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Home My WebLink About05040226-Truss Info912 912 8 2×4// G DG 18-00-02 HO 4-07 2 E Si D 4x6~- 3x6~ 4x6~- 3x5~ 00 LATE~L Bp~CING: TOP CHORD ~ CONTINUOUS BTM CHORD * CONTINUOUS TRUSS SPACING · 24.0 IN LOAD CASE ~1 LUMBER STRESS INCREASE; 15.0% PLATE STRESS INCREASE: 15.0% LOADING LIVE DEAD {PSF WIDTH HOR RIGHT p(LRSI M~iST M~2ND TOP CHORDS .68 1581 C 1316 -370£ 85 t35 -3700 G-C 0.66 1581 C 3700 -13L6 BOTTOM CHORDS 1328 T 377 -2094 DL+LL DEPL = 0.27" IH LL DEFL = 0.05" < BRG-SPANZ360 SPAN/DEFL (DL+LL = 999 PLATING CONFORIdS TO TP/ GROSS AREA METHOD: VERIFY PLATE VALUES WITH TEE-LOK CORROR.ATPON GRIP BASED ON SYP LUMBER PLATES ~ 20 GAUGE TL-20 GRIPPING 561-393 PSI PER PAIR B 30lQ S.O0 X 6~00 CTR 2,2 C 2001 3.00 X 6.00 ~,6 2~6 D 1010 4~00 X ~ 00 ~CTR CTR E 1010 4,00 X 6,00 CT~ CTR F 1OOI 2.00 X 4~00 CTR CTR G 1001 2 00 X ~.00 CTR CTR DAVIDSON INDUSTRIES 2~ ANALYSIS CONFOE~S TO UBC (ANSI TPI 1~1995 T~USS IS DESIGNED AS A MAIN WIND-FORCE RES SYSTEM LE EL.B ZRASC367 14-09-12 14-09-12 29-07-08 E 2x4 UniStar -- Version 40,O.IiB RUN DATE: 2- 6-00 CSI SIZE LUMBER i.t5FB TOP 0.63 2X 4 SP-~2 1720 BTM 0.80 2X 4 SP-~2 1720 WBS 0.73 2X 4 SP-~3 980 EXCEPTIONS: LATERAL BRACING TOP CHORD - CONTINUOUS BTM CHORD ~ MAX DIST FOR THE FOLLOWING MEMBERS IS 99 IN. A-F P-D MAX DIST FOR ALL OTHER MEMBERS IS 120 IN. TRUSS SPACING - 24.0 IN LOAD CASE #1 LUMBER STRESS INCREASE: 15.0% 0 .£ [TBRIA TYPE HORZ VERT WIDTN LBS LBS IN -SX PIN 0 1237 3 ' HOEZ RLR 0 1237 3- RIGHT MEMBR CSI R(LBS) M@iST M@BND TOP CHORDS 0.63 3051 C 3031 -2711 OVERttANGS 9i2 0 HO 4-07 8 2x4\% G 4x4 -- ASHVILLE EL.B ZRASC367 DG HO $415 _/~TRUSS"~_f"REou~RES TOP CHQRD SCAB TO BE FIELD APPLIED PER ~OTE ~ BELOW, 5X6~ E RUN DATE: 3 29-00 CSI SIZE LUMBER 1.15FB LATERAL BRACING: TOP CHORD - CONTINUOUS BTM CHORD - CONTINUOUS TRUSS SPACING ~ 24.0 IN DTH LBS IN-S~ LEFT RIGHT HEEL 0IN - 3EX 0IN - 4EX E 200i 5.00 X 6 00 4.~ 3.5 NOTES: DAVIDSON INDUST[IES 2. ANALYSIS CONFORMS TO 3. BUILDING DESIGNER IS RESPONSIBLE FOR ADEQUATE PLATE CONNECTION WHICH ALLOWS 0.55 INCHES OF HORZ. MOVEMENT AT JOINT D 4 FASTEN EACH ADDED SCAB W! 1740 C O 0 2032 C 0 52929 E-D 0.68 581 C-5292~ O BOTTOM CHORDS OCT 19 ~ 10-02-08 HO 6-01 ASR%tILLE EL.B ZP~%S DG 15~05~13 RUN ~ATE: 3-29-00 2X 8 SP2250MS 2250 EPTIONS: NOTES: · TRUSSES MANUFACTURED BY - DAV I DSON INDUSTRIES 2. ANALYSIS CONFORMS TO UBC (ANSI TPI 1-1995). 3. EFPIRICAL ANALOG IS USED. BLOCK-J~_ LONG REQUrP~D AT BEARING XT JOINT(S} _~_~_' LOCATE AS SHOWN WITH-~LO~K TIGHT AGAINST BEARING. NAIL BbOCK IO tRUSS WITH (J~) OCT 19 2000 67 Version 40.0.112 DATE: tOP 0 36 2X 4 SP~2 1720 LATERAL BRACING TOP CRORD - CONTINUOUS BTM CHORD - CONTINUOUS TRUSS SPACING - 24.0 IN LOAD CASE ~t LU~BEE STRESS INCREASE: 15.0% PLATE STRESS INCREASE: 15.0% LOADING DEAD (PSF JT REACT WIDTH LBS IN-SX A 906 3- 8 TRUSS CONTAINS SHORT CANT- 536 MEMER CSI P(LES) M~iST M@2ND D-F 242 C DL+LL DEFL = 0.29" IN L DEFL - 0 03~ < BRG-SPAN/3S0 SPAN/DEFL (DL+LL) ~ 999 PLATING CONFC~MS TO TP1 (GROSS AREA METHOD VERIFY PLATE VALUES WITH TEE~LOK CORPORATION GRIP BASED ON SYE LUMBER PLATES - 20 GAUGE. TL, 20 GRIPPING 561-393 PSI PER PAIR 'INCLUDES 15~0%INCEEASE TENSION 1090- 924 PLt' 9ER PAIR SHEAR 970- 49~ PLI PERPAIR 3T tYPE PLATE SIZE X Y h 2002 5,00 X 6,00 2.2 2 2 TRUSSES ~ANUFACTGRED BY DAVIDSON IMDUSTRIES 4, ~IND LOADS ~ UEC, 1989 EDITN TRUSS IS DESIGNED AS A _ o NO, 60910419 s ~ OCT 1 ~ ZRASC367 HO 4-13 Si D 3x10 20-11408 00 REACT WIDTH JT REACT WIDTH TRUSS CONTAINS SHORT CANT. OUTSIDE FACE OF EARING J~C 0 .9 BOTTOM CH( A F-SI 0.86 052 WEBS C F-H = 2039 T OCT ! 9 200O 3X4~ D CSt SIZE LUMBER 1.15FB pLATING CONFORMS TO ~GROSS AREA METHOD). VERIFY PLATS VALUES WITH TEE-LOK CORPORATIO5 GRiP BASED ON SYP LUMBER PLATES - 20 GAUGE GRIPPING 561-393 PSI PER PAIE INCLUDES 15~0~ INCREASE NOTES: 2. ANALYSIS CONFCRMS TO 3. EMPIRICAL ANALOG IS USED. RIGHT MEMBR CSI P LBS M@iST M,~2ND TOP CHORDS 985 C 91 -1626 729 I 1626 -810 ) C 810 ~1626 ~0 985 C 1626 -91 SOTTOM SPAN/DEFL {DL+LL = 999 2 4.3 :L.B ZRASC367 HO 4-07 5x8~ UniStar ~- Version 40~0~112 RUN DATE; 2- * 2-PLY TRUSS I SIZE LUMBER FR TOP 0,75 2X 4 SP-~ 1500 PLATES AR5 FO~ EACH PLY PLATING CONFORMS TO TPI (GROSS AREA METHOD VERIFY PLATE VALUES WITH TEE-LOK COEPCtATION BTM 0.79 2X 6 SP2250MS 2250 WSS 0.45 2X 4 SP-~2 1506 LATERAL BRACING: TOP CHORD - CONTINUOUS RTM CHORD - CONTINUOUS TRUSS SPACING - 24 0 IN. LOAD CASE ~1 LUMBER STRESS INCREASE: 15.0% GRIP BASED ON SYP LUMBER PLATES - 20 GAUGE TL*20 850 GRIPPING 561-393 PSI PER PAIR INCLUDES 15-0% INCREASE TENSION 1030~ 924 PLI PER PAIR SHEAK 97)- 498 PLI PER PAIR JT TYPE PLATE SIZE X Y A 2015 5 00 X $ 00 7,2 4.6 B 3010R 5.00 X 6.~0 2.5 CTR C 2015 5 O0 X 8.00 7.2 4.6 D 1010R 3 00 K1£.00 CTR CTR E 1)iOR 3.00 XI0.O0 CTE CTE F 1001 2 00 X 4.00 ~TR~ CTR G 1001 2,00 X 4.00 CTR CTR Si 1100 5.00 X 6.00 CTR 8.2 R = PLATE IS ROTATED BY 90 DEG LEFT RIGHT HEEL C~N - 4SX OIN - 4SX MEMBER FORCES * EACH PLY MEMBR CSI P(LBS) M~tST M@2ND TOP CHORDS A~F 0.75 3846 C ~1708-818 E-B 0 41~798 C 810 NOTES: 1. TEUSSES I.L~NUFACTU~ED BY - DAVIDSON INDUSTRIES ~ ENPIRICAL ANALOG IS USED 4. WIND LOADS USC, 1988 EDITN TRUSS IS DESIGNED AS A MAIN WIND-FORCE RES SYSTEM OCT 1 9 2000 CSI SIZE LUNBER 1,15FS TOP 0.36 2X 6 SP-~i 1900 ~TM 0.28 2X 6 SP-~t i900 BS 0.08 2X 4 SP-~I 980 LUMBER STRESS INCREASE: 15.0% REPETITIVE MEMBER STRESS USED- LATERAL BRACING: TOP CHORD - CONTINUOUS BTM CHORD - CONTINUOUS LOADING LIVE DEAD (PSF) TOP CHD 20,0 10 0 BTM CHD 0.0 1] 0 PLATING CONFORMS TO TPI (GROSS AREA METHOD) VERIFY pEATS VALUES WITH TEE~L]K CORPORATION GRIP BASED ON SYP LUMBER PLATES - 20 GAUGE TL-2( JT TYPE PLATE SIZE X Y A 2005 ].00 X 4.00 5.0 4.£ B 3001R 3.0) X 6.00 CTR CTR C 2005 3.00 X 4.00 5.0 4.[ D 1001 ] DO X 6.00 CTR CTR PLATE rS ROTATED BY 90 [EG NOTES l. TRUSSES MANUFACTURED BY - DAVIDSON INDUSTRIES 2. ANALYSIS CONFORMS TO USC (ANS]/TPI 1-t995). 3. EMPIRICAL ANALOG IS USED. 4. ANCHOR TRUSS FOR A IOTAL HORIZONTAL LOAD OF 138 LBS. SUPPORT CRITERIA JT REACT WIDTH JT REACT WIDTH LBS IN'SX LBS IN-SX A 538 3- 8 C 1210 l- 8 LEFT RIGHT MEMSR CSI PfLBS) M~IST M@2ND -827 D'C 0.28 470 T 1501 365C WEBS D-B = 225 T DL+LL DEFL = 0,05" IN B'C LL DEFL = 0.00" < BRG~SPAN/36f SPAN/DEPL (DL+LL = 999 OCT 1 9 2000 T