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9926 (SFD) Structural Calcsthe flying buttress IL SHEET 72-757 Fred Waring Drive, 1/5 BY 17� DATE �qo W. 0. NO. q D — Zl4 Palm Desert, CA 92260 CKD DATE JOB �TRA1"F+��rL (619) 346-5445 oiQC�i-t7��� R� DFsnJG� rz�w 7-3-91 PREPARED' FOR: STF�QTi L: �, C�NSTI=UGTIohi c -lo 7z+- 4 1- 4-41- 0161+7 'e�c'hlo� bovT spn�-t:Nt�- af` l.l� l.otyp 41112, 1(�'`i41Iz P -.,I - GSI LI NCS l.o�C�s� 40 uoL 10,0 P- f% Io�;'Li IoIJ (,o rli�. I -21%b* J i, L_ I u L I.o '><;) 1 0• D P6•r- l.l� l.otyp 41112, 1(�'`i41Iz P -.,I - GSI LI NCS l.o�C�s� 40 uoL 1 , 7 PAF Io�;'Li IoIJ (,o rli�. I -21%b* J i, L_ I u L I.o '><;) 1 0• D P6•r- I `18e> j ec- the flying buttress " SHEET 72-757 Fred Waring Drive, //5 BY ORP DATE _ `10 W.O. NO. X10 -214 el Palm Desert, CA 92260 CKD ___DATE JOB �y (619) 346-5445 _ i PREPARED' FOR: �w 8 o. 1375 UJOL-, f�'l.Ywo WINS �= c" c�:"Tss 0,7- 4 1, -5 I (o PSF ICU ri 1 �- -r, - iox��f . pc t P sT>zew (T4 IEPi - 3� rpt,. ►?1r't s b)�s� P I-'� 135o 85 I��Ti�il�- ► 45b � l,7 � ►nom r�r`� �*Z o A] No. 33446 Exp, 6.30.94 M. 11 ov W -1 -AIN IV 4/3 � 108-1'1..TI_E: ;�rROfIIER C:CJN �RUC:fICJtJ PLAN ' NAME CALIFORNIA RANCH I -SE DA'r[:: 1. /0N,/90 0PERAT0R NP)IlF 1.,1,111 .4; :t::{::{: V: j: A: * ;{; :}; * "J." :4: ;K'A::}; .A::V I' :i,. *3: * .k if: f::4- A :}'- :4.- .4; :4::A' if. k'. *A: :}::}: ;4: :4::4: A: 3: =001` RAFTERS R1 OVER --ALL LENGTH: :3.1.60 ROTS AT: 4.20 31..60 APPLIED LOAD,-.; ( DOWN -I-) 42 FROM 0 TO 4..19 P'TL LOAD #/LF 32 FROM 4 . 1.9 TO 31 .. P' TL LOAD #/I._F RE: -:ACTIONS (UP .J_ ) : . . LEFT- 628.2 RIGI-IT :. 4.2 4 , 9 � * l_18E NO.1. DFL_ 4•X:.1.4 A= 46.3/-75 8= 10�'.. 41..1. 1.-- 678.476 3 _ 1&d a �. 29-"o L FV= 9.5. E=.1800000. DF=.1...25 CRIT SHEAR = 41.7. AT 5.. 30 1 . 5*V/ (A*FV*DF) = 11. L_F'i CANT MAX MOrI = •::)70 ., FT. 1_.80 AT 4. 20 FB = 1.731... ISI/ ( FB*S*DF) _ .01-1 DEFI_. = 14 AT 00 {._,r .=, a0 ,. SPAN MAX MOM = 282 .1 „ FT . I...BS AT 1.8...32. 1=B=:1.73.1 .. M/ ( FB*S*DF) _ .15 DEFL.= .31: AT 1.8.c)3 L.../36,C,..= ,.91 A v _wOE�S No.33446 �e Exp.6.30.9� a, ROOF RAFTERS R2 \F OF L%% OVER—ALL. LENGTH: 31;. 60 ROTS AT: .. 00 .1.6.90 27 . 40 APPLIED LOADS ( DOWN +) 4.:3 FROM O TO 1.6.39 P'TI._ LOAD #/LF 55 FROM 16.. 89 TO 3.1..6 P' TL LOAD #/LI REACTIONS ( UP + l I.._EF`r : '95.6 MID: 792 .. 72 RIGHT : 457.0 *y } IJ E N0.1. DFL. 2X A= 10.375 S== 1.•:3 .. 1.11 .1 1: = _i 7 , 63)5 F V 7 9 CD .. E'7-1800000. f)F :: . . CRIT SHEAR = :1.04.. Al' 1.6.30 1.. 5*V/ (A*FV*DF) = 47 L.FT SPAN MAX MOM = .11.4.4 . F- "f" . L_ 1-.;S AT 161. 90 1=13 =1.750. M/ (FB *S",DF) ., 48 DE::FL_.= 52 AT 7.67 L_/ 36C) . = S6 1 s RGT SPAN MAX MOM = 1.144.. Ff„L8S AT 16„90 FB =1 7 50 . M/ (FB*S*DF) _ .. 4L=! 10,5 DEF-- L = .06 AT 20 .. 23 L_ / 360 :. 35 4, Z RGT C.AN'f MAX MOM = 485. FT. LBS AT 2.7.40 1:8=.17.50.. M/(FB*S*DF)= ..20 DFFL.. = .. 13 AT 31.. 60 1.-/',6C) 1 4 ROOF RAFTERS R;;. OVER-ALL LENG-fI-i: 12 . 86 ROTS AT : 3.86 12.86 APPLIED LOADS ( DOWN +) 34. UNIF LOAD #/L.F REACTION (UP r ) I_..EFT : 77.1..8 RlGI IT : 508., `S SJ- N 01. [r L:: I .. 2 X 1. A= 1= 16.8-75 ._> .= .._> .1... 6 el. l I.:. 1, '771 . i a r=V= 95.. E=180000?0,. DF=1.. C l'ZIT SI-IEF;R = 361` .. r'1'1 i . ,:afi 1.., 5*V/ (A*FV*DF) _ .. 2.8 L- F" T C: A N T MAX MOM = N:.. F T . L.: B S A'T 3 . F.-3 6 FB=.1750. M/ ( FB:+: :cDF):7 .. 1. .1 Py DEFL = C)O AT 2 . OF, 1...1/360. - 1.:s SPAN MAX MOM = 626. F"T",.I._.=.S A•1 3„86 F8=1750. M/( FB*S3DF) _. 1 i. DEFL= ,.h2 AT 8.78 I__/360,. ..30 No. 33446 Exp, 6.30.94 TF F C.)VFR•-•AL_.I_. L...ENGTFI = 44. • 00 i,C l ° AT : 6 ,.00 20 .. 00 44.00 APPLIED LOADS ( DOWN +) 0 AT 0 532 AT 441 P'TL.. L 001) #/LF REACTIONS (UP +): I....EFT :1. 73.0 MID: 7426.. 43 RIG1-IT : 4450.6 Y'.P• W�. C1F;E N01_ DFL_ _:X.16« /a= 85,25x, 5_ 22c:),<'_2? f.= 1.7C)6,..77h F V = J3 c> . E: =1 600000. D F:: ].. (K) CRIT SHEAR = 45.13. AT =_'1.,,'_":? 1...5*V/(A*FV*DF') _ .93 L.1:: r CAN r rfA:>: f'101`1 = 4:' `:, . "'T. L...B; Al 6 . 00 F8--131" .. M/ (F8*l:,*DF )= 01-1 4- DEFL= •-.:11. AT .00 L._/360. = 20 I_F T SPAN MAXMOM = 1854-4. FT. LBSAT 20.00 FB=.131:'. M/(FB*S*DF)= .77 DEF"I.._= „ 1.0 AT 14.50 L/360 „ _ ..4-7 RG f `SPAN MAX MOM 2.00i::): , .. r- r . L..B<> h T 34 . t:,4 � p�ESSIp F 8 =:1.312 ,. rl/ (FB*S*DF) '25 = .83 Q A DEFL= - . c.,4 AT 33. I._./;360 . _ .80 No. 33446 Exp, 6.30.94 TF F HIP B OVER-ALL LENGTH: 14.50 ROTS AT: 3.50 APPLIED LOADS (DGWN +) 646 REACTIONS (UP .14.50 UNIF LOAD #/L_F LEFT: 6173.7 RIGHT: 3L93-1) -1) ****** USE NO.1 Df=L. 6X.12 A= 63.250 S= 12.1„229 T= 697,.068 FV= 85. E=1600000. DF=1.00 CRIT SHEAR = 3294.. AT 4..46 1.,S*V% (A*FV*DF) _ LFT CANT MAX MOM = 3957.. FT.LBS AT 3.50 FB=1350„ M/(FB*S*DF)= 29 DEFL= .10 AT .00 L./360.= .12 :.SPAN MAX MOM = 7893. 1= T . LBS AT 9.56 FB = 1350 , M/ (FB *S*DF) _ SE-; DE_FL._= 14 AT 9..25 L/360.= .37 .92 HIP OVER-ALL LENGTH: 29.00 ROTS AT: 7..00 29,.00 APPLIED LOADS ( DOWN f) 0 AT 0 4.1.8 AT 29 P' TL LOAD #/L_F REACTIONS (UP +): LEFT: 2663,.2 RIGHT: 3397..8 ****** USE 24F GLM 5.125X 19.5 ****** A= 99.938 S= 324 .. 797 I= 3166.770 FV=165. E=1800000,. DF=1. 00 CRIT SHEAR = 2737.. AT 27.38 1..S*V/(A*FV*DF) _ LFT CANT MAX MOM = 824. FT . L..BS AT 7.00 FB=2274., M/ (1=B*S*DF) = .0.1 DE:.FL. = .22 AT .00 L./ 360. _ .23 SPr1N MAX MOM = 154813.. c l .L...BS AT 19,.23 FB=2274,. M/(FB*S*DF)= 25 DE:FL._= -.23 AT .1.8.33 L/360.= ..73 ,.25 ^ HIP [ OVER-ALL LENGTH- 20'00 R(�TS AT9'00 20'00 APPLIED LOADS (DDWN +) 456 UNIF LOAD #/LF REACTIONS (UP +)� LEFT: 8290'9 AIGHT: 829'l USE 24F GLM 5.125X 18'0 A= 92'2-50 S= 276'750 I:= 2490'750 FV=165. E=1.800000' DF=l'O0 CRIT SHEAR 3503' AT 10'50 1'S*V/(A*FV*DF) '35 LFT CANT MAX MOM 18468. FT.LBS AT 9'00 FB=2294' M/(F8*S*DF5 DEFL= -'29 AT '00 1 360. 30 SPAN MAX MOM l8468FT,LQS AT 9'00 FB=2294. M/(F8*S*DF)-- .35 DEFL= '02 AT 12'50 L/360'= '37 HIP E OVER-ALL LENGTH- 40'00 r,CTS AT- 3'00 17'00 29'50 APPLIED LOADS (DOWN +) 532 AT 0 0 AT 40 P'TL LOAD #/LF REACTIONS (UP +)� LEFT4287'0 MID4 6 RIG'IT: 1680'3 NO). DFL A� 63'250 S1.2l.�29 L� 697068 FV= 85'E�1600000' $F=l.00 CRIT SHEAR 253C,' AT 16'04 1'5*V/(A*FV*DF) '}l LFT CANT MAX MOM 233 4. FT'LBS AT 3'00 F8=1350' M/(FB*S*DF)= 'l7 DEFL= '09 AT '00 L/360.= -10 LFT SPAN MAX MOM = 5966' FT, LBS AT 17'O FB=l35O. M/(FB*5*DF) '44 DEFl- 1.5AT q.50 L/3�0.� �47 A�T SPAN MAX MOM = 5966' FT. LBS AT 17., 00 F8�l350' M/(FB*S3-DF) 44 bEFL02 AT 20'42 1-/360.� '42 c 1114 ' QGT OANT MAX MOM � �S�6' FT.LBS AT 29'5O FB --135O. M/(FB*S*DF)� .lq DEFL= -- 18 AT 40'00 L/3. 0.� '�5 HIP F OYER -ALL LENGTH-. 43'0O R, TS AT8.00 24'0O 3` '0O APPLIED LOADS (DOWN +) 266 AT 0 0 AT 24 P'TL LOAD #//LF 1,90 AT 24 0 Al 43 `P'TL LOAD #/LF RIEACTIONS ((JP +)� /P: f - r' I :�9 A MT r) 9q7'8� �I�HT� 839'5 ^ HIP G UVEA -ALL LENGTH: 12l'00 RCTS AT APPLIED LOAD3 (DOWN �) 3O4 R`EACTI0N3 (UP +)� '32 6'00 2l'00 UNIF LOAD #/LF LEFT- 4488'8 QIG-IT 0FL 6,X16 USE A. 86'250 � S� �20'229 l� 1706'776 82'7�9 I� �92'q64 FV 85' E 3. 600000 DF�l.O0 CRIT SHEAR `2404' Al" b'79 0QIT F;!AF AP 1,531:` MAX MOM 5472. 5AV/(Al, FV*DF) ` LFT CANT MAX MOM 7566 FT'LB DEFL= .12 AT 8., 00 FB�l3l2 M/(FB*5*DF)� MOM � t03�' F1' Al 1.4'70 FB_-l35O' M/(FB*S*DF DEFL= -'23. AT 'O0 60'� AT 14.OR '27 '50 LFT SPAN MAX MOM 7566. FT'L8S Al 8.00 F8=1312' M/(FB*3*DF 33. DEF[_ 04 AT 13.67 L/6O 53) RGT SPAN MAX MOM '22l FT.LBS AT 30'04 C��13i2' M/(FB*S*DF)� '09 DEFL= -'02 AT 30.33 L/360. 42z) R GT CANT MAX MOM = 360' FT'L6/ AT 37'00 F8=1312. M/(F8*S*DF 01. DEFLm, 'O3 AT 4 O0 L/1560'= .Z0 HIP G UVEA -ALL LENGTH: 12l'00 RCTS AT APPLIED LOAD3 (DOWN �) 3O4 R`EACTI0N3 (UP +)� '32 6'00 2l'00 UNIF LOAD #/LF LEFT- 4488'8 QIG-IT 1.n1.52 USE N01 DFL 6Xl0 82'7�9 I� �92'q64 FV 85' E 3. 600000 DF�l.O0 CRIT SHEAR `2404' Al" b'79 l'5-rV/(A*FV*DF) � LFT CANT MAX MOM 5472. FT'LBS AT 6'O0 F8=1350' M/(FB*S*DF)= '59 DEFL= .12 AT '00 L/36O' 20 3PAN MAX MOM � t03�' F1' Al 1.4'70 FB_-l35O' M/(FB*S*DF 65 DEFL= -'34 AT 14.OR L '50 '8l v t 1`JERA ...._ LENGTH: 27.00- POTS AT: 7.00 � OO APPLIED C_ `:� (DOWN + 0 AT 0 336 AT 7 � W TL LOAD #/ LF REACTION a (UP + LEFT: 2041.2 RIGHT ; 2494 4170.7 *� ** USE 24F GLM 5.125X 19.5 A= 99.938 A= 60.375 S= 173.578 � 1..�' 7 ,. 1.1.1. FV= 95. E= .1.800000. ^.5.. _ 2 - 5- 56 KV/ (A*F'V*DF) - ..42 CRIT SHEAR = 2025.. /f1 3218. AT 21.38 LFT CANT MAX ' M = 711. C= 'C .. I__ "": AT 7 .. 00 C -=B=144:.1. I/ (F'B*S*DF) = 03. FB=2274.. DEFL= . 28 AT 00 L../360. _ ..23 ;PAN MAX MOM = 10359. FT .. 1._BS AT 18.:1.1 FE''= 41 . M/ ( FES*S*DF) = .40 / 3t� 0 = 67 u�� DL -FL, = 27 AT17.33 4.... .. .. VALLEY C' OVE:R•••AL...L... LENGTH: 29.00 ROTS AT: 4.00 23.,00 APPLIED LOADS ( DOWN 4 ) 0 AT 0 608 AT 23 P'TL LOAD #/LF REACTIONS (UP +)z LEFT: 2821.3 RIGHT: 4170.7 *� ** USE 24F GLM 5.125X 19.5 A= 99.938 S= 324.797 T= 1166. 770 F V = .165. E=1800000. DF-" = 1.00 CRIT SHEAR = 3218. AT 21.38 .1 .5*V/ (A*FV*DF) _ LFT CANT MAX MOM = 282.. FT .. LBS AT 4.00 FB=2274.. M/ (FB*S*DF) = .00 DEFL= .12 AT .00 L._/360.= .13 SPAN MAX MOM = :16:195. F T . I -.-.BS AT 14.61 FB =27'.74. M/ (FB*S*DF) = . 26 0EFL..:= - ,, 18 AT .13.7.5 L_/ 060. = ,63 RGT CANT MAX MOM = 0. FT . LBS AT 23 . Oc3 0 I=B =2274,. M/ (FB*S*DF) o .00 DEFT-...= .19 AT 29.00 L/360.= 2' 29 VALLEY P OVER-Al...L LENGTH: 29,.00 ROTS AT: .. 00 10.00 .23.00 APPLIED LOADS (DOWN +) 304 UNIF LOAD #/LF REACTIONS (UP +),: LEFT: 1.1.46.4 MID: 3735.99 RIGHT: 3933.6 A= .2 5L' 50 62,.729 :92..`?64 FV 8-5. E= 16C)0000 ,. DF = I1 00 CRIT SHEAR = 1868.. AT 2 . L1 1...5*V/ (A*FV*DF) _ ..63 LFT SPAN MAX MOM = 3736. FT. LBS AT 10 . 00 FB =.1 350 .. M/ (FB*:S*l�F) .. .40 DEFL= -.05 AT 4.25 L/360.= .33 RGT SPAN MAX MOM = 5472.. FT. i....BS AT 2-3,. 00 FB=1350. M/(FB*S*DF•)= .59 DEFL= -.04 AT* 1.6,.00 1._/360.= ,43 RGT CANT MAX MOM = 5472... FT.LSS AT 23.00 FB=.1350. M/ (F8*S*DF) _ .. 59 DEFL= -.20 AT 29.00 L/360.= .210 VALLEY E OVER --Al L I...ENGTH : 26..00 RC,TS AT : 6.00 '126 . 00 APPLIED LOADS ( DOWN + ) 41.8 AT 6 o AT 26 P' TL LOAD #/LF REACTIONS (UP ) 1 -EFT : ,-786.7 RT.G1-IT .: I.:: t 7 S E N 01. D F L. 6 Y.1. iS A-- 96. 250 S 6, F V = 85. E:: 16C)0000 , DF'-- J.. C)( -,j C)PIT SF -TEAR = 211.9q . AT 7 .46 1 . 5*V/ (A*FV*DF= ) LFT CAN"FMAX MOM = 0 F:.'1' .. I_. E; S AT 00 il,-B=12.95. M/ ( FB,f:S*DF DEFL= .90 AT 00 L /360. _ �='0 `:iPAN MAX NIOri l.c)7:<6. I= r . I._Bu AT 1.4..4S F:'B = 129- . M/ (FB*S;+:DF')= 35 DE:F1..=: - . ).9 AT 1.5 . 58 1.../ : 60..:_ 67 No. 33446 Exp, 0.30-94 tOFV, �c B J.. B 2 FASCIA t.)VER--AL_.L... l_.ENGTFI: 1.3.00 Ri.:'f:3 A'1 00 9.. 50 APPLIED LOADS (DOWN 4-) 270 AT 0 0 AT 13 P'TL._ LOAD #/LF REACTIONS (UP +);. LEFT: 9.54 .. 5 RIGHT,: 800 ,. '_ ****** USE 24F GI -M 3 ..125X 9 . 0 �*� *��: C� ✓F� 3 ��8 X � � ���l�J A= '28.125 S= 42.188 1. = 1.89. 844 FV=165. E=I800C)00. DF=1.2`. CRIT SHEAR = 7.58. AT 7`=, 1.5*V/(A*FV*DF) = 20 SPAN MAX MOM = 1.884.. F f . L_8S AT 4 . 22 F13=2100_ M/(f--B:,KS:c[) )= . DEFL = --.09 AT 4 .. 5£i 1.../ 360 . = 3.2 RGT ;'ANT MAX MOM = 14 -8, , FT „ l_8S AT 9.50. FB=2400. 11,/ ( FPS S*:DF) = C.:J. D E F L._ _ .. 0 9 A T L3. 00 L.. ;6 0„= '121 No. 33446 s Exp, 6-30-94 OF OVER -A_ LENGTH-. 16.50 ROTS AT: .00 8.. APPLIED L DS (DOWN +) 2495 AT .1.6 . S C LOAD # 955 AT 16.5 �tONC LOAD # RE_.ACTIONS (UP +,- LEFT: —3665.6 �R•:f`GHT : 711S.6 *** USE 24F Gt�.,1;1 6,.7.5tJX 21..0 ****** A=141.750 8= 496.125 'I=y , 5209.33.3 FV=165. E=1.800000,. DF''.]"- 0 CRIT SHEAR = 3666. 1.75 �,\ 1...5*V/ (A*FV*DF) = 24 SPAN MAX MOM =% 29325 „ f= T . L.88 8 ., 00 FB=2255_ I�/��F'E1+8*DF')_ :�J. �.. DEFL= . 02 i t�T 4 .. S8 1-/ 6t) .. ' 27 RG'f CAN // MAX MOM = x'9'325. FT . LBS Al 8 . OCx F8=1?���°.5=% M/(FB.,S.r.DF)= ,:>.I. DEFT]- � . 25 AT 16.50 L_. / 36C) . Z8 8 3 OVER-ALL LENGTH: .16.50 RCTS AT: .00 8.,00 APPLIED LOADS (DOWN +) .168 FROM 8 TO 16..5 P' TL. LOAD #/I....F 955 AT 16.5 CONC LOAD # REACTIONS (UP +)= LEFT: -1773.3 RIGHT: 4.156.3 USE 24F (al_h1 6.750X 13.5 A= 91.125 S= 205,.031. I= 1.383.961 F"V�:16S.. E=1800000. DF=.1..00 CRIT SHEAR = 2.194. AT 9.13 .1.5*V/(A*FV*DF) _ SPAN MAX MOM = 141.87. FT . L_BS AT 8..00 FB=2369. M/(FB*S*DF)= .3S DF_FL= ..04 AT 4..S8 L-/360,.= .27 RG'r CANT MAX MOM = 14187. FT.LBS AT 8.00 FB --2369. M/ (FB:fzS*DF) _ _35 DEFL.= -.43 AT 16.50 1.._/240.= .43 1 OVER-ALL LENGTH: :1.6.50 ROTS AT:, ,.00 10. SO APPLIED LOADS (DOWN +) 168 FROM 10.5 TO 16.5 P'TL LOAD #/L.F 9SS AT 16.5 CONC LOAD # REACTIONS (UP +): LEFT: -833.7 RIGHT: 2796.7 USE 24F GLM 6,.7.50X. 12.0 ****** A= 81..000 S= 162.000 1.= 972.000 FV -.165,. E=1800000.. DF=.1...00 CRIT SHEAR = 1795.. AT 11.50 .1.5*V/(A*FV*DF) SPAN MAX MOM = 87S4.. FT . LBS AT 10 . SO FB -2400. M/ (FB*S*DF") = .27 DEFL= .06 AT 6.08 1-_/:360 . _ „ tiS RG-(. CANT MAX MOM = 87S4.. FT . L.BS AT 10 . SO FB -2400„ M/(FB*S*DF')= 27 DEFL.= -.28 AT 16.50 L/240.= 1-30 e i. ►.G .20 8 5 OUTRIGGER 1± All OVER-ALL LENGTH: 26.00 RCTS AT: .00 16.00 APPLIED LOADS (DOWN +) 351 UNIF LOAD #/LF 2041 Al 5 •CONC LOAD # 800 AT 26 CONC LOAD # REACTIONS (UP +): LEFT: 2614.3 RIGHT: 9352.7 ****** USE 24F GLM 6.75OX 19.5 **¥*** A=131.625 S= 427,781 T: 4170,867 FV=165. E=1800000. DF=1.00 CRIT SHEAR = 4472. AT 14.38 1.5*V/(A*FV*DF) SPAN MAX MOM = 25550. FT.LBS AT 16.00 E8=2274. M/(FB*S*DF): .32 DEFL= -.02 © AT 4.75 L/360.= .53 RGT CANT MAX MOM : 25550, ET,LBS AT 16.00 FB=2274. M/(FB*S*DF): .32 DEFL= -,28 AT 26.00 L/360.= .33 8 7 RIDGE OVER-ALL LENGTH: 6.50 RC[S AT: .00 6.50 APPLIED LOADS (DOWN +) 272 UNIF LOAD #/LF REACTIONS (UP +): LEFT: 884.0 RIGHT: 884.0 ****** USE NOl DFL 6X 6 *®**** A= 30.250 S: 27.729 I= 76.255 . FV= 85. E=1600000. DF=1.00 CRIT SHEAR = 760. AT 6.04 1.5*VZ(A*FV*DF) _ SPAN MAX MOM = 1437. FI.LBS AT 3.25 E8=1200. MZ(FB*S*DF)= .52 DEFL= -.09 AT 3.25 L3360.: 22 31 44 ' 8 9 OUTRIGGER OVER --ALL LENGTH: 37.00 RCTS AT. '.00 2.6..00 APPLIED LOADS (DOWN +) 35.1 UNIF LOAD #/L..F 2041 AT 1.6 CONC LOAD # 800 AT 37 CONC LOAD # REACTIONS (UP +)r LEFT: 4.192.8 RIGHT: 11635.2 *** ** USE 24F GLM 6.75OX 15.0 *****►: A=101.250 S= 253.125 I= 1898. 438 FV=.165. E=.1800000. DF=1.00 CRIT SHEAR = 6535„ AT 24.75 1..5*V/(A*FV*DF) = S9 SPAN MAX MOM = 30036. FT.LBS AT 26.00 FB =234.1 .. M/ (FB*S*DF) _ .61. DEFL= -.77 AT 12.08 L/360.= .87 RGT CANT MAX. MOM = 30036. FT . LBS AT 2.6.00 FB=2341. M/(FB*S*OF)= .6.1 DEFL= ,.07 AT 29.83 L/360.= .37 OVER-ALL LENGTH: 29.00 RCTS AT: 5.50 29.00 APPLIED LOADS (DOWN +) 437 .UNIF LOAD #/L.F 31.93 AT 0 CONC LOAD V 4451 AT 0 CONC LOAD # REACTIONS (UP +): LEFT: .172.52.5 RIGHT: 3064„5 ****** USE 24F GLM 6.750X 24.0 ****** A=162.000 S= 648.000 T= 7776. 000 FV=165. E=1800000. DF=.1..00 CRIT SHEAR = 9174. AT 3.50 1.5*V/('A*FV*DF) _ LFT CANT MAX MOM = 48652. FT.L.BS• AT 5.50 F'B=2222. M%(FB*S*DF)= ..41 DEFL= -.16 AT .00 L/360.= .18 SPAN MAX MOM = 48652. 1=T..LBS AT 5..50 FB=2222. M/(FB*S*DF)= .41 DEFL= ..03 AT 9.67 L/360.= ..78 .51 No. 33446 Ev. 6.3014 OF C B 13 LOW (REVISED) OVER-ALL LENGTH: 9.00 RCTS AT: .00 8.00 APPLIED LOADS (DOWN +) 8929 AT 9 CONC LOAD # REACTIONS (UP +): LEFT: -1116.1 RIGHT: 10045.1 ****** USE 24F GLM 5.125X 13.5 ****** A= 69.188 S= 155.672 I= 1050.785 FV=165. E=1800000. DF=1.00 CRIT SHEAR = 1116. AT 1.13 1.5*V/(A*FV*DF) _ SPAN MAX MOM = 8929. FT.LBS AT. 8.00 FB=2369. M/(FB*S*DF)= .29 DEFL= .03 AT 4.58 L/240.= .40 RGT CANT MAX MOM = 8929. FT,LBS AT 8.00 FB=2369. M/ (FB*S*DF) _ .2c" DEFL= -.02 AT 9,00 Li36C).= .03 3 .14 OVER-ALL I-ENGTH : 16.00 APPLIED LOADS (DOWN +) 76 REACTIONS (UP +): .15 ROTS AT: .00 4,.00 14.00 UNIF LOAD #/L.F LEFT: -14.9 MID: 7.50..50 RIGHT: 480.4 USE NO1 DFL. 6X 6 A= 30.250 S= 27.72_'9I= 76,.2.5.5 FV= 85. E=1600000. DF=1...00 CRIT SHEAR = 397,. AT 4.46 .1,,.5*V/(A*FV*DF) _ LFT SPIN MAX MOM = 668. FT.LBS AT 4.00 F8=.1200. M/(FB*S*DF)= .24 DEFL= .01 AT 2,50 1_1360.= .1.3 RGT SPAN MAX MOM = 66£3.. FT . I....BS AT 4.00 FB=1200. M/(FB*S*DF)= .24 DEFL-= -..07 AT 9.42 L/360.= .33 RGT CUNT MAX MOM = 152. FT.LBS AT 14.00 FB =.1200 ,. M/ (FB.*S*DF) _ .OS DEFL-= .04 AT 16.00 L/360._ .07 .23 FESSIo* No. 33446 a� CIV � �� OF CWLo 13 1.5 RIDGE OVER --ALL LENGTH: 12.00 RCTS AT: APPLIED LOADS (DOWN +) 570 REACTIONS (UP +): 00 8.50 UNIF LOAD #/I -..F LEFT: 2011.8 RIGHT: 4828.2 ****** 118E NO1 DFL 6X10 *** *= A= 52.250 8= 82.729 I= x92..964 FV= 85. E=1600000. DF=1.00 CRIT SHEAR = 2.382.. AT 7..7.1 1..5*V/(A*FV*DF) _ SPAN IhAX MOM = 3550. FT. LBS AT 3.53 F8=1350. M/(F8*S*DF)_ ..38 DEFL= -.06 AT 3.92 L/360.= .2.8 RGT CANT MAX MOM = 3491„ FT.LBS AT 8..50 F8=1350.. M/(F8*S*DF)= .3c, DEFL= 02. AT .1.2.00 1..../360. = .12 B 1.6 LOW 8I" OVER-ALL_ LENGTH: 23.00 RCT`; AT: 00 23.00 APPLIED LOADS (DOWN +) 8806 AT :14..5 CONC LOAD # REACTIONS (UP +): LEFT : 3.2.54.4 RIGHT: 555.1 .. 6 ****** USE 24F GLM 5..125>C 18.0 ****** A= 92,.250 S= 276,.750 I= 2490.750 FV=165. E=1800000. DF=1..0C) CRIT SHEAR = 5552. AT 2:1.50 .1..5*V/(A*FV*DF) _ >PAN MAX M011 = 47,189. FT . L8 3 AT 14.50 I=8=2294. M/ (F8*S*,DF") = 1.89 DEFL= -.79 AT 12.33 L/360.= 7'1 I EEO 13 16 LOW BM CAMBER OVER-ALL LENGTH- 23.00' RCTS AT: „ 00 23.00 APPLIED LOADS (DOWN +) 5107 AT .14.5 CONC LOAD # REACTIONS (UP + ) : I_..EFT : :1.887.4 RIGHT : 3.219 .. 6 +:W*. USE 24F GLIM ...125X 18.07W A= 92,.250 S= 276..750 1= 2490.750 FV=16.5. E=18000100. DF=1.00 CRIT SHEAR = 3212C) _ A1, 2.1 .. 50 1 ..5"f'V/ (A*FV*DF) _ .32 SPAN MAX MOM = 27367. F.r .. LBS AT 14.50 F13=2294. M/(FB*S*DF)= .,52 DEFL= -.46 AT 12.33 L/360.= .77 3 17 I__ 0 W B I"I OVF_ R-ALI__ L.ENGTI-; : 4.00 RCTS AT: .00 4..00 APPLIED LOADS (DOWN +) 4828 AT 1.5 CONC LOAD # 5552 AT 1.5 CONC LOAD # REACTIONS (UP +): LEFT: 6487.5 RIGHT: 38921.5 ****** I.JSE 24F GLM 5.:1.25X 12.0 ****** A= 61.500 S= 123.000 I= 738.000 FV=.165. E=1800000,. DF=.1.00 CRIT SHEAR = 6488. AT 1.00 .1.5*V/(A*FV*DF) _ _96 SPAN MAX MOM = 977,1.. FT . L.BS AT 1 " 50 FB=2400. M/(FB*S*DF)= .40 DEFL= -..02 AT 1'.83 I__/360..= 13 B lB OVER-ALL LENGTH: 8'5O RCTS AT: 'OD 8'5O APPLIED LOADS (DOWN +) 434 UNIF LOAD #/LF REACTIONS (UP +)� LEFT: 1844'5 RIGHT: 1844'5 USE NOl DFL 6X 8 A= 41'2SO S= 51'563 I= 193'359 FV= 85' E=1600000' DF=1'00 CRIT SHEAR 1574' AT 7'88 1'5*V/(A*FV*DF) '67 SPAN MAX MOM 3920' FT^LBS AT 4'25 F8=1350. M/(FB*S*DF)= '68 ' DEFL= -'16 AT 4'26 L/360'= '28 G 19 OVER-ALL LENGTH: 13'00 ACTS AT: .00 13'00 APPLIED LOADS (DOWN +) 240 UNIF LOAD #/LF 7426 AT 5'5 CONC LOAD # REACTIONS (UP +): LEFT: 5844'2 RIGHT: 4701'8 USE 24F GLM 5'125X 13'5 A= 69.188 S= 155.672 fm 1050'785 FV=165' E=1800000' DF=1'00 CRIT SHEAR 5574' AT 1'13 1.S*V/(A*FV*DF) .73 SPAN MAX MOM = 28513' FT'L8S AT 5'5O F8=2369' M/(F8*S*DF)= '93 DEFL= -'38 AT 6'25 L/360'= '43 B 20 OVER-ALL.. LENGTH. 7.00 ROTS AT: APPLIED LOADS (DOWN +) 563 REACTIONS (UP I....EFT: 1970.5 RIGHT: 1970.5 00 7.00 UNIF LOAD #/LF ****** USE NO1 DFL 6X 8:** A= 4.1.250 8= 5.1.563 I= 193.359 FV= 85. E=1600000. DF=1.00 CRIT SHEAR = 1.61.9.. AT 6.. 38 .1.. 5*V/ (A*FV*DF) _ SPAN MAX MOM = 3448. FT. LBS AT 3.50 i=B=1350,. M/(FB* S3.'DF)= ..S9 DEFL= -.10 AT 3.50 L./360._ .23 B 21 OVER-ALL. LENGTH: 7.00 ROTO AT APPLIED LOADS (DOWN +) 225 REACTIONS (.UP +): LEFT: 787.5 RIGHT-. 787.5 .69 ,00 7,.00 UNIF LOAD #/I...F ****** USE NO1 DFI... 6X 6 A= 30.250 8= 27.729 I= 76.2.55 FV= 85. E=1600000. DF=.1..00 CRIT SHEAR = 684. AT .46 1.5*V/('A*FV*DF,) _ SPAN MAX MOM = 1378. FT.LBS AT 3.50 M/(FB*S*DF)= „S0 DEFL= -.10 AT 3.50 L/360.= .23 .40 No. 33446 Exp, 6.30.64 OF 13 22 OVER-ALL. LENGTH: 11..00 APPLIED LOADS (DOWN +) 399 REACTIONS (UP +): RCTS AT: ,.00 LEFT: 2194,.5 RIGHT: 2194.5 11.00 UNIF LOAD #/LF ***** USE NO1 DFL 6X10 A= 52.2 .SO S= 82.729 1= 392.964 FV= 85. E=1600000. DF=1-.00 CRIT SHEAR = 1.879. AT .79 1..5*V/(A*FV*DF) _ SPAN MAX MOM = 603.5- FT. L8S AT 5.50 FB=1350. M/(FB*S*DF')= ..6.5 DEFL= -.21 AT 5.50 - L/360.= .37 u 23 OVER --ALL. I....ENGTH : 8.00 ROTS AT: 00 8.00 APPLIED LOADS (DOWN +) 563 UNIF LOAD #/L.F REACTIONS (UP +) LEFT: 2252.0 RIGHT: 2252..0 ****** USE NO.]. DFL 6X 8 ****** A= 41.250 S= 5.1.563 I= .193.359 FV= 85. E=1600000. DF=1.00 CRIT SHEAR = 1900. AT 7.38 1.,.5*V/(A*FV*DF) _ SPAN MAX MOM = 4.504. FT.LBS AT 4.00 FB=1350. M/(FB**DF)= 78 DEFL=.-.17 AT 4.00 L/360.= .27 SSI 81 v N.. 33446ff °C Exp. 6.30.94 Cl IS OF B 24 (REVISED) OVER-ALL LENGTH: 15.50 RCTS AT: .00 15.50 APPLIED LOADS (DOWN +) 480 UNIF LOAD #/LF REACTIONS (UP +): LEFT: 3720.0 RIGHT: 3720.0 ****** USE 24F GLM 5.125X 12.0 ****** A= 61.500 S= 123.000 I= 738.000 FV=165. E=1800000. DF=1.00 CRIT SHEAR = 3240. AT 1.00 1.5*V/(A*FV*DF) _ .48 SPAN MAX MOM = -14415. FT.LBS AT 7.75 FB=2400. M/(FB*S*DF)= .59 DEFL= -.47 AT 7.75 L/360.= .52 B 24 (REVISED) CAMBER OVER-ALL LENGTH: 15.50 RCTS AT: .00 15.50 APPLIED LOADS ( DOWN '+ ) 320 UNIF LOAD #/LF REACTIONS (UP +): LEFT: 2480.0 RIGHT: 2480.0 ****** USE 24F GLM 5.125X 12.0 ****** A= 61.500 , S= 123.000 I= 738.000 FV=165. E=1800000. DF=1.00 CRIT SHEAR = 2161. AT 14.50 1.5*V/(A*FV*DF) _ .32 SPAN MAX MOM = 9610. FT.LBS AT 7.75 FB=2400. M/(FB*S*DF)= .39 DEFL= -.31 AT 7.75 L/360.= .52 3 2S OVER-ALL LENGTH: 10.00 RC TS AT: .00 1.0 ,. 00 APPLIED LOADS ( DOWN f) 432 AT 0 0 AT 1.n P' "1'I._. LOAD #/LF REACTIONS (UP f):: LEFT: 1440.0 RIGHT: 720.0 k: = USE NOI DFL. 6X S �W�*� ►: A= 41.250 S= 51.563 J= 193.359 F V = 85. E=1600000. DF = 1 . UC) CRIT SHEAR = 1178. AT .63 I.., 5*v/ (A*FV* DF) _ 50 SPAN MAX MOM 2771. FT..I__E;S AT 4.22 08=1350. M/ (FB*S DF) = .48 DEFL= -.16 AT 4.83 L/360.7 3 26 OVER--AL.L.. LENGTH: 1.5.00 RC''TS AT: ..00 15.,00 APPLIED LOADS (DOWN f) 450 s l_1NIF" LOAD #/LF REACTIONS (UP LEFT: 3600,.0 RIGHT: 3600.t� USE 24F GLM 5.125X 12.0 x� � k_�►*: �1 - C = r� - 61... _, 0 0 :;� - 123.000 T _. 73e.000 . FV= .165. E=1800000. DF z l .. C!('.) CRIT SHEAR _ 3.120. AT 1.00 1. , .5:1:4'/ (A*FV*DF) - .46 ,`•_'iPAN MAX MOM = 13500. F'T.I__BS AT 7.50 F8=2400. M/ (FEs:a <.*DF) = .55 DEFL= -.41 AT 7.50 L/360.= .50 SSI No. 33446 Exp, 01014 OF 8 26 CAMBER OVER-ALL.. LENGTH: 15.00' ROTS AT: .00 .15.00 APPLIED LOADS (DOWN +) 320 UNIF LOAD #/LF REACTIONS (UP +):: LEFT: 2400.0 RIGHT: :400,.0 ****** USE 24F GLM 5.1.2SX 12.0** A= 61.500 S= 123.000 I= 738.000 FV=165. E=1800000. DF=..1.00 CRIT SHEAR = 2081. AT 14.00 1 ., .5*V/ (A*FV*DF) _ .31' SPAN MAX MOM = 9000. FT.LBS AT 7..50 FB=2400. M/(FB*S*D1=)= .37 DEFL= -.27 AT 7.50 L/360.= .50 8 27 OVER-ALL LENGTH: 8..00 RCTS AT: .00 8.00 APPLIED LOADS (DOWN +) 480 UNIF LOAD #/I._.1= 7115 AT 6.5 CONC LOAD # REACTIONS (UP +): LEFT: 3254.1 RIGHT: 7700.9 ***** USE 24F GLM 5.125X 13.5 *****= A= 69.188 S= 155.67; I= 10.50.785 FV=.1.65.. E=1800000.. DF=1,.00 CRIT SHEAR 7161. AT 6.88 1.5*V/(A*FV*DF) _ .94 SPAN MAX MOM = 11011. FT .. L..BS AT 6.50 FB=2369. M/(FB*S*DF)= .36, DEFL.= .-,.06 AT 4.33 L/360.= .27 23/3 B 27 CAMBER OVER, -ALL I._ENGTH : 8.00 ROTS AT: '.00 8.,00 APPLIED LOADS (DOWN +) 320 UNIF LOAD #/L.F 4743 AT 6.5 CONC LOAD # REACTIONS (UP +): LEFT: 2169 . 3 RIG[ -IT : 5.1.33 . ****** USE 24F GLM 5.12.SX 13.5 **** * A= 69.188 S= 155.672 I= 1050.785 FV=165., E=1800000,. DF=.1 ,.00 CRIT SHEAR = 4774. AT 6.88 .1.S*V/(A*FV*DF) _ .63 SPAN MAX MOM = 734.1. FT .. L..BS AT 6.50 FB=2369. M/(FB*S*DF)= .24. DEFL = -,.04 AT 4.33 L/360.= .27 B 28 OVER-ALL. LENGTH: 1.5.00 RCTS AT: .00 15.00 APPLIED LOADS (DOWN +) 409 UNIF LOAD #/LF REACTIONS (UP +): LEFT: 3067.5 RIGHT: 3067.5 ****** USE NO1 DFL 6X10 * *** A= 52.250 S= 82.729 I= 392.964 F V = 85. E=1600000. DF =1.. '2 5 CRIT SHEAR = 2.744.. AT ..79 1,.S*V/(A*FV*DF) _ .74 SPAN MAX MOM = 11503.. FT.LBS AT 7.50 FB=1350. M/(FB:*S*DF)= .99 DEFL.= -.74 AT 7.SO L/240.= .7.S '3 2.9 OVER-Al._L. 1._.ENGTI-1 : I.L ..00 APPLIED LOADS (DOWN +) 401 REACTIONS (UP, +) 24XI RGTS A1' . .00 .1.1.00 UNIF I....OAD #/LF LEFT: 4.205..5 RIGHT: :2205.. S ****** USE N01 DFL 6X10 *****3' A= ..52 . 250 S= 82.729 T.= 392. 964 FV= 85. E=1600000. DF=1.00 CRIT SHEAR = .1.888. AT 10.2.1 1.5*V/(A*FV*DF) _ SPAN MAX MOM = 6065. FT.I_.BS AT 5.50 FB=.1350. M/(FB*S*DF.)= .65 DEFL= -.2.1 AT "-).SO L./360.= .37 8 30 OVER-ALLLENGTH : 3.00 RCT:_> AT APPLIED LOADS (DOWN +) 534 REACTIONS (UP +): LEFT: 801.0 RIGHT: 801.. 0 .. 6 4 . 00 3.00 UNIF LOAD #/LF ****�►:* USE NO]. DFL 6X 6 ****** A= 30 . 2SO S=:.'_7.729 I= 76 ., 25S FV= 85. E=1600000.. DF=,1..00 CRIT SHEAR = 5.56. AT .:46 1.5*V/(A*FV*DF) _ SPAN MAX MOM = 601. FT.L BS AT 1.50 'B =.1200 .. NI/ ( FB*S*DF) _ .. 22 - DEFL= -.01 AT 1.50 L/360,.= ..10 .32 13 3.1 OVER-ALL LENGTH: 8.50 RCTS AT: .00 8..50 APPLIED LOADS (DOWN +) 315 UNIF I.._OAD #/LF REACTIONS (UP +;1~ I._.EFT: `1338.8 RIGHT- 1338.8 ****** USE NO1 DFL 6X 8 ****** A= 41.250 S= 5.1..563 1:= 193.359 FV= 85. E.=1600000. DF=1.00 CRIT SHEAR = 1. 1.4 '... A7 SPAN MAX MOM = 2845. FT . L B'; AT 4. 25 FB = 1.350. M/ (FB*S*DF) = .49 DEFL= -.12' AT 4.I C. 1-/:')6(?,.= 28, B 32 OVER-ALL LENGTH: 12'. 50 RCTS AT,-. APPLIED LOADS (DOWN +) 4.1.8 REACT I OP4S (UP +) I._.EFT: 261.2,.5 RIGHT 2•x:1. 5 ..00 12:,50 UNIF LOAD #/I._F USE NO1 DFL 6X10 ****** A= 52.250 S= 82.729 I= 1.)92.,964 F,V = 85 . E =1.600000. DF = .1.. 00 CRIT SHEAR = 2282. AT 79 1.5*V/(A*FV*DF) _ SPAN MAX MOM = 8164. FT . LBS AT 6. 25 FB=1350. M/(FB*S*DF)= .88 DEFL= -.37 AT 6.25 L/360. 42 49 .77 8 33 OVER-ALL LENGTH- 5.00, RCTS AT: ., 00 .5 ,. 00 APPLIED LOADS (DOWN +) 7.12 UNIF. LOAD #/LF REACTIONS (UP +): LEFT: 1780.0 RIGHT: .1780 ,. 0 ****** USE NO1 DFL 6X 6 A= 30,.250 S= 27.729 I= 76..255 FV= 85. E=1600000. DF=1,.00 RIT SHEAR = 1.454.. AT ..46 1.5*V/(.A*FV*DF.) _ .8s. SPAN MAX MOM = 2225. FT.LBS AT 2.50 FB=1200. M/(FB*S*DF)= .80 DEFL= -.08 AT 2.50 L../360. _ ..17 13 34 OVER-ALL LENGTH: 17.00 RCTS AT: „00 .14,.00 APPLIED LOADS (DOWN +) 437 UNIF LOAD #/LF REACTIONS (UP +) I.._EFT: 291.8,.5 RIGHT: 45.10,.5 ** USE NO1 DFL 6X].2 ****** A = 63.2-1150 S'= 121.2219 1= 697.068 FV= 85. E=.1600000.. DF=]..00 CRIT SHEAR = '4278.1., AT .1.3.04 1.. 5*V/ (A*FV*DF) _ SPAN MAX MOM = 9021. FT . LCIS AT 8.50 FB=.13.50. M/ (FB*S*DF) = 66 DEFL = -.28 AT 8.50 L / 360 ., _ .47 RGT CANT MAX MOM = 0.. F1'..I.._BS AT ..00 FB =1350. M/ (FES i:S*DF) = .,00 DEFI.._= .00 AT .00 1__/:ti60. = LO 78 35 RIDGE OVER-ALL LENGTH: 10.00 RCTS AT: APPLIED LOADS ( DOWN f) 4.18 REACTION:: (UP LEFT: 2090.0 RIGHT: 2090.0 00 10..00 UNIF LOAD #/LF *,***** USE.: NO1 'DFL. 6X 8 ****** A= 41.250 S= 5.1...563 I= 193.359 FV= 85. F_=1600000 DF=1.00 CRIT SHEAR = 1829.. AT .63 1 5*'V/ (A*FV*DF ) SPAN MAX MOM = S225. FT . L_88 AT 5.00 F8=1350. M/ (FB*S*DF) = 90 DEFL= -.30 AT 5.00 L/360.= _33 ..78 8 36 OVER-ALL LENGTH: 7..00 ROTS AT: .00 7,.00 APPLIED LOADS (DOWN +) 268 UNIF LOAD #/LF REACTIONS (UP +);: LEFT: 938.0 RTGHT : 918.0 *:*:*** * USE NOI Iif._.L 6X 6 *:*:*:*:*:*: A= 30. 050 S= 27.729 :I= 76.. 25.5 FV= 85. E=1600000. DF=.1.00 CRIT SHEAR = 81.5.. AT .. 46 1 .. 5*V/ (A*FV*DF ) SPAN MAX MOM = 1642. FT.LBS AT 3.50 F8 = 1200. M/ (FB*-S*DF) - 59 DEFL= -.12 AT 3.50 L!360._ .23 Exp, 6.30-94 OF .48 3 37 OVER—ALL LENGTH: 7,.00 ROTS AT APPLIED LOADS (DOWN .F) S34 REACTIONS (UP +) LEFT : 1.869..0 RIGHT : .1.869. 0 ..00 7.00 UNIF LOAD #/LF USE. NO1 DFL. 6X 8 �:**:**�► A= 41.2-150 S 5.1....56 J= 1'93 .. 359 FV= 85., E=1600000. DF=1.00 CRIT :' HEAR = 1..5;5.5.. AT c:, � 1 ..SSV/ (A*FV*DF) _ SPAN MAX MOIl = 3271.. FT. L..B Al 3. 50 FB=.1.350. M/(.F13*3*DF)_ 56 DEFL= 09 AT 3.50 L./360.= .23 .. 6 6 OVER --ALL I....ENGTH: S.. 50 RC',T`3 AT: .00 5.50 APPLIED LOADS ( DOWN +) 439 UNIF LOAD #/LF REACTIONS (UP + ) I....E:FT: 1.207,.3 RIGHT, 1207.3 USE NO1. DFL_ 6): 6 A= 30.250 S= 27,.729 I= 76..2S5 FV = 85. E = 1600000. . DF=1.. 00 i;R.IT :SHEAR = 1.006. AT ..46 [. ..5:9V/ (A*FV*DF) _ .. 59 SPAN MAX. MOM = 1660,. F f .,LB AI' 2.75 F13=1.200. M;' ( FR i14,:1)F) DEFL= —.07 AT 2. 7`; L./3610,= lEl 76.33446 ) mx fqp 6-30-94 13 ,S9 OVER--AI.-I.... L_ENG TH : L.0 ,. 51.E R01AT : .00 LO ..:50 APPLIED LOADS (DOWN +) 45x.3 UNIF LOAD #/L.F REACTIONS (UP +); LEFT: 2404.5 RIGHT- 2404 ,. S + **� USE N01 DFL 6X10 *** * A- 50-' S= 8�.729 'f 392,.964 FV= 85., E:=1600000. DF=.1..00 CRIT :'.SHEAR = 2:042.. AT .1. '1.. 5'+V/ (A*FV*DF) :SPAN MAX MOM = 6312.. FT . LB'S AT S.25 F8=.1350. 11IJ [ FB:,rSl:DF ):- 68 DEFL= - . 20 AT' 5.2's 1-/360 = 35 13 40 OVER-ALL- i.._ENGTH: 6..00 RCTS AT: ..00 6.00 APPLIED LOADS (DOWN +) 1680 AT 3 CONC LOAD # REACTIONS (UP +).- t EFT ):L...EFT ,: 1340. 0 RIGHT: 840.0USE 1\101 Df L. 6X 6 A= 30.2.50 S= 27.,729 I- 76.255 F'V- 85. L_-.1600000. DF::,:]..Uc., CRIT SHEAR = 840.. AT 46 1 ,. S*V/ (A*FV*DF) _ .49 SPAN MAX 1`101,1 = 2520. FT . L_B'1 AT 3.00 .-r-1200. M/ i F13*Sa:DF .91 DEFL= -.11 AT 3.00 1_./ :360. = 2,0 No. 33446 �c Elp, 6.39.94 * OF 4t OVER --ALL I....ENGTH: 3..00 RCTS AT: APPLIED LOADS (DOWN +) 38G • REACTIONS (UP 1. EFT : 573 ,. 0 RIGHT,. 57:5. 0 00 3.00 UNIF LOAD #./LF USE NO1 DFt.. E,>< 6 A = 30 ,. 250 S = 27. 7.29 1 = 76.2.5.5 FV= 85. E=.16-00000.. DF=1...00 �98., A T 'I....5*V/ (A*FV*DF).RIT ,HEAR _ _ SPAN MAX MOM 4.3Ci .. 1 I'.. L. i- `; AT 1 . 50 Fra = 1.2t)0 .. M( F'B-*,:S*DF ; _ .5 DEFL= -' .01. A.r.. 1.50 L._/ 360..:- L0 I3 42 .. 2.3 OVER--AL...L LENGTH: 10..50 ROTS AT: „00 10...50 APPLIED LOADS ( DOWN -+' ? 382 UNIT I....OAD #/I....F REACTION,':.', (UP + LEFT : 2005., 5 FIGHT: 2- )o5.. 5 A'= 41-2150 S= 51 . 563 1 = 1. 3.59 FV= 85. E:=1600000. DF=1.00 t.Ri"r ;HEAL;: = 1 -167 .. AT L .. 5 *V/ (A *FV*Dr=) _ SPAN MAX MOM = 5264. FT. LBS AT 5.25 i=B=1350. M/(FB*S*DF)= 91 DEFL= —.34 AT 5.25 L/ 1.=122.33 75 B 43 OVER-ALL LENGTH: 22.00 APPLIED LOADS (DOWN +) 313 884 AT •5.5 3065 AT 5.5 REACTIONS (UP +): RCTS AT: .00 6.00 22.00 UNIF LOAD #/LF CONC LOAD # CONC LOAD # LEFT: -88.8 MID: 8928.69 RIGHT: 1995.2 e �3 ***** USE 24F GLM 5.125X. 7.5 ****** A= 38.438 S= 48.047 I= 180.176 FV=165. E=1800000. DF=1.00 CRIT SHEAR = 2817. AT 6.63 1.5*V/(A*FV*DF) _ .67 LFT SPAN MAX MOM = 8142. FT.LBS AT 6.00 FB=2400. M/(FB*S*DF)= .85 DEFL= .05 AT 3.75 L/240.= .30 RGT SPAN MAX MOM = 8142. FT.L.BS AT 6.00 FB=2400. M/(FB*S*DF)= .85 DEFL= --.74 AT 14.92 - L/240.= .80 81 44 OVER-ALL.. LENGTH. 8..00 RCT:; AT: .00 8.00 APPLIED LOADS (DOWN t1 11.7 UNIF LOAD #/LF REACTIONS (UP LEFT: 468.0 RIGHT: 458,.0 ****** USE NO1 DFL 6X 6 ***** A= 30..250 S= 27.. 729 1= 76..2.55 FV= 85. E=1600000. DF=1.00 CRIT SHEAR = 41.4., AT 46 1,.5*V/(A*FV*DF) = 24 SPAN 11AX. 11011 = 936. F'f . L.BS Al 4.00 1=3=1200. M%(FB*S*DF)= 34 DEFL.= -.09 AT 4 00 L../ 360 . = 27 R 4 GARAGE C)VER•-AL_L L...E..Pd(a'1'II: 18.00 ROTS AT: .00 18.00 APPLIED LOADS ( DOWN +) 0 AT 0 544 (1T 13 P''1'I... L 0 A D #/I._1= 544 A "F 9 C) AT 1.8 P''fL LOAD #/LF •.7...?54 F11" 4 CONC LOAD # REACTIONS (UP �7 LEFT- 4973. 9 RIG1-1T : :1-11 :1... 1. t"1 eE 24.F GLI'll 5 . 1 5): 1.5 . Ci �:�� *�► .-- 76.337.5 _ .1 2...1f819 T::: 1.441... 406 FV =1.6 5 . E. = I800000 .� I.')F 1.. Ci C) CRIT SHEAR = 49 3) 2,) . AT A. 25 1.. 53'V/ (A*FV*DF) _ ,. 58 SPAN MAX' MOM = 21703 . FT . LBS AT 7.56, FB=2341. M/(FB*S*DF)= 58 DEFL = —.48 AT 8 . 67 L/ 36.v0 .. - 6f:) B 4.6 OVER—ALL. I...ENGTH : :10.00 ROTS AT: .00 .10.00 APPLIED LOADS (DOWN .1) 449 UNIF LOAD #/LF REACTIONS ( UP +) +..EFT: 224.5.0 RIGHT: 2.245.0 USE: NO 1. 1)FL. 6,>/\ Ft A= 4.1 ,. 250 S= 51...563 1= :193 „ 3.59 FV= 85. E 1600000. DF=.1.C)C) CRI,r. SI -TEAR = 1965. AT 9.3.8 1 „5*V/ (A*FV*DF) _ ,.334 SPAN MAX. MOM = 56.1:1. FT . LElS AT S. 00 FB='.1.350.. M/ ( F8 2-+1:)F DEF L = —.33 AT 5 .. 00 L/360. = 33 13 47 OVER-ALL LENGTH:, 9.50 APPLIED LOADS (DOWN +) 133 REACTIONS (UP +): RCT: AT: .. 00 9.50 UNIF LOAD #./LF LEFT: 631.8 RIGF-IT: 63.1.8 ** * USE N01 DFL. 6X 6 ****** A= 30.250 S= '127.729 1= 76.255 F V = 85. E = 1600000 . DF = l.. 0O CRIT SHEAR = 571. AT .4.6 .1.5*V/('A*FV*DF) SPAN MAX MOM = 1500. FT. LBS AT 4.75 FCS=1200. M/(FB*S*DF)= .54 DEFL= -.20 AT 4.75 L/240.= 47 3 48 OVER-ALL LENGTH: 7.50 RCTS AT: ..00 APPLIED LOADS (DOWN �) 632 AT 1 CONC LOAD # REACTIONS (UP +') LEFT: 547.7 RIGHT. : 84..y ****** USE NOI DFL 6X 6 ****** A= 30.230 S= 27.7219 'T.:: 76 . 2.55 FV= 85. E=.1.600000.. DF=:1.00 C::RIT SHEAR= 54L'.. AT 46 1. ,. 5*VI (A::FV*DF ) SPAN MAX MOM = 548. F1' .. L.BS AT 1.00 =8 =.1200. M/ (FC *S+:DF) _ .20 DEFL = =,::; AT 3.2 L../ 2 40,. = 38 0 .33 ..32' `ho. 33446 Exp.B•30-9� OF B 49 OVER-ALL LENGTH: 4.50 RCTS AT: APPLIED LOADS ( DOWN + ) 486 REACTIONS (UP +): LEFT: 1093.5 RIGHT: 1093.5 00 4.50 UNIF LOAD #/LF ****** USE NO1 DFL. 6X 6 ****** A= 30.250 S= 27.729 I= 76.255 FV= 85, E=1600000. DF=1.00 CRIT SHEAR = 871. AT .46 1.5*V/(A*FV*DF) _ SPAN MAX MOM = 1230. FT.LBS AT 2.25 FB=1200. M/(FB*S*DF)= .44 DEFL= -.04 AT 2.25 L/240.= .22 x OVER-ALL LENGTH: 11.00 APPLIED LOADS (DOWN +) 486 REACTIONS (UP +): .51 RCTS AT: .00 4.50 11.00 UNIF LOAD #/LF LEFT: 644.6 MID: 3432.64 RIGHT: 1268.7 ****** USE N01 DFL 6X 6 ****** A= 30.250 S= 27.729 I= 76.255 FV= 85. E=1600000. DF=1.00 CRIT SHEAR = 1668. AT 4.96 1.5*V/(A*FV*DF) _ LFT SPAN MAX MOM = 2020. FT.LBS AT 4.50 FB=1200. M/(FB*S*DF)= .73 DEFL= .01 AT 3.67 L/240.= .22 RGT SPAN MAX MOM = 2020. FT.LBS AT 4.50 FB=1200. M/(FB*S*DF)= .73 DEFL= -.09 AT 8.08 L/240.= .32 .97. RT.=t3 the flying buttress I SHEET 72-757 Fred Waring Drive, 115 BY DATE _ W.O. NO.o -Z 33 Palm Desert, CA 92260 CKD DATE JOB 3 ' (619) 346-5445 f �. Pte. P• = 15av �'� ��-ssurt �� . PREPARED' FOR: Iz" t 8° ,p P• F-tas (TYF?� . Nl�� cwt✓ 1- T P L01>19 I i�. _. '<-.- 2I'i'50 2-2 IZ'G00r..1:-fC, Icc) njT �✓TG�27/�- N^P �Z t2 all �4�5 �.LU, �« Uj ti I�i;Q. pe>v J wr l.� (.��%W- U 11 p 12-1:50 X3/4 X ��r.� 3�" �� P 4= q -s r .w PTI, 17 G6 (o Iz i'co 11&35 P•L. `3CoSQ P� �} � -� E,l,U, o -rL, 2.1 DtL • 15 P7 ZCaI 4 Co3/4 x 12 &LG S4-" ✓o Pv�. �Z' �-'> �,uj- P-rL,-• 17 Ga Co 12 P8 1 Co �7 I Co x7 �{-Z` SQ t",(�•'Y� ' X47 E. UJ, G G % CO y4 �EESSIppo l 0 446 MI Exp. 6 30.64 Q sr CIV\ �pQ '�rE OF C��'� the flying buttress 12. SHEET 72-757 Fred Waring Drive, 115 BY DSP DATE W.O. NO. �o IfF+ Palm Desert, CA 92260 CKD DATE JOB (619) 346-5445 PREPARED' FOR: O �E5 ock moor- w��s ► 37 5 = Zq-4 PLt- L %J) V Z 3 u� ups= (7-Z P'51r- x ;a) -r C"1,5 X 1a P5$:_ -,K 3 �x ©,i71 = 2LP SSID uJ�,� 2 2 p�F crov f� til S �Fq� . OCo 3 I x CoPjI 0. (37a = _2Co5 z FBF_ acv 2 z P� f9L F- C-�ov S N S W�=�ZZ �'S1✓ �- �o�� -� `�� X I :'� P��� >C Z , x p , X375 '-. Z19- G p V IS the flying buttress 72-757 Fred Waring Drive, IIS BY 02-f DATE I z / _ o W.O. NO. 610- 214 — SHEET 3�0 Palm Desert, CA 92260 (619) 346-5445 CKD DATE JOB f� l 1 PREPARED' FOR: FESSiO CIO m No.33446 ?, Exp. 6.39-94 sr cry qTE OF Cp�� o J o o 3 rdJ d34S\ 1 — 1T t ¢ kD J O r 1� 1s dJ 4- _-_ cp + �" S' + � � N - 4- KI) s 3 T ?- en I SHEET BY the fling buttress BY - PAP DATE _ � W.O. NO. cl 72-757 Fred Waring Drive, 115 CKD DATE JOB O'/ eiR TV OZ 10 � Palm Desert,.CA 92260 2 (619) 346-5445 : PREPARED .FOR: : o"-/E/RTtJ R•N I NCS 'j+ �, P. �s � � . '; _ � _... _------� • i Q FoR ►tet,. �T, L . Fro" {}Qu�now#'j .5..►� �t� . 2Z. (... f30C?......... j-.�-..._.. .A�+�'�..2Z.:. - --Q - 26o S I �1 ! 1 [41 .14-' c� s cl z 6154-7 - i --...�. i-7��. `i Cj•�: .2 �.��:..:.-......_... ►-r:,P��►-hoz ... i • i w.1.... to i:.. 'Z 441 ,J. 4104 Q�pfEs 4� )Z 2ci r:.l IBJ% K+ 1 'L' • .5, No. 33 B Exp, 5.3 -94 - �-� 130 .Z • .. `7 OF v p���o 3d I Y z �- 10 2 coz— ....' 307_ ..2_ . Lo Zoo _..;✓.?-- .__ ._. ! i the; fling buttress 2� SHEET 72-757 redWaririg Drive, q5 BY DATE '11 W.O. NO. :. CKD . DATE JOB t�IQ/�L� Fb12 C�Palm. Desert, CA 92260. j (619) M'_5445 ! PREPARED FOR: _ ji ----::,-.. ..!`..:---� .... ' _�._..(�. � ISS .1. ,, ;`•► � t� - d co UK"`���v�������� \ N ; : rn A- • N - -._. _..�...... .7 0- A< N... \� S vA ESSIONA , - _ v . cll — — W No. 33446- - A� i tclF the flying buttress 72-757 Fred Waring Drive, 115 Palm Desert, CA 92260 (619) 346-5445 BY C42 -,e DATE o W.O. NO. 4 o— 2 14 CKD DATE JOB SHEET /Sq PREPARED' FOR: 1W Cox/ 5`rKUG'f S PLi Wo V�) lod 011 ' CIO "mc- eUCotip TaP /Z� Gt�X� 5Yi2l�CiT {2[_. V•1Y' W/ C'i ToP �. ��TTor'1 Pt,.d��-.=� 1 12.`'vL F 1 ��� , 'P, � . � 3� . /►, tp ,e�-NG{brp- et;L"fi -rc'- ✓ 25 -F P-;,. I -/ P(-F- ���� I q (�o �ZoG ?Zt¢ f2` 7 ,034- U)'6eutr 19, c' i'l'l-iI �- I.pl (�1J,U_) Q, V"\ I V, Non -Negotiable Time Certificate of Deposit Not -Transferable ELDORADO-BANK PALM DESUC SErI'IIMM :18, 1991 :',-A ' 75 days ' BRANCH California, Date Type ' This Certifie§That *1A iias/Have: •*: t ter. H•..� •r•. - •, Deposited In This Bank •" c �� ..Dol -14,,000.00*. +� r 4 -*TBE. CITY OF .IA * � t- .-Principal Payable To _ z Upon Maturity and. Presentation and, Surrender Of i M.6a top sed. ' r K] This deposit bears interest at S•0"5o per a nu t eft o i$posi t01 turity, payable �� Z[fontlzly •.r IMatunty/Monthly/ouarterly/Semi-Annualty/Annually) ❑ This deposit bears an initial interest rate of iialwi ►tli7 S'nd i11a1 ' e a variable rate tied to the rate on in effect on the first working day of each month payable )Matuf y/Mont hly/ouarterly/Semi-Ann ua lly/Annually) 13L The certificate will be automatically renewed fora similar maturity at the interest rate then prevailing for these deposits unless within ten (10) days after this or any subsequent maturity date the owner presents it for redemption. ❑ This deposit shall �ber�oe a demand funds and cease to earn interest on the maturity date. This certificate will not automatically renew: Interest shall be and based on a 365 day year. If certificate is redeemed before maturity, an interest penalty Compounded/Non•Compounded 12-2-91 will be assessed which is in accordance with applicable law. T1 maturity of this certificate is from date of issue. The Bank Day/Months/rears reserves the right to(a) Redeem this certificate on the original or any subsequent maturity date or(b) Change the terms or the method of interest calculation applicable to this account after providing at least thirty (30) days rit ten notice to the owner of record prior to the beginning of such extension of maturity. Not Subject to Check Authorized onature •" TCD -2 5/82 9 DESERT SANDS UNIFIED SCHOOL DISTRICT 82-879 Highway 111 NOTICE: Indio, CA 92201 Document Cannot Be Duplicated (619) 347-8631 Date 9/12191 1 Type of Permit I La Quinta No. 110862 Permit M Log # Owner Name La Quinta Orchards Partners No. suet see below city La Quinta Zip 92253 Study Area 117 APN # I I Tract #i I j Lot • Square Footage 110296 Type of Development I Single Family Residence No. of units Comments 79-295 Stnnegatp 4504/792 a - f}_ (glipsthnusp) 79-420 Riramnod 5000 s!_ ft - At At the present time, the Desert Sands Unified School District does not collect fees on garages/carports, covered patios/walkways, residential additions under 500 square feet, detached accessory structures or replacement mobilehomes. It has been determined the above-named owner is exempt from paying school fees at this time due to the following reason: EXEMPTION NOT APPLICABLE - This certifies that school facility fees imposed pursuant to Government Code M80 in the amount of 1.68 _ X 10 or $ 16,267.68 have been paid to DAU.&D. for the property bsted above and that building permits and/or Certificates of Occupancy for this square footage in this proposed project may now be issued. Fees Paid By Charles R. Strother Name on the check By James E. Lively Assistant Superintendent, Business Services Fee collected/esem d by Diana M. Allard Signature Telephone Payment Received - , � i , ' Check No. 000432 Collector. Attach a copy of county or city plan check application form to district copy for all waivers. Embossed Original- Building Dept./Applicant Copy - Applicant/Receipt Copy - Accounting