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Name: FLA Customer:Lamperts Apple V 110:326591 TI:A Qty19 <br /> TC FORCE AU, END Cal Cr TC: 4x 2 SPP 24007-2.00 2x6 continuous strongback. Attach to each - Joint Locations <br /> 1- 2 0 0.00 0.17 0.17 C EC: 4x 2 SPr 24007-2.00 truss with 3-3.5"x 0.135" nails. Splice 1) 0- 0- 0 8) 16- 4- 4 15) 23- 9-12 <br /> 2- 3 -3444 0.11 0.17 0.29 C WD: 4x 2 SPP STUD (N) strongback on truss vertical. 2) 2- 7-12 9) 19- 1- 8 16) 1s- 9-12 <br /> 3- 4 -3444 0.14 0.12 0.27 C 11 or (): Plato(s) 0878ET from joint canter. NOTE: Maximise truss spacing is 19.2" o.c. 3) 5- 1- 4 10) 18- 9-12 17) 13-10-12 <br /> The Joint Detail Report must be included All COMPRESSION Chords are assumed to be 4) 7- 6-12 11) 21- 3- 4 18) 11-11- 0 <br /> 4- 5 -5200 0.32 0.13 0.45 C with my submittal, inspection, and/or continuously braced unless noted otherwise. 5) 10- 0- 4 12) 23- 8-12 19) 10- 0- 4 <br /> 5- 6 -5200 0.35 0.17 0.52 C fabrication documentation. In-Plant Quality Assurance with Cq- 1.11 6) 12- 5-12 13) 25-11- 0 20) 5- 1- 4 <br /> 6- 7 -5488 0.28 0.06 0.34 C This truss is designed in accordance with In-Plant Quality Assurance, per 7) 13-10-12 14) 25-11- 0 21) 0- 0- 0 <br /> 7- 8 -5486 0.39 0.18 0.57 C the 2006 International Residential Code see. 3.2.4 of TPI-1-02, for joint(s)1 ------------ TOTAL DESIGN lows ------------ <br /> 8- 9 -4503 0.24 0.12 0.36 C sections 8502.31.1 and 8802.10.2 and 2,4,8,12,14,15,19,20,21 Uniform PLY Prom PLT To <br /> referenced standards, U.N.O. TC Vert L+D -79 0- 0- 0 -79 18- 1- 8 <br /> 9-10 -4503 0.19 0.12 0.31 C ----yam, REACTICNS PER BERRIM LOCATION----- TC Vert L+D -95 16- 1- 8 -95 25-11- 0 <br /> 10-11 -4503 0.24 0.15 0.39 C X-Loo Beet Vert Boris Uplift Y Type EC Vert L+D -7 0- 0- 0 -7 25-11- 0 <br /> 11-12 -1794 0.03 0.17 0.20 C 0- 1-12 1 1158 0 0 a Pin <br /> 12-13 0 0.00 0.17 0.17 C 25- 9- 4 1 1246 0 0 B B Roll <br /> PROVIDE UPLIFT CONNECTION PER SCHEDULE <br /> --------GLOBAL NAR DEPLECTIONS--------- <br /> BC FORCE AXL END CSI Cr LL TL <br /> 21-20 1974 0.20 0.07 0.26 C in./Ratio in./Ratio Jnt(s). <br /> 20-19 4499 0.45 0.06 0.51 C I-Span -0.49/619 -0.62/369 17-18 <br /> 19-18 5481 0.54 0.05 0.59 C Boris. 0.08 0.13 NA <br /> 16-17 5491 0.54 0.05 0.59 C Long term deflection factor - 1.50 <br /> 17-16 5179 0.51 0.07 0.58 C <br /> 16-15 3354 0.33 0.06 0.39 C <br /> 15-14 1785 0.19 0.03 0.20 C <br /> Web PORCH Web FORCE <br /> 21- 1 -89 17- 7 -146 <br /> 21- 2 -2236 17- 8 355 Typical Panel-28.75" <br /> 2-20 1664 8-16 -774 <br /> 20- 3 -187 16-10 -224 25-11-0 <br /> 20- 4 -1208 16-11 1317 <br /> 4-19 803 11-15 -1799 1 2 3 4 5 6 7 8 9 10 11 12 13 <br /> 19- 5 -203 15-12 909 <br /> 19- 6 -322 12-14 -2125 0-3-8 1.50 2E4 1.50 0-3-8 <br /> 6-17 10 14-13 -86 W 4:12 2E4 2x4 3E4 2E4 3X4 �'i'�� 4x12 E6 ZE4 <br /> See explanation of Repetitive Z o o Z <br /> 1-6-0 1-6- <br /> Member ractor, Cr, on 0 <br /> reverse side of paper or <br /> TEC Form 8.14.2007. 618 4:12 316 W-MT18 3X1,26 4:12 1601 618 <br /> N-1.5x3 <br /> 1158.50" 1246#3.50" <br /> 25-11-0 <br /> 1 0 19 is 17 16 IS 4 <br /> EXCEPT AS BROWN PLATZ8 ARE MiTak MT20 Scale 0.23% <br /> HARMING: Eng Job: NO: 326591 <br /> Raw ALL NOTES ON TSxe OMMT. A cora or Tsse DRAwLNs To as arm To <br /> SRaCTDAo CORTRRCTOR. ERRCINO RAdlNxNGt Dwq: TI: A <br /> 040 "elkb� Bmkgd�mddidmwmsf,°o`onomoe-xyy y�, 1.r ym"bus'i�oe'no Dsgnr:aW) Chk: 11/13/2009 <br /> exp-d*Woemdb.maWdiwW a. .��part <br /> m.mbm o*m t.dm.buckHn hq* mos b.mad.m-.hx hbml bm.l.p R endr.iw dmd imdo- <br /> d bym.bdld�Sd..�w.ndamo-1>..oleorm.o-mu.w.a.om.yb. (MeFi®A1o[TM.For TC Live 40.0 ps! Lbr Dr: 1.00 <br /> TFIN DrM, se°my�m�oom.mbwwbwa.°-.(rnwPb">munro'TP1 f-k""d sde:>m-' TC Dead 10.0 e! Plt DF: 1.00 <br /> Odw,l,4dl.oa weeo-ln s3Tls:. P <br /> compon.d Engines%by:Tnw 6oSin wing Co.,PA,918 Sounddd.Rd sa-mo.NC 2M2 BC Live 0.0 pef O.C.: 1- 7- 3 <br /> IAC-06/TPI-02/NDB-OS <br /> BC Dead 5.0 ps! Code: MN-Ree <br /> TOTAL 55.0 oaf v5.5.19-8031453 <br /> Design: Matrix: Analysis Profile Path: 7:\trusjcbs\326000\326591\7LR\A.prx <br />