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J0.06r¢410r- O..LLJ V IV .O.• OOLL• 1.-30..J000 ACCOUNT : (S) RICHCO STRUCTURES SUPPORTING CALCULATIONS FOR DRAWING #M40685 FLORTRUS ANALYSIS: 4/ 6/1983 TRUSWAL SYSTEMS CORP. - MADISON HTS., MI. JOB NAME: FOX CITIES - TULIP- SHAPE: 1 DEPTH AT LEFT: 16. 00" LEFT CANT.: 0. 00" LENGTH: 21'- 11.0" PANEL LENGTH: 60.00" RIGHT CANT.: 0.00" LOADING: 40+ 10+ 5 = 55PSF WEB ANGLE DEG: 23.96 TOP PITCH: 0.00/12.0 SPACING: 24. 0" O. C. 1 PLY BOT PITCH: 0. 00/12. 0 DUR. FACTOR 1. 00 K - WEB CONFIGURATION BRG. 1- 3. 5" @ O'- 0. 0" CODE: WIC 1. 15FB -- USED BRG. 2- 3. 5" @ 21'- 11.0" MEMBER FORCES FROM LEFT TO RIGHT - LD. COND. 1 TOP CHORD BOTTOM CHORD WEBS REACTIONS T 1= -1340 13 1= 0 W 1= 1730 W 8= -250 (V) R 1= 1175 T 2= -1340 B 2= 3126 W 2= -199 W 9= 545 (V) R 2= 1176 T 3= -4395 13 3= 5043 W 3= -1984 W 10= -1119 (H) R 1= 0 T 4= -4395 13 4= 4683 W 4= 1409 W 11= -250 T 5= -5173 B 5= 2046 W 5= -250 W 12= 1808 T 6= -5173 W 6= -719 W 13= -2291 T 7= -3674 W 7= 145 W 14= -119 T 8= -3674 T 9= 0 TOP AND BOTTOM CHORD LUMBER ANALYSIS (TPI74) TOP CHORD: (MINIMUM GRADE ) (1) 4X2 #2 DENSE KD15 S. PINE 1700000 E PAN PITCH L -ACT L-AVG FA(PSI) FB(PSI) AXIAL BENDING SHEAR CSI 6 0.00 2.50 2. 50 1350 2255 0.730 0.253 0.000 0.983 BOT CHORD: ( MINIMUM GRADE ) (1) 4X2 #1 DENSE KD15 S. PINE 1900000 E PAN PITCH L -ACT L -AVG FA(PSI) FB(PSI) AXIAL BENDING SHEAR CSI 3 0.00 5.00 5.00 1250 2695 0.769 0.085 0.000 0.853 WEB ANALYSIS: ALL WEBS 2X4 #3 /STUD KD15 S. PINE DEFLECTION ANALYSIS [LOADING CONDITION 1] : PAN. PT. @ 11'- 5. 7" LL DEFL. - 0. 390" ALLOW. LL DEFL. (L/360) - 0. 712" DL DEFL. - 0. 146" RECOMMENDED CAMBER - 0. 292" TOT. DEFL. - 0. 536" NOTES: REMARKS: NEED WIS. SEAL. PLOT WAS REQUESTED II\ I /\ I /\ I /\ I /\ I ^^ \I/ \I/ \I/ \I/ \II SUPPORTING CALCULATIONS FOR DRAWING # M40685 FLORTRUS ANALYSIS: 4/ 6/1983 TRUSWAL SYSTEMS CORP. - MADISON HTS., MI. JOB NAME: FOX CITIES - TULIP- SHAPE: 1 DEPTH AT LEFT: 16. 00" LEFT CANT.: 0. 00" LENGTH: 21' -11. 0" PANEL LENGTH: 60. 00" - RIGHT CANT.: 0. 00 ' LOADING: 40+ 10+ 5 = 55PSF WEB ANGLE DEG: 23.96 TOP PITCH: 0.00/12.0 SPACING: 24. 0" 0. C. 1 PLY BOT P ITCH: 0. 00/12. 0 DUR. FACTOR 1. 00 K - WEB CONFIGURATION BRG. 1- 3. 5" @ 0'- 0. 0" CODE: WIC 1. 15F8 -- USED BRO. 2- 3. 5" @ 21 ' -11. 0" MEMBER FORCES FROM LEFT TO RIGHT - LD. COND. 1 TOP CHORD BOTTOM CHORD WEBS REACTIONS T 1= -1340 13 1= 0 W 1= 1730 W 8= -250 (V) R 1= 1175 T 2= -1340 B 2= 3126 W 2= -199 W 9= 545 (V) R 2= 1176 T 3= -4395 13 3= 5043 W 3= -1984 W 10= -1119 (H) R 1= 0 T 4= -4395 B 4= 4683 W 4= 1409 W 11= -250 T 5= -5173 13 5= 2046 W 5= -250 W 12= 1808 T 6= -5173 W 6= -719 W 13= -2291 T 7= -3674 W 7= 145 W 14= -119 T 8= -3674 T 9= 0 LUMBER CALCULATIONS: DURATION FACTOR OF 1.00 TOP CHORD AXIAL (P /A /FA) = -5173/ 5.25/1350 = 0.73 TOP CHORD BENDING (M /S /FB) = 750+ 0/1.31/2255 = 0.25 (P /A /FA) +(M /S /FBY = 0.73 +0.25 = 0.98 <= 1.00 BOT CHORD AXIAL (P /A /FA) = 5043/ 5.25/1250 = 0.77 130T CHORD BENDING (M/S/FB) = 300+ 0/1. 31/2695 = 0. 08 (P /A /FA) +(M /S /FB) = 0.77 +0.08 = 0.85 <= 1.00 REQUIRED MINIMIUM PLATE AREAS (SQ. IN.) JOINT# PLATE MEM. AREA MEM. AREA MEM. AREA MEM. AREA MEM. AREA ---wow - - -- - - -- 1 5 -6 T 3. 7 W 1 1.9 2 1 -3 T 1.0 W2 0..5 3 3. 5 -8 T 8. 4 W 3 5.3 W 4 4.0 4 1 -3 T 1.0 W 5 0.5 5 2. 5 -4 T 2. 2 W 6 1. 9 W 7 1. 1 6 1 -3 T 1.0 W 8 0.5 7 3-5 T 4.1 W9 1.6 W10 3.0 8 1 -3 T j.0 W11 0.5 9 - 3.5 -10 T 10.2 W12 5.2` W13 6.1 N 10 1 -3 T 1.0 W14 0.5 11 4 -10 13 8. 6 W 1 5. 1 W 2 0. 5 W 3 5. 3 12 3-8 13 5. 3 W 4 4. 0 W 5 0. 5 W 6 1. 9 13 2. 5 -6 13 1.0 W7 1. 1 11 8 0. 5 W 9 1.6 14 3.5 -10 13 7.3 Wi0 3.0 W11 0.5 W12 5.2 15 3.5 -8 13 5. W13 6.1 W14 0.6 r ----- __ 1 • • M Z 0 co in W \ CD Q .13 .00 —..4 1.__ i t—, C17 .1•11111 ■ {..1 O ri; on a ' li 0 • N //� LL z op ¢ - a - o ^ F— :: W 3 0 J • z N f.L O. I n • W W M • Z Z W 4,.. 1 .. Z d d •-• - x rn to O_ fl-S.? F ~ IA N (!7 Z J.� c •-r O _ _ Ox0 W 3 W � W Y Y O W J V) 1-- W = x u Y W _ W W N x Q °°+� W Z NfAO Wt,� 0 Z Z= x W o .•- x (f) InCILI O O (0 Z > 1 • •-• O O � u a s N N (T) • N 1 U. toN m N N N o • c w x x x .. F-I '., 9 -S'2 o o to to ¢ n) ♦ N H W •-. to r . 1..) (� J = x • Z 0 . ' o u u wz c CC •• J W O m m O a o ta m t W W J J z .. •• O 3 3 > ¢ o J � 1 ZM ■� 0 J QU CD CD .J o u 1- O x x x x Q CC L) I •.00 W 1 m 1- t!) Z Z , m e = 1J¢.z d t.- .. ¢ ¢Jr d0�.-w- lyw. -. yt O O W H 1- II-S ms J¢ :momo J¢o I- to 3 N :::::::::::::: Wi¢J.Z J r_ .W O 11.d WQ¢O1r ¢¢ Or m `' I.tttttt , 0 Wr >Y � mWZ•.O:: ��, 1) , •I� m�rr Z60J \• 3 �I SU O W¢ •• •• 4;1,./ ♦ I W J ^XmWLO • • ♦ d-W.+WO Wr • • .. U OWr •. • J F"• • (/ ¢WUZ ¢r.. .O ¢2 W 2 �¢ •¢NO UO. -ZQri- ¢WW i O • � S • .. Inmr JNOln ^ YI¢� WO W.+ : )• Q 0 • . : ¢ z�J z or m � / J � • O c • mm.. m' LW . • .-•1 • C • Q • � .. Zm � . m -.m ¢ ' • • • O I ;:'g::::;;:;:1:6g O Z W 06Q r F`O ° \ - 9 -� WZWCWW c c.+ I • \ �� t •1Z SU mJ�O ..10 • • •• • JO; m6 O f O0.. I • • , ` U .W.+ W W U O r ._.. ♦ ♦ • • •• � �,, . 00 6� t CZr� ►m WO C OW 7 , �� , i • tn2 0=2Z8-7 r ►Z W i 1: cJ N , ,, ,, ttt., �11' H W UU • 0 tirm1 -.a2 - W IL ¢ JOOW2U ¢ 2 2 ¢W=s-Z¢W /. 4 .. •l roOW m ¢ ¢0o •W m U0 % 10-. W2 ter 0 Z a O QUrW ZZOr.•.2WWI- 0- .x= m WUL L Z CC n WOM -V.m¢L •1,20 . W x MO- >_ . ... w0==inu =¢OQ¢UY • t•. t m Q•f O.+. -r2 .. OOJ� .j ZW.O Y)m*N • QO ON rWJ U O O h¢ ; ^ ^ ^^ O r OWJ WOU W • •IC¢r¢ Q Z >¢SOI 0 F• �md¢� uln ¢... J W Q d/_ Q O rF-Jd a0a=1.8 (N..1 U ¢ iJ ..,p- ¢W WWQWL d181aaa.�r ¢m OZ d0 d O.^.O ZOSMOU> -Om ...F.. CC NON 1 wy.y)N . 0.--, OZW¢O JW OQW W W ZMZ 1 Na......-. 218.0‘11- WC2J¢r2ZLW W h ~ F• 1 la 0 ....=WOWtU0N•- Q.I�..LFZ• L)• W c cc 6.•• 2Z ZLZO ¢W O W CO W WUOF' W •U2.-1 -�ULS W 0 Z 1� N c¢02s.¢¢ ¢..- W ¢dmlum.-mu¢.-msusm¢ _ 1O co d 1 J ¢ 0 1 001.7 ZW Q J 0 i d z 7 0 F'40if -O uS ar • ¢ 2 • W W Z. x lO W¢F.W 0 J 7127 UJU LIWO 0¢ dOU 127 OV1212712 7 1Jl._U W �2F ¢rc Wd M C F • U' IC 7 !!!'=!! Q 1 OOW0 J O WO S rm mU U> 00=0 t2 JF¢ - > u WNO.n O J ZS O .d ZGWGJ J Od IL oam =uW¢¢• Or -=00w Q I.JS N 1.11212.41-.,,, Q.i..W_aOLWU..- m ¢ ZO OZ. - rd. ¢ cu i F•IZWUOZWWOXW. -•O¢Ld m¢t Omd• c..JLO¢ ACCOUNT : (S) RICHCO STRUCTURES SUPPORTING CALCULATIONS FOR DRAWING 40440684 FLORTRUS ANALYSIS: 4/ 6/1983 TRUSWAL SYSTEMS CORP. - MADISON HTS., MI. JOB NAME: FOX CITIES - TULIP- SHAPE: 1 DEPTH AT LEFT: 16.00" LEFT CANT.: 0. 00" LENGTH: 13'- 5. 5" PANEL LENGTH: 60. 00" RIGHT CANT.: 0. 00" LOADING: 40+ 10+ 5 = 55PSF WEB ANGLE DEG: 23.96 TOP PITCH: 0.00/12.0 SPACING: 24.0" 0.C. 1 PLY BOT PITCH: 0.00/12.0 DUR.FACTOR 1.00 K - WEB CONFIGURATION BRG. 1- 3.5" @ 0'- 0.0" CODE: WIC 1. 15FB -- USED BRG. 2- 3. 5" @ 13'- 5. 5" MEMBER FORCES FROM LEFT TO RIGHT - LD. COND. 1 TOP CHORD BOTTOM CHORD WEBS REACTIONS T 1= -1326 B 1= 0 W 1= 1437 W 5= 86 (V) R 1= 712 T 2= -1863 B 2= 1326 W 2= -526 W 6= -661 (V) R 2= 712 T 3= -1863 B 3= 1785 W 3= 593 W 7= -250 (H) R 1= 0 T 4= -1190 B 4= 0 W 4= -253 W 8= 1322 T 5= -1190 TOP AND BOTTOM CHORD LUMBER ANALYSIS (TPI74) TOP CHORD: ( MINIMUM GRADE ) (1) 4X2 #2 DENSE KD15 S.PINE 1700000 E PAN PITCH L -ACT L -AVG FA(PSI) FB(PSI) AXIAL BENDING SHEAR CSI 2 0.00 2.56 2.73 1350 2255 0.263 0.302 0.000 0. 565 BOT CHORD: ( MINIMUM GRADE ) (1) 4X2 #2 DENSE KD15 S.PINE 1700000 E PAN PITCH L -ACT L -AVG FA(PSI) FB(PSI) AXIAL BENDING SHEAR CSI 3 0.00 5.00 4.50 1050 2255 0.324 0.082 0.000 0.406 WEB ANALYSIS: ALL WEBS 2X4 #3 /STUD KD15 S.PINE DEFLECTION ANALYSIS [LOADING CONDITION 13 : PAN. PT. @ 5'- 5.5" LL DEFL. - 0.054" ALLOW. LL DEFL. (L/360) - 0.432" DL DEFL. - 0.020" RECOMMENDED CAMBER - 0.041" TOT. DEFL. - 0. 075" NOTES: REMARKS: NEED WIS. SEAL. PLOT WAS REQUESTED II\ I\ I /\ I /II \I \I/ \I/ ^^ A SUPPORTING CALCULATIONS FOR DRAWING # M40684 FLORTRUS ANALYSIS: 4/ 6/1983 TRUSWAL SYSTEMS CORP. - MADISON HTS.• MI. JOB NAME: FOX CITIES - TULIP- SHAPE: 1 DEPTH AT LEFT: 16.00" LEFT CANT.: 0. 00" LENGTH: 13'- 5. 5" PANEL LENGTH: 60. 00" RIGHT CANT.: • 0. 00" LOADING: 40+ 10+ 5 = 55PSF WEB ANGLE DEG: 23. 96 TOP PITCH: 0. 00/12. 0 SPACING: 24.0 O. C. 1 PLY BOT PITCH: 0. 00/12. 0 DUR. FACTOR 1. 00 K - WEB CONFIGURATION BRG. 1- 3. 5" @ 0'- 0. 0" CODE: WIC 1. 15FB -- USED BRG: 2- 3. 5" @ 13'- 5. 5" MEMBER FORCES FROM LEFT TO RIGHT - LD. COND. 1 TOP CHORD BOTTOM CHORD WEBS REACTIONS T 1= -1326 B 1= 0 W 1= 1437 W 5= 86 (V) R 1= 712 T 2= -1863 B 2= 1326 W 2= -526 W 6= -661 (V) R 2= 712 T 3= -1863 13 3= 1785 W 3= 593 W 7= -250 (H) R 1= 0 T 4= -1190 B 4= 0 W 4= -253 W 8= 1322 T 5= -1190 LUMBER CALCULATIONS: DURATION FACTOR OF 1.00 TOP CHORD AXIAL (P /A /FA) = -1863/ 5.25/1350 = 0.26 TOP CHORD BENDING (M /S /FB) = 893+ 0/1.31/2255 = 0.30 (P /A /FA) +(M /S /FB) = 0.26 +0.30 = 0. 56 <= 1.00 BOT CHORD AXIAL (P /A /FA) = 1785/ 5.25/1050 = 0.32 BOT CHORD BENDING (M /S /FB) = 243+ 0/1.31/2255 = 0.08 (P /A /FA) +(M /S /FB) = 0.32 +0.08 = 0.41 <= 1.00 REQUIRED MINIMIUM PLATE AREAS (SQ. IN.) JOINT# PLATE MEM. AREA MEM. AREA MEM. AREA MEM. AREA MEM. AREA - -- - - -- MEW MEM -- - MOP MIND - - - -- - - -- 1 4 -6 T 3.7 W 1 1.2 - - -- - - -- - - -- 2 2. 5 -4 T 1. 5 W 2 0.9 W 3 1.7 3 1 -3 T J.0 W 4 0.5 4 2 . 5 T 1.9 W 5 1. 1 W 6 1.8 5 1 -3 T ).0 W 7 0.5 6 4 -6 T 3. 3 W 8 3. 7 3-5 13 3.7 W 1 4. 1 W 2 0.9 8 2. 5-6 13 1. 3 W 3 1.7 W 4 0. 5 W 5 1. 1 9 3 -8 13 4. 9 W 6 1.8 W 7 0. 5 W 8 3. 8 I i - - U m Z W CD ic2 O a M . I • ° N ! ■-1 co • N 6 -S�Z r,�t E-2 • . M U) �\ o w %, a.eu•a n .D L.) O %.14.; ri- 21-it r a ° O L N - a vo : E „ o ' C W I M 0� co 21-fi '\ L4 °••. .• 1 4 ) 1 � .,. • 4 • I-M ' E -M W 3 CD E-1 � , 8 -E o J x ' LL i-M = y . 1 Z M 1,J 2 N Q CL a fi S -M J N /n • J N co- N i - „ -.1 1-1 N 0x0 -. vs O O u7 W 3 t!J c = N X o w E -1 ■ 9-5'2 0 stn ° NCC X N W W �}- co zz =xw s o ocic W W H 1 O 1- OO(A2 O I - M mxx • .V. NNm .O / S-M } c- CV CV as fi-5•Z' N 4.4 in o otn LIJ I w . 1 - 1 -. 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Q W .O = 1 W 0 O 20 O• 1 W W ¢LL 020 O Zyy 20 O m0 C W J H 11)2 N 0 mU 00 C L Z m= Q d�W } O•m u C 3 Cu WO d.+ Z O a 00000 O 1 W ZI-¢ a Wa OJOQC.-¢0 O .-,. Z }yj W FO mm.+ •-. 60=00 ..Aryl L d. 0 1.3 1� ¢W ZUJ(J - •LUWmu¢ a Z Z J. CmC 1 .00m.+mylyf... -.yl • ^ .. W JO d 0^ ZU .•W¢ O WQ••W O 0l 1Zl •Z mm • 'l4 g•••• L 1., .m¢WO�¢r¢Wd V) C =■.III W aiOl00 INCN22N I X -MOW a yfW 0 =2 U.• UL1.[ 0 0-I 03515 2 0 35 0.1:0- J 2 00} ^ 0 ¢mW c 00 0} 0 r-¢ 0050 J W..- -- mLL� d W... WW ^m m u•.N•1S 0 ION W .1 W DC • WJx d> • Wtl10N.+0 O U> 0020 0 J U0 1 1 1 1 1 1 1 Ur Wx} U W 2 d TOL Jm0 •d 2 CWO J Zdm -O¢ a N333Z 2 Z3 '- it 5...0 ..J W¢. o. - WmQ..Z O¢ SU¢¢ O.- WOOWO J 0. N J O O J JZ Y W.m.. }W ¢^ O.d YY.• 0 Ua NO =MO N OU 1 ¢ .3 mu J.- QZ O ZOS .-.¢L¢ ..... = ^ ^ T LL MU =00.00. -. N 0 F.O¢}¢VfL. -r °F...., r i mm¢• Omy.• ¢.-.JL0. ;.COUNT : (S) RICHCO STRUCTURES ;UPPORTING CALCULATIONS FOR DRAWING # M40050 fLORTRUS ANALYSIS: 3/23/1983 TRUSWAL SYSTEMS CORP. - MADISON HTS., MI. JOB NAME: FOX CITIES SHAPE: 1 DEPTH AT LEFT: 16.00" LEFT CANT.: 0.00" LENGTH: 24'- 6.0" PANEL LENGTH: 60.00" RIGHT CANT.: 28.25" LOADING: 40+ 10+ 5 = 55PSF WEB ANGLE DEG: 23.96 TOP PITCH: 0.00/12.0 SPACING: 19.2" O.C. 1 PLY BOT PITCH: 0.00/12.0 DUR.FACTOR 1.00 K - WEB CONFIGURATION BRG. 1- 3.5" @ 0'- 0.0" CODE: WIC 1.15FB -- USED BRG. 2- 3.5" @ 22'- 0.0" SPECIAL CONDITIONS: DOUBLE VERTICAL AT 19'- 6.0" - LOAD OF 860 LBS. ADDITIONAL LOADING: CANTILEVER LOAD AT 24'- 6.0" OF 127 LBS. MEMBER FORCES FROM LEFT TO RIGHT - LD. COND. 1 TOP CHORD BOTTOM CHORD WEBS REACTIONS T 1= -1909 B 1= 0 W 1= 2121 W 9= 255 (V) R 1= 1031 T 2= -1909 B 2= 3343 W 2= -200 W 10= -714 (V) R 2= 2079 T 3= -4363 B 3= 4754 W 3= -1592 W 11= -218 (H) R 1= 0 T 4= -4363 B 4= 4786 W 4= 1132 W 12= 1340 T 5= -5015 B 5= 2925 W 5= -165 W 13= 20 T 6= -5015 B 6= 2925 W 6= -487 W 14= -3751 T 7= -4142 B 7= 0 W 7= 289 W 15= -197 T 8= -4142 W 8= -200 W 16= -507 T 9= 452 W 17= 9 T 10= 452 • MEMBER FORCES FROM LEFT TO RIGHT - LD. COND. 2- TOP CHORD BOTTOM CHORD WEBS REACTIONS T 1= -1927 B 1= 0 W 1= 2140 W 9= 235 (V) R 1= 1039 T 2= -1927 B 2= 3378 W 2= -200 W 10= -695 (V) R 2= 1919 T 3= -4414 B 3= 4817 W 3= -1611 W 11= -218 (H) R 1= 0 T 4= -4414 B 4= 4883 W 4= 1151 W 12= 1320 T 5= -5095 B 5= 3057 W 5= -165 W 13= 20 T 6= -5095 B 6= 3057 W 6= -501 W 14= -3732 T 7= -4256 B 7= 0 W 7= 308 W 15= -121 T 8= -4256 W 8= -200 W 16= -339 T 9= 303 W 17= 9 T 10= 303 TOP AND BOTTOM CHORD LUMBER ANALYSIS (TPI74) TOP CHORD: ( MINIMUM GRADE ) (1) 4X2 #2 DENSE KD15 S.PINE 1700000 E PAN PITCH L -ACT L -AVG FA(PSI) FB(PSI) AXIAL BENDING SHEAR CSI 8 0.00 2.63 2.56 1350 2255 0.601 0.342 0.000 0.942 BOT CHORD: ( MINIMUM GRADE ) (1) 4X2 #2 DENSE KD15 S.PINE 1700000 E PAN PITCH L -ACT L -AVG FA(PSI) FB(PSI) AXIAL BENDING SHEAR CSI 4 0.00 5.00 4.56 1050 2255 0.886 0.068 0.000 0.953 WEB ANALYSIS: ALL WEBS 2X4 #3 /STUD KD15 S.PINE DEFLECTION ANALYSIS [LOADING CONDITION 27 : PAN. PT. @ 11'- 7.5" LL DEFL. - 0.464" ALLOW. LL DEFL. (L/360) - 0. 725" DL DEFL. - 0. 197" TOT. DEFL. - 0.661" NOTES: 0=MAPU . I.tTG q:AI SUPPORTING CALCULATIONS FOR DRAWING #1440050 FLORTRUS ANALYSIS: 3 /23/1993 TRUSWAL SYSTEMS CORP. - MADISON HTS. , MI. ,JOB NAME: FOX CITIES SHAPE: 1 DEPTH AT LEFT: 16. 00" LEFT CANT.: 0. 00" LENGTH: 24'- 6.0" PANEL LENGTH: 60.00" RIGHT CANT.: 28.25" LOADING: 40+ 10+ 5 = 55PSF WEB ANGLE DEG: 23.96 TOP PITCH: 0.00/12.0 SPACING: 19.2" 0.C. 1 PLY BOT PITCH: 0.00/12.0 DUR.FACTOR 1.00 - K - WEB CONFIGURATION BRG. 1- 3.5" @ 0'- 0.0" CODE: WIC 1.15FB -- 'USED BRG. 2- 3.5" @ 22'- 0.0" SPECIAL CONDITIONS: DOUBLE VERTICAL AT 19'- 6.0" - LOAD OF 860 LBS. ADDITIONAL LOADING: CANTILEVER LOAD AT 24'- 6.0" OF 127 LBS. MEMBER FORCES FROM LEFT TO RIGHT - LD. COND. 1 TOP CHORD BOTTOM CHORD WEBS REACTIONS T 1= -1909 B 1= 0 W 1= 2121 W 9= 255 (V) R 1= 1031 T 2= -1909 B 2= 3343 W 2= -200 W 10= -714 (V) R 2= 2079 T 3= -4363 B 3= 4754 W 3= -1592 W 11= -218 (H) R 1= 0 T 4= -4363 B 4= 4786 W 4= 1132 W 12= 1340 T 5= -5015 B 5= 2925 W 5= -165 W 13= 20 T 6= -5015 B 6= 2925 W 6= -487 W 14= -3751 T 7= -4142 B 7= 0 W 7= 289 W 15= -197 T 8= -4142 W 8= -200 W 16= -507 T 9= 452 W 17= 9 T 10= 452 MEMBER FORCES FROM LEFT TO RIGHT - LD. COND. 2 TOP CHORD BOTTOM CHORD WEBS REACTIONS T 1= -1927 B 1= 0 W 1= 2140 W 9= 235 (V) R 1= 1039 T 2= -1927 B 2= 3378 W 2= -200 W 10= -695 (V) R 2= 1919 T 3= -4414 B 3= 4817 W 3= -1611 W 11= -218 (H) R 1= 0 T 4= -4414 B 4= 4883 W 4= 1151 W 12= 1320 T 5= -5095 B 5= 3057 W 5= -165 W 13= 20 T ..6= -5095 B 6= 3057 W 6= -501 W 14= -3732 T 7= -4256 B 7= 0 W 7= 308 W 15= -121 T 8= -4256 W 8= -200 W 16= -339 T 9= 303 W 17= 9 T 10= 303 LUMBER CALCULATIONS: DURATION FACTOR OF 1.00 TOP CHORD AXIAL (P /A /FA) = -4256/ 5.25/1350 = 0.60 TOP CHORD BENDING (M /S /FB) = 1011+ 0/1.31/2255 = 0.34 (P /A /FA) +(M /S /FB) = 0.60 +0.34 = 0.94 <= 1.00 BOT CHORD AXIAL (P /A /FA) = 4883/ 5.25/1050 = 0.89 BOT CHORD BENDING (M /S /FB) = 199+ 0/1.31/2255 = 0.07 (P /A /FA) +(M /S /FB) = 0.89 +0.07 = 0.95 <= 1.00 REQUIRED MINIMIUM PLATE AREAS (SQ. IN.) JOINT# PLATE MEM. AREA MEM. AREA MEM. AREA MEM. AREA MEM. AREA 1 4 -8 T 5. 3 W 1 1.7 2 1 -3 T /.0 W2 0.5 3 3 -8 T 6.9 W3 4.3 W4 3.3 4 1 -3 T /. 0 W 5 0. 5 5 2.5 -4 T . 1.9 W6 1.3 W7 1.1 6 1 -3 T /. 0 W 8 0. 5 7 2.5 -4 T 2.4 W9 1.1 W10 1.9 8 1 -3 T •1. 0 W11 0.5 9 4 -12 T 12.7 W12 3.8 W13 1.0 W14 10.0 10 2 -3 T 1 0 W15 0. 5 11 2.5 -5 T 1.3 W16 1.4 W17 1.2 12 4 -10 B 9.3 W 1 6. 1 W 2 0. 5 W 3 4. 3 13 2.5 -8 B 4.0 W4 3.3 W 5 0.5 W6 1.3 14 2.5 -6 8 0.2 W7 1.1 W8 0.5 W9 1.1 15 3 -8 B 5. 1 W10 1.9 W11 0.5 W12 3.8 16 2 -3 B 1 0 W13 1.0 17 4 -12 B 8.5 W14 10.1 W15 0.5 W16 1.4 18 2 -3 13 ,/.0 W17 1.0 • • . - ' -� ' ' ' ' ' , / i / - _ ^/ /, __ ~.��__ - _ �__��_ __�__'��-��^�� ~ ^ -' ` / i «�- - Ali. � �� °�~~ � __'/__-- �������� . .... _ _ ...... .C4.1"LAO .. _ . -414....4.1....r1.211).42P 1 / .e_c4 . ____ ..... • .."' � __-�-__-___-__-_� ________-_-�___'___ ______^ -__-__�___-_ --_-__ _-_-_- ~^-____-______-__ ^______---___-__-____-______--___ �___�_ _-__-__��__�_____�_- -_--____-__.__ ___ _____.___-_-�--__ _ __-___.__-__-^__--�__�- ____' ______-____�_-___-_-__^___'____ . 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