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1 W 1ST ST - SHADE STRUCTURE DRAWINGS 1/4 End Cap ; Z3 o � 3/4' Column Bracket Test Report No.3636033TX-01 Date:December 08,2014 L 2 Shackle Pin (/ CL Fbm Protoaaation of Twdks and Flims 1/2 Shackle _ --_ _ _ _ _ _ _ _ _ _ _ _ _ ------------------------------ _ NFPA 701 Test Method 2(Flit Specimens)-2010 Edition - 5/$' EY eNut W � z Blue Q speg(lrrien Dimensions Char Length AM Flame Flamina Residues ( INMd§:0UMM (seconds-nearest 3AIV V1 0:5 1 olurin `5.5 'Ilk 1 5x47 9.0 OA 0.0 W 2 5x47 10.0 0.0 0.0 �Ll 3 5x47 8.0 0.0 0.0 4 5x47 9.1 0.0 0.0 5/8x 12 3/16 5 5x47 9.4 0.0 0.0 Tension Nut /j ui 5x47 8.4 0.0 0.0 3,16 Threaded Drive Qt i 7 5x47 9•6 0.0 0.0 9 ` 8 5x47 10.1 0.0 0.0 9 507 8.8 0.0 0.0 10 5x47 8.4 0.0 0.0 3 FABRIC CORNER DETAIL orz�iratio�l:• Slight charring,shrinking. STANDARD 5/8" DRIVE ' gea��ements: A material tested in single sheets shall not continue flaming for more than 2 seconds after the test flame is 1/4' Sail Fa removed from contact with the specimen.The char length of any single fiat specimen shag not exceed 17.1 > inches.Portions or residues of material being tested that break or drip from the specimen shall not continue to flame for more than 2 seconds after reaching the floor of the test apparatus. Fabric Sall r M conclusion• Corner The submitted samplemeets the requirements of NFPA 701 Test Method 2 Flat mens -2010 - eq ( Specimens) r �$ L3 Edition,when tested in its original state. l` AQ Q -♦- COO Selected was as requested by applicant against specified requirement 1 test request form;quotation. *••End of Report,•« �-y 2' r•• 0 V- 0 Q Signed for and on behalf of r Cyr-, 0 P� SGS North America Inc. /J/j W OnE =:) 0 V Prashanthi Alapati Greg S.Kolbeck / V Supervisor Textile Laboratory Manager-Textile Laboratory �r This document is d by the Company"ad to its General Conditions of service printed overleaf,available on request or , accessible at :jC ard, for electronic format documents, subject to Terms grad \ / C:) Conditions for Electronic Documents at Attention is drawn to \\ J the limitation of liability,indemnification and jurisdiction muss defined therein.Any holder of this document is advised that information contained hereon reflects the Company's findings at the tirne of its intervention only and within the knits of Client's instructions,if any. The Company's sole responsibility is to its tient and this document does not exonerate parties to a transaction from exercising all 12 ! / their rights and obligations under the transaction documents.This document cannot be reproduced except in full,without prior written \ / approval of the Company.Arty unauthorized alteration.forgery or fslatkabon of the content or appearance of this document is \ / unlawful and offenders may be prosecuted to the West extent of the law.Unless otherwise stated the results shown in this test report r refer only to the sample(s)tested and such sample(s)are retained for a minimum of 45 days only, SGS I firth krwea,tic. Consumer TeWg Se+wces 291 FairW Avenue.FaidiAl.hod 07004 t(973)575.6252 1(973)575-7t75 W*WAg.eown - - - - - - - - - - ANenenn d ftSGs GMUP 5 2 � CIO: DESIGN CRITERIA C1 C1 0- FLORIDA BUILDING CODE 5TH EDITION, 2014 Q DEAD LOAD: [� Q FABRIC:0.50 PSF COLUMN LAYOUT - Calw ,J SNOW LOAD: N/AO.Of SEISMIC DESIGN:N/A PLAN VIEW I EW 0 LIVE LOAD: ROOF LIVE LOAD:5 PSF r„J WIND LOAD: LL, I-- W M RISK CATEGORY:I BASIC WIND SPEED WITH FABRIC: 105 MPH w BASIC WIND SPEED WITHOUT FABRIC: 155 MPH U. WIND EXPOSURE GUST EFFECT FACTOR:0.02 RY•C TRIANGLE SAIL SHADE 0 I_ W Q Vult.: 175 MPH 0 12.8" x 222" Vasd.: 121 MPH Q W WIND ENCLOSURE TYPE: OPEN ELEVATION:±7 FT. AMSL (ABOVE MEAN SEA LEVEL) COVER 1/4" Galvanized Steel F- _ FABRIC O i b F Within n arc OWNER NOTES HPDE KNITTED FABRIC TO HAVE Ca I _ W 1. MEMBRANE(S) MUST BE REMOVED IF LIVE LORD/ROOF SNOW LOAD IS EXPECTED TO SUPPORT PERIMETER CABLE INSI[ I Perimeter Hem EXCEED 5 PSF AND/OR THE BASIC WIND SPEED IS EXPECTED TO EXCEED 90 MPH 3 SEC n GUST OR 76 MPH SUSTAINED WIND LOADS ( HURRICANE CATEGORY 1). A 4 LAYER 2 WIDE HEM, ATTACHED I 2. THE OWNER ACCEPTS FULL RESPONSIBILITY OF REMOVING THE FABRIC FROM THE STEEL TO TENSION DRIVE ASSEMBLY ( I 1 FRAME WHEN ANY OR ALL OF THESE CONDITIONS MAY OCCUR. I I 3. THE STEEL STRUCTURE WITH THE FABRIC REMOVED, WAS DESIGNED TO WITHSTAND I DEAD LOADS,ROOF LIVE LOADS AND WIND SPEEDS AS SPECIFIED ABOVE PER THE ( I LOCAL CODE REQUIREMENTS. ( I 3 4. IF THE ABOVE LOADS ARE EXCEEDED OR ADDITIONAL LOADS ARE INDUCED I p W I •�� � W W � STRUCTURAL FAILURE MAY OCCUR.THE OWNER IS RESPONSIBLE FOR AND ACCEPTS I U > D" FULL LIABILITY FOR ANY ISSUES CAUSED BY EXCEEDING THE DESIGN CRITERIA LOADS. W GENERAL NOTES I I p 3 D 1. FABRIC MEETS NFPA 701-04. I ICL L = U V W 2. ALL EXPOSED STEEL TO BE POWDERCOATED. I I w = W FOUNDATION DESIGN Ll CONCRETE COMPRESSIVE STRENGTH AFTER 28 DAYS:3,000 PSI = � ooa STEEL REINFORCEMENT:ASTM-A615, GRADE 60 VERTICAL FOUNDATION PRESSURE:2,000 PSF Z LATERAL BEARING PRESSURE: 100 PSF/F "-' (W _ FOUNDATION NOTES C 1 010.8x 18O " � C 012.8" x 222" z W � ~ W � 5. THE FOUNDATION DESIGN IS BASED ON TABLE 1806.2 OF THE BUILDING CODE, CLASS 5 3 m O SOIL MATERIAL. IF DIFFERENT SOIL CONDITIONS ARE ENCOUNTERED,IT IS cr RECOMMENDED THAT A SITE SPECIFIC GEOTECHNICAL REPORT IS CONDUCTED TO cx� W ~ Z 4- DETERMINE THE LOAD BEARING VALUES OF THE SOIL. \ C) Z - z 6. THE VERTICAL AND LATERAL BEARING PRESSURE VALUES WERE CONSIDERED PER Z Fes- at O CONDITIONS OF 2014 FLORIDA BUILDING CODE.FOR DEEP FOOTINGS A GEOTECHNICAL INVESTIGATION REPORT PREPARED BY OTHERS IS MANDATORY TO �- W M W in CONFIRM THE PRESUMED SOIL BEARING VALUES.OWNERS ASSUME FULL LIABILITY FOR t I C1 �s10.8" x1 $0" � � ono � ANY STRUCTURAL DAMAGE, IF NO GEOTECHNICAL REPORT IS PROVIDED 5 FOOTING DETAIL I i O = a Z = W 7. IF THE FOOTING DEPTH DOES NOT MEET LOCAL FROST REQUIREMENTS, FOOTINGS NOTE: A HOLE IS PROVIDED AT L._...� Q 3 SHALL BE RE-DESIGNED UNDER THE DIRECTION OF AN ENGINEER. 1T IS THE CONTRACTOR'S RESPONSIBILITY TO VERIFY THE LOCAL FROST DEPTH. THE BASE OF EACH COLUMN FOR ONE #5 ROD, Revisions; MATERIALS Date: 8 ALL MATERIALS LISTED BELOW MAY NOT BE SPECIFIC TO THIS PROJECT. GRADE MEMBER TYPE ASTM MIN. YIELD STRENGTH W SHAPES A992 50 KSI 6' ( • i RECTANGULAR HSS TUBES A500(GRADE B) 46 KSI I 1 SQUARE HSS TUBES A500(GRADE B) 46 KSI ROUND HSS TUBES A500(GRADE B) 42 KSI 3' L'- SCHEDULE PIPE A53 (GRADE B) 35 KSI _ _. /_0# ROUND MECHANICAL TUBING A519 45 KSI 3 1 MISCELLANEOUS PLATES/SHAPES A36 36 KSI i I CONNECTION BOLTS A325 92 KSI co HEADED ANCHOR BOLTS F1554 36 KSI 2/-6# Drawn.-l_� K. MADDEN HOOKED ANCHOR BOLTS A307 36 KSI AS PER SELF TAP SCREWS SS410 150 KSI 1 Date: 12Z5/2016 TABLE #1 0NCn d: 1/4"GALVANIZED AIRCRAFT CABLE SHALL HAVE A NOMINAL STRENGTH OF 7,000 LBS. L_Jv v c0 l l k _1 Z M N 0) Date: SEE FOOTING DETAIL 5/1 ©``I�L M1 0 0 0 REINF. AS PER TAB E #1 W to %-" THIS SHEET FOR SIZE AND .. # 105816 T EW TOP & BOTTOM REINFORCEMENT CO NT 0 °Q a TABLE 1U u. STRUCTURE COLUMN COLUMN COLUMN FOOTING SIZE FOOTING " TY P STYLE ID HEIGHT SIZE REINFORCEMENT ""s 011'"iN°IS"""' A°F SMVM"'11D s"""PUM USED W C°a0 'LTM 01r T MtA1 trCON'ETIT of 11tE AM INF Jt. 20 e b�Y WAY M7110UT M IS TO CER11Flr 1FMT I WINE N£MEMED 7W PLAN AIS FOUND TO 03MANCE 12'-0" 3.5' x 3.5' (5) 15 EW AS PER �, cooE LATEST EDITION. HYPERBOLIC C1 Above Grade 010.8 Sch40 3«0' Deep Top & Bottom TABLE #1A - SAIL �� � I SHADE C2 15'-6" l 12.8" Sch40 4.0'� x 4.0' (6) #5 EW RCOM AM A. 7W Ei. S A P.E. NUM Above Grade 3.0 Dee To & Bottom �F Tl �N NOT V t P P INTH Tt1E srfssNc DOMMeS SEAL Sheet N O. 1/4 End Cap v 0 3/4 Column Bracket Test Report No.3636033TX-01 Date.December 08,2014 Shackle Pin a. Fila no Propagation of Textiles and Flims 1/2 Shackle _ _ _ _ _ _ _ _ _ _ _-_ _ _ _ _ _-- i------------------------------ NFPA 701 Test Method 2(Flat Specimens)-2010 Edition �$ 5/8' Eye Nut Q imen Dingy nslons Char Length Air Flame Flamina Residues \ (inches) llnd,"I tsecands-nearest (seconds-nearest 3/16` 507 s.o 9&o0.0 luMn ' 5.5 5x47 10.0 0.0 0.0 _ W 3 5x47 8.0 0.0 a.0 4 5x47 9.1 0.0 0.0 + ► 5 5x47 9.4 0.0 0.0 5/8 x 12 3/lb Tension Nut 3/16 Qu s 5x47 8.4 0.0 0.0 Threaded DrlVe � , Ck $ 7 5x47 9.6 0.0 0.0 8 5x47 10.1 0.0 0.0 9 5x478.8 0.0 0.0 10 5x47 8.4 0.0 0.0 - 3 FABRIC CORNER DETAIL } Qbsenadlons: \ Slight charring,shrinking. STANDARD 5/8" DRIVE Reauliremenfa: A material tested in single sheets shall not continue flaming for more than 2 seconds after the test flame is 1/4' Sall Fan removed from contact with the specimen.The char length of any single flat specimen shall not exceed 17.1 \ / Inches.Portions or residues of material being tested that break or drip from the specimen shall not continue to flame for more than 2 seconds after reaching the floor of the test apparatus. Fabric Sail a° candusion., Corner The submitted samplemeets the requirements of NFPA 701 Test Method 2 Flat ens -2010 eq ( Specimens) � 0 Edition,when tested in its original state. �,) �8��1. [� L_ Selected teas requested by applicant against specified requirement!test request tam i quotation. nds End of Report •`« Po O �. Signed for and on behalf of -' O SGS North America Inc. W In , i1 E 0 Q V Prashanthi Alapati Greg S.Kolbeck / -0 Supervisor-Textile Laboratory Manager-Textile Laboratory Q This document is issued by the Company subject to its General Conditions of Service printed overleaf,available on request or to accessible at httn:.geM.& .- tions.MA and, her electronic format documents, sutyect to Terms and r C:) Conditions for Electronic Documents at wn Attention is dram to the limitation of liability,indemnification and jurisdiction issues defined therein.Any holier of this document is advised that information contained hereon reflects the Company's findings at the time of its Intervert ion only and within the limbs of Client's instruction,ti any. The Company's sots responsibility is to its Client and this document does not exonerate parties to a transection from exercising all 12 f their rights and obligations under the transaction documents.This document cannot be reproduced except in full,without prior written approval of the Company.Any unauthorized alteration,forgery or falsification of the content or appearance of ibis document is unlawful and offenders may be prosecuted to the fullest extent of the law.Unless otherwise stated the results shown in this test report refer only to the sample(s)tasted and such sample(s)are retained for a mimlrrium of 45 days only. SGS Norlh ,na h+c. Consumer Tealinp Ser om 291 Fmf*Mt Awwe,F&UW,NJ 07M t(973)5754252 f(973)575-7175 www.sgn.otrn _ _ _ _ ------ _ _ _ _ S A1ens.r d VNe GS€'soup 25 _�_ _ ... _ _ _ � DESIGN CRITERIA C1 a- FLORIDA BUILDING CODE STH EDITION, 2014 C1 Q DEAD LOAD: FABRIC:0.50 PSF � 2 COLUMN LAYOUT Ck: SNOW LOAD:N/A W LJ_ SEISMIC DESIGN: N/A 1 PLAN VIEW OW Ck: _ LIVE LOAD. ROOF LIVE LOAD:5 PSF J :2 (P) ,,t WIND LOAD: to 1-` WM RISK CATEGORY:I M C-14 BASIC WIND SPEED WITH FABRIC: 105 MPH BASIC WIND SPEED WITHOUT FABRIC. 155 MPH WIND EXPOSURE CATEGORY:C W GUST EFFECT FACTOR:0.902 �� 1 TRIANGLE SAIL SHADE wLLJ Q Vult.: 175 MPH 012.8 X 222 >_ VClsd.: 121 MPH V) WIND ENCLOSURE TYPE:OPEN " ELEVATION:±7 FT.AMSL (ABOVE MEAN SEA LEVEL) FABRIC COVER 1/4Galvanized Steel F- W= OWNER NOTES _ HPDE KNITTED FABRIC TO' Cable Within Fabric - - - -- Q 1. MEMBRANE(S) MUST BE REMOVED IF LIVE LOAD/ROOF SNOW LOAD IS EXPECTED TO SUPPORT PERIMETER CABLE INSIDE Perimeter Hem m EXCEED 5 PSF AND/OR THE BASIC WIND SPEED IS EXPECTED TO EXCEED 90 MPH 3 SEC A 4 LAYER 2" WIDE HEM, ATTACHED I GUST OR 76 MPH SUSTAINED WIND LOADS ( HURRICANE CATEGORY 1). 2. THE OWNER ACCEPTS FULL RESPONSIBILITY OF REMOVING THE FABRIC FROM THE STEEL TO TENSION DRIVE ASSEMBLY I I FRAME WHEN ANY OR ALL OF THESE CONDITIONS MAY OCCUR. I I 3. THE STEEL STRUCTURE WITH THE FABRIC REMOVED, WAS DESIGNED TO WITHSTAND I l DEAD LOADS, ROOF LIVE LOADS AND WIND SPEEDS AS SPECIFIED ABOVE PER THE l LOCAL CODE REQUIREMENTS. I I 3 Z 4. IF THE ABOVE LOADS ARE EXCEEDED OR ADDITIONAL LOADS ARE INDUCED l I W w STRUCTURAL FAILURE MAY OCCUR.THE OWNER IS RESPONSIBLE FOR AND ACCEPTSI U FULL LIABILITY FOR ANY ISSUES CAUSED BY EXCEEDING THE DESIGN CRITERIA LOADS. l E'= 0 '� > :01 W GENERAL NOTESl D Q D 1. FABRIC MEETS NFPA 701-04, l I J W IY W F- 0EC282016 X � WxQ 2. ALL EXPOSED STEEL TO BE POWDERCOATED. l I W = FOUNDATION DESIGN CONCRETE COMPRESSIVE STRENGTH AFTER 28 DAYS:3,000Z:= Q 0 p Q STEEL REINFORCEMENT:ASTM-A615,GRADE 60 VERTICAL FOUNDATION PRESSURE:2,000 PSF Z LATERAL BEARING PRESSURE: 100 PSF/F "- V) _ FOUNDATION NOTES C 1 010.8 x 180 Li C 012.8" x 222" Z W F- �-- 5. THE FOUNDATION DESIGN IS BASED ON TABLE 1806.2 OF THE BUILDING CODE, CLASS 5 SOIL MATERIAL. IF DIFFERENT SOIL CONDITIONS ARE ENCOUNTERED, IT IS �f S Q ~ a" M RECOMMENDED THAT A SITE SPECIFIC GEOTECHNICAL REPORT IS CONDUCTED TO p rn t ,• 0 LA_ b Z �- C, fit! M OFFICE COPY O - DETERMINE THE LOAD BEARING VALUES OF THE SOIL. .� � 1'tt �'- \ Z Z 6. THE VERTICAL AND LATERAL BEARING PRESSURE VALUES WERE CONSIDERED PER m 0 D Z }� 0 Q CONDITIONS OF 2014 FLORIDA BUILDING CODE. FOR DEEP FOOTINGS A � *" t- /O GEOTECHNICAL INVESTIGATION REPORT PREPARED BY OTHERS IS MANDATORY TO E0-. V) W M FULL LIABILITY FOR yi » N 0 V I E: >- 0 _j M CONFIRM THE PRESUMED SOIL BEARING VALUES.OWNERS ASSUME UL L ANY STRUCTURAL DAMAGE, IF NO GEOTECHNICAL REPORT IS PROVIDED t I C 1 01 0.8 X 1 80 o RJacksonville Fire Prevention v a- u' O o = ix 7. IF THE FOOTING DEPTH DOES NOT MEET LOCAL FROST REQUIREMENTS, FOOTINGS FOOTING DET'A`IL ( I v M Z C? 0 = tr Z W SHALL BE RE-DESIGNED UNDER THE DIRECTION Of AN ENGINEER. IT 1S THE NOTE: A HOLE IS PROVIDED AT L_..J rn �' '- °- `� � °- n t) DEC 2 8 2016 CONTRACTORS RESPONSIBILITY TO VERIFY THE LOCAL FROST DEPTH. THE BASE OF EACH COLUMN Revisions: MATERIALS FOR ONE #5 ROD, f O ; b 13NO EXCEPTIONS ALL MATERIALS LISTED BELOW MAY NOT BE SPECIFIC TO THIS PROJECT. GRADE Z = r_ E3 EXCEPTIONS AS NOTE© Dote: By: � � SHEET## cn1 � MEMBER TYPE ASTM MIN.YIELD STRENGTH 6 W SHAPES A992 50 KSI c1 RECTANGULAR HSS TUBES A500(GRADE B) 46 KSI I I v SQUARE HSS TUBES A500(GRADE B) 46 KSI I ROUND HSS TUBES A500(GRADE B) 42 KSI 3# �-J SCHEDULE PIPE A53 (GRADE B) 35 KSI err ROUND MECHANICAL TUBING A519 45 KSI 3 MISCELLANEOUS PLATES/SHAPES A36 36 KSI ( I CONNECTION BOLTS A325 92 KSI HEADED ANCHOR BOLTS F1554 36 KSII 2/-6# L J _ � Drawn: K. MADDEN HOOKED ANCHOR BOLTS A307 36 KSI AS PER SELF TAP SCREWS SS410 150 KSI I I ,Q Date: 12Z5/2016 TABLE #1 I . �' �N 1/4"`GALVANIZED AIRCRAFT CABLE SHALL HAVE A NOMINAL STRENGTH OF 7,000 LBS. Lr_J J ca� � N Chkd: Z n N Date: SEE FOOTING DETAIL 5/1 0 C4 CO ° ° ° ° REiNF. AS PER TABLE #1 THIS SHEET FOR SIZE AND W a .• # 105816 Q TABLE 1 T EW TOP & BOTTOM REINFORCEMENT COUNT V) a U_ STRUCTURE COLUMN COLUMN COLUMN FOOTING SIZE FOOTING 3 TY P STYLE ID HEIGHT SIZE REINFORCEMENT w"oRAtirlNt: """"`�""`"e "T Of tl AND S'""' "'""7*4 MY WAY HE QTY OF 1Wt T OF THE a20116 NOT P UBUSHED 7FMs °° IS 70 CERTIFY THAT t HAVE ih WEND 7HR4 PLAN AND i 70 K IN COMPUANCts 2'-0" 3.5' x 3.5' is} 5 EW AS PER �FIORgA CODE LATEST IM HYPERBOLIC G� Above Grade 0 10.8 Sch40 3.0' Deep Top & Bottom TABLE #1 4 SAIL RAM A. GOEL. Ph.D., P.E. 4743 SHADE '- " 4.0 x 4.0 C2 �5 s ��2.8„ sen4o (s) #5 EW EMBOWD NTH� �UMESS s SEAL Above Grade 3.0 Deep Top & Bottom Sheet No.el 4ag w r • ;'. IVR -' J ttt eFrrs[ ! r • - F 44, -.:. .k \.Y b:{ i ; 47 .T ft x r. e1r i t Worm .; F'• s f Y r.r4 f .� • R ! �s4az>,-iu &S"vni ^ • of 1 x tr r f•[' � � X `�� x 0 v%eNx- ; !!s»RISrlT,r �: � i:;� (3 �itrrN•e.. 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