||************* RZ = 3.2 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|

| L/R-Y = 10.0 BOLT DIA = 16 MM FA = 246.1 || L/R-Z = 22.2 BOLT CAP = 43.83 KN fa = 241.2 || KL/R = 22.2 # BOLT = 28 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* * ||* DESIGN SUMMARY ( KN -METR) *||* -------------- *|

|* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.980 13 || 1211.95 C 0.0 0.0 0.71 ||* *||**************************************************** **********************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2774

DETAILS OF CALCULATION

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----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNES S RATIO---------------------------

VALUE OF L/r : 22.18

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 22.18

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 13.5 : 171.5 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.43

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 246.14 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1211949.38 N

ACTUAL AXIAL COMP. STRESS :1211949.38 / 5025.0 : 241.18 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2775

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69 .76 KN

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 BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 28DXF IMPORT OF TOWER.DXF -- PAGE NO. 2776

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 55 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 55 * | INDIAN SECTIONS | AX = 50.2 || * | ST ISA200X150X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 15.0 |

| IS-802 * =============================== SY = 181.9 || * SZ = 76.0 || * |< ---LENGTH (ME= 1.10 --->| RY = 7.1 ||************* RZ = 3.2 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 15.6 BOLT DIA = 16 MM FA = 240.8 || L/R-Z = 34.4 BOLT CAP = 43.83 KN fa = 237.6 || KL/R = 34.4 # BOLT = 28 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 |

| C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.987 13 |

| 1194.02 C 0.0 0.0 1.10 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2777

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

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TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO

---------------------------

VALUE OF L/r : 34.40

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 34.40

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRES S---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 13.5 : 171.5 MM

(b/t)lim : 210/sqrt(fy) : 1 3.28

(b/t)cal : 11.43

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 240.81 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1194022.00 N

ACTUAL AXIAL COMP. STRESS :1194022.00 / 5025.0 : 237.62 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2778

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 28DXF IMPORT OF TOWER.DXF -- PAGE NO. 2779

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STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 56 IS NOT A TRUSS MEMBER.

THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 56 * | INDIA N SECTIONS | AX = 50.2 || * | ST ISA200X150X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 15.0 || IS-802 * =========================== ==== SY = 181.9 || * SZ = 76.0 || * |< ---LENGTH (ME= 1.10 --->| RY = 7.1 ||************* RZ = 3.2 || |

| ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 15.5 BOLT DIA = 16 MM FA = 240.9 || L/R-Z = 34.3 BOLT CAP = 43.83 KN fa = 239.9 || KL/R = 34.3 # BOLT = 28 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || |

|**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ============================ ========================== || PASS COMPRESSION 0.996 13 || 1205.68 C 0.0 0.0 1.10 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2780

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

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 RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 34.31

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 34.31

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS

: 200.0 - 15.0 - 13.5 : 171.5 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.43

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 240.86 MPA

CHECK AGAINST PERMISSIBLE STRESS-------------------------- ------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1205680.75 N

ACTUAL AXIAL COMP. STRESS :1205680.75 / 5025.0 : 239.94 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2781

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 28DXF IMPORT OF TOWER.DXF -- PAGE NO. 2782

STAAD.Pro MEMBER SELECTION - (I802)

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**************************

WARNING : THE MEMBER 57 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|--------------------------------------------- ----------------------------- || Y PROPERTIES |

|************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 57 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.65 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 8.2 BOLT DIA = 16 MM FA = 247.8 |

| L/R-Z = 16.5 BOLT CAP = 43.83 KN fa = 220.5 || KL/R = 16.5 # BOLT = 30 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||*************************************** ***********************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *|

|* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.890 13 || 1274.72 C 0.0 0.0 0.65 ||* *||**************************************************************************|| ||------------------------------------ -------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2783

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

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 VALUE OF L/r : 16.54

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 16.54

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 247.83 MPA

CHECK AGAINST PERMISSIBL E STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1274722.25 N

ACTUAL AXIAL COMP. STRESS :1274722.25 / 5780.0 : 220.54 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2784

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30DXF IMPORT OF TOWER.DXF -- PAGE NO. 2785

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 58 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

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|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |========== ===================| ------------ ||MEMBER 58 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 |

| IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.65 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 8.2 BOLT DIA = 16 MM FA = 247.8 || L/R-Z = 16.6 BOLT CAP = 43.83 KN fa = 224.5 || KL/R = 16.6 # BOLT = 30 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 |

| LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.906 13 || 1297.74 C 0.0 0.0 0. 65 |

|* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2786

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 16.61

EQN. USED TO FIND KL/r : L/r

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ACTUAL VALUE OF KL/r : 16.61

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 24 7.81 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1297742.75 N

ACTUAL AXIAL COMP. STRESS :1297742.75 / 5780.0 : 224.52 MPA

RESULT : PASSDXF IMPORT OF TOWER.D XF -- PAGE NO. 2787

BOLTING

-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30DXF IMPORT OF TOWER.DXF -- PAGE NO. 2788

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 59 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONS IDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT |

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| * |=============================| ------------ ||MEMBER 59 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.68 --->| RY = 7.9 ||************* RZ = 3.9 || |

| ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 8.6 BOLT DIA = 16 MM FA = 247.6 || L/R-Z = 17.4 BOLT CAP = 43.83 KN fa = 219.6 || KL/R = 17.4 # BOLT = 29 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************|

|* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.887 13 || 1269.01 C 0.0 0.0 0.68 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2789

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 17.38

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 17.38

ALLOWABLE KL/r : 120.00

RESULT : PASS

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 CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265 *3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS

: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1-0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 247.61 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1269013.62 N

ACTUAL AXIAL COMP. STRESS :1269013.62 / 5780.0 : 219.55 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2790

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 29DXF IMPORT OF TOWER.DXF -- PAGE NO. 2791

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 60 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 60 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 |

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| * SZ = 112.6 || * |< ---LENGTH (ME= 0.68 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 8.6 BOLT DIA = 16 MM FA = 247.6 |

| L/R-Z = 17.4 BOLT CAP = 43.83 KN fa = 222.9 || KL/R = 17.4 # BOLT = 30 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RAT IO/ LOADING/ *|

| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.900 13 || 1288.17 C 0.0 0.0 0.68 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2792

DETAILS OF CALCULATI ON----------------------

CHECK FOR MINIMUM THICKNESS

---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO----------------- ----------

VALUE OF L/r : 17.38

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 17.38

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : C OMPRESSION

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 Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= C c

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 247.61 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1288168.25 N

ACTUAL AXIAL COMP. STRESS :128 8168.25 / 5780.0 : 222.87 MPA

RESULT : PASS

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2793

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30DXF IMPORT OF TOWER.DXF -- PAGE NO. 2794

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 61 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIE S ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 61 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.66 --->| RY = 7.9 ||************* RZ = 3.9 || || |

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|PARAMETER BOLTING STRESSES ||IN NEWT MM IN N EWT MM||--------------- ------------- -------------|| L/R-Y = 8.4 BOLT DIA = 16 MM FA = 247.7 || L/R-Z = 17.0 BOLT CAP = 43.83 KN fa = 221.2 || KL/R = 17.0 # BOLT = 30 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 |

| LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS C OMPRESSION 0.893 13 || 1278.59 C 0.0 0.0 0.66 ||* *|

|****************************************** ********************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2795

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 17.00

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 17.00

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS----------------------- ----------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

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 (b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 247.71 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1278592.12 N

ACTUAL AXIAL COMP. STRESS :1278592.12 / 5780.0 : 221.21 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2796

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30DXF IMPORT OF TOWER.DXF -- PAGE NO. 2797

STAAD.Pro MEMBER SELECTION - (I802)***************** *********

WARNING : THE MEMBER 62 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 62 * | INDIAN SECTIONS | AX = 57.8 |

| * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254 .1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.66 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 8.4 BOLT DIA = 16 MM FA = 247.7 || L/R-Z = 17.0 BOLT CAP = 43.83 KN fa = 225.5 |

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| KL/R = 17.0 # BOLT = 30 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************|

|* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.910 13 || 1303.21 C 0.0 0.0 0.66 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DX F -- PAGE NO. 2798

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 17.00

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 17.00

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS

---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(f y) : 13.28

(b/t)cal : 11.33

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(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 247.71 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1303210.75 N

ACTUAL AXIAL COMP. STRESS :1303210.75 / 5780.0 : 225.47 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2799

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30DXF IMPORT OF TOWER.DXF -- PAGE NO. 2800

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 63 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|------------------------------------------------------------------------- -|| Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 63 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * ================= ============== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.45 --->| RY = 7.9 |

|************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 5.7 BOLT DIA = 16 MM FA = 248.9 || L/R-Z = 11.6 BOLT CAP = 43.83 KN fa = 219.9 || KL/R = 11.6 # BOLT = 29 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 |

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| ELA = 1.0 || NSF = 1.0 || ||******************************************************************* *******||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|

| FX MY MZ LOCATION || ================== ==================================== || PASS COMPRESSION 0.884 13 || 1271.24 C 0.0 0.0 0.38 ||* *||**************************************************************************|| ||---------------------------------------------------------------- ----------|DXF IMPORT OF TOWER.DXF -- PAGE NO. 2801

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 11.55

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 11.55

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 248.91 MPA

CHECK AGAINST PERMISSIBLE STRESS

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--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1271241.62 N

ACTUAL AXIAL COMP. STRESS :1271241.62 / 5780.0 : 219.94 MPA

RESULT : PASS

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2802

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 29

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2803

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 64 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|----------------------------------- --------------------------------------- |

| Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 64 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.45 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLT ING STRESSES ||IN NEWT MM IN NEWT MM|

|--------------- ------------- -------------|| L/R-Y = 5.7 BOLT DIA = 16 MM FA = 248.9 || L/R-Z = 11.5 BOLT CAP = 43.83 KN fa = 226.1 || KL/R = 11.5 # BOLT = 30 FYB = 436.0 || FYLD = 250.0 FVB = 21 8.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||***************************** *********************************************||* *|

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|* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.908 13 || 1307.13 C 0.0 0.0 0.37 ||* *|

|**************************************************************************|| ||-------------------------- ------------------------------------------------ |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2804

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 11.48

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 11. 48

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 248.92 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1307135.25 N

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 ACTUAL AXIAL COMP. STRESS :1307135.25 / 5780.0 : 226.15 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2805

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30DXF IMPORT OF TOWER.DXF -- PAGE NO. 2806

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 65 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 65 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 |

|DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.45 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 5.7 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 11.6 BOLT CAP = 43.83 KN fa = 247.0 || KL/R = 11.6 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 |

| GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION |

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| ====================================================== || PASS TENSION 0.988 13 || 1170.24 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2807

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO

---------------------------

VALUE OF L/r : 11.55

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 11.55

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1170238.12 N

ACTUAL AXIAL TENSILE STRESS :1170238.12 / ( 5780.0*0.820 ) : 247.00 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

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NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2808

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 66 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|----------------------------------------------------- --------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 66 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.45 --->| RY = 7.9 |

|************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 5.7 BOLT DIA = 16 MM FA = 2 49.9 || L/R-Z = 11.6 BOLT CAP = 43.83 KN fa = 249.5 || KL/R = 11.6 # BOLT = 27 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 |

| NSF = 0.8 || ||*********************************************** ***************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.998 13 || 1182.15 T 0.0 0.0 0.00 ||* *||**************************************************************************|

| ||-------------------------------------------- ------------------------------ |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2809

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

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 ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 11.55

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 11.55

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS---------------------- ----------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1182151.75 N

ACTUAL AXIAL TENSILE STRESS :1182151.75 / ( 5780.0*0.820 ) : 249.51 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 27DXF IMPORT OF TOWER.DXF -- PAGE NO. 2810

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 67 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ |

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CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORC E : 1139593.50 N

ACTUAL AXIAL TENSILE STRESS :1139593.50 / ( 5780.0*0.820 ) : 240.53 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26STAAD.Pro MEMBER SELECTION - (I802)**************************

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 68 * | INDIAN SECTIONS | AX = 57.8 |

| * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.57 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 7.2 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 14.6 BOLT CAP = 43.83 KN fa = 240.8 || KL/R = 14.6 # BOLT = 27 FYB = 436.0 |

| FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|

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| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.963 13 || 1140.81 T 0.0 0.0 0.00 ||* *||***************** *********************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2813

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 14.62

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 14.62

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS

---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1140814.62 N

ACTUAL AXIAL TENSILE STRESS :1140814.62 / ( 5780.0*0.820 ) : 240.79 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

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 NO. OF BOLTS REQD. : 27

WARNING : THE MEMBER 69 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES |

|************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 69 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.45 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 5.7 BOLT DIA = 16 MM FA = 249.9 |

| L/R-Z = 11.6 BOLT CAP = 43.83 KN fa = 239.8 || KL/R = 11.6 # BOLT = 26 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *|

|* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.960 13 || 1136.23 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 11.55

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 EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 11.55

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1136230.88 N

ACTUAL AXIAL TENSILE STRESS :1136230.88 / ( 5780.0*0.820 ) : 239.8 2 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 70 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 70 * | INDI AN SECTIONS | AX = 57.8 |

| * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * ========================== ===== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.45 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 5.7 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 11.5 BOLT CAP = 43.83 KN fa = 239.9 |

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| KL/R = 11.5 # BOLT = 26 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************|

|* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || =========================== =========================== || PASS TENSION 0.960 13 || 1136.43 T 0.0 0.0 0.00 ||* *||**************************************************************************|| ||------------------------------------------------------------------------- -|DXF IMPORT OF TOWER.DXF -- PAGE NO. 2817

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 11.48

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 11.48

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS

---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1136433.38 N

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ACTUAL AXIAL TENSILE STRESS :1136433.38 / ( 5780.0*0.820 ) : 239.86 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26DXF IMPORT OF TOWER.DXF -- PAGE NO. 2818

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 71 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 71 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 |

| * |< ---LENGTH (ME= 0.70 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 8.9 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 18.0 BOLT CAP = 43.83 KN fa = 218.9 || KL/R = 18.0 # BOLT = 24 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 |

| ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.876 13 || 1037.15 T 0.0 0.0 0.70 |

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|* *||******************************* *******************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2819

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 17.98

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 17.98

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1037151.56 N

ACTUAL AXIAL TENSILE STRESS :1037151.56 / ( 5780.0*0.820 ) : 218.91 MPA

RESULT : PASS

BOLTING

-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 24DXF IMPORT OF TOWER.DXF -- PAGE NO. 2820

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STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 72 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 72 * | INDIAN SECTIONS | AX = 46.6 || * | ST ISA200X200X12 | --Z AY = 16.0 ||DESIGN CODE * | | AZ = 16.0 || IS-802 * =============================== SY = 208.2 || * SZ = 93.1 || * |< ---LENGTH (ME= 1.39 --->| RY = 7.9 ||************* RZ = 3.9 || || |

|PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 17.5 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 35.5 BOLT CAP = 43.83 KN fa = 227.0 || KL/R = 35.5 # BOLT = 20 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************|

|* *||* DESI GN SUMMARY ( KN-METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.908 13 || 867.64 T 0.0 0.0 1.39 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2821

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 12.0 MM

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RESULT : PASS

CHECK FOR SLENDERNESS RATIO------------------------ ---

VALUE OF L/r : 35.47

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 35.47

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSIO N

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 867636.25 N

ACTUAL AXIAL TENSILE STRESS : 867636.25 / ( 4661.0*0.820 ) : 2 27.02 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 20DXF IMPORT OF TOWER.DXF -- PAGE NO. 2822

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 73 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 73 * | INDIAN SECTIONS | AX = 34.0 || * | ST ISA200X150X10 | --Z AY = 13.3 ||DESIGN CODE * | | AZ = 10.0 |

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| IS-802 * =============================== SY = 126.3 || * SZ = 50.2 || * |< ---LENGTH (ME= 1.41 --->| RY = 7.2 ||************* RZ = 3.2 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|

| L/R-Y = 19.6 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 43.8 BOLT CAP = 43.83 KN fa = 231.9 || KL/R = 43.8 # BOLT = 14 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *|

|* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX M Y MZ LOCATION || ====================================================== || PASS TENSION 0.928 13 || 595.10 T 0.0 0.0 1.41 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2823

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 10.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 43.81

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 43.81

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

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CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 595100.25 N

ACTUAL AXIAL TENSILE STRESS : 595100.25 / ( 3400.0*0.755 ) : 231.87 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 14DXF IMPORT OF TOWER.DXF -- PAGE NO. 2824

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 74 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------- ------------------------ || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 74 * | INDIAN SECTIONS | AX = 25.0 || * | ST ISA125X95X12 | --Z AY = 10.0 ||DESIGN CODE * | | AZ = 7.6 || IS-802 * =============================== SY = 55.7 || * SZ = 24.4 || * |< ---LENGTH (ME= 0.70 --->| RY = 4.4 ||************* RZ = 2.0 || |

| ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 16.0 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 35.0 BOLT CAP = 43.83 KN fa = 247.9 || KL/R = 35.0 # BOLT = 11 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.7 |

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| ||******************************************** ******************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== |

| PASS TENSION 0.992 13 || 440.33 T 0.0 0.0 0.70 ||* *||**************************************************************************|| ||----------------------------------------- --------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2825

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 12.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 34.99

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 34.99

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS

------------------- -------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 440326.62 N

ACTUAL AXIAL TENSILE STRESS : 440326.62 / ( 2498.0*0.711 ) : 247.87 MPA

RESULT : PASS

BOLTING-------

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BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 11

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2826

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 75 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES |

|************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 75 * | INDIAN SECTIONS | AX = 57.8 || * | ST ISA200X200X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 20.0 || IS-802 * =============================== SY = 254.1 || * SZ = 112.6 || * |< ---LENGTH (ME= 0.70 --->| RY = 7.9 ||************* RZ = 3.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|

| L/R-Y = 8.9 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 18.0 BOLT CAP = 43. 83 KN fa = 216.2 || KL/R = 18.0 # BOLT = 24 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *|

|* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || =================================================== === || PASS TENSION 0.865 13 || 1024.18 T 0.0 0.0 0.70 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOW ER.DXF -- PAGE NO. 2827

DETAILS OF CALCULATION

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----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 17.98

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 17.98

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1024177.75 N

ACTUAL AXIAL TENSILE STRESS :1024177.75 / ( 5780.0*0.820 ) : 216.17 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 24DXF IMPORT OF TOWER.DXF -- PAGE NO. 2828

STAAD.Pro MEMBER SELECTION - (I802)**************************

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WARNING : THE MEMBER 76 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 76 * | INDIAN SECTIONS | AX = 42.8 |

| * | ST IS A150X150X15 | --Z AY = 15.0 ||DESIGN CODE * | | AZ = 15.0 || IS-802 * =============================== SY = 137.4 || * SZ = 60.0 || * |< ---LENGTH (ME= 1.39 --->| RY = 5.8 ||************* RZ = 2.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 23.8 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 47.6 BOLT CAP = 43.83 KN fa = 247.1 || KL/R = 47.6 # BOLT = 20 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 |

| GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== |

| PASS TENSION 0.988 13 || 845.88 T 0.0 0.0 1.39 ||* *||******************************************************* *******************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2829

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS R ATIO---------------------------

VALUE OF L/r : 47.62

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EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 47.62

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS

---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 845885.06 N

ACTUAL AXIAL TENSILE STRESS : 8 45885.06 / ( 4278.0*0.800 ) : 247.05 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 20

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2830

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 77 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGN ED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- |

| Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 77 * | INDIAN SECTIONS | AX = 29.8 || * | ST ISA130X130X12 | --Z AY = 10.4 ||DESIGN CODE * | | AZ = 10.4 || IS-802 * =============================== SY = 83.5 || * SZ = 36.9 || * |< ---LENGTH (ME= 1.41 --->| RY = 5.1 ||************* RZ = 2.5 || || ||PARAMETER BOLTING STRESSES |

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|IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 27.7 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 55.4 BOLT CAP = 43.83 KN fa = 248.8 || KL/R = 55.4 # BOLT = 14 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 |

| ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.995 13 || 584.70 T 0.0 0.0 1.41 ||* *||**************************************************************************|

| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2831

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 12.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 55.36

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 55.36

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL T ENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

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LOAD NO. : 13

DESIGN AXIAL FORCE : 584697.81 N

ACTUAL AXIAL TENSILE STRESS : 584697.81 / ( 2982.0*0.788 ) : 248.81 MPA

RESULT : PASS

BOLTING

-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 14DXF IMPORT OF TOWER.DXF -- PAGE NO. 2832

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 78 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |===================== ========| ------------ ||MEMBER 78 * | INDIAN SECTIONS | AX = 22.6 |

| * | ST ISA100X100X12 | --Z AY = 8.0 ||DESIGN CODE * | | AZ = 8.0 || IS-802 * =============================== SY = 47.4 || * SZ = 20.5 || * |< ---LENGTH (ME= 0.70 --->| RY = 3.9 ||************* RZ = 1.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 18.3 BOLT D IA = 16 MM FA = 249.9 || L/R-Z = 36.2 BOLT CAP = 43.83 KN fa = 247.3 || KL/R = 36.2 # BOLT = 10 FYB = 436.0 |

| FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|

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| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.989 13 || 424.91 T 0.0 0.0 0.70 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2833

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------- -----

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 12.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 36.25

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 36.25

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS

---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIB LE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 424912.72 N

ACTUAL AXIAL TENSILE STRESS : 424912.72 / ( 2259.0*0.761 ) : 247.30 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

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 NO. OF BOLTS REQD. : 10DXF IMPORT OF TOWER.DXF -- PAGE NO. 2834

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 79 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 79 * | INDIAN SECTIONS | AX = 50.2 || * | ST ISA200X150X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 15.0 || IS-802 * ================== ============= SY = 181.9 || * SZ = 76.0 |

| * |< ---LENGTH (ME= 0.70 --->| RY = 7.1 ||************* RZ = 3.2 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.9 BOLT DIA = 16 MM FA = 246.2 || L/R-Z = 22.0 BOLT CAP = 43.83 KN fa = 223.8 || KL/R = 22.0 # BOLT = 26 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 |

| ELA = 1.0 || NSF = 1.0 || ||******************************************************************** ******||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || =================== =================================== || PASS COMPRESSION 0.909 13 || 1124.82 C 0.0 0.0 0.00 ||* *|

|**************************************************************************|| ||----------------------------------------------------------------- ---------|DXF IMPORT OF TOWER.DXF -- PAGE NO. 2835

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

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MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 21.97

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 21.97

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 13.5 : 171.5 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.43

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 246.21 MPA

CHECK AGAINST PERMISSIBLE STRESS

----------------- ---------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1124819.62 N

ACTUAL AXIAL COMP. STRESS :1124819.62 / 5025.0 : 223.84 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2836

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26DXF IMPORT OF TOWER.DXF -- PAGE NO. 2837

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STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 80 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|------------------------------------ -------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 80 * | INDIAN SECTIONS | AX = 42.8 || * | ST ISA150X150X15 | --Z AY = 15.0 ||DESIGN CODE * | | AZ = 15.0 || IS-802 * =============================== SY = 137.4 || * SZ = 60.0 || * |< ---LENGTH (ME= 1.39 --->| RY = 5.8 ||************* RZ = 2.9 || || ||PARAMETER BOLTI NG STRESSES |

|IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 23.8 BOLT DIA = 16 MM FA = 232.4 || L/R-Z = 47.6 BOLT CAP = 43.83 KN fa = 220.1 || KL/R = 47.6 # BOLT = 22 FYB = 436.0 || FYLD = 250.0 FVB = 218 .0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||****************************** ********************************************||* *|

|* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.947 13 || 941.68 C 0.0 0.0 0.00 ||* *||**************************************************************************|| ||--------------------------- ----------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2838

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

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 CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 47.62

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 47.6 2

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 150.0 - 15.0 - 12.0 : 123.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 8.20

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 232.44 MPA

CHECK AGAINST P ERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 941675.56 N

ACTUAL AXIAL COMP. STRESS : 941675.56 / 4278.0 : 220.12 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2839

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 22DXF IMPORT OF TOWER.DXF -- PAGE NO. 2840

STAAD.Pro MEMBER SELECTION - (I802)**************************

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 WARNING : THE MEMBER 81 IS NOT A TRUSS MEMBER.

THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |= ============================| ------------ |

|MEMBER 81 * | INDIAN SECTIONS | AX = 29.0 || * | ST ISA150X150X10 | --Z AY = 10.0 ||DESIGN CODE * | | AZ = 10.0 || IS-802 * =============================== SY = 96.7 || * SZ = 42.8 || * |< ---LENGTH (ME= 1.41 --->| RY = 5.9 ||************* RZ = 2.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 23.7 BOLT DIA = 16 MM FA = 232.2 || L/R-Z = 48.0 BOLT CAP = 43.83 KN fa = 228.0 || KL/R = 48.0 # BOLT = 16 FYB = 436.0 |

| FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION |

| ====================================================== || PASS COMPRESSION 0.982 13 || 661.95 C 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2841

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 10.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 47.99

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 EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 47.99

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 150.0 - 10.0 - 12.0 : 128.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 12.80

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*f y : 232.16 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 661947.12 N

ACTUAL AXIAL COMP. STRESS : 661947.12 / 2903.0 : 228.02 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2842

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 16

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2843

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 82 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESI GNED CONSIDERING AXIAL FORCE ONLY

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|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 82 * | INDIAN SECTIONS | AX = 21.0 || * | ST ISA125X95X10 | --Z AY = 8.3 ||DESIGN CODE * | | AZ = 6.3 || IS-802 * =============================== SY = 47.5 || * SZ = 20.3 |

| * |< ---LENGTH (ME= 0.70 --->| RY = 4.4 ||************* RZ = 2.0 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 15.9 BOLT DIA = 16 MM FA = 240.6 || L/R-Z = 34.8 BOLT CAP = 43.83 KN fa = 226.9 || KL/R = 34.8 # BOLT = 11 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 |

| NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.943 13 || 476.98 C 0.0 0.0 0.00 ||* *||**************************************************************************|

| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2844

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 10.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 34.81

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 34.81

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ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 125.0 - 10.0 - 9.0 : 106.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 10.60

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1-0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 240.59 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 476983.72 N

ACTUAL AXIAL COMP. STRESS : 476983.72 / 2102.0 : 226.92 M PA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2845

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 11DXF IMPORT OF TOWER.DXF -- PAGE NO. 2846

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 83 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 83 * | INDIAN SECTIONS | AX = 50.2 |

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| * | ST ISA200X150X15 | --Z AY = 20.0 ||DESIGN CODE * | | AZ = 15.0 || IS-802 * =============================== SY = 181.9 || * SZ = 76.0 || * |< ---LENGTH (ME= 0.70 --->| RY = 7.1 ||************* RZ = 3.2 || || ||PARAMETER BOLTING STRESSES |

|IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.9 BOLT DIA = 16 MM FA = 246.2 || L/R-Z = 22.0 BOLT CAP = 43.83 KN fa = 219.7 || KL/R = 22.0 # BOLT = 26 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *|

|* -------------- *||* *||* RESULT/ CRITICAL COND / RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.893 13 || 1104.23 C 0.0 0.0 0.00 ||* *||*********************************************************************** ***|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2847

DETAILS OF CALCULATION

----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO

---------------------------

VALUE OF L/r : 21.97

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 21.97

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS

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---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 200.0 - 15.0 - 13.5 : 171.5 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.43

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 246.21 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1104229.88 N

ACTUAL AXIAL COMP. ST RESS :1104229.88 / 5025.0 : 219.75 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2848

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 26DXF IMPORT OF TOWER.DXF -- PAGE NO. 2849

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 84 IS NOT A TRUSS MEMBER.

THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 84 * | INDIAN SECTIONS | AX = 42.8 || * | ST ISA150X150X15 | --Z AY = 15.0 ||DESIGN CODE * | | AZ = 15.0 || IS-802 * =============================== SY = 137.4 || * SZ = 60.0 || * |< ---LENGTH (ME= 1.39 --->| RY = 5.8 |

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|************* RZ = 2.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 23.8 BOLT DIA = 16 MM FA = 232.4 || L/R-Z = 47.6 BOLT CAP = 43.83 KN fa = 216.6 || KL/R = 47.6 # BOLT = 22 FYB = 436.0 |

| FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* * ||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== |

| PASS COMPRESSION 0.932 13 || 926.43 C 0.0 0.0 0.00 ||* *||********************************* *****************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2850

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 47.62

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 47.62

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

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 b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 150.0 - 15.0 - 12.0 : 123.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 8.20

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 232.44 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 926433.75 N

ACTUAL AXIAL COMP. STRESS : 926433.75 / 4278.0 : 216.56 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2851

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 22DXF IMPORT OF TOWER.DXF -- PAGE NO. 2852

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 85 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES |

|************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 85 * | INDIAN SECTIONS | AX = 29.0 || * | ST ISA150X150X10 | --Z AY = 10.0 ||DESIGN CODE * | | AZ = 10.0 || IS-802 * =============================== SY = 96.7 || * SZ = 42.8 || * |< ---LENGTH (ME= 1.41 --->| RY = 5.9 ||************* RZ = 2.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM|

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|--------------- ------------- -------------|| L/R-Y = 23.7 BOLT DIA = 16 MM FA = 232.2 || L/R-Z = 48.0 BOLT CAP = 43.83 KN fa = 222.8 || KL/R = 48.0 # BOLT = 15 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 |

| NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || =============================================== ======= || PASS COMPRESSION 0.960 13 || 646.88 C 0.0 0.0 0.00 ||* * ||**************************************************************************|| |

|-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2853

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 10.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 47.99

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 47.99

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 150.0 - 10.0 - 12.0 : 128.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

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 (b/t)cal : 12.80

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 232.16 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 646877.75 N

ACTUAL AXIAL COMP. STRESS : 646877.75 / 2903.0 : 222.83 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2854

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 15DXF IMPORT OF TOWER.DXF -- PAGE NO. 2855

STAAD.Pro MEMBER SELECTION - (I802)

**************************

WARNING : THE MEMBER 86 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|---------------------------------------------------------------- ----------|| Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 86 * | INDIAN SECTIONS | AX = 20.2 || * | ST ISA130X130X8 | --Z AY = 6.9 ||DESIGN CODE * | | AZ = 6.9 |

| IS-802 * =============================== SY = 58.4 || * SZ = 26.3 || * |< ---LENGTH (ME= 0.70 --->| RY = 5.2 ||************* RZ = 2.5 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 13.6 BOLT DIA = 16 MM FA = 235.2 || L/R-Z = 27.6 BOLT CAP = 43.83 KN fa = 231.0 || KL/R = 27.6 # BOLT = 11 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 |

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| GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||********************************************************** ****************||* *||* DESIGN SUMMARY ( KN -METR) *|

|* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.982 13 || 467.07 C 0.0 0.0 0.00 ||* *||**************************************************************************|| ||------------------------------------------------------- ------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2856

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 8.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 27.58

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 27.58

ALLOWABLE KL/r : 120. 00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 130.0 - 8.0 - 10.0 : 112.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 14.00

(b/t)cal > (b/t)lim

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(b/t)lim (modified) : 378/sqrt(fy) : 23.91

(b/t)cal <= (b/t)lim (modified) AND KL/r <= Cc

Fcr : (1.677 - (0.677*(b/t)cal/(b/t)li m))*fy : 240.81 MPA

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*Fcr : 235.15 MPA

CHECK AGAINST PERMISSIBLE STRESS

--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 467069.75 N

ACTUAL AXIAL COMP. STRESS : 467069.75 / 2022.0 : 230.99 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2857

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 55.81 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 11DXF IMPORT OF TOWER.DXF -- PAGE NO. 2858

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 87 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 87 * | INDIAN SECTIONS | AX = 50.8 || * | ST ISA150X150X18 | --Z AY = 18.0 |

|DESIGN CODE * | | AZ = 18.0 || IS-802 * =============================== SY = 159.9 || * SZ = 69.0 || * |< ---LENGTH (ME= 0.45 --->| RY = 5.8 ||************* RZ = 2.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 7.8 BOLT DIA = 16 MM FA = 248.1 || L/R-Z = 15.5 BOLT CAP = 43.83 KN fa = 246.1 || KL/R = 15.5 # BOLT = 29 FYB = 436.0 |

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| FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *|

|* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.992 13 || 1250.11 C 0.0 0.0 0.45 ||* *||********************* *****************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2859

DETAILS OF CALCULATION

----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 18.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO

---------------------------

VALUE OF L/r : 15.52

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 15.52

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 150.0 - 18.0 - 12.0 : 120.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 6.67

(b/t)cal <= (b/t)lim AND KL/r <= Cc

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 ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 248.08 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1250114.88 N

ACTUAL AXIAL COMP. STRESS :1250114.88 / 5079.0 : 246.13 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2860

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 29DXF IMPORT OF TOWER.DXF -- PAGE NO. 2861

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 88 IS NOT A TRUSS MEMBER.

THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 88 * | INDIAN SECTI ONS | AX = 50.8 || * | ST ISA150X150X18 | --Z AY = 18.0 ||DESIGN CODE * | | AZ = 18.0 || IS-802 * =============================== SY = 159.9 || * SZ = 69.0 || * |< ---LENGTH (ME= 0.45 --->| RY = 5.8 ||************* RZ = 2.9 |

| || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 7.8 BOLT DIA = 16 MM FA = 248.1 || L/R-Z = 15.4 BOLT CAP = 43.83 KN fa = 246.2 || KL/R = 15.4 # BOLT = 29 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 |

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| NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION |

| =================================== =================== || PASS COMPRESSION 0.992 13 || 1250.66 C 0.0 0.0 0.45 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2862

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 18.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 15.42

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 15.42

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 150.0 - 18.0 - 12.0 : 120.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 6.67

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 248.11 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

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 LOAD NO. : 13

DESIGN AXIAL FORCE : 1250664.62 N

ACTUAL AXIAL COMP. STRESS :1250664.62 / 5079.0 : 246.24 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2863

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 29DXF IMPORT OF TOWER.DXF -- PAGE NO. 2864

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 89 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|---------------------------------------------------- ---------------------- || Y PROPERTIES |

|************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 89 * | INDIAN SECTIONS | AX = 50.8 || * | ST ISA150X150X18 | --Z AY = 18.0 ||DESIGN CODE * | | AZ = 18.0 || IS-802 * =============================== SY = 159.9 || * SZ = 69.0 || * |< ---LENGTH (ME= 0.57 --->| RY = 5.8 ||************* RZ = 2.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|

| L/R-Y = 9.8 BOLT DIA = 16 MM FA = 247.0 || L/R-Z = 19.5 BOLT CAP = 43.83 KN fa = 245.9 || KL/R = 19.5 # BOLT = 29 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||********************************************** ****************************||* *||* DESIGN SUMMARY ( KN -METR) *|

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|* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.996 13 || 1249.18 C 0.0 0.0 0.57 ||* *||**************************************************************************|

| ||------------------------------------------- ------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2865

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 18.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 19.54

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 19.54

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 150.0 - 18.0 - 12.0 : 120.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 6.67

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 246.99 MPA

CHECK AGAINST PERMISSIBLE STRES S--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1249175.88 N

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ACTUAL AXIAL COMP. STRESS :1249175.88 / 5079.0 : 245.95 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2866

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 29DXF IMPORT OF TOWER.DXF -- PAGE NO. 2867

STAAD.Pro MEMBER SELECTION - (I802)

**************************

WARNING : THE MEMBER 90 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |================= ============| ------------ ||MEMBER 90 * | INDIAN SECTIONS | AX = 50.8 || * | ST ISA150X150X18 | --Z AY = 18.0 ||DESIGN CODE * | | AZ = 18.0 |

| IS-802 * =============================== SY = 159.9 || * SZ = 69.0 || * |< ---LENGTH (ME= 0.57 --->| RY = 5. 8 ||************* RZ = 2.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 9.9 BO LT DIA = 16 MM FA = 247.0 || L/R-Z = 19.6 BOLT CAP = 43.83 KN fa = 246.5 || KL/R = 19.6 # BOLT = 29 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 |

| C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== |

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| PASS COMPRESSION 0.998 13 || 1251.91 C 0.0 0.0 0.57 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2868

DETAILS OF CALCULATION

----------------------

CHECK FOR MINIMUM THICKNESS------------------ ---------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 18.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 19.64

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 19.64

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 150.0 - 18.0 - 12.0 : 120.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 6.67

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 246.96 MP A

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1251914.75 N

ACTUAL AXIAL COMP. STRESS :1251914.75 / 5079.0 : 246.49 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2869

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|-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2871

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 15.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 11.55

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 11.55

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.1415 9265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS

: 200.0 - 15.0 - 15.0 : 170.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.33

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 248.91 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 1281645.88 N

ACTUAL AXIAL COMP. STRESS :1281645.88 / 5780.0 : 221.74 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2872

BOLTING-------

BOLT DIA : 16 MM

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BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 30DXF IMPORT OF TOWER.DXF -- PAGE NO. 2876

STAAD.Pro MEMBER SELECTION - (I802)

**************************

WARNING : THE MEMBER 93 I S NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 93 * | INDIAN SECTIONS | AX = 19.0 || * | ST ISA100X100X10 | --Z AY = 6.7 ||DESIGN CODE * | | AZ = 6.7 || IS-802 * =============================== SY = 40.8 |

| * SZ = 17.7 || * |< ---LENGTH (ME= 1.39 --->| RY = 3.9 ||************* RZ = 1.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM ||--------------- ------------- -------------|| L/R-Y = 35.7 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 71.7 BOLT CAP = 43.83 KN fa = 233.1 || KL/R = 71.7 # BOLT = 8 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 |

| LEG = 1.0 || ELA = 1.0 || NSF = 0.8 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.933 13 || 337.85 T 0.0 0.0 1.39 |

|* *||************************************************* *************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2877

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

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 MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 10.0 MM

RESULT : PASS

CHECK FOR SLENDER NESS RATIO---------------------------

VALUE OF L/r : 71.68

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 71.68

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------- -----

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 337849.59 N

ACTUAL AXIAL TENSILE STRE SS : 337849.59 / ( 1903.0*0.762 ) : 233.09 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 69.76 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 8DXF IMPORT OF TOWER.DXF -- PAGE NO. 2878

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 94 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES |

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|************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 94 * | INDIAN SECTIONS | AX = 10.1 || * | ST ISA100X75X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 3.0 || IS-802 * =============================== SY = 18.7 || * SZ = 7.4 || * |<---LENGTH (ME= 1.41 --->| RY = 3.6 ||************* RZ = 1.6 |

| || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 39.3 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 88.4 BOLT CAP = 41.86 KN fa = 244.6 || KL/R = 88.4 # BOLT = 5 FYB = 43 6.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.7 || |

|**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.979 14 || 169.31 T 0.0 0.0 1.41 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |

DXF IMPORT OF TOWER.DXF -- PAGE NO. 2879

DETAILS OF CALCULATION------------------- ---

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 88.44

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 88.44

ALLOWABLE KL/r : 400.00

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RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 3DXF IMPORT OF TOWER.DXF -- PAGE NO. 2882

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 96 IS NOT A TRUSS MEMBER.

THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------- ------|| Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 96 * | INDIAN SECTIONS | AX = 17.0 || * | ST ISA110X110X8 | --Z AY = 5.9 ||DESIGN CODE * | | AZ = 5.9 || IS-802 * ============ =================== SY = 41.2 || * SZ = 18.2 || * |< ---LENGTH (ME= 1.39 --->| RY = 4.3 ||************* RZ = 2.1 |

| || ||PARAMETER BOLTING STRE SSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 32.0 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 65.0 BOLT CAP = 43.83 KN fa = 243.6 || KL/R = 65.0 # BOLT = 8 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.8 |

| ||************************************************************** ************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ============= ========================================= || PASS TENSION 0.975 13 || 320.07 T 0.0 0.0 1.39 ||* *||**************************************************************************|

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| ||----------------------------------------------------------- ---------------|DXF IMPORT OF TOWER.DXF -- PAGE NO. 2883

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THIC KNESS : 6.0 MM

ACTUAL THICKNESS : 8.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 64.98

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 64.98

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 320074.06 N

ACTUAL AXIAL TENSILE STRESS : 320074.06 / ( 1702.0*0.772 ) : 243.58 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 55.81 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 8DXF IMPORT OF TOWER.DXF -- PAGE NO. 2884

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 STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 97 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 97 * | INDIAN SECTIONS | AX = 10.1 || * | ST ISA100X75X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 3.0 || IS-802 * =============================== SY = 18.7 || * SZ = 7.4 || * |< ---LENGTH (ME= 1.41 --->| RY = 3.6 ||************* RZ = 1.6 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM|

|--------------- ------------- -------------|| L/R-Y = 39.3 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 88.4 BOLT CAP = 41.86 KN fa = 242.4 || KL/R = 88.4 # BOLT = 4 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.7 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *|

|* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.970 14 || 167.84 T 0.0 0.0 1.41 ||* *||***************** *********************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2885

DETAILS OF CALCULATION

----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

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CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 88.44

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 88.44

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 14

DESIGN AXIAL FORCE : 167837.02 N

ACTUAL AXIAL TENSILE STRESS : 167837.02 / ( 1014.0*0.683 ) : 242.44 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 4DXF IMPORT OF TOWER.DXF -- PAGE NO. 2886

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 98 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 98 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 |

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| * |< ---LENGTH (ME= 0.70 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.3 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 50.6 BOLT CAP = 41.86 KN fa = 180.2 |

| KL/R = 50.6 # BOLT = 3 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.6 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION |

| ====================================================== || PASS TENSION 0.721 13 || 108.86 T 0.0 0.0 0.70 ||* *||************************************************************************* *|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2887

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 50.59

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 50.59

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

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ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 108855.73 N

ACTUAL AXIAL TENSILE STRESS : 108855.73 / ( 955. 0*0.633 ) : 180.20 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 3DXF IMPORT OF TOWER.DXF -- PAGE NO. 2888

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 99 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXI AL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 99 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0 .69 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES |

|IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.0 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 50.0 BOLT CAP = 41.86 KN fa = 167.3 || KL/R = 50.0 # BOLT = 3 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.6 || ||**************************************************************************|

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|* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.669 14 || 101.05 T 0.0 0.0 0.69 |

|* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2889

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 49.98

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 49.98

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 2 49.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 14

DESIGN AXIAL FORCE : 101050.73 N

ACTUAL AXIAL TENSILE STRESS : 101050.73 / ( 955.0*0.633 ) : 167.28 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

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SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 3DXF IMPORT OF TOWER.DXF -- PAGE NO. 2890

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 100 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|------------------------------------ -------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ |

|MEMBER 100 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0.70 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTI NG STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.1 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 50.1 BOLT CAP = 41.86 KN fa = 152.7 |

| KL/R = 50.1 # BOLT = 3 FYB = 436.0 || FYLD = 250.0 FVB = 218 .0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.6 || ||****************************** ********************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|

| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.611 15 || 92.25 T 0.0 0.0 0.70 ||* *||**************************************************************************|| ||--------------------------- ----------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2891

DETAILS OF CALCULATION----------------------

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CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 50.12

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 50 .12

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 15

DESIGN AXIAL FORCE : 92252.98 N

ACTUAL AXIAL TENSILE STRESS : 92252.98 / ( 955.0*0.633 ) : 152.72 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43 .83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 3DXF IMPORT OF TOWER.DXF -- PAGE NO. 2892

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 101 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

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| KL/R = 50.6 # BOLT = 3 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.6 || ||**************************************************************************|

|* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TEN SION 0.601 15 || 90.69 T 0.0 0.0 0.53 ||* *||******************************************** ******************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2895

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 50.58

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 50.58

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS

----------------------- ----------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 15

DESIGN AXIAL FORCE : 90687.68 N

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ACTUAL AXIAL TENSILE STRESS : 90687.68 / ( 955.0*0.633 ) : 150.13 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 3DXF IMPORT OF TOWER .DXF -- PAGE NO. 2896

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 103 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 103 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 |

| * |<---LENGTH (ME= 0.71 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.3 BOLT DIA = 16 MM FA = 217.8 || L/R-Z = 50.7 BOLT CAP = 41.86 KN fa = 111.4 || KL/R = 50.7 # BOLT = 3 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 |

| ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN-METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.512 14 || 106.43 C 0.0 0.0 0.00 |

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|* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2897

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 50.72

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 50.72

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 100.0 - 6.0 - 8.0 : 86.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 14.33

(b/t)cal > (b/t)lim

(b/t)lim (modified) : 378/sqr t(fy) : 23.91

(b/t)cal <= (b/t)lim (modified) AND KL/r <= Cc

Fcr : (1.677 - (0.677*(b/t)cal/(b/t)lim))*fy : 236.56 MPA

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*Fcr : 217.77 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 14

DESIGN AXIAL FORCE : 106425.91 N

ACTUAL AXIAL COMP. STRESS : 106425.91 / 955.0 : 111.44 MPA

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| 100.78 C 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2900

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS------------------- --------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 50.58

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 50.58

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 100.0 - 6.0 - 8.0 : 86.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 14.33

(b/t)cal > (b/t)lim

(b/t)lim (modified) : 378/sqrt(fy) : 23.91

(b/t)cal <= (b/t)lim (modified) AND KL/r <= Cc

Fcr : (1.677 - (0.677*(b/t)cal/(b/t)lim))*fy : 236.56 MPA

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*Fcr : 217.87 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 15

DESIGN AXIAL FORCE : 100776.55 N

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ACTUAL AXIAL COMP. STRESS : 100776.55 / 955.0 : 105.53 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2901

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 3DXF IMPORT OF TOWER.DXF -- PAGE NO. 2902

STAAD.Pro MEMBER SELECTION - (I802)

**************************

WARNING : THE MEMBER 105 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 105 * | I NDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 |

| IS-802 * ======================= ======== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0.69 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.0 BOLT DIA = 16 MM FA = 218.3 || L/R-Z = 50.0 BOLT CAP = 41.86 KN fa = 116.1 || KL/R = 50.0 # BOLT = 3 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 |

| C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||************************************************************************* *||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ======================== ============================== |

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| PASS COMPRESSION 0.532 14 || 110.90 C 0.0 0.0 0.00 ||* *||**************************************************************************|| ||---------------------------------------------------------------------- ----|DXF IMPORT OF TOWER.DXF -- PAGE NO. 2903

DETAILS OF CALCULATION

----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 49.98

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 49.98

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 100.0 - 6.0 - 8.0 : 86.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 14.33

(b/t)cal > (b/t)lim

(b/t)lim (modified) : 378/sqrt(fy) : 23.91

(b/t)cal <= (b/t)lim (modified) AND KL/r <= Cc

Fcr : (1.677 - (0.677*(b/t)cal/(b/t)lim))*fy : 236 .56 MPA

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*Fcr : 218.31 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 14

DESIGN AXIAL FORCE : 110903.72 N

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 ACTUAL AXIAL COMP. STRES S : 110903.72 / 955.0 : 116.13 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2904

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 3DXF IMPORT OF TOWER.DXF -- PAGE NO. 2905

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 106 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PRO PERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 106 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 |

|DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0.70 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.1 BOLT DIA = 16 MM FA = 218.2 || L/R-Z = 50.1 BOLT CAP = 41.86 KN fa = 108.4 || KL/R = 50.1 # BOLT = 3 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 |

| GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION |

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| ====================================================== || PASS COMPRESSION 0.497 15 || 103.50 C 0.0 0.0 0.00 ||* *||************************************ **************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2906

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO

---------------------------

VALUE OF L/r : 50.12

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 50.12

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS----------------- ----------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 100.0 - 6.0 - 8.0 : 86.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 14.33

(b/t)cal > (b/t)lim

(b/t)lim (modified) : 378/sqrt(fy) : 23.91

(b/t)cal <= (b/t)lim (modified) AND KL/r <= Cc

Fcr : (1.677 - (0.677*(b/t)cal/(b/t)lim))*fy : 236.56 MPA

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*Fcr : 218.21 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 15

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DESIGN AXIAL FORCE : 103498.76 N

ACTUAL AXIAL COMP. STRESS : 103498.76 / 955.0 : 108.38 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2907

BOLTING

-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 3DXF IMPORT OF TOWER .DXF -- PAGE NO. 2908

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 107 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 107 * | INDIAN SECTIONS | AX = 17.0 |

| * | ST ISA110X110X8 | --Z AY = 5.9 ||DESIGN CODE * | | AZ = 5.9 || IS-802 * =============================== SY = 41.2 || * SZ = 18.2 || * |<---LENGTH (ME= 1.39 --->| RY = 4.3 ||************* RZ = 2.1 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 32.0 BOLT DIA = 16 MM FA = 217.3 || L/R-Z = 65.0 BOLT CAP = 43.83 KN fa = 216.0 || KL/R = 65.0 # BOLT = 9 FYB = 436.0 |

| FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN-METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|

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| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.994 14 || 367.56 C 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2909

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 8.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 64.98

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 64.98

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS

---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 110.0 - 8.0 - 10.0 : 92.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.50

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 217.35 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 14

DESIGN AXIAL FORCE : 367556.31 N

ACTUAL AXIAL COMP. STRESS : 367556.31 / 1702.0 : 215.96 MPA

RESULT : PASS

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DXF IMPORT OF TOWER.DXF -- PAGE NO. 2910

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 55.81 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 9DXF IMPORT OF TOWER.DXF -- PAGE NO. 2911

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 108 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 108 * | INDIAN SECTIONS | AX = 11.7 || * | ST ISA100X10 0X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 4.0 || IS-802 * =============================== SY = 26.1 || * SZ = 11.6 || * |< ---LENGTH (ME= 1.41 --->| RY = 4.0 |

|************* RZ = 1.9 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 35.4 BOLT DIA = 16 MM FA = 199.5 || L/R-Z = 72.1 BOLT CAP = 41.86 KN fa = 185.5 || KL/R = 72.1 # BOLT = 6 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 |

| NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRIT ICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.93 0 13 || 216.46 C 0.0 0.0 0.00 ||* *|

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RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2913

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 6DXF IMPORT OF TOWER.DXF -- PAGE NO. 2914

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 109 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 109 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 |

| * |< ---LENGTH (ME= 0.70 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.3 BOLT DIA = 16 MM FA = 217.9 || L/R-Z = 50.6 BOLT CAP = 41.86 KN fa = 119.1 || KL/R = 50.6 # BOLT = 3 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 |

| ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.547 14 || 113.77 C 0 .0 0.0 0.00 |

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|* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2915

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 50.59

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 50.59

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159 265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 100.0 - 6.0 - 8.0 : 86.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 14.33

(b/t)cal > (b/t)lim

(b/t)lim (modified) : 378/sqrt(fy) : 23.91

(b/t)cal <= (b/t)lim (modified) AND KL/r <= Cc

Fcr : (1.677 - (0.677*(b/t)cal/(b/t)lim))*fy : 236.56 MPA

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*Fcr : 217.87 MPA

CHECK AGAINST PERMISSIBLE STRESS---------------------- ----------

LOAD NO. : 14

DESIGN AXIAL FORCE : 113771.62 N

ACTUAL AXIAL COMP. STRESS : 113771.62 / 955.0 : 119.13 MPA

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 RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2916

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 3DXF IMPORT OF TOWER.DXF -- PAGE NO. 2917

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 110 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|----------------------------------------- --------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 110 * | INDIAN SECTIONS | AX = 17.0 || * | ST ISA110X110X8 | --Z AY = 5.9 ||DESIGN CODE * | | AZ = 5.9 || IS-802 * =============================== SY = 41.2 |

| * SZ = 18.2 || * |< ---LENGTH (ME= 1.39 --->| RY = 4.3 ||************* RZ = 2.1 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 32.0 BOLT DIA = 16 MM FA = 217.3 || L/R-Z = 65.0 BOLT CAP = 43.83 KN fa = 211.8 || KL/R = 65.0 # BOLT = 9 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 |

| LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||*********************************** ***************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.975 14 |

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| 360.55 C 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------- ------------------------------------------ |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2918

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 8.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 64.98

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 64.98

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 110.0 - 8.0 - 10.0 : 92.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 11.50

(b/t)cal <= (b/t)lim AND KL/r <= Cc

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*fy : 217.35 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 14

DESIGN AXIAL FORCE : 360554.88 N

ACTUAL AXIAL COMP. STRESS : 360554.88 / 1702.0 : 211.84 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2919

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BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 55.81 KN

BOLT CAP : 43.83 KN

NO. OF BOLTS REQD. : 9DXF IMPORT OF TOWER.DXF -- PAGE NO. 2920

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 111 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |====== =======================| ------------ ||MEMBER 111 * | INDIAN SECTIONS | AX = 11.7 || * | ST ISA100X100X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 4.0 || IS-802 * =============================== SY = 26.1 || * SZ = 11.6 || * |< ---LENGTH (ME= 1.41 --->| RY = 4.0 ||************* RZ = 1.9 || || |

|PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 35.4 BOLT DIA = 16 MM FA = 199.5 || L/R-Z = 72.1 BOLT CAP = 41.86 KN fa = 178.9 || KL/R = 72.1 # BOLT = 5 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************|

|* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.897 13 || 208.80 C 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |

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DXF IMPORT OF TOWER.DXF -- PAGE NO. 2921

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 72.11

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 72.11

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 100.0 - 6.0 - 8.5 : 85.5 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 14.25

(b/t)cal > (b/t)lim

(b/t)lim (modified) : 378/sqrt(fy) : 23.91

(b/t)cal <= (b/t)lim (modifie d) AND KL/r <= Cc

Fcr : (1.677 - (0.677*(b/t)cal/(b/t)lim))*fy : 237.62 MPA

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*Fcr : 199.46 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 208798.72 N

ACTUAL AXIAL COMP. STRESS : 208798.72 / 1167.0 : 178.92 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2922

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 BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 5DXF IMPORT OF TOWER.DXF -- PAGE NO. 2923

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 112 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|------------------------------------------------------------------- -------|| Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 112 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =========== ==================== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0.70 --->| RY = 3.5 ||************* RZ = 1.4 || |

| ||PARAMETER BOLTING STR ESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.3 BOLT DIA = 16 MM FA = 217.9 || L/R-Z = 50.6 BOLT CAP = 41.86 KN fa = 116.3 || KL/R = 50.6 # BOLT = 3 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || |

|************************************************************* *************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ============ ========================================== || PASS COMPRESSION 0.534 13 || 111.10 C 0.0 0.0 0.00 ||* *||**************************************************************************|| |

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|---------------------------------------------------------- ---------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2924

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THI CKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 50.59

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 50.59

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS

: 100.0 - 6.0 - 8.0 : 86.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 14.33

(b/t)cal > (b/t)lim

(b/t)lim (modified) : 378/sqrt(fy) : 23.91

(b/t)cal <= (b/t)lim (modified) AND KL/r <= Cc

Fcr : (1.677 - (0.677*(b/t)cal/(b/t)lim)) *fy : 236.56 MPA

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*Fcr : 217.87 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 111097.36 N

ACTUAL AXIAL COMP. STRESS : 111097.36 / 955.0 : 116.33 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2925

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BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 3DXF IMPORT OF TOWER.DXF -- PAGE NO. 2926

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 113 IS NOT A TRUSS MEMBER.

THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 113 * | INDIAN SECTIONS | AX = 9. 6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0.70 --->| RY = 3.5 ||************* RZ = 1.4 |

| || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.1 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 50.1 BOLT CAP = 41.86 KN fa = 144.2 || KL/R = 50.1 # BOLT = 3 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.6 |

| ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.577 15 || 87.08 T 0.0 0.0 0.64 ||* *||************************ **************************************************|

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| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2927

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 50.12

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 50.12

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 15

DESIGN AXIAL FORCE : 87080.50 N

ACTUAL AXIAL TENSILE STRESS : 87080.50 / ( 955.0*0.633 ) : 144.15 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 3DXF IMPORT OF TOWER.DXF -- PAGE NO. 2928

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 STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 114 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 114 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0.70 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM|

|--------------- ------------- -------------|| L/R-Y = 20.1 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 50.1 BOLT CAP = 41.86 KN fa = 139.3 || KL/R = 50.1 # BOLT = 3 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.6 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *|

|* -------------- *||* *||* RESULT/ CRITICAL COND/ RAT IO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.557 15 || 84.16 T 0.0 0.0 0.70 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2929

DETAILS OF CALCULATI ON

----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

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CHECK FOR SLENDERNESS RATIO----------------- ----------

VALUE OF L/r : 50.12

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 50.12

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 15

DESIGN AXIAL FORCE : 84160.62 N

ACTUAL AXIAL TENSILE STRESS : 84160.62 / ( 955.0*0.633 ) : 139.32 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 3DXF IMPORT OF TOWER.DXF -- PAGE NO. 2930

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 115 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORC E ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 115 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 |

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| * |< ---LENGTH (ME= 0.72 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.7 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 51.7 BOLT CAP = 41.86 KN fa = 134.7 |

| KL/R = 51.7 # BOLT = 2 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.6 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION |

| ====================================================== || PASS TENSION 0.539 15 || 81.39 T 0.0 0.0 0.60 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2931

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THIC KNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 51.68

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 51.68

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

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ALLOWABLE AXIAL TENSILE STRESS : 249.94 M PA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 15

DESIGN AXIAL FORCE : 81393.38 N

ACTUAL AXIAL TENSILE STRESS : 81393.38 / ( 955.0*0.633 ) : 134.74 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 2DXF IMPORT OF TOWER.DXF -- PAGE NO. 2932

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 116 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|------------------------------------------- ------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 116 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0.72 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES |

|IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.7 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 51.7 BOLT CAP = 41.86 KN fa = 135.5 || KL/R = 51.7 # BOLT = 2 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.6 || ||************************************* *************************************|

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|* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.542 13 || 81.87 T 0.0 0.0 0.60 |

|* *||**************************************************************************|| ||---------------------------------- ---------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2933

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 51.68

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 51.68

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 81869.79 N

ACTUAL AXIAL TENSILE STRESS : 81869.79 / ( 955.0*0.633 ) : 135.53 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

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SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 2DXF IMPORT OF TOWER.DXF -- PAGE NO. 2934

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 117 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ |

|MEMBER 117 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0.70 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.1 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 50.1 BOLT CAP = 41.86 KN fa = 116.8 |

| KL/R = 50.1 # BOLT = 2 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.6 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|

| FX MY MZ LOCATION || ============================================ ========== || PASS TENSION 0.467 15 || 70.58 T 0.0 0.0 0.70 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2935

DETAILS OF CALCULATION----------------------

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|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 118 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 |

| IS-802 * =============================== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0.70 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT M M||--------------- ------------- -------------|| L/R-Y = 20.1 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 50.1 BOLT CAP = 41.86 KN fa = 118.5 || KL/R = 50.1 # BOLT = 2 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 |

| LEG = 1.0 || ELA = 1.0 || NSF = 0.6 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.474 13 || 71.60 T 0.0 0.0 0.70 |

|* *||************************************************ **************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2937

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 50.12

EQN. USED TO FIND KL/r : K*L/r

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ACTUAL VALUE OF KL/r : 50.12

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS--------------------------- ------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 71602.60 N

ACTUAL AXIAL TENSILE STR ESS : 71602.60 / ( 955.0*0.633 ) : 118.53 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 2DXF IMPORT OF TOWER.DXF -- PAGE NO. 2938

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 119 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT |

| * |=============================| ------------ ||MEMBER 119 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 || * |<---LENGTH (ME= 0.69 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|

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DESIGN AXIAL FORCE : 51393.27 N

ACTUAL AXIAL TENSILE STRESS : 51393.27 / ( 955.0*0.633 ) : 85.08 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 2DXF IMPORT OF TOWER.DXF -- PAGE NO. 2940

STAAD.Pro MEMBER SELECTION - (I802)

**************************

WARNING : THE MEMBER 120 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |============== ===============| ------------ ||MEMBER 120 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 |

| IS-802 * =============================== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0.70 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.1 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 50.1 BOLT CAP = 41.86 KN fa = 90.0 || KL/R = 50.1 # BOLT = 2 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 |

| C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.6 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== |

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| PASS TENSION 0.360 13 || 54.35 T 0.0 0.0 0.70 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2941

DETAILS OF CALCULATION

----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 50.12

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 50.12

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 54349.59 N

ACTUAL AXIAL TENSILE STRESS : 54349.59 / ( 955.0*0.633 ) : 89.97 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 2

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DXF IMPORT OF TOWER.DXF -- PAGE NO. 2942

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 121 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|------------------------------------------------------------------- -------|| Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 121 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =========== ==================== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0.97 --->| RY = 3.5 ||************* RZ = 1.4 |

| || ||PARAMETER BOLTING STR ESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 28.0 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 69.7 BOLT CAP = 41.86 KN fa = 27.8 || KL/R = 69.7 # BOLT = 1 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.6 |

| ||************************************************************* *************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ============ ========================================== || PASS TENSION 0.111 15 || 16.76 T 0.0 0.0 0.97 ||* *||**************************************************************************|| |

|---------------------------------------------------------- ---------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2943

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THI CKNESS : 6.0 MM

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ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 69.74

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 69.74

ALLOWABLE KL/r : 400.0 0

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 15

DESIGN AXIAL FORCE : 16763.79 N

ACTUAL AXIAL TENSILE STRESS : 16763.79 / ( 955.0*0.633 ) : 27.75 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 1DXF IMPORT OF TOWER.DXF -- PAGE NO. 2944

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 122 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 122 * | INDIAN SECTIONS | AX = 9.6 |

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| * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0.97 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES |

|IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 27.9 BOLT DIA = 16 MM FA = 249.9 || L/R-Z = 69.6 BOLT CAP = 41.86 KN fa = 30.0 || KL/R = 69.6 # BOLT = 1 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 0.6 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *|

|* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS TENSION 0.120 13 || 18.15 T 0.0 0.0 0.97 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2945

DETAILS OF CALCULATION

----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO

---------------------------

VALUE OF L/r : 69.60

EQN. USED TO FIND KL/r : K*L/r

ACTUAL VALUE OF KL/r : 69.60

ALLOWABLE KL/r : 400.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRES S

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---------------------------------

CRITICAL CONDITION : TENSION

ALLOWABLE AXIAL TENSILE STRESS : 249.94 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 18149.56 N

ACTUAL AXIAL TENSILE STRESS : 18149.56 / ( 955.0*0.633 ) : 30.04 MPA

RESULT : PASS

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 1DXF IMPORT OF TOWER.DXF -- PAGE NO. 2946

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 123 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 123 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 || * |< ---LENGTH (ME= 0.97 --->| RY = 3.5 |

|************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 28.0 BOLT DIA = 16 MM FA = 201.0 || L/R-Z = 69.7 BOLT CAP = 41.86 KN fa = 21.0 || KL/R = 69.7 # BOLT = 1 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 || LEG = 1.0 |

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| ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|

| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.104 15 || 20.02 C 0.0 0.0 0.00 ||* *||************************************************************************ **|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2947

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 69.74

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 69.74

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 100.0 - 6.0 - 8.0 : 86.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 14.33

(b/t)cal > (b/t)lim

(b/t)lim (modified) : 378/sqrt(fy) : 23.91

(b/t)cal <= (b/t)lim (modified) AND KL/r <= Cc

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 Fcr : (1.677 - (0.677*(b/t)cal/(b/t)lim))*fy : 236.56 MPA

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*Fcr : 201.03 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 15

DESIGN AXIAL FORCE : 20021.46 N

ACTUAL AXIAL COMP. STRESS : 20021.46 / 955.0 : 20.96 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2948

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 1DXF IMPORT OF TOWER.DXF -- PAGE NO. 2949

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 124 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORC E ONLY

|-------------------------------------------------------------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 124 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 || * SZ = 5.6 |

| * |< ---LENGTH (ME= 0.97 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 27.9 BOLT DIA = 16 MM FA = 201.2 || L/R-Z = 69.6 BOLT CAP = 41.86 KN fa = 23.2 || KL/R = 69.6 # BOLT = 1 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 || C = 1.0 |

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| LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||**************************************************************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *||* *|

|* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.115 13 || 22.18 C 0.0 0.0 0.00 ||* *||**************************************************************************|| ||-------------------------------------------------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2950

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THIC KNESS

---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 69.60

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 69.60

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 1 27.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 100.0 - 6.0 - 8.0 : 86.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 14.33

(b/t)cal > (b/t)lim

(b/t)lim (modified) : 378/sqrt(fy) : 23.91

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(b/t)cal <= (b/t)lim (modified) AND KL/r <= Cc

Fcr : (1.677 - (0.677*(b/t)cal/(b/t)lim))*fy : 236.56 MPA

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*Fcr : 201.17 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 13

DESIGN AXIAL FORCE : 22181.51 N

ACTUAL AXIAL COMP. STRESS : 22181.51 / 955.0 : 23.23 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2951

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 1DXF IMPORT OF TOWER.DXF -- PAGE NO. 2952

STAAD.Pro MEMBER SELECTION - (I802)**************************

WARNING : THE MEMBER 125 IS NOT A TRUSS MEMBER.THIS MEMBER HAS BEEN DESIGNED CONSIDERING AXIAL FORCE ONLY

|--------------------------------------------------- ----------------------- || Y PROPERTIES ||************* | IN CM UNIT || * |=============================| ------------ ||MEMBER 125 * | INDIAN SECTIONS | AX = 9.6 || * | ST ISA100X65X6 | --Z AY = 4.0 ||DESIGN CODE * | | AZ = 2.6 || IS-802 * =============================== SY = 16.9 |

| * SZ = 5.6 || * |< ---LENGTH (ME= 0.69 --->| RY = 3.5 ||************* RZ = 1.4 || || ||PARAMETER BOLTING STRESSES ||IN NEWT MM IN NEWT MM||--------------- ------------- -------------|| L/R-Y = 20.0 BOLT DIA = 16 MM FA = 218.3 || L/R-Z = 50.0 BOLT CAP = 41.86 KN fa = 61.4 || KL/R = 50.0 # BOLT = 2 FYB = 436.0 || FYLD = 250.0 FVB = 218.0 || GALVA = 0.0 |

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| C = 1.0 || LEG = 1.0 || ELA = 1.0 || NSF = 1.0 || ||********************************************* *****************************||* *||* DESIGN SUMMARY ( KN -METR) *||* -------------- *|

|* *||* RESULT/ CRITICAL COND/ RATIO/ LOADING/ *|| FX MY MZ LOCATION || ====================================================== || PASS COMPRESSION 0.281 15 || 58.65 C 0.0 0.0 0.00 ||* *||**************************************************************************|| ||------------------------------------------ -------------------------------- |DXF IMPORT OF TOWER.DXF -- PAGE NO. 2953

DETAILS OF CALCULATION----------------------

CHECK FOR MINIMUM THICKNESS---------------------------

TYPE : PAINTED

MIN. ALLOWABLE THICKNESS : 6.0 MM

ACTUAL THICKNESS : 6.0 MM

RESULT : PASS

CHECK FOR SLENDERNESS RATIO---------------------------

VALUE OF L/r : 49.98

EQN. USED TO FIND KL/r : L/r

ACTUAL VALUE OF KL/r : 49.98

ALLOWABLE KL/r : 120.00

RESULT : PASS

CALCULATION OF ALLOWABLE STRESS---------------------------------

CRITICAL CONDITION : COMPRESSION

Cc : sqrt(2*3.14159265*3.14159265*E : 127.24

b : LENGTH OF LEG - WEB THICKNESS - ROOT RADIUS: 100.0 - 6.0 - 8.0 : 86.0 MM

(b/t)lim : 210/sqrt(fy) : 13.28

(b/t)cal : 14.33

(b/t)cal > (b/t)lim

(b/t)lim (modified) : 378/sqrt(fy) : 23.91

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 (b/t)cal <= (b/t)lim (modified) AND KL/r <= Cc

Fcr : (1.677 - (0.677*(b/t)cal/(b/t)lim))*fy : 236.56 MPA

ALLOWABLE AXIAL COMP. STRESS : (1 -0.5*(KL/r/Cc)*(KL/r/Cc))*Fcr : 218.31 MPA

CHECK AGAINST PERMISSIBLE STRESS--------------------------------

LOAD NO. : 15

DESIGN AXIAL FORCE : 58650.68 N

ACTUAL AXIAL COMP. STRESS : 58650.68 / 955.0 : 61.41 MPA

RESULT : PASSDXF IMPORT OF TOWER.DXF -- PAGE NO. 2954

BOLTING-------

BOLT DIA : 16 MM

SHEARING CAP : 43.83 KN

BEARING CAP : 41.86 KN

BOLT CAP : 41.86 KN

NO. OF BOLTS REQD. : 2DXF IMPORT OF TOWER.DXF -- PAGE NO. 2955

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STEEL TAKE-OFF--------------

PROFILE L ENGTH(METE) WEIGHT(KN )

ST ISA200X200X15 43.39 19.266ST ISA200X200X18 2.81 1.485ST ISA200X150X15 7.50 2.894ST ISA200X200X12 1.39 0.498ST ISA200X150X10 1.41 0.367ST ISA125X95X12 0.70 0.135ST ISA150X150X15 4.17 1.371ST ISA130X130X12 1.41 0.322ST ISA100X100X12 0.70 0.122

ST ISA150X150X10 2.81 0.627ST ISA125X95X10 0.70 0.114ST ISA130X130X8 0.70 0.109ST ISA150X150X18 2.04 0.796ST ISA100X100X10 1.39 0.203ST ISA100X75X6 2.81 0.219ST ISA100X65X6 23.52 1.725ST ISA110X110X8 4.17 0.545ST ISA100X100X6 2.81 0.252

----------------TOTAL = 31.052

MEMBER PROFILE LENGTH WEIGHT(METE) (KN )

1 ST ISA200X200X15 0.76 0.3372 ST ISA200X200X15 0.76 0.3373 ST ISA200X200X15 0.76 0.3374 ST ISA200X 200X15 0.76 0.3375 ST ISA200X200X15 0.76 0.3376 ST ISA200X200X15 0.76 0.3377 ST ISA200X200X15 0.79 0.3498 ST ISA200X200X18 0.79 0.4159 ST ISA200X200X15 1.00 0.446

10 ST ISA200X200X18 1.00 0.53111 ST ISA200X200X15 1.02 0.45312 ST ISA200X200X18 1.02 0.539

13 ST ISA200X200X15 0.62 0.27414 ST ISA200X200X15 0.62 0.27515 ST ISA200X200X15 0.62 0.27416 ST ISA200X200X15 0.62 0.27517 ST ISA200X2 00X15 1.02 0.45318 ST ISA200X200X15 1.02 0.45319 ST ISA200X200X15 1.00 0.44620 ST ISA200X200X15 1.00 0.44621 ST ISA200X200X15 0.77 0.34322 ST ISA200X200X15 0.77 0.34323 ST ISA200X200X15 0.77 0.34224 ST ISA200X200X15 0.77 0.34225 ST ISA200X200X15 0.76 0.337

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26 ST ISA200X200X15 0.76 0.33727 ST ISA200X200X15 0.76 0.337DXF IMPORT OF TOWER.DXF -- PAGE NO. 5127

28 ST ISA200X200X15 0.76 0.33729 ST ISA200X200X15 0.45 0.20130 ST ISA200X200X15 0.45 0.19931 ST ISA200X200X15 0.66 0.29532 ST ISA200X200X15 0.66 0.295

33 ST ISA200X20 0X15 0.68 0.30234 ST ISA200X200X15 0.68 0.30235 ST ISA200X200X15 0.65 0.28736 ST ISA200X200X15 0.65 0.28837 ST ISA200X200X15 1.10 0.48938 ST ISA200X200X15 1.10 0.48739 ST ISA200X200X15 0.71 0.31540 ST ISA200X200X15 0.71 0.31541 ST ISA200X200X15 0.69 0.30842 ST ISA200X200X15 0.69 0.30843 ST ISA200X200X15 0.54 0.24144 ST ISA200X200X15 0.54 0.24145 ST ISA200X200X15 0.57 0.25346 ST ISA200X200 X15 0.57 0.25347 ST ISA200X200X15 0.57 0.253

48 ST ISA200X200X15 0.57 0.25349 ST ISA200X150X15 0.54 0.20950 ST ISA200X150X15 0.54 0.20951 ST ISA200X150X15 0.69 0.26852 ST ISA200X150X15 0.69 0.26853 ST ISA200X150X15 0.71 0.27454 ST ISA200X150X15 0.71 0.27455 ST ISA200X150X15 1.10 0.42556 ST ISA200X150X15 1.10 0.42457 ST ISA200X200X15 0.65 0.28758 ST ISA200X200X15 0.65 0.28859 ST ISA200X200X 15 0.68 0.30260 ST ISA200X200X15 0.68 0.30261 ST ISA200X200X15 0.66 0.295

62 ST ISA200X200X15 0.66 0.29563 ST ISA200X200X15 0.45 0.20164 ST ISA200X200X15 0.45 0.19965 ST ISA200X200X15 0.45 0.20166 ST ISA200X200X15 0.45 0.20167 ST ISA200X200X15 0.57 0.25368 ST ISA200X200X15 0.57 0.25469 ST ISA200X200X15 0.45 0.20170 ST ISA200X200X15 0.45 0.19971 ST ISA200X200X15 0.70 0.31272 ST ISA200X200X1 2 1.39 0.49873 ST ISA200X150X10 1.41 0.36774 ST ISA125X95X12 0.70 0.13575 ST ISA200X200X15 0.70 0.312

76 ST ISA150X150X15 1.39 0.45777 ST ISA130X130X12 1.41 0.32278 ST ISA100X100X12 0.70 0.12279 ST ISA200X150X15 0.70 0.27180 ST ISA150X150X15 1.39 0.45781 ST ISA150X150X10 1.41 0.31482 ST ISA125X95X10 0.70 0.11483 ST ISA200X150X15 0.70 0.271DXF IMPORT OF TOWER.DXF -- PAGE NO. 5128

84 ST ISA150X150X15 1.39 0.45785 ST ISA150X150X10 1.41 0.31486 ST ISA130X130X8 0.70 0.109

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87 ST ISA150X150X18 0.45 0.17688 ST ISA150X150X18 0.45 0.17589 ST ISA150X150X18 0.57 0.22290 ST ISA150X150X18 0.57 0.22391 ST ISA200X200X15 0.45 0.20192 ST ISA200X200X15 0.45 0.20193 ST ISA100X100X10 1.39 0.20394 ST ISA100X75X6 1.41 0.11095 ST ISA100X65X6 0.70 0.052

96 ST ISA110X110X8 1.39 0.18297 ST ISA100X75X6 1.41 0.11098 ST ISA100X65X6 0.70 0.05299 ST ISA100X65X6 0.69 0.051100 ST ISA100X65X6 0.70 0.051101 ST ISA100X65X6 0.71 0.052102 ST ISA100X65X6 0.70 0.052103 ST ISA100X65X6 0.71 0.052104 ST ISA100X65X6 0.70 0.052105 ST ISA100X65X6 0.69 0.051106 ST ISA100X65X6 0.70 0.051107 ST ISA110X110X8 1.39 0.182108 ST ISA100X100X6 1.41 0.126109 ST ISA100X65X6 0.70 0.052110 ST ISA110X110X8 1.39 0.182

111 ST ISA100X100X6 1.41 0.126112 ST ISA100X65X6 0.70 0.052113 ST ISA100X65X6 0.70 0.051114 ST ISA100X65X6 0.70 0.051115 ST ISA100X65X6 0.72 0.053116 ST ISA100X65X6 0.72 0.053117 ST ISA100X65X6 0.70 0.051118 ST ISA100X65X6 0.70 0.051119 ST ISA100X65X6 0.69 0.051120 ST ISA100X65X6 0.70 0.051121 ST ISA100X65X6 0.97 0.071122 ST ISA100X65X6 0.97 0.071123 ST ISA100X65X6 0.97 0.071124 ST ISA100X65X6 0.97 0.071

125 ST ISA100X65X6 0.69 0.051126 ST ISA100X65X6 0.70 0.051127 ST ISA100X65X6 0.70 0.051128 ST ISA100X65X6 0.70 0.051129 ST ISA100X65X6 0.72 0.053130 ST ISA100X65X6 0.72 0.053131 ST ISA100X65X6 0.70 0.051132 ST ISA100X65X6 0.70 0.051

----------------TOTAL = 31.052

************ END OF DATA FROM INTERNAL STORAGE ************

DXF IMPORT OF TOWER.DXF -- PAGE NO. 5129

700. STEEL MEMBER TAKE OFF LIST 269 TO 577DXF IMPORT OF TOWER.DXF -- PAGE NO. 5130

STEEL TAKE-OFF--------------

PROFILE LENGTH(METE) WEIGHT(KN )

ST ISA100X65X6 325.08 23.849

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ST ISA100X100X6 12.42 1.114ST ISA100X75X6 1.83 0.142ST ISA100X100X8 8.77 1.036ST ISA125X75X6 10.59 0.949

----------------TOTAL = 27.090

MEMBER PROFILE LENGTH WEIGHT(METE) (KN )

269 ST ISA100X65X6 1.11 0.082270 ST ISA100X65X6 1.11 0.082271 ST ISA100X65X6 1.10 0.081272 ST ISA100X65X6 1.10 0.081273 ST ISA100X65X6 1.11 0.082274 ST ISA100X65X6 1.11 0.082275 ST ISA100X65X6 1.10 0.081276 ST ISA100X65X 6 1.10 0.081277 ST ISA100X65X6 1.13 0.083278 ST ISA100X65X6 1.13 0.083279 ST ISA100X65X6 1.68 0.123280 ST ISA100X65X6 1.69 0.124

281 ST ISA100X65X6 1.70 0.125282 ST ISA100X65X6 1.69 0.124283 ST ISA100X65X6 1.10 0.081284 ST ISA100X65X6 1.10 0.081285 ST ISA100X65X6 1.69 0.124286 ST ISA100X65X6 1.69 0.124287 ST ISA100X65X6 1.10 0.081288 ST ISA100X65X6 1.10 0.081289 ST ISA100X65X6 1.65 0.121290 ST ISA100X65X6 1.65 0.121291 ST ISA100X65X6 1.11 0.082292 ST ISA100X65X6 1.11 0.082293 ST ISA100X65X6 1.16 0.085294 ST ISA100X65X6 1.16 0.085

295 ST ISA100X65X6 1.70 0.125296 ST ISA100X65X6 1.70 0.125297 ST ISA100X65X6 1.10 0.081298 ST ISA100X65X6 1.10 0.081299 ST ISA100X65X6 1.69 0.124300 ST ISA100X65X6 1.69 0.124301 ST ISA100X65X6 1.10 0.081302 ST ISA100X65X6 1.10 0.081303 ST ISA100X65X6 1.70 0.125304 ST ISA100X65X6 1.69 0.124305 ST ISA100X65X6 1.68 0.123306 ST ISA100X65X6 1.69 0.124307 ST ISA100X65X6 1.12 0.082308 ST ISA100X65X6 1.12 0.082

DXF IMPORT OF TOWER.DXF -- PAGE NO. 5131

309 ST ISA100X65X6 1.10 0.081310 ST ISA100X65X6 1.10 0.081311 ST ISA100X65X6 1.12 0.082312 ST ISA100X65X6 1.12 0.082313 ST ISA100X65X6 1.10 0.081314 ST ISA100X65X6 1.10 0.081315 ST ISA100X65X6 1.11 0.082316 ST ISA100X65X6 1.11 0.082317 ST ISA100X65X6 0.44 0.032318 ST ISA100X65X6 0.44 0.032319 ST ISA100X65X6 0.58 0.043

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320 ST ISA100X65X6 0.58 0.043321 ST ISA100X65X6 0.40 0.030322 ST ISA100X65X6 0.77 0.056323 ST ISA100X65X6 0.77 0.056324 ST ISA100X65X6 0.40 0.030325 ST ISA100X65X6 1.12 0.082326 ST ISA100X65X6 1.12 0.082327 ST ISA100X65X6 1.13 0.083328 ST ISA100X65X6 1.13 0.083

329 ST ISA100X65X6 1.10 0.080330 ST ISA100X65X6 1.08 0.079331 ST ISA100X65X6 0.61 0.045332 ST ISA100X65X6 0.61 0.045333 ST ISA100X65X6 0.93 0.068334 ST ISA100X65X6 0.93 0.068335 ST ISA100X65X6 0.62 0.046336 ST ISA100X65X6 0.61 0.045337 ST ISA100X65X6 0.98 0.072338 ST ISA100X65X6 0.98 0.072339 ST ISA100X65X6 0.90 0.066340 ST ISA100X65X6 0.90 0.066341 ST ISA100X65X6 0.97 0.071342 ST ISA100X65X6 0.97 0.071343 ST ISA100X65X6 1.08 0.079

344 ST ISA100X65X6 1.08 0.079345 ST ISA100X65X6 0.75 0.055346 ST ISA100X65X6 0.75 0.055347 ST ISA100X65X6 0.77 0.056348 ST ISA100X65X6 0.77 0.056349 ST ISA100X65X6 0.73 0.053350 ST ISA100X65X6 0.73 0.053351 ST ISA100X65X6 0.61 0.045352 ST ISA100X65X6 0.61 0.045353 ST ISA100X65X6 1.09 0.080354 ST ISA100X65X6 1.10 0.081355 ST ISA100X65X6 1.10 0.081356 ST ISA100X65X6 1.09 0.080357 ST ISA100X65X6 0.98 0.072

358 ST ISA100X65X6 0.97 0.071359 ST ISA100X65X6 0.97 0.071360 ST ISA100X65X6 0.98 0.072361 ST ISA100X65X6 1.03 0.075362 ST ISA100X65X6 1.01 0.074363 ST ISA100X65X6 1.01 0.074364 ST ISA100X65X6 1.03 0.075DXF IMPORT OF TOWER.DXF -- PAGE NO. 5132

365 ST ISA100X65X6 1.14 0.084366 ST ISA100X65X6 1.15 0.084367 ST ISA100X65X6 1.15 0.084368 ST ISA100X65X6 1.14 0.084369 ST ISA100X65X6 0.61 0.045

370 ST ISA100X65X6 0.61 0.045371 ST ISA100X65X6 0.73 0.053372 ST ISA100X65X6 0.73 0.053373 ST ISA100X65X6 0.77 0.056374 ST ISA100X65X6 0.77 0.056375 ST ISA100X65X6 0.75 0.055376 ST ISA100X65X6 0.75 0.055377 ST ISA100X65X6 1.08 0 .079378 ST ISA100X65X6 1.08 0.079379 ST ISA100X65X6 0.97 0.071380 ST ISA100X65X6 0.97 0.071381 ST ISA100X65X6 0.90 0.066382 ST ISA100X65X6 0.90 0.066

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383 ST ISA100X65X6 0.98 0.072384 ST ISA100X65X6 0.98 0.072385 ST ISA100X65X6 0.62 0.046386 ST ISA100X65X6 0.61 0.045387 ST ISA100X65X6 0.93 0.068388 ST ISA100X65X6 0.93 0.068389 ST ISA100X65X6 0.56 0.041390 ST ISA100X65X6 0.56 0. 041391 ST ISA100X65X6 1.10 0.080

392 ST ISA100X65X6 1.08 0.079393 ST ISA100X65X6 1.13 0.083394 ST ISA100X65X6 1.13 0.083395 ST ISA100X65X6 1.12 0.082396 ST ISA100X65X6 1.12 0.082397 ST ISA100X65X6 0.45 0.033398 ST ISA100X65X6 0.45 0.033399 ST ISA100X65X6 0.77 0.056400 ST ISA100X65X6 0.77 0.056401 ST ISA100X65X6 0.58 0.043402 ST ISA100X65X6 0.58 0.043403 ST ISA100X65X6 0.44 0.0 32404 ST ISA100X65X6 0.44 0.032405 ST ISA100X65X6 0.77 0.057406 ST ISA100X65X6 0.77 0.057

407 ST ISA100X65X6 0.56 0.041408 ST ISA100X65X6 0.56 0.041409 ST ISA100X65X6 0.57 0.042410 ST ISA100X65X6 0.57 0.042411 ST ISA100X65X6 0.56 0.041412 ST ISA100X65X6 0.56 0.041413 ST ISA100X65X6 0.73 0.054414 ST ISA100X65X6 0.74 0.055415 ST ISA100X65X6 0.44 0.033416 ST ISA100X65X6 0.43 0.03 2417 ST ISA100X65X6 0.44 0.032418 ST ISA100X65X6 0.44 0.032419 ST ISA100X65X6 0.76 0.056420 ST ISA100X65X6 0.51 0.038

DXF IMPORT OF TOWER.DXF -- PAGE NO. 5133

421 ST ISA100X65X6 0.51 0.038422 ST ISA100X65X6 0.76 0.056423 ST ISA100X65X6 0.55 0.040424 ST ISA100X65X6 0.55 0.040425 ST ISA100X65X6 0.72 0.053426 ST ISA100X65X6 0.72 0.053427 ST ISA100X65X6 0.50 0.037428 ST ISA100X65X6 0.50 0.037429 ST ISA100X65X6 0.55 0.040430 ST ISA100X65X6 0.55 0.041431 ST ISA100X65X6 0.55 0.041432 ST ISA100X65X6 0.55 0.040

433 ST ISA100X65X6 0.43 0.031434 ST ISA100X65X6 0.43 0.031435 ST ISA100X65X6 0.43 0.031436 ST ISA100X65X6 0.43 0.031437 ST ISA100X65X6 0.48 0.035438 ST ISA100X65X6 0.48 0.036439 ST ISA100X65X6 0.48 0.035440 ST ISA100X65X6 0.48 0.036441 ST ISA100X65X6 0.61 0.044442 ST ISA100X65X6 0.61 0.045443 ST ISA100X65X6 0.61 0.045444 ST ISA100X65X6 0.60 0.044445 ST ISA100X65X6 0.50 0.037

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446 ST ISA100X65X6 0.50 0.037447 ST ISA100X65X6 0.72 0.053448 ST ISA100X65X6 0.72 0.053449 ST ISA100X65X6 0.55 0.040450 ST ISA100X65X6 0.55 0.040451 ST ISA100X65X6 0.76 0.056452 ST ISA100X65X6 0.51 0.038453 ST ISA100X65X6 0.76 0.056454 ST ISA100X65X6 0.44 0.032

455 ST ISA100X65X6 0.44 0.032456 ST ISA100X65X6 0.44 0.033457 ST ISA100X65X6 0.43 0.032458 ST ISA100X65X6 0.73 0.054459 ST ISA100X65X6 0.74 0.055460 ST ISA100X65X6 0.56 0.041461 ST ISA100X65X6 0.56 0.041462 ST ISA100X65X6 0.57 0.042463 ST ISA100X65X6 0.57 0.042464 ST ISA100X65X6 0.56 0.041465 ST ISA100X65X6 0.56 0.041466 ST ISA100X65X6 0.77 0.057467 ST ISA100X65X6 0 .77 0.057468 ST ISA100X65X6 1.83 0.134469 ST ISA100X65X6 1.83 0.134

470 ST ISA100X65X6 2.19 0.160471 ST ISA100X65X6 2.19 0.160472 ST ISA100X65X6 2.20 0.161473 ST ISA100X65X6 2.20 0.161474 ST ISA100X65X6 1.83 0.134475 ST ISA100X65X6 1.83 0.134476 ST ISA10 0X65X6 2.19 0.160DXF IMPORT OF TOWER.DXF -- PAGE NO. 5134

477 ST ISA100X65X6 2.19 0.160478 ST ISA100X65X6 2.20 0.161479 ST ISA10 0X65X6 2.20 0.161480 ST ISA100X65X6 1.83 0.134481 ST ISA100X65X6 1.83 0.134

482 ST ISA100X65X6 1.75 0.128483 ST ISA100X65X6 1. 77 0.130484 ST ISA100X65X6 1.77 0.130485 ST ISA100X100X6 1.83 0.164486 ST ISA100X75X6 1.83 0.142487 ST ISA100X100X8 2.19 0.259488 ST ISA100X100X6 2.19 0.196489 ST ISA100X100X8 2.20 0.260490 ST ISA100X100X6 2.20 0.197491 ST ISA100X65X6 1.83 0.134492 ST ISA100 X65X6 1.83 0.134493 ST ISA125X75X6 2.19 0.196494 ST ISA100X65X6 2.19 0.160495 ST ISA125X75X6 2.20 0.197

496 ST ISA100X65X6 2.2 0 0.161497 ST ISA100X65X6 1.83 0.134498 ST ISA100X65X6 1.83 0.134499 ST ISA100X100X6 1.83 0.164500 ST ISA125X75X6 1.83 0.164501 ST ISA100X100X8 2.19 0.259502 ST ISA100X100X6 2.19 0.196503 ST ISA100X100X8 2.20 0.260504 ST ISA100X100X6 2.20 0.197505 ST ISA100X 65X6 1.83 0.134506 ST ISA100X65X6 1.83 0.134507 ST ISA125X75X6 2.19 0.196508 ST ISA100X65X6 2.19 0.160

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509 ST ISA125X75X6 2.20 0.197510 ST ISA100X65X6 2.20 0.161511 ST ISA100X65X6 1.83 0.134512 ST ISA100X65X6 1.83 0.134513 ST ISA100X65X6 1.77 0.130514 ST ISA100X65X6 1.77 0.130515 ST ISA100X65X6 1.74 0.127516 ST ISA100X65X6 1.83 0.134517 ST ISA100X65X6 1.83 0.134

518 ST ISA100X6 5X6 2.19 0.160519 ST ISA100X65X6 2.19 0.160520 ST ISA100X65X6 2.20 0.161521 ST ISA100X65X6 2.20 0.161522 ST ISA100X65X6 1.83 0.134523 ST ISA100X65X6 1.83 0.134524 ST ISA100X65X6 2.19 0.160525 ST ISA100X65X6 2.19 0.160526 ST ISA100X65X6 2.20 0.161527 ST ISA100X65X6 2.20 0.161528 ST ISA100X65X6 1.83 0.134529 ST ISA100X65X6 1.83 0.134530 ST ISA100X65X6 1.60 0.117531 ST ISA100X65 X6 1.58 0.116532 ST ISA100X65X6 1.43 0.105

DXF IMPORT OF TOWER.DXF -- PAGE NO. 5135

533 ST ISA100X65X6 1.43 0.105534 ST ISA100X65 X6 1.29 0.095535 ST ISA100X65X6 1.29 0.095536 ST ISA100X65X6 1.14 0.084537 ST ISA100X65X6 1.14 0.084538 ST ISA100X65X6 1.00 0.073539 ST ISA100X65X6 1.01 0.074540 ST ISA100X65X6 1.10 0.081541 ST ISA100X65X6 1.09 0.080542 ST ISA100X65X6 1.60 0.117543 ST ISA100X65X6 1.28 0.094544 ST ISA100X65X6 1.11 0.082

545 ST ISA100X65X6 1.11 0.082546 ST ISA100X65X6 1.28 0.094547 ST ISA100X65X 6 1.60 0.117548 ST ISA100X65X6 1.43 0.105549 ST ISA100X65X6 1.12 0.082550 ST ISA100X65X6 1.02 0.075551 ST ISA100X65X6 1.02 0.075552 ST ISA100X65X6 1.12 0.082553 ST ISA100X65X6 1.43 0.105554 ST ISA100X65X6 1.43 0.105555 ST ISA100X65X6 1.12 0.082556 ST ISA100X65X6 1.02 0.075557 ST ISA100X65X6 1.02 0.075558 ST ISA100X65X6 1.12 0.082

559 ST ISA100X65X6 1.43 0.105560 ST ISA100X65X6 1.60 0.117561 ST ISA100X65X6 1.28 0.094562 ST ISA100X65X6 1.11 0.082563 ST ISA100X65X6 1.11 0.082564 ST ISA100X65X6 1.28 0.094565 ST ISA100X65X6 1.60 0.117566 ST ISA100X65X6 1.10 0.081567 ST ISA100X65X6 1.09 0.080568 ST ISA100X65X6 1.00 0.073569 ST ISA100X65X6 1.01 0.074570 ST ISA100X65X6 1.14 0.084571 ST ISA100X65X6 1.14 0.084

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572 ST ISA100X65X6 1.29 0.095573 ST ISA100X65X6 1.29 0.095574 ST ISA100X65X6 1.43 0.105575 ST ISA100X65X6 1.43 0.105576 ST ISA100X65X6 1.60 0.117577 ST ISA100X65X6 1.58 0.116

----------------TOTAL = 27.090

************ END OF DATA FROM INTERNAL STORAGE ************

701. STEEL MEMBER TAKE OFF LIST 1001 TO 1072 1501 TO 1 612 2001 TO 2031DXF IMPORT OF TOWER.DXF -- PAGE NO. 5136

STEEL TAKE-OFF--------------

PROFILE LENGTH(METE) WEIGHT(KN )

ST ISA100X65X6 222.36 16.313----------------

TOTAL = 16.313

MEMBER PROFILE LENGTH WEIGHT(METE) (KN )

1001 ST ISA100X65X6 0.69 0.0501002 ST ISA100X65X6 0.69 0.0501003 ST ISA100X65X6 0.92 0.0681004 ST ISA100X65X6 0.92 0.0681005 ST ISA100X65X6 1.36 0.1001006 ST ISA100X65X6 1.36 0.1001007 ST ISA100X65X6 1.43 0.105

1008 ST ISA100X65X6 1.43 0.1051009 ST ISA100X65X6 2.05 0 .1501010 ST ISA100X65X6 2.05 0.1501011 ST ISA100X65X6 0.69 0.0501012 ST ISA100X65X6 2.06 0.1511013 ST ISA100X65X6 0.77 0.0571014 ST ISA100X65X6 0.77 0.0571015 ST ISA100X65X6 2.06 0.1511016 ST ISA100X65X6 0.69 0.0501017 ST ISA100X65X6 0.94 0.0691018 ST ISA100X65X6 0.94 0.0691019 ST ISA100X65X6 1.17 0.0861020 ST ISA100X65X6 1.19 0.0871021 ST ISA100X65X6 1.40 0.103

1022 ST ISA100X65X6 1.42 0. 1041023 ST ISA100X65X6 1.38 0.1011024 ST ISA100X65X6 1.38 0.1011025 ST ISA100X65X6 1.46 0.1071026 ST ISA100X65X6 1.46 0.1071027 ST ISA100X65X6 1.19 0.0871028 ST ISA100X65X6 1.19 0.0871029 ST ISA100X65X6 2.06 0.1511030 ST ISA100X65X6 2.06 0.1511031 ST ISA100X65X6 1.42 0.1041032 ST ISA100X65X6 1.42 0.1041033 ST ISA100X65X6 2.02 0.1491034 ST ISA100X65X6 2.02 0.149

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1035 ST ISA100X65X6 0.76 0.0 561036 ST ISA100X65X6 0.76 0.0561037 ST ISA100X65X6 0.76 0.0561038 ST ISA100X65X6 0.76 0.0561039 ST ISA100X65X6 2.02 0.1491040 ST ISA100X65X6 2.02 0.1491041 ST ISA100X65X6 2.00 0.1471042 ST ISA100X65X6 1.42 0.1041043 ST ISA100X65X6 1.42 0.104

1044 ST ISA100X65X6 2.00 0.147DXF IMPORT OF TOWER.DXF -- PAGE NO. 5137

1045 ST ISA100X65X6 1.19 0.0871046 ST ISA100X65X6 1.19 0.0871047 ST ISA100X65X6 1.40 0.1031048 ST ISA100X65X6 1.40 0.1031049 ST ISA100X65X6 1.37 0.1011050 ST ISA100X65X6 1.37 0.1011051 ST ISA100X65X6 1.40 0.10 31052 ST ISA100X65X6 1.42 0.1041053 ST ISA100X65X6 1.17 0.0861054 ST ISA100X65X6 1.19 0.0871055 ST ISA100X65X6 0.94 0.0691056 ST I SA100X65X6 0.94 0.069

1057 ST ISA100X65X6 2.05 0.1511058 ST ISA100X65X6 0.76 0.0561059 ST ISA100X65X6 0.76 0.0561060 ST ISA100X65X6 2.05 0.1511061 ST ISA100X65X6 0.69 0.0501062 ST ISA100X65X6 0.69 0.0501063 ST ISA100X65X6 2.05 0.1501064 ST ISA100X65X6 2.05 0.1501065 ST ISA100X65X6 1.44 0.1051066 ST ISA100X65X6 1.44 0.1051067 ST ISA100X65X6 1.36 0.1001068 ST ISA100X65X6 1.36 0.1001069 ST ISA100X65X6 0.92 0.0681070 ST ISA100X65X6 0.92 0.068

1071 ST ISA100X65X6 0.69 0.0501072 ST ISA100X65X6 0.69 0.0501501 ST ISA100X65X6 0.43 0.0321502 ST ISA100X65X6 0.42 0.0311503 ST ISA100X65X6 0.72 0.0531504 ST ISA100X65X6 0.70 0.0521505 ST ISA100X65X6 0.77 0.0561506 ST ISA100X65X6 0.77 0.0561507 ST ISA100X65X6 1.25 0.0921508 ST ISA100X65X6 1.25 0.0921509 ST ISA100X65X6 0.40 0.0291510 ST ISA 100X65X6 0.40 0.0291511 ST ISA100X65X6 1.30 0.0951512 ST ISA100X65X6 1.30 0.095

1513 ST ISA100X65X6 1.32 0.0971514 ST ISA100X65X6 1.32 0.0971515 ST ISA100X65X6 1.31 0.0961516 ST ISA100X65X6 1.31 0.0961517 ST ISA100X65X6 1.00 0.0731518 ST ISA100X65X6 1.00 0.0731519 ST ISA100X65X6 0.69 0.0501520 ST ISA100X65X6 0.69 0.0501521 ST ISA100X65X6 0.77 0.0561522 ST ISA100X65X6 0.77 0.0561523 ST ISA1 00X65X6 0.61 0.0451524 ST ISA100X65X6 0.62 0.0461525 ST ISA100X65X6 0.89 0.065

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1526 ST ISA100X65X6 0.89 0.0651527 ST ISA100X65X6 1 .25 0.0921528 ST ISA100X65X6 1.04 0.076DXF IMPORT OF TOWER.DXF -- PAGE NO. 5138

1529 ST ISA100X65X6 1.04 0.0761530 ST ISA100X65X6 1 .25 0.0921531 ST ISA100X65X6 1.30 0.0951532 ST ISA100X65X6 1.31 0.096

1533 ST ISA100X65X6 1.38 0.1011534 ST ISA100X65X6 1.38 0.1011535 ST ISA100X65X6 1.31 0.0961536 ST ISA100X65X6 1.30 0.0951537 ST ISA100X65X6 1.00 0.0731538 ST ISA100X65X6 1.03 0.0751539 ST ISA10 0X65X6 1.03 0.0751540 ST ISA100X65X6 1.00 0.0731541 ST ISA100X65X6 0.61 0.0451542 ST ISA100X65X6 0.61 0.0451543 ST ISA100X65X6 0. 64 0.0471544 ST ISA100X65X6 0.64 0.0471545 ST ISA100X65X6 0.87 0.0641546 ST ISA100X65X6 0.87 0.0641547 ST ISA100X65X6 1.03 0.075

1548 ST ISA100X65X6 1.01 0.0741549 ST ISA100X65X6 1.01 0.0741550 ST ISA100X65X6 1.03 0.0751551 ST ISA100X65X6 0.62 0.0461552 ST ISA100 X65X6 0.62 0.0461553 ST ISA100X65X6 1.32 0.0971554 ST ISA100X65X6 1.32 0.0971555 ST ISA100X65X6 1.38 0.1011556 ST ISA100X65X6 1.3 8 0.1011557 ST ISA100X65X6 1.38 0.1011558 ST ISA100X65X6 1.38 0.1011559 ST ISA100X65X6 1.32 0.0971560 ST ISA100X65X6 1.32 0.0971561 ST ISA100X65X6 0.62 0.046

1562 ST ISA100X65X6 0.62 0.0461563 ST ISA100X65X6 1.03 0.0751564 ST ISA100X65X6 1.01 0.0741565 ST ISA100X 65X6 1.01 0.0741566 ST ISA100X65X6 1.03 0.0751567 ST ISA100X65X6 0.88 0.0641568 ST ISA100X65X6 0.88 0.0641569 ST ISA100X65X6 0.64 0.0471570 ST ISA100X65X6 0.64 0.0471571 ST ISA100X65X6 0.61 0.0451572 ST ISA100X65X6 0.61 0.0451573 ST ISA100X65X6 1.00 0.0731574 ST ISA100X65X6 1.03 0.0751575 ST ISA100X65X6 1.03 0.075

1576 ST ISA100X65X6 1.00 0.0731577 ST ISA100X65X6 1.30 0.0951578 ST ISA100X6 5X6 1.31 0.0961579 ST ISA100X65X6 1.38 0.1011580 ST ISA100X65X6 1.38 0.1011581 ST ISA100X65X6 1.31 0.0961582 ST ISA100X65X6 1.30 0.0951583 ST ISA100X65X6 1.25 0.0921584 ST ISA100X65X6 1.04 0.076DXF IMPORT OF TOWER.DXF -- PAGE NO. 5139

1585 ST ISA100X65X6 1.04 0.0761586 ST ISA100X65X6 1.25 0.092

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1587 ST ISA100X65X6 0.89 0.0651588 ST ISA100X65X6 0.89 0.0651589 ST ISA100X65X6 0.61 0.0451590 ST ISA100X65X6 0.62 0.0461591 ST ISA100X65X6 0.77 0.0561592 ST ISA100X65X6 0.77 0.0561593 ST ISA100X65X6 0.69 0.0501594 ST ISA100X65 X6 0.69 0.0501595 ST ISA100X65X6 1.00 0.073

1596 ST ISA100X65X6 1.00 0.0731597 ST ISA100X65X6 1.31 0.0961598 ST ISA100X65X6 1.31 0.0961599 ST ISA100X65X6 1.32 0.0971600 ST ISA100X65X6 1.32 0.0971601 ST ISA100X65X6 0.43 0.0321602 ST ISA100X65X6 1.30 0.0951603 ST ISA100X65X6 1.30 0.0951604 ST ISA100X65X6 0.43 0.0321605 ST ISA100X65X6 1.25 0.0921606 ST ISA100X65X6 1.25 0.0921607 ST ISA100X65X 6 0.77 0.0561608 ST ISA100X65X6 0.77 0.0561609 ST ISA100X65X6 0.72 0.0531610 ST ISA100X65X6 0.70 0.052

1611 ST ISA100X65X6 0.43 0.0321612 ST ISA100X65X6 0.42 0.0312001 ST ISA100X65X6 0.66 0.0482002 ST ISA100X65X6 0.66 0.0482003 ST ISA100X65X6 0.65 0.0472004 ST ISA100X65X6 0.65 0.0472005 ST ISA100X65X6 0.59 0.0432006 ST ISA100X65X6 0.59 0.0432007 ST ISA100X65X6 0.58 0.0432008 ST ISA100X65X6 0.57 0.0422009 ST ISA100X65X6 0.61 0.0452010 ST ISA100X65X6 0.61 0.0442011 ST ISA100X65X6 0.61 0.0442012 ST ISA100X65X6 0.61 0.045

2013 ST ISA100X65X6 0.54 0.0402014 ST ISA100X65X6 0.54 0.0402015 ST ISA100X65X6 0.54 0.0402016 ST ISA100X65X6 0.54 0.0402017 ST ISA100X65X6 0.54 0.0402018 ST ISA100X65X6 0.54 0.0402019 ST ISA100X65X6 0.54 0.0402020 ST ISA100X65X6 0.54 0.0402021 ST ISA100X65X6 0.61 0.0452022 ST ISA100X65X6 0.61 0.0442023 ST ISA100X65X6 0.61 0.0442024 ST ISA100X65X6 0.61 0.0452025 ST ISA100X65X6 0.57 0.0422026 ST ISA100X65X6 0.59 0.043

2027 ST ISA100X65X6 0.59 0.0432028 ST ISA100X65X6 0.65 0.047DXF IMPORT OF TOWER.DXF -- PAGE NO. 5140

2029 ST ISA100X65X6 0.65 0.0472030 ST ISA100X65X6 0.66 0.0482031 ST ISA100X65X6 0.66 0.048

----------------TOTAL = 16.313

************ END OF DATA FROM INTERNAL STORAGE ************

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 702. STEEL MEMBER TAKE OFF LIST 197 TO 204 10476 10520 10521 10537 155 TO 166 -DXF IMPORT OF TOWER.DXF -- PAGE NO. 5141

STEEL TAKE-OFF--------------

PROFILE LENGTH(METE) WEIGHT(KN )

703. 173 TO 196 207 TO 230 235 TO 246 3018 3019 3030 3031 3038 3039 3050 3051 4018 -704. 4019 4030 4031 4038 4039 4050 405 1 5018 5019 5030 5031 5038 5039 5050 5051ST ISA100X65X6 108.72 7.976

----------------TOTAL = 7.976

MEMBER PROFILE LENGTH WEIGHT(METE) (KN )

155 ST ISA100X65X6 0.80 0.058156 ST ISA100X65X6 0.80 0.058157 ST ISA100X65X6 0.80 0.058

158 ST ISA100X65X6 0.80 0.058159 ST ISA100X65X6 0.80 0.058160 ST ISA100X65X6 0.80 0.058161 ST ISA100X65X6 0.89 0.065162 ST ISA100X65X6 0.89 0.065163 ST ISA100X65X6 0.89 0.065164 ST ISA100X65X6 0.89 0.065165 ST ISA100X65X6 0.89 0.065166 ST ISA100X65X6 0.89 0.065173 ST ISA100X65X6 0.84 0.062174 ST ISA100X65X6 0.84 0.062175 ST ISA100X65X6 0.84 0.062176 ST ISA100X65X6 0.84 0.062177 ST ISA100X65X6 0.84 0.062

178 ST ISA100X65X6 0.84 0.062179 ST ISA100X65X6 1.16 0.085180 ST ISA100X65X6 1.16 0.085181 ST ISA100X65X6 1.16 0.085182 ST ISA100X65X6 1.16 0.085183 ST ISA100X65X6 1.16 0.085184 ST ISA100X65X6 1.16 0.085185 ST ISA100X65X6 1.23 0.090186 ST ISA100X65X6 1.23 0.090187 ST ISA100X65X6 1.23 0.090188 ST ISA100X65X6 1.23 0.090189 ST ISA100X65X6 1.23 0.090190 ST ISA100X65X6 1.23 0.090191 ST ISA100X65X6 0.84 0.062

192 ST ISA100X65X6 0.84 0.062193 ST ISA100X65X6 0.84 0.062194 ST ISA100X65X6 0.84 0.062195 ST ISA100X65X6 0.84 0.062196 ST ISA100X65X6 0.84 0.062197 ST ISA100X65X6 0.20 0.015198 ST ISA100X65X6 0.20 0.015199 ST ISA100X65X6 0.22 0.016200 ST ISA100X65X6 0.22 0.016201 ST ISA100X65X6 0.22 0.016202 ST ISA100X65X6 0.22 0 .016DXF IMPORT OF TOWER.DXF -- PAGE NO. 5142

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203 ST ISA100X65X6 0.20 0.015204 ST ISA100X65X6 0.20 0.015207 ST ISA100X65X6 0.84 0 .062208 ST ISA100X65X6 0.84 0.062209 ST ISA100X65X6 0.84 0.062210 ST ISA100X65X6 0.84 0.062211 ST ISA100X65X6 0.84 0.062212 ST ISA100X65X6 0.84 0.062213 ST ISA100X65X6 1.16 0.085

214 ST ISA100X65X6 1.16 0.085215 ST ISA100X65X6 1.16 0.085216 ST ISA100X65X6 1.16 0.085217 ST ISA100X65X6 1.16 0.085218 ST ISA100X65X6 1.16 0.085219 ST ISA100X65X6 1.23 0.090220 ST ISA100X65X6 1.23 0. 090221 ST ISA100X65X6 1.23 0.090222 ST ISA100X65X6 1.23 0.090223 ST ISA100X65X6 1.23 0.090224 ST ISA100X65X6 1.23 0.090225 ST ISA100X65X6 0.84 0.062226 ST ISA100X65X6 0.84 0.062227 ST ISA100X65X6 0.84 0.062228 ST ISA100X65X6 0.84 0.062

229 ST ISA100X65X6 0.84 0.062230 ST ISA100X65X6 0.84 0.062235 ST ISA100X65X6 0.80 0.058236 ST ISA100X65X6 0.80 0.058237 ST ISA100X65X6 0.80 0.0 58238 ST ISA100X65X6 0.80 0.058239 ST ISA100X65X6 0.80 0.058240 ST ISA100X65X6 0.80 0.058241 ST ISA100X65X6 0.89 0.065242 ST ISA100X65X6 0.89 0.065243 ST ISA100X65X6 0.89 0.065244 ST ISA100X65X6 0.89 0.065245 ST ISA100X65X6 0.89 0.065246 ST ISA100X65X6 0.89 0.065

3018 ST ISA100X65X6 1.25 0.0923019 ST ISA100X65X6 1.26 0.0933030 ST ISA100X65X6 1.83 0.1343031 ST ISA100X65X6 1.83 0.13 43038 ST ISA100X65X6 1.83 0.1343039 ST ISA100X65X6 1.83 0.1343050 ST ISA100X65X6 1.25 0.0923051 ST ISA100X65X6 1.26 0.0934018 ST I SA100X65X6 1.25 0.0924019 ST ISA100X65X6 1.26 0.0934030 ST ISA100X65X6 1.83 0.1344031 ST ISA100X65X6 1.83 0.1344038 ST ISA100X65X6 1.83 0.1344039 ST ISA100X65X6 1.83 0.134

4050 ST ISA100X65X6 1.25 0.0924051 ST ISA100X65X6 1.26 0.0935018 ST ISA100X65X6 1.25 0.0925019 ST ISA100X65X6 1.26 0.093DXF IMPORT OF TOWER.DXF -- PAGE NO. 5143

5030 ST ISA100X65X6 1.83 0.1345031 ST ISA100X65X6 1.83 0.1345038 ST ISA100X65X6 1.83 0.1345039 ST ISA100X65X6 1.83 0.1345050 ST ISA100X65X6 1.25 0.0925051 ST ISA100X65X6 1.26 0.09310476 ST ISA100X65X6 0.22 0.016

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10520 ST ISA100X65X6 0.20 0.01510521 ST ISA100X65X6 0.20 0.01510537 ST ISA100X65X6 0.22 0.016

----------------TOTAL = 7.976

************ END OF DATA FROM INTERNAL STORAGE ************

705. STEEL MEMBER TAKE OFF LIST 140 141 145 146 151 TO 154 167 TO 170 231 TO 234 -DXF IMPORT OF TO WER.DXF -- PAGE NO. 5144

STEEL TAKE-OFF--------------

PROFILE LENGTH(METE) WEIGHT(KN )

706. 247 TO 250 255 256 260 261 133 TO 139 142 TO 144 147 TO 150 171 172 205 206 -707. 251 TO 254 257 TO 259 262 263 TO 268 3001 TO 3006 3011 TO 3014 3016 3021 -708. 3023 TO 3026 3028 3033 3036 3041 3043 3044 TO 3046 3048 3053 3055 TO 3058 -709. 3063 TO 3068 4001 TO 4006 4011 TO 4014 4016 4021 4023 TO 4026 4028 4033 4036 -710. 4041 4043 TO 4046 4048 4053 4055 TO 4058 4063 TO 4068 5001 TO 5006 -

711. 5011 TO 5014 5016 5021 5023 TO 5026 5028 5033 5036 5041 5043 TO 5046 5048 -712. 5053 5055 TO 5058 5063 TO 5067 5068ST ISA100X65X6 138.35 10.150ST ISA100X100X6 28.73 2.575

----------------TOTAL = 12.725

MEMBER PROFILE LENGTH WEIGHT(METE) (KN )

133 ST ISA100X65X6 1.91 0.140134 ST ISA100X65X6 0.83 0.061

135 ST ISA100X65X6 0.83 0.061136 ST ISA100X65X6 1.91 0.140137 ST ISA100X65X6 2.36 0.173138 ST ISA100X65X6 2.36 0.173139 ST ISA100X65X6 1.88 0.138140 ST ISA100X65X6 1.79 0.131141 ST ISA100X65X6 1.79 0.131142 ST ISA100X65X6 1.88 0.138143 ST ISA100X100X6 3.83 0.344144 ST ISA100X100X6 3.83 0.344145 ST ISA100X65X6 1.22 0.089146 ST ISA100X65X6 1.22 0.089147 ST ISA100X65X6 2.31 0.170148 ST ISA100X100X6 3.30 0.296

149 ST ISA100X100X6 3.30 0.296150 ST ISA100X65X6 2.31 0.170151 ST ISA100X65X6 1.78 0.131152 ST ISA100X65X6 2.52 0.185153 ST ISA100X65X6 2.52 0.185154 ST ISA100X65X6 1.78 0.131167 ST ISA100X65X6 1.22 0.089168 ST ISA100X65X6 1.72 0.126169 ST ISA100X65X6 1.72 0.126170 ST ISA100X65X6 1.22 0.089171 ST ISA100X65X6 0.81 0.060172 ST ISA100X65X6 0.81 0.060205 ST ISA100X65X6 0.88 0.064

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206 ST ISA100X65X6 0.88 0.064231 ST ISA100X65X6 1.22 0.089232 ST ISA100X65X6 1.72 0.126233 ST ISA100X65X6 1.72 0.126234 ST ISA100X65X6 1.22 0.089247 ST ISA100X65X6 1.78 0.131248 ST ISA100X65X6 2.52 0.185DXF IMPORT OF TOWER.DXF -- PAGE NO. 5145

249 ST ISA100X65X6 2.52 0.185250 ST ISA100X65X6 1.78 0.131251 ST ISA100X65X6 2.38 0.174252 ST ISA100X100X6 3.35 0.300253 ST ISA100X100X6 3.35 0.300254 ST ISA100X65X6 2.38 0.174255 ST ISA100X65X6 1.22 0.089256 ST ISA100X65X6 1.22 0.089257 ST ISA100X100X6 3.88 0.348258 ST ISA100X100X6 3 .88 0.348259 ST ISA100X65X6 1.87 0.138260 ST ISA100X65X6 1.79 0.131261 ST ISA100X65X6 1.79 0.131262 ST ISA100X65X6 1.87 0.138263 ST ISA100X65X6 2.36 0.173

264 ST ISA100X65X6 2.36 0.173265 ST ISA100X65X6 1.91 0.140266 ST ISA100X65X6 0.83 0.061267 ST ISA10 0X65X6 0.83 0.061268 ST ISA100X65X6 1.91 0.140

3001 ST ISA100X65X6 0.12 0.0093002 ST ISA100X65X6 0.05 0.0033003 ST ISA100X65X6 0. 05 0.0033004 ST ISA100X65X6 0.05 0.0033005 ST ISA100X65X6 0.05 0.0033006 ST ISA100X65X6 0.12 0.0093011 ST ISA100X65X6 0.31 0.0233012 ST ISA100X65X6 0.64 0.0473013 ST ISA100X65X6 0.64 0.047

3014 ST ISA100X65X6 0.31 0.0233016 ST ISA100X65X6 0.85 0.0623021 ST ISA100 X65X6 0.85 0.0623023 ST ISA100X65X6 0.49 0.0363024 ST ISA100X65X6 1.12 0.0833025 ST ISA100X65X6 1.12 0.0833026 ST ISA100X65X6 0.4 9 0.0363028 ST ISA100X65X6 1.10 0.0803033 ST ISA100X65X6 1.10 0.0803036 ST ISA100X65X6 1.10 0.0803041 ST ISA100X65X6 1.10 0.0803043 ST ISA100X65X6 0.49 0.0363044 ST ISA100X65X6 1.12 0.0833045 ST ISA100X65X6 1.12 0.083

3046 ST ISA100X65X6 0.49 0.0363048 ST ISA100X 65X6 0.85 0.0623053 ST ISA100X65X6 0.85 0.0623055 ST ISA100X65X6 0.31 0.0233056 ST ISA100X65X6 0.64 0.0473057 ST ISA100X65X6 0.64 0.0473058 ST ISA100X65X6 0.31 0.0233063 ST ISA100X65X6 0.12 0.0093064 ST ISA100X65X6 0.05 0.0033065 ST ISA100X65X6 0.05 0.0033066 ST ISA100X65X6 0.05 0.0033067 ST ISA100X65X6 0.05 0.0033068 ST ISA100X65X6 0.12 0.009

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DXF IMPORT OF TOWER.DXF -- PAGE NO. 5146

4001 ST ISA100X65X6 0.12 0.0094002 ST ISA100X65X6 0.05 0.0034003 ST ISA100X65X6 0.05 0.0034004 ST ISA100X65X6 0.05 0.0034005 ST ISA100X6 5X6 0.05 0.0034006 ST ISA100X65X6 0.12 0.0094011 ST ISA100X65X6 0.31 0.023

4012 ST ISA100X65X6 0.64 0.0474013 ST ISA100X65X6 0.64 0.0474014 ST ISA100X65X6 0.31 0.0234016 ST ISA100X65X6 0.85 0.0624021 ST ISA100X65X6 0.85 0.0624023 ST ISA100X65X6 0.49 0.0364024 ST ISA100X65X6 1.12 0.0834025 ST ISA100X65X6 1.12 0.0834026 ST ISA100X65X6 0.49 0.0364028 ST ISA100X65X6 1.10 0.0804033 ST ISA100X65 X6 1.10 0.0804036 ST ISA100X65X6 1.10 0.0804041 ST ISA100X65X6 1.10 0.0804043 ST ISA100X65X6 0.49 0.0364044 ST ISA100X65X6 1.12 0.083

4045 ST ISA100X65X6 1.12 0.0834046 ST ISA100X65X6 0.49 0.0364048 ST ISA100X65X6 0.85 0.0624053 ST ISA100X65X6 0.85 0.0624055 ST ISA100X65X6 0.31 0.0234056 ST ISA100X65X6 0.64 0.0474057 ST ISA100X65X6 0.64 0.0474058 ST ISA100X65X6 0.31 0.0234063 ST ISA100X65X 6 0.12 0.0094064 ST ISA100X65X6 0.05 0.0034065 ST ISA100X65X6 0.05 0.0034066 ST ISA100X65X6 0.05 0.0034067 ST ISA100X65X6 0.05 0.0034068 ST ISA100X65X6 0.12 0.009

5001 ST ISA100X65X6 0.12 0.0095002 ST ISA100X65X6 0.05 0.0035003 ST ISA100X65X6 0.05 0.0035004 ST ISA100X65X6 0.05 0.0035005 ST ISA100X65X6 0.05 0.0035006 ST ISA100X65X6 0.12 0.0095011 ST ISA100X65X6 0.31 0.0235012 ST ISA100X65X6 0.64 0.0475013 ST ISA100X65X6 0.64 0.0475014 ST ISA100X65X6 0.31 0.0235016 ST ISA100X65X6 0.85 0.0625021 ST ISA100X65X6 0.85 0.0625023 ST ISA100X65X6 0.49 0.0365024 ST ISA100X65X6 1.12 0.083

5025 ST ISA100X65X6 1.12 0.0835026 ST ISA100X65X6 0.49 0.0365028 ST ISA100X65X6 1.10 0.0805033 ST ISA100X65X6 1.10 0.0805036 ST ISA100X65X6 1.10 0.0805041 ST ISA100X65X6 1.10 0.080DXF IMPORT OF TOWER.DXF -- PAGE NO. 5147

5043 ST ISA100X65X6 0.49 0.0365044 ST ISA100X65X6 1.12 0.0835045 ST ISA100X65X6 1.12 0.0835046 ST ISA100X65X6 0.49 0.0365048 ST ISA100X65X6 0.85 0.062

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5053 ST ISA100X65X6 0.85 0.0625055 ST ISA100X65X6 0.31 0.0235056 ST ISA100X65X6 0.64 0.0475057 ST ISA100X65X6 0.64 0.0475058 ST ISA100X65X6 0.31 0.0235063 ST ISA100X65X6 0.12 0.0095064 ST ISA100X65X6 0.05 0.0035065 ST ISA100X65X6 0.05 0.0035066 ST ISA100X65X6 0.05 0.003

5067 ST ISA100X65X6 0.05 0.0035068 ST ISA100X65X6 0.12 0.009----------------

TOTAL = 12.725

************ END OF DATA FROM INTERNAL STORAGE ************

713. STEEL MEMBER TAKE OFF LIST 3007 TO 3010 3015 3017 3020 3022 3027 3029 3032 -DXF IMPORT OF TOWER.DXF -- PAGE NO. 5148

STEEL TAKE-OFF--------------

PROFILE LENGTH(METE) WEIGHT(KN )

714. 3034 3035 3037 3040 3042 3047 3049 3052 3054 3059 TO 3062 4007 TO 4010 4015 -715. 4017 4020 4022 4027 4029 4032 4034 4035 4037 4040 4042 4047 4049 4052 4054 -716. 4059 TO 4062 5007 TO 5010 5015 5017 5020 5022 5027 5029 5032 5034 5035 5037 -717. 5040 5042 5047 5049 5052 5054 5059 TO 5062ST ISA100X65X6 6 6.57 4.884

----------------TOTAL = 4.884

MEMBER PROFILE LENGTH WEIGHT

(METE) (KN )

3007 ST ISA100X65X6 0.98 0.0723008 ST ISA100X65X6 1.00 0.0733009 ST ISA100X65X6 0.97 0.0713010 ST ISA100X65X6 0.99 0.0733015 ST ISA100X65X6 0.79 0.0583017 ST ISA100X65X6 0.81 0.0593020 ST ISA100X65X6 0.79 0.0583022 ST ISA100X65X6 0.81 0.0593027 ST ISA100X65X6 0.98 0.0723029 ST ISA100X65X6 1.00 0.0733032 ST ISA100X65X6 0.98 0.0723034 ST ISA100X65X6 1.00 0.073

3035 ST ISA100X65X6 0.98 0.0723037 ST ISA100X65X6 1.00 0.0733040 ST ISA100X65X6 0.98 0.0723042 ST ISA100X65X6 1.00 0.0733047 ST ISA100X65X6 0.79 0.0583049 ST ISA100X65X6 0.81 0.0593052 ST ISA100X65X6 0.79 0.0583054 ST ISA100X65X6 0.81 0.0593059 ST ISA100X65X6 0.98 0.0723060 ST ISA100X65X6 1.00 0.0733061 ST ISA100X65X6 0.97 0.0713062 ST ISA100X65X6 0.99 0.0734007 ST ISA100X65X6 0.98 0.072

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4008 ST ISA100X65X6 1.00 0.0734009 ST ISA100X65X6 0.97 0.0714010 ST ISA100X65X6 0.99 0.0734015 ST ISA100X65X6 0.79 0.0584017 ST ISA100X65X6 0.81 0.0594020 ST ISA100X65X6 0.79 0.0584022 ST ISA100X65X6 0.81 0.0594027 ST ISA100X65X6 0.98 0.0724029 ST ISA100X65X6 1.00 0.073

4032 ST ISA100X65X6 0 98 0 0724034 ST ISA100X65X6 1 00 0 073