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HomeMy WebLinkAboutFL30797_R0_AE_RT1206.01_13 9/15/20American Test Lab of South Florida 6801 Nlq 17 Ave Ft Lauderdale, cL 33309 ©fflca 954-972-6208 fax 954-972-628k5 :"Op" atisf-r-09I cis il:lnfr�nla#Icf rnm Client: Crown Building Products of Florida, LLC Report Date. 12/6/13 6018 S.W. Highway 72 ATLSF Report 4: RT 1206.01-13 Arcadia, Florida 34266 Att. Mr. Juan Prestamo Re: Calculations for Aerodynamic Multiplier per FBC, Section 1518.8.4.5 Calculations for Weight and Restoring Moment Due to Gravity per TAS 101-95 Sections 10.2 & 10.2, TAS 102-95 & 102A-95 Sections 9.1 & 9?. Service Authorized by: Juan Prestamo Manufacturer: Crown Building Prc Model: Sanibel, Concrete R Imprint: ACT Nominal Dimensions (in.), 17.0 x 13.25 x NIP 0 x w x h), provided by supplier: Nominal Thickness (in.), 0.56 rovided by Supplier: Nominal Weight (lbf): 11.33 as provided by su her: Classification: Type I a- High Profit Purpose: New Product Appro` Comments: Attachment Resistan obtained from Tile R ducts of Florida, LLC oof Tile e, Interlocking, Class III al :e Expressed as a Moment Data to be aof Institute data on file. ATLSF Acereditations & Miami -Dade: 13-0228.09 Certifications: A2LA: 2650.01 testing FBC Organization #: TST3782 Page-1 of 2 Client: Crown Building Products of Florida, LLC Report #:RT1206.01-13 Roof Tile: Sanibel, concrete roof the Calculations: 1. Weight (W): W= m x 1 lbf s2/ft x 32.2 ft/s2 32.1741bm. W = 11.33 x 1.0008 W = 11.339 lbf 2. Restoring Moment Due to Gravity (Mg): M�— W x cos (0 — a) x L9 Ms = 11.339 cos [(9.462° — 4.016] x 0.802 Mg = 9.05 ft-lbf Pitch Equation Restoring Moment Due to 2:12 Ms = 11.339 x cos [( 9.462 — 4.016] x 0.802 M = 9.05 3:12 Mg = 11.339 x cos [( 14.036 — 4.016] x 0.802 M = 8.96 4:12 Mg = 11.339 x cos [( 18.435 — 4.0161 x 0.802 M. = 8.81 5:12 Ms = 11.339 x cos [( 22.620 — 4.016] x 0.802 M. = 8.62 6:12 Mg = 11.339 x cos [( 26.565 — 4.016] x 0.802 M = 8.40 7:12 Mg = 11.339 x cos [( 30.256 — 4.016] x 0.802 M = 8.16 3_ Aerodynamic Multiplier (X): Direct Deck Application X=0.156xbx12 k=0.156x 1.000x 1A172 k=.313 4. Aerodynamic Multiplier (),): Batten Application X=0.144xbx12 )� = 0.144 x 1.000 x 1.4172 X _ .289 The calculations provided in report ATLSF #: RTI206.01-13 has been performed in full accordance with the requirements of Miami -Dade County, with no deviations. Disclaimer: This test report was prepared by American Test Lab of South Florida, (ATLSF), for the exclusive use of the above named client and does not constitute certification of this product. The results relate to the particular specimens tested and does not imply that the quality of similar or identical products manufactured or installed from specifications or shop drawings identical to the product tested. ATLSF is an independent testing laboratory and assumes that all information provided by the client is accurate and does not guarantee or warrant any product tested or installed. American Test Lab of South Florida, its employees, and witnessing engineers do not own, operate, or are controlled by any manufacturer and have no financial interest in the manufacture, manufacture of any related parts, specification, or installation of this or a competing product. %OttllIfrfrr�� End of report. �Q E�..W A,4T" //. t � rr Prep d by I �<'� .�`GEHs"t-' F� Reviewed by:Z7 Co f 0,54395 Tony Force lo, RRO re = Stephen W. Warter, P.E. Chief Executive Officer I Reg. State of Florida # 54395 American Test Lab of South Firs-. j P �American Test Lab of South Florida O. OR1 � `��/' IONA�-�����