Loading...
HomeMy WebLinkAbout39514 AVIATION AVE -� / . : STEBL BOILDING SYSTEMS, I�C, P.O. BOX 447 ADBL, GA 316Z0 '� (912) 896-7428 FRAME SUM.�ARY PAGE 1 ------------- DATE 2/ 2/Z000 • TIME 09:37:18 PRQJECT: SBS' 00-01-030"B" PROFESSIONAL AIRCRAFT � FRAME : Frame Number 1 FRAME TYPE IS SC LT SPAN (ft) 20,00 ' _ EAVE HEIGHT (ft) 21.33 ROOF SI.OPB (ft) 1.00 BAY SPACING (ft) 25,00 GIRT DEPTH (in) 8.00 PURLIN DEPTH (inj 8,00 FLANGE YIfiLD (KSI) 50.00 WEB YIEI�D (KSI) 50,00 � LIVE (SNOW) LOAD (psf) 12.00 SVOW I,OAD (psf) .00 WIND LDAD _ (psf) 27.7T AUX DEAD LOAD (psf) .00 DEAD LOAD (psf) 2,30 RAFTER FLANGE HRACE bOCATIONS For design purposes the rafter was assumed braced at purlins (numbered from left sidewail); • 1 2 3 4 COLUMN BRACIYG For design purposes the column Was assumed braced at girts (numbered from floor line): 3 � i � _ � - ��., � ' `��;� _ � �_ 1`� � " - - , °�� - - ^ ' STEEL BUILDIYG SYSTBMS, INC. P.O, BOX 447 � ADEL, GA 316Z0 (912) 89fi-7428 FRAME DESI6N PAGE 1 ------------ DATE 2/ 2/2000 TIHE 09:37:17 PROJBCT: S9S 00-01-030"B' PROFESSIONAL AIRCRAFT FRA�ME : Fra�e Number 1 STRBSS ANALYSIS FOR MEHBBRS: 1 - 1 LEFT EXTREMITY RIGHT EXTRBMITY WEB --------------------------------------------- --------------------------------•------------ ----- � PT A%IAL STRESS BENDING STRESS STRESS AXIAL STRESS BENDING STRESS STRESS SHEAR NO , COHPUTED ALLOwABLE COHPUTED A�LO�ABLE RATIO COHPUTED ALLOWABLE COMPUTED ALLOWABLE RATIO RATIO (KSI) (KSI) (KSI) (KSI) (KSI) (KS1� (KSI) (KSI) 1 .7B 21.51 .00 28,26 ,036 .78 Z1,51 .00 30.00 ,036 .150 2 -,70 30.00 -5.91 30,00 .Z20 -.70 30.00 5.91 10,26 .552 .098 3 -.70 30.00 -9.36 30.00 .335 -.70 30,Q0 9.36 10.26 .889 ,047 9 -.70 30,00 -10.35 30.00 .369 -.70 30.00 10.35 10.26 ,986 ,005 5 -,70 30.00 -8.89 30.00 .320 -,70 30,00 8.89 10.Z6 .643 .056 6 -.70 30.00 -8.87 30.00 .319 -.70 30.00 8.87 10.26 .842 .057 ' 7 -,70 30,00 -5.70 30.00 .214 -,70 30.00 5.70 10.Z6 ,533 .100 8 -.70 30.OD -.77 30,00 .099 -1.02 30.00 -,35 3D.00 ,046 ,14g GEOMETRIC PROPERTIES FOR HEMBERS: 1 - 1 S E C T I 0 N D E S C R I P T I 0 N FU1L SECTION PROPERTIES -------------------------------------------------------------- ------------------------------- P 0 I N T LEFT FLAYCE RIGHT FLANGE W E B MOM OF SECTION MODULU5 NO LOCATION WIDTH THK UNBR LGTH �IDTH THK UNBR LGTH THK HEIGHT S SPACE AREA INERTIA LEFT RIGHT (FT) (IN) (IN) (IN) ([N) (IN) (IN) (IN) (IN) (IN) (IN2) (IN4) (IN3) (IN3) 1 ,00 6.0 .250 88.0 6.0 ,250 208.0 .134 10.00 244.0 4.3 90.0 I7,15 17.15 2 3.50 6.0 .250 88,0 6.0 .250 Z08.0 .134 1D.00 244.0 4,3 90.0 17,15 17,15 3 7.00 6.0 .250 88.0 6.0 .250 208,0 .134 10.00 249.0 4.3 90.0 17.15 17.15 4 10.50 fi.0 .250 60.0 6.0 .250 209,0 ,134 10,00 244,0 4,3 90,0 17.15 17,1a S 14.00 6,0 .250 60.Q 6.0 .250 208.0 ,134 10.00 Z44.0 4,3 90.0 17.15 17,15 6 14.08 6.0 .ZSO 60.0 6,0 .250 208.0 .134 1Q.00 244.0 4,3 90.0 17,15 17,15 7 16,99 6.0 ,250 60.0 6,0 ,ZSO 208,0 .134 10.00 244,0 4.3 90.0 17,1'a 17.1"a � 8 19,95 fi.0 .250 31.4 6.0 .2�0 31.4 .134 10.00 244.0 4.3 90.0 17,15 I7.la FLAVCES WEB YIELD STRBSSES (K5I} 50.0 50,0 _ � � i� ��� � �f: ! - L' f ��` _ - - � � = <_ . , ST�EEL B�JILDIN� SYST�Ef(�, INC. _ P.O. BOX 447 ADEI,, GA 31620 (912) 896-7928 FRA�►IE llESIGN PAGE 2 """""'- DATE 2f 2/2400 TIME 09:37:17 PROJECT; SBS 00-01-030"B" PROFESSIOYAI. AIRCRAFT FRA�#B : Frame Number 1 PROPERTIES FOR STRESS AMALYSIS FDR MEMBERS: 1 - 1 I, E F T FI,ANCE RICHT FLANGE PT -------•------------------- --------------------------- YO CB L/RT LD/AF CB I,/RT LD/AF KL/RX KL/RY CM F'E 1 1.750 54,471 616,000 1.750 128.750 1456.000 53,613 61.137 .850 51.952 2 1.750 54,471 616,000 1.000 12B.750 1456.000 53.613 61.137 .850 51,952 3 1.750 54,471 616,000 1.Q00 128.750 1456.000 53,613 61.137 ,850 51.952 4 1.000 37.139 420.000 1.000 128.750 1456.000 53.613 41.685 .B50 51.952 5 1.00Q 37.139 420.000 1,000 128,750 1456.000 53.613 41.685 .850 51.952 6 1,000 37,139 420.000 1.000 128,750 1456.000 S3.fi13 41.685 .850 51.95a 7 1.000 37.139 420.000 1.000 128.T50 1456.000 53,613 41.68� .850 51.952 8 1.000 19,457 220,035 1.000 19.457 220.035 53.613 21.838 .850 51.952 � � � k' - � ' - = �� � . _ =� = - -- - STEEL BUILDINC SYSTEKS, INC, P,O. BOX 447 ADEL, CA 31620 (912) 896-7428 FRAME DESIGN PAGE 4 � ------------ DATE Z/ 2/2000 TI�E 09:37;17 �' PAOJECT: SBS 00-01-030"B" PROFESSIONAL AIRCRAFT FRAKE : Frame Number 1 STRESS ANALYSIS FOR MEMBERS: 2 - Z LEFT EXTREMITY RIGHT EXTREMITY WEB ----•---------------------------------------- --------------------------------------------- ----- PT ARIAL STRESS B$YDING STRESS STRESS A%IAL STRESS BENDING STRESS STRESS SHEAR NO COHPUTED ALLOWABLE COMPUTED ALLOWABLE RATIO COHPUTED ALLOWABLE COMPUTgD ALLOWABLE RATI� RATIO , (KSI) (KSI) (RSI) (KSI) (KS1) (KSI) (KSI) (KSI) 1 -,82 30.00 -.87 30.00 .056 ,2a 24.19 1,40 30.00 ,055 .224 2 .25 24.19 -4.89 30.00 .153 .25 24.19 4,89 30,00 ,171 .198 3 ,25 24.19 -4.94 30.00 ,155 .25 24.19 4.94 30.00 .173 .198 4 .29 24.19 -10.87 30,00 .352 .24 24.19 IO.B7 30,00 .370 .145 5 .24 2d.19 -14.95 3U.00 .489 ,Z4 24,19 14.95 30,00 .507 ,092 6 .24 24.19 -17.21 30.00 .564 ,24 24.19 17.21 30.00 .582 .039 7 .24 24.19 -17.22 30.00 .564 .24 24.19 17.22 30.00 ,582 .038 8 .24 24.19 -17.64 30.00 ,578 .24 24,I9 17,64 30,00 .59fi .013 GEOMETRIC PROPBRTIES FOR MENBERS: 2 - 2 S E C T I 0 N D E S C R I P T I 0 N FULL SECTION PROP$RTI$S ---------------•---------------------------------------------- --------------------------�---- P 0 I N T LEFT FLANGE RIGHT FLANGE W E B HOM OF SECTION HODULUS NO LOCATION WIDTH THK UNBR LGTH WIDTH THK UNBR LGTH THK HBIGHT S SPACE AREA INERTIA LEFT RIGHT (FT) (IN) (IY) (IN) (I�) (IN) (IN) (IN) (IN) (IN} (IN2) (IN4) (IN3) (IN3) 1 ,38 5.0 ,250 36.4 5.0 .250 31,8 ,134 10,00 107,8 3,8 76.9 14.64 14.64 2 1.42 5.0 .250 36.4 5.0 .250 31,8 .134 10.00 107.8 3.8 76.9 14.64 14.64 3 1.44 5.0 ,250 36,4 5.0 .250 31.8 ,134 10,00 107.8 3.8 76,9 14.64 14,64 4 3.60 5.0 .250 49,0 S.0 .250 49.0 ,134 1U.00 107.8 3.8 76,9 14,64 14,6Q 5 5,76 5.0 .250 99.0 5.0 .2a0 49,0 ,13k 10.00 107.8 3.8 76,9 14.64 14.69 6 7.93 5.0 .250 49,0 5.0 .250 49.0 .134 10.00 1�7.8 3.8 76.9 14.64 14.64 7 7.95 5,0 .250 49.0 5,0 ,250 49.0 ,134 10.00 107.8 3.8 76.9 14.64 14.69 8 8,98 5,0 .250 49.0 5,0 .2a0 49,0 .134 10,00 107.8 3,B 76.9 14.64 14.64 FLANCES WEB YIELD STRESSES (KSI) 50.0 50.0 - '�1 J_ !� G� � �.� " - �� __ � - 2� - - � � STEE1 BUILDIYG SYSTEMS, INC. P.O. BOK 447 ADEL, GA 31620 (912) 896-7428 FRANE DESIGY PAGE 5 ------------ DATE 2/ 2/2000 �'I TIME 09:3T:11 PROJECT: SBS 00-01-Q3�"B" PROFESSIONAI, AIRCRAFT FRAME : Frame Num6er 1 '�� PROPERTIES FOR STRESS AYALYSIS FOR MEMBERS; Z - 2 � � � L E F T FLANGE RIGHT FLANGE PT --------------------------- --------------------------• NO CB L/RT LD/AF CB I,JRT I,D/AF KL/RX KL/RY CM F'E � 1 1,100 27.365 305.522 1,100 23.904 266.876 51.033 27,293 .850 57,339 2 1.100 27,365 305,522 1,100 23,904 26fi.B76 51.033 27.293 .850 57.339 3 1,100 27.365 305.522 1,100 23.904 266,876 51,033 27.293 ,850 57.339 4 1,000 36.867 411.fi00 1.000 36,867 411,600 51.033 42,093 ,850 57.339 5 1.000 36.867 411.600 1.000 36,867 411.600 51,033 42.093 ,850 57.339 6 1.000 36.867 411.600 1..000 36.867 411.600 51.033 42.093 .850 57.339 T 1,000 36.86T 411.600 1,000 36.867 411.600 51.033 42.093 .850 57,339 B 1.000 36.867 411,600 1.000 36.867 411.600 51.033 42,093 .850 57.339 � I �_ � , ' �_ ��� . � _ - ��� __ - r. _ _ . ( __ . ,'� _ _ �� f � STEEL BUILDIYG SYSTE�S, INC. P,O. BOX 447 ADE1, GA 31620 (912} 896-74Z8 FRA�NE DESIGN PAGE 6 ------------ DATE 2/ 2/2000 TIHE 09:37:17 PROJECT: SBS 00-01-030"B" PROFESSIONAL AIRCRAFT FRA�fE : Frame Number 1 MBHBER FORCES FOR MEMDERS: 2 - 2 ABSOLUTE MOMENTS AND AXIAL FORCES PTMEMBER MAXIMOM --------------------------------------------------------------------------- NO NUHBER SHEAR HOMBNT AXIAL MOMBNT AXIAL MOKENT AXIA1 MOMENT A%IAL � (KIPS) (K-FT) (KIPS) (K-FT} (KIPS) (K-FT) (RIPSJ (K-FT) (KIPS) 1,OD+1.OL 1,ODt1.Ok� C1 1.OD+1.OW C1 1,OD+1.0z 1.OD+1.05 1.OD+ .SS+1.OW C1 1,OD+ ,5S+1,OW Cl 1.OD+1.05+ .5W C1 1.OD+1.OS+ .SW C1 1.OD+1,OS+1.OZ 1 2 4.36 -1.21 .27 1.71 .95 1.D6 -3.I6 -.20 ,05 -.20 .04 1.71 ,95 1.06 -3,16 .78 .49 .45 -1.56 -,20 ,05 2 2 3.8fi -4.44 .24 S,9T .94 3.69 -3.16 -.11 ,04 -.71 ,04 5.97 ,94 3.69 -3.16 2.72 ,49 1.58 -1.57 -.71 .04 3 2 3.86 -4.49 .24 6,03 ,94 3,73 -3,16 -,72 .04 -.72 .04 6.03 .94 3.73 -3,16 2.75 .49 1.60 -1.57 -,72 .04 4 2 2.82 -9.86 .17 13.Z6 .94 8,20 -3.17 -1.59 .03 -1.59 .03 13.26 ,94 8,20 -3.17 6.Q4 .48 ' 3.51 -1,67 -1.59 .03 5 2 1,79 -13.57 .11 18,25 .93 11.29 -3.18 -2.19 ,02 -2.19 .02 18.25 .93 11.29 -3.18 8.31 .47 4.82 -1,58 -2.18 .02 6 2 .75 -15.61 .05 21.00 ,92 12.99 -3.18 -2.51 .O1 -2,51 .Ol 21,00 ,92 12.99 -3,18 9,56 ,46 �� 5.55 -1.59 -Z.51 .Ol , 7 2 .75 -15.62 .0� 21.02 .92 13.00 -3,16 -2.52 .O1 -2,52 ,Ol 21.02 .92 13.00 -3,18 9.57 .46 5.56 -1.59 -2,52 ,Ol 8 2 .25 -16.00 .02 21,53 .92 13.32 -3.19 -2,58 .00 -2.58 .00 21.53 .92 13.32 -3.19 9,80 ,46 5,69 -1,59 -2,58 ,00 ;' � ��_ � � ( � �� � � ���� � _ STEEL BUILDIYG SYSTEMS, INC, P.O, 80X 447 ADEL, GA 31620 (912) 896-7428 FRAME DESIGN PAGE 7 ------------ DATE 2/ 2/Z000 TIHE 09:37:17 PROJECT: SBS 00-01-030"B" PROFESSIONAL AIRCRAFT FRA�E : Frame Number 1 STRESS ANALYSIS FOR �E�BERS: 3 - 3 LEFT EXTREHITY RICHT EXTREMITY WEB --------------------------------------------- --------------------------------------------- ----- PT AXIAL STRfiSS BENDI�G STRESS STRESS AXIAL STRESS BEYDING STRESS STRESS SHEAR NO COMPUTED ALLOWAflLE COMPUTBD ALLOWABLB RATIO CO�PUTED ALLOWABLE COMPUTED ALLOWABLE RATIO RATIO (KSI} (KS1� (KSI) (KSI) (KSI) (KSI) (KSI) (KSI) 1 -.64 30,00 .00 25.93 .028 -,84 30.00 ,00 30.00 .028 .233 2 .23 29.19 4.33 25.93 .175 .23 24.19 -4.33 30.00 .135 .203 3 .23 24.19 4,39 25.93 .177 .23 24.19 -4.39 30.00 .137 .202 4 ,23 29.19 11.24 25.93 ,441 .23 24.19 -11.24 30.00 .365 ,141 5 .24 24,19 15.64 25.93 .611 ,24 24.19 -15.64 30.00 .512 .079 6 .24 29,19 17.59 30,00 ,594 .24 24.19 -17.59 30.00 .577 .018 7 .24 24.19 17.60 30.00 .594 ,24 24.19 -17.60 30.00 .5T7 .018 B .24 24.19 17.64 30.00 .596 .24 29,19 -17,64 30.00 .578 .013 GEOMETRIC PROPERTIES FOR ME�{BERS; 3 - 3 S E C T I 0 N D E S C R I P T I 0 N FULL SBCTION PROPERTIBS -------------------------------------------------------------- ------------------------------- P 0 I N T 1EFT FLANGE RIGHT FLANGE W E 8 MOM OF SECTION HODOLUS YO LOCATION WIDTH THK UNBR bGTH WIDTH THR UNBR LGTH THK HEIGflT S SPACB AREA IYERTIA LEFT RIGHT (FT) (IY) (IN) (IN) (IN) (I�) (IN) (IN) (IN) (IN} (IN2) (IN4) (IY3) �IN3) 1 ,00 5,0 ,250 93.8 5,0 .250 44,8 ,134 1Q.00 120.4 3,8 76.9 14,64 14.64 � 2 1.25 5.0 .250 93.8 5.0 .250 44.8 .134 10.00 120.4 3,8 76,9 14.64 14.64 � 3 1,26 5,0 ,250 93.8 5.0 ,Z50 44,8 .139 10,00 120.4 3.8 76.9 14,64 14.64 4 3.77 5,0 .250 93.8 5,0 .250 49.0 .134 lO.OD 120.4 3.8 76.9 14.64 14.64 5 6,27 5.0 ,250 93,8 5,0 .Z�O 49,0 ,134 10,00 120,4 3,8 76.9 14,64 14,64 6 8.77 5.0 .250 49.0 5.0 ,250 49,0 ,134 10,00 120.4 3.8 76.9 14.64 19.64 7 8,79 5.0 ,250 49.0 5,0 .2�0 49.0 .134 10.00 120,4 3,8 76,9 14.69 14,64 8 10,03 5,0 .2a0 49.0 �,0 ,250 49,0 ,134 10.00 120.4 3.8 76,9 14.64 19.64 FLA�YGES WEB YIELD STRESSES (HSI� 50,0 50,0 ( j _\� J �__�i,.- - - i� `�����_ _ ; _ � _ _ � � -- = ' ' STEEL BUILDI�G SYSTBMS, INC, P.O. BOX 447 - ADEL, GA 31620 (912) 896-7428 FRAME DESIGY PAGE B """"---- DATE Z/ 2/2000 TIME 09:31;17 PROJECT; SBS 00-01-030"B" PROFESSIONAL AIRCRAFT FRAHE : Frame Number 1 PROPERTIES POR STRESS ANALYSI$ FOR MEMBERS: 3 - 3 L E F T FLA�GE RIGHT FLANGE PT ------- ------------------- ------------------------ � YO CB L/RT LD/AF CB I,/ftT LDJAF KL/RX KL/RY CH F'E � 1 1.1Q0 70.598 T88,188 1.100 33,73I 3T6.588 51.033 38.512 .850 57,339 2 1.100 70,598 788.188 1.100 33.731 376.588 51.033 38.512 .8�0 57.339 3 1.100 70,598 786,188 1.1U0 33,731 376,588 51,033 38.512 .850 57.339 4 1.100 70.598 788.188 1.000 36.867 411.600 51.033 42.093 .850 57.339 5 1,100 70,598 188.I88 1.000 36.867 411,600 51.033 42.093 .850 57.339 6 1.000 36,867 411.600 1.000 36,867 411,600 51.033 42.093 .850 57,339 7 1,000 36.861 411.600 1.000 36.867 411,600 51.033 42.093 ,BSO 57.339 8 1.000 36.B69 911.600 1.00D 36.867 911.600 51.033 42.093 .850 57.339 . � �_„� _ � �� - - , 2 l"-_�� -� __ • • STEEL $�ILDI�G SYSfiEKS, INC. P.O, BOX 447 ADEL, GA 31620 (912) 896-7428 FRA�KE DESIGY PAGE 9 - � -------- UAT� 2J 2/20QQ ' TIHE 09;37:17 PROJECT: SBS 00-01-U30"9" PROFESSIONAL AIRCRAFT ' FRA�'�� : Frame fii�mber I ' MEMBER FORCES FOR I�E�BERS: 3 - 3 ABSOLUTE MOMENTS AND AJ( IAL FORCES PT ME�BER MAXIRUM --------------------------------------------------------------------------- NO NUHHER SHEAR MOt�ENT AXIAL t{O�ifiNT AXIAL HOMENT A%IAL HOHBNT AXIAb � (KIPS1 {K-FT) (KIPS! (K-F'fJ (KIPS) (K-FT) (KIPS) (K-FTJ (!(IPSJ I.OD+I.OL 1.OD+1.OW CI 1.OD+l.OW CI 1.OD+l.OZ 1,OD+1.OS 1,OD+ ,5S+1,OW C1 1,OD+ ,55+1.OW C1 1,OD+1.QS+ ,5�' C1 I.OD+I.OS{ .5W Cl I.OD+I,OS+2.OZ 1 3 4.54 .Oq -,28 .00 .88 .00 -3.22 ,00 -.04 .00 -,05 .00 .88 .00 -3.22 .6Q .d2 ,00 -1,63 .00 -,04 _. Z 3 3.95 3.93 -,24 -5.29 .69 -3.2? -3.22 .63 -.Q4 .63 -,09 -5.29 ,89 -3.27 -3.22 -2.41 .43 -1.40 -1,62 .63 -.04 3 3 3.9� 3.9$ -.Z4 -5.35 .89 -3,3t -3.22 ,S4 -.04 .64 -.09 -5.35 .89 -3.31 -�.22 -2,44 .43 -1.42 -1.62 .64 -.04 9 3 2,14 I0.20 -.17 -13.72 .90 -8.49 -3,21 1.64 -.03 1.64 -.03 -13.72 .9Q -8.49 -3.21 -6,25 .94 -3.63 -1.62 1.64 -.03 5 3 I.55 14.19 -,10 -19,09 .90 -11.81 -3.20 2.29 -.Q1 2.29 -.Q2 -I9.09 .90 -11.81 -3.20 -8.69 ,�a ' -5.05 -1.61 2.29 -,O1 6 3 .35 I�,96 -.�Z -21.47 .31 -13.28 -3.19 2.57 .D� 2.57 ,00 -21,4'f .91 -13,28 -3.19 -9,77 ,46 -5.68 -1.60 Z.57 .QQ 1 3 ,34 Ia.96 -.02 -21,d8 .91 -13.29 -3,19 2,57 .00 2.57 .UO -2I.48 .91 -13.29 •3.19 -9,78 .46 -5,68 -1.60 2.�7 .00 8 3 ,25 16.00 .02 -21.53 ,92 -13.32 -3.19 2.58 .00 2.58 .00 -Z1.53 .92 -13.32 -3.I9 -9.80 .d6 -5,69 -1,59 2,58 .DO � � - l/. �/ , �-'' �� -� - ' ' STEEL BUILDING SYSTEMS, IYC. P,O. BOX 447 ADEL, GA 31fi20 (912) 896-7428 FRAME DESIGY PACE 10 ------------ DATE 2/ 2/2000 TI4E 09:37:18 PROJECT; SBS 00-01-030"8" PROFESSIONAL AIRCRAFT FRA��4E : Fr2me Number 1 FORCES ACTING ON SUPPORTS LOADINC COYDITION ------------------------- ------------------------------------------- SUPPORT HORIZONTAL VERTICAL MOPtENT � NO D E S C R I P T I 0 N NO (KIPS) (KIPS) (K-FT} 1 1.OD+1,OL 1 .00 3,39 .00 1 1.OD+1.OI, 4 ,QO 3.39 .00 TOTAL FORCES ACTING .00 6.78 TOTAL FORCES APPLIED .00 6,78 ' 2 1.OD+1.OW C1 1 1,32 -4.45 .00 2 1.ODt1.OW C1 9 ,50 -4.60 .00 TOTAL FORCES ACTINC 1.83 -9.OS TOTAL FORCES APPI,IED 1,83 -9.05 3 1.OD+1,Ob' C1 1 -Z,91 -3.06 .OD 3 1.OD+1,OW C1 4 -3.45 -2,53 .00 TOTAL FORCES ACTING -6.36 -5.60 TOTAI, FORCES APPLIED -6.36 -5,6U 4 1.OD+1,OZ 1 .00 .55 .00 4 1.OD+1.0z 4 .00 .55 .p0 TOTAL FORCES ACTIyG .00 1.09 TOTAI, FORCES APPLIED ,00 1.09 a 1.OD+1.OS 1 ,00 .55 ,00 a I,OD+I.OS 4 ,00 ,55 .00 TOTAL FORCES ACTING .00 1.09 TOTAL FORCES APPLIED ,00 1.09 6 I.OD+ .SS+I.OW C1 1 1.32 -4.45 ,00 6 1,OD+ .5S+I.01� C1 4 ,50 -4,60 .00 TOTA1 FORCES ACTINC 1.83 -9,05 TOTAL AORCES APPI,IED 1.B3 -9.05 7 1.OD+ .5S+1.OW C1 1 -2,91 -3.06 ,00 7 1,OD+ .5S+l.OW C1 4 -3.45 -2,53 .00 TOTAb FORCES ACTING -6.36 -5.60 TOTAL FORCES APPf,IED -6,36 -S.fiO 8 1.OD+l.OS+ .5W C1 1 ,66 -2,02 .00 . , , � . _ �� . _ /� ��d _ L�� � � • STEE1 BUILDIYG SYSTBMS, IVC. � P.O, 80� �d7 ADEb, GA 31624 (912f $9&-742$ FRAME DESIGN ' PAGE lI ._._.....__. �AT� �J 2J�000 TIMB ti9,37,1$ PROJECT: SBS 00-QI-030"9" PRpFB5SI0NAL AIRCRAFT FRAKE : Frame vuarber t PQBC�S ACTIN6 ON SUPPOR'FS 14ADING CQNDITIDY ---------------------•--- -------_...-------------------------------- SUPPORT HORIZONTAb VERTICAI� �iOMB�IT � NO D E S C R I P T I 0 N NO (KIP5) (KIPS} (K-FTj B l.OD+1.OS+ ,5W Ci d .25 -2.I0 .04 TOTAb FORGES ACTI�iG ,91 -4,12 TOTAL F4RCES APPLIED .91 -4,12 9 I.OD+I.OS+ .5W C1 1 -1.46 -1.33 .00 9 t.OD+I,OS} .SW C1 4 -1,72 -1,06 ,00 TOTAL FORCES ACTING -3,18 -2.39 TO'�AL FORCES APPLIBD -3.18 -2,39 10 I..flD+1.DSf1.02 1 .QR .55 .40 10 1.4D+1,OSt1,QZ 4 .04 .55 .00 1'QTAL PQRCES ACTING .Q4 1.09 TOTA1 FQRCfiS APPLIED .00 1.09 _ � �� .= _ _ � _ � �� ��� �-. e .-� Gs'T, .� ; r� ` ' -� - � : .' �°(., " � _u� .., . �.,.� - .. ' ' STEEL BUILDINC SYSTEMS, IYC, , P.O, BOX 447 ADEL, GA 31fi20 (912) 896-74Z8 FRAi4E DESIGY PAGE 12 ------------ DATE 2/ Z/2000 TIME Q9:37:18 PROJECT: SBS 00-01-030"B" PROFE5SIONAL AIRCRAFT FRAME : Frame Number 1 E�TERNAL M$MBER LOADS � UNIFORMLY LOADING CONDITION DISTRIBUTED LDADS C 0 N C E N T R A T E D L 0 A D S ----------•-------------- MEMBER -------------------- -------------------------------------- HO D E S C R I P T I 0 N NUMBER VBRTICAL HORIZONTAL LOCATION VEHTICAL HORIZONTAI, MOMENT � (KfFT} (K/FT) (PT) �KIPS) (KIPSf (K-FT} 1 1.OD+1.OL 1 ,000 .000 1 1.OD+l,OL 2 ,358 .000 1 1.OD+1,OL 3 .358 .000 2 1.OD+1.OW C1 1 .000 .130 2 1.OD+1.0� C1 Z -.4T7 -,521 2 1.OD+1,OW Cl 3 -,478 -.521 , 3 1.OD+1.OW C1 1 .000 -.286 � 3 I.OD+I.OW C1 2 -.295 -,338 3 1.OD+1.OW C1 3 -.295 -.338 4 1.OD+1.OZ 1 ,000 .000 4 1.OD+1.OZ 2 .058 .000 ' 9 1,OD+1,OZ 3 .058 .OQO 5 1.OD+1.OS 1 .000 .000 5 I.OD+I,OS 2 .058 .00U I � 1.OD+1.OS 3 .058 .000 , 6 1,OD+ .5S+1.OW C1 1 ,000 ,130 � 6 1.OD+ ,SS+1,OW Cl 2 -.477 -.521 6 1.OD+ ,SS+1.OW C1 3 -.918 -,521 , 1 I.OD+ ,5S+1.OW C1 1 .000 -.286 , 7 1.OD+ .5S+1.OW C1 2 -.295 -.338 T 1.OD+ ,SS+1,OW Cl 3 -.295 -.339 8 I.OD+I.OS+ .5W C1 1 .000 .O6S 8 I,OD+I,OS+ .5W C1 2 -.217 -.260 8 1.OD+1.OS+ ,5W C1 3 -.217 -.260 9 I.OD+I.OS+ .SW C1 1 .000 -.143 9 1,OD+1.OS+ .SW C1 2 -.126 -.1fi9 9 1.OD+l.OS+ .5W C1 3 -.126 -.169 :0 1.DD+1.OS+1.OZ 1 .000 .000 !0 1.OD+1.OS+1.OZ 2 .056 .000 :0 1,OD+1,OS+1,OZ 3 .058 .000 � _, . -� � -��- � � ���� - � _=.-�-���_ . . _- - _ -_ r f � � STEEL BUIIDI�G SYSTE�S, INC. P,O. 80X 447 AD�L, CA 3162Q (912� 896-742$ FRAME DESIGN PAGE I3 ------------ DATE 2J 2j2000 TI�B 09;37:18 PROJBCT: SBS 00-01-030"B" PROPESSiOYAL AIBCRAFT PRAMB : Frame Number 1 EXTER�AL J4INT LQADS bOADING C4NDITION d 0 I N T � 0 A D -------------------------- JOINT ----------.._..------------- �0 Il E S C R,I P I T I 0 N NU�iBER VERTICA� HORIZ0�1'�L MO�ENT (xIPSj (KIPS) (K-Ffi} - 4 I.ODiI.OZ 2 .00 10 1,OD+I,OS+1.02 2 .04 �-�...._— � � �� � . 3 � � STEEL BUILDING SYSTEMS, I�C. P.O. BOX 447 ADEL, GA 31620 (912) 896-7428 FRAME DESICN PAGE 14 ------------ DATE 2/ 2/20�0 TIHE 69:37:18 'ROJECT; SBS 00-01-030"B" PROFESSIONAL AIRCRAFT �RAME ; Frame Yu�ber 1 IE�tBER END TRANSLATIONS I,OADINGCONDITION EflD TRANSLATIONS ------------------------- --------------------------------------------- fEKBER NO D E S C R I P T I 0 N JOI,tT VEET HORZ JOINT VERT , HORZ - NO (IY� (IK) NO (IN) (I�) I 1 1.OD+1,01 1 .00 .00 2 -,O1 .00 1 2 1.OD+l,OW C1 1 ,00 .00 2 .Ol .00 1 3 1.OD+1.OW C1 1 .00 .00 Z .O1 -.O1 1 4 1.OD+1.OZ 1 ,00 ,00 Z .00 .00 1 5 1,OD+1.OS 1 .UO .00 2 .00 .00 1 6 1.0➢+ .55+1.0{� Cl 1 .OD .00 2 .O1 .00 1 7 1.OD+ .5S+1.OW C1 1 ,00 .00 2 .O1 -.O1 1 8 1.OD+1.OS+ .5W C1 1 .00 .00 2 .00 .00 1 9 1.OD+1.OS+ .5W C1 1 ,00 .00 2 .00 .00 1 10 1,OD+l,OS+1.0z 1 .00 ,00 2 ,00 .00 2 1 1.OD+1,UL 2 -.O1 .00 3 -.46 .04 2 2 1.OD+1.OW C1 2 .O1 .06 3 ,6Z -,05 Z 3 1.OD+1.OW C1 2 .O1 -,O1 3 .39 -.04 2 4 1.OD+1.OZ 2 .00 ,00 3 -.07 .O1 2 5 1,OD+1.OS 2 .00 .DO 3 -,07 .O1 2 6 1.OD+ ,SS+1.0� C1 2 .O1 .00 3 .62 -,65 2 7 1.OD+ ,5S+1.OW C1 2 .O1 -.O1 3 .39 -.04 2 8 1.OD+1,OS+ .5W Ct 2 ,00 ,00 3 ,28 -,02 2 9 1.OD+1.OS+ .SW C1 2 .00 .00 3 .17 -.02 2 10 1.OD+1,OS+1,OZ 2 .00 ,00 3 -.O7 ,O1 3 1 1.OD+1.OL 4 .00 .00 3 -,46 .04 3 2 1,OD+1,OW C1 4 .00 .00 3 .62 -.OS 3 3 1,OD+1.OW C1 4 .00 .00 3 .39 -,04 3 4 1.OD+1.OZ 9 .00 ,00 3 -.07 .O1 3 5 1.OD+1.OS 4 ,00 .00 3 -,07 .O1 3 6 1.OD+ ,5S+1,UW Cl 4 ' .00 .00 3 .62 -.05 3 7 1.QD+ .SS+1.OW C1 4 .DO .00 3 ,39 -.0� 3 8 1.OD+1.OS+ ,5W C1 4 .00 ,00 3 .28 -,02 3 9 1.Q➢+1,OS+ ,5W Cl 4 .00 .00 3 .17 -.02 3 10 I,OD+I.OS+I,OZ 4 ,00 ,OQ 3 -,07 .O1 ODULUS OF ELASTICITY (KS1) 29000.00 �� - __ J(� �- - �.-��� ' - ' ` STEEL BUILDIYG SYSTEMS, IYC. P.O. BOX 447 ADEL, GA 31620 (912� B96-7428 FRA�NE DESIGR PAGE IS ------------ DATE 2/ 2/2000 , TIME 09:37:18 �OdECT; SBS 00-Q1-030"B" PROFESSIONAL AIRCRAFT �AHE : Frame Number 1 ` 3KB FLANGE F L A v G E T H I C K FLANGE WIDTH TO THICKNESS FLC/WEB WEB �IQ THK/THK L E F T RIGHT L E F T RIGHT THICK �EB THICKNESS HT/THK MAR MIN KAX MIN MAX MAX MIN KAX MIY HIN �IY MAX HAg 1 2,5 .150 2.000 ,150 2.000 41.000 B.00Q 41,000 B.000 .900 .100 .875 236.000 � 2 a.5 ,150 2.Q00 .150 2,000 41.000 6.Q00 41.000 8.000 .900 .100 .875 236.000 - 3 2.5 .150 2.000 .150 2.000 41.000 8,000 41.000 8.000 .900 .100 .895 236.000 � / , ,' o v � 1i� ; - - � i •• STEEL BUILDINC SYSTEMS, INC, P,O, BOX 447 ADEL, GA 31fi20 (912) 896-9428 FRAME D�SIGY PAGB 16 __.._._.___. DATE 2/ ZJ2000 TIKE 09:37:18 PROJECT; SBS 00-01-030"B" PROFESSIONAL AIRCRAFT FRAME : Frame Nu�ber 1 KEMBER HEMBER �^ � �__ Y TYPE N0, LE�GTH WEICHT (FT) (LB) 1 1 19.95 E95. - Z B.60 112. 3 10,03 131, SUBTOTAL 538. HAUNCH 11. TOT�iL 38.59 549. DENSITY (I,B/IN3) ,2833 ; , � _ U �' � ^ � -��� _ � -"`. - �� _ . ' �, ' � ' STEEL BUILDING SYSTEKS, INC. P.O. BOX 497 AD�L, GA 31620 (912) 896-1428 FRA�E SUHMARY PAGE 1 ------------- DATE 2/ 2/2000 TIME 10:52:01 PROJECT: SBS 00-01-030"A" PROFESSIONAL AIRPORT FRAKE ; Frame Number 1 FRAME TYPE IS TC GB SPAY (ft) 100.00 . EAVE HEIGHT (Pt� 23.00 ROOF SLOPE (ft) 1.D0 ' BAY SPACING (ft} 25,00 GIRT DEPTH (in) 8.00 ', PURI,IN DEPTH (in) 8,00 , FI,ANGE YIELD (KSI) 50.00 WEB YIELD (KSI) 60.00 ' LIVE (SYOW) LOAD (psf) 12,00 � SNOW LOAD (psf) .00 ' WIND LOAD (psf) 28.37 AUX DEAD LOAD (psf� .00 DEAD LOAD (psf) 3.22 tAFTER PLANGE BRACE LOCATIONS For design purposes the rafter Was assueed - braced at purlins (numbered from left sidewall): � 1 2 3 4 6 810 ;OI,IIKN BRACING For design purposes the column was assumed � braced at girts (nvmbered from-floor line): Left sidewall: 3 Right sidewall: 3 i . ^ � I - . - ���� � _. . � . � STEEL BUILDING SYSTEMS, INC. P.O. BOX 447 ADEL, CA 31620 (912� 896-7428 FRAME DESIGN PAGE 1 ------------ DATE 2/ Z/2000 TIME 10:51:59 PROJECT: SBS 00-01-030"A" PROFESSIONAL AIBPORT FRA�KE : Frame Yumber 1 STRESS ANALYSIS FOR MEMBERS: 1 - 2 LEFT EXTREMITY RIGHT EXTREMITY �EB --------------------------------------------- --------------------------------------------- ----- PT AXIAL STRESS BENDING STRESS STRfiSS AxIAL STRESS BENDING STRESS STRESS SHEAR YO COMPUTED ALLOWABLE COKPOTED ALLOWABLE RATIO COMPUTED ALLOWABLE COMPUTE� ALLO�ABLE RATIO RATIO (KSI) (KSI) (RSI) (KSI) (KSI) (KSI) (KSI) (KSI� 1 2.20 24,70 .00 30,00 .089 2,20 24.70 .00 30.00 ,OB9 .417 Z -2.30 30.00 11.83 27,Z2 .356 2.02 24.59 7.30 18.71 .957 .443 3 -2,13 30.00 17,98 Z6,fi3 ,604 1.88 24,48 11.46 18.35 .687 ,535 4 -1.99 30.00 21.36 26.12 .751 1.75 29.37 14.03 17,98 .839 .620 5 -1.87 30.00 23.21 25.67 .842 1,63 24.26 15,71 17.61 .946 .699 6 -1.79 30,00 20.73 29.79 .686 1.56 24.39 15.39 17.48 .930 .699 7 -1.68 30.00 21.7fi 26.82 .755 1.46 23,98 16.51 17.05 1.017 .779 8 -1.58 30,00 23.20 25.52 .817 -1,58 30.00 -19.32 30.00 ,697 .884 �EOHETRIC PROPERTIES FOft MBMBERS: 1 - 2 S E C T I 0 N D E S C R I P T I 0 N FULI, SECTION PROPERTIES -------------------------------------------------------------- ------------------------------- P 0 I iV T LEFT FLANGE RIGHT FLA�ICE W E B �tOM OF SECTION MODULUS �0 LOCATION �'IDTH THK UNBR LGTH WIDTH THK UNBR LGTH THK HEIGHT S SPACE AREA INERTIA LEFT RIGHT (FT) (IN) (IN) (IN) (IN) (IN) (IN) (IN) (IN) (IN) (IN2) (IN4) (IN3) (IN3) 1 ,00 8.0 ,313 88.0 8.0 .500 208.0 .188 12.00 251.8 8.8 Z67.5 36.10 49,53 2 3.16 8,0 .313 88.� B.0 .500 208,0 .188 15.86 251.8 9.5 477,1 49,89 67.10 3 6,32 8.0 .313 88.0 8,0 ,500 208.0 .188 19.72 251.8 10,2 7a6,3 64.74 8a,46 4 9.�8 8.0 .313 60.0 B.0 .500 206.0 ,186 23.58 Z51.8 10.9 1111.0 80.63 104.66 . a 12.64 8.0 ,313 60.0 8.0 .500 209.0 .188 27.49 251,8 ll,fi 1546,9 97.55 124,71 6 12.66 8.0 .375 60,0 B4O .500 208.0 ,188 27,46 251.8 12.1 1610.1 109.36 127,84 7 16,15 8.0 .375 60.0 8.0 .500 208,Q .188 31:73 251,8 12,9 2290.6 130,90 151.63 8 19.65 B.0 .375 27.5 8.0 .500 27.5 .188 36.00 251.8 13.8 3029.0 153.63 176.52 FLANGES WBB YIELD STRESSES (KSI) 50.0 50.0 . _ ^ _ � o2�'�a-_ _ � STEBL BUILDING SYSTEMS, INC. ' P.O. BOX 447 ADEL, GA 31620 (912) 896-7428 FRAKE DESIGN PACE 2 ------------ DATE 2/ 2/2000 TIME 10:51:59 PROJECT; SBS 00-01-030'A" PROFESSIONAL AIRPORT FRAME : Frame Number 1 PROPERTIES FOR STRgSS AYALYSIS FOR MEHBERS: 1 - 2 L E F T FLANGE RIGHT FLAN6E PT --------------------------- --------------------------- v0 CB LJRT LD/AF CB L/RT LD/AF KL/BX KL/RY CM F'E 1 1.451 41,348 451.000 1.451 93.452 666.250 47.T53 44,201 .850 65.486 2 1.451 42,282 586,873 1.000 94.604 866,972 48.435 45,997 .85U 63,655 3 1.451 43.183 722,746 1.D00 95,762 1067,693 49.156 47.121 ,850 61.800 9 1.000 30.037 585.42Z 1.000 96.923 1268.415 49.870 33.671 .850 60,043 5 1.000 30,614 678,063 1.000 98.084 1469.136 50.559 34.767 .850 58.919 6 1.000 29.740 566.714 1,OQ0 98.511 1473.455 99,729 34,220 .8�0 60,366 7 1.000 30.262 652,107 1.000 99.817 1695.478 50,462 35,329 ,850 58,643 8 1.000 19.112 338.194 1.000 13.375 253.646 51,154 16.693 .850 57.068 , , - - ,, ` - l�J� s �=��;a - � STEEL BUILDING SYSTEMS, IYC. ' � P.O. BOX 447 � ADEL, GA 31620 (912) 896-7428 FRA;KE DESIGy PAGE �3 ------------ DATE 2/ 2/2000 TIME 10:51:59 'ROJECT: SBS 00-01-030"A" PROFESSIONAL AIRPORT �RAKE : Frame Number 1 :E�fBER FORCES FOR MBNBERS: 1 - 2 ABSOLUTE MOMENTS AND AXIAL FORCBS 'T MB+fBER MAXIMU►1 --------------------------------------------------------------------------- 0 MIHBER SHEAR MOMENT AXIAL MOMENT AXIAL MOMENT AXIAL MOHENT AXIAL (KIPS) (K-FT) (KIPS) (H-FT) _ (KIPS� (K-FTJ (KIPS� (K-FTJ (KIPS� I.OD+I.OL 1.OD+1,Ok! C1 1,OD+1,OW C2 1.OD+1.OZ 1,OD+1.OS 1.OD+ ,55+1.0� C1 I.OD+ .5S+1,OW C2 I.OD+I.OS+ .5� C1 , 1,0➢+1.OS+ .5W C2 1.OD+1.OS+1,OZ 1 1 15.77 .00 19.24 ,00 -21.78 .00 -11.36 .00 4.07 � .00 4.07 ,00 -Z1.78 .00 -11.36 ,00 -9.36 .00 -9,15 .00 4.07 1 2 15.77 .00 19.24 ,00 -15.50 .00 -5.07 .00 4.06 .00 4.07 .00 -15.50 .00 -5.07 .00 -6.22 ,DO -1.01 .00 4,08 2 1 15.3a 40.79 19,18 -49,17 -21.77 -33.12 -11,31 8.61 4.06 8.64 4.06 -49.17 -21.77 -33.12 -11.31 -21.34 -9.36 -13,32 -4.13 8.61 4.06 2 2 15.35 90.79 19.19 -26.53 -15,55 -10.49 -5.10 8,66 4.07 8.69 4.06 -26.53 -15,55 -10.49 -5,10 -10.03 -6.25 -2.00 -1.02 8.66 9.U7 3 1 14.93 81.59 19.12 -97.00 -21,76 -62.80 -11.27 17.23 4.05 17,2B 9.05 -97.00 -21.76 -62.80 -11.27 -42,Q2 -9,36 -24,91 -4.12 17,23 4.05 3 2 14.93 81.59 19.12 -55,98 -15.61 -21.98 -5.12 17,32 4.05 17.28 4.05 -55.98 -15,61 -21.78 -5.12 -21.51 -6.28 -4.40 -1.04 17,32 4,05 4 1 14.51 122.40 19.07 -143.51 -21,75 -89.02 -11.23 25.85 4.03 25.92 4.04 -143,51 -21.7a -89.02 -11.23 -62.03 -9.36 -34.78 -4,10 25.85 4.03 4 2 19.51 122.90 19.07 -88.35 -15,66 -33.86 -5.14 25.98 4.0� 25,9Z 4.04 -88.35 -15.66 -33.86 -5.19 -34.45 -6.31 -7.20 -1.05 25.98 4.04 a 1 14.09 163,21 19.01 -188.70 -21,74 -111,80 -11,18 34.47 4.02 34,56 9.03 -188.70 -21.74 -I11.B0 -11.18 -81,38 -9.36 -42.93 -4.08 34.47 4,02 a 2 14.09 163.21 19.01 -123.63 -15,71 -46.73 -5.16 34,64 4,03 34.56 4.03 -123.63 -15.71 -96.73 -5.18 -48.84 -6.35 -10.39 -1.07 34.64 4.03 6 1 14,08 163.43 19,01 -188,94 -21,74 -l1t.91 -11,18 34.51 4.02 - 34.61 4.03 -188.94 -21.74 -111.91 -11.18 -B1,48 -9.3fi ` -42.97 -4.08 34,51 4.02 6 2 14.OB 163.�3 19.01 -123.82 -1a.11 -46.80 -5.16 34.69 9.03 " 34.61 4.03 -123,82 -15,71 -46.80 -5.16 -48,92 -6.35 -10.41 -1.07 34.69 9.03 �� 7 1 13.62 208.59 18.94 -237.36 -21,73 -133.07 -11.14 4�.05 4.01 � - - 44.17 4.01 -23T.36 -21.73 -133,07 -11.14 -102.10 -9.36 -49.96 -4.06 49.05 4.01 }� � ' � ' 2 13,62 208.59 18,99 -166.2fi -15.77 -61,97 -a,1B 44.27 4.02 � ✓p�.V`� ' 44,17 4.01 -166.26 -1�.77 -61,97 -a,18 -66.5a -6.38 -19.41 -1,09 94.27 9.02 �__ - - Qa����� s v � 00'fi 99'ES OI'I- 88'BI- I6'9- 96'S9- iZ'S- II'8L- £8'SI- 9ti'ZIZ- DO'V 6L'£5 00'6 98'ES IZ'S- II'8E- E8'SI- 9Z'ZIZ- 8B'Bi 9L'ESZ G9'EI Z 8 00'� 6S'ES fi0'6- �8'65- I 9E'6- I6'ili- 60'tt- ZO'OSI- IL'IZ- GI'68Z- OD'Y bt'ES , 00'6 6S'ES 60'II- ZO'OSI- il'IZ- LI'�9Z- 88'8I 9L'ESZ L9'EI � I 8 � STEEL BUILDING SYSTEMS, INC. ' P.O, BOX 441 ADEL, GA 31620 (912) 896-T428 FRANE DESIGY PAGE 4 ------------ DATE 2/ 2/2000 TIME 10:51:59 ROJECT: SBS 00-01-030"A" PROFESSIONAL AIRPORT RA�KE ; Frame Nu�ber 1 1'RESS ANALYSIS FOR MEMBERS: 3 - 4 I, EFT EXTREMITY RIGHT EXTREMITY WEB t AXIAI, STRESS BENDING STRESS STRESS AXIAL STRESS BEYDING STRESS STRESS SHEAR IO COMPUTBD ALLOWABI,E COMPUTED ALLOWABLE RATIO COMPUTED ALLOWABI,E COMPUTED ALLOWABLE RATIO RATIO (KSI) (KSI) (KSI) (KSI) (KSI) (RSI) (KSI) (KSI) 1 -1.18 30.00 23,20 25.47 .872 1,13 22,26 20.94 25.47 .B66 .507 2 -1.25 30.U0 20.81 26.00 .759 1.19 Z2.06 19.03 26.00 .778 .4Z2 3 -1,34 30.00 18.07 26,31 .642 1.26 21.76 16.81 26.31 ,687 .345 � -1.44 30.00 14.65 26.66 .509 1.34 Z1.29 14.18 26.66 .582 .275 a -1.86 30.00 18.87 22,59 .773 1.74 19.56 18,02 22.59 .875 .652 i -1.99 30.00 14.45 23.04 .561 1.84 18,22 14.36 Z3.04 .703 .S1B 1 -2.15 30.00 10.13 23.59 ,359 1.95 17,62 9.88 23.54 .503 .400 :3 -2.32 30.00 5,74 24.09 ,161 2.09 16.57 4.13 24.09 .2B8 -,297 80METRIC PROPERTIES FOR MEMBERS; 3 - 4 S E C T I 0 N D E S C R I P T I 0 N FULL SECTION PROPBRTIES -------------------------------------------------------------- ------------------------------- ' 0 I N T LEFT FLA;YGE RIGHT FLANGE W E B MOM OF SECTION MODULUS l I,OCATION WIDTH THK UNBR I,GTH WIDTH THK IINBR LCTH THK HEIGHT S SPACE AREA INERTIA LEFT RIGHT (FT) (IN) (IN) (IN� (IN) (IN)' �IN) (IN7 (IN) (IN) (IN2) (IN4� (IN3) (IN3) 1.32 8.0 .313 24.7 8,0 .313 8.9 .250 36.00 244.0 14.0 2620.3 143.09 143.09 � 4.6� 8.0 .313 60.0 B.0 .313 60.0 .250 32,67 244.0 13,2 2086.6 125.33 125.33 ' 7,98 8.0 .313 60.0 8.0 ,313 60,0 .250 29.34 244.0 12,3 1625.9 108.50 106.50 11.31 8,0 .313 60,0 8.0 .313 60,0 .250 26.02 244.0 11.5 1233.4 92.59 9Z.59 11,33 8.0 ,250 60.0 8.0 .250 60.0 .188 26.00 244,0 8.9 963.7 72.73 72,73 14.33 8,0 ,250 60.0 B.0 .250 60.0 .16B 23,00 244.0 B,3 730.7 62.19 62.19 ' 17,33 8.0 ,250 60.0 8,0 .250 120.0 .168 20.00 294.0 7.7 535.1 52.20 5Z.20 ZD,33 B.0 .250 60.0 8.0 .250 120.0 .1B8 17,00 244.0 7.2 379.3 42.78 92.78 FLANGES WEB ELD STRESSES (KSI) 50,0 50,0 .. s �-��-� �� � STEEL BUILDING SYSTEMS, INC. ' P,O. BOX 447 ADEL, GA 31620 (912j 896-7428 FRA�B DESIGV PAGE a ------------ • DATE Z/ 2/Z000 TIME 10:52:00 30JECT: SBS 00-01-030"A" PROFESSIONAL AIRPORT RAHE : Frame Number 1 30PERTIES FOft STRESS ANALYSIS FOR MEMBBRS: 3 - 4 L E F T FLANGE RIGHT FLANGE r --------------------------- ---------------------•----- - } CB L/RT LD/AF CB I./RT LDJAF KL/RX KL/RY CM F'E ! 1.240 13.552 362,469 1.240 4.890 130,T88 4Z.157 6.463 ,850 84.025 : 1.000 32.289 799,132 1.000 32.289 199.132 45.616 42.129 .850 71,139 3 1.000 31,704 719.264 1.000 31.704 719.Z64 50.237 40.780 .850 59,169 ': 1.000 31.108 639.395 1.000 31.108 639.395 55.700 39.384 .650 48.133 � 1.000 30,809 794.990 1,000 30.809 794.990 55.347 38.686 ,850 48,748 i 1,000 30.29Z 704.993 1.000 30.292 T04,993 61.515 37.942 .850 39.462 ' 1.000 29,765 614.997 1,000 59.529 1229.993 69.410 36.154 .850 30.996 1.000 29.228 525.000 1.000 58.457 1050.000 79,916 34.819 .850 23.382 � �, --a0�� STEEL BUILDINC SYSTEKS, iYC. • � P.O. BOX 447 ADEL, GA 31620 � (912) 99fi-7428 FRAME DBSIGY PAGE 6 ------------ DATE 2J Z/2000 TIME 10:5Z:00 �OJECT: SBS 00-01-030"A" PROFESSIONAL AIRPORT tA�E ; Frame Number 1 iMBER FORCES FOR ME�BERS: 3 - 4 ABSOLUTE MOMENTS AND AXIAL FORCE.S ' MEMBER MAxIMUM --------------------------------------------------------------------------- ) NUMBER SHEAR MOMENT AXIAL MOMENT AXIAL MOMBNT AXIAL NOMENT AXIAL (KIPS) (K-FT) (KIPS) (K-FT) (KIPSj (K-FT) (KIPS) (K-FT) (KIPS) 1.OD+1.OL 1,OD+1,OW C1 1.OD+1.OW C2 1.OD+1,OZ . 1,OD+1.DS 1.OD+ .55+1.0I� C1 1.OD+ ,5S+1,OW C2 1,OD+1.OS+ ,SW Cl 1.OD+1.OS+ .SW C2 1.OD+1.OS+1.OZ 1 3 18.58 249.66 15.86 -276.6fi -I6.47 -192.04 -5.61 52.72 3.37 52.87 3.36 -276,66 -16,47 -142.04 -5.61 -118.49 -6,97 -51.18 -1.54 52,71 3,37 1 4 18.58 249.66 15.86 -213.49 -16.54 -78.88 -5.68 53.00 3.37 52.87 3.36 -213.49 -16.54 -78,88 -5.68 -86,90 -7.01 -19.60 -1.58 53.00 3.37 2 3 17,U1 198.76 15.71 -217.39 -16.49 -110.41 -5.63 41,95 3.33 42.09 3,33 -219.39 -16.49 -110,41 -5.63 -92.90 -7.00 -39.41 -1.51 41.95 3.33 I� 2 9 17.01 198.76 15,71 -172.21 -16.57 -65,23 -5.71 42.21 3.33 42.09 3.33 -172,21 -16.57 -65,23 -5.71 -70,31 -7.04 -16.82 -1.60 42.21 3,33 i 3 3 15.43 152.01 15.56 -163.37 -16.52 -81.66 -5.66 32.06 3.30 I 32.19 3.29 -163.37 -16.52 -91,66 -5.66 -69.60 -7.02 -28,75 -1.59 32.06 3.30 3 9 15.43 152.01 15.56 -134.10 -16.59 -52,39 -5.73 32.30 3.30 32.19 3,29 -13�.10 -16,59 -52.39 -5.73 -54.97 -7.06 -14.11 -1.63 32.30 3.30 I 3 13.86 109.42 15.90 -11�.59 -16.54 -55.78 -5.68 23.06 3,27 23.1T 3.26 -114,59 -16.59 -55.78 -5.68 -46.60 -7.05 -19.19 -1.62 23.05 3.27 ! 4 13.86 109,43 15.40 -99.17 -16.62 -40,36 -5.76 23.28 3.27 23,17 3.26 -99.17 -16.62 -40,36 -5.76 -4Q.89 -9.08 -11,4B -1.65 23.28 3.27 i 3 13.85 109.2Z 15,40 -114.35 -16,54 -55.66 -5.68 23.01 3.27 23.13 3.26 -114.35 -16,54 -55,66 -5.68 -48.50 -7.05 -19.15 -1.62 23.01 3.27 i 4 13.85 109.22 15.40 -99.00 -16.62 -90.30 -5.76 Z3.23 3.27 23,13 3,26 -99.00 -16,62 -40.30 -5.76 -40.82 -7,08 -11.47 -1.65 23.23 3.27 i 3 1Z.43 74,41 15.26 -74,89 -16,57 -34.81 -5,70 1�,65 3.24 15.76 3.23 -74.89 -16.57 -34.81 -5,70 -31.53 -7.07 - � -11.49 -1,64 15.65 3.24 - � ; 4 12,43 74,41 15,26 -70.24 -16.64 -30.1T -5.78 15.85 3.24 15,76 3.23 -70.29 -16,64 -30,17 -5.78 -29,21 -7,11 �' -9.17 -1.68 15.85 3.24 1 ' 3 11.02 42,99 15.13 -39.69 -16.59 -16.31 -5.73 9.01 3.21 `� 9.10 3.Z0 -39,69 -16.59 -16.31 -5.73 -16.43 -7.09 � ( � -9.74 -1.66 9.01 3.21 I � ��� D� � 4 11,02 42,99 ,1a,13 -44.07 -16.66 -20.69 -�.80 9,19 3.21 9,10 3,20 -44,07 -16,66 -20.69 -a,80 -18,62 -7.13 -6,93 -1.70 9.19 �.Z1 ��-��-� - - _ � s 8I'E SZ'E ZL'I- �L'6- SI'L- SO'6- 28'S- L8'II- 89'9I- L�'OZ- LI'E 9i'E 8i'E 5Z'E Z8'S- G8'Ii- 89'9I- G6'OZ- 66'tii ti6'YI 09'fi b B 8I'£ 80'E 89'i- Zi'i It'L- Bi'E- St'S- Si'- t9'9I- Y6'B- Li'C 9i'£ BI'£ BO'E Sl'S- Si'- i9'9i- 6L'8- 66'�i 66'�i 09'6 � E 8 STEEL BUILDING SYSTEMS, INC. '� ' P.O. BOX 447 ADEL, GA 31620 (91Z) 896-7425 FRANE DESIGY PAGE 7 ------------ DATE 2/ 2/2000 TIMB 10:52;00 PROJECT: S9S 00-01-030"A" PROFESSIONAL AIRPORT FRA�E : Frame Number 1 STRESS ANALYSIS FOR MEMBERS: 5 - 6 LEFT EXTRE � ITY RIGHT EXTREMITY WEB --------------------------------------------- --------------------------------------------- ----- PT AXIAL STRESS BENDING STRESS STRESS AXIAL STRESS BENDING STRESS STRESS SHEAR , YO COMPUTED ALLOWABLE COMPUTED ALLOWABLE RATIO CO�PUTED ALLOWAB6E COMPUTED ALLOWABLE R�TIO RATIO (KSI) (KSI) (KSI) (KSI) (KSI) (KSI) (KSI) (KSI) 1 -2,58 30.00 6,09 22.93 .180 2.30 16,38 4,45 22.93 .322 .883 � Z -2.48 30.00 -5,66 30.00 .271 -2.48 30.00 5.66 22.66 .167 .822 ' 3 2.16 16.79 9.05 22.40 ,503 -2.42 30.00 11,57 22.40 .43fi .744 4 2.09 16.81 13.14 E2.16 .691 -2.36 30.00 15.63 Z2,16 .627 .647 a 2.09 16,81 13.16 22.16 - .692 -2.36 30.00 15.65 22.16 .627 ,647 6 2.02 16,76 16.10 21,85 .834 -2.30 30.00 18,34 21.85 ,763 ,546 7 1.96 16.65 17.80 21,44 .927 -2,24 30,00 19.64 21.44 .841 .460 8 1.90 16.50 18.50 21.03 .976 -2.18 30.00 19.B0 21,03 .869 .373 9 1.90 16.49 I8.50 21.03 .976 -2.18 30.00 19,80 21.03 .869 ,372 10 1.84 16.33 18.92 20.64 .988 -2.13 30,00 19.13 20.64 .855 .280 tl 1,79 16.14 17,76 20,25 .973 -2.09 30,00 17,81 20.25 .810 .184 �Z 1.7� 15.94 16.62 19,29 .957 -2.04 30.00 15,96 19.B5 .736 .365 ;EOMETRIC PROPERTIES FOR MEMBERS: 5 - 6 S E C T I 0 N D E S C R I P T I 0 N FUI,L SECTION PROPERTIES -------------------------------------------------------------- ------------------------------- P 0 I N T LEFT FLANGE RIGHT FLANGE W E B MOM OF SECTI0�1 �ODULUS IQ I,OCATION WIDTH THK UNBR LGTH WIDTH THK ONBR LGTH THR NEIGHT S SPACE AREA INERTIA LEFT RIGHT (FT) (IN) (IN) (IN) (IN) (IN) (IN) (I�f) (IH) (IN) (IN2) (IN4) (IN3) (IN3) 1 .00 8.0 .250 60.0 8,0 ,250 120.0 ,134 17,00 333.0 6.3 352.6 40.30 40.30 2 3.00 B,U .250 60.0 8.0 .Z50 120,0 ,134 18.30 333.0 6.5 412.6 43,91 43.91 3 5,99 8.0 .250 60.0 8.0 .250 120,0 ,134 19,59 333.0 6.6 478,0 47,58 41,58 � 8.99 8.0 .250 60.0 8,0 ,250 120.0 ,134 20.89 333,0 6.8 549.0 51.34 51,34 a 9.01 8,0 .250 fi0,0 8.0 .250 120.0 .134 20.90 333,0 6.8 549,4 51.36 51.3fi 6 12.25 8.0 .250 60.0 B.0 .250 120.0 .134 22,30 333,0 7.0 632.7 55.51 55.51 7 15.50 8.0 ,250 60,0 8,0 ,250 120.0 .134 23.70 333.0 7.2 722.9 59.74 59.74 8 18.74 8.0 .25� 60.0 B.0 .250 120.0 .134 25.10 333.0 7.4 820.2 64.07 64.07 9 18.76 8.0 .250 60.0 B4O .250 120.0 .134 25.11 333.0 7.4 820.7 64.09 64.09 0 21,T5 8.0 .250 60.0 B4O .Z50 120.0 .134 26.41 333,0 7.6 91T.1 68.16 68.16 1 24,75 8.0 .250 60.0 8.0 .250 120.0 ,134 27,70 333.0 7,1 1019.8 72.31 72.31 2 27.75 8.0 .250 12,0 B.Q .250 120.0 .134 29.00 333.0 7.9 1126.9 76.54 76,5� FLAYGES tdEB - - I@LD STRESSES (KSI) 50,0 50,0 . �� �-� '� 0 STEEL BUILDIYG SYSTEKS, INC. ' P.O. BOX 447 ' ADEL, GA 31620 (912) 896-7428 � FRA�4E DESIGN PAGE 8 ------------ DATE 2/ Z/2000 TIHE 10:52:00 • ROJECT: SBS 00-01-030"A" PROFESSIONAL AIRPORT RA�E ; Fra�e Number 1 ROPERTIES FOR STRESS ANALYSIS FOR MEMBBRS: 5 - 6 L E F T FLANGE RICHT FLAYGE T --------------------------- --------------------------- 0 CB L/RT LD/AF CB L/RT LDJAF KL/RX KL/RY CM F'E 1 1.00D Z8.348 525.000 1.000 56.696 10�0.000 77.004 32.568 .850 Z5.184 Z 1,000 28.521 563.885 1.000 57.041 1127.770 72.168 33.016 .850 28.672 3 1,000 28,692 602.769 1.000 57.384 1205,539 67,948 33.459 .850 32.344 � 1.000 28.862 641.654 1.000 57.725 1283.308 64.232 33.895 ,850 36.195 •i 1.000 28.863 691.873 1,000 57.727 1283.745 69.212 33.898 .850 36.218 6 1.000 29,047 683.958 1.00Q 58.093 1367.915 60.659 34.369 ,850 40.565 1 1.000 29.229 726,042 1,000 58.457 1452.Q85 57.509 34.823 .850 45.152 3 1.000 Z9,410 768.127 1.000 58.819 1536.255 54.695 35.277 .850 49.817 � 1.000 29,411 768,346 1.000 58.821 1536.692 54.682 35.280 .850 49.992 l 1.000 29.577 807,230 1.000 59.154 1614.461 52.337 35.694 .850 54.517 l 1.000 29.742 896.115 1.000 59.484 169Z.230 50.201 36.1Q3 ,850 59.254 � 1.000 5.961 1T7,000 1.000 59.613 1770.000 48.247 7.302 .850 64.151 � �� ����J��� � STEEL BUILDING SYSTE�S, INC. ` P.O. BOX 447 ADEI,, GA 31620 (912) 896-7428 FRAME DESIGN PAGE 9 ------------ DATE 2/ 2/Z000 TI4E 10:52:00 ?ROJECT: SBS 00-01-030"A" PROFESSIONAL AIRPORT ?RAKE : Frame Yumber 1 :dBMBER FORCES FOR MEMBERS: 5 - 6 ABSOI,UTE MOMENTS AND AXIAL F6RCES 'T ME�lBER MAXIM(J�t --------------------------------------------------------------------------- t0 NUMBER SHEAR MOMENT AXIAL MOMENT AXIAL HOMENT AXIAI, MOMENT ARIAL (KIPS) (K-FT) (KIPS) (K-FT� (KIPS) (K-FT} (KIPS) (K-RTJ (KIPS) 1,OD+1.OL 1.OD+1.OW C1 1.OD+1.OW C2 1,OD+1.OZ 1.OD+1.OS 1.OD+ ,5S+1.OW Cl 1.OD+ .5S+1.OW C2 1.OD+1.05+ ,5W Cl 1,OD+1.OS+ .5W C2 1.OD+1.OS+1.OZ 1 5 10.53 14.94 14.46 -8.74 -16.04 -.14 -5.96 3.08 3.07 3.16 3.06 -8.7� -16.04 -.14 -5.46 -3.18 -6.87 1.12 -1.58 3.08 3.07 1 6 10.53 14.94 14.96 -20.9T -16.23 -11.87 -5.65 3.25 3.07 3.16 3.06 -20.47 -16.23 -11.87 -5.65 -9.05 -6.97 -4.75 -1.68 3,25 3.07 2 5 9,11 -12.18 14.39 20.70 -16.05 14.62 -5.47 -2.65 3.05 -2.58 3.OS 20,70 -16.05 14.62 -5.47 9.3B -6.88 6.34 -1.59 -2.65 3.05 2 6 9.I1 -12.18 14.39 3.33 -16.24 -2.T5 -5.66 -2.51 3.05 -2.58 3.05 3,33 -16.24 -2,75 -5,66 .69 -6.98 -2.34 -1.69 -Z.51 3.05 3 5 7.70 -35.90 14.32 45.89 -16.06 27.05 -5.48 -7.67 3.04 -7.60 3,03 95.89 -16,06 27.05 -5.46 20.09 -6.89 10.67 -1,60 -7,67 3,04 3 6 7.70 -35.90 14,32 24.56 -16.26 5.72 -5.67 -7.54 3.D4 -7.fi0 3,03 24.56 -16.26 5.72 -5.67 9.43 -6.99 .00 -1.70 -7,54 3.04 9 5 6.29 -56,22 14.24 66,85 -16.07 37.16 -5,49 -11,96 3,02 -11.91 3.02 66.85 -16.07 37.16 -5.49 26.96 -6,9D 14.11 -1.61 -11.96 3.02 9 6 6,29 -56,22 14.29 43.22 -16.27 13,53 -5.69 -11,85 3.02 -11,91 3.02 43,22 -16,27 13,53 -5.69 17.14 -7.00 2.30 -1.71 -11.85 3.02 a 5 6,28 -56.32 14.24 66.96 -16.07 37.21 -5,49 -11.98 3.02 -11.93 3.02 66,96 -16.07 37.21 -5.49 29.00 -6.90 14.13 -1.61 -11.98 3,02 � 6 6.28 -56.32 14.29 43.32 -16.27 13.57 -5.69 -11.87 3.02 -11.93 3.02 43.32 -16,27 13.57 -5.69 17.18 -7,00 2,31 -1.71 -11.67 3.02 6 5 4,97 -74.45 14.16 84.89 -16.08 45.52 -5.50 -15,81 3.00 -15.71 3.00 84.84 -16.08 45.52 -5.50 36.50 -6.92 16.84 -1.63 -15.81 3.00 - � 6 6 4,97 -74,g5 14.16 60.6Z -16.28 Z1.29 -5,70 -15.72 3.01 " r ' -15.77 3.00 6Q.62 -16.28 21.29 -5,70 Z4.39 -7.01 � � ' 4.73 -1.72 -15.72 3.01 7 5 3.99 -B8.59 14,OB 97.76 -16.10 51.10 -5.52 -18.79 2.99 ` � � -18.76 2.98 97.76 -16.10 51,10 -5.52 41.84 -6.93 18.51 -1,64 -18.79 2.99 ����� � i 6 3.94 -88.59 14.08 74.91 -16.29 26.24 -�.71 -18.72 2,99 - -18,76 Z,98 7�.91 -16,29 28,24 -a.71 30,91 -7,03 - 7.08 -1.74 -1B,72 Z.99 - 8 5 � 3.02 -98.75 14.00 105.72 -16.11 53.96 -5.53 -20.93 2.97 ' -20,91 2.9fi 105.72 -16,11 53.96 -5.53 45.01 -6.94 19.13 -1.65 •Z0.93 2.97 8 6 3,02 -98.75 14.00 86.20 -16.31 34.43 -5.72 -20.88 2,97 -Z0.91 2.96 66.20 -16,31 34.43 -5.92 35.25 -7.04 9.37 -1,75 -20,88 2.97 9 5 3.01 -98.99 14,00 105.75 -16.11 53.96 -5.53 -20.94 2.97 -Z0.92 2.96 105.T5 -16.11 53.96 -5.53 45,02 -6.94 19.13 -1.65 -20.94 2,97 9 6 3.01 -98.79 14,00 86.25 -1fi.31 34.46 -5.72 -20.89 2.97 � -20.92 2.96 86.25 -16,31 34.46 -5.72 35.27 -7.04 9.38 -1.75 -20.89 2.97 10 5 2.16 -104.61 13.93 108.66 -16.12 54,17 -5.54 -22.16 2.96 -22.15 2.95 108,66 -16.12 54,11 -5.54 46,02 -6,95 16.77 -1.66 -2Z.16 2,96 l0 6 2.16 -104.61 13,93 93.99 -16.32 39,49 -5.74 -22.13 2.96 � -22.15 2.95 93.99 -16.32 39.99 -5.79 38.68 -7.05 11.43 -1,76 -22.13 2.96 II 5 1.35 -107.02 13.85 107.34 -16.13 52.05 -5.55 -22.66 2.94 -22.66 2.93 107.34 -16.13 52.05 -5,55 45.16 -6.97 17.52 -1.68 -22.66 2.94 � ll 6 1.35 -107.02 13.85 99,17 -16,33 43.8T -5,75 -22,65 2,94 -22.66 2.93 99.17 -16.33 43.87 -5.75 41.08 -7.06 � 13.43 -1,77 -22.65 2.94 l2 5 2.56 -106.03 13.78 101,78 -16.14 47,6Q -5.56 -22.44 2.92 -22,45 2,92 101,78 -16.14 47.60 -5,56 42,46 -6.98 15.37 -1.69 -22.44 2.92 i2 6 2.56 -106.03 13.78 101.78 -16.34 47.60 -5.76 -22.44 2.92 -22.45 2.92 1D1.78 -16.34 41.60 -5,76 42.46 -7,OB 15.37 -1.78 -22,44 Z,92 r - � - �.-�c�-� 5TBEL BUILDIKG SYSTENS, INC. r ` P.O. BOX dd7 ADEL, GA 3I620 (912) 89fi-7426 FkA��B DESIGY PAGB i0 ------------ DATE 2/ Z/�404 TIME 10:52:40 tOJECT: SB5 00-01-030"A' PROFESSIONAL AIRPORT tA��E : Frame Number 1 )RCES ACTING ON SOPPORTS bOADIYG G4YDITIQ� •----------------------- ------------------------------------------- . SUPPORT HORIZONTAL VBRTIEAL NOMENT ) D E 5 C R I P T I 0 N NO (KIP5} (KIPSj (K-FT) t i.OD�I.OL 1 -I3.8I I8.60 .00 i 1,OD+1.OL 7 13.$1 18.60 ,00 TOTAL FORCES ACTI�G .00 39,20 TQTAL FORCES APPLIED .00 37.20 ' 1.OD+1.OW C1 1 16.79 -Z1.OQ .4� ; 1.OD+1,OW C1 7 -8.66 -15.10 .00 TOTAL FORCES ACTING 8.12 -36,11 TOTAL FORCES APPLIED 8.12 -36,11 1 i.ODtl.6� C2 1 11,55 -10,$2 .QO � 1.QD+1.4W C2 7 -3.43 -4.92 .00 TOTAL FORCBS ACTING 8.12 -15.?3 TOTA� FORCES APPLIED 8.12 -15,73 I�OD+I.OZ 1 -2,92 3.94 .00 I.OD+I.OZ 7 2.93 3.99 .00 TOTAL FORCES ACTI�G .Ol 7.86 TOTAL FORCES APPLIED .Ol 9,88 1.OD+1.45 1 -2.92 3.94 .04 1,OD+1.05 7 2.92 3.94 ,00 TOTAL FORCES ACTING .00 7.86 TOTAb FORCE5 APPLIED .00 7.88 t,OD+ .SS+1.OW CI 1 I6.79 -21.00 .00 I.OD+ .55+1.0� Cl 7 -$.66 -25.10 ,OQ TQTAL FQRCES ACTING $.12 -36.11 TOTA� FORCBS APPLIED 8,1� -36.11 1.OD+ .5S+1.OW C2 1 11:55 -10.82 .00 I,DD+ ,�S+I,OW C2 7 -3.93 -4.92 .00 TOTAL FORCES ACTINC 8,12 -I5.73 TOTAL AOkCES APPLIED 8.12 -15.93 _ 1.QD+l.qS+ .5W G1 1 7.30 -9.QZ .00 � � --�b -� STEEL BUILDIYG SYSTEMS, INC. ' � P.O. BOX 447 ; ADEL, CA 31620 (912) 896-7428 FRA�NE DESIGN PAGE 11 ------------ DATE 2/ 2/2000 TIME 10:52:00 ')JECT; SBS 00-01-030"A" PROFBSSIONAL AIRPORT �I �KE ; Frame Number 1 �'I 3CES ACTING ON SUPPORTS LOADING CONDITION � ----------------------- ------------------------------------------- SUPPORT HORIZONTAL VERTICAL MOMBNT � D E S C R I P T I 0 N NO (KIPS) (KIPS) (K-FT) � 1.OD+1.OS+ ,5W C1 7 -3.23 -6.07 .00 TOTAL FORCES ACTING 4.06 -15.10 TOTAL FORCES APPLIED 4.06 -15,10 1.OD+1.OS+ .5W C2 1 4.66 -3.93 .00 1,OD+1.OS+ ,5W C2 7 -.62 -.98 .00 TOTAL FORCES ACTING 4,06 -4.91 TOTAL FORCES APPLIED 9.06 -4.91 1.OD+1,OS+1.OZ 1 -2.92 3.94 .00 1.OD+1.OS+1.OZ 7 2.93 3.99 .00 TOTAL FORCES ACTING .O1 7.88 TOTAL FORCES APPLIED .O1 7.BB _ ' _� � - �--ao -��; STEEL BUILDIYG SYSTEMS, INC. ' � � P.O. BOX 447 ADEL, GA 31620 (912� 896-7428 FRAME DESIGN PAGE 12 ------------ DATE 2/ 2/2000 TIME 10:52:00 JECT: SBS 00-01-030"A" PROFESSIONAL AIRPORT HE ; Frame Number 1 . ERYAL MEMBER LOADS UNIFORMLY LOADING CONDITION DISTRIBUTED LOADS C 0 N C E N T R A T E D L 0 A D S ---------------------- MENBER -------------------- -------------------------------------- D E S C R I P T I 0 N NU�iBER VERTICAL HORIZONTAL LOCATION VERTICAL HORIZONTAL MOMENT (K/FT) (K/FT) (FT) (KIPS) (KIPS) (K-FT) 1.OD+1.OL 1 .381 ,000 I.OD+I,OL 2 ,361 .D00 1.OD+1.OL 3 .381 ,000 , 1.OD+1.OL 4 ,381 .000 I 1,OD+1.OL 5 .381 .000 ' 1.OD+1,0� 6 ,381 .000 � 1.OD+1.OW C1 1 .060 .133 I.OD+I.OW C1 2 .060 .293 ' 1.OD+1.OW C1 3 -.472 -,532 1.OD+1,OW C1 4 -.285 ,346 , 1.OD+1.OW C1 5 -.471 -.532 1.OD+1.OW C1 6 -.285 .346 I,OD+I.OW C2 1 .060 .346 1,OD+1.OW C2 2 .061 .080 1,OD+1.OW C2 3 -.259 -,319 1.OD+1,OW C2 4 -.072 .133 � 1.OD+1.O�f C2 S -.259 -,319 1.OD+1.OW C2 6 -.072 .133 1.OD+1,OZ 1 .OB1 .000 1.OD+1.OZ 2 ,081 .000 1.OD+1,0z 3 ,081 .000 1.OD+l,OZ 4 ,081 .000 I,DD+I.OZ 5 .081 .000 I.OD+1.0z 6 .081 .000 1.OD+1.OS 1 .OB1 .000 1,DD+1,OS 2 ,081 ,000 1.OD+1.05 3 .081 .000 1.OD+1.OS 4 .081 .000 1.OD+1,OS 5 .OB1 .000 I,OD+I.OS 6 ,OB1 .000 1.OD+ ,SS+1.OW C1 1 ,060 .133 1,OD+ ,SS+1.OW C1 2 .060 .293 I,ODt ,5S+1.OW C1 3 -.472 -.53Z 1.OD+ ,5S+1.OW C1 4 -.285 .346 l.OD+ .5S+1,OW Cl 5 -.471 -,532 - � - _ � I,OD+ .5S+1,OW C1 6 -.285 .346 - , � � S^ � � � � � � STEEL BUILDIYG SYSTEKS, INC, ` � � � P,O. BOX 447 ADEL, GA 31620 (912) 896-1428 FRAKE DESIGN PAGE 13 ------------ DATE Z/ Z/2000 TIME 10:52:00 )JECT; SBS 00-01-030"A" PROFESSIONAL AIRPORT �NE : Frame Number 1 �_ � ' fERNAL MEMBER LOADS UNIFORMLY LOADIYG COYDITION DISTRIBUTED LOADS C 0 N C E N T R A T E D L 0 A D S ----------------------- NEMBER -------------------- -------------------------------------- D E S C R I P T I 0 N NUMBER VERTICAL HORIZONTAL LOCATION VBRTICAL HORIZONTAL MOHENT (K/FT) (K/FT) (FT) (KIPS) (KIPS) (K-FT) 1.OD+ ,SS+1.OW C2 1 .060 .346 1.OD+ .5S+1,OW C2 Z ,061 .OBO 1.OD+ .5S+1.QW C2 3 -.259 -.319 1.OD+ .5S+1.OW C2 4 -.072 .133 1,OD+ .5S+1.OW C2 5 -.259 -,319 1.OD+ ,5S+1,OW C2 fi -.072 ,133 1.OD+1.OS+ ,5W Cl 1 .061 ,067 1.OD+1,OS+ .5W C1 2 ,061 ,14fi I.OD+1,05+ .5W C1 3 -.2Q6 -.266 1,OD+1.OS+ ,5W C1 4 -.112 ,173 1.OD+1.OS+ ,SW C1 5 -.205 -.266 1,OD+l,OS+ ,5W C1 6 -.112 .173 1.OD+1.OS+ .5W C2 1 .061 .173 1.OD+1.OS+ .5W C2 2 .061 ,046 ' 1.OD+1,OS+ ,5W C2 3 -.099 -.160 1,OD+1,OS+ ,5W C2 4 -.006 .067 1.OD+1.OS+ ,SW C2 5 -.099 -.160 1.OD+l.OS+ ,5W C2 6 -.006 .066 1.OD+1.OS+1.OZ 1 .081 ,000 I.OD+I.OS+I.OZ 2 .081 .000 1.OD+1.OS+l.OZ ' 3 .081 .000 1.OD+1.OS+1.OZ 4 .081 .000 I.OD+I.OS+I,OZ 5 ,081 .000 1.OD+1,OS+1,OZ 6 .081 ,000 . .. � �`��- � STEEL BUILDIYG SYSTEMS, IYC. ' ' � � P,O. BOX 447 ADEL, GA 31620 (912) 896-7428 FRA�E DESIGN PAGE 14 ------------ DATE 2/ 2/2000 TIMB 10:52:00 JECT: SBS 00-01-030"A" PROFESSIONAL AIRPORT KE : Frame Number 1 ERYAL JOINT LOADS lOADING CONDITION J 0 I N T L 0 A D ----------------------- JOINT ---------------------------- D E S C R I P I T I 0 N NUMBER VERTICAL HORIZONTAL MOMENT _ (KIPS) (KIPS) (K-FT) I.OD+I.OZ 2 ,O1 1.OD+1.OS+1.OZ 2 .O1 r I s . _ -� . . . ���� � � , ,. , � STEEL BUILDI�G SYSTEHS, INC, - P.O, BOX 447 ADEL, GA 31620 ' (912� 896-1428 �� FRA�E DESIGN PAGE 15 ------------ DATE 2/ 2/Z000 TIME 10:52:01 IECT: SBS 00-01-030"A" PROFBSSIONAL AIRPORT fE : Fra�e Number 1 )ER END TRANSLATIONS LOADIYG CONDITION g N D T R A N S L A T I 0 N S lER NO D E S C R I P T I 0 N JOINT VERT HORZ JOINT VERT HORZ NO (IN) (IN� NO (IN) (IN) ' ( 1 1.OD+1,OI, 1 .00 ,00 2 ,00 -.37 _ 2 I,OD+I.OW C1 1 .00 .00 2 -.O1 ,52 � 3 I,OD+l.OW C2 1 .00 .00 2 -.O1 .34 4 1.OD+1.OZ 1 ,00 .00 2 .00 -,07 ', ( 5 1.DD+1.OS 1 ,00 .00 2 .00 -.08 '. 6 1,OD+ ,5S+1.OW C1 1 .00 .00 2 -.O1 .52 , 7 1.OD+ ,5S+1.OW C2 1 ,00 .00 Z -.O1 .34 B 1.OD+1.OS+ .5W C1 1 .00 .00 2 ,00 .23 9 1.OD+1.OS+ .5� C2 1 .00 ,00 Z .00 .14 _ 10 1.OD+1,OS+1.OZ 1 .00 .00 2 .00 -.07 ' : 1 1.OD+1.OL 7 .00 .00 6 .OQ .37 ' 2 1,OD+1.OW C1 7 .00 ,00 6 ,00 -.18 ' 3 1.OD+1.OW C2 7 .00 .00 6 .00 .00 4 1,QD+1.OZ 7 ,00 ,00 6 .00 ,08 5 1.OD+l.OS 7 .00 .00 6 .00 .08 6 1.OD+ .5S+l.OW C1 7 .00 .00 6 .00 -.18 7 1.OD+ .5S+1.OW C2 7 .00 .00 6 .00 .00 8 1,OD+1.OS+ ,5W C1 7 .00 .00 6 .00 -.O6 9 1.OD+1.OS+ .SW C2 7 .00 .00 6 ,00 .03 10 I.OD+l.OS+I.OZ 7 .00 .00 6 .00 .OB 1 1.OD+1.OL 2 ,00 -.37 3 -1.99 -.14 2 1.OD+1,OW Cl 2 -.O1 .52 3 2,10 .28 3 1.OD+1.OW C2 2 -.Ol .34 3 1,08 .21 9 1,OD+1.OZ 2 .00 -.OT 3 -.42 -,03 � 1.OD+1.OS 2 .00 -.OB 3 -.42 -.03 6 1.OD+ ,SS+1,OW C1 2 -.O1 .52 3 2,10 .28 7 1,OD+ .5S+1.OW CZ 2 -.O1 .34 3 1.08 .21 8 1.OD+1.OS+ ,5� C1 2 ,00 .23 3 .89 .13 9 1.OD+1.OS+ ,5W C2 2 .00 .14 3 .38 .09 10 1,OD+1,OS+1.OZ 2 ,00 -.07 3 -,42 -,03 • 1 I.OD+I.OL 6 .00 .37 � -1.99 ,14 2 1.OD+1,OW C1 6 .00 -.18 a 1.77 .02 3 1,OD+1.OW C2 6 .00 ,00 a .75 .D9 9 I.OD+I.OZ 6 .00 .08 a -,42 .03 5 1.ODf1.OS fi .00 .OB a -.42 .03 _ - - � 6 1.OD+ ,SS+I.OW C1 6 .00 -.18 a 1,7T .02 - - s � �o � �� STEBL BUILDIYG SYSTEMS, IYC. , , � � P,O. BOX 4�7 �ADEL, GA 31620 (912� 896-7428 FRA�ME DESIGN , PAGE 16 ------------ DATE 2/ Z/Z000 TIME 10:52;01 JECT: SBS 00-01-030"A" PROFESSIOYAL AIRPORT NE : Frame Number 1 9ER END TRANSLATIONS LOADINC CONDITION E N D T R A N S L A T I 0 N S , ------------------------- --------------------------------------------- 3ER NO D E S C R I P T I 0 N JOINT VERT HORZ JOINT VERT HORZ NO (IY) (IN) NO (IN} (IN) 1 7 1,OD+ .55+1.0� C2 6 ,00 .00 5 .75 .09 1 8 1.OD+1,OS+ .SW C1 6 .00 -.06 5 .73 ,02 I 9 1.OD+1.OS+ .5W CZ 6 .00 .03 5 .a2 ,05 I 10 1.OD+1.OS+1.OZ 6 .00 .OB 5 -.42 .03 .i 1 1.OD+1.�L 3 -1.99 -.14 4 -4,45 .00 � 2 1,OD+1,OW C1 3 2.10 .28 4 4.32 .16 i 3 1.OD+1.OW C2 3 1.08 .21 4 2.02 .16 i 4 1.OD+1.OZ 3 -.42 -,03 9 -.94 .00 i 5 1.OD+1,OS 3 -.42 -.03 4 -.94 .00 .i 6 1.OD+ .5S+1.OW C1 3 2.10 .28 4 4.32 .16 i 7 1.OD+ ,SS+1.OW C2 3 1.08 .21 4 2.02 .16 i B 1.OD+1,OS+ .5W C1 3 .89 .13 4 1.81 .OS i 9 1,OD+1.05+ .5W C2 3 .36 .09 4 .66 .08 � 10 1.OD+1.OS+1.OZ 3 -.42 -.03 4 -.94 .00 � 1 1.OD+1.OL S -1.99 .14 4 -4.45 .DO � Z 1,OD+1.OW C1 5 1.97 ,02 4 9.32 .16 i 3 1.OD+1,OW C2 5 .7� .09 9 2.02 .16 i 4 I,OD+1.02 5 -.42 .03 4 -.94 .00 � 5 1.OD+1.OS 5 -.42 .03 4 -.94 .00 , fi 1,OD+ .SS+1,OW Cl 5 1.77 .OZ 9 4.32 .16 � 7 1.OD+ ,SS+1,OW C2 5 .7S .09 4 2.02 .16 � 8 1.OD+1.OS+ .SW C1 5 .73 .02 4 1.81 .08 � 9 1,OD+1.OS+ ,SW C2 5 ,22 .05 4 .66 .08 � 10 1.OD+1.OS+1.OZ 5 -.42 .03 4 -.94 .00 :LUS OF ELASTICITY (RSI) 29000.00 � - s ; _ ��-�.�_��� � �. � • STBEL BUILDING SYSTEMS, INC. P.O, BOX 447 ADEL, GA 31620 (912} 896-7428 FRAME DBSIGN PAGE 17 �, ------------ DATB 2/ 2/Z000 I TIME 10:52:01 i JECT: SBS 00-01-03�"A" PROFESSIOYAL AIRPORT KE : Frame Number 1 � B FLANGE F L A N G E��T H I C K FLANGE WIDTH TO THICKNESS FLG/WEB WEB I THK/THK L E F T RIGHT L E F T RICHT THICK WEB THICKNESS HT/TNK MAX MIN MAX MIN MAX MAX MIN MAX MIN �iIN MIN MAX MAX 2.5 .150 2.000 ,150 2.000 41.000 B.000 41.000 8.000 ,900 .100 .875 236,000 _ 2.5 ,150 2.000 .150 Z.000 41.000 B4O00 41.000 8.000 .900 .100 .875 236.000 'I 2.5 .150 2.000 .150 2,000�, 41.OU0 8.000 41.000 8.000 .900 .100 .875 23fi.000 I _� , - „- rJ - . .� �v � ��� + s I T . � a STEEL BUILDING SYSTE�S, INC. �, F.O, BOX 447 � ADBL, GA 31620 � (912} 836-742$ � FRA��fE DESIG�'Y PAGE 16 � """""�' DATE 2/ 2/2Q00 TIME 10:52:01 PROJBCT. SBS OQ-01-030"A" PROPESSIO�JAL AIRPORT FRA�ME ; Frame Number 1 ME!(BER �fEMBER � � TYPE N4. I,ENGTH WEIGHT � c��� c�Br 1 19.65 7�7. 2 19.65 747. 3 19.42 6&0, 4 19,02 680. � 5 27.75 663. • 6 27,75 669, S�B'fOTAL 4191, HAUNCH 272, TOTAL 132.83 44fi3. DfiNSITY (LB/IN3j .2833 i I � � ��'��-Y � `� a t__.. ;3fI.r�G`�.' :? - L�G111� d)T'SCR�F"�Z�Y�I ��IC_ �'�orrsszor�n.r� 11II:CR�1I'�' P��1IN�r�N��vcr .. TA�I,`_4"�0 11PRIL 30, 2_OQO r,�c���, z��sc�z�_RD�rX��J: � Y"LAFlC,U:�A.1 BS 7�ti • JI Commc�nce at: the NorthwesL cori2er o� Sec�ion 13, Township 2G South, Itany� 21 I:ast, Pasc.o County, Florida; thence rT_ P9°54 ' 37"�. along tYze Nort�.�. 7_ir�e of s�id Section 13 a C�1S�c121CF3 of 1, ?39 .57 f.eei:; th.�nce S .UO°07 ' 19"E. � c�istance of "1, 068 .9:� fe��t; thenc� N. Ci9°5<< ' 37"�. parallel to th� Nor�h laa�e o� saic� Section J.� a c�ist�nce o� 421_29 feet; thence S . O�J°7_n ' 49"�. a. distance o_� 1.;L0 .00 �eet; thence N. 89°41 ' 11"E. a clisi:ance o:F 62�3.85 F�eL; t��e�ce N.00°1�3 ' 49"W. a distance of 13y . E37 ieet t=o the Nox�ther_ly �rJ,g�� c�:E a taxiway for a POINT UF B�GINNING; thAnce con�inue N.�O°:L�3 ' �9"W. a distance of 7.35.13 :�eeL� tl�ence AT. 4t3°27_ ' 10"T' . , � c?i.st_ance of 374. �31. .feet to -the WesterJ._y eclge oL a. taxiway; �t.lience along said Westerly edge th� fo].low�_ng courses; S . �:1.°37 ' 50"E. a di�tance of �Ul .50 :�eet to the b�ginni�ig oL a curvc� concave to the Southwest hzvizig a l2�dius of 173.QO feet, Chord Bear:ing of � . 21°09 ' 5�"W. , 120.97 fee�i�; t}rence along the arc a distance ol "1"L3 . 58 ree.t i:o tki� J�e��i_xanin.g o� a curve concave to the �loxth�uest izavix�g a Rac�ius of ��� .OU feet, Chord Bearing of S .44°17 ' 57"W. , 90.51 �'ee�t tlzezice along the arc a dis�tance ' of 100 . 53 feei::; therice S .�39°17 ' S7"W. a distance o.f 526.10 feet to thc poir.,� of beginnii�.g_ `.��C}i��Tki�� L31f.'�.'�� �n easement �or_ iiic�.ress and egress aver ai�.d acr_oss ��he Following descril:.aecl �_�nd.s: �Cca�.�a.ir►c�ra.c:�.aas� a�L- �ti�e aforexueii�ki.Qz�ed. I'oint of beginning; thence �I�.00°li3 ' 49"��1. a disi:�nce o:E 235 .13 fee�t; thence N.4B°7_2 ' 10"E. �. distance c�i 35. 69 �eet #_or � POINT OI' BFGINNING OF EASEMEPI`.L'; �t�zenca �T. 43"29 ' 51"[n1. a distance o.f 195 .52 feet; thence S. �5°59 ' 44"W. a clist�zice af 27. 45 feet to the Westerly l a_i�.e o L Parcc�l "A" ; Lk��r�c,� Tv'.�i°�4 ' 1:�"i�7 . aJ_ozlg said G�lesterl.y ].irze a dist��nc�� �n:f: _1. �.00 feet; thence N. 45°59 ' 44"I:. • a dista.nce oi' 44. 6,f3 .feet; �th�rzce 5 .43°29 ' 51"E. a distance of 714 .26 �ee�t �to the Soutller_l;� 1 i.ne of said Parcel "A" ; thence 5 .48°77 ' 10"W. �lang said linc a clistance o:E 18.00 feet to the poin�t c�i beginning. i Said p�rcel containiriy 4. 43 a�_,r_e� �iare or less. Page is too large to OCR. Page is too large to OCR. Page is too large to OCR. i - - - - - - - H - - " 1 DTL L . - [ I L 1`S �1 [ 11 1`" L! i 1p��t LU ', CLJ ¢g ! I 1 1 "J 2�ot /O0 __ / _ \/- It L LQ ETE 7 S 2oD t Lamm tci_ 1-Iars. L (? I to ) L tL '\ LS f-F < <_ " I / ≤ ≤LA EIII::: ________ __ uJzuJ Z NJ a W \J W V Q Z WoOQ - m W W U G W pL \ a W = WZ a � H G ce 0� H W Q W W F_ Z H Q UoH � O Z p- Luwr Z X d a _ c. OUa K �O C W Z Q ~ 2 wWC W LU W W ___ > U N O Z W V QXZQZ (jam • • • • • • • • • • • • i- O k Q F m NJ LL W Q V 2 Z N Q W I-- N W Q W F O W\ N 2 1� �AtL ~ ate WZ 2 Q LL X3 N Nai 3kS i31�� '' D .Lf L L_ _/ T ® \__ 4 6, IE r hrL �t Page is too large to OCR. 22' 4— 5/ 8 HOLE DIAMETER: .$7SO 12' 7-13 16 go 8 DETAIL OF TPL11 i� v5— 1/ 4" iv 'r 19'_6-11416 2— 3/ 4" 2- 1/ 2" 12' 4 co — 7' 4 17' 4 _ as -- IL _ C1 8 • N DETAIL OF CPL11 3-15/16" 3' 8- 1 16 1 ei oo ° cD DETAIL OF BPL1 1 - 8"L iv . II II 5- 5/ 8" 22' 3-13/16 ,n N 3' 2— 7/16 n 3' 6— 1/16 21' 9-13, 6 HOLE DIAMETER: 1.0000 I. . \ __ MAKE 3 PCS. MARK: MFC 1 19' 4 I 00-01 -030A_______________________ j 10' 6-13/16 !3' 4- 4h PROFESSIONAL AIRCRAFT 12 O MAINTENANCE ►t' 9 , 1 L '-' N M 0 12 8' 7-15 16 3' 4— 1 16 Frame Number 1 PRIMITIVE PARTMARK: MFC 1 FABRICATE 10 AS SHOWN DRAWING UNIT: FEET & INCHES PART MARK PART DESCRIPTION LENGTH WIDTH THICKNESS QTY QTY/BLDG YIELD WEIGHT BPL11 BASE PLATE 1 0 13/16 0 8 0/16 .5000 1 10 50.0 14.5 TPL11 TOP PLATE 3 8 1/ 2 0 8 0/16 .3125 1 10 50.0 31.5 STF11 STIFFENER PLATE 3 0 0/16 0 4 0/16 .3125 2 20 50.0 25.5 CPL11 CONNECTION PLATE 3 8 1/16 0 8 0/16 .7500 1 10 50.0 74.9 WEB11 WEB PLATE 10 6 13/16 2 1 3/16 .1875 1 10 50.0 125.3 WEB12 WEB PLATE 12 0 0/16 3 0 0/16 .1875 1 10 50.0 242.7 FLG11 FLANGE PLATE 12 7 13/16 0 8 0/15 .3125 1 10 50.0 107.5 FLG12 FLANGE PLATE 9 8 0/16 0 8 0/16 .3750 1 10 50.0 98.6 FLG13 FLANGE PLATE 19 4 0/16 0 8 0/16 .5000 1 10 50.0 262.9 Cl 8 GIRT CUP 0 7 0/16 0 6 0/16 .1900 4 40 50.0 11.3 C3 FLANGE BRACE CLIP 0 4 0/16 0 2 0/15 .1900 2 20 50.0 1.0 TOTAL WEIGHT 995.7 22' 4- 5 8 HOLE DIAMETER: .S7So 12' 7-13 16 9, 8 DETAIL OF TPL11 2- 1, 2 `d 4 19'_6-11416 2- 3/ 12 17' 4 i iE ° �- Cl 8 DETAIL OF CPL11 3-15/16 3' 8- 1 16 DETAIL OF BPL11 3 8" om_ 3' 8 1 16 �N IT. II 2" 5- 5/ 8" 22' 3-13/16 ,n N 3' 2- 7/16 oy 21' 9-136 3' 6- 1/16 s �� HOLE DIAMETER: 1.0000 14 \ -x _ MAKE 3 PCS. MARK: MFC 2 00-01 -030A 10' 6-13/16 (3' 4- 1 16 PROFESSIONAL AIRCRAFT MAINTENANCE 1t' 9 , to wet31ft1 _ 2 --� ' N 0 P = 8' 7-15/16 3' 4— 1/16 Frame Number 1 PRIMITIVE PARTMARK: MFC 1 FABRICATE 10 AS SHOWN DRAWING UNIT: FEET & INCHES O� PART MARK PART DESCRIPTION LENGTH WIDTH THICKNESS QTY QTY/BLDG YIELD WEIGHT C BPL11 BASE PLATE 1 0 13/16 0 8 0/16 .5000 1 10 50.0 14.5 TPL11 TOP PLATE 3 8 O/1 , 0 8 0/16 .3125 1 10 50.0 31.5 STF11 STIFFENER PLATE 3 0 0/16 0 4 0/16 .3125 2 20 50.0 25.5 (' CPL11 CONNECTION PLATE 3 8 1/16 0 8 0/16 .7500 1 10 50.0 74.9 WEB11 WEB PLATE 10 6 13/16 2 1 3/16 .1875 1 10 50.0 125.3 WEB12 WEB PLATE 12 0 0/16 3 0 0/16 .1875 1 10 50.0 242.7 FLG11 FLANGE PLATE 12 7 13/16 0 8 0/16 .3125 1 10 50.0 107.5 FLG12 FLANGE PLATE 9 8 0/16 0 8 0/16 .3750 1 10 50.0 98.6 FLG13 FLANGE PLATE 19 4 0/16 0 8 0/16 .5000 1 10 50.0 262.9 � s � Cl 8 GIRT CUP 0 7 0/16 C 6 0/16 .1900 4 40 50.0 11.3 C3 FLANGE BRACE CLIP 0 4 0/16 C 2 0/16 .1900 2 2C 50.0 1.0 TOTAL WEIGHT 995.7 L � �O b 22' 4-_5/_8 DETAIL OF TPL11 HOLE DIAMETER: 0 750 12' 7-13/16 9, 8 5- 1/ 4" * 4 5- 1/ 2" 19'_6-11416 2- 3/ 4" 2- 1/ 2" 12' 4 ft11 h.t::- co 7' 4 17 4 {0�4N ioo =fib- C 1 8 2 L DETAIL OF CPL1 1 N N� Y 3-15/16" 3' 8- 1/16j C3 °pU __ .• ii 00 Oi N DETAIL OF BPL11 19' 4 I8" II 4� 2" '- 5- 5/ 8" 22' 3-13/16 ,n N 3' 2- 7/16 3' 6- 1/16 21' 9-13 6 HOLE DIAMETER: 1.0000 MAKE 1 PCS. MARK: MFC 3 1s' 4 00-01 -030A________________________ J10' 6-13/16 3' 4- i/1' PROFESSIONAL AIRCRAFT WLW 12 o MAINTENANCE we 2 co ---"" M � N I o M 10' 7— 1 2 8' 7-15/16 3' 4— 1 16 Frame Number 1 PRIMITIVE PARTMARK: MFC 1 FABRICATE 10 AS SHOWN DRAWING UNIT: FEET & INCHES PART MARK PART DESCRIPTION LENGTH WIDTH THICKNESS QTY QTY/BLDG YIELD WEIGHT BPL11 BASE PLATE 1 0 13/16 0 8 0/16 .5000 1 10 50.0 14.5 TPL11 TOP PLATE 3 8 1/ 2 0 8 0/16 .3125 1 10 50.0 31.5 STF11 STIFFENER PLATE 3 0 0/16 0 4 0/16 .3125 2 20 50.0 25.5 CPL1 1 CONNECTION PLATE 3 8 1/16 0 8 0/16 .7500 1 10 50.0 74.9 WEB11 WEB PLATE 10 6 13/16 2 1 3/16 .1875 1 10 50.0 125.3 WEB12 WEB PLATE 12 0 0/16 3 0 0/16 .1875 1 10 50.0 242.7 FLG11 FLANGE PLATE 12 7 13/16 0 8 0/16 .3125 1 10 50.0 107.5 FLG12 FLANGE PLATE 9 8 0/16 0 8 0/16 .3750 1 10 50.0 98.6 FLG13 FLANGE PLATE 19 4 0/16 0 8 0/16 .5000 1 10 50.0 262.9 Cl 8 GIRT CLIP 0 7 0/16 0 6 0/16 .1900 4 40 50.0 11.3 C3 FLANGE BRACE CLIP 0 4 0/16 0 2 0/16 .1900 2 20 50.0 1.0 TOTAL WEIGHT 995.7 zoo 22' 4—_5/_8 HOLE DIAMETER: S?SO 12' 7-13 16 9' 8 DETAIL OF TPL11 _ " 5- 1/ 2" 19'_6-11416 2— 3/ 4' ' j\ 2- 1/ 2` 12' 4 7' 4 17' 4 •• lD � as =--� C1 8 N w Zvi" DETAIL OF CPL11 " 3-15/16 3' 8— 1 16 L h o; ;; ao DETAIL OF BPL11 914 8` N — -T 3' 8— 1 16 � II - 2" II 5— 5/ 8" 3' 2— 7/16 22' 3-13/16 v N 3' 6— 1/16 u -� 21 9-13 6 HOLE DIAMETER: 1.0000 MAKE j. PCS. MARK: MFC 4 00-01 -030A 10' 6-13/16 3' 4- 16 PROFESSIONAL AIRCRAFT WLW 12'o MAINTENANCE II' 9 co N o Nio 10' Z12 2 f N� 8' 7-15/16 3' 4- 1 16 Frame Number 1 PRIMITIVE PARTMARK: MFC 1 FABRICATE 10 AS SHOWN DRAWING UNIT: FEET & INCHES O.9 PART MARK PART DESCRIPTION LENGTH WIDTH THICKNESS QTY QTY/BLDG YIELD WEIGHT BPL11 BASE PLATE 1 0 13/16 0 8 0/16 .5000 1 10 50.0 14.5 TPL11 TOP PLATE 3 8 O/1 C, 0 8 0/16 .3125 1 10 50.0 31.5 STF11 STIFFENER PLATE 3 0 0/16 0 4 0/16 .3125 2 20 50.0 25.5 CPL1 1 CONNECTION PLATE 3 8 1/16 0 8 0/16 .7500 1 10 50.0 74.9 WEB11 WEB PLATE 10 6 13/16 2 1 3/16 .1875 1 10 50.0 125.3 WEB12 WEB PLATE 12 0 0/16 3 0 0/16 .1875 1 10 50.0 242.7 FLG11 FLANGE PLATE 12 7 13/16 0 8 0/16 .3125 1 10 50.0 107.5 FLG 12 FLANGE PLATE 9 8 0/16 0 8 0/16 .3750 1 10 50.0 98.6 FLG13 FLANGE PLATE 19 4 0/16 0 8 0/16 .5000 1 10 50.0 262.9 Cl 8 GIRT CUP 0 7 0/16 0 6 0/16 .1900 4 40 50.0 11.3 C3 FLANGE BRACE CLIP 0 4 0/16 0 2 0/16 .1900 2 20 50.0 1.0 TOTAL WEIGHT 995.7 22' 4- 5/ 8 HOLE DIAMETER: .S-7SO 12' 7-13 16 9' 8 DETAIL OF TPL1 1 5- 1/ 2" i9'_6-11416 2- 3/ 4' N 2- 1/ 2 12' 4 CO 7 4 17' 4 ! E4 v2" N DETAIL OF CPL1 1 3-15/16" h3' 8- 1/161 DETAIL OF BPL1 1 8" c — �- 3' 8- 1 16 1 r 20 -T' 5- 5/ 8" 22' 3-13/16 ,oN 3 2- 7/16 _ 3' 6- 1/16 " - 21' 9-13 6 HOLE DIAMETER: 1.0000 srg� MAKE _L Pcs. MARK: MFC 5 is' 4 00-01 —O3OA 10' 6-13/16 3' 4- ifi PROFESSIONAL AIRCRAFT 1 ' O MAINTENANCE u' 99 , I o ' M I 0 .d- OO 12 8' 7-15/16 3' 4— 1 16 Frame Number 1 PRIMITIVE PARTMARK: MFC 1 FABRICATE 10 AS SHOWN DRAWING UNIT: FEET & INCHES PART MARK PART DESCRIPTION LENGTH WIDTH THICKNESS QTY QTY/BLDG YIELD WEIGHT BPL11 BASE PLATE 1 0 13/16 0 8 0/16 .5000 1 10 50.0 14.5 TPL11 TOP PLATE 3 8 1/ 2 0 8 0/16 .3125 1 10 50.0 31.5 r STF11 STIFFENER PLATE 3 0 0/16 0 4 0/16 .3125 2 20 50.0 25.5 CPL11 CONNECTION PLATE 3 8 1/16 0 8 0/16 .7500 1 10 50.0 74.9 WEB11 WEB PLATE 10 6 13/16 2 1 3/16 .1875 1 10 50.0 125.3 WEB12 WEB PLATE 12 0 0/16 3 0 0/16 .1875 1 10 50.0 242.7 FLG11 FLANGE PLATE 12 7 13/16 0 8 0/16 .3125 1 10 50.0 107.5 FLG12 FLANGE PLATE 9 8 0/16 0 8 0/16 .3750 1 10 50.0 98.6 FLG13 FLANGE PLATE 19 4 0/16 0 8 0/16 .5000 1 10 50.0 262.9 Cl 8 GIRT CUP 0 7 0/16 0 6 0/16 .1900 4 40 50.0 11.3 0.3 FLANGE BRACE CLIP 0 4 0/16 0 2 0/16 .1900 2 20 50.0 1.0 TOTAL WEIGHT 995.7 22' 4- 5 8 HOLE DIAMETER: .S750 12' 7-13 16 9' 8 L11 PLi12 1 DETAIL OF TPL11 / 1/ 4r 2 2- 1 2 ^ 12' 4 19' 6-11SftTT 16 2- 3/ 4' ,a / r Co 714 17' 4 iO �Ndl i f fi as =�- C1 8 N Z./Z.• DETAIL OF CPL11 . " 3-15/16- 3' 8- 1 16 A88, C3 • 2L11 LL ao .. .. m DETAIL OF BPL11 " N1N1 �8 3' 8- 1 16 \\ 2" II 5- 5/ 8" J ` /cZ '' 22' 3-13/16 ,n N 3' 2- 7/16 cr�s N " 3' 6— 1/16 21 9_13i6 HOLE DIAMETER: 1.0000 MAKE PCS. MARK: MFC (o 19' 4 00-01 -030A 10' 6-13/16 3' 4- �6 PROFESSIONAL AIRCRAFT 2'O MAINTENANCE ca � N p I O 8' 7-15/16 3' 4— 1/1 Frame Number 1 PRIMITIVE PARTMARK: MFC 1 FABRICATE 10 AS SHOWN DRAWING UNIT: FEET & INCHES PART MARK PART DESCRIPTION LENGTH WIDTH THICKNESS QTY QTY/BLDG YIELD WEIGHT C ; BPL11 BASE PLATE 1 0 13/16 0 8 0/16 .5000 1 10 50.0 14.5 TPL11 TOP PLATE 3 8 O/1 , 0 8 0/16 .3125 1 10 50.0 31.5 STF11 STIFFENER PLATE 3 0 0/16 0 4 0/16 .3125 2 20 50.0 25.5 CPL11 CONNECTION PLATE 3 8 1/16 0 8 0/16 .7500 1 10 50.0 74.9 WEB11 WEB PLATE 10 6 13/16 2 1 3/16 .1875 1 10 50.0 WEB12 WEB PLATE 125.3 12 0 0/16 3 0 0/16 .1875 1 10 50.0 242.727 FLG11 FLANGE PLATE 12 7 13/16 0 8 0/16 .3125 1 10 50.0 107.5 FLG 12 FLANGE PLATE 9 8 0/16 0 8 0/16 .3750 1 10 50.0 98.6 FLG13 FLANGE PLATE 19 4 0/16 0 8 0/16 .5000 1 10 50.0 262.9 C 8 GIRT CUP 0 7 0/16 C 6 0/16 .1900 4. 40 50.0 FLANGE BRACE CLIP C 4 0/16 C 2 C/'6 90G 2 2C 50.0 'OTAL WEIGH?' 995.7 DETAIL OF CPL31 CO DETAIL OF CPL32 w W W T 00 19' 0- 3/16 \\ 5- 1 2" 10' 0 8'1O-15/16 2- 1/ 2" N N 5- 1/ 2" coin I i 5' 4-13/16 15' 4-13 6 2- 1/ 2" M �4-1 16" 10' 4-13 6 C 1 8 S.CO fl ¶ H _ -�- T I LLJ •• Co ) °'e _t g' 2-11 16 HOLE DIAMETER: .7500 HOLE DIAMETER: 1.0000 18'10-15/16 16' 8-13 16 15' 8-13 16 1 MAKE Co PCS. MARK: MFB 1 00-01 -030A PROFESSIONAL AIRCRAFT BUILDERS 10' 19' 2-11 16 3" 10' 0 8'10 1 16 co N M Q Q Frame Number 1 PRIMITIVE PARTMARK: MFB 1 FABRICATE 10 AS SHOWN DRAWING UNIT: FEET & INCHES PART MARK PART DESCRIPTION LENGTH WIDTH THICKNESS QTY QTY/BLDG YIELD WEIGHT CPL31 CONNECTION PLATE 3 8 1/16 0 8 0/16 .7500 1 10 50.0 74.9 CPL32 CONNECTION PLATE 2 0 1/ 4 0 8 0/16 .5000 1 10 50.0 27.5 WEB31 WEB PLATE 10 3 0/16 3 0 0/16 .2500 1 10 50.0 265.5 WE832 WEB PLATE 8 10 15/16 2 1 13/16 .1875 1 10 50.0 121.7 FLG31 FLANGE PLATE 10 0 0/16 0 8 0/16 .3125 1 10 50.0 85.04s . FLG32 FLANGE PLATE 8 10 15/16 0 8 0/16 .2500 1 10 50.0 60.6 FLG33 FLANGE PLATE 10 0 0/16 0 8 0/16 .3125 1 10 50.0 85.0 FLG34 FLANGE PLATE 9 2 11/16 0 8 0/16 .2500 1 10 50.0 62.7 ` C Cl 8 PURLIN CLIP 0 7 0/16 0 6 0/16 .1900 4 40 50.0 11.3 C3 FLANGE BRACE CLIP 0 4 0/16 0 2 0/16 .1900 8 80 50.0 4.0 TOTAL WEIGHT 798.2 DETAIL OF CPL41 DETAIL OF CPL32 , co : Lo 27' 4- 5/ 8 N 5- 1/ 2" N in I , ,h 20' 0 7' 3- 1 2 5- 1/ 2" iv i I 2- 1/ 2 r o 6' 4- 5 16' 4- 5/ 8 26' 4- 5/ 8 2- 1/ 2" N o 1' - 5 -ii T 8 11' 4- 5 8 21' 4 5 8 N N �' 1111 _L1111 Cl 8 �' •. lc-l) C3• o H _______ ••• N HOLE DIAMETER: .7500 7 1- 5 16 HOLE DIAMETER: .8750 27' 3- 1/ 2 17' 9-11 16 16' 9_11161 -11 16 26'10- 1 8 MAKE PCS. MARK: MFB 2 8 b -T 00-01 -030A PROFESSIONAL AIRCRAFT BUILDERS 27' 1- 5 16 ' 3- 1/ 2 12' 0 12' 0 d 2— 7/16" Frame Number 1 PRIMITIVE PARTMARK: MFB 2 FABRICATE 10 AS SHOWN DRAWING UNIT: FEET & INCHES PART MARK PART DESCRIPTION LENGTH WIDTH THICKNESS QTY QTY/BLDG YIELD WEIGHT CPL32 CONNECTION PLATE 2 0 1/ 4 0 8 0/16 .5000 1 10 50.0 27.5 CPL41 CONNECTION PLATE 3 0 9/16 0 8 0/16 .6250 1 10 50.0 51.8 WEB41 WEB PLATE 3 3 1/ 2 1 6 7/16 .1345 1 10 50.0 26.7 WEB42 WEB PLATE 12 0 0/16 1 11 3/ 4 .1345 1 10 50.0 115.9 WEB43 WEB PLATE 12 0 0/16 2 5 0/16 .1345 1 10 50.0 143.7 FLG41 FLANGE PLATE 20 0 0/16 0 8 0/16 .2500 1 10 50.0 136.0 FLG42 FLANGE PLATE 7 3 1/ 2 0 8 0/16 .2500 1 10 50.0 49.6 FLG43 FLANGE PLATE 20 0 0/16 0 8 0/16 .2500 1 10 50.0 136.0 FLG44 FLANGE PLATE 7 1 5/16 0 8 0/16 .2500 1 10 50.0 48.3 Cl 8 PURUN CLIP 0 7 0/16 0 6 0/16 .1900 6 60 50.0 17.0 C3 FLANGE BRACE CUP 0 4 0/16 0 2 0/16 .1900 6 60 50.0 3.0 TOTAL WEIGHT 755.3 DETAIL OF CPL31 is DETAIL OF CPL32 co co op 19' 0— 3/16 5— 1 2" I I i rj 10' 0 8'1O-15/16 2— 1/ 2" N `n N co I 5— 1/ 2 coin I I / 5 4-13 16 15' 4-13/ 6 2— 1/ 2" 1 1 1 1 4- 6" 10' 4-136 r- �- `� 1 1 1 1 41 I ZL zyz C o ao C3 N . -11 16 HOLE DIAMETER: .7500 HOLE DIAMETER: 1.0000 18'10-15/16 16' 8-13 16 15' 8-13 16 -T MAKE 4 PCS. MARK: MFB 3 00-01 -030A PROFESSIONAL AIRCRAFT BUILDERS 10' 3 19' 2-11 16 3" Wb.b5 16 co N M ol o _ I _ 0 N Frame Number 1 PRIMITIVE PARTMARK: MFB 1 FABRICATE 10 AS SHOWN DRAWING UNIT: FEET & INCHES PART MARK PART DESCRIPTION LENGTH WIDTH THICKNESS QTY QTY/BLDG YIELD WEIGHT CPL31 CONNECTION PLATE 3 8 1/16 0 8 0/16 .7500 1 10 50.0 74.9 CPL32 CONNECTION PLATE 2 0 1/ 4 0 8 0/16 .5000 1 10 50.0 27.5 WEB31 WEB PLATE 10 3 0/16 3 0 0/16 .2500 1 10 50.0 265.5 WEB32 WEB PLATE 8 10 15/16 2 1 13/16 .1875 1 10 50.0 121.7 FLG31 FLANGE PLATE 10 0 0/16 0 8 0/16 .3125 1 10 50.0 85.0 FLG32 FLANGE PLATE 8 10 15/16 0 8 0/16 .2500 1 10 50.0 60.6 FLG33 FLANGE PLATE 10 0 0/16 0 8 0/16 .3125 1 10 50.0 85.0 FLG34 FLANGE PLATE 9 2 11/16 0 8 0/16 .2500 1 10 50.0 62.7 Cl 8 PURLIN CLIP 0 7 0/16 0 6 0/16 .1900 4 40 50.0 11.3 C3 FLANGE BRACE CLIP 0 4 0/16 0 2 0/16 .1900 8 80 50.0 4.0 TOTAL WEIGHT 798.2 2Y 17' 3" 2�,2 21 ' c3, ZYL DETAIL OF CPL32 co DETAIL OF CPL41 v\i 27' 4- 5 8 M\\ r- � 7' 3— 1 2 `na' 5— 1/ 2" iV io r� 20' 0 1 5- 1/ 2" iv I I I 2- 1/ 2" r 6' 4- 5 16' 4- 5 8 26' 4- 5 8 M 2- 1/ 2" o 1' - 5 8 11' 4- 5 8 21' 4 5 8 * 1 ! L 1 1 o .. 2YZY� 2'�Z( ZVZ Gw,. I iv o HOLE DIAMETER: .7500 1- 5 16 HOLE DIAMETER: .8750 27' 3- 1/ 2 17' 9-11 6 16' 9-11 16 26'10- 18 � MAKE j PCS. MARK: MFB 4 -T 00-0 1 -030A _ Pa _ PROFESSIONAL AIRCRAFT BUILDERS 27' 1— 5116 ' 3- 1 12' 0 12' 0 co tfJ r' N 0 2— 7/16' Frame Number 1 PRIMITIVE PARTMARK: MFB 2 FABRICATE 10 AS SHOWN DRAWING UNIT: FEET & INCHES PART MARK PART DESCRIPTION LENGTH WIDTH THICKNESS QTY QTY/BLDG YIELD WEIGHT CPL32 CONNECTION PLATE 2 0 1/ 4 0 8 0/16 .5000 1 10 50.0 27.5 CPL41 CONNECTION PLATE 3 0 9/16 0 8 0/16 .6250 1 10 50.0 51.8 WEB41 WEB PLATE 3 3 1/ 2 1 6 7/16 .1345 1 10 50.0 26.7 WE842 WEB PLATE 12 0 0/16 1 11 3/ 4 .1345 1 10 50.0 115.9 WEB43 WEB PLATE 12 0 0/16 2 5 0/16 .1345 1 10 50.0 143.7 FLG41 FLANGE PLATE 20 0 0/16 0 8 0/16 .2500 1 10 50.0 136.0 FLG42 FLANGE PLATE 7 3 1/ 2 0 8 0/16 .2500 1 10 50.0 49.6 FLG43 FLANGE PLATE 20 0 0/16 0 8 0/16 .2500 1 10 50.0 136.0 OcT) FLG44 FLANGE PLATE 7 1 5/16 0 8 0/16 .2500 1 10 50.0 48.3 Cl 8 PURLIN CLIP 0 7 0/16 0 6 0/16 .1900 6 60 50.0 17.0 C3 FLANGE BRACE CLIP 0 4 0/16 0 2 0/16 .1900 6 60 50.0 3.0 TOTAL WEIGHT 755.3 1 OUNDARY SURVEY SECTION 13, TOWNSHIP 26 S., RANGE 21 E. Client: CITY OF ZEPHYRHILLS Work order number: 12525—ZH C-1 PA SCO COUNTY, FLORIDA Date of Survey: 8/9/99 SIR Radius = 173.00' Arc = 123.58' TIE—IN SURVEY � Tangent = 64.56' Client: Professional Aircraft Maintenance s, q, Chord = S.21'09'58"W., 120.97' Date of Survey: 4/30/2000 C-2 Radius = 64.00' ps Arc =100.53' Tangent .44 64.00' Chord =S. '17'57"W., 90.51 x�r coin OF 1X' �� L-1 = S. 4559'44" W., 27.45' SECTION 18-26-21 NORTH LINE OF SECTION SS �• �� L-2 = N. 45.59'44 E., 44.88' N. 89'54'37' E. T SIR t 1339.5r I �� SCALE: 1" = 100' PARCEL "A" �o�� NOT INCLUDED Aq '� 0' 100' 200' FIR 1/2" ti\\ �, LB 107 j \ ,� r� SURVEYORS NOTES: 1� 1. No underground installations or improvements have been 1�� s. 5 y� located except as noted. Rte x�2 \ ti 2. No instruments of record reflecting easements, rights of /� \ way, and/or ownership were furnished this surveyor except ov�T, s, \" O' as shown. tx�q ' k F` 3. aTis survey was prepared without the benefit of a title A� earch. 4. Basis of Bea-ings: The Easterly line of the Subject Parcel \ n D ry�ry' being S. 41'37'SO E. (ASSU ). . FIR 1/2" 1 62.3 Legend O LB 1 D7 \ FOJ P.O.C. Pont of Canmcncemerrt T.O.B. Top of Bank T �s P.C.P. Pemwnent Control Point T.O.S. Too of sikpe u r \�O i� L j'•`� ' SIR P.R .idPem mffd Reference vonument Cot . Concrete E1 P.O.B. Pohit of BeYmn ng A 'H. Mptmtt nt on Line WS. oecny b VACANT F.LF. farad ionhon Rod F. FrorM SP. Screened Porch urrront C.?. Carport F.W. Found Nai &D C.LF. Oith Link Fence Vj I EE7EA'TC:', POND Slk Set 1/7 ion Rod (LB 107) W.F. Wee Force i 4 S.N . Set tNNeaaifll&Disk (LB 107) D.F.k' Wood Fence ( Deecnphon or Record Pint Of( eerheod UtlOty line 3 I ►( —,ew Measured E/P Edge of Pmement• %o _ r" —� SIR Be Pr oned Section Breakdown SEC. Sectioonof� ay { D �^ CD: Chord Distance 1 R/fAY a jfatu'ed Bane o CB,= gwrd Bung ZHCCI. Zeptythits Cofay Compary lams `L P.CS C Pico County Seciion Corti P'of— Centai ak z GE OF P6`TLG Gi Page �` QG S. 89'17'57' W. 526.10'L SIR SIR T 1 T ', L Z P 'RP�� S UNIG1 -:':L AIRPORT 6 `'r ed n 9 'E :soo '� A " N. s9'54'37' E. Zpphyrhffis St. Petersburg 4_1 29 roi i ,GE Or P IVING x ^l, Certificate of authorization number LB 107 Not valid without the signature and the original 'o o • raised seal of a Florida licensed surveyor and mapper. The prcperty described hereon was surveyed under my �,•' �• direction and supervision, the sketch hereon is a true and o• o. — — accurate representation of the same an this survey meets the N. 841'1f E. ( �_� t Minimum Technical Standards set forth by the Florida Board of 628.85' SEE SHEET 2 FOR LEGAL DESCRIPTION Professional Land Surveyors in Chapter 61G17-6 Florida Administrative Code pursuant to TS(e�ctitiron(�472.027, Florida Swta�t}utte]s. f �► ��v' , OTi xT H. DT li d1O1 T e.L ..-PE! 4P 'da Su.rveayo 's Regi ire i n 1'.% . 672 20 8— 5 8 1O' 7- 718 1 0' p DETAIL OF TPL1 1 DETAIL OF BPL11 4- 4— 1/ 2" 7'd4 1 ' 4 17' 4 — 3/ 4" N `r DETAIL OF CPL11 1— 1 2 s / 10 9 16" I I � --f- C i 8 C 3 rn •• - � 19' 10- 37 i0 9i6" i6" HOLE DIAMETER: .8750 20' 7- 7/ 8 HOLE DIAMETER: .8750 20' 1- 7 8 MAKE 5 PCS. MARK: MFC 1 a 00-01 -030"B" PROFESSIONAL AIRCRAFT 20' 8-11/16 MAINTENANCE 12' 0 8_'88-111r 16 11'11— 3/16 1 O 2 r o O Frame Number 1 PRIMITIVE PARTMARK: MFC 1 FABRICATE 5 AS SHOWN DRAWING UNIT: FEET & INCHES II - PART MARK PART DESCRIPTION LENGTH WIDTH THICKNESS QTY QTY/BLDG YIELD WEIGHT BPL11 BASE PLATE 0 10 1/ 2 0 6 0/16 .5000 1 5 50.0 8.9 1 , TPL1 1 TOP PLATE 1 6 5/16 0 6 0/16 .2500 1 5 50.0 7.8 N CPL11 CONNECTION PLATE 0 10 9/16 0 6 0/16 .5000 1 5 50.0 9.0 WEB1 1 WEB PLATE 8 8 11/16 0 10 0/16 .1345 1 5 50.0 39.9 �"` WEB12 WEB PLATE 12 0 0/16 0 10 0/16 .1345 1 / 5 50.0 54.9 FLG11 FLANGE PLATE 10 7 7/ 8 0 6 0/16 .2500 1 5 50.0 54.3 FLG12 FLANGE PLATE 10 0 0/16 0 6 0/16 .2500 1 5 50.0 51.0 FLG13 FLANGE PLATE 19 1O 3/$ 0 6 0/16 .2500 1 5 50.0 101.0 Cl 8 GIRT CLIP 0 7 0/16 0 6 0/16 .1900 3 15 50.0 8.5 C3 FLANGE BRACE CLIP 0 4 0/16 0 2 0/16 .1900 1 5 50.0 .5 TOTAL WEIGHT 335.8 DETAIL OF CPL21 DETAIL OF CPL22 ,� 18' 6 ¢ `t 8 _ _ 9'1 i -15 16 4 1/ 2" co ro I i 1 - 1/ 2" 6' 7- 3 6 14' 8' 5- 1 / 9- 3 16 4- 1/ 2" o ,.o 6- 3 1 1 ' 8- 3 16 1 - 1/ 2" -� Cl 8 _ C3 0 8' 5- t $ 9'11 -15/16 HOLE DIAMETER: .8750 18' 5 HOLE DIAMETER: .8750 1 H it l 7' 1 MAKE 5 PCS. MARK: MFB 1 00-01 -030"B" PROFESSIONAL AIRCRAFT MAINTENANCE 8' 5-15/16 0-13/16" 8' 5— 1 8 9'11 -15/16 N i O 7Io Frame Number 1 PRIMITIVE PARTMARK: MFB 1 FABRICATE 5 AS SHOWN DRAWING UNIT: FEET & INCHES PART MARK PART DESCRIPTION LENGTH WIDTH THICKNESS QTY QTY/BLDG YIELD WEIGHT CPL21 CONNECTION PLATE 0 10 9/16 0 6 0/16 .5000 1 /7 CPL22 CONNECTION PLATE 0 10 9/16 0 6 0/16 .5000 1 5 50.0 9.0 5 50.0 9.0 WEB21 WEB PLATE 8 5 15/16 0 10 0/16 .1345 1 5 50.0 38.8 WEB22 WEB PLATE 9 11 15/16 0 10 0/16 .1345 1 5 50.0 4 FLG21 FLANGE PLATE 8 5 1/ 8 0 5 0/16 .2500 1 5.7 / 5 50.0 35.8 FLG22 FLANGE PLATE 8 5 1 / E 0 5 0/16 .2500 1 5 50.0 36.1 FLG23 FLANGE PLATE 9 11 15/16 0 5 0/16 .2500 1 5 FLG24 FLANGE PLATE 50.0 42.5 9 1 1 15/16 0 5 0/16 .2500 1 5 50.0 42.5 Cl 8 PURLIN CLIP 0 7 0/16 0 6 0/16 .1900 4 20 50.0 11 .3 C3 FLANGE BRACE CLIP 0 4 0/16 0 2 0/16 .1900 4 20 50.0 2.0 TOTAL WEIGHT 272.6 REVISIONS [1] 2] [3] [4] [5] DESIGN CRITERIA F OH ' r wi r ONI v LtJ BUILDING DESIGNATION BUILDING "B" BUILDING CODE SBC'97 � I 'h I ' I LLB CLASSIFICATION ENCLOSED LIVE LOAD 12.0 PSF j FRAMES 121 112 Id. LIVE LOAD 20.0 PSF j SECONDARY v� ;• _ � SNOW LOAD 0.0 PSF gw N WIND LOAD 110.0 MPH U. IMPORTANCE 1.0 o a. SEISMIC 0.05 Av � VELOCITY SEISMIC 0.05 Aa ACCELERATION X N DEAD LOAD 2.30 PSF m 0 � N COLLATERAL LOAD 0.0 PSF SPECIAL LOADINGS : NONE W L+- u W FOUNDATION DESIGN : STEEL BUILDING SYSTEMS, INC. IS NOT RESPONSIBLE FOR THE DESIGN, MATERIALS, AND WORKMANSHIP OF THE FOUNDATION. Cl) ANCHOR BOLT PLANS PREPARED BY SBS" ARE INTENDED TO SHOW ONLY OD LOCATION, SIZE, AND PROJECTION OF ANCHOR BOLTS. "SBS IS RESPON - /2 SIBLE FOR PROVIDING THE LOADS IMPOSED BY THE BUILDING(S) ON THE 1 IL FOUNDATION. IT IS THE RESPONSIBILTY OF THE CUSTOMER TO ENSURE o - THAT ADEQUATE PROVISIONS ARE MADE FOR FOUNDATION DESIGN. jw NO BY 00-01-030B 02-02-2000 ME stye NONE lint DESIGN REVISIONS [1] [2 [3) 14] [5] L V BUILDING "A" ---------------------- i Z w I I { I I I I I I ( i o o I I I I I o cis o I I ( 01 e o mi o l u. t o CD .. o .i Ooi � O I o ❑0 5' 4 I I I I o 0 o *I I I I I o o{o 0 Q 0 0{0 GIG 0{0 CIO r O O A 92'10 O r r 1 ' 0 24' 0 25' 0 25' 0 24' 0 1 ' 0 100' 0 � � co NOTE: ALL TAIL DIMENSIONS FOR OPENINGS ARE FROM EDGE OF SLAB. z 5 uiw � r a ° W O0-01-0308 7(( 02-02-2000 MSS 'NONE TME, A/BOLT PLAN MuweEa 9 O B REVISIONS A ['] r2] r3] DETAIL DETAIL 0� A� [4] 1 4 r5] v NOTE: POSITIVE REACTIONS ARE UP AND TO THE LEFT. 0' 2 0' 4 - REACTION (KIPS) DESCRIPTION SUPPORT HORIZ VERT Z * * o W 1 1 .OD+1 .OL 1 .00 3.39 0 1 1 .OD+1 .OL 4 .00 3.39 N w o 2 1 .OD+1 .OW C 1 1 1 .32 -4.45 0 LOCATION O 2 1 .OD+1 .OW C 1 4 .50 -4.60 O U 3 1 .OD+1 .OW Cl 1 -2.91 -3.06 d °- 3 1 .OD+1 .OW Cl 4 -3.45 -2.53 USE (2) 1 /2 x 12 A/BOLTS USE (2) 1 /2 x 12 A/BOLTS o 4 1 .OD+1 .OZ 1 .00 .55 O 4 1 .OD+1 .OZ 4 .00 .55 DETAIL© DETAIL H� w a- c Q 5 1 .OD+1 .OS 1 .00 .55 4" .. O 5 1 .OD+1 .OS 4 .00 .55 1 -1/2 1 -1 /2" MO 6 1 .OD+ .5S+1 .OW Cl 1 1 .32 -4.45 - - z1 6 1 .OD+ .5S+1 .OW Cl 4 .50 -4.60 7 1 .OD+ .5S+1 .OW Cl 1 -2.91 -3.06 z 7 1 .OD+ .5S+1 .OW Cl 4 —3.45 —2.53 0 - o a 8 1 .OD+1 .OS+ .5W Cl 1 .66 —2.02 0 0 8 1 .OD+1 .OS+ .5W Cl 4 .25 —2.10 1 LOCATION p T 9 1 .OD+1 .OS+ .5W Cl 1 -1 .46 -1 .33 9 1 .OD+1 .OS+ .5W Cl 4 -1 .72 -1 .06 USE (2) 5/8 x 12 A/BOLTS USE (2) 3/4 x 12 A/BOLTS w O 10 1 .OD+1 .OS+1 .OZ 1 .OZ 1 .00 .55 10 1 .OD+1 .OS+1 .OZ 4 .00 .55 y O Z J ti W QTY DESCRIPTION PROJECTION (IN) u N 8 AB.5x 12 1 .50 4 AB.63x12 1 .50 a 10 AB.75x 12 2.00 A/BOLT PROJECTION :1! )v C J°°"°`00-01-030B v-t __________ BY: 02-02-2000 MSS I NONE ,mE A/BOLT DETAILS : 9 0 REVISIONS [z] BUILDING „A„--�"-----------------------------------------i 1 -P 1 2 2 1 -P 2 1 1 1 -P 2 2 2 [4] 1 -P 1 PURLINS [5] III III IIILU O- - Vc< o w ___________ ___________H___________ ___________I ______ ______ TIJ______ H II __________ __________ N = 0 EAVE STRUTS: 1 -EP1 1 -EP1 1 -EP1 1 -EP1 t Q LU 25' 0 25' 0 25' 0 25' 0 O I�u 100' 0 a 2 3 4 5 PURLIN ENDWALL CONNECTION DETAIL FOR FRAME LINE 1 IS ROOF03 -- PART LEFT RIGHT— ax PURLIN ENDWALL CONNECTION DETAIL FOR FRAME LINE 5 IS ROOF03 QTY MARK DESCRIP LENGTH LAP LAP PURLIN FRAME CONNECTION DETAIL AT FRAME LINE(S) 2 - 4 IS ROOF04 2 1 -CB1 CBL .25 26 1 - 5/16 EAVE STRUT ENDWALL CONNECTION DETAIL FOR FRAME LINE 1 IS ROOF05 2 1 -C82 CBL .25 26' 7 o EAVE STRUT ENDWALL CONNECTION DETAIL FOR FRAME LINE 5 IS ROOF05 4 1 -EP1 8 ES 14 24'1 1 - 1 2 w L EAVE STRUT FRAME CONNECTION DETAIL AT FRAME LINE(S) 2 - 4 IS ROOF05 4 1 -P 1 8Z25 14 27' 0 22 w LONGITUDINAL BRACING DETAIL DESIGNATIONS 4 1 —P 1 8Z25 14 27' 0 22 C'3 ti a = CBLO1 4 1 —P 2 8Z25 14 28' 0 11 22 Z o b = CBL01 4 1 —P 2 8Z25 14 28' 0 22 11 a N c = CBLO1 SECTION LAP AT SUPPORTS Fio LAP INDICATOR LAP LENGTH (FT & IN o. x ci3 2 2' 0 Jae No 00-01-0308 o�. 02-02-2000 J/1 ) 7O MSS I NONE Cdr ROOF FRAMING NUMBER. REVISIONS [l] 2] [3] [4] DETAIL ROOF03 DETAIL ROOF04 DETAIL ROOF05 [5] w LAP V 1 ' 0" PURLIN �� (8)M.5x1 .0 (2) M.5x1.0 EAVE STRUT e o__of4X2x14AN 1 of 0 [RAKE ANGLE] O (2) M.5x1.0 o o oI o I a PURLIN PURLIN COLUMN[MAINFRAME] RAFTER ENDWALL RAFTER [EXPANDABLE] [FLUSH] [MAINFRAME] .� ® ISO LL 0 PURLIN TO ENDWALL RAFTER PURLIN CONNECTIONS AT MAINFRAME EAVE STRUT CONNECTION AT MAINFRAME DETAIL ROOFO6 DETAIL OBL01 cb 2 M.5x1.0 CABLE PURLIN ( ) 20 EAVE STRUT a M c GRIP COLUMN OR ; o 1 o 0 Q' RAFTER i i w C7 LL o i0 of 0 � O RAFTER EYE-BOLT ' [ANY TYPE] HILLSIDE FTER FLANGE w [MAINFRAME] BRACE (2x2x14AN) ' CO o M.5x1.0 / _____ '' d. 00-01-0308 EAVE STRUT CONNECTION AT ENDWALL CABLE INSTALLATION DETAIL FLANGE BRACE DETAIL 0 02-02-2000 ME I NONE ,q - ROOF DETAILS REVISIONS [1] [2] [3] [4] [5] Lii O O O G 2 W OJ 3 1 1 3 2 SECTION LAP INDICATORS _ ICI 2±1 - Q O 1-J 3 _H 1-J 3 Q Q 1-S 1J _________________________fi_________________________ ________________________ VJJ N 1—FGfl. 0 h d 1—H 1 — 1—G 3 —GUT 1—G 3 `� Q 1—S 1 .. N J O Q 4X2X14AN BASE SUPPORT 25' 0 25' 0 25' 0 25' 0 10010 � n r SIDEWALL AT A GIRT CONNECTION DETAIL FRAME LINE DESCRIPTION ®. 1 SWO3 O 4' 5 SW03 O* N PART LEFT RIGHT- 2 -4 SW04 QTY MARK DESCRIP LENGTH LAP LAP W C7 L 2 1-CB3 CBL .25 31' 9-11/16 W �p 3 1-G 3 8Z25 14 28' 0 11 32 SECTION LAP AT SUPPORTS N LAP INDICATOR LAP LENGTH (FT & IN .`d' 3 1—G 3 8Z25 14 28' 0 23 11 � J ti 3 1—G 3 8Z25 14 28' 0 32 1 1' 0 2 2' 0 W co 3 1—FG3 8Z25 16 1' 7— 3/ 4 2 2' 0 2 1—FG4 8Z25 16 4'11— 1/ 2 3 1—FG6 8Z25 14 20' 7— 3/ 4 23 LONGITUDINAL BRACING DETAIL DESIGNATIONS a _ 2 1—J 3 8C35 14 20' 7— 1 2 b =CBL01 2 1-H 1 8C35 14 5' 0 �- 2 1-S 1 8C35 14 5' 0 ,NO, 00-01-030B /( 02-02-2000 ,. MSS s NONE S W FRAMING s REVISIONS [1] z [3] [4) [5] W DETAIL SWO3 DETAIL SW04 1"sD SCREW V' i BASE ANGLE) EACHGIRT) ENDWALL EAVE STRUT) COLUMN [FLUSH] COLUMN SW GIRT [MAINFRAME] [MAINFRAME] --�*** GIRT LI 8)M.5x1.0 3x3x14AN Io o; a o o I0 0; I II 1 1 , (2) M.5x1.0 0 I o 0; o ' ----- (TYPICAL) ------ ' JJGIRT 3x3x14AN GIRT �--- LAP GIRT EW GIRT W N J SIDEWALL [CORNER ANGLE] LL SIDEWALL [BYPASS] [BYPASS] ***NOTE:CUT 8-1/4" OFF I/S FLANGE OF GIRT. GIRT CONNECTIONS AT EXPANDABLE ENDWALL GIRT CONNECTIONS AT MAINFRAME CORNER ANGLE DETAIL DETAIL CBL01 DETAIL F002 DETAIL F005 DETAIL F006 w4 (2) M.5x1.25 CABLE EAVE STRUT [IF GREQ'D] c -- c • tD j GRIP COLUMN OR (2) H.5x1.25 o SILL I I d. 00 RAFTER (IF REQ'D) (2) M.5x1.0 W cc EYE-BOLT JAMB JAMB JAMB o o O HILLSIDE (2) A8.5x12 (2) M.5x1.0 w 1 A (2) H.5x1.25 0 HEADER GIRT W {,j :r � � acm CABLE INSTALLATION DETAIL FRAMED OPENING JAMB SIDEWALL FRAMED OPENING JAMB GIRTS TO JAMB ®'` ra __O 1 00-01-0308 u : iHI 02-02-2000 ME sr2 NONE S/W DETAILS OF 1 REVISIONS [1] 1.0012 a I KE ANGLE i / RA t [ ] I 1 [4] I 1 [51 U I sa t — PART tU ¢ I N QTY MARK DESCRIP LENGTH I 3 1—G 1 8Z25 16 9' 7— 1/ 2 st 1—G 1 1—G 2 i J 6 1—G 2 8Z25 16 10' 3— 1 2 m o � m i 3 1—FG1 8Z25 16 1' 3— 1/ 2 W N �t v i 3 1—FG2 8Z25 16 1' 7— 1 2 m iN I 2 1—FG5 8Z25 16 5'11— 1/ 2 Z 1 1—J 1 8C35 14 20' 1-11/16 1 -- 1 1—J 2 8C35 14 20' 7-11/16 BASE SUPPORT 2 1-H 2 8C35 14 6' 0 JO 4X2X14AN • 10' 0 10' 0 2 1-S 2 8C3514 6' 0 SWL = LEFT SIDEWALL tt771� I'M 20' 0 4" SWR = RIGHT SIDEWALL ENDWALL AT FRAME LINE 5 g Q ENDWALL COLUMNS L1 PART MARK LOCATION LENGTH DESCRIPTION TOP OF COL BASE OF COL GIRT TO COL .. N 1-IC1-5 I 1 I 20' 9-11/16 I8C4O 12 IEWii IEWO8 IEW23 0. rj 1.00/12 RAKE I i'd1 4 -`-- ANGLE x tt\ a I 1-FG5 O t9 � a Z N Q rq Ui' 1-FG1 1- G5 1-FG2 U !a W 1-G 2l1-H2Z N 1-S 2 BASE SUPPORT c1tL 4X2X14AN • ��, 10' 0 10' 0 4" 20' 0 JW N0 00-01-0308 02-02-2000 oae: BY; IBCME; ENDWALL AT FRAME LINE 1 I j MSS NONE ENDWALL COLUMNS ,mE PART MARK LOCATION LENGTH DESCRIPTION TOP OF COL BASE OF COL GIRT TO COL E FRAMING 1-IC1-1 1 I 20' 9-11/16 I 8C40 12 I EW11 I EW08 I EW23 REVISIONS [1] [2] [3] [4] [5] DETAIL EW08 DETAIL EW11 DETAIL EW23 w v o BASE PLATE ENDWALL "-"' [FLUSH] GIRT o o is LLI 9 (2) 5/8"x 12"A/B (2) H.5x1.25 (2) M.5x 1.0 o: _ [FIELD LOCATE] COLUMN ENDWALL J COLUMN BRACKET COLUMN [FLUSH] U. _ ® _ _ o o CJ W (2) H.5x1.25 0 [SINGLE CEE] (2) M.5x1.0 ---- o, EDGE OF RAFTER Q SLAB . (EXPANDABLE] COLUMN GIRT [ANY TYPE] O. N SINGLE CEE INTERIOR COLUMN EXPANDABLE RAFTER / COLUMN CONNECTION ENDWALL GIRTS TO INTERIOR COLUMN A" DETAIL F001 DETAIL F002 DETAIL F006 RAFTER s- GIRT- [SINGLE OR DOUBLE CEE] [IF REQ'D] r; o 1 • ____ I (2) H.5x1.25 0 (2) H.5x1.25 o SILL (IF REQ'D) (2) M.5x1.0 all JAMB JAMB JAMB o o W (2) AB.5x 12 (2) M.5O.0 o (2) H.5x1.25 Ifo O HEADER GIRT ••;cb :? • ' a !7 vQ+ aA F1O2G I ENDWALL FRAMED OPENING JAMB FRAMED OPENING JAMB GIRTS TO JAMB U 00-01-0308 n , 02-02-2000 : ME I NONE E DETAILS r_4� REVISIONS ['] z [3] 16' 4 [4] 4 © 4' 1 [5] W V Q et w--1 ot: FB 2 FB 3 FB 4 FB5 ----------- ----- ± _ 5® z c; o > p w L r L VJ CL 00 IUL O ® I I/ N I IL O I � � -------------------� 0' 8 20' 0 V_ N JOINT INFORMATION a w JOINT PARTMARK DEPTH THICKNESS BOLT QTY DESCRIPTION 1 MFC 1 0' 10 0. 1345 2 AB.75x12 2 MFC 1 0' 10 0.1345 4 H.75X2.5 2 MFB 1 0' 10 0.1345 z 3 MFB 1 0' 10 0.1345 4 H.75X2.5 Li FLANGE BRACE TABLE a PARTMARK LENGTH PLACEMENT QTY/FRAME QTY/BLDG FB 1 2' 3- 7/ 8 NS 1 5 - FB 2 2' 3- 7/ 8 NS 1 5 00-01-0308 FB 3 2' 3- 7/ 8 NS 1 5 02-02-2000 MSS I NONE FB 4 2' 3- 7/ 8 NS 1 5 `' CROSS SECTION FB 5 2' 3- 7/ 8 NS 1 5 : C REVISIONS C1] [2 [3] (4] [5] BUILDING "A" ; 3„ LAP W � NT0 "A" flu N O 4" 11 8 0/HANG PANEL FASTENERS 1. PANEL ENDS: SPACING FOR PANEL TO PURLIN FASTENERS TO BE IN x A 4-8-4-8-4-8 IN. PATTERN LOCATED 2 IN. FROM THE CENTER LINE ON BOTH SIDES OF EACH MAJOR RIB. FASTENER TO BE A NO. 12 SELF-DRILLING SCREW. X 2. INTERIOR OF PANEL: çLLlLL SPACING FOR PANEL TO PURLIN FASTENERS TO BE IN A 12-12-12 IN. PATTERN LOCATED 2 IN. FROM THE CENTER LINE OF EACH MAJOR RIB. FASTENER TO BE Z A NO. 12 SELF-DRILLING SCREW. 3. SIDE LAPS: 4 Cy^ SPACING FOR PANEL TO PANEL FASTENERS AT SIDE LAPS TO BE 30 IN. ON CENTER. FASTENER TO BE A NO. 14 SELF-DRILLING SCREW. NOTE: TAPE SEALER REQUIRED AT SIDE LAPS WHEN USED AS ROOF PANELS. I 00-01-0308 i' 02-02-2000 �/ � MSS x NONE ROOF PANELS Musa, O REVISIONS [1] [2) [a] . [4] [5] W OPEN AND COMMON V G LU z W SIDEWALL AT B v O 28 = O IfL Q N � N SIDEWALL AT A Q PANEL FASTENERS O V_ TJ111. PANEL ENDS: ' S SPACING FOR PANEL TO PURLIN FASTENERS TO BE IN W A 4-8-4-8-4-8 IN. PATTERN LOCATED 2 IN. FROM �O THE CENTER LINE ON BOTH SIDES OF EACH MAJOR RIB. ca CD v FASTENER TO BE A NO. 12 SELF-DRILLING SCREW. Z r r 0 2. INTERIOR OF PANEL: r 0 N r o p N N SPACING FOR PANEL TO PURLIN FASTENERS TO BE IN N N �- Q N A 12-12-12 IN. PATTERN LOCATED 2 IN. FROM THE N N N N N N r CENTER LINE OF EACH MAJOR RIB. FASTENER TO BE N a A NO. 12 SELF-DRILLING SCREW. ,_,,,� 3. SIDE LAPS: SPACING FOR PANEL TO PANEL FASTENERS AT SIDE 0 jw No 00-Oi-0308 ENDWALL AT 5 LAPS TO BE 30 IN. ON CENTER. FASTENER TO BE ENDWALL AT 1 A NO. 14 SELF-DRILLING SCREW. r r 02-0 -2000 MSS I NONE NOTE: TAPE SEALER REQUIRED AT SIDE LAPS f *WALL PANELS WHEN USED AS ROOF PANELS. Al su o REVISIONS [1] 2 [3] [4] [5] OPEN AND W U COMMON LL SIDEWALL AT B U dj w s •• GUTTER Q Q IL kflJ* 0 a o (� BASE TRM SIDEWALL AT A 0 * HEAD TRM W L :< * 4 < 1 j tl it Z W n I O* tl z i o i 11 o i �, IL ( t m i *1E;J* 0 20 jmNO: I 00-01-0308 BASE TRM 1 t I BASE :TRM r ! 02-02-2000 -------, L------- � �I \ 1 f' er. ME NONE ENDWALL AT 5 ENDWALL AT 1 t` TRIM LOCATIONS O REVISIONS [1] 7/8w LAP SCREW ROLL CAULK (24"ON CENTER) WALL PANEL [21 ROOF PANEL [3] 0/S CORNER TRIM [4] �--RAKE TRIM 7/8"LAP SCREW [5) (24"ON CENTER) LU 7/8"LAP SCREW (24"ON CENTER) WALL PANEL WALL PANEL. Q = RAKE TRIM DETAIL 0/S CORNER DETAIL 'N ROOF PANEL I/S CLOSURE (IF UN-INSULATED) 7/8"LAP SCREW (24" ON CENTER) GUTTERg3 ji RAKE TRIM LL GUTTER WALL PANEL- 0 FLUSH WITH ANGLE 'X" BOTTOM OF u CORNER CO I/S CLOSURE GUTTER AND FOLD (IF UN-INSULATED) TABS INTO D'SPOUT BASE TRIM �'• rj DOWNSPOUT WALL PANEL END ER NOTE: INSTALL GUTTER STRAPS 3'0" ON CENTER. NOTE: INSTALL D'SPOUT STRAPS 5'0" ON CENTER. =4 O T61 • c*3 GUTTER DETAIL GUTTER END DETAIL BASE TRIM DETAIL W HEAD TRIM y w W uJ WALL PANEL Q N 1"SD SCREW y �. (12 ON CENTER) p� 1"SD SCREW (12" ON CENTER) WALL PANEL HEAD TRIM 1"SD SCREW WALL PANEL W HEAD TRIM (24" ON CENTER) 0 sae NO : 00-01-030B f au� 02-02-2000 MENONE im TRIM DETAILS Nu HEAD TRIM DETAIL AT HEADER HEAD TRIM DETAIL AT SILL HEAD TRIM DETAIL AT JAMB REVISIONS [1] s] [3] [4] [5] DESIGN CRITERIA V t C, BUILDING DESIGNATION BUILDING "A" p t>C _____ FOB E'fl3LMflLQNLY BUILDING CODE SBC'97 W CLASSIFICATION ENCLOSED I I OT tr 01 LIVE LOAD 12.0 PSF FRAMES 0 O LIVE LOAD 20.0 PSF SECONDARYFit I T 1 O N SNOW LOAD 0.0 PSF O 8 o W WIND LOAD 110.0 MPH .• O N IMPORTANCE 1.0 CL SEISMIC 0.05 Av VELOCITY SEISMIC 0.05 Aa ACCELERATION h 4— DEAD LOAD 2.22 PSF 2 O � N. COLLATERAL LOAD 0.0 PSF a t*i SPECIAL LOADINGS : NONE W C9 LL qt Lu FOUNDATION DESIGN : STEEL BUILDING SYSTEMS, INC. IS NOT RESPONSIBLE Cl) < FOR THE DESIGN, MATERIALS, AND WORKMANSHIP OF THE FOUNDATION. ANCHOR BOLT PLANS PREPARED BY "SBS" ARE INTENDED TO SHOW ONLY LOCATION, SIZE, AND PROJECTION OF ANCHOR BOLTS. "SBS" IS RESPON - o g SIBLE FOR PROVIDING THE LOADS- IMPOSED BY THE BUILD1NG(S� ON THE O. FOUNDATION. IT IS THE RESPONSIBILTY OF THE CUSTOMER TO NSURE THAT ADEQUATE PROVISIONS ARE MADE FOR FOUNDATION DESIGN. JOB No 00-01-030A 02-02-2000 ar aruE MSS NONE C2 a DESIGN NUR REVISIONS m 1 [1] T T T T T 2 i 3] of I 1 I I [4] N [5] I I I I I v I I I i I I i I Ia I I I I w o I I I I I �. I I I I I I i I 0 I I I I I° I I I .. I a $ I I I I I N I I I I I 0O I I I I I to � a I I I I 1 I I I I I I I t o - I I I i N X I t t I I I I I I C5 Ig I I I I i I 1 I I o I I N t� I I I I I w � a Ce rA 1 0 24' 0 25' 0 25' 0 24' 0 ' 0 £B N0: 00-01-030A DATE: 02-02-2000 100' 0 MSS I NONE 1 5 A/BOLT PLAN NUIeFA BUILDING B" 0 REVISIONS [1] (2] (3] (4] A B [5] LU V 1 7 � o DETAIL 0❑ DETAIL© NOTE: POSITIVE REACTIONS ARE UP AND TO THE LEFT. REACTION (KIPS) 0' 2 0' 4 I DESCRIPTION SUPPORT HORIZ VERT 1 1 .OD+1 .OL 1 -13.81 18.60 N O 1 1 .OD+1 .OL 7 13.81 18.60 LL X Z N Z * 2 1 .OD+1 .OW Cl 1 16.79 -21 .00 0 O 2 1 .OD+1 .OW Cl 7 -8.66 -15.10 v 3 1 .OD+1 .OW C2 1 11 .55 -10.82 0 J B 3 1 .OD+1 .OW C2 7 -3.43 -4.92 I w CL 4 1 .OD+ 1 .OZ 1 -2.92 3.94 p N o 4 1 .OD+1 .OZ 7 2.93 3.94 USE (2) 1/2 x 12 A/BOLTS USE (2) 5/8 x 12 A/BOLTS E 5 1 .OD+ 1 .OS 1 -2.92 3.94 DETAIL H • 5 1 .OD+1 .OS 7 2.92 3.94 ❑ - „ 1 -1 /2" T, 6 1 .OD+ .5S+1 .OW Cl 1 16.79 -21 .00 11 /2 6 1 .OD+ .5S+1 .OW Cl 7 -8.66 -15.10 7 1 .OD+ .5S+1 .OW C2 1 11 .55 -10.82 2 7 1 .OD+ .5S+1 .OW C2 7 -3.43 -4.92 8 1 .OD+ 1 .OS+ .5W C 1 1 7.30 -9.02 8 1 .OD+ 1 .OS+ .5W C 1 7 -3.23 -6.07 � w � tL 9 1 .OD+1 .OS+ .5W 02 1 4.68 -3.93 0 ( w 9 1 .OD+1 .OS+ .5W C2 7 -.62 -.98 C3 10 1 .OD+1 .OS+1 .OZ 1 -2.92 3.94 0 LOCATION w 10 1 .OD+1 .OS+1 .OZ 7 2.93 3.94 USE (4) 3/4 x 24 A/BOLTS QTY DESCRIPTION I PROJECTION (IN) 12 AB.63x 12 1 .50 JW _ 00-01-030A 40 J AB.75X24 I 2.00 1 02-02-2000 A/BOLT PROJECTION 4BY: MSS 'NONE A BOLT DETAILS 1 1-P 3 1 1 1-P 1 2 2 1-P 2 1 1 1-P 2 2 2 1-P 1 PURUNS III 1-EP2 I I I 1-EP1 III 1-EP1 III 1-EP1 EAVE STRUTS: (1, REVISIONS O = A . 1 2 PART LEFT RIGHT- [37 MARK DESCRIP LENGTH LAP LAP [4] 4 1-CB1 CBL .25 28 7 4 1-CB2 CBL .25 30' 9 [5] = _______________ 11 4 1-CBS CBL .25 31' 5- 5/18 6 1-EP1 8 ES 14 24'11- 1 2 W 2 1-EP2 8 ES 12 27'11- 1/ 2 O 20 1-P 1 8Z25 14 27' 0 11 22 Zr a 20 1-P 1 8Z25 14 27' 0 22 G 20 1-P 2 8225 14 28' 0 11 22 W 20 1-P 2 SZ25 14 28' 0 22 11 u 20 1-P 3 SZ25 18 5' 0 11 W OJ SECTION LAP AT SUPPO I = L6. LAP INDICATOR LAP LENGTH (FT & IN z 1 1' 0 I 2 2' 0 3 3' 0 LONGITUDINAL BRACING DETAIL DESIGNATIONS LL a _CBLO1 b =CBL01 �/J ft c =CBLo1 W LU N 0 � O __ H________ __ ____ H 1 . = II "\ H . bb ________ IlL_______ .11 _______ : u. _______ _______ _______ r r OWEW ®. - 1—EP2 1—EP1 1—EP1 1—EP1 EAVE STRUTS:3 J25' 0 25' 0 25' 0 25' 0 � W 0/HANG 100' 0 F- O 0 Q 5 = N CL BUILDING B' I .Joe No 00-01 -030A PURUN ENDWALL CONNECTION DETAIL FOR FRAME UNE 1 IS R00F033 ame PURUN ENDWALL CONNECTION DETAIL FOR FRAME UNE 5IS ROOF03 02-02-2000 PURUN FRAME CONNECTION DETAIL AT FRAME UNE(S) 2 -4 IS ROOF04 MSS ,NONE EAVE STRUT ENDWALL CONNECTION DETAIL FOR FRAME UNE 1 IS ROOF05 � ROOF FRAMING EAVE STRUT ENOWALL CONNECTION DETAIL FOR FRAME UNE 5IS ROOF05 p( NJMM EAVE STRUT FRAME CONNECTION DETAIL AT FRAME UNE(S) 2 -4 IS ROOF05 2 o H REVISIONS [1] 2 [3] [4] DETAIL CBL01 DETAIL R00F03 [5] v PURLIN PURLIN 1! D» CABLE 2 0 �� r W OJ GRIP COLUMN OR ; o o o o c 4x2x14AN RAFTER i i i [RAKE ANGLE] W O 0' EYE—BOLT O i O i (2) M.5x 1.0 HILLSIDE c V [MA�RA BRACEFLAE RAFTER ENDWALL a �j (2x2x14AN) [EXPANDABLE] [FLUSH] O M.5x1.0 Q ILtJ��J.. .. O J CABLE INSTALLATION DETAIL FLANGE BRACE DETAIL PURLIN TO ENDWALL RAFTER DETAIL R00F04 DETAIL R00F05 DETAIL R00F033 LAP (8)M.5x1.0 (2) M.5x1.0 /4x2x14AN EAVE STRUT i 0 O; O O i0 Oi O N O P 0 10 0: O 1 i 1 CO- J PURLIN PURLIN COLUMN PURLIN (8) M.5x1.0 [MAINFRAME] RAFTER ENDWALL [MAINFRAME] RAFTER W W [EXPANDABLE] W PURLIN CONNECTIONS AT MAINFRAME EAVE STRUT CONNECTION AT MAINFRAME PURLIN TO ENDWALL RAFTER AT RAKE EXTENSION ] a ioe ra 00-01-030A 02-02-2000 MSS ;f / __ sa�E NONE mom: ROOF DETAILS REVISIONS [1] 2 L/ C) O O C5 13] 3 3 2 1 3 3 SECTION LAP INDICATORS 4] ICI Ih Ifl c5] Ii 1—C 1 b bw V ___ IN ______ ___ I . 11. NV _______ 1—G 5 1—G 6 —G II 1—G 5 N uJ LL 9 'i ____________________ ____________________ __ 4X2X14AN 250 BASE SU RT PPO 25' 0 j, 25' 0 25' 0 ' 3' 0 100' 0 EXT. SIDEWALL AT A v, GIRT CONNECTION DETAIL PART LEFT RIGHT- FRAME UNE DESCRIPTION = SECTION LAP AT SUPPORTS MARK DESCRIP LENGTH LAP 5 SWO3 INDICATOR LAP LENGTH (FT & IN y a 4 1-CB4 CBL .313 32'10- 3/ 8 2 -4 SW04 1 1' 0 I 6 ao 1-G 5 8Z25 14 28' 0 33 2 2' 0 L j g 6 1-G 5 8Z25 14 28' 0 33 3 3' 0 � 6 1-G 6 8Z25 14 29' 0 33 21 LONGITUDINAL BRACING DETAIL DESIGNATIONS 8 1-G 7 8Z25 14 30' 0 21 33 a s CBLO1 O. 2 1-C 1 8C35 18 4 3- 1/ 2 b -CBLO1 O O O O O rJ I ( I I 1 2 3 3 SECTION LAP INDICATORS '— IlI I � I 1 b b 1—C1 • N __ • fl • NV 1L II M 1—G 5 —G 1—G6II 1—G5 LuLL' ,,G a CN ___ 4X2X14AN 0 BASE SUPPORT x 25' 0 25' 0 25' 0 25' 0 100' 0 3' p SIDEWALL AT B EXT. roe 00-01-030A GIRT CONNECTION DETAIL a FRAME UNE DESCRIPTION 02-02-2000 _ MSS sr 5 SW03 NONE 2 —4 SW04 im,e: S/W FRAMING o . Va REVISIONS [1] [3] [4] [5] LU U r Q LU or w o w DETAIL SW03 DETAIL SW04 DETAIL CBL01 1 S SCREW Q v+ CL 0 BASE ANGLE) ENDWALL ((( 0 EACH GIRT) _ COLUMN ] [FLUSH] [MACOLUMN INFRAME] ® EAVE STRUT) SW GIRT [MAINFRAME) CABLE GIRT --�*** (8)M.5x1.0 GRIP COLUMN OR 3x3x14AN Lt. RAFTER �O 3 J Lo Oi 0 0 0 i0 of EYE-BOLT o o; o (2) M.5x1.0 0 ;o o; o HILLSIDE ------ (TYPICAL) ---"-- ti r GIRT 3x3x14AN GIRT k LAP GIRT EW GIRT SIDEWALL [CORNER ANGLE] r [BYPASS] SIDEWALL m [BYPASS] ***NOTE:CUT 8-1/4" OFF I/S FLANGE OF GIRT. O r N GIRT CONNECTIONS AT EXPANDABLE ENDWALL GIRT CONNECTIONS AT MAINFRAME CABLE INSTALLATION DETAIL CORNER ANGLE DETAIL LIZ. a o� o1 [� � aN a ,, scZ,fqY _ JwN0: 00-01-030A acre: 02-02-2000 { BY: MSS I NONE ydS W DETAILS Mina REVISIONS RAKE ANGLE RAKE ANGLE 1.00/12 _ [1] r-- - — 2 [3] o [4] xd' N 04 .r a [sl - PART N z z K DESCRIP LENGTH .r O 1- 3 1-G 1-G 8 1-G 1 9 W 3 1-G 1 8225 16 811- 1 2 at U 3 / 1- 516 9' r + 3 1-G 3 8225 12 19' 3- 1/ 2 �------ 12 1- 8 82 12 19' - 1 1 2 3 4 1-C 9 8225 12 19' 7- BASE SUPP 4X2X104AANN 4' L 2 1-C 3 8CC35 16 7-11- 1L. 4. 2 W O 20' 0 20' 0 4. 20' 0 20' 0 20' 0 4 1-C4 8_3516 9' 7- 1 2 4. 4. U. 8 1-C 5 8C35 16 9' 3- 1 2 100' 0 _ 6 8C35 18 _ ENDWALL AT FRAME UNE 5 2 1-C 7 8C35 16 8' 9- 1 2 i ENDWALL COLUMNS I PART MARK LOCATION LENGTH DESCRIP1ION TOP OF COL BASE OF COL GIRT TO COL O O SWL - LEFT SIDEWALL U) N SWR - RIGHT SIDEWALL 1.00/12 DF1 DF2 F3 F4 DF5 F4 DF3 DF2 ---- DF1 W� 1-C2 1-C2 � .. Q 8 0 J N O 7 *OPEN SIDE OF 1-C 2 IS DOWN. ALL OTHER CEE GIRTS HAVE '� o 4 OPEN SIDE UP. t 1-G 2 N 1 1-G 1 Z i rj U U I !9 2 1 BASE SPORT X2X14ANN 9' 8 10' 4 10' 0 10' 0 10' 6 9' 6 10' 0 10' 0 10' 4 9' 8 -44 tt^DD ENDWALLIAT'FRAME UNE 1 d E! ENDWALL COLUMNS PART MARK LOCATION LENGTH DESCRIPTION TOP OF COL BASE OF COL GIRT TO COL 9-11/16 W LL i w '3.00/1Z RAKE ANGLE RAKE ANGLE J W DF6 DF7 DFB DF9 DF10 DF11 OF10 DF9 DF8 DF7 DF6 Q N 1—C3 1—C4 1—05 1—05 1—C6 1—C7 1—05 1—05 1—C4 1—C3 (/) o i N I IC, iIL o SEE DRAWING 40F OF 8 (� FOR DOOR FRAMING DETAILS. sae 00-01-030A L --------------------------------------------------- -� 02-02-2000 er: saw MSS NONE 9' 84. 10' 4 10' O 4. 10' 0 10' 6 9' 6 4. 10' 0 10' 0 10' 4 9' c2-2 0 8 r ® E FRAMING 100' 0 rux�een. ENDWALL AT OVERHANG 4I O REVISIONS [1] (2 [3] [4] [5] w v LU IL w DETAIL EW1 0 DETAIL EW1 1 p a - ETAI L EW25 ovc 1 ' 0 a N BASE PLATE-1ENDWALL GIRT [FLUSH] (2) 5/8"x12"AfB 2) H.5x1 .25 (2) M.5x1 .0 [FIELD LOCATE] CO 11 8 LUMN 0 o .. .i COLUMN O BRACKETENDWALL COLUMN • FLUSH (2) H.5x1 .25 _--- o [MILL] 0 0 [ ] V_ EDGE OF RAFTER (2) M.5x 1 .0 ' o1; w SLAB [EXPANDABLE] COLUMN ----'- [ANY TYPE] GIRT JJ w � LL.MILL INTERIOR COLUMN EXPANDABLE RAFTER / COLUMN CONNECTION ENDWALL GIRTS TO INTERIOR COLUMN Z 418 g r N X d r 00-01-030A : (J 1 (,IO2-02-2000 er. aou.E MSS !NONE £)C) E DETAILS 4D O REVISIONS [1] (2] [3] (4] [5] LLB V z DF12 Bpo9 (TYPICAL) L I DF12 RAFTER o o I < F5 I� CEE GIRT CEE GIRT W N RAFTER DF7 DF1-DF5 DF6-DF11 20' 0 (4)H.63x1 .5 (4)H.63x1 .5 A.F.F. (TYPICAL) rh 20' 0 (TYPICAL) ^ A.F.F. 19' 0 19' 0 X cm A.F.F. D F 13 A.F.F. IC DF14 (TYPICAL) -1 / IC2-1 ® �, N ZEE GIRT � L N U ii o � SECTION AT Ic1 - 1 / IC2 - 1 SECTION AT REMAINING FRAMES JOB NO: 00-01-030A DATE 02/15/2000 Br: 4CA E HEF I NONE DOOR FRAMING NLM --- 27' 45 8_ REVISIONS p- 3 16 MFB 4 19' MFB 4 19' D] MFB 3 MFB 3 F86 F87 F88 FB8 F87 FB B4 FB 5 6 FB 5 FB FB 2 F8 3 FB 4 FB 3 FB 2 � W t ® O o z i o m m I N t N W N 8 0' 8 0' 8 50' 0 50' 0 0 e►!t FRAME LINE 1 B 2 A JOINT INFORMATION a JOINT PARTMARK DEPTH THICKNESS BOLT QTY DESCRIPTION 1 MFC 4 1' 0 0.1875 4 AB.75X24 W W 2 MFC 4 3' 0 0.1875 8 H.88x2.5 2 MFB 1 3' 0 0.2500 W 3 MFB 1 1' 5 0.1875 8 H.63x2.0 to C'3 3 MFB 2 1' 5 0.1345 4 MFB 2 2' 5 0.1345 8 H.75x2.5 Q FLANGE BRACE TABLE Oi PARTMARK LENGTH PLACEMENT QTY FRAME QTY BLDG FB 1 3' 7- 3/16 NS/FS 4 20 FB 2 3' 8-13/16 NS/FS 4 20 FB 3 3' 4-13/16 NS/FS 4 20 00-01-030A FB 4 3' 1 NS/FS 4 20 01"E FB 5 2' 9- 5/ 8 NS/FS 4 20 � 02-O2000 FB 6 2' 9 NS/FS 4 20 II ii II jMSS NONE FB 7 2' 11- 7/ 8 NS/FS 4 20 CROSS SECTION FB 8 3' 3- 3/16 NS/FS 4 20 REVISIONS El] z 27 ' 4- 5 8 ' 4- 5 19' 0- 316 MFB4 27 MFB4 8 19' Q_ 3 i+] MFB 3 MFB 3 16 £51 45' 0 45' 16 0 LL! /16 U FB6 FB7 FB8 F88 FB7 W Q FB2 F83 FB4 F85 FB6 O --- __ ---- ® FB 5 FB 4 FB 3 FB 2 t� 1 0 o ® o 0 U, o tL co I N I V t7 st Li N I N = I N d N L._____--- N IN L CL B tL -- O' 8 O' 8 50' 0 50' 0 100' 0 FRAME LINE 2 . A BN JOINT INFORMATION 0 �, r JOINT PARTMARK DEPTH THICKNESS BOLT QTY DESCRIPTION Id. 1 MFC 2 1' 0 0.1875 4 AB.75X24 2 MFC 2 3' 0 0.1875 8 H.88x2.5 W g Lr- 2 MFB 1 3' 0 0.2500 W 3 MFB 1 1' 5 0.1875 8 H.63x2.0 O 3 MFB 2 1' 5 0.1345 z 4 MFB 2 2' 5 0.1345 8 H.75x2.5 LU W R FLANGE BRACE TABLE Q N PARTMARK LENGTH PLACEMENT QTY FRAME QTY BLDG o FB 1 3' 7- 3/16 NS/FS 4 20 N O. FB 2 3 8-13/16 NS/FS 4 20 FB 3 3' 4-13/16 NS/FS 4 20 FB 4 3' 1 NS/FS 4 20 roe NO FB 5 2' 9- 5/ 8 NS/FS 4 20 00-01-030A FB 6 2' 9 NS/FS 4 20 02-02-2000 FB 7 2' 11- 7/ 8 NS/FS 4 20 MSS 'NONE CROSS SECTION FB 8 3' 3- 3/16 NS/FS 4 20 REVISIONS s]3 16 27 MFB 2 27 MFB 2 8 19' MFB 1 MFB 16 (3] 45' 0 [4] 4' 15] g © 5'5' 0 /16 LU V FB 6 F87 FB 8 FB 8 FB 7 j Q 2 FB FB6 FB5 FB 3 FB - 4 FB Q I --- -- - 3 F84 F85 ® ® U, w Q a a z 00 It) �- 00 QC x I O W N i2 ® U.U. it) Lt) r.- O W (� >¢ Joi M I N R (� N .. Z 0' 8 0 8 (L 50' 0 50' 0 100' 0 FRAME LINE 3 - 4 x JOINT INFORMATION ®®®® JOINT PARTMARK DEPTH THICKNESS BOLT QTY DESCRIPTION t:} 1 MFC 2 1' 0 0.1875 4 AB.75X24 2 MFC 2 3' 0 0.1875 8 H.88x2.5 r ' 2 MFB 1 3' 0 0.2500 LL! LL 3 MFB 1 1' 5 0.1875 8 H.63x2.0 L� 3 MFB 2 1' 5 0.1345 � c 4 MFB 2 2' 5 0.1345 8 H.75x2.5 J LLl FLANGE BRACE TABLE PARTMARK LENGTH PLACEMENT QTY FRAME QTY BLDG y FB 1 3' 7- 3/16 NS/FS 4 20 FB 2 3' 8-13/16 NS/FS 4 20 FB 3 3' 4-13/16 NS/FS 4 20 FB 4 3' 1 NS/FS 4 20 FB 5 2' 9- 5/ 8 NS/FS 4 20 '10B NO: 00-01-030A FB 6 2' 9 NS/FS 4 20 0 02-02-2000 FB 7 2' 11- 7/ 8 NS/FS 4 20 MSS NONE FB 8 3' 3- 3/16 NS/FS 4 20 u: CROSS SECTION 8 REVISIONS 27' 4- 8 27' [2l 19'r31F8 2 4- 5 8 [2] MFB 1 [3] FB 219' o316 19' 0— 3 16 MFB 1 [4] 45' 0 45' p [5] �16 W U FB 6 FB 7 FB 8 FB 8 FB 7 FB 6 g 2 FB 3 FB 4 FB 5 FB F94 FB 3 FB r--- -- ® w O i ® L C °D o ® ® o to OZ jKJ L�] I IVL M M I0 > I L N N I N = O' j8 0' 8 0. 0 50' 0 50' p 100' 0 � ^ FRAME LINE 5 m GGGVVV JOINT INFORMATION a JOINT PARTMARK DEPTH THICKNESS BOLT QTY DESCRIPTION Q cr? 1 MFC 2 1' 0 0.1875 4 AB.75X24 �- 2 MFC 2 3' 0 0.1875 8 H.88x2.5 ` g 2 MFB 1 3' 0 0.2500 W 3 MFB 1 1' 5 0.1875 8 H.63x2.0 3 MFB 2 1' 5 0.1345 4 MFB 2 2' 5 0.1345 8 H.75x2.5 FLANGE BRACE TABLE PARTMARK LENGTH PLACEMENT QTY FRAME QTY BLDG Cj ' FB 1 3' 7- 3/16 FS 2 18 FB 2 3' 8-13/16 FS 2 18 p. FB 3 3' 4-13/16 FS 2 18 FB 4 3' 1 FS 2 18 FB 5 2' 9- 5/ 8 FS 2 18 '°°NO' 00-01-030A FB 6 2' 9 FS 2 18 0 02-02-2000 FB 7 2' 11- 7/ 8 FS 2 18 _ fl, ; I1MX; 9 / _ FS 8 3' 3- 3/16 FS 2 18 MSS NONE CROSS SECTION : REVISIONS [1] 2] [3] [4] [5] w V PANEL FASTENERS Q - N 1. PANEL ENDS: SPACING FOR PANEL TO PURLIN FASTENERS TO BE IN I A 4-8-4-8-4-8 IN. PATTERN LOCATED 2 IN. FROM O THE CENTER LINE ON BOTH SIDES OF EACH MAJOR RIB. FASTENER TO BE A NO. 12 SELF-DRILLING SCREW. Lei �• N 0 O 2. INTERIOR OF PANEL: .. � SPACING FOR PANEL TO PURLIN FASTENERS TO BE IN A 12-12-12 IN. PATTERN LOCATED 2 IN. FROM THE CENTER LINE OF EACH MAJOR RIB. FASTENER TO BE A NO. 12 SELF-DRILLING SCREW. 3. SIDE LAPS: SPACING FOR PANEL TO PANEL FASTENERS AT SIDE II LAPS TO BE 30 IN. ON CENTER. FASTENER TO BE C9N A NO. 14 SELF-DRILLING SCREW. NOTE: TAPE SEALER REQUIRED AT SIDE LAPS WHEN USED AS ROOF PANELS. O v- w CL o , = = = = = = = = = = = = = = = = = = = = = = = = = - 5q - ' 00-01-030A oae: i 02-02-2000 I i NO E BUILDING 'B' ROOF PANELS I I ,)o_ pp Vo I I i I REVISIONS [1] [2] [3] [4] [5] w V IJ- INSULATION 17- 3" X 8' X 123' ROLLS •• o N ...1 1- 3" X 4' X 123' ROLL " a4 I - -- 0 9" w --- --- ---- -- --- 00-01-030A BUILDING "B" 02-02-2000 i MSS s_ NONE ROOF INSULATION REVISIONS ;;, Cl] [2] [3] [4] [3] PANEL FASTENERS W SIDEWALL AT A 1. PANEL ENDS: V SPACING FOR PANEL TO PURUN FASTENERS TO BE IN 4" Q A 4-8-4-8-4-8 IN. PATTERN LOCATED 2 IN. FROM THE CENTER UNE ON BATH SIDES OF EACH MAJOR RIB. FASTENER TO BE A NO. 12 SELF-DRILLING SCREW. 2. INTERIOR OF PANEL W SPACING FOR PANEL TO PURUN FASTENERS TO BE IN A 12-12-12 IN. PATTERN LOCATED 2 IN. FROM THE CENTER LINE OF EACH MAJOR RIB. FASTENER TO BE A NO. 12 SELF-DRIWNG SCREW. � J�! 3. SIDE LAPS: LLLLLLLLLLLSPACING FOR PANEL TO PANEL FASTENERS AT SIDE � Fr LAPS TO BE 30 IN. ON CENTER. FASTENER TO BE '� A NO. 14 SELF-DRIWNG SCREW. NOTE: TAPE SEALER REQUIRED AT SIDE LAPS WHEN USED AS ROOF PANELS. o � iIYJ W L SIDEWALL AT B I----- Th1JJTTTffffffl1JTFTTTfTTEffTJJm ----- LLN I a BUILDING *W M ;r in m b m o i� 7` c n 70 1a '� N o OPEN FOR �( !LJ '! FUNNCAR DOOR BUILDING '8' I Oa v- ENDWALL AT 5 ^_--^-___J ENDWALL.AT 1 � W � LL W C J � •r n o � w n a •- * n o m .r n o_ - o n r -- o n .r � o n w o n t o � � � 't 't in Tn in in m o io i• i� i� m n T. i� m ;o To 10 Tq Tn Tn in w t w OPEN FOR OWNERS HANGAR DOOR ____ ,�� 00-01-030A 02-02-2000 ENDWALL AT OVERHANG / (J MSS arm NONE T WALL PANELS o REVISIONS [2] EAVE TRM N 2 HEAD [3] TRM [4] [5] C HEAD TRM r 'Q SIDEWALL AT A 0 Llf. W GUTTER < ® l O l HEAD'b' I TRM BASETRM I SIDEWALL AT 8 LLB O PEAKBOX r t RAKE TRM RAKE TRM !9 HEAD TRM HEAD TRM Tht F3 z a z 2 8 8 o I � � N rn z m o O 0 99 O 9 W L-__- BASE TRM HEAD TRM c ENDWALL AT 5 ENDWALL AT I HEAD TRM ------ C9 cc WWy W PEAKB0X RAKE TRM RAKE TRM O r Joe No 00-01-030A juo c44" 02-02-2000 MSS NONE TRIM LOCATION '( C� «urw ENDWALL AT OVERHANG C REVISIONS [17 L2 ROLL CAULK 7/8"LAP SCREW ROOF PANEL (24"ON CENTER) 131 RAKE TRIM GUTTER RAKE TRIM EAVE TRIM (41 RAKE TRIM [5] RAKE TRIM W 7/8°LAP SCREW (24"ON CENTER) �� E�XNER RAKE END WALL PANEL Lu O PEAK BOX z END ER X RAKE TRIM DETAIL PEAK BOX DETAIL GUTTER END DETAIL RAKE END DETAIL ROOF PANEL Q I/S CLOSURE 1� (IF UN-INSULATED) WALL PANEL SCREW ROOF PANEL 7/8"LAP SCR (24" ON CENTER) I/S CLOSURE 0/S CORNER TRIM (IF UN-INSULATED) GUTTER WALL PANEL 7/8"LAP SCREW •• (24 ON CENTER) EAVE TRIM n "X" BOTTOM OF I/S CLOSURE +-FLUSH WITH ANGLE GUTTER AND FOLD (IF UN-INSULATED) °•, ° TABS INTO D'SPOUT BASE TRIM DOWNSPOUT WALL PANEL WALL PANEL r WALL PANEL w• NOTE: INSTALL GUTTER STRAPS 3'0" ON CENTER. NOTE: INSTALL D'SPOUT STRAPS 5'0" ON CENTER. N GUTTER DETAIL BASE TRIM DETAIL 0/S CORNER DETAIL EAVE TRIM DETAIL , g HEAD TRIM ca C z J n W WALL PANEL 1"SD SCREW (12" ON CENTER) 1"SD SCREW (12" ON CENTER) WALL PANEL HEAD TRIM CV �. HEAD TRIM 1"SO SCREW WALL PANEL (24' ON CENTER) Jae NO: 00-01-030A 02-02-2000 MSS I ec NONE tmz: TRIM DETAILS HEAD TRIM DETAIL AT HEADER HEAD TRIM DETAIL AT SILL HEAD TRIM DETAIL AT JAMB "`