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fl ECEI 1 /F1 Consulting 11114KIIIII ■Pr IIIM FEB 0 8 Structural 2007 Engineers ENGINEERS, INC. T CI" �y Structural Calculati f aiiir ods - Building 9 Job Number: 061253 Codes: 2003 IBC Amended by Oregon Structural Specialty Code with 2004 revisions. Date: 2 -7 -2007 Location: 14982 SW 109 Ave., Tigard, OR 97224 Client: Horizon Restoration • T 7301 SW Kable Ln. Suite 100 1($.0 PRop 4 ; Portland, OR 97224 ��5 <SINEFq`r�0 Phone: 503- 620 -2215 1 5 = 5 Engineer: Douglas S. Meltzer P.E. ` Cameron T. Carroll F.E. � REGON BMGP Engineers, Inc. Q � 19 Acs 1045 13 St. SE LASS.1J1E Salem, OR 97302 EXPIRES: 2 - 31 0 8 Phone: 503- 399 -1399 Scope of Services: Repair to existing condo building damaged by fallen trees. Contents: Truss Repair 1.1 — 1.3 Risa Print Out R.1— R.34 doe - rfi 7� // q5,2 5 W ! O9y-1-7 Q/e LIMITATIONS: Engineer was retained in a limited capacity for this project. Design is based upon the information provided by the client, who is solely responsible for accuracy of same. No responsibility and/or liability is assumed by, or is to be assigned to the Engineer for items beyond those shown on these sheets. 1 t i ' Oa (X-C-s ,Z. TR.LSS a r2,0 r /G€ OuE BE.: !ZOO Ai , it 000- ' -rif Q Chia IMS — SElAG T STf L CT. rA, E. - t5 I r Y W "y v-3 »r 4 6 ' - " r b' & yr 7'1-3rr `j IL. : 5- 6 r ' r•d # y y r o -d �L tc = IS rsF � = 3C) PGF OL,3c, = S PsF (21 = /0 ?G• arc. -- as rPSI (2 = SO PGF 12.1 PJZMJT 0uT (� 1 — /2 , 11 (P P. Ex, ST'A X 7' SEE Rj.SA ?tam our : A ,1Z - 12,13 AC..s-1s TucS AA AL'r'S '^ /AJitti 13 EA PP i ou 4 Por ki r) FILE NO. JC / � / .2. -6 SHEET NO. / ' Yom/ MADE BY DATE Z SALEM, OREGON CLIENT '`«? P C) ,c /- PROJECT (- .U 5(J lr } 13 G '12)(1 g 1'2c1s �'IZvss P12.O 00 ufA} r2A M-t I' Lrc. " 15 est (2') = GLT� = 2 5 PST (2' ) = 5� PG F OZ. d S Av (.2') = 10 ?C,F SEE ►a►sA p ►2,tiT O : 2.2L( -- 12 . 3 y Ilripurr F: % 1: 1 \ F: 1: 11 ti, I % 1'. SALEM, OREGON k.Wb C. 12,4tES I'S t3 d6ioki S = .2( 'r STrauc7: FILE NO. 0 1 Z--C 2 SHEET NO. i / 2 MADE BY �� C _ DATE 2 ._O X CLIENT Y:6 2.., -c O'€ , E-1.77 i As7 -io. PROJECT ��t4' - r . C:r..�rz.Y,' -- (...?,.(...L4 9 X7-1Z — : ` rn.7Zr3,1(y i croa or/ 0 _ E ._ 31V0 ? 3 7 3)?' s 2 vj ( ) ryl,11) ,, ON 133HS C" r 90 ON 31IA (5 / ,4.Z t Ztl (530 7 T) (, 5'1 )All /� NOJ3a0'VOWS 1%1 'S H "I I \ I '1 \ '1 f� ( 11 z>' 7l ' y Cob = it c77 - 7 "X V zi^ M s � �y t l l' 7 / � ` 171 /6 C1 �` ?ii y (1`Z do, , - . > oz '‘? 11 1 5'J7 v .L:;-(4 3 <= 3 I = CS if 0502 (rv/w) „ 20'Y (. // s7lie(Y o v /7 090z' 090' = 3�doj I a►3 l'�3`h' e S�CnS t x i, 1s (s� c z �/4f f ) o/ : s 37c■dig rr11 -') S/ • 2 (53Q SZ� �' s �� ) , 574.1,3/ ''-,4 of l /,01 Z Q7 /Xy' /Yj-( :1 '"id (l ,n o /7 • 75 ,, ,i 37c+i► ' /.hZ = (ST•1J Jc+t�ts / h 9 <= S3�VJ5 'V"0 51 - s . ojry >� S • <= 109 rY7 S7 /ten' C 1 0 017 c► ooh 3(7/3379 W 109N7 371v crfnp /7 / S'- l3S7c7v (f©cX'f AAi7ci ,6A 31 ZI i }/cj n`Z- X Mz 2 Ni\ 4170 �13 ao M� � A ' 14 2 3 4 5 T16 . 7 Solution: Envelope BMGP Engineers Inc. Canterbury Truss Analysis CTC p2C c Feb 2, 2007 at 3:23 PM 061252 ",/pt,') 7f 4?-6' , Truss #3 Analysis.r3d 12. -- - ' Y Z X .ilk‘ Solution: Envelope BMGP Engineers Inc. Canterbury Truss Analysis CTC Feb 2, 2007 at 3:23 PM 061252 Truss #3 Analysis.r3d Company : BMGP Engineers Inc. Feb 2, 2007 Designer : CTC 3:24 PM Job Number : 061252 Canterbury Truss Analysis Checked By: Global Display Sections for Member Calcs 5 Max Internal Sections for Member Calcs " 97 Include Shear Deformation Yes IncludeWarping Yes _ Area Load Mesh (inA2) _ 144 Merge Tolerance (in) .5 P -Delta Analysis Tolerance I 0.50% Vertical Axis Y Hot Rolled Steel Code AISC: ASD 9th Cold Formed Steel. Code AISI 99: ASD Wood Code ! NDS 91/97: ASD Wood Temperature < 100E Concrete Code ACI 2002 Number of Shear Regions 4 Region'Spaclnq'Increment (in) a,: `4 Biaxial Column Method PCA Load Contour Parme Beta Factor (PCA) , ;':65' `'. Concrete Stress Block Rectangular Use Cracked Sections: Yes Bad Framing Warnings I No Unused Force Warnings 1Yes , Wood Material Properties Label Species Grade Cm Emod Nu Therm...Dens[k/f 1 DF Larch Douglas Fir -Larch Select Structural 1 3 3 .035 2 So Pinef :A), '4$autNn e F tne € ; ; ii ?; ' ' ,, Noll :`; i� ,, 1 .: s ,'3 , .3 ' ,b35 Wood Section Sets Label Shape Type Design List Material Design Rules A [in2l Ivy fin41 Izz fin4] J [in4[ 1 IWOODIA 1 2X4 Beam Rectangular I DF Larch Typical I 5.25 .984 1 5.359 2.877 Member Primary Data Label I Joint J Joint K Joint Rotate(deg) Section /Shape Type Design List Material Design Ru... 1 M1 N8 N10 WOOD1A Beam Rectangular DF Larch Typical 2 M2 'N10 N7 11 . ;,WOOD1A Beam Rectangular DF Larch Typical 3 M3 N1 N7 WOOD1A Beam Rectangular DF Larch Typical 4 M4 N1 N8 ' °' WOOD1A Beam Rectangular DF Larch Typical 5 M5 N2 N9 WOOD1A Beam Rectangular DF Larch Typical 6 M6 N3 N10 WOOD1A . Beam Rectangular DF Larch Typical 7 M7 N4 _ N11 WOOD1A Beam Rectangular DF Larch Typical 8 M8 N5 N12 WOOD1A Beam Rectangular DF Larch Typical 9 _ M9 N6 N13 WOOD1A Beam Rectangular DF Larch Typical 10 M10 N8' N2 WOOD1A Beam Rectangular DF Larch Typical 11 M11 N9 N3 WOOD1A Beam Rectangular DF Larch Typical 12 M12 N3 N11 WOOD1A Beam Rectangular DF Larch Typical 13 M13 N4 N12 WOOD1A Beam Rectangular DF Larch Typical 14 M14 N5 N13 WOOD1A Beam Rectangular DF Larch Typical RISA -3D Version 6.0.1.5 [H:\Jobs 200610612521Calculations\Truss #3 Analysis.r3d] Page 1 l� .1 Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 3:24 PM Job Number 061252 Canterbury Truss Analysis Checked By: Joint Coordinates and Temperatures ` Label X [ftl Y [ft] Z [ft] Temp [F] Detach From Diap.., 1 N1 0 0 0 0 2 N2 7.25 0 0 0 3 N3 13.96 0 0 0 - 4 N4 20.6667 0 0 0 5 N5 27.91667 0 0 0 6 N6 34.08333 0 0 0 -- 7 N7 42 0 0 0 8 N8 0 4.75 0 0 9 N9 7.25 7.1667 _ 0 0 10 NiO 13.96 9.403 0 0 11 N11 20.6667 7.1667 0 0 12. N12 27.917 1 4.75 0 0 13 N13 34.08333 2 6944 0 0 - - - - -- - - -- 14 N14 0 { 0 0 0 Joint Boundary Conditions Joint Label X [k/in] Y [k/inl Z [k/in] X Rot.[k- ft/rad] Y Rot.[k- ft/rad] Z Rot.[k-ft/rad] Footing n.:4r-,,,,arP2'.3"?, I N1 Reaction Reaction Reaction r7.' ,1 k1 i x e § ' Reaction .' , N 10 Fixed V. k ll';- s 2 Fixed' _ Wood Design Parameters Label _ Shape Length... le2[ft] lel [ft] le -bend top[ftL_ le -bend bot[ft] Kvy Kzz CH Cr y sway z sway 1 M1 WOOD1A 14.715 1 7 I Yes 2, M2 WOOD1A 28.575 ' 1 6.5. ' ',: - . 1 1 x.. Al ' A VG5 'Z" 3 M3 WOOD1A 42 1 7 , M4 WOOD1A 4.75 1 .- Yes 5 M5 WOOD1A 7.167 3.5 Yes ?: M6 wooD1 A 9.4031" 1.: 475 J (7' 'q , , ' "< 7 M7 WOOD1A 7.167 3.5 �• 8 M8 WOOD1A 4.75 Yes Yes' , , ,'I_., 9 M9 WOOD1A 2.694 Yes 10 . , M10 WOOD1A 8.667 4.33 Yes 11 M11 WOOD1A 9.818 5 Yes 12 M12 WOOD 9.815 5 '' r a: ,: Ye : : 13 M13 WOOD1A 8.668 4.33 Yes 14 M14 WOOD1A 6.73 3.5 ;�. .r' `` w: k` , Member Distributed Loads (BLC 9 : Dead Load) Member Label Direction Start Magnitude[k/ft,d..End Magnitude[k/ft,d... Start Location[ft. %] End Locationtft,%) 1 M1 ¥ -.03 -.03 0 0 2 M2 .Y -.03 03 ; . 0. - 0 3 M3 Y -.01 -.01 0 0 Member Distributed Loads (BLC 2 : Snow Load) Member Label Direction Start Magnitude[k/ft,d..End Magnitude[k/ft,d... Start Location[ft, %1 End Locationjft,%1 1 M1 Y -.05 -.05 0 0 2 M2 Y -.05 -.05 0 0 RISA -3D Version 6,0.1.5 [H:1Jobs 200610612521Calculations\Truss #3 Analysis.r3d] Page 2 Company : BMGP Engineers Inc. Feb 2, 2007 Designer C TC 3:24 PM Job Number : 061252 Canterbury Truss Analysis Checked By: Basic Load Cases BLC Description Category X GravityY Gravity Gravity Joint Point Distribu...Area (M..Surface... 1 Dead Load DL o- .. -�a 3 ^4}i�' ��� a 't ' +r ro �t - t r� ?" - '�seaf q 1 to '' .' L-._ k gbits.`a i 3 �z yi } ply r t _ a ,:SnowLadt. <a +, x.:.r, . .e . , ... , ..t 's. +a e .- ;.k:S. ._c -.., ..t;. a, r cr n.s: H$.. Load Combinations • Description Solve PDelta SRSS BLC act...BLC Fact.. BLC act...BLC Fact. .BLC Fact,..BLC act.. BLC Fact..BLC Fact... 1 Dead Load Yes DL 1 a rk . _ m E 3¢ E x . E : ME e ' 1 - ?e R . ' erF :. Envelope Joint Displacements Joint X [in] Ic Y [in] Ic Z [in] Ic X Rotation ... Ic Y Rotation .. Ic Z Rotation [... Ic 1 N1 max 0 2 0 1 0 1 0 1 0 1 -2.467e-3 1 '1 74: 3 N2 ® 0 © -.093 0 5 0 ® 0 _ 0 0 0 -5 104e -4 0 �:. 4�iy, IR 16 c IF: e� 9`OI � 21141�4 A TREE .3.�.. T vs F'I I :t` , E ' y 5 N3 max 014 E � 157 0 0 0 0 0 0 Ell -8.261e-4 0 � _ �M �t '0-fl ' 1 , $ r ?' „ }�a.. fa7 7 ® N4 C .038 © -.214 y 0 0 EEllE y 0 0 -6.886e-4 0 b CS v1 " $ TEI i `T'. e ;4 t� J '1 ,. �" MIN ,- ^� �A 6 . t gY 't - , 9 N5 .073 © 24 m 2 � �Fy, 0 d� 0 ( 0 0 0 Ell 1 815e -4 0 - $ '-� i. . � �- 5.4`k� & 9.s..d.a'k (,.'!� C K_, IMENVELEMEA Y'�. 2.' 47 11 N6 max .11 © 2 0 0 0 0 0 ` 0 Ell 1.92e-3 FM 13 N7 MEM .157 © 0 0 0 0 0 0 0 0 8.432e-3 OM I " MOI' T: ITER DITERVEM 15 N8 max .104 ® -.005 El 0 0 0 i 0 0 Ell -5.126e-3 0 e t� , ^y, +Ts�^' i� �. ,i� t <. s 0 - �. -� '` •o f. r ,. '� - . 3, .. ® $ ' *.� 2 ' ` ', - e ' " �, a �fid 17 N9 max .156 © -.096 0 0 .0 0 0 0 Ell -3.271e-4 0 ,. mi ; a e ] : _ or" R v E . -° Pi's, 6; I. $ , i -5 9 q 19 N10 max .18 © -.153 0 0 0 0 0 0 0 -3.945e-3 0 21 N11 ® .117 © -.21 0 0 0 0 0 0 -3.024e-4 Ell 23 N12 ® .064 © 241 0 2.269e-3 � 0 O 0 D 0 24k ais $ r *j a 1 ,'e 80 ' S vd a I' Q z s w In � Q� ®' � � ' St 3 2� � � � s tj� �r � �� � . 25 N13 max .043 © -.222 0 0 0 0 0 0 0 -1.4e-3 0 ,� ,,,; ,� �. , � >a-� r� - t , k.�::. A a fTllfl _f .0 9 a . .. 502 . 2= . EMN itTAS :? . . , ' 0 5..' Vii: `a,i�.t ,.. tlii - 4`..77e,- 27 N14 ® 0 MI 0 1 0 1 0 MI 0 1 0 fP', #r .t M; =,1 nt ,1„ q 5 ktir!O ARP Envelope Joint Reactions Joint X_k] Ic Y [11_ Ic Z [k] lc MX [k -ft] Ic MY [k -ft] Ic MZ [k -ft] Ic 1 N1 max 0 1 1.983 2 0 1 0 1 <. htrl' ag + . rr`ur . =,' 0 ,. :VW , 3 .,.. 875. ,' 1-' d. , NOM .v `.1 } ` rxQ° : ", ..: 3 ae f 0 . 1.° b...' .1 "' 3 N7 max 0 1 1.98 2 0 1 0 1 0 1 0 1 5 Totals: max 0 1 3.963 2 0 1 RISA -3D Version 6.0.1.5 [H: \Jobs 2006 \061252 \Calculations \Truss #3 Analysis.r3d] Page 3 Company : BMGP Engineers Inc. Feb 2, 2007 Designer : CTC 3:24 PM Job Number : 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Forces Member Sec Axialjkl Ic v Shearfkl Ic z Shearfkl Ic Torque[k -... Ic v-y Mome... Ic z -z Momentfk -ft] Ic 1 M1 1 max 1.905 2 .224 2 0 1 0 1 0 1 0 1 2 min .835 1 .084 1 0 1 0 1 0 1 0 . 1 3 2 max 1.812 2 -.021 1 0 1 0 1 0 1 -.117 1 4 min .8 1 -.055 2 0 1 0 1 0 1 -.311 2 5 3 ,max 1.719 2 -.125 1 0 1 0 1 0 1 .406 2 6 min .765 1 .334. 2 0 1 0 1 0 1 .151 1 7 4 max 2.104 2 .082 2 0 1 0 1 0 1 -.08 1 ;;`:8 min .928 1. .031 1 0 1 0 1 0 1 -.212 2 9 5 max 2 2 -.074 1 0 1 0 1 0 1 0 1 .10 mm .894 1 .197 2 0 1 0 1 0 1' 0 1 11 M2 - __ 1 max 2.009 2 .206 2 0 1 0 1 0 1 0 1 _12 in. .893 1 .077 1 0 1 0 I 1 0 1 0 1 13 1 2 max 3.042 2 .2912 ' 0 1 0 I 0 1 -_ -_.341 2 14 mm 1.348 1 1 .109 1 0 1 0 1 1 0 1 1 .127 1 15 3 max 4.135 2 .213 21, 0 1 0 1 0 1 .23 2 46` min ., ,1:829 1 .08 4 - :1 0 1 0 1 0 1 .086 1 17 4 max 5.118 2.295 2 0 1 0 1 - __0 1 .107 2 'H'8 I min 2,265 1 .11 1 0 1 0 1 0 1 .036 1 19 1 5 max 5.306 2 1 -.1- 1 0 1 1 0 1 0 1 0 1 20 min 2.335 1 I . 266 2 0 } 1 0 1 0 1 - 0 ;2'i 21 M3 1 max 0 1 .03 -_ -2 0 11 0 1 0 1 ' 22 ' min 0 1 0 - 1 .029 1 0 1 0 1 0 1 0 1 23 2 max - .766 1 .004 1_I 0 1 0 1 0 1 -.015 1_ -- 24 r - _ min - 1.,737 2 .003. 2 _0 1 0 _1 0 1 -.017 2 25 3 max -1.76 1 .034 1 0 1 0 1 0 1 .028 1 26 mm = 3:988 2 033 2 _ 0 -1 0 1 __. 0 1 _021 _< - 2:4 27 28 - -, - 4 max -4.946 2 r = 0022- - -- 0 1 � 0 1 0 1 -.018 1 - - 004 1 0 1 0 1 0 1 -.041 2 - 29 _ __ - 5 max -2.182 1 - .036 1 0 1 0 1 0 1 0 1 30 - -- mm 4.946 2 -.041 2 0 1 0 1 0 1 0 1 31 M4 1 max 1.953 _2 0 1 0 1 0 1 0 1 0 1 32 min .846 1 0 1 0 1 0 1 0 1 0 1 33 _ 2 max 1.953 2 0 1 0 1 0 1 0 1 0 1 34 min .846 1: 0 1 0 1 0, ., . 1' 0 1 0 1 35 3 max 1.953 2 0 1 0 1 0 1 0 1 0 1 36 min .846 1 0 1 0 1. 0 • 0 1 0 1 37 4 max 1.953 2 0 1 0 1 0 1 0 1 0 1 38 min ,.846 1 0 1 0 1 0 1 0 1 .. 0 1 39 5 max 1.953 2 0 1 0 1 0 1 0 1 0 1 40 min .846 1 0 1 0. 1 0 1 0 1 0 1 41 M5 1 max 1.06 2 0 1 0 1 0 1 1 0 1 0 1 42 min .422 1 0 1 0 1 0 1 I 0 1 0 1 • 43 2 .max 1.06 2 0 1 0 1 0 1 0 1 0 1 44 min .422 1 0. 1 0 1 ..,. 0 1 0 1 0 1 45 3 max 1.06 2 0 1 0 1 0 1 0 1 0 1 . . 46 min .422 '1 0 1 0 . 1 0 _1 0 1 0 1 47 4 max _ 1.06 2 0 1 0 1 0 1 0 1 0 1 48 min .422 1 0 1 0 1 0 1_ 0 1 0 1 49 5 max 1.06 2 0 1 0 1 0 1 0 1 0 1 1'50 min .422 1 0 1 0 1 0 1 0 1 0 1 51 M6 1 max -.423 1 0 1 0 1 0 1 0 1 0 1 52 min -.892 2 0 1 0 1 0 1 0 1 0 1' 53 2 max -.423 1 0 1 0 1 0 1 0 1 0 1 54 min -.892 , 2 0 1 0 1 0 1 0 1 0 1 55 3 max -.423 1 0 1 0 1 0 1 0 1 0 1 56 min -.892 2 0 1 0 1 0 1 0 _ 1 0 1 RISA -3D Version 6.0.1.5 [H:\Jobs 200610612521Calculations\Truss #3 Analysis.r3d] Page 4 2 .6 Company : BMGP Engineers Inc. Feb 2, 2007 Designer CTC 3:24 PM Job Number : 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Forces (Continued) Member Sec Axial[k] Ic y Shear[k Ic z Shear[k Ic Torque[k -... Ic -y Mome... Ic z -z Moment[k -ft] Ic 57 4 max -.423 1 0 1 0 1 0 1 0 1 1 ' e' t'�.a,"'�c�°�' ;xt. ' ..,K "�' s . � ' k`a. z l 7. e `�a'4 c €k'. r 4� '� ',!' y Y 0 0. "k 1 U A F �° g - ...� � c '�. ,'� �'z' � x1�., �,ix � �" ` � .�- 3��''� . - �' a 3�r �z 1.� e��k:�. ' �3. � # ��` ' ; �{�x+. , �x �.I`� 59 - ©� -.423 0 0 1 0 0 0 0 0 II ` y r i '£ f i �. iy . t k ' 'kf. ! - .. .. „ ... y 2 w :.+Y YSQ , e ® � °»��sa. " ;a .e��, o ® II t2`. ���,�, ©�"�'o�k.a. 1,'�` � �t ':.. 9 �3 ' a �� .k ^ 1 Y r ., n� 61 M7 a 66 � 0® 365 0 0 1 0 0 . ' t Kok r iN4 k° p .� •» ,��°. F ..: dr n 4 '. � 0 � 0 0 0 , w'.v' ;n ' : $'.� :�:n ; ?g.:x' r „ 73 ?%' X2 MOM ":�-�F k ;.::a.� Uc e^s . z i4 V..0 r . , 1 ; V i 4 . 4 l� Y o li �.': 63 - ©� 365 0 0 1 0 0 0 0 0 11 • 0 0 m^ ' =k ,, T w t t ae ,a :e ` -`7z:s a - . ,a°a�&°ap.u;,k7i as a ti �� `Its' ;_ rx_. . A n : �� x f 65 ©M -.365 0 0 1 0 0 0 IN 0 D 0 0 9 e '.'4+ lit - e R4A: Z7; W1 t`' AV o wa i; a t g >` PlajJ4MITIElk i k Sc' 67 - 4 -.365 0 0 1 0 0 0 0 0 0 0 0 a � r z. s 'a ' 8 - k., ,'p a 0Men il R 0 E , 69 - - ©M .365 0 0 1 0 0 0 0 0 0 0 0 ' ll s i, Z,7 3�" a .�a a ` ` > 4 h :. '" ins. - n L t g s 2 sue-+° x e 71 M8 0® 251 0 0 1 0 0 0 0 0 0 0 0 73 - ©® 251 0 0 1 0 0 0111 0 ✓ i R' O 0 IM �' �i' E � ` r a IEME a M NE�M� E E a h 75 - j - 251 0 0 1 0 0 0 0 0 L arc p U. F 1 X5'2 F � . £e KI y f 77 • . 4® -.251 0 0 1 0 0 0 0 0 11 0 Ell F ISIINZWBEEENLWMEMLSIEEEZFMNMZEIUMIJIEIIIIIEIWMIMEGPVSEIIEIELIIAIBAREMW. " 79 • ©® 251 II 0 1 0 SE 0 IN 0 0 0 0 81 M9 =ME -.062 © 0 1 0 0 0 0 0 11 0 0 83 ®® -.062 © o 1 0 1 0 Ill o 0 0 i �, 0 85 g ©� -.062 © 0 1 0 1 0 0 0 A 0 0 87 4IMEI -.062 © 0 1 0 0 0 0 0 0 o 0 ® i- o A'7 . : BEY a MINWAIREa k 89 -©MI -.062 © 0 1 0 1 0 0 0 0 o 0 EXQ ' " & , M 8. n . l k Y ''<<a Iri 9 is _ s .. &: s° i s 91 M10 0= -.915 0 0 1 0 1 0 p II 93 - rill riMI ▪ 915 0 0 • 1 0 1 0 0 0 0 0 0 95 eg- ©® -.915 0 0 1 0 1 0 0 0 0 0 0 97 .. 4 IZEIN ▪ 915 El 0 1 0 1 0 0 0 0 0 0 : c . ; „ is t r r,t s.. 9 v.. x ..11 ® q " ; -,: t x , 99 - ©® -.915 1 0 1 0 1 0 s � F: x 1� �°�s0 � , 0 0 0 0 1 • �l - ��5.® �2<?. �0 a a tMg 2Vddud` mi %1 ?t 'x 6 st fm p 101 M 11 =® ▪ 154 1 0 1 0 1 0 0 0 11 f -E . .. Y k ' Ei `£ - 41 n :. �a. -17 , ." 1 S" 6; � ' Ile Ir �"" s '7 I w i Y� ' -- Y ( a,. °a> 5 . m, n t+Y `n iz l y � t � ,t Q � � . t� 9 �� 4� 1 W f � 103 1 0 2 mal -.154 1 • 0 1 0 1 0 1 0 ,Vit. ee+d+s.,Y.�. .�4:.`av,.o S.K;�,' thi ' .a..34'LLi.s>.a 'j :t,�. 0 M,3tiF;,. a '. ^'r,.0 ?. . 1 mug z .?;: AR: MAWS ,' a... i.�'rM M4 ._,"+Y` M.d... E ', 105 3 max 154 1 0 1 0 1 0 1 0 1 0 1 10 . , },� �.,,t mm nyfgA4:1.. ,2 . = fi` 0 . "iiCM . 14 ,,. . _. ,.T,.> 107 4 max 154 1 0 1 0 1 0 1 0 1 0 1 06 < <., t , =;fi.Y, , . mine .341.....'2 0' f , . 0">. ,f; 1 < :' 0 . > ,1 .!6 u O r. 109 5 max 154 1 0 1 0 1 0 1 0 1 0 1 1140 ri miri .341 2 0, 1, Y 0 :: 1 0 •1 0. 1 > :0` f . 1.. 111 M12 1 max 1.474 2 0 1 0 1 0 1 0 1 0 1 1'12 mm .64.6 :1. 0 ... .1 0 1 i 0 '`'1 'p 1 0 1.,: 113 2 max 1.474.2 0 1- 0 1 0 1 0 1 0 1 RISA -3D Version 6.0.1.5 [H: \Jobs 2006 \0612521Calculations \Truss #3 Analysis.r3d] Page 5 Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 3:24 PM Job Number 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Forces (Continued) u-I • - k Shear I h .. - - - Mitt ; i t -• ERV'k'_itttgiMEFAM 40 re THEIRIZA111KWIIIIMIEEMMITA 1 1 5 - ©rn 1 474 © 0 0 0 0 0 0 0 0 0 0 ®- 4 frn 1.474 © 0 0 0 0 0 0 0 0 o 0 mn wk :AO t,s, .,ffi6 FEMME 0:: WEIRIDIM 0 1 Ci� 0r xs ` 119 - ©= 1.474 © 0 0 0 0 0 0 0 0 0 0 SEMI M13 NEM 1.209 © 0 11111 0 0 0 0 .. � o 0 o 0 r 123 - ©NEO 1.2o9 © 0 0 o Q 0 O o 0 o ETA 1413110615 0 125 - ©max 1 4 © 0 0 0 0 0 _� IFI a : 0 0 0 0 127 4 r 1209 © 0 0 0 • - '�tyz��'^`",�- .b.i3.a x� ®;;.' t . .gs, Ow o `, j•�:'R O * .tc 04 'a T " 0 'w III 129 a t ,I e = ©�209 ���' � � 1 © o 0 3 L 0 0 0 0 0_ 131 M14 1.046 0? a' . -.STM i �v "'l; ic 0 j }a� :i..0 E-04 . a Y3 }; � Y q . ' trx� 0� 1 � ® � r .. © 0 O 0 a , •= x -� „a '� t l `� R S 4 . ° ® n `` ?C ` 7 0 e'.. `• -, "AWL." 0 _a a . i . o ,a€,�; UZI T s. I 0 ' s :::;4 El 133 ©max 1.046 © 0 0 0 UI 0 135 - ®max 1.046 © 0 0 0 0 0 0 D 0 D 0 ® ; af s~f 5 3F F }'i `s- "`a�.�"2a e ,�' "• .°{ 9 - r�-a&�. `'��. E.Ls$ 9pts +�� axe D sr ss' 137 - 4 EIMI 1.046 n 1111 o o o El o 0 yt 0 " a. a ® 4g O ft 4`�0 0 b> 00 „x # t ' y 139 - © max 1.046 © 0 0 0 0 0 7f � . .yS �Y�, b, S * ` ms ; 0 0 ,4 . ® '-- tea $ €, e`a • , u F C ttlY• t 0 r ,a � 0� 9 LTIA Envelope Member Section Deflections Member Sec x [in] Ic y [in] Ic z [in] Ic x Rotate [r... Ic n) Uy Ratio Ic (n) Liz Ratio Ic 1 M1 1 max .095 2 -.019 1 0 1 0 1 NC 1 NC 1 . . si 3 -© max .087 © -.164 NM 0 0 0 0 1655.095 0 NC 0 r�: € . e'z3 ^'x.*! ✓ 1' 9 9 i40.� e K ' .� P w0 � '.21 1 0R 0 . . eL ”" IRMA 5 ©® .079 © 113 I ry 0 0 0 El 9442.102 0 NC 0 R,- 4 07 © -.196 El 0 0 0 to 2751.772 0 NC 0 , 467. � g® 1:6Aa Al 2 ��aa ® Rat: M � � q. f • 9 - ©® .061 © -.17 El 0 0 0 0 NC 0 NC NE '4 ;x emmr1° :0 $ `G1 '� t 38® , ��` S: etriti 9 E` 1. a ct 4. d: tar' ° tt n '` w 0 ® 28 © 119 fi 0 0 0 0 NC 0 NC 0 11 M2 ml 4 r: s c t 0 j_ s s • 13 272 r MIK .261 © -.186 El 0 0 0 0 3497.302 Ui NC 0 v . tYl<m 1 y , X44 1 r .� 9 , 0 �� f o 3,,:. . s I 15 © max .233 © ' 'AEI 0 A E t , : � 4 . ,: 0 0 � 2087 402 0 NC 0 �� 4 . MI .195 © �� 'f ® 2> - .. ' , Di°; ,�, _fix '. ,.,® 0 01 42 0 6 261 111111174•11111 © �, *�ti� �^�� e � " tit � � +v�.� ]'+��x 19 a ©® .148 © 05 ©��.�0 o NI NC ©� Lac v1n fat s � r � A s 'txg � t r %' rF � - � �§..t� r- , ,. 21 11111XMI111111117, 0 0 0 11111111M1M11111 0 NC IKE 22 III P 44's 0 : t • 23 - © ® �� 0�7 '� -.13 �1�, ��ta�,. � �.� g ���� , -, "�, .:� � � ': 0 ,:.., 0 0 0 3• •• 88 O NC 24 ''' F �L�3 ® =.289 0 1 rto " 08 NC IMO 25 ©I .04 © - .21 7 0 o 0 0 MI 2326.363 In NC 0 26 mI ` .017 1 - .489 " 0 1 0 1 1030.77 2. NC 1 RISA - 3D Version 6.0.1.5 [H: \Jobs 2006 \061252 \Calculations \Truss #3 Analysis.r3d] Page 6 Company : BMGP Engineers Inc. Feb 2, 2007 Designer : CTC 3:24 PM Job Number : 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Deflections (Continued) Member e x in Ic in Ic z in Ic x Rotat- r... Ic n U Rati. Ic n U Rati. I ' 27 4 max .094 © -.239 1 0 0 0 0 2110.26 0 NC 0 28 ® min .042 11 -.546 2 0 ® 0 ® 922.385 U NC MI 29 © max .157 © 0 1 0 E 0 0 NC NC 0 30 min .069 0 0 1 0 0 ® NC ® NC Ell 31 M4 0 max 0 0 0 1 0 0 0 0 NC 111 NC 0 32 ® min 0 ® 0 1 0 0 0 ® NC NC 33 © max -.001 0 -.012 1 0 II 0 0 NC H NC 0 34 ®`min -.003 ® -.026 2 0 ® 0 ® 2191.415 NC 35 3 max -.002 1 -.023 1 0 IN 0 0 NC 0 NC 1 36 min -.006 -.052 2' 0 ® 0 ® 1095.707 ® NC 1M 37 4 MIMI -.004 - -035 1 0 0 0 NC 1 NC E 38 ® ®' -.008 -.078 2 0 0 ® 730.472 2 NC 39 © max -.005 0 -.046 1 0 0 0 NC 1 NC 0 40 ®' -.011 ® -.104 2 0 ® 0 ®`547.854' 2 NC MI 41 M5 1 max -093 1 0 1 0 Ell 0 0 NC 0 NC 42 min - 209" ®' 0 1 0 ` 0 ® NC NC 43 2 max - 094 0 -.017 1 0 1 0 0 NC NC 1M 44: ;, ® - .212 ® -.039 2 0 1 0 ®' NC ® NC . 45 © max -.094 0 -.034 1 0 0 0 0 NC 0 NC 0 - 46 ® -.214 ® -.078 2 0 ® 0 1 NC 2 NC 1 47 4 max -.095 -.052 1 0 0 ' 1 NC 1__ NC 1_ 48 ® min ' -.216 ' ` -.117 2 0: U 0 ® NC 2 NC 1 49 5 max -.096 U -.069 1 0 0 0 NC NI NC 50 min -.219 ® -.156 2 0 0 ® NC NC r 51 M6 1 max -.157 Ci - . 006 1 ! 0 1 0 1 NC 0 NC 52 min _ 357 2 -.014 2` 0 1 0 ® NC ®` NC IIM 53 2 max - 156 1 - 024 1 0 1 ' 0 0 6171.656 NC __ 0 54 min -.354 2 -.055 2 7;0 1 0 ® 2727.418 NC 55 i 3 max -.155 1 -.043 1 0 li 0 0 3085.828 1 NC 56 _ min -.352 2 - .097'. 2 0 0 0 1363.709. 2 NC 57 4 maxi - .154 1 -.061 1 0 1 0 1 2057.219 1 NC 58 I 1 min -.349 2 -.138 2 0 1 0 ® 909.139 2 NC 59 5 Imax -.153 1 -.079 1 0 0 0 0 1542.914 U NC U 60 IIII min - .347 2 . -.18 2 0 0 1 681`.855` NC 61 M7 max -.214 1 -.017 1 0 0 _ 1 NC ® NC 62 ® min -.483 2 - .038 2 0 0 ® NC ® NC 63 i 2max - 213 1 -.025 1 0 0 0 1 NC 1M NC 64 min -.482 2 -.058 2 0 ® 0 ® NC E NC 65 3 max -.212 1 -.034 1 0 1 0 0 NC NC U 66 min -.48 2 -.078 2 0 ® 0 ® NC ® NC . 67 I 4 max -.211 1 -.043 1 0 0 0 NC 0 NC HI 68 ®® -.479 2 - .097 2 0 0 ® NC ® NC u�- 69 © -.21 1 -.052 1 0 0 0 0 NC 0 NC U - ` <70 ®® -.477 2 - . 1 1 7 2 0 ® 0 M I N C I M I N C I M 71 M8 0M -. 242 1 -.032 1 0 0 0 0 NC 0 NC E/ 72 73 ® min max - - .242 .548 21 1 -.073 031 2 1 0 0 ® 0 0 ® NC NC ` Ell NC NC II 74 ® min -.547 2 -.071 2 0 0 ANC NC 75 max -.242 1 -.03 1 0 111 0 III NC 111 NC 76 min -.547 2 -.068 2 0 1 0 1 NC NC 1 77 4 max -.241 1 -.029 1 0 1 0 1 NC NC 1 78 min -.546 2 -.066 2 0 1 0 1 NC NC 1 79 5 max -.241 1 -.028 1 0 1 0 1 NC NC 1 80 III min -.545 2 -.064 2 0 0 NC 81 M9 max -.222 1 -.048 1 0 ® 0 111 NC ® NC NC 82 III min .502 2 -.11 2 0 II 0 111 NC IN NC IIII 83 max -.222 1 -.041 1 0 0 NC NC RISA -3D Version 6.0.1.5 [H: \Jobs 2006 \061252 \Calculations \Truss #3 Analysis.r3d] Page 7 9 Company : BMGP Engineers Inc. Feb 2, 2007 Designer : CTC 3:24 PM Job Number : 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Deflections (Continued) Member Sec x [inl Ic v [in] Ic z [in[ Ic x Rotate [r... Ic (n) Uy Ratio Ic (n) Liz Ratio Ic • 84 min -.502 2 -.093 2 0 1 0 1 NC 2 NC 1 85 3 max -.222 1 -.034 1 0 1 0 1 NC 1 NC 1 86 min -:502 2 -.076 2 0 1 0 1 NC 2 NC 1 87 4 max -.222 1 -.026 1 0 1 0 1 NC 1 NC 1 88 min -.502 2 -.06 2 0 1 I 0 1 NC 2 NC 1 89 5 max -.222 1 -.019 1 0 1 0 1 NC 1 NC 1 90 min -:502 2 -.043 2 0 1, 0 1 NC 2 NC 1 91 M10 1 max .093 2 .048 2 0 1 0 1 NC 2 NC 1 92 min .041 1 .021 1 0 1 0 1 NC 1 NC 1 93 2 max .099 2' -.003 1 0 1 0 1 NC 1 NC 1 94 min., ,044_ 1 -.008 2 0 1 0 1 1866:563 '2 NC 1 95 3 max .104 2 -.028 1 0 1 0 1 NC 1 NC 1 , .96 min. .046 1 .064'` 2 _ 0 1 0 1 933.282 2 NC 1 97 4 max .109 2 -.053 1 0 1 1 0 1 NC 1 NC 1 l9$r< " min .048 1 -.119 2 0 1 .1 0 1 622.183 2 NC =1i 99 5 max .115 2 -.077 1 0 1 0 1 NC 1 NC 1 :1fc4:6K k; , ,. : ;'min __051 1 _175. 2' 0 1.< i' 0 _ 1 466.641 2 N 04,16 iltli 101 M11 1 maxi .266 2_ 1 0 1 I 0 1 NC 1 NC 1 XMETEEMNLIMT' in' 1 17_ 1 -.036 2 0 1 0 1 NC 2 NC 1 103 2 max .267 2 -.037 1 0 1, 0 1 NC 1 NC _ - 1 IdiVitr'. #. 118 1 : 085 2 0 1 0 1 NC 2 NC 1 105 3 max .268 2 -.059 1 _ - __ - 0 1 0 1 NC 1 NC 1 106` , O !Rh .118 ,i,1 _,i. -.135 2 0 1 0 1 NC _ 2 NC ,_ 1 107 4 max .269 2 -.081 1 0 1 1 0 1 NC 1 NC 1 108 _ min .119 1 -,184 2 __ 0 1 1 0 1 NC 2 NC 1_ 109 5 max .27 2 - .103 1 0 1 0 1 NC 1 NC 1 <110 min .119 1 -:234 2 1 0 1 0 1 NC 2. NC 1 111 M12 1 max -.111 1 -.112 1 0 1 I 0 1 NC `1 NC 1 112 min -.251 2 -.254 2 0 1 0 1 NC 2 NC , 1 113 2 max -.113 1 -.129 1 0 1 0 1 6789.865 1 NC 1 114 min -.255 .2 -.293 .2. 0 1 0 1 NC 2 NC 1 115 1 3 max -.115 1 -.147 1 0 1 0 1 3394.933 1 NC 1 116 min -.26 2 -.333 2 0 1 0 1 NC 2 NC 1 117 4 max 116 1 - -164 1 0 1 0 ' 1 2263.288 1 NC 1 118 min - .264 2 -.372 2 0 1 0 . 1:.. • ";: 2 NC 1 119 5 max -.118 1 -.181 1 0 1 0 1 1697.466 1 NC 1 120 min -.268 2 -.411 2 0 1 0 1 NC 1 2 NC 1 121 M13 1 max -.103 1 -.188 1 0 1 0 1 _ NC 1 - -NC 1 122 min -.233 2 -.425 2 0 1 0 1 NC ' 2 NC 1 123 2 max -.104 1 -.195 1 0 1 0 1 NC 1 NC 1 124 min .236.: , ,:.2 -.442 2 0 1 0 1 6301.562 2 NC 1 125 3 max -.106 1 -.202 1 0 1 0 1 NC 1 NC 1 126 min -.239 2 -.458 2 0 1 0 1 3150:781 2 NC 1 . 127 4 'max -.107 1 -.21 1 0 1 0 1 NC 1 NC 1 128 min -.242 2 -.475 ' 2 0 1 0 1 2100.521 2 NC 1 129 5 max -.109 1 -.217 1 0 1 0 1 NC 1 NC 1 , 130 min -.246 2 -.491 2 0 1 0 1 1575:391 2 NC 1 131 M14 1 max -.068 1 -.235 1 0 1 0 1 NC 1 NC 1 132 min -.153 2 -.531 2 0 1 0 1 1494.699 2 NC 1 133 2 max -.069 1 -.229 1 0 1 0 1 NC 1 NC 1 134 min -.155 2 -.518 2 0 1 0 1 1992.931 2 NC 1 135 3 max -.069 1 -.223 1 0 1 0 1 NC 1 NC 1 136 min -.157 2 -.504 2 0 1 0 1 2989.397 2 NC ' 1 137 4 max -.07 1 -.217 1 0 1 0 1 NC 1 NC 1 138 min -.159 2 -.491 2 0 1 0 1 5978.794 2 NC 1 139 5 max -.071 1 -.211 1 0 1 0 1 NC 1 NC 1 140 min -.161 2 -.477 2 0 1 0 1 NC 2 NC 1 RISA -3D Version 6.0.1.5 [H:\Jobs 200610612521Calculations\Truss #3 Analysis.r3d] Page 8 Company : BMGP Engineers Inc. Feb 2, 2007 Designer : CTC 3:24 PM Job Number : 061252 Canterbury Truss Analysis Checked By: Envelope Wood Code Checks Memb... Shape Code Check Loc... Ic She... Lo...... Ic Fc' [... Ft' [k..Fb1'...Fb2'...Fv' [... Eon 1 M1 2X4 1.537 7.664 2 1.041 7.5..,y 2 .856 1.5 2.587 2.846 .095 3.9 -3 2 M2 2X4 6.347 26:.':: 2 11098 21... y 2 .962 1.5 2.587,2.846 ,095 3.9 -3 • 3 M3 2X4 .756 -. _ 38.... 2 .128 34... v . 1 .856 1.5 2.587 2.846_ .095 3.9 -1 .4 M4 2X4 .263 0 2 .000 0 z 1 1.413 1.5 2.587 2.846 .095 3:6:3 5 M5 2X4 __ .306 0 2 .000 0 z 1 .66 1.5 2.587 2.846 .095 3.6.3 6 M6 2X4 .113 0 2 :000 0 z '1 .377 1.5 2.587 2.846 .095 3.9 -1 7 M7 _ 2X4 .093 0 2 .000 0 z 1 .66 1.5 2.587 2.846 .095 3.9 - 8 M8 2X4 .062 0 2 .000 0 z 1 :377 1.5 2.587 2.846 .095 3.9 -1 9 M9 2X4 .009 0 1 .000 0 z 1 1.011 1.5 2.587 2.846 .095 3.9 - 10 . M10 2X4 .264 0 2 _000: 0 z 1 `448 1.5 2.587 2.846 .095 3.9 -1 11 M11 2X4 .043 0 2 .000 0 z 1 .342. 1.5 2 - 587 2.846 .095 3.9 - .4 M12 2X4 .821 0 2 ,000 " 0 z '1 :342 1.5' 2.587 2.846 .095 3.6.3 13 M13 2X4 .514 0 2 .000 0 z 1 .448 1.5 2.587 2.846 .095 3.6.3 14 M14 2X4 .302 0 2 .000 0 z 1 .66 1.5 2.587 2.846 .095 3.6.3 RISA -3D Version 6.0.1.5 [H:1Jobs 200610612521Calculations\Truss #3 Analysis.r3d] Page 9 2, )r Y � X • m M2 QQ o J ,114 2 3 c ig5 A ' 15 6 '7 Solution: Envelope BMGP Engineers Inc. Canterbury Truss Analysis CTC i.✓4� L) r � � Feb 2, 2007 at 3:35 PM 061252 / Truss #3 Analysis with New Bearin... Y Z X • _4 Solution: Envelope BMGP Engineers Inc. _ Canterbury Truss Analysis CTC Feb 2, 2007 at 3:35 PM 061252 Truss #3 Analysis with New Bea Ys nn... 12 t 13 Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 3:36 PM Job Number 061252 Canterbury Truss Analysis Checked By: Global Display Sections for Member Calcs 5 . Max Internal Sections for Member Calcs 97 Include Shear Deformation Yes Include Warping Yes . Area Load Mesh (inA2) 144 Merge Tolerance (in) .5 P -Delta Analysis Tolerance 0.50% Vertical Axis Y Hot Rolled Steel Code AISC: ASD 9th . Cold Formed Steel Code AISI 99: ASD Wood Code NDS 91/97: ASD — Wood Temperature < 100F Concrete Code ACI 2002 Number of Shear Regions 4 Region Spacing Increment (in) 4 Biaxial Column Method PCA Load Contour Parme Beta Factor (PCA) .65 Concrete Stress Block Rectangular Use Cracked Sections Yes Bad Framing Warnings No Unused Force Warnings Yes Wood Material Properties Label Species Grade Cm Emod Nu Therm...Densjk/f... 1 DF Larch Douglas Fir -Larch Select Structural 1 .3 .3 .035 2 So Pine Southern Pine No.1 1 .3 .3 .035 Wood Section Sets Label Shape Type Design List Material Design Rules A fin21 Ivy [in4] lzz [in4] J [in4] 1 WOOD1A 2X4 Beam Rectangular DF Larch Typical 5.25 .984 5.359 2.877 Member Primary Data Label I Joint J Joint K Joint Rotate(deg) Section /Shape Type Design List Material Design Ru... 1 M1 N8 N10 WOOD1A Beam Rectangular DF Larch Typical 2 M2 N10 N7 WOOD1A Beam Rectangular DF Larch Typical 3 M3 N1 N7 WOOD1A Beam Rectangular DF Larch Typical 4 M4 N1 N8 WOOD1A Beam Rectangular DF Larch Typical 5 M5 N2 N9 WOOD1A Beam Rectangular DF Larch Typical • 6 M6 N3 N10 WOOD1A Beam Rectangular DF Larch Typical 7 M7 N4 N11 WOOD1A Beam Rectangular DF Larch Typical 8 M8 N5 N12 WOOD1A Beam Rectangular DF Larch Typical . 9 M9 N6 N13 WOOD1A Beam Rectangular DF Larch Typical 10 M10 N8 N2 WOOD1A Beam Rectangular DF Larch Typical 11 M11 N9 N3 WOOD1A Beam _Rectangular DF Larch Typical 12 M12 N3 N11 WOOD1A Beam Rectangular DF Larch Typical 13 M13 N4 N12 WOOD1A Beam Rectangular DF Larch Typical 14 M15 N15 N16 WOOD1A Beam Rectangular DF Larch Typical 15 M15A N17 N15 WOOD1A Beam Rectangular DF Larch Typical 16 MI6 N15 N13 WOOD1A Beam ,Rectangular DF Larch Typical RISA -3D Version 6.0.1.5 [HAJobs 200610612521Calculations\Truss #3 Analysis with New Bearing.r3d] Page ' Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 3:36 PM Job Number 061252 Canterbury Truss Analysis Checked By: Joint Coordinates and Temperatures Label X [ftl Y [ftl Z fftl Temp FF1 Detach From Diao... 1 N1 0 0 0 0 2 N2 7.25 0 0 0 3 N3 13.96 _ 0 0 0 _ - • 4 N4 20.6667 0 0 0 5 N5 _ 27.91667 0 _ 0 0 _ 6 N6 34.08333 0 0 J 0 1 7 _ N7 . 42 0 0 0 8 N8 0 4.75 0 _ 0 9 N9 7.25 7.1667 0 0 10 N10 13.96 9.403 0 0 1 11 N11 20.6667 7.1667 0 0 12 N12 27.917 4.75 0 0 13 N13 34.08333 2.6944 0 0 14 N14 0 0 0 0 15 N15 31.5 0 0 0 16 N16 31.5 3.5 0 0 17 N17 27.98 I 4.7015 0 0 Joint Boundary Conditions Joint Label X [k/in] Y [k/in] _ Z [din] X Rot.[k- ft/rad] Y Rot.[k- ft/rad] Z Rot.[k- ft/rad] Footing __ 1 N1 Reaction Reaction Reaction 2 N7 Reaction _ 3 N10 Fixed 4 N12 Fixed 5 N15 Reaction Reaction Reaction Wood Design Parameters Label Shape Length... le2[ft] le1[ft] le -bend too[ft] _ le -bend bot[ft] Kyy Kzz CH Cr y sway z sway 1 M1 WOOD1A 14.715 1 6.5 Yes 2 M2 WOOD1A 29.575 1 6.5 1 1 Yes 3 M3 WOOD1A 42 1 7 Yes 4 M4 WOODIA 4.75 1 Yes 5 M5 WOOD1A 7.167 3.5 Yes 6 , M6 WOOD1A 9.403 4.75 Yes 7 M7 7.167 3.5 Yes 8 M8 WOODIA 4,75 Yes 9 M9 WOOD1A 2.B94 Yes 10 M10 WOOD1A 8.667 4.33 Yes 11 M11 WOOD1A 9.818 5 _ Yes 12 M12 wooD1A 9.815 5 Yes ' 13 M13 WOOD1A 8.668 4.33 Yes 14 M15 WOOD1A 3.5 15 M15A WOOD1A 5.873 3 - 16 M16 woOD1A 3.733 Member Distributed Loads (BLC 1 : Dead Load) Member Label Start Magnitude[k/ft.d..End Magnitudejk/ft.d... Start Location[ft, %1 End Location[ft. %] 1 M1 Y _ -.03 -.03 0 _ 0 _ 2 M2 Y -.03 -.03 0 0 3 M3 Y _ -.01 -.01 0 0 RISA -3D Version 6.0.1.5 [H:1Jobs 20061061252 \Calculations \Truss #3 Analysis with New Bearing.r3d] Page 2 Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 3:36 PM Job Number 061252 Canterbury Truss Analysis Checked By: Member Distributed Loads (BLC 2 : Snow Load) Member Label Direction Start Magnitude[k/ft.d.,End Magnitude[k/ft.d... Start Location[ft. %] End Location[ft. %] 1 M -.05 -.05 -.05 0 0 4 -.05 - .;.���.„ 4 w. 4t-1:4,4!:•14`4, r "1 ° g ,. ` Basic Load Cases BLC Description Category X Gravi Y Gravi Z Gravity Joint Point Distribu...Area (M..Surface... 1 Dead Load DL 2 Snow Load T _= SL ;6,f, ,�'41.x4 , k Load Combinations Description Solve PDelta SRSS BLC Fact...BLC Fact...BLC Fact...BLC Fact...BLC Fact...BLC Fact...BLC Fact...BLC Fact... 1 Dead Load Yes DL 1 « +Sno =g DL i i1 . = 5I ' 1 Envelope Joint Displacements Joint X [in] Ic Y [in] Ic Z jin] Ic X Rotation ... Ic Y Rotation ... Ic Z Rotation [... Ic 1 N1 max 0 1 0 1 0 1 0 1 0 1 - 1.64e -3 1 2 min 0 2 0 2 0 1 0 1 0 1 -2.021e-3 ' 2 3 N2 max -.003 1 -.023 1 0 1 0 1 0 1 2.311 e -4 1 4 min -.007 2 -.052 2 0 . 1 0 .; 1 0 1 7.104e -6 2 5 N3 max -.002 1 -.031 1 0 1 0 1 0 1 - 9.52e -5 1 6 min -.004 2 -.07 2 0 1 0 1 0 1 1.257e -4 2 7 N4 max 0 2 -.029 1 0 1 0 1 0 1 1.912e -5 2 8 min 0 1 065= 2 0 1 0 1 0 1 -6.527e-5 1 9 N5 max 0 2 - .014 1 0 1 0 1 0 1 1.111e -3 2 10 min 0 1 -.03 2 0 1 0 1 0 1 6.462e -4 1.i 11 N6 max 0 2 -.003 1 0 _ 1 0 1 0 1 -7.002e-4 1 12 min 0 1 -.006 2 0 1 0 1 0 1 - 8.34e -4 2 N7 max .001 2 0 1 0 1 0 1 0 1 1.969e -3 2 14 min 0 1 0 2 0 1 0 1 0 1 1.856e -3 1 15 N8 max .004 2 -.003 1 0 1 0 1 0 1 - 4.3e -3 1 16 min .002 1 -.008 2 0 1 0 1 0 1 -1.135e 2, 17 N9 max .009 2 -.025 1 0 1 0 1 0 1 1.082e -3 2 18 min !:004 1 -.058 2 ''',4----17715-1 0 1 0 1 3.888e-4 l 19 N10 max 0 2 -.029 1 0 1 0 1 0 1 -3.176e-3 1 20 min 0 1 -.066 2 0 1 0 1 0 1 -8.458e-3 2 N11 max -.005 1 -.03 1 0 1 0 1 0 1 8.447e-4 2 22 min -.011 2 -.068 42 ' .::0,. 1 0 ° ` `;'9 .. ' 1 3.01e-4 k ` 23 N12 max -.006 1 -.013 1 0 1 0 1 0 1 3.644e -3 2 min -.012 2 -.03 1 0 taM. 1.48: e- 3 25 N13 max 0 2 -.002 1 0 1 0 1 0 1 -2.099e-3 1 min 1 4:005 . `; , 1 0 ... 1 , -5.5 .q`; 3.. r 27 N14 max 0 1 0 1 0 1 0 1 0 1 0 1 ,$t. $ "� s` ' •'s ; ,:. �} i" .y 0 :. 3 SIV$::; 29 N 15 max 0 0 1 0 1 0 1 0 1 2.297e - 2 30 ml 7 ��. 0 1 �� � �1 .1.597e ' 71 4 V- 31 N16 max 0 2 0 2 0 1 IIIIMMINE 0 1 2 32 z T .. ., mite; _6'11'1 , ": t l:? t ;,. s §c k'� x <: t 1 ' 3 N 7 m r' 112 1 I 1 0 1 gg , �� 2 § .4calf a > � s < � p+`• • �"E,_' � ; u"'x L+, , ' `.- -k: ..` 0 1 (i d .;'� .. 1.36 :+" �_ r RISA -3D Version 6.0.1.5 [H: \Jobs 2006\061252\Calculations \Truss #3 Analysis with New Bearing.r3d] Page 3 r' ' Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 3:36 PM Job Number 061252 Canterbury Truss Analysis Checked By: Envelope Joint Reactions Joint X [kJ Ic Y [k] Ic Z jk] Ic MX jk -ft) Ic MY [k -ft] Ic MZ 1k-ft] Ic 1 N1 max .798 2 1.431 2 0 1 0 1 0 1 0 1 2 min .351 1 .631 1 0 1 0 1 0 1 0 1 • 3 N7 max 0 1 .329 2 0 1 0 1 0 1 0 1 4 min 0 1 .144 1 0 1 0 1 0 1 0 1 5 N15 max -.351 1 2.204 2 0 1 0 1 0 1 0 1 6 min -.798 2 .974 1 0 1 0 1 0 1 0 1 7 Totals: max 0 1 3.963 2 0 1 8 min 0 2 1.749 1 0 1 Envelope Member Section Forces Member Sec Axial k Ic Shear k Ic z Shear k Ic Torquefk -... Ic v -v Mome... Ic z -z Moment[k -ft] Ic M1 Il lmax 1.317 .223 0 0 1 0 1 0 1 min .575 .084 0 0 1 0 1 0 1 max 1.224 -.021 0 0 1 0 1 -.116 1 4 min .541 -.056 0 0 0 -.308 2 5 3 max 1.131 -.126 0 0 0 .41 21 6 min .506 -.335 0 0 0 153 1 7 4 max 1.239 .083 0 0 0 -.079 1 8 min .547 .031 0 0 0 -.209 2 9 5 max 1.146 -.074 0 0 0 0 1 10 min .512 -.196 0 0 0 0 1 11 M2 1 max 1.144 .205 0 0 0 0 1 12 min .511 .077 0 0 0 0 1 13 2 max 1.363 .292 0 0 0 .347 2 14 min 606 . 11 0 0 0 13 1 15 3 max 1.085 -.425 0 0 0 .31 2 16 min .482 -.927 0 0 0 .12 1 17 4 max -.003 .306 0 0 0 .19 2 18 min -.016 .115 0 0 0 .071 1 19 5 max .173 -.095 0 0 0 0 1 20 min .067 -.255 0 0 0 -.001 2 21 1 max .798 .03 0 0 0 0 1 22 111 min .351 0 .029 1 0 0 0 I 0 0 0 1 23 max -.168 .004 0 0 0 -.015 1 24 min -.381 .004 0 0 0 -.017 2 25 max .065 .036 0 0 0 .031 1 26 min .029 .035 i 0 i 0 i 0 11 .03 2 27 4 max -.034 -.012 0 0 0 .033 2 2 8 min -.083 -.02 0 0 0 .01 1 29 5 max -.034 -.032 0 0 0 0 1 3 0 min 083 033 0 0 1 0 1 0 1 . 31 M4 1 max 1 0 0 0 1 0 1 0 1 32 min .602 0 0 0 1 0 1 0 1 33 2 max 1.401 0 0 0 1 0 1 0 1 34 min .602 0 0 0 1 0 1 0 1 35 3 max 1.401 0 0 0 1 0 1 0 1 36 min .602 0 0 0 1 0 1 0 1 37 4 max 1.401 0 0 0 1 0 1 0 1 38 min .602 0 0 0 1 0 1 0 1 39 5 max 1.401 0 0 0 1 0 1 0 1 40 min .602 0 0 0 1 0 1 0 1 41 M5 1 max .693 0 0 0 1 0 1 0 1 42 min .26 0 0 0 1 0 1 0 1 43 2 max .693 0 0 0 1 0 1 0 1 44 min .26 1 0 1 0 1 0 1 0 1 0 1 RISA -3D Version 6.0.1.5 [H:1Jobs 200610612521Calculations\Truss #3 Analysis with New Bearing.r3d] Page 4 ' Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 3:36 PM Job Number 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Forces (Continued) Member Sec Axial [k] Ic y Shear[k] Ic z Shear k] Ic Torque[k -... Ic y -y Mome... Ic z -z Moment[k -ft] Ic 45 3 max .693 2 0 1 0 1 0 1 0 1 0 1 46 min .26 1 0 1 0 1 0 1 0 1 0 1 47 4 max .693 2 0 1 0 1 0 1 0 1 0 1 48 min .26 1 0 1 0 1 0 1 0 1 0 1 49 5 max .693 2 0 1 0 1 0 1 0 1 0 1 50 min .26 1 0 1 0 1 0 1 0 1 0 1 51 M6 1 max -.181 1 0 1 0 1 0 1 0 1 0 _ 1 52 min -.345 2 0 1 0 1 0 1 0 1 0 1 53 2 max -.181 1 0 1 0 1 0 1 0 1 0 1 54 min -.345 2 0 1 0 1 0 1 0 1 0 1 55 3 max -.181 1 0 1 0 1 0 1 0 1 0 1 56 min -.345 2 0 1 0 1 0 1 0 1 0 1 57 4 max -.181 1 0 1 0 1 0 1 0 1 0 1 58 min -.345 2 0 1 0 1 0 1 0 1 0 1 59 5 max -.181 1 0 1 0 1 0 1 0 1 0 1 60 min -.345 2 0 1 0 1 0 1 0 1 0 1 61 M7 1 max .353 2 0 1 0 1 0 1 0 1 0 1 62 min .115 1 0 1 0 1 0 1 0 1 0 1 63 2 max .353 2 0 1 0 1 0 1 0 1 0 1 64 min .115 1 0 1 0 1 0 1 0 1 0 1 65 3 max .353 2 0 1. 0 _ 1 0 1 0 1 0 1 66 min .115 1 0 1 0 1 0 1 0 1 0 1 67 4 max .353 2 0 1 0 1 0 1 0 1 0 1 68 min .115 1 0 1 0 1 0 1 0 1 0 1 69 5 max .353 2 0 1 0 1 0 1 0 1 0 1 70 min .115 1 0 1 0 1 0 1 0 1 0 1 71 M8 1 max -.049 2 0 1 0 1 0 1 0 1 0 1 72 min -.058 1 0 , 1 0 1 0 1 0 1 0 1 73 _ 2 max -.049 2 0 1 0 1 0 1 0 1 0 1 74 _ min -.058 1 0 1 0 1 0 _ 1 0 1 0 1 75 3 max -.049 2 0 1 0 1 0 1 0 1 0 1 76 min -.058 1 0 1 0 1 0 1 0 1 0 1 77 4 max -.049 2 0 1 0 1 0 1 0 1 0 1 78 min -.058 1 0 1 0 1 0 1 0 1 0 1 79 5 max -.049 2 0 1 0 1 0 1 0 1 0 1 80 min -.058 1 0 1 0 1 0 1 0 1 0 1 81 M9 1 max -.075 2 0 1 0 1 0 1 0 1 0 1 82 min -.083 1 0 1 0 1 0 1 0 1 0 1 83 2 max -.075 2 0 1 0 1 0 1 0 1 0 1 84 min -.083 1 0 1 0 1 0 1 0 1 0 1 85 3 max -.075 2 0 1 0 1 0 1 0 1 0 1 86 min -.083 1 0 1 0 1 0 1 0 1 0 1 87 4 max -.075 2 0 1 0 1 0 1 0 1 0 1 88 min -.083 1 0 1 0 1 0 1 0 1 0 1 - 89 5 max -.075 2 0 1 0 1 0 1 0 1 0 1 90 min -.083 1 0 1 0 1 0 1 0 1 0 1 91 M10 1 max, -.621 1 0 1 0 1 0 1 0 1 0 1 • 92 min -1.41 2 0 1 0 1 0 1 0 1 0 1 93 2 max -.621 1 0 1 0 1 0 1 0 1 0 1 _ 94 min_ -1.41 2 0 1 0 1 0 1 0 1 0 1 95 3 max -.621 1 0 1 0 1 0 1 0 1 0 1 96 min -1.41 2 0 1 0 1 0 1 0 1 0 1 9 4 max -.621 1 0 1 0 1 0 1 0 1 0 1 . 98 min -1.41 2 0 1 0 1 0 I1 0 1 0 1 99 5 max -.621 1 0 1 0 1 0 1 0 1 0 1 .100 min -1.41 2 0 1 0 1 0 1 0 1 0 1 101 M11 1 max .043 2 0 1 0 1 0 1 0 1, 0 1 RISA -3D Version 6.0.1.5 [H:\Jobs 200610612521Calculations\Truss #3 Analysis with New Bearing.r3d] Page 5 R , 1 , ( • Cbmpany BMGP Engineers Inc. Feb 2, 2007 Designer CTC 3:36 PM Job Number 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Forces (Continued) Member Sec Axialfkl Ic v Shearfkl Ic z Shearfkl Ic Torauefk -... Ic v -v Mome... Ic z -z Momentfk -ftl Ic 102 min .016 1 0 1 0 1 0 1 0 1 0 1 103 2 max .043 2 0 1 0 1 0 1 0 1 0 1 104 min .016 1 0 1 0 1 0 1 0 1 0 1 105 3 max .043 2 0 1 0 1 0 1 0 1 0 1 • 106 min .016 1 0 1 0 1 0 1 0 1 0 1 107 4 max .043 2 0 1 0 1 0 1 0 1 0 1 108 min .016 1 0 1 0 1 0 1 0 1 0 1 109 5 max .043 2 0 1 0 1 0 1 0 1 0 1 110 min .016 1 0 1 0 1 0 1 0 1 0 1 111 M12 1 max .345 2 0 1 0 1 0 1 0 1 0 1 112 min .148 1 0 1 0 1 0 1 0 1 0 1 113 2 max .345 2 0 1 0 1 0 1 0 1 0 1 114 min .148 1 0 1 0 1 0 1 0 1 0 1 115 3 max .345 2 0 1 0 1 0 1 0 1 0 1 116 min .148 1 0 1 0 1 0 1 0 1 0 1 117 4 max .345 2 0 1 0 1 0 1 0 1 0 1 118 min .148 1 0 1 0 1 0 1 0 1 0 1 119 5 max .345 2 0 1 0 1 0 1 0 1 0 1 120 min .148 1 0 1 0 1 0 1 0 1 0 1 121 M13 1 max -.344 1 0 1 0 1 0 1 0 1 0 1 122 min -.779 2 0 1 0 1 0 1 0 1 0 1 123 2 max -.344 1 0 1 0 1 0 1 0 1 0 _ 1 124 min -.779 2 0 1 0 1 0 1 0 1 0 1 125 3 max -.344 1 0 1 0 1 0 1 0 1 0 1 126 min -.779 2 0 1 0 1 0 1 0 1 0 1 127 4 max -.344 1 0 1 0 1 0 1 0 1 0 1 128 min -.779 2 0 1 0 1 0 1 0 1 0 1 129 5 max -.344 1 0 1 0 1 0 1 0 1 0 1 130 min -.779 2 0 1 0 1 0 1 0 1 0 1 131 M15 1 max -.03 1 0 1 0 1 0 1 0 1 0 1 132 min -.079 2 0 1 0 1 0 1 0 1 0 1 133 2 max -.03 1 0 1 0 1 0 1 0 1 0 1 134 min -.079 2 0 1 0 1 0 1 0 1 0 1 135 3 max -.03 1 0 1 0 1 0 1 0 1 0 1 136 min -.079 2 0 1 0 1 0 1 0 1 0 1 137 4 max -.03 1 0 1 0 1 0 1 0 1 0 1 138 min -.079 2 0 1 0 1 0 1 0 1 0 1 139 5 max -.03 1 0 1 0 1 0 1 0 1 0 1 140 min -.079 2 0 1 0 1 0 1 0 1 0 1 141 M15A 1 max 2.06 2 0 1 0 1 0 1 0 1 0 1 142 min .91 1 0 1 0 1 0 1 0 1 0 1 143 2 max 2.06 2 0 1 0 1 0 1 0 , 1 0 1 144 min .91 1 0 1 0 1 0 1 0 1 0 1 145 3 max 2.06 2 0 1 0 1 0 1 0 1 0 1 - 146 min .91 1 0 1 0 1 0 1 0 1 0 1 147 4 max 2.06 2 0 1 0 1 0 1 0 1 0 1 148 min .91 1 0 1 0 1 0 1 0 1 0 1 • 149 5 max 2.06 2 0 1 0 1 0 1 0 1 0 1 150 min .91 1 0 1 0 1 0 1 0 1 0 1 151 I M16 1 max .848 2 .005 2 0 1 0 1 0 1 .018 2 152 min .375 1 .003 1 0 1 0 1 0 1 .011 1 153 2 max .848 2 .005 2 0 1 0 1 0 1 .013 2 154 min .375 1 .003 1 0 1 0 1 0 1 .008 1 155 3 max .848 2 .005 2 0 1 0 1 0 1 .009 2 156 min .375 1 .003 1 0 1 0 1 0 1 .005 1 157 4 max .848 2 .005 2 0 1 0 1 0 1 .004 2 158 min .375 1 .003 1 0 1 0 1 0 1 .003 1 RISA -3D Version 6.0.1.5 [H: \Jobs 2006 \061252 \Calculations \Truss #3 Analysis with New Bearing.r3d] Page 6 • Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 3:36 PM Job Number 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Forces (Continued) Member Sec Axial[k] Ic y Shearlk] Ic z Shear[k] Ic Torque[k -... Ic y -y Mome... Ic z -z Moment[k -ft] Ic 159 5 max .848 2 .005 2 0 1 0 1 0 1 0 1 . 160 ir> <.37<< 1 .003b4i 4. = 0 1 0 1 0 1 0 1 - Envelope Member Section Deflections Member Sec x [in] Ic y [in] Ic z [in] Ic x Rotate [r... Ic (n) lJy Ratio Ic (n) Uz Ratio Ic 1 M1 1 max .002 2 -.004 1 0 1 0 1 NC 1 NC 1 tftWhi *,z ern 0 1 1 ' =, 2 0 1 0 .... NC 2 NC 1 3 2 max -.001 1 -.112 1 0 1 0 1 1724.243 1 NC 1 1' 4 VW *- min -.004 2 -.293 2 0 1 0 1 652.739 2 NC 1 5 3 max -.004 1 -.028 1 0 1 0 1 NC 1 NC 1 6 min -.009 2 -.065 2 0 1 0 1 6022.049 2 NC 1 7 4 max -.006 1 -.081 1 0 1 0 1 2952.868 1 NC 1 8 min - .015 2 -.205 2 0 1 0 1 1125.876 2 NC 1 9 5 max - .009 1 -.027 1 0 1 0 1 NC 1 NC 1 10 min - .02 2 - .063 2 0 1 0 1 NC 2 NC 1 11 M2 1 max .022 2 -.027 1 0 1 0 1 NC 1 NC 1 12 min' .009 1 .062 2 0 1 0 1 5769.945 2 NC 1 13 2 max .011 2 -.03 1 0 1 0 1 NC 1 NC 1 14 min .005 1 -.069 2 0 1 0 ' 1 5202.464 2 NC 1 15 3 max -.001 1 -.013 1 0 1 0 1 NC 1 NC 1 16 min - .002 2 -.029 2 0 1 0 1 NC 2 NC 1` 17 _.. -_ 4 max .002 2 -.038 1 0 1 0 1 9305.19 1 NC 1 18 min 0 --. 1 -.101 2 0 1 . ,. 0 1 3527.117 2 NC 1 19 5 max 0 2 0 1 0 1 0 1 NC 1 NC 1 20 min' 0 1 0 2 0 1 0 1 NC 2 NC 1 21 M3 1 max 0 1 0 1 0 1 0 1 NC 1 NC 1 x, 22- min 0 1 0 1 0 1 0 1 NC 1 NC 1 23 2 max -.002 1 -.032 1 0 1 0 1 NC 1 NC 1 24 min -.005 2 -.068 2 0 1 0 1 7379.651 2 NC 1 25 3 max 0 2 -.03 1 0 1 0 1 NC 1 NC 1 26 min" 0 1 - .066 2 0 1 0 1 7674.899 2 NC 1 27 4 max 0 1 0 1 0 1 0 1 NC 1 NC 1 '2 8.. min 0 1 0 1 0 1 0 1 NC 1 NC 1 29 5 max .001 2 0 1 0 1 0 1 NC 1 NC 1 30 min 0 1 0 1 0 1 0 1 NC 1 NC 1 31 M4 1 max 0 1 0 1 0 1 0 1 NC 1 NC 1 r32 ,., ,:; min ,�,.;.0 1 0 1 0 1 0 1 NC - s, NC 1 33 2 max 0 1 0 1 0 1 0 1 NC 1 NC 1 34 min -.002 2 -.001 2 0 1 0 1 NC 2 NC 1 35 3 max -.002 1 -.001 1 0 1 0 1 NC 1 NC 1 36 A min -.004 2 -.002 ' 2 0 1 0 . .. 1 NC 2 . e .. .NC 1 37 4 max -.003 1 -.002 1, 0 1 0 1 NC 1 NC 1 min -.006 2 -:003 2 0 1 0 1 NC 2 NC 1 39 5 max -.003 1 -.002 1 0 1 0 1 NC 1 NC 1 40 min -.008 2 -.004 > '2 0 1 0 1 NC 2 NC 1 41 M5 1 max -.023 1 .007 2 0 1 0 1 NC 2 NC 1 42 Vim:.:. ` . . = ..'min $ :: .052E, 1/4 .003 ' t V't 1 0 , . 1 NC 1 NC ,x. 43 2 max -.024 1 .003 2 0 1 0 1 NC 2 NC 1 44 min -.054 2 .001 1 0 1 0 y =' 1 NC 1 NC 14 45 3 max -.024 1 0 1 0 1 0 1 NC 1 NC 1 u 46 1 min -1%61 2 .001 ' 2 0 1 0 1 ' WNC 2 . NC 1 L,: 47 4 max -.025 1 -.002 1 0 1 0 1 NC 1 NC 1 4t 4 ,,, min -.057 2 .005 2 0 1 0 1 NC B` NC 1' ,, 49 5 max -.025 1 -.004 1 0 1 0 1 NC 1 NC 1 4.50 &, nun -.058 2 -.009 2 0 1 0 1 NC 2 NC 1 51 M6 1 max -.031 1 .004 2 0 1 0 1 NC 2 NC 1 RISA -3D Version 6.0.1.5 [H: \Jobs 2006 \061252 \Calculations \Truss #3 Analysis with New Bearing.r3d] Page 7 2, 2a Company : BMGP Engineers Inc. Feb 2, 2007 Designer : CTC 3:36 PM Job Number : 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Deflections (Continued) Member Sec x fin] Ic v finl Ic z fin] Ic x Rotate fr... Ic n) Uv Ratio Ic n) Liz Ratio Ic 52 min -.07 2 .002 1 0 1 0 1 NC 1 NC 1 53 2 max -.03 1 .003 2 0 1 0 1 NC 2 NC 1 54 min -.069 2 .001 1 0 1 0 1 NC 1 NC 1 55 3 max -.03 1 .002 2 0 1 0 1 NC 2 NC 1_ - 56 min -.068 11 0 0 0 111 0 1 NC 111 NC 1 57 4 max -.029 0 0 0 NC NC 1 58 min -.067 0 0 0 NC NC 1 59 5 m ax -.029 0 0 0 NC NC 1 60 min -.066 0 0 0 NC NC 61 M7 1 max 029 0 0 0 NC NC 62 min -.065 0 0 0 NC NC 63 2 max -.029 .002 0 0 NC NC 64 min -.066 0 0 0 NC NC 65 3 max -.029 .005 0 0 NC NC 66 min -.067 .002 0 0 NC NC 67 4 max -.03 .008 0 0 NC NC 68 min -.068 .004 0 0 NC NC 69 5 max -.03 .011 0 0 NC NC 70 min -.068 .005 0 0 NC NC 71 M8 1 max -.014 0 0 0 NC NC 72 min -.03 0 0 0 NC NC 73 2 max -.014 .003 0 0 NC NC 74 min - .001 0 0 NC NC 75 3 max -.013 .006 0 0 8928.387 NC 76 min -.03 .003 0 0 NC NC 77 4 max -.013 .009 0 0 5952.258 NC 78 min -.03 .004 0 0 NC NC 79 5 max -.013 .012 0 0 4464.194 NC 80 min -.03 .006 0 0 9966.608 NC 81 M9 1 max -.003 0 0 0 NC NC 82 min -.006 0 0 0 NC NC 83 2 max 002 0 0 0 NC NC 84 min -.005 0 0 0 NC NC 85 3 max -.002 0 0 0 NC NC 86 min -.005 0 0 0 NC NC 87 4 max -.002 0 0 0 NC NC 88 min -.005 1111 0 ill 0 III 0 III NC NC 89 max -.002 0 0 0 NC NC 90 min -.005 0 0 0 NC NC 91 M1 0 U .008 © -.002 El 0 II 0 0 NC 0 NC 0 92 min .004 - 93 2 max .012 -.007 .004 0 0 0 0 NC NC NC NC 94 min .005 -. 0 0 96 48.011 N C 95 3 max .015 -.011 0 0 NC NC • 9 6 min .007 -.026 0 0 4824.006 NC 97 4 max .019 -.016 0 0 7183.195 NC 98 min .008 -.037 0 0 3216.004 NC • 99 5 max .023 -.021 0 0 5387.396 NC 100 min .01 -.047 0 0 2412.003 NC 101 M11 1 max .049 -.014 0 0 NC NC 102 min .021 -.033 0 0 NC NC 103 2 max .049 - .016 0 0 NC NC 104 min .021 -.037 0 0 NC NC 105 3 max .048 -.018 0 0 NC NC 106 min .021 -.042 0 0 NC NC 107 4 max .048 -.02 0 0 NC NC 108 min .021 1 -.046 2 0 1 0 1 8970.096 2 NC 1 RISA -3D Version 6.0.1.5 [H:IJobs 200610612521Calculations\Truss #3 Analysis with New Bearing.r3d] Page 8 (., ?_ ) ' Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 3:36 PM Job Number 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Deflections (Continued) Member _ Sec x [in] Ic y finl Ic z finl Ic x Rotate [r... Ic fn) Uv Ratio Ic (n) Liz Ratio Ic 109 5 max .048 2 -.022 1 0 1 0 1 NC 1 NC 1 110 min .021 1 -.05 2 0 1 0 1 6727.572 2 NC 1 111 M12 1 max -.024 1 -.02 1 0 1 0 1 NC 1 NC 1 112 min -.054 2 -.045 2 0 1 0 1 NC 2 NC 1 113 2 max -.024 1 -.019 1 0 1 0 1 NC 1 NC 1 114 , min -.055 2 -.043 2 0 1 0 1 NC 2 NC 1 115 3 max -.024 1 -.018 1 0 1 0 1 NC 1 NC 1 116 min -.056 2 -.042 2 0 1 0 1 NC 2 NC 1 117 4 max -.025 1 -.018 1 0 1 0 1 NC 1 NC 1 118 min -.057 2 -.04 2 0 1 0 1 NC 2 NC 1 119 5 max -.025 1 -.017 1 0 1 0 1 NC 1 NC 1 120 min -.058 2 -.039 2 0 1 0 1 NC 2 NC 1 121 M13 1 max -.016 1 -.024 1 0 1 0 1 6352.081 1 NC 1 122 min -.035 2 -.055 2 0 1 0 1 NC 2 NC 1 123 2 max -.015 1 -.02 1 0 1 0 1 8469.442 1 NC 1 124 min -.033 2 -.046 2 0 1 0 1 NC 2 NC 1 125 3 max -.014 1 -.016 1 0 1 0 1 NC 1 NC 1 126 min -.031 2 -.037 2 0 1 0 1 NC 2 NC 1 127 4 max -.013 1 -.012 1 0 1 0 1 NC 1 NC 1 128 min -.029 2 -.028 2 0 1 0 1 NC 2 NC 1 129 5 max -.012 1 -.008 1 0 1 0 1 NC 1 NC 1 130 min -.027 2 -.018 2 0 1 0 1 NC 2 NC 1 131 M15 1 max 0 1 0 1 0 1 0 1 NC 1 NC 1 132 min 0 1 0 1 0 1 0 1 NC 1 NC 1 133 2 max 0 2 0 1 0 1 0 1 NC 1 NC 1 134 min 0 1 0 2 0 1 0 1 NC 2 NC 1 135 _ 3 max 0 2 0 1 0 1 0 1 NC 1 NC 1 136 min 0 1 0 2 0 1 0 1 NC 2 NC 1 137 4 max 0 2 0 1 0 1 0 1 NC 1 NC 1 138 min 0 1 0 2 0 1 0 1 NC 2 NC 1 139 5 max 0 2 0 1 0 1 0 1 NC 1 NC 1 140 min 0 1 0 2 0 1 0 1 NC 2 NC 1 141 M15A 1 max .015 2 -.011 1 0 1 0 1 6255.215 1 NC 1 142 min .006 1 -.025 2 0 1 0 1 2798.239 2 NC 1 143 2 max .011 2 -.008 1 0 1 0 1 8340.287 1 NC 1 144 min .005 1 -.019 2 0 1 0 1 3730.986 2 NC 1 145 3 max .007 2 -.006 1 0 1 0 1 NC 1 NC 1 146 min .003 1 -.013 2 0 1 0 1 5596.479 2 NC 1 147 4 max .004 2 -.003 1 0 1 0 1 NC 1 NC 1 148 min .002 1 -.006 2 0 1 0 1 NC 2 NC 1 149 5 max 0 1 0 1 0 1 0 1 NC 1 NC 1 150 min 0 1. 0 1 0 1 0 1 NC 1 NC 1 151 M16 1 max 0 1 0 1 0 1 0 1 NC 1 NC 1 152 min 0 1 0 1 0 1 0 1 NC 1 NC 1 153 2 max 0 1 .001 2 0 1 0 1 NC 2 NC 1 154 min 0 2. .001 1 0 1 0 1 NC 1 NC 1 155 3 max 0 1 0 1 0 1 0 1 NC 1 NC 1 156 min -.002 2 0 2 0 1 0 1 NC 2 NC 1 157 4 max -.001 1 0 1 0 1 0 1 NC 1 NC 1 158 min -.003 2 -.001 2 0 1 0 1 NC 2 NC 1 159 5 max -.002 1 -.002 1 0 1 0 1 NC 1 NC 1 160 min -.004 2 -.004 2 0 1 0 1 NC 2 NC 1 RISA -3D Version 6.0.1.5 [H:1Jobs 200610612521Calculations\Truss #3 Analysis with New Bearing.r3d] Page 9 • Company : BMGP Engineers Inc. Feb 2, 2007 Designer : CTC 3:36 PM Job Number : 061252 Canterbury Truss Analysis Checked By: Envelope Wood Code Checks Memb... Shape Code Check Loc... lc She... Lo... .... lc Fc' [... Ft' [k..Fb1'... Fb2'... Fv' [... Eon 1 M1 2X4 1.042 7.664 2 1.042 7.5.. y 2 .962 1.5 2.587 2.846 .095 3.9 -3 2 M2 2X4 .933 7.086 2 2.789 14.... y 2 .962 1.5 2.587 2.846 .095 3.9 -3 3 M3 2X4 .178 0 2 .140 34... y 1 .856 1.5 2.587 2.846 .095 3.6.3 4 M4 2X4 .189 0 2 .000 0 z 1 1.413 1.5 2.587 2.846 .095 3.6.3 5 M5 2X4 .200 0 2 .000 0 z 1 .66 1.5 2.587 2.846 .095 3.6.3 6 M6 2X4 .044 0 2 .000 0 z 1 .377 1.5 2.587 2.846 .095 3.9 - 7 ` M7 2X4 .102 0 2 .000 0 z 1 .66 1.5 2 587 2.846 .095 3.6.3 8 M8 , 2X4 _ .007 0 1 .000 0 z 1 .377 1.5 2.587 2.846 .095 3.9 -1 9 M9 2X4 .011 0 1 .000 0 z 1 1.011 1.5 2.587 2.846 .095 3.9 -1 10 M10 2X4 .179 0 2 .000 0 z 1 .448 1.5 2.587 2.846 .095 3.9 - 11 M11 2X4 .024 0 2 .000 0 z 1 .342 1.5 2.587 2.846 .095 3.6.3 12 M12 2X4 .192 0 2 .000 0 ,z 1 .342 1.5 ,2.587 2.846 .095 3.6.3 13 M13 2X4 .099 0 2 .000 0 z 1 .448 1.5 2.587 2.846 .095 3.9 - 14 M15 2X4 .010 0 2 .000 0 z 1 .66 1.5 2.25 2.475 .095 3.9 - 15 M15A 2X4 .458 0 2 .000 0 z 1 .856 1.5 2.25 2 .095 3.6.3 16 M16 2X4 .275 0 2 .014 0 y _ 2 .589 1.5 2.252.475 .095 3:6.3 RISA -3D Version 6.0.1.5 [H:1Jobs 200610612521Calculations\Truss #3 Analysis with New Bearing.r3d] Page 10 • x N 4,77 �s ��. M2 M /0 8A 9 Mg 3 �� � 2 10A ,I ■• 15 10A 12 7 Solution: Envelope BMGP Engineers Inc. Canterbury Truss Analysis CTC _ Feb 2, 2007 at 10:34 AM 061252 Truss #3 Analysis.r3d Y 11► Z x ihihk ,... 7. 14v4 lell )1 1010.„ 4 7 Solution: Envelope BMGP Engineers Inc. Canterbury Truss Analysis CTC _ Feb 2, 2007 at 10:34 AM 061252 Truss #3 Analysis.r3d Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 10:35 AM Job Number 061252 Canterbury Truss Analysis Checked By: Global Display Sections for Member Calcs 5 ' Max Internal Sections for Member Calcs 97 a °' Include Shear Deformation Yes Include Warping . , Yes • Area Load Mesh jn ^2) 144 Merge Tolerance (in) `_ '— _5 P -Delta Analysis Tolerance 0.50% Vertical Axis . Y Hot Rolled Steel Code AISC: ASD 9th CO, ✓ 6 diSteel Code AISI 99: ASD Wood Code NDS 91/97: ASD Mee Temperature < 100F Concrete Code - ACI 2002 Number of Shear Regions _ 4 Re•ion S•acins Increment in 4 Biaxial Column Method _ PCA Load Co_ ntou_ r Par ii Beta,Factor PCA 1.65 Concrete Stress Block _ Rectangular Use Cracked Sections, 1 Yes Bad Framing Warnings I No Unused Force Warnings - I, . Yes 1 i Wood Material Properties Label Species Grade Cm Emod Nu Therm...Densjk/f... 1 DF Larch Douglas Fir -Larch Select Structural 1 _ .3 .3 .035 l 2" - So l`ne _ "r `SEitith t #i , -' No.1 1 . .3 .3 .035 J Wood Section Sets Label Shape Type Desion List Material Design Rules A lint] Iw fin41 lzz fin4l J fin4l 1 lWOOD1A 2X4 Beam Rectan ular 1 DF Larch 9 Typical 5.25 1 .984 1 5.359 2.877 Member Primary Data Abel I Joint J Joint K Joint Rotate(deg) Section /Shape Type Desi n List Material Desi.n Ru. 1 M1 N8 N10 WOOD1A Beam Rectangular DF Larch . 2 M2 N10 N7 WOOD1A Beam ` Rectangular DF Larch Typical 3 M4 N1 N8 WOOD1A Beam _Rectangular DF Larch Typical 4 M5 N2 N9 WOOD1A Beam Rectangular DF Larch T •ical 5 M6 N3 N10 WOOD1A Beam Rectangular DF Larch T •ical 6 - M10 N8 N2 WOOD1A Beam Rectangular DF Larch T •ical 7 M11 N9 N3 WOOD1A Beam Rectangular DF Larch Typical -8 M8 N1 N8A WOOD1A Beam Rectangular DF Larch T •ical " 9 M9 N10A N11 WOOD1A Beam Rectangular DF Larch T •ical 10 M10A N10A N7 - WOOD1A Beam Rectangular OF Larch Typical:'. 11 _M11A N3 N9A WOOD1A Beam Rectangular OF Larch T •ical 12 M12 N9A' N8A WOOD1A Beam Rectangular DF Larch Typical 13 M13 N10A N13 WOOD1A Beam Rectangular OF Larch Typical 14 M14 N13 N12 WOOD1A Beam Rectangular DF Larch Typical 15 M15 N12 N14 WOOD1A Beam Rectangular DF Larch Typical RISA -3D Version 6.0.1.5 [H: \Jobs 2006 \061252 \Calculations \Truss #3 Analysis.r3d] Page 1 Ir 7f-; • Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 10:35 AM Job Number 061252 Canterbury Truss Analysis Checked By: Joint Coordinates and Temperatures • Label X IIft] Y (_ft] Z 0 T [F] Detach From Diap 1 Ni 0 0 2 N2 7.25 1.208 0 0 - 3 N3 13.96 2.3267 0 0 4 N7 42 0 0 0 , 5 N8 0 4.75 0 0 6 N9 7.25 7.1667 0 0 __1 7 N10 13.96 9.403 0 0 8 I N8A 23 ...3.8333 0 ' 0 9 N9A 18.86 7.75 0 0 10 N10A - 23 ' 0 0 0 11 N11 23 6.4 0 0 12 N12 31 � 0 0 0 13 N13 28.22 4 0 0 14 . N14 33.6 2.8 0 0 i J 15 N15 0 0 0 0 Joint Boundary Conditions Joint Label - X [k/inJ_ Y jk /inl Z fk/in] X Rot.[k- ft/radl Y Rot.fk - ft/rad] Z Rot.[k - ft/rad] Footing 1 I N1 Reaction Reaction Reaction 2 N7 I L Reaction , 3 N10 I Fixed }} — 4 N 10A Reaction I Reaction Reaction rrk Wood Design Parameters Label Shape Length„ le2fftl let[ft] le- bend top[ft] le-bend bot[ft] Kyy- Kzz CH Cr v sway z sw.y 1 M1 WOOD1A 14.715 1 7 Yes 2 M2 WOOD1A ,2WA 1 7 '' 'I, 1 ..,r 3 M4 WOOD1A 4.75 1 Yes: Yes 4 M5 WOOD1A 5.959 3.5 k 1. . ,1 41 *'**** ' Yes`; 5 _ M6 WOOD1A 7.076 4.75 -_ -__ Yes ` 6 M10 WOOD1A 8.069 4.33 Yes 7 M11 WOOD1A 8.273 5 Yes 8 M8 WOOD1A 23.317 1 7 9 M9 WOOD1A 6.4 3.2 10 M10A WOOD1q"k =19 1 7 ,11 t�t'T_,z 11 M11A WOOD1A 7.309 3.75 12 M12 WOOD1.05 699 3 13 I M13 WOOD1A 6.997 3.5 14 M14 WOOD1A 5.604 3 . 15 M15 WOOD1A 3.602 Member Distributed Loads (BLC 1 : Dead Load) Member Label _ Direction Start Magnitude[k/ft,d..End Magnitude[k/ft,d... Start Location[ft,%] End Location[ft, %] 1_ M1 Y -.014 _ -.014 0 0 2 M2 Y -.014 -.014 0 0 3 M8 Y -.016 - -.016 0 0 4 M 10A Y -.016 -.016 0 0 — Member Distributed Loads (BLC 2 : Snow Load) Member Label Direction Start Magnitude[k/ft,d..End Magnitude[k/ft,d... Start Locationtft, %] End Location[ft, %1_ 1 M1 Y -.05 -.05 0 0 2 M2 „ Y -.05 -.05 0 0 RISA -3D Version 6.0.1.5 [H:1Jobs 200610612521Calculations\Truss #3 Analysis.r3d] Page 2 Company : BMGP Engineers Inc. Feb 2, 2007 Designer : CTC 10:35 AM Job Number : 061252 Canterbury Truss Analysis Checked By: Basic Load Cases BLC Description Category X Gravity_Y Gravity Z Gravity Joint Point Distribu...Area (M..Surface... 1 Dead Load DL 4 t 'r °f aq .. oz 4 , p .,'" 'r q ' "'r8 Y 0 Load Combinations Description Solve PDelta SRSS BLC Fact...BLC Fact...BLC Fact...BLC Fact...BLC act...BLC Fact...BLC act...BLC Fact.. 1 Dead Load Yes DL 1 VT � � "f � ,.,' ... .e. c- n t ,' L 'd�l`. 1•., �W ® .., ... 0 &��.t � F' "� �^ �. SihM.. p v���' � ..�. l , MINE �' .�.Y.''xITIg «IQMkN .. Envelope Joint Displacements Joint X [in] Ic Y [in] Ic Z [in] Ic X Rotation .. Ic Y Rotation .,. Ic Z Rotation [... Ic 1 N1 max 0 2 ,� 0 1 0 1 0 1 0 1 -2.684e-3 1 i _,�,:, EN T MM O A m9;�.� � a I 76 ` yam 3 N2 ® 01 © -.015 0 0 0 0 0 0 KM 1.14e-3 0 5 N3 .022 © -.016 0 0 0 0 0 " 0 0 1861e3 7 N7 EMI "s : . _ n u.. EU 7.365e-3 015 © 0 0 o 0 0 0 0 a�` - � -� ;�'�� kx. Q .. . t ' . `z C " .. 3 Sf he � a r li-"°' .� v f 9 N8 01 © -.002 0 0 2 066e -3 0 0 -� 0 0 0 0 "` 'hJ, sue. Rii M E 11 N9 fZ ® .023 © 016 0 0 111 0 0 0 0 9.235e-4 13 N10 .016 © -.015 0 0 0 0 0 U ' -7.096e-4 0 it " l 00 ® � . ?• Y k ... r s '�. - �° is , c 31E ,°` M ¢ I I MI 15 N8A .026 © 002 0 0 0 0 0 0 0 -7.586e-5 0 I a �� 0 N9A 1111111 � 014 © � .011 ��� � 01.05 � ,�� A� tt ��-; ® �_• � � ��r � a � = w � ,@ 0 0 0 0 0 0 0 1.858e-3 r- 5 7 -pir aT F „ 6" I •� ti of g J 7 r t Ti ;,. g 19 g N 10A l 0 II 00 0 0 0 0 0 � -2.025e-3 U 9 il~ .�' .4..v -.., ' ' ' ; `,S'` ,r ks��; w , E : r.k 2 "i. € � 4 . J VAIVIMFIERINA 21 N11 Ertl .025 1111 _ 003 0 0 0 0 0 0 0 -2.169e-4 0 • Q ® � � 'v %' .. t :klY "��}Y'i�ffigk_....IsM' 23 N12 .002 ® -.019 0 0 NI 0 0 0 0 -1.999e-3 0 tillati - �R06g m 25 N13 .02 1411 -.012 ® 0 0 0 0 0 0 1.157e-3 xX , }a3 I, at:. &F A '; °•,'. �x -`�g s. «fv "i,�� a '� + + • PA., �'p 27 N14 007 #' �� © -.021 0 0 0 0 0 0 0 -1.424e-3 0 g.-4 a �. r: 3 .31gkt F ; `�xY".dK -.'+M f ' y sl.?k. g „'tai' <?+.,& 4 - �; I � M O � L'. y£' � r M � '%�� '� �� � � tt fF t& �i�k� � B �.�i '- 6 tt 29 N15 ® 0 0 0 IN 0 BM 0 . ., s*��.,; . . ?a „`t � .� �.5 .�� .'.3ITA ° 4N1 , ,... {7 w .�.. KIM $�.• a (� u �:.; 'k� t 'f`. iF � z".. Envelope Joint Reactions Joint X [k] Ic Y [k] Ic Z [k] Ic MX [k -ft] Ic MY [k -ft] Ic MZ [k -ft] Ic 1 N1 max -.163 1 .832 2 0 1 0 1 0 1 0 1 2 s ', .....mm rc. .445... 2G. .309, 1; 0 , : 1 «: 0 14 E. ,..• . 0 , 3 N7 max 0 1 .632 2 0 1 0 1 0 1 0 1 4 rn 5 N10A max .445 2 2.048 2 0 1 0 1 0 1 0 1 7 Totals: max 0 1 3.512 2 0 1 8 m`iri . .0 . 2 1.297 1 01 RISA -3D Version 6.0.1.5 [H: \Jobs 2006 \061252 \Calculations \Truss #3 Analysis.r3d] Page 3 2.2,Fs' • Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 10:35 AM Job Number 061252 Canterbury Truss Analysis Checked By. Envelope Member Section Forces Member Sec Axial k Ic Shear Ic z Shear k Ic Tor. ue k Ic Mome... Ic z-z Mom n k -ft 0 M1 11111 max .915 0 .179 0 0 0 0 0 o 0 o 0 . t " . miry .328 1 039' °; 0 � r , ©- ©max 841 2 L 01 0oi'0 0 0 o IN -.055 0 r a", m in 7; .312 1 . - .04411 0 0 Ii . .,t'- a;. € ry DDaE 'k`3 x'. Rs? 1 © -© max .766 2 -.058 0 0 0 0 0 0 0 .327 � `� � � �" ..295 .2 "•� �,� 1 , 0- 4 .708 2 066 0 a 0 0 0 0 0 -.037 El $ ' `: '� gtI I<i@t i ...272 , .1.; • .014 .,L ` 1: r. �� F {ati k ' :I _ .ia 9 ©® 3 .63 0 ., , � r� ��, n _ © 035 1 0 0 0 o 10 >, � E•x€' e ® . x.,..,-157. spcw'al i iM c - W "aNIM x� n '1 '�� E 11 M2 max .642 © .131 0 0 _ 13 ©® -.176 0 -.003 0 0 0 0 0 0 0 0 0 O V i ft s � mid • Aa17® U 4 3 0 tn Q1�"t �., 1 0 � �� 0 `r � -� k�s``a �r� �� x u b � 15 - ©max 16 0 -.03 0 0 0 0 0 0 0 .056 ?.a-llti is.. ,�i,£ , s„ ''�v • r' •'.�Y. ^� i.J,'', I ' " ,�` MEI a .s �•..v. Fl z 17 4 ® .965 © .228 Fl 0 0 0 0 0 0 .028 El 1 t er mi s 5 x = � � Zu:` o � £ u E� ti•� g �dgx9 x �i 19 - ©® 1.116 El -.048 El 0 D 0 D 0 D 0 0 21 M4 IN max .856 © 0 0 0 0 0 0 0 0 • ' _ o 0 ` t 08� 0� � 0� _L� -'f 0i a`,a r a O .. ,.. 5ZfAB! figa'. AZE i 23 -0M .856 © 0 0 0 0 0 0 0 0 0 ° . 25 - ®max .856 © 0 0 0 0 0 El 0 0 � 0 0 12142: VPklhli§lttlFdlfffiMEIB.iflTirttk4:iMlVlgi.?;:RietM,EEIJMttrRFjTeatnEfili:j5:.', 27 4 .856 0 0 II 0 0 0 0 0 0 0 0 29 MI max .856 © 0 0 0 n 0 0 0 0 kill PG x a $ A _ i '•3 ,1 ,5"" 1'. 0 'a. P Mgr h �,. O �a A W .,'' sr r 's" , r `S" `* '"n,?r1 , 4 i, .,r. 31 LL M5 O max .417 © 0 0 0 0 0 0 0 0 0 u L t, <.- l. a tGS " h '.;. ' Ps 5fe'a x x i n3 ,:. 40 33 - ©111M .41 ® 0 0 0 D 0 D 0 D 0 0 0 0 °t� r # �. x �� r`W� -sub ,�.t�� � 4 35 - ©max .417 0 0 0 0 EN o IN o IRI S @ ; s 0w: 1 r0 .<. U n_ a,k E . : at.. r • � 4. . 474! `A 37 4 2 � q 417 © 0 D�i�O 0 111•0 h 0 0 0 • RI II €tt -M t� a .� ',� ),.0 '' 0 @ s;4 r `, 3z `#` Cig - t axi 3 39 ©® .417 © 0 0 0 0 0 0 0 0 .. " 0 El • �: R i '. . ' .•': Wn f - ®n '^ ` ' ' x a '4 R. 34 ' l u s _ .,,.d..; c,�wxxn z f 0 . a � � 0 �f ,� E j<+u s 41 M6 Omax -.102 0 0 0 0 0 0 II 0 0 0 0 • x "+ nk4 2 6 fG ^° kt'S'dM • 43 ©® -.102 El 0 0 0 o 0 o EN ,, a. MiliNAVAZ d`: 45 -©® ▪ 102 0 0 0 0 0 0 0 0 0 0 2 w.� �` r . , -C T, }e:. M. h:� +,F� • }g. p�`�w �, EMI WAS tofvl 47 4® ▪ 10 0 0 OHO r.t 0 0 0 0 0 tr -,311E512":. 49 © � ® �T�i� �i I'II 0 �NEM•0 0 0 0 0 • II ® a`i., 1 :,i,,,;.: 2. iW@p19 �c' �' .3;a `` ' t � k t .r' R� ? .' 3 tr ,� f!;'�:� & ? :,;, • ?a* k.. 0MIV0 0 y ' y F� M10 D 0 D 0 O�i�O • -3 . r li: 1 :., irx', " r9 7M + ' . 4 �: ,� Y Q.,. {` > s n� uV f . t : ®'4i� w u P ''�5. z , x'V " o 0 , o E o E o 55 ra .333 0 0 0 o 0 o 0 o 0 0 0 6:. 444; 4m.; - . 33 ' 0 . 1x. . 0 0 0 0 d: RISA -3D Version 6.0.1.5 [H: \Jobs 20061061252\Calculations \Truss #3 Analysis.r3d] Pa e 4 Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 10:35 AM Job Number 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Forces (Continued) Member Sec Axial[kl Ic y Shearikt Ic z Shear[k] Ic Torquelk -... Ic v -y Mome... Ic z -z Moment[k -ft] Ic 57 4 max -.333 1 0 1 0 1 0 1 0 1 0 1 58 min -.903 2 0 1 0 1 0 1 0. 1 0 1 59 5 max -.333 1 0 1 0 1 0 1 0 1 0 1 • :60 min -.903 2 0 1 0 1 0 1 0 1 0 1 61 M11 1 max .199 2 0 1 0 1 0 1 0 1 0 1 62 min .056 1 0 1 0 1 0 1 0 1 0 1 63 2 max .199 2 0 1 0 1 0 1 0 1 0 1 ' 64 min .056 1 0 1 0 1 0 1 0 1 0 1 65 3 max .199 2 0 1 0 1 0 1 0 1 0 1 66 min ' .056 1 0 1 0 1 0 1 0 1 _ 0 1 67 4 max .199 2 0 1 0 1 0 1 0 1 0 1 68 min .056 1 0 1 0 1 0 , 1 0 1 0 1 69 5 max .199 2 0 1 0 1 0 1 0 1 0 1 70 min .056 1 0 1 0 1 0 1 0 1 0 T°` -.157 1 71 M8 1 max .049 2 0 1 0 1 0 - _ - -1 0 1 72 min -.442 2 = 049 1 i 0 1 0 1 0 1 0 1:;: 73 2 'max -.172 1 -.043 2 0 1 0 1_ -. 0 1 -.016 1 74 min -.458 2 .043 1 0 1 0 1 0 1 -.018 ` °§ 75 3 max -.472 1 -.022 1 0 1 - 0 1 0 1 .015 1 76 min 1.277 2 .022 12 0 1 _ - 0 11 0 ' 1 012 21.k 77 4 max -.324 1 .033 1 0 1 0! 1 0 1 - 079 1 f 78 min -:931 2 .032 2 0 1 0 1 0 1 r -.08 ' ` `2 79 5 max -.339 1 .059 1 0 1 0 1 0 1 0 1 ='.80 min -.947: 2 -.06 2 0 1 0 1 % 0 1 0 1 81 M9 1 max 1.432 2 .005 2 ,' 0 1 0 1 0___ -- 1_ 0_ - -- 1 '82 min .5 1 .002' 1 0 1 0 1 0 1 0 1 83 2 max 1.432 2 .005 2 0 1 0 1 0 1 -_ 003 1 7 8 7- 1 "I:- ,'µ.;,., min .5 . 1. :002 1 0 1 0 1 0 1 -.008 2 85 3 max 1.432 2 1 .005 2 0 1 0 1 0 1 ' -.006 1 86= .' 1' min - .5 1 -.002 1 0 1 0 1 0 1 � -.017 2 87 4 max .331 2 -.003 1 0 1 0 1 0 1 -.004 1 88 v't - mm . .074' :1 -.008' 2 0 1,: .0.:.._ 1 I ..0 1 .012 2 89 5 max .331 2 -.003 1 0 1 0 1 0 1 0 1 90 min .074 1 -.008 2 0 1: 0 ' 1 0 1 0 1 91 M10A 1 max -.069 1 .045 2 0 1 0 1 0 1 0 1 92 min -.189 2 .044 1 0.. 1 0 1 0 1, 0 1 93 2 max -.069 1 -.031 2 0 1 0 1 0 1 -.031 1 ' 94 min -.189 2 -.032 1 0;' 1 0 1 0 1 -.035 2 95 3 max -.343 1 .084 1 0 1 0 1 0 1 .076 1 =96 mm - .988' 2 .083 2 0 1 0 1 0 1 .07 2 97 4 max -.343 1 .008 1 0 1 0 1 0 1 -.143 1 :,98 min - -.988 2 .007 2 0 1 0 1 0 1 - -.145 2 99 5 max -.343 1 -.068 1 0 1 0 1 0 1 0 1 100 min -.988. 2 -.069 2 0- 1 0 1 0 1 0 1 101 M11A 1 max -.136 1 0 1 0 1 0 1 0 1 0 1 102 min -.255 2 0 1 0 1 0 1` 0 1 0 1 _ 103 2 max -.136 1 0 1 0 1 0 l 1 0 1 0 _ 1 104 min -.255- 2 0 1 0 1 0 1 0 1 0 1P: 105 3 max -.136 1 0 1 0 1 0 1 0 1 0 1 106 thin -.255 2 0 1 0 1 0 1 0 1 0 1; 107 4 ,max -.136 1 0 1 0 1 0 1 0 1 0 1 108 min -.255 2 0 1 0 1 0 1 0 1 0 1 109 5 max -.136 1 0 1 0 1 0 1 0 1 0 1 110 min -.255 2 0 1 0 1 0 1 0 1 0 1 111 M12 1 max 1.29 2 0 1 0 1 0 1 0 1 0 1 112 min .454 1 0 1 0 1 0 1 ' 0 1 0 1 113 2 max 1.29 2 0 1 0 1 0 1 1 0 1 0 1 RISA -3D Version 6.0.1.5 [H :\Jobs 2006 \061252 \Calculations \Truss #3 Analysis.r3d] Page 5 Company : BMGP Engineers Inc. Feb 2, 2007 Designer : CTC 10:35 AM Job Number : 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Forces (Continued) Member Sec Axialfk Ic Shear k .454 1111 0 Ic z Shearjkl Ic Torquefk -... Ic v -v Mome... Ic z -z Momentjk -ftl _ Ic • 114 min 1 0 1 0 1 0 1 0 1 115 3 max 1.29 0 1 1 0 1 0 1 0 1 0 1 116 min .454 1 0 j 1 0 11 0 1 0 1. 0 1 . 117 4 max 1.29 2 0 1 0 1 0 1 0 1 0 1_ 118 min .454 0 1 0 1 0 1 0 1 0 1 119 5 max 1.29 ® 0 1 0 1 0 1 0 1 0 1 X120 min :454 1 0 1 0 1 0 1 0 1 0 1 121 M13 1 max .856 2 0 1 0 1 0 1 0 1 0 1 :122 min ..313 1 0 11 0 1 0 1 0' 1 0 1 123 2 max .856 2 0 11 0 1 0 1 0 1 1 0 1 124 rrifif C; .313 1 1 0 i 1. 0 1 0 1 0 1 0 1 125 3 max .856 ' 2 0 1 1 0 1 1 0 1 1 0 1 0 1 126 min" ` .313 1 1 0 1 1 0 1 1 0 : 1 0 1 0 1 127 4 'max .856 2 0 1 0 1 1 0 1 0 1 0 1 128 min .313 1 1 0 1 1 0 , ' 1 0 1 0 1 0 1 1291 ! 5 max .856 .1 2 0 1 0 1 0 1 0 1 0 1 X130 I Imin .313 " 1 1 0 1 0 1 1 0 1 0 1 0 1 131 M14 1 max -.349 1 1 0 1 1 0 1 0 1 0 1 I 0 1 t132I Amin 775 2 0 1 0 11 0 1 0 1 .. . 1 133 1 2 !max -.349 1 0 1 0 1 0 ! 1 0 1 0 1 1464 min -.775 1 2' 0 ! 1 0 1 1 i 0 i 1 0 1 ` :_F 1 135 3 'max -.349 1 0 1 0 1 0 } 1 0 1 0 1 :136 Imin -,775 2 0 1 0 1 0 I'1 0 1 - 0 '� , 137 4 'max -.349 11 0 1 0 1 0 1 1 i0 1 i 0 1 X138 min -.775' 1 2 1, - 1 1 0 1 1 0 1 1 0 1 0 1z+` 139 5 max -.349 1 0 ! 1 0 1 1 0 1 1 0 1 0 1 -140 1 4 fn : -.775 12 j 0 i 1 1 0 1 1 0 1 0 1 0 =1 141 M15 1 max .585 1, 2 l 0 1 1 1 0 1 0 1 0 1 0 1 142 min 127 r1 0 1 0 11 1 0 1 0 1 0 1 143 1 2 rrp .585 ' 2 0 1 0 i 1 0 1 0 1 f 0 1 ;8144 min .127 1 0 1 0 , 1 1 0 1 0 1 0_ 1 145 3 max .585 [ 0 1 0 1 0 1 0 1 1 0 1 x.146 min .127 11 0 1 0 1 0 1 0 1 0 1 147 4 'max .585 2 0 1 0 1 0 1 0 1 J 0 1 _148 min , .127 1 0 '1' 0 1 0 11 0 1 0 1 149 5 Amax .585 ; 2 0 1 0 1 0 1 0 1 0 1 150 'min .127 1 1 0 11• 0 1 0 1 0 1 0 1 Envelope Member Section Deflections Member Sec x [in] Ic y [in) Ic z fin] Ic x Rotate (r.., Ic (n) Uy Ratio Ic (n) Liz Ratio Ic 1 Ml 1 max .016 2 - .004 1 0 1 0 1 NC 1 NC 1 r 2 , min .006 1 - .01 2 0 1 0 1 NC 2 NC 1 3 2 max .012 2 - .057 1 0 1 0 1 3534.795 1 NC 1 4 min .005 1 -.238 2 0 1 0 1 806.509 2 NC 1 5 3 max .008 2 -.019 1 0 1 0 1 NC 1 NC 1 - 6 min .003 1 -.054 2 0 1 0 1 6498.859 2 NC 1 7 4 max .005 2 -.043 1 0 1 0 1 5863.311 1 NC 1 8 min .002 1 -.163 2- , 0 1 0 1 1378.982 2 NC 1 9 5 max .002 2 -.016 1 0 1 0 1 NC 1 NC 1 -10 min 0 1 -.044 2 0 1 0 1 NC 2 NC 1 11 M2 1 max .028 2 -.012 1 0 1 0 1 NC 1 NC 1 12 min .01 1 -.034 2 0 1 0 1 NC 2 NC 1 13 2 max .025 2 -.002 1 0 1 0 1 NC 1 NC 1 14 min .009 1 -.003 2 0 1 0 1 NC 2 NC 1 15 3 max .029 2 -.01 1 0 1 0 1 NC 1 NC 1 16 min .011 1 -.029 2 0 1 0 1 NC . 2 NC 1 RISA -3D Version 6.0.1.5 [H:IJobs 200610612521Calculations\Truss #3 Analysis.r3d] Page 6 R:3 / Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 10:35 AM Job Number 061252 Canterbury Truss Analysis Checked By Enve lope Member Section Deflections (Continued) Member Sec x Finl Ic v [inl Ic z lint Ic Rotate [r... Ic n) Uy Ratio Ic n) Liz Ratio Ic • 17 4 max � 0_23 2 -.055 1 0 1 0 1 6670.77 1 NC 1 ,• �m r s � of s s k i`[ ., ' r a F x y �� � �. � fi� , . ' � � 1$ ? � � g ��'���a �. 164 4 0 � , 2i 19 - © tr ® .014 ® .005 © 0 0 0 0 NC -r N . 1 l 0WM. '0 � �'r t r y ,� i x z 4 j _ . .� y y © I ' V C 0 21 M4 o E 0 o o 1111 Nc ME Nc • t .t ;air: 27 S3 5T 7 tit rit -' �`L .x SS EMI 'D. +b _ Y ^.' K°T" Y 3 FT © W" 0 > > � ` o � o lam' V' , 23 00 2 0 NC El NC 0 25 - worn 0 B 003 Ell 0 0 o 0 NC El NC E ¢_ =� ems. 27 - 4 max -.001 005 0 0 3 �,a„ D NC Y itt zi , ,,k` , A , '£: ' . � d � . t .. �E'. i ; ::' T '.ms ?� V o 4 r `` � N .+x :. � _ rte,-,', - 29 worn - 002 007 Ell 0 0 0 NC MI NC • __ 0 k k s M 9 � ��9 ° st ' 8 � � �a1 * ri. r° rNEVINb, 31 M5 0 max -.015 0 -.004 El 0 NC }'a -i " ,_ � aE c - ' , i ; ..� -~r, ",.,`" �"4 3 ; n 7 £ ' , ,� 7m�If `` . � :�'- - 'I r x ;( ` ".+. ;-; �'z' 2e` 3b' 0 El NC NC 33 worn 015 005 4. 0 0 r 0 El '' • E 77yy �kkkk, � O NC O 35 - worn -.015 0 -.006 El 0 0 -- . , � i . - ' 42`n - I, - 2 :zS, Q 0 #4 o D i4 NC : ri NC 37 - 4 max -.015 Ell -.007 11 0 0 0 � NC _ NC MI 39 -worn -.016 NM 009 0 4y A 04 wu n 0 � 0 0 NC 0 NC 0 t t a ` `:. " "1 5:$i 7 Q^3 a'^ e s :t?s p ' m ® rgs ®'; ;,,rg F314 Mai 41 M6 0 max -.016 - .008 0 0 0 0 0 NC y..2. - 042 ' _' = 022 2` 0 >�� " �' '� `, ` 0 NC MEN x - 43 © max 015 1 007 0 NC EN � 0 D 0 � NC S T ,ilt. > i - 042 2 u,.. 0 i � VM3 14? 131115M,EitaiMBE 45 -®® -.015 El -.007 0 0 D 0 D NC D NC Ell '.Ex ?t .aY I K.�v 041 ', 019. _.> 47 4 ® -.015 El 006 1 0 f 10041' 2 •'--.017> ' - °2 �. � O * ' N D NC II 49 -worn -.015 EN - 006 1 I 0 NC EN g E h nirx .t.i� 0 1:' � A 2 1 0 'META � NC R, 51 M10 Ell max .019 © 004 2 0 Nc Ell ',Y. �.A 0 a NC z 53 - worn .021 © -.002 . . 55 worn 023 © -.005 E 0 1 0 1 NC 0 NC Si e + a t 8:; r . hurry ;�t a X91 #v I 57 4 ® .025 © -.008 '4� O. 1 "� 1 0 - � ,� fi� � KN �� . t a ® %�.,i:::f j tea » t� `ra'ltr4ta.r ,` g..t 9 a .. e O 0 1 NC � � s NC KM 59 - worn .027 ©- ▪ 012 0 0 0 0 1 NC 0 NC 0 61 M11 0® .044 ® -0 08 ® III 0 0 fi NC g 0 NC III � tv � s"'3i n'I °s' .y:' . iCF �.,_ 5 d a3M i 'tt " "' �'s 4; 3:x .Yi� 1r` k �& 3� �" ��e l:$542) 63 - t ® .044 © -.008 NM 0 0 � 0 0 NC 0 NC to t� • 1 - 022 a n ® r w t� 65 - ® ® .043 r 04 _ 2 - 008 x ����� ���� 6 n. „a : � 0 0 0 0 ®0 NC 0 _ �_� 6 a 6 1 - 021 ` ®;, k�� ` fi I 67 4® .043 ©- ▪ 0 NI 0 0 0 0 NC � 0 OHO S Ia � � �:. .. V ' g S Rc q$ £r � 69 worn .042 ©- ▪ 108 Ell 0 0 MI NC 0 70 . .::". � h h a} +;' y }.gut. � I 71 M8 U. 0 El 0 El 0 O 0 O NC 0 ®0 73 2 max .003 2 -.044 1 0 1 0 1 6549.019 1 NC 1 RISA -3D Version 6.0.1.5 [H: \Jobs 200610612521Calculations \Truss #3 Analysis.r3d] Page 7 L • Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 10:35 AM Job Number 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Deflections (Continued) Member Sec x in Ic in Ic z in Ic x Rotate r... Ic n U Ratio Ic n Uz Ratio Ic • 74 min .001 1 -.066 II 0 ® 0 111 4425.204 II NC 1 75 3 max .011 2 .002 0 0 NC NC 1 76 min .004 -.028 0 0 NC NC II • 77 4 max .018 ® -.131 111 0 II 0 II 2192.229 ® NC 78 ®rnin .007 ® -.153 ® 0 ® 0 1931.309 NC III 79 max .025 -.004 0 0 NC NC 80 M® .009 1 - .011 ` ® 0 0 0 - NC NC MI 81 M9 1 max 0 1 1 0 0 II 0 NC NC 82 1 min 0 ®:;. 0 ', 0 0 NC g 0 NC so 83 2 max 0 1 -.005 0 0 0 0 0 NC ' 1 NC 0 84 min -.003 2 -.014 0 0 NC NC 1 85 3 max -.002 1 -.009 ® 0 1111 0 ® NC NC 1 86 min -.006 2 -.024 0 0 6726.199 NC 1 87 4 max -.002 1 - .01 ® 0 II 0 II NC NC 1 88 11111 min -.007 2_r -.027 ` ® 0 IffM1111111M111111 9168.417 n NC IIIII 89 IMO max -.003 1 - 009 1 0 0 0 0 NC M NC 0 90 't• ; . ;. “--, 111111M1 -.008 2 -.025 ®;. 0 1 0'` . i.IM NC .. IM NC IIIII 91 M10A 1 max 0 ' 1 0 0 0 0 0 _ 0 NC 0 92 ®® 0 M 0 0 ;. 0:'., ;� NC NC ® NC ill 93 2 max .001 © - .038 0 1 0 0 6036.659 11 NC 0 94 ' min ? 1 0: ® - .061 0 1 0 °, t, 3737.759 NC 1 95 3 max 003 2 -.064 0 1 0 IN 3555.415 1 NC III 96 min _ .001 1 _. - 097 0 1 0 < , ,o 2358.969 2 NC 97 4 max - _009 _. 2 -. 1 0 1 0 U 921.678 1 NC 0 98. _ `` - min .003 1 -.269 2 0 1 0 ''' ,A* 847.261 2 NC Bil 99 ! 5 max .015 2 j 0 1 0 1 0 0 NC 1 NC 1 100 min .005 ' 1 I 0 1 0 1 0 NC 1 NC Mil 101 M11A 1 ,max -.006 1 , -.016 1 0 1 0 NC 1 NC 1 102 min -.017 2 i -.044 ' 2 0 ® 0 NC 2 -1\14Gii ' 1 103 - ®max -.006 U -.015 0 0 NM 0 0 NC 1 NC 1 104 min -.016 2 - .041 2 0 II 0 ® NC 2 NC IN 105 3 max -.006 1 -.014 1 0 0 NC 1 NC 106 ME ® min - .015 2 - .038 ® 0 ® 0 ® NC ® NC Ell 107 - 4 max -.005 1 I -.013 0 0 0 NC _ NC 0 108 0 = -2' '; • min > -.015 2 -.035 0 0 NC NC 1 109 max -.005 1 -.011 ® 0 0 NC NC 1 110 ' ® -.014 ® .032 0 0 NC NC ME 111 M12 1 !max .032 2! -.005 0 _ 0 NC NC 0 112 min .012 1 . -.014 0 0 NC NC 113 2 max .03 2 -.002 ® 0 0 NC II NC 114 II I min .011 II ` =:0 2 0 II 0 II NC ® NC max .028 116. ®® .01 0 0 ® 0 ® 0 U NC © NC- MI 117 - 4 we .026 2 .006 © 0 0 0 11 NC © NC 0 118 ®® .009 1 ' .002Z <' ® 0 E 0 ® NC NC III 119 - ©1241 .024 © .013 © 0 0 0 NC NC 0 120 ®® .008 ® .005 ® 0 ® 0 ® NC NC Ell 121 M13 max 0 0 III 0 II 0 111 NC 1111 NC 122 min 0 0 0 0 NC NC 123 ma 0 -.003 0 0 NC NC 124 ® 002 ® 009 ® 0 ® 0 ® NC ® NC 125 3 max -.001 III -.007 NI 0 0 NC NC . 126 min -.004 -.019 0 0 NC NC 127 4 max -.002 - .01 0 0 8178.48 NC 128 min -.005 2 .028. ` 2 0 1 0 1 NC 2 NC 1 129 5 max -.003 1 -.014 1 0 1 0 1 6133.86 1 NC 1 130 min -.007 2 -.038 2 0 1 0 1 NC 2 NC 1 RISA -3D Version 6.0.1.5 [H: \Jobs 200610612521Calculations\Truss #3 Analysis.r3d] Page 8 X2. 6. Company BMGP Engineers Inc. Feb 2, 2007 Designer CTC 10:35 AM Job Number 061252 Canterbury Truss Analysis Checked By: Envelope Member Section Deflections (Continued) Member Sec x [inl Ic y finl Ic z fin] Ic x Rotate fr... Ic (n) Uy Ratio Ic (n) Uz Ratio Ic • 131 M14 1 max .039 2 0 1 0 1 0 1 NC 1 NC 1 132 min .014 1 -.002 2 0 1 0 1 NC 2 NC 1 133 2 max .04 2 -.003 1 0 1 0 1 NC 1 NC 1 . 134 , min .015 1 .008 2 0 1 0 1 NC 2 NC 1 135 3 max .041 2 -.005 1 0 1 0 1 NC 1 NC 1 136 min .015 1 -.014 2 0 1 0 1 NC 2 NC 1 137 4 max .042 2 -.008 1 0 1 0 1 9601.978 1 NC 1 138 min .016; . 1 -.021 2 0 1 0 1 NC .. NC 1 139 5 max .044 2 -.01 1 0 1 0 1 7201.484 1 NC 1 ) 140 min .016 1 027 - 2 0 1 0 1 NC 2 NC 1 141 M15 1 max -.014 1 -.013 1 0 1 0 1 NC 1 NC 1 142 min -.039 2 -.034 2 0 1 0 1 NC 2 NC 1 143 _ 2 max - .015 1 - .013 1 0 1 0 1 NC 1 NC 1 :144 m m , s4 03 1 1�, ' : 2 . .036` 2 0 1 0 1 NC 2 NC 1 ` 145 3 max - .015 1 -.014 1 0 1 0 ' 1 NC 1 NC 1 146 a. mm - .038 2 0 1 0 I 1 NC 2 NC 1 147 4 max , 1 -.014 1 1 0 1 NC 1 NC 1 - 7 ` `` Hirt. ": 04` ' ; 2 -.04 2 0 1 , 0 1 7202:938 ' 2 ` ( 1'6:x=,' 1 149 5 max -.015 1 -.015 1 0 1 0 NC 1 NC 1 X150 min -.041 2 -.042 2 0 1 0 1 5402.203 2 ?: 1 Envelope Wood Code Checks Memb... Shape Code Check Loc... Ic She... Lo.,.... Ic Fc' [... Ft' [k..Fb1'... Fb2'.,. Fv' [... Eqn 1 M1 2X4 .741 7.664 2 .833 7.5.. y 2 .856 1.5 2.587 2.846 .095 3.9 -3 2 M2 2X4. .812 25.... > 2 ':911 20.: 'Si Y i''' 1.5 2:587 2.846 :095 339 =3' 3 M4 2X4 .115 0 2 .000 0 z 1 1.413 1.5 12.587 2.846 .095 3.6.3 ., 4 : M5 2X4 .120 0 2 .000 . ; z :1' .66 ; 1 ! .5`12 .5872:846 .095 3:6;3 5 M61 2X4 .017 0 2 .000 0 z 1 .377 1.5 2.587 2 - 846 .095 3.9 - ' 6 M10 2X4 .115 0 2 ':000 0 z .1 ' 1.5 2 .587 2.846 .095 3.9 -1 7 M11 2X4 0 2 .000 0 z 1 .342 1.5 2.587 2.846 .095 3.6.3 8 M8 2X4 .357 14.... 2 :248 14..:, y ..1 ' :856 1 2.25 2.475 .095 3.9 -1 9 M9 2X4 .354 0 2 .023 3.8.. y 2 .77 1.5 2.25 2.475 .095 3.6.3 10 M 10A 2X4 ,405 8:51 >2 .300 8 .51 y 1 '.856 1.5 2.25 2.475 .095 3.9 -1 11 M11A .032 0 2 .000 0 z 1 .584 1.5 2.25 2.475 .095 3.9 -1 12 M12 2X4 .287 0 2 '.000 0 z 1 .856 1`.5 ,095 3.6.3 13 M 13 2X4 .247 0 2 .000 0 z 1 .66 1.5 2.25 2.475 .095 3.6.3 14 M14 2X4 .098 0 2 .000 0 z 1 .856 1.5 2.25 2.475 .095 3.9 -1. 15 M15 2X4 .178 0 2 .000 0 z 1 .627 1.5 2.25 2.475 .095 3.6.3 RISA -3D Version 6.0.1.5 [H:1Jobs 200610612521Calculations\Truss #3 Analysis.r3d] Page 9 12.3 [Page Too Large for OCR Processing] [Page Too Large for OCR Processing] [Page Too Large for OCR Processing] [Page Too Large for OCR Processing] [Page Too Large for OCR Processing] [Page Too Large for OCR Processing]