Laserfiche WebLink
vx L mwtwm,P�E- <br /> STRUCTALL BUILDING SYSTEMS DESIGN NOTES: MAXIMUM ALLOWAB No 'E�04 oft <br /> EPS FOAM COREROOF PANELS - METAL SKIN POSITIVE AND NEGATIVE DESIGN PRESSURES DESIGN PRESSURES:== <br /> CALCULATED FOR USE WITH THIS SYSTEM .. :: <br /> HAVE BEEN CALCULATED IN ACCORDANCE In- <br /> WITH ASCE 7-10 AND THE FLORIDA BUILDING AS NOTED IN CLEAR 6'AZ --41, <br /> CODE USING ALLOWABLE STREW DESIGN SPAN TABLES :% —.01 <br /> METHODOLOGY WITH THE CRITERIA. <br /> OUTLINED HEREIN. <br /> TOP&BOTTOM FACING: ENCLOSED STRUCTURELOADS: it I <br /> 0 024'ALUM/0,024-ALUM <br /> 0:030*ALUM/ 0.03D'ALUM 1. CALCULATIONS <br /> BASED ON ASCE 7-10,Vult-130 MPH-180 MPH, <br /> 26 ENCLOSED STRUCTURE COMPONENTS&CLADDING,RISK CATEGORY-11, Kd­O.BS,Kzt-1.0,.Kz-TABLE <br /> ga STEEL I 26ga STEEL 30.3-1, GCP1-+/-0.I8,15'MMEAN ROOF HEIGHT. R co <br /> ­36"MAX OVERHANG SCREENED ENCLOSURE LOADS: <br /> (SEj Al CLEAR AT FRONT,25%OF 2. WIND LOADS ARE TAKEN AS'THE MAXIMUM BETWEEN ASCEENCLOSED STRUCTURE COMPONENTS <br /> S0�0_�,Z'Pft LAST PANEL WIDTH DESCRIBED ABOVE)AND THE GOVERNING LOADS AS ILLUSTRATED IN FBC TABLE 2002A fn ALONG SIDES,TYP. CLADDING(AS <br /> FOR VERTICAL LOADS ON SOLID ROOFS,UP TO 15'MFAN ROOF HEIGHT,Vult-110 MPH-180 MPH: ow fil <br /> OVERHANG*- OPEN STRUCTURE LOADS: <br /> 3. CALCULATIONS BASED ASCE 7-10,ROOF OVER OPEN STRUCTURE COMPONENTS lk CLADDING, <br /> OBSTRUCTED WIND FLOW,RISK C4TEGORY=11,Kd-0,85,KA-1,0,V-0,85,15'MEAN ROOF HEIGHT], <br /> Vult-130 MPH-180 MPH. <br /> 'LOA LIJ <br /> 0 COMBINATIONS UTILIZED IN THIS MASTER PLAN SHEET HAVE BEEN[HiPLIVED FROM THE <br /> ALLOWABLE STRESS DESIGN LOAD COMBINATIONS 11"STRATED IN ASCE 7-10 <br /> 4' ALL WIND SPEEDS LISTED HERE ARE Wit WIND SPEEDS.Yaw WIND SPEEDS MAY BE CALCULATED WITH <br /> THE FOLLOWING CONVERSION;Vult-VaW x 1/0.6 >_ -9 <br /> PE ...CALCULATIONS CONSIDER 9.46-ROOF-SLOPE.ROOF LIVE LOADS USED IN CALCULATIONS CONSIDER W Z <br /> G <br /> INC; NG. OPTIONAL 20 PEP AS DEFINED IN FBC SECTION 1607. �R- <br /> CONNECTION ATOO�J GENERAL NOTES: <br /> UTTER OR <br /> MOST STRUCTURE I DRIP PAP 1. THIS SPECIFICATION HAS BEEN DESIGNED AND SHALL BE FABRICATED IN ACCORDANCE WITH THE. <br /> PER SEPARATE PANEL REQUIREMENTS OF THE FLORIDA BUILDING CODE SIXTH EDMOW17)FOR USE WITHIN AND OUTSIDE RE W Z.COMPOSITE ROOF.PANEIS SHALL COMPLY WITH CHAPTER 7 SECTION 720,CHAPTER.8 SECTION <br /> ENGINEERING OEM THE R be 4 <br /> 803, S5A LFINISH, AND CHAPTER 26 SECTION 2604 OF THE FBC,. to 1 -2. COLD4.010HAP L INVBSTIGATE,ANO CONFORM To ALL I.OM BUILDING CODE AMENDMENTS <br /> CONNECTION AND I WHICH MAY APPLY. DESIGN CRITERIA BEYOND AS STATED HEREIN MAY REQUIRE ADDITIONAL <br /> MOST STRUCTUREIII I, ISPECIFIC SEALED ENGINEERING, <br /> 3 N 33-1/3% CREASE IN ALLOWABLE STRESS HAS BEEN USED IN THE DESIGN OF THIS SYSTEM.1 . I � <br /> PER SEPARATE 4: 0 IN <br /> DESIGN PRESSURES AS NOTED HEREIN ARE WED ON A MAXIMUM TESTED PRESSURE DIVIDED BY A <br /> ENGINEERING I i 2.0 FACTOR OF SAFETY. <br /> 5, THE A NGINUR OF RECORD FOR THE PROJECT SUPERSTRUCTURE WITH.WHICH THIS <br /> DESIGN IS 0970 BE RESPONSIBLE FOR THE INTEGRITY OF ALL SUPPORTING SURFACES TO THIS <br /> in DESIGN WHICH qHALL�,E COORDINATED BY THE PERMITTING CONTRACTOR. <br /> 6. SEPARATE Srrfi�PECIFIV'SEALED ENGINEERING SHALL 09 REQUIRED IN ORDER TO DEVIATE FROM <br /> LOADS OR SPANS CONTAINED HEREIN, LINEAR INTERPOLATION OFT EA <br /> ��SUPPORTING MUCTURE PER T) H LLOWASUESPAN <br /> ABLE LISTED HEREIN SHALL HOT BE PERMITTED.CONTACT THIS ENGINEER FOR ALTERNATE SPAN <br /> SEPARATE ENGINEERING CALCULATIONS AS MAY <br /> BE REWILREDIS GENERIC AND DOES NOT PROVIDE INFORMATION FORA C M <br /> 7. THE SYSTEM DETAILED HEREIN SpEcin <br /> SITE, FOR SITE CONDITIONS DIFFERENTFROM THE CONDITIONS DETAILED HEREIN,A LICENSED <br /> ENGINEER OR REGISTERED ARCHITECT SHALL PREPARE SITE SPECIFIC DOCUMENTS FOR USBIN <br /> CLEAR SPAN ISOMETRIC CONJUNCTION WITH THIS DOCUMENT. <br /> N.T.S, ISOMETRIC B. EPS PANEL PERFORMANCE CHARACTERISTICS FOR SELF IGNITION FLAME SPREAD AND SMOKE <br /> DENSITY HAVE BEEN FOWALIFIED THROUGH APPLICABLEASTM TEST STANDARDS,SEE EVALUATION REPORT I <br /> FOR MORE INRMATI N. <br /> 9. THE CONTRACTOR SHALL CAREFULLY CONSIDER POSSIBLE IMPOSING LOADS ON ROOF INCLUDING <br /> rT BUT NOT LIMITED TO ANY CONCENTRATED.LOADS WHICH MAY'LlITIPY GREATER DESIGN <br /> SHALL BE ROOF LOAD CRITERIA SHAE PROPERLY ANALYZED. A LICENSED ENGINEER OR <br /> REGISTERED ARCHITECT <br /> SEAL ALL JOINTS 10. EPS CORE COMPOSITE PANELS SHALL BE CONSTRUCTED USING TYPE 3105-H254 ALUMINUM FACINGS <br /> OR ASTM AM,CS TYPE B HOT DIP GALVANIZED 690 COATED STEEL FACINGS.EXPANDED POLYSTYRENE <br /> zr <br /> 1 <br /> WITH CONTINUOUS 0,024-ALUMINUM, FOAM SHALL HAVE TCkL DENSITY OF 1.0 PCF.THE EPS FOAM SHALL BE ADHERED TO THE ALUMINUM <br /> TS <br /> R 26GA STEEL <br /> CAULICU10 0.030'ALUMINUM FACING WITH MORAO M640 SERIES ADHESIVE(BY ROHN AND HAAS COMPANY),FABRICATION SHALL <br /> ILS DENSITY EPS <br /> ACCORDANCE WITH APPROVED FABRICATION METHODS BY MANUFACTURER <br /> TURER FOR ALL PANELS. <br /> /fO 11. THE CONTRACTOR 15 RESPONSIBLE TO INSULATE A MEMBERS FROM DISSIMILAR MATERIALS To .4 <br /> CORE FOAF� .QNS PREVENT ELECTROLYSIS. <br /> 12, ENGINEER SEAL AFFIXED HERE To vAuCATus srRUCTURALbESIGN AS SHOWN ONLY.USE OPTHIs <br /> SPECIFICATION BY CONTRACTOR at.al.INDEMNIFIES&SAVES HARMLESS THIS ENGINEER FOR ALL COST F <br /> _T SOAMAGES INCLUDING LEGAL F ES&APPELLATE FEES RESULTING FROM MATERIAL FABRICATION <br /> SYSTEM ERECTION,&CONSTRUCTION PRACTICES BEYOND TMATWHICR 15 CALLED FOR BY E65�STATE, <br /> FEDERAL CODES&FROM DEVIATIONS OF THIS PLAN.13 EXCEPT AS EXPRESSLY PROVIDED HEREIN,No ADDITIONAL CERTIFICATIONS OR AFFI RMATIO NS ARE <br /> INTENDED. <br /> 14. ALTERATIONS,ADDITIONS,OR OTHER MARKINGS TO THIS DOCUMENT ARE NOT PERMITTED AN. <br /> INVALIDATE THIS CERTIFICATION. 15^2409a <br /> CROSS BECKON A'I <br /> TYPICAL K TABLE VALUE DERIVATIONS: SCALE8 <br /> Pon aptamly1mi <br /> E <br /> PANELINTERLOCK 1.6MkP'pgolp 5060275,506027C, <br /> DETAIL L AECSMTC%RALPROPERTLES DERIVED CERTIFIED TEST REPORTS NmYT- <br /> S060270,509014A.5090148 BY TERRAPIN TESTING,ESP0I23SIP-1,ESP0123SIP-2,ESP01235IP-3, for <br /> ESPOI23SIP-3A,ESP01235IP4,ESP0I235IP-5,ESP012351P-6,EXP0123SIP-6A,ESP0123SIP-7, <br /> ESPOI23SIP-6,ESP0I2.351P-9,ESP017.351P-9A BY ELEMENT MATERIALS TECHNOLOGY. - <br /> N.T.S. DETAIL 2. PANEL DEAD LOADS HAVE BEEN FACTORED INTO CALCULATIONS FOP.LIVE LOADS OR UPLIFT AS WELL <br /> AS CALCULATIONS FOR PANEL PROPERTIES, <br />