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LYMAN WO:4a14o WE:44�47.3 Truss ID:W TOP CHOR�S: 2-4x2 SPF 1650E-1.5E 2xti continuous strongback. Attach to each -.;oTnt Locations BOT CHORDS: 4x2 SPF 2100E-1.8E � truss with 3-lOd nails. Splice stiffback 1) 0- G- i� �) I3- 7- 8 15) 16- 1- 0 4x2 SPf 2400f-2.OE 1 on truss vertical. 2) 2- •-1� 9) l6- 1- 0 16) 14- 0- 0 WEBS: 4x2 SPF STANDARD NOTE: Maximim truss spacing is 16.0" o.c. 3) 4-11- G 10) 18- 6- 8 17) 11- 2- 0 2-4x2 SPF 1650E-1.5E 2.3 All COFPRESSION Chords are assumed to be 4) 5- 7- 0 li) 21- 0- 0 18) 9-10- 0 4x2 SPF 1650E-1.5E 13,16 continuously braced unless noted otherwise. 5) 7- 4- S 12? 23- 8- 8 19) 4-11- 0 6) 9-10- 0 13) 23- 8- 8 20) 0- 0- 0 ..TC...FORCE...CSI ..BC...FORCE...CSf �) 11- 2- O la) ZI- O- O i- 2 -z� o.si zo-i9 soas o.ss ---- TOTAI. DESIGN LOAUS ------------ 2- 3 -8098 0.69 i9-ie eo9e o.se Uniform PLF From PLF To 3- 4 -8098 0.�s �e-i> >eso o.eo TC Vert -76 0- 0- 0 -76 1- 3- 0 4- 5 -8098 0.52 11•16 6713 0.73 TC Yert -317 1- 3- 0 -317 4-11- � 5- 6 -7850 0.53 16-15 6113 0.88 TC Vert -66 4-11- 0 -66 23- 8- 8 6- 7 -7549 0.34 15-14 d092 0.56 BC Vert -6 �- 0- � -6 23- 8- 8 7- 8 -7549 o.si i�-i3 2367 o.s2 Concentrated LBS Location 8- 9 -5652 o.3s TC Vert -1325 4-11- 0 9-10 -5652 0.34 10-11 -2367 o.2t � h�� 11-12 -I 7 0.10 � � �� O► (�� .MEB...FORCE...C51 .MEB...FORCE...CSI W� � � � « �b� �-.M� 1-20 -179 0.04 8-17 947 0.80 �� m� � � a � R�� 2-20 -5628 0.33 8-15 -1202 0.34 V�d( � � � � � d � 2-19 3526 0.33 9-15 -230 0.05 3-19 -1737 0.35 10-15 1768 Q.33 �� 5-19 4 0.00 10-14 -1955 0.56 - -- � 5-18 -277 0.08 i1-14 9l2 0.80 6-18 153 0.13 11-13 -2623 0.38 6-17 -422 0.09 12-13 -B6 0.02 ��e�f Z'�Z �-i� -�s 2 0.0 3 ��-- ---- � No. 12489 28.� s 23-8-8 1 2 3 4 5 6 7 8 8 10 11 12 1.5X32 1.5X3.2 TL16-8X17.5 W=3X4.8 1.5X4.8 ST18-5X10.4 1.5X4.8 1.SX4.8 3X6.4 4X4 4X4 6X6.4 1.SX4.8 6X8 -�' ' _ a �- 1-6-0 1-6-0 �- TL16-6X13.7 8X16 3X4 3X6.4 N=3X6.4 4X12 4X6.4 4X12 �- W=TL16-3Xt 1.2 � 23-8-8 � � 20 19 18 17 16 15 14 13 2736#3.50' 1260#3.50' 23-8-8 � EXCEPT WHERE SHOWN,ALL PLATES TO BE TEE-1_OK 2aGA ST scale = 0.2500 W�iRNING: R�D ALL NOTES ON THIS SHEET. TC Live 40.0 psf Designed By:BS �DQDQA COPY OF TIIIS DRAWING TO BE GIVEN TO ERECTING CONTRACTOR. TC Dead 10.0 psf (� BRAC[NGR'ARNING DESIGNINFORMATIOIY BC LIVQ 0.0 pSf Checked By: M Bracing shown on this d�aM'ing fa not ercuion Fracing,wind 6racing, This deri$n u for an indi��d building canponent a+J ha.r 6een 6aard on in forma- pvrral6mcing o�rimilar 6racing which is a�+an o f the building Cvn prmaded by the cGent The design�r duclmma any rcaporvi6ility for damagea derian and which must 6e consider�ed 6 y the E��ilding designer. ar a rciu@ o f fmdty w incorrce�in jomwtian,apeci f�caticns and/w de:igns BC Dead 5.0 P� Date:10-30.92 �� Braung shown u/or laterd uppore o f durr mem6en on!y to rcduae fumuhed ra the war desianer by the cfient and the rnrrcewear or ammcy of TOTAL 55.0 F1Sf buckling lengd�Prowions muat 6e made m�mchor laleral bracing thi.r in fom�ion aa)t may rclate ro a rpeciticpro�t,Thia dvu haa been at mdr and apeufied 7xatlonr determined by the 6uilding deaigner. deaignedin accordarae with'TPI-85"and NDS-86"ro 6e inco�poraecd as part of Design Criteria•TPI Additional bmcing of the overall rwcmre nt.��•be requi�ed. the buildirtg derign 6y a Bui/ding Derignn.A'hen m�irwed jor approvd 6y the LOAD DUR.FAC: 1.00 ' (Set NIB-91 of TPI).For speci f lt tfltSS bla�tttg Kqu vemtntr, building dtaignn,tht deaign loadings shown muat be chetked to 6e twe that the --•WOOD TRUSS SYSTEMS- contact buildir,g dui�ner. (Tn/aa Plate Inrtimrc,TPI,it locaud dam rhawn ax in agrcement wit/t the lacar 6uilding codea,local cli�C reco'dt SPAC I NG: 16.0" Sef�n:08.17.92-73147 at 58?D'Ono f rio Dnvc,Madvon,A'itmnrin 53719). far wi+td or rnow loads,pro ject apeci f'tcations or aprcid applied baAs.