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STRUCTURAL ANALYSIS
May 23, 2017 0 �S ear DEC 19 2011 L a x Dennis Demarco MasTec Network Solutions, LLC E N G IN E E R ING .G R O UP 6100 Broken Sound Parkway, Suite 6By' """""""""""' Boca Raton, FL 33487 SCANNED BY Subject: Structural Analysis - Antenna Mounts [3C] St. Lucie County Carrier Designation: AT&17-01 .37 [FA# 10070076] OPY APX Project: 17-0107.37LE C Site Information: 3301 Orange Avenue Fort Pierce, Saint Lucie County, FL 34947 Latitude 27.4461800 N, Longitude 80.3595720 W Existing Antenna Mounts (Worst -Case) Dear Mr. Demarco: APX Engineering Group, LLC (APX) is pleased to submit this Structural Analysis to determine if the subject existing antenna mounts are able to support certain worst -case proposed loads. It is our understanding that AT&T, who has retained the services of MasTec Network Solutions, LLC (MNS), desires to install new telecommunication equipment on the subject mounts. This analysis was based on the supporting information listed in Table 2. Our services were performed in accordance with the terms and conditions of the master service agreement between APX and MNS. This report summarizes the results of our findings. The purpose of this analysis is to determine the suitability of the aforementioned structures to support the loading indicated in the attached calculations. This analysis has been performed in accordance with the Florida Building Code based upon an ultimate 3-second gust wind speed of 158 mph using RISA-3D structural software. Based on our analysis, subject to the assumptions and recommendations noted, it is our opinion that the subject structures will support the proposed loading. Existing Members: Pass at 88.3%, Existing Connections: Pass at 61.4% This report has been prepared for the purpose of -providing a structural evaluation of the subject structures for the loading conditions indicated. It is intended for the exclusive use of AT&T and MNS. The information, assumptions, and recommendations contained in this report should not be used by others for any purpose without express written authorization from APX. We appreciate the opportunity to provide our professional services to you and look forward to continuing our relationship. If we can be of any further assistance, please do not hesitate to contact us.-asaaea9Fa; ,• Sincerely, APX Engineering Group, LLC Gertha Wesh Michael A. Phillips, P.E. Junior Project Engineer Chief Engineer Florida License #68312 //-,Fill 0 AT&T: AABN [FA# 100234931 Structural Analysis Report Table 1: Analysis Criteria Criterion Building Code Description Florida Building Code, 50h Edition (2014) Standard - Loads TIA-222-G, Structural Standard for Antenna Supporting Structures and Antennas FBC 3108.1 Standard - Steel AISC LRFD 14th Edition Risk Category II Ultimate Wind Speed 158 mph, 3-Second Gust (FBC Figure 1609A) Nominal Wind Speed 122 mph, 3-Second Gust (FBC 1609.3.1 for use with TIA-222-G) Exposure Category C Structure Class II (1 = 1.0) Radial Ice Thickness No Ice Topo. Category 1 Crest Height Zero Feet Analysis Assumptions and Limitations 1. Information in the supporting documentation that could not be verified by APX personnel is assumed to be correct. 2. All components are assumed to be in adequate condition to carry their full design capacity. 3. The configuration of equipmentlappurtenances is assumed to be as specified in this report. 4. Emergency/essential communication equipment will not be supported by this assembly. If any of the above assumptions are not valid or have been made in error, these calculations may be affected, and APX should be allowed to review any new information to determine its effect on the structural integrity of the subject structure. Recommendations 1. Relocate the stiff -arm brace connection point at the mount to within one foot of the top mount face elevation. 2. Check all bolts for proper tightening in accordance with AISC "Snug -Tight" method prior to installation of proper equipment. 3. Replace any rusted/corroded hardware with new galvanized hardware. APX Engineering Group, LLC Wind Load -Appurtenance In Accordance Kith The TIA-222-G Standard APX Engineering Group, LLC 3400 Lakeside Drive, #525, Miramar, FL 33027 AT&T FP12 [FA# 100700761 17-0107.37 M. Phillips, May 2017 i zt t . Design Parameters Wind Speed, Vasa = 122 mph (TIA 2.6.1 and Annex 8) Exposure = C (TIA 2.6.5) Structure Class = I I (TIA Table 2-1) (TIA 2.6.6.2) Topo CategoryItN/O H =ft (Crest Height Above Surrounding Terrain)Structure Type = Mast =ft (Height of structure) Wind Load Appurtenance Type z H W D (ft) (ft) (ft) (ft) Page 1 of 1 1 = 1.0 (TIA Table 2-3) K:, nm = 0.85 (TIA Table 2-4) Gh = 0.85 (TIA 2.6.7) Ka = 1.0 (TIA Table 2-4) f = N/A (TIA Table 2-5) zg = 900 (TIA Table 2-4) Kt = N/A (TiA Table 2-5) e = 2.72 (Nat. Log Base) a = 9.5 (TIA Table 2-4) Kh = N/A (TIA 2.6.6.4) Ka = e<iow (nA 2.6.9.2) Ca = a<iw (Force Coefficient, TIA Table 2-8) Skew 1, 61 = 0° (TIA Figure 2-4) qi = 0.00256KiKvKdV21 (Velocity Pressure, TIA 2.6s. s) Skew 2, 62 = 10 (TIA Figure 2-4) F = q:Gh(EPA)A (nA 2.6..9.2) Round Ka K� K:t Kd q: Ca Ca Fr,°at Fslde Skew of 61 Skew of 02 Wt. ? (pst) Front Side (Ibs) (Ibs) FFront Fside FFront Fside (Ibs) Andrew SBNHH-1 D85B Panel 150 6.08 0.99 0.59 N 0.8 1.38 1.0 0.85 44.6 1.36 1.51 249 164 249 164 249 164 42.1 Ericsson RRUS-32 (Side) Radio 150 2.27 0.68 1.01 N 0.8 1.38 1.0 0.85 44.6 1.26 1.20 50.6 83.2 51 83 51 83.2 50.6 Ericsson RRUS-12 (Side) Radio 150 1.52 0.67 1.48 N 0.8 0.8 1.38 1.0 0.85 44.6 1.20 1.20 36.8 81.9 37 82 37 81.9 60.0 54.0 20.0 Ericsson RRUS-11 (Side) Radio 150 1.42 0.77 1.48 N 1.38 1.0 0.85 44.6 1.20 1.20 39.5 76.5 40 76 40 76.5 Raycap DC6-08-60-18-SF squid OVP 150 2 0.92 0.92 Y 0.8 1.38 1.0 0.95 49.9 0.70 0.70 43.5 43.5 44 44 44 43.5 Mount Type z (ft) (EPA)N (ft) (EPA)T (ft) (EPA)A (ft) Kz Kit Kd qz (psf) Ka Frr°°t (Ibs) Fside (Ibs) - - FF,°at (pli) Fside (PM - 14' V-Frame (round) Frame 150 16.44 14 1.38 1.0 0.85 44.6 0.8 499 425 17.8 21.2 Dish Type z (ft) D (ft) A (ft) CA Cs Cm Kz Kz Kd qz (pst) FAm (Ibs) Fsm (Ibs) Mm (Ib-ft) Wt. (Ibs) Definitions: Panel = Panel or Directional Antenna, Omni = Omni -Directional Antenna, Dish = Microwave Dish Antenna, Radio = Remote Radio Unit (RRU), TMA = Tower Mounted Amplifier Step 1: Select frame PIN from table below. Standard mount with (1) tie back. Sector mounts are hot -dip galvanized and include all required hardware to attach mount to tower. Step 1. Select frame PIN based on tower face spread. Frame Support Assembly ; `iStrai NtLe t ' Pah No. Face Spread ) KY2016A 8'Max. KY1993A 8'Min. - 14'Max. FrameSuppor, ssembly'� . -7a ererhle'�` Part No. Face Spread KY2006A 8'Max. KY2015A 8'Min. - 14'Max. SECTOR MOUNT [FOLLOW STEPS 1-3 TO ORDER] \Step 3: Select leg / 1 \ mounting kit from table below. — Face Spread (See Step 1) �— Step 2. 1 Select antenna mast from 3,5„ table below. ( * Horizontal boom also available in 12'-18'lengths (1'increments). Add desired width to end of frame support part number if less than a 20'width is desired Example: For an 18' width, order part number KY2016A18. (Refertotableforstep 1.) SECTOR MOUNT ORDERING INFORMATION (Qty. is for (1) sector only) Step 2. Select antenna mast kits (2 min.) (1) Kit per mast tube Antenna Mast Kit Part"No. Mast. " VY4935A 2.38"O.D. (0.154" wall) x 5'Long VY4935A8 2.38"O.D.(0.218"wall)x8'Long Step 3. Select leg mounting kit. PQeg;MouniftKit Strai NtC6 Part No. .Leg O.D. KY1994A 2.38"O.D. KY1995A 2.88"O.D. KY1996A 3.50"O.D. KY1997A 4.00"O.D. KY1998A 4.50"O.D. KY1999A 5.56"O.D. KY2000A 6.63"O.D. KY2001A 8.63"O.D. Leg Mounting Ta ered K Le Part No. LegO.D. KY2007A 2.38"O.D. KY2008A 2.88"O.D. KY2009A 3.50"O.D. KY2010A 400"D.D. KY2011A 4.50"O.D. KY2012A 5.56"O.D. KY2013A 6.63"O.D. KY2014A 8.63"0.D. Phone (309) 566-3000 * Fox (309) 566-3079 * www.rohnnet.com * The Industry Standard M. 207 0 2011 ROHN PRODUQS LLC P/wtb w' Envelope Only Solution APX Engineering Group, M. Phillips 17-0107.37 FP12 - Antenna Mount Analysis 3D RENDERED VIEW SK-1 May 23, 2017 at 2:12 PM FP12 - Antenna Mounts.r3d Envelope Only Soluban APX Engineering Group, ... ISK - 2 M. Phillips FP12 -Antenna Mount Analysis May 23, 2017 at 2:13 PM 17-0107.37 RELOCATED BRACE CONNECTION FP12-Antenna Mounts.r3d z x Envelope Only Solution APX Engineering Group, M. Phillips 17-0107.37 FP12 -Antenna Mount Analysis JOINT NUMBERS SK-3 May 23, 2017 at 2:13 PM FP12 -Antenna Mounts.r3d z x Solution APX Engineering Group, ... SK - 5 M. Phillips FP12 - Antenna Mount Analysis May 23, 2017 at 2:14 PM 17-0107.37 MEMBER NUMBERS FP1 2 -Antenna Mounts.r3d Z X Envelope Only Solution APX Engineer M. Phillips 17-0107.37 FP12 -Antenna Mount Analysis MEMBER SIZES SK-4 May 23, 2017 at 2:14 PM FP12 -Antenna Mounts.r3d z x Member Length (X) Displayed Envelope Only Solution APX M. Phillips FP12 - Antenna Mount Analysis 17-0107.37 MEMBER LENGTHS SK-6 May 23, 2017 at 2:14 PM FP12 -Antenna Mounts.r3d AX -50.611 201 d2.11 1 0.61b d2.71 Loads: BLC 1, Dead Load APX Engineering Group, ... SK - 7 M. Phillips FP12 -Antenna Mount Analysis May 23, 2017 at 2:16 PM 17-0107.37 DL FP12 - Antenna Mounts.r3d AX 21.21b1k 83.21b 1641b 2 6 b i 83.21b 1641b Loads: BLC 3. -WLX APX Engineering Group, ... FP12 -Antenna Mount Analysis +WLX SK - 8 M. Phillips May 23, 2017 at 2:17 PM 17-0107.37 FP12 - Antenna Mounts.r3d A IXz 1.21b/ b --------------------------- -63.21b -1641b %lalb -1641b �-03.2Ib -1641b Loads: BLC 4, -WLX APX Engineering Group, ... SK - 9 M. Phillips FP12 -Antenna Mount Analysis May 23, 2017 at 2:17 PM 17-0107.37 -WLX FP12 -Antenna Mounts.r3d .V �x z 17.81b/ft .51b n.81blft Z 504db Loads: BLC 5, +WLZ APX Engineering Group, ... SK - 10 M. Phillips FP12 - Antenna Mount Analysis May 23, 2017 at 2:17 PM 17-0107.37 +WLZ FP12-Antenna Mounts.r3d A IX14 43. il -17.81blt .50. -2491b / / � f -17.8Ib/8 -2491b -50 b 2491b Loads: BLC 6, -WLZ APX Engineering Group, ... SK - 11 M. Phillips FP12 - Antenna Mount Analysis May 23, 2017 at 2:17 PM 17-0107.37 -WLZ Flat 2-Antenna Mounts.r3d Cme Deck (Env ) N' Cel fi]-X 90.1.0 15-.60 0:.50 NC n ti �O 4 �0 4 2 4 z Z h O o Q O Ib` O o w 0 5 N aO 4 m 19 Member Code Checks Displayed (Enveloped) Envelope Only Solution APX Engineering Group, ... SK - 12 M. Phillips FP12 - Antenna Mount Analysis May 23, 2017 at 2:18 PM 17-0107.37 UNITY CHECK FP12-Antenna Mounts.r3d Member Shear Checks Displayed (Enveloped) APX Enqin( I M. Phillips I 17-0107.37 FP12 - Antenna Mount Analysis SHEAR CHECK No C.I. n 1.0 900.1.0 .rs•.m sass e:.se SK-13 I May 23, 2017 at 2:18 PM I FP12 -Antenna Mounts.r3d I Company APX Engineering Group, LLC May 23, 2017 MSe , Designer M. Phillips Job Number : 17-0107.37 Checked By: i Model Name FP12 -Antenna Mount Analysis Global Way Sections for Member Calcs 5 emal Sections for,Member.Calcs 97 Include Shear Deformation? Yes Increase Nailing Capacity for Wind? Yes ` Include War in ? Yes Trans-Load,Btvm�lntersectin °WoodWall?==Yes= _ =�a .`.. Area Load Mesh(in A2 144 Mende Tolerance in .12 =' P-Delta Analysis Tolerance 0.50% Include P-Delta for Walls? "Yes,; Automaticall Iterate Stiffness for Walls? No Max lterabons for WaI, Stiffness ° 3 Gravity Acceleration ft/secA2 32.2 Wall`Mesh'Size in 12' Ei ensolution Convergence Tol. 1.E- 4 Vertical Axis Y Global Member Orientation Plane xz Static5olver Sparse Accelerated Dynamic Solver Accelerated Solver Hot Rolled Steel Code AISC 13th 360-05 : LRFD Ad'ustS6ffness? Yes Iterative RISAConnection Code AISC 13th 360-05 :ASD l oldlFormed Steel Code -AISI NAS-01: ASD Wood Code AF&PA NDS-05/08: ASD Wood-Tem erature. 1D0F Concrete Code ACI 318-05 Masonry Code ' ACI<530-05: ASD Aluminum Code AA ADM1-05: ASD - Building Number of Shear Regions 4 Region Sacin Increment in 4 Biaxial Column Method PCA Load Contour Parma Beta Factor PCA .65 Concrete Stress Block Rectangular Use Cracked Sections? as, Use Cracked Sections Slab? Yes Bad Framin Wamin s? No Unused Force Warnin s? Yes Min 1!Bar Diam.=.S acin ? ° No; : v Concrete Rebar Set IREBAR SET ASTMA615 Min % Steel for Column . 1 Max % Steel for Column 8 RISA-3D Version 13.0.1 [f:\... \... \... \... \4C installation [2017]\FP12 -Antenna Mounts.r3d] Page 1 Company APX Engineering Group, LLC May 23, 2017 , w: Designer M. Phillips htk-,oss4 Job Number : 17-0107.37 Checked By: Model Name FP12-Antenna Mount Analysis Global, Continued Seismic Code ASCE 7-05 Seismic Base Elevation ft Not Entered Add Base Weight? No Ct X :035 _ Ct Z .035 T X sec Not Entered T Z sec Not Entered RX. 8.5 _ R Z 8.5 Ct Exp. X .75 Ct Exp. Z .75 SQ1 : 1 SIDS 1 S1 TL sec Not Entered Occu anc Cat 1orfl Om Z 1 mX> 1 , Rho Z 1 Rho`X; 1` Envelope A/SC 13th(360-05): LRFD Steel Code Checks 1 M13 PIPE_2.5 .259 11•••• 9 .059 11.... g 50966... 60858 51786 51786 1 Ht-1b -., 14 (PIPE 2.5 ` 'f191 it.... g.. q5 11,... `..•g `50966... D 51786 51786 1H7=1b 3 M15 PIPE_2.0 .097 .95 16 .027 0 8 22640... 38556 26951.4 26951.4 ... H1-1b 4' M PIPE 2A 10 T.01 1 0 ' ` 0 9 22640._ 55 26951A26951. .s HI lb 5 M17 PIPE_2.0 .240 1.01 9 .068 .63 8 22640... 38556 26951.426951.4... H1-1b M1 PIPE 20 :236 1.01, '9 ; 0 22640.;: 38556 26951: 2695t. ... H1-1ti 7 M20. PIPE_2.0 _160 3 9 .103 3 13 22969... 38556 26951.426951.41... H1-1b 3.`. 10 . 123 " 3 °. 9 <. 22969... 5 26951. 26951; :.. H1'-tb 9 M23 PIPE_2.0 .191 3 9 .091 3 9 22969...3855626951.426951.4... H1-1b 0 M22A, PIPE 1.25 .009 0 ^ 1 1.0071 0 9 16635... 23625 11529 11 1 H1-1b 11 M23A PIPE_1.25 .019 2.014 1 1.0151 0 8 14207..• 23625 11529 11529 .- H1-lb 12 M24 ` PIPE 1.25 ' .015 0 1 .006 '0 9 18695... 23625 11529 11529 1; Ht-tti 13 M25 PIPE_1.25 .013 2.014 1 .013 0 8 14207... 23625 11529 11529 •• H1-lb 14 M26 i'PIPE 24 '.0 .0050 9 32593- .38556 26951A 26951 .j 1:. 1-11-1b 15 M27 PIPE_1.25 .017 0 9 .016 0 9 635... 23625 11529 11529 1 H1-1b 16 M28 PIPE 1.25 032 2.014 9 D1 .11 16 74207... 3 2 11 2 11 9.a H14b 17 M29 PIPE_1.25 .028 0 9 .008 0 9 16635...23625 11529 11529 1 H1-1b M .'?IPE t25 "022 Ot" 1; 1t D 1a267..:23625 11529 11529 ••: Ht-1t 19 M31 PIPE_2.0 .883 2.42 8 .200 2.42 8 32593... 38556 26951.426951. ... H1-1b 20` M PIPE 2.0 9 •66 : 8 .013 .32 17815... 8556 26951A 26951.4.„ Ht-1b Load Combinations n.... infinn Cn P CRCC R P. RI r` Pa R Ce R Pe R Pe R Pn R Fe R P. R P. R P. RISA-3D Version 13.0.1 [T:\... \... \... \... \4C installation [2017]\FP12 -Antenna Mounts.r3d] Page 2 x Company APX Engineering Group, LLC Designer M. Phillips s Job Number : FP12-Ant Model Name FP12-Antenna Mount Analysis May 23, 2017 Checked By:_ Load Combinations (Continued) necnAMinn en D eoee C a- DI r e.. D .- D .- D .- o r.. e- o .- o C- 1 • � 1 ®� • ®� ilAll ®®®®II�R ®® RISA-3D Version 13.0.1 [TA ... \... \... \... \4C installation [2017DFP12 - Antenna Mounts.r3d] Page 3 Company APX Engineering Group, LLC May 23, 2017 ■ _ a, Designer M. Phillips +11711R' ,■ Job Number 17-0107.37 Checked By:_ "'! � + , Model Name FP12 -Antenna Mount Analysis Joint Loads and Enforced Displacements (BLC 1 : Dead Load) Inl .I nk-n I I nn 1 ANTI L Y -42.1 2 ANT2 L Y - " -42.1 3 ANT4 L Y -42.1 ° 4 RRUS32' R2 -50-6 5 RRUS12 E L Y -60 6 RRUSI1 f E - Y -54 7 SQUID L Y -20 8 `RR PI' L ` Y 6 Joint Loads and Enforced Displacements (BLC 3: +WLX) Inin.I h.1 I n nn n:.nn.:nn nn..,.e:A.A..mh Ir.:..\ 1:... A% n..... 1 ANTI L X 164 2 ANT2 L : X 164 3 ANT4 L X 164 4 RRUS32 .P2 L - X 83.2 5 13RU512 E L X 81.9 ' 6. ">R USI1,fE L;' X 765 7 SQUID L X 43.5 RRUS32 P1 L ' X 83.2'- Joint Loads and Enforced Displacements (BLC 4 : -WLX) 1 ANTI L X -164 ANT L X -164 3 ANT4 L X -164 4 RRUS32 P2 L 7 X -83.2 5 RRUS12 E L X -81.9 '..6 RRUST E . X -M5 7 SQUID L X -43.5 8; RRU 32 P1 L : X -83.2 Joint Loads and Enforced Displacements (BLC 5 +WLZ) .Ininf I nh.1 I n nn ti In1 11, —d\ ❑.Je 1 ANT1 L Z 249 2 ANT2 249 3 ANT4 L Z 249 4�: JRR Z 0 5 RRUS12 E L Z 36.8 6�RRUS11 `.E L".'= Z�'39.5 7 S UID L Z 43.5 a 8 > `:RRUS32 P,1 L' :'. :, `' Z = 50 6 Joint Loads and Enforced Displacements (BLC 6 : -WLZ) 1 ANT1 L Z -249 2 =' ANT2 -' L Z _ 4 3 ANT4 L- - - Z ----249 -`4,':. ',RRUS32(P2) Z - ,,-50.6 5 RRUS12 E L Z -36.8 �.� 7 SQUID L Z -43.5 F .. !tRRUS32 ` P1 - _ _ L ''"_. ., Z _ ' ii;-5t).6 7,7771 RISA-313 Version 13.0.1 [f:\... \... \... \...\4C installation [20171TP12 -Antenna Mounts.r3d] Page 4 Company Designer ``■■ 5 Job Number Model Name APX Engineering Group, LLC M. Phillips 17-0107.37 FP12-Antenna Mount Analysis Envelope Member Section Forces May 23, 2017 Checked By:_ nTomhor Q., Arhlnhl 1 C v Sh.ornhl 1 r` 7 Rhu.rrlhl I C Tnm.,.nh-inl I C v.v Mnm I C 7-7 Mnmenlrlh-inl 1 C 1 M1 1 max 3.417 1 5.205 12 14.795 13 79.885 8 240.144 8 604.367 2 min 2-197 23 -4.739 A -23.59" `'8 -64.079 13 •126.863 14 -474t755 3 2 max 3.417 1 5.205 12 14.795 13 79.885 8 158.109 9 551.012 4-^ - min i 7� .23 - 4:T39.= 19 -23 59- s8 :-84:079� =13: =to2 622 r14 . _'=426M175= -" 5 3 max 3.417 1 5.205 12 14.795 13 79.885 8 305.065 13 497.851 K23 min 21 T 23'.739 19 - 3 5 ° " 64:079 13 -243 49a° _77758 7 q max 3.417 1 5.205 12 14.795 13 79.885 8 456.733 13 445.666 in 2.4 3 -4.739 19 -23 5 4:079 13. 495.314 -332i 33 g 5 max -15.803 12r65.799 13 71.965 14 79.885 8 456.753 23 741.76 LID mi -24. 3-"'1 8 -55.479 : -64.079 13 -72TAM -644. 7 13'°11 M2 1 max 0 113 13.021 8 70.772 13136.37812 429.803 23 1 miri 1 $ -9 33'`1 90;797 8 124.143 58 ':00 8 13 2 max 0 113 13.021 8 70.772 13 268.701 12 336.472 23 '1 ' min 0 1 ;8 -9 3 1 90.797 8 -223 876 453 5715 3 max 0 113 13.021 8 70.772 13 401.023 12 243.355 19 16 min ;0° '1 8 -9: 13 -90:797 8 -323:608 9 -323307 12 17 4 max 0 1 9.121 13 13.021 8 70.772 13 534.433 8 150.708 19 18 _ min t _ .0 1 -12.7,2 3 '13 1 -90. 97 8 1-424.305 :13 493 537 1,2 19 5 max 0 1 9.121 13 13.021 8 1 70.772 13 1667.915 8 58.06 19 :K'- � Min 10 1 - 2.7.6 .833 13 -90.79 -525.1a2 `13 -63=768 12 ' 21 M3 1 max 143.307 8 332.114 13 1315.003 8 6.892 8 16886.873 13 2261.629 13 22 min -98.756 13 444.701 1019.029 9 6 8 _ 14 -8922.881 8 - 014: 41 8 23 2 max 143.307 8 332.114 13 1315.003 8 6.892 8 4558.098 12 1544.087 8 24 min -9 7 1 ` -044.701 g -1019.029 -3.698 1 -3559.587, -1142:'876 13,- 25 3 max 98.756 13 409.885 12 1048.267 9 26.12 12 18037.64 12 6291.743 12 26 1 min -143.307 8 -31 3 -1351.149` -2 .4 7_. -14005.6.. - 082 27 4 max 98.756 13 409.885 12 1048.267 9 26.12 12 4128.815 8 2090.015 12 ` min -143.307 8':_ 1'33 9 -1351149°'8 - 5 _7 -3177.83, 13.' -16 6.854 9,°`... 29 5 max 98.756 13 409.885 12 1048.267 9 26.12 12 7569.865 9 1574.673 13 ' mi -143.307 :_ 11. 3 ''9 -1351.149'8 -25.407 9. -9723.406..12, - 111 �712 12 - 31 M4 1 max 0 1 96.188 9 39.582 9 548.913 13 916.004 12 1124.907 13 32 min 0 1 -125.689 12 -5MU 1 -713,746 8 1-713.5G9 : -146&956 8 33 2 max 0 1 96.188 9 39.582 9 548.913 13 396.816 12 139.307 13 34 min AR' 1 725. 889:12 - 0.652 12 713.746 ^30T.792 1 9 -178 876 -8, 35 3 max 0 1 96.188 9 39.582 9 548.913 13 97.926 1 9 1110.036 12 36 1 min 0 1 -125:689 12 -50.652 12R535.361 6 -122.371, 12' -84 .21 9 37 4 max 0 1 96.188 9 39.582 93 13 503.643 9 2398.366 12 38 min =4 1 -125.689 12 -50.662'` 26 8 .-641.559 12' -1833`144 9 39 5 max 0 1 96.188 9 39.582 93 13 909.361 9 3686.696 12 40 min 1 -125.sa9 , 52 126 -1160-74612 -281907 41 M5 1 max 0 1 114.253 19 13.006 91 13 698.61 12 3558.122 9 min 0° 1 44T. . `1 -16 521 ` -549.528 ;9 -46 7.9 443 2 max 0 1 114.253 19 13.006 91 13 529.271 12 2418.317 13 44 i 0 1 -14709 12 -16: 21 12 8 . -416-243 3 30.8 7 45 3 max 0 1 114.253 19 13.006 9 535,361 13 360.143 8 1282.08 13 46. min :'-0 1 -147,09 12 -16.5 12 - - -283,119 . -1626.668 8 ° 47 4 max 0 1 1114.25319 13.006 9E209.529 13191.251 8 145.844 13 48 in : 0 ``-1 7. 2 -1 1.1 7150 277' .13 -155. 49 5 max 0 1 114.253 19 13.006 9 13 22.358 8 1392.85 12 509 ' min , , 0- 47: 9 12 -16.521- 1 -17.436 'I -1d31:641 19 51 M6 1 max 0 1 13.551 19 1.097 8 8 12 411.44 19 min s- 0 1. �15.23 1 10 16 1 ' 191 13 1253 2 max 0 1 13.551 19 1.097 8 8 12 281.16mi 0 1 -15.238 -1 3: b 13 W237.826 357 1255 3 max 0 1 13.551 19 1.097 8 .9 8 8 187.381 13 S6 min 0 1 -1 8 12 -1.10 13 -16679 13 1 -204724 RISA-3D Version 13.0.1 [f:\... \... \... \... \4C installation [2017]\FP12 - Antenna Mounts.r3d] Page 5 t Company APX Engineering Group, LLC May 23, 2017 e� Designer M. Phillips j-T Job Number 17-0107.37 Checked By:_ +3 Model Name FP12-Antenna Mount Analysis Envelope Member Section Forces (Continued) Member Sao AxialObI LC z Shearnbl LC Tor ue Ib-in LC v-v Mom LC z-z Momentnb-inl LC 57 4 max 1 0 1 1 t3.551 19 1.097 S 209.529 8 249.066 8 93.756 13 58 min 0 1 -15:2 8 12 - ,103 13 -166 796 13 -196.542 13 -110.54 10 59 5 max 0 1 13.551 19 1.097 8 209.529 8 260.306 8 110.9 12 6 in 0 1 - 5.238 12 -1.1 3 1 -166>7 6 13 -207.843 13-' 2 225' 0 61 M7 1 max 0 1 88.798 8 17.587 9 802.565 8 67.295 12 790.601 8 62 min 0 1 7:37 3-2.82212 -2231 1' -6.8 19 -67.7113 63 2 max 0 1 88.798 8 17.587 9 802.565 8132.74 13 88.926 23 64 min 1-67.337 1 - 8 2 12 - 22 131 3.'-16zo0fi " 119: 89 65 3 max 0 1 88.798 8 17.587 9 802.565 8 312.643 131 772.705 13 66Imin. 0 1 ' _ 7. 3 -22.822 12, -622.131 13, 400f642 8 -1029,779 8 67 4 max 0 1 88.798 8 17.587 9 802.565 8 492.863 9 1462.914 13 68 -- min -f -67 337 ` -2 82 2 -622:931 ' 13 -634.491 12 -1939.969 8 69 5 max 0 1 88.798 8 17.587 9 802.565 8 673.131 9 2153.122 13 70 Mill 0 1 - 7. 3 13 -22:822 12 -622.131 13 -868,42 12 .159 8 71 M8 1 1 195.64 8 41.329 9 624.315 12 1268.91 12 5708.02 8 72 _ 1 -148.029 4 2 -495 375 _ -994:598 -4374.6M 13 73 2 Ifi 1 195.64 8 41.329 9 624.315 12 731.8 12 3702.692 8 74 _ 1'_ -14aA29M -52 4 12 -495 375 9 -570,971 9 - S 57 9 75 3 1 195.64 8 41.329 9 624.315 12 194.69 12 1698.805 12 76 min ` 0 148:029 2 -52 12 495:375 9 -t48:851 19' -1389:546 9 77 4 max 0 1 195.64 8 41.329 9 624.315 12 276.284 9 215.327 23 78 -- + min 0 1 - -14a.029 23 -52 4 _ 12 -495.375 9' -342A19 12 -307.965 '8 79 5 max 0 1 195.64 8 41.329 9 624.315 12 699.911 9 1732.635 23 80 min 0 1 -148.029 23 -52.4 12 -495.375 9 -879.529 12i -231.293 8 81 M9 1 max 0 1 18.765 8 5.173 8 161.358 9 239.268 13 316.977 8 8 min 0 T -1382 3 -3.854 23 -195 353 '1 -312.038 8 -241. 1 2 83 2 max 0 1 118.765 8 5.173 8 161.358 9 202.335 13 125.262 12 4 min 0 1 -11826 23,-3.854 23 -1 5.3 3 12 -259.013 8 -10 .121 19 85 3 max 0 1 18.765 8 5.173 8 161.358 9 165.40313 76.212 14 8 min 1 -13.826 2 54 2 A95353. 12 -205.988 67.71 8 87 4 max 0 1 18.765 8 5.173 8 161.358 9 128.531 9 195.206 14 88 i 0 `1 -1 : 3 -3.854 23 -1 53 1 1-153,087 12' 4 Sg 5 max 0 1 18.765 8 5.173 8 161.358 9 91.811 9 325.668 23 90 min 0 L -13826 2 -3,864`23 .7195.353 12 -100-301 12' 452.3 7 91 M10 1 max 0 1 108.175 12 70.557 12 329.432 23 881.984 9 2320.294 12 2 min 0 1 8.024 9 "-55: -437:2 2 8 , -1061.418 12 959.629 _ 9 93 2 max 0 1 108.175 12 70.557 12 329.432 23 72.602 9 752.144 12 94min 0 1 - 4 9 -55833 9 - -437: 0 -53.003 20, _ - 93 9 95 3 max 0 1 108.175 12 70.557 12 329.432 23 984.402 8 613.657 23 96 " min 0 1 z88.Q24 9' -55 8 3 9 -437.202 -7411312 Z3 417.524 97 4 max 0 1 108.175 12 70.557 12 329.432 23 1 2007.06 12 1869.31 13 min 7 o 1 . 48.024 202 8--1546.163 2 5;273 8 _ 99 5 max 0 1 108.175 12 70.557 12 329.432 23 3029.886 12 3144.693 13 1 min '; 0 =88:024 9 -5 . 4 7 `-2355.545 9 022 8 101 M11 1 max 0 1 51.417 9 82.103 12 -509.997 8 2754.231 9 1866.849 13 1 2 min _ 0 1 8 32 2 -63.741 -3 :0 -3541.781 12 -24 7.7 4 103 2 max 1 0 1 51.417 9 82.103 12 509.997 8 1830.211 9 1121.569 13 104 inin D 1 - :2 b 3.741 9 398.00 9 -2351.5761 488.712 8. 105 3 max 0 1 51.417 9 82.103 12 509.997 8 906.235 13" 376.289 13 106 min 0 1 -68.23 1 1 9 -398.006 9-1161.561 8 9 651 8 107 4 max 0 1 51.417 9 82.103 12 509.997 8 28.834 12 489.898 12 108 min -0 :1 -68.232 12 -63.74' -39&006 9" -7 .693 19 - 69.507 9 109 5 max 0 1 51.417 9 82.103 12 509.997 8 1219.039 12 1479.016 12 110 min -; 0 1 -68.232 12 -63.74 -398.006 9 -941.85 9 -11' 4374 111 M12 1 max 0 1 6.146 16 13.469 13 12.724 8 462.762 8 158.733 8 112 min 0 -1 -6.985 Y3 -17: 4 8 =12.463 t3 -359.316 13' _ =1 .094 13 113 2 max 0 1 6.146 16 13.469 13 12.724 8 215.704 8 72.64 8 RISA-3D Version 13.0.1 [TA ... \... \... 1...\4C installation [2017]\FP12 -Antenna Mounts.r3d] Page 6 1 Company m, Designer Job Number Model Name APX Engineering Group, LLC M. Phillips 17-0107.37 FP12 -Antenna Mount Analysis Envelope Member Section Forces (Continued) May 23, 2017 Checked By:_ Member Sec Axialnbl LC v Shearnbl LC z Shearrlbl LC Torauenb-inl LC v-v Mom... LC z-z Momentnb-in] LC 114 •. min 0 1 -6.985 13 -17.043 8. -12A63 13 -164.063 13 $1-841 -13 ' 115 3 max 0 1 6.146 16 13.469 13 12.724 8 31.19 13 19.412 13 116 .: min 0 : 1 -6.985 93 -17.043 8 -12.463 13 -31.3 4 8" -30.044 10 117 4 max 0 1 6.146 16 13.469 13 12.724 8 226.443 13 120.665 13 min. � 0 �1-i 6.985=.;13 =17 043.r8 =12 463 - 13 278.412 ,ga =: 17066 - ` ` 16• 119 5 max 0 1 6.146 16 13.469 13 12.724 8 421.696 13 221.918 13 120 min _ 0 ` 1 -6.985 13 17.043 , -12.463 13 1525.471 ' 8 -20 .1 5 1 121 M13 1 max 0 1 0 1 0 1 0 1 0 1 0 1 122 min _ 0 1 0 1 0 0 1 0 1 1 --0 1 .. 123 2 maxI 653.97 20 46.308 16 142.2531 9 1 621.587 10 11129.04714 1295.398 16 124' `' mi -1063.835 1 12 339 13. 158.132 14 - 89 1 3 13 -10966.8.. 9 51T983 93 125 3 max 1653.97 20 21.654 16 35.453 9 621.587 10 6416.114 14 459.481 9 26 min-1063.835'9 1 -6.251 13 - 1' 32 14 -389.183 13 =6968.462' ' -267. 77 1.2 127 4 max 968.548 20 -3.081 12 469.809 14 1128.117 9 9247.657 14 1926.122 8 8 min:1471.761 9 -226.049 g ,561.149•' 9 ' -1 0120 14 -9533.977 13 -34 .9 "'1 129 5 max 0 1 0 1 0 1 0 1 0 1 0 1 1 0 " min __ 0 1 0 0 1 0- 1 '` 0 1' `0 1 131 M14 1 max 0 1 0 --L 1 0 1 0 1 1 1 0 1 0 1 1 min.,0 1..- 0- 0' .i:1 1 0 0 1 133 2 max 498.198 16 43.556 10 85.806 13 390.596 10 8331.381 10 1473.435 16 4 •: On -460.234 3-`17:304 13 117.034 i10 -2863 9 13 -7225.896 13' 371.585 13 135 3 max 498.198 16 18.903 10 16.503 12 390.596 10 5467.859 10 149.845 8 1 6 ; : rn n -460.234 i 1 -1 " 5 - .41 .9 - 1 -5767.631 :13 =6.75 2 ; 137 4 max 568.955 16P1.386 13 201.15 10 898.988 9 7800.661 10 1832.043 9 138' min ` 5ss.72s 13 8 -184.718 `13 -528 31 14 -8385.758 1 - 7 1; 139 5 max 0 11 0 1 0 1 0 1 0 1 14 _n 1 1 0 1 0 1 0. 141 M15 1 max 365.666 13 1 77.047 8 83.562 13 0 1 0 1 14 �' ' in 4380.736 10 `. 3 =7 39 .13 -231017 16 t 0 t'' 0 ' 1 143 2 max 634.576 1313 40.41 8 57.495 13 946.31 12 -1108.887 13 144 min. -1027.46' 1' - 71..1 -1:. 7 1 .-1002.456 ;9 -1 76. 7 �. 1 145 3 max 670.616 13 13 3.505 8 57.495 13 1342.883 8 90.331 8 146 min 1027.46• 1p -109.633' 1 -2.093 14 -199:467 16 -1302.139 1 -3,259 1 147 4 max 857.04 9 -4.169 12 40.412 9 62.551 13 964.584 8 633.741 1 1'48 min'-808.648'14-22-725 9 -33.85-'12 -252747 10 -969.713 131 339.196 12 149 5 max 893.082 9 148.8281 1 77.718 9 62.551 13 0 1 0 1 150 > mi" -808.s43 14 67.56 '12 -70.936 I12 -252.747 10 '; 0 1`: 0 1 151 M16 1 max 900.514 9 208.437 1 71.858 12 430.432 14 0 1 0 1 %152 " • `' mi -1 4 4' 124.414' 13 -7 .111: ` 9. ` 4 6:124 9 0 1;: 0' 1 153 2 max 936.553 9 -62.217 13 34.042 12 430.432 14 971.018 8 -1090.51 13 4 ' ' min1 -104.003 14 -10 .87 J -40.2 5 9 496 124 T 1015a816 9 i -1843 412 1 155 3 max 972.593 9 -66.968 13 2.053 14 430.432 14 1255.089 12 106.283 9 1 6 : in -104.003 14 - 09 6 -496- 4 9 -1414.403 'g' 9 157 4 max 690.319 9 -2.237 13 35.179 13 464.615 14 970.847 12 666.181 8 158 ' min:-372.387 4 -26. 02 8 -40.977 8 -472.377 1109zo51 . 294.307 13 159 5 max 535.623 13 167.544 8 72.422 13 527.54 14 0 1 0 1 16 min ;-550.615, 10 56 133 13 - . 3 -478 61 9 1 -A ' 161 M17 1 max 2334.049 13 400.181 9 18.652 16 297.12 10 0 1 0 1 162 F. min Jo50.975 8 12 -19. 5. 13'' - . 1 ' , 1 1 163 2 max 2936.18 13 -26.341 12 26.61 19 348.557 10 215.916 14 577.934 12 64 min -2781.0983 -16s 9 -2 5 2 -66.558 13 -164.368 5 165 3 max 2900.14 13 -31.091 12 55.728 9 348.557 10 785.387 19 119.792 19 166: ' ' i •2745.058 -201024 9 6 .462 -1 -66:5 1 -882.908 12 -53 899 '.12 ' 167 4 max 3288.252 9 -15.121 14 88.569 9 443.1 10 1840.359 19 1162.01 9 1 i -2536. : 1 -34737 1 -107.757 1 8. 29 1 -2360.226 12 12 169 5 max 1894.337 9 263.974 9 748.156 8 443.1 10 0 1 0 1 1 " MIA-1342.672 2' q 564.327''23 `- 8.92 13 '� 1` a0 1 RISA-3D Version 13.0.1 [TA ... \ ... \ ... \ ... \4C installation [2017]11=1312 - Antenna Mounts.r3d] Page 7 -"' + - .-...; �, \�` S-A-i' Company Designer Job Number APX Engineering Group, LLC M. Phillips 17-0107.37 May 23, 2017 Checked By:_ _ _ V Model Name FP12-Antenna Mount Analysis Envelope Member Section Forces (Continued) Mpmhpr Sor. Avinlflhl I r. v Shparnhl I C v Sh.prnhl I r` Tnrnuprlh inl I C v_v Mnm I C _> Mnmanfflh_fnl I C 171 M18 1 max 2797.052 9 397.688 9 37.514 12 585.115 9 0 1 0 1 172 min -1009.852 12 12 -49 45 9 -324.804 20 0 1 0 1 173 2 max 2761.008 9 -22.055 12 6.877 14 585.115 9 286.698 16 -569.298 12 014 1min -973.813 2 -201.68 _ -1 4 9 -324M4. 20 -392s19 9 3 93 743 9 175 3 max 2724.968 9 -26.806 12 26.619 13 585.115 9 268.971 14 244.521 9 17 min -937.773 ; 2 -208.014 ;9 736.083 324: 4 -250A61 9, 1 3.4 4. 12 177 4 max 1918.287 9 -3.039 13 64.397 13 592.085 9 847.624 23 1058.111 1 178 i -1005:108 12 3 1 8 -373 5 5 14 -1145-021 574.395, 12 179 5 max 830.367 13 250.231 1 266.4 1121 592.991 9 0 1 0 1 t 1 min : <685.98s 16 134t972 13 -202-793 1 -461526 j4 0 1 181 M20 1 max 0 1 0 20 .003 10 0 1 0 1 0 1 ;1 2 in'' 0 1 0 9 -003 9 _0 1 10 1 1831 2 max 178.372 8 1115.717 12 51.897 13 753.779 20 1777.493 13 81.503 13 184 'min -1 2 '13 -107.84 9 -108.689 1 -1081.972 ` 9 -2189.148 16 -207.218 10 185 3 max 172.124 8 409.023 13 419.713 141 1193.099 13 3739.399 9 2012.125 9 186 min -184.102 g -401.584 8 -475863 1 9 t -1561.038 8 -4145;558 -2085.813 12 187 4 max 7.289 1 .005 9 .012 10 0 1 .143 9 .093 9 188 in 4.686 `12 -.002 8 -.0 8- 0 '1 '1 -.216 10` -.035 8 189 5 max 0 1 .005 9 .012 10 0 1 0 1 0 1 L190 '. min 0 1. -.002 8 `-.008. 9 0 1,' 0 1" 0 1 191 M22 1 max 1 0 1 0 10 .005 10 0 1 0 1 0 1 192 min 0 1 0 13 -.004 9 0-` 1, 0 1 0 1` 193 2 max 99.537 1 8 1173.702 8 142.012 13 920.042 9 1092.991 13 756.857 9 194 min 5.283 13'- 2.714 1 -171.114 = 125.289 .1471304,961 10 322.712 20 195 3 max 93.29 8 1381.843 9 311.4911141 1900.442 9 4092.103 9 1334.439 13 196 min - 6. -240s82 '12 -340.788 9 -1238.673 2().-4385,021 10 2623.9 4 197 4 max 7.289 1 1 .003 9 .003 16 0 1 1 .033 9 .052 9 1 min 4.6 22" A06 :,8 -.002 a '1 1 -.047, 16. e:.10 8" 199 5 max 0 1 .003 9 .003 16 0 1 1 0 1 0 1 200 i 0 -` 002 9 Q: A 0_1 '' 0 1_ 201 M23 1 max 0 1 0 20 .004 10 0 1 0 1 0 1 min 0 1 -.001 9 . 5 0, 0, 1' 0 1. 203 2 max 118.251 9 56.697 112 176.11 13 916.485 20 842.152 13 -317.174 12 204 min -4.448 12 -160,576 g -178.495 110 -1383186 ,9 -1332.764 10 _-550.627 1- 205 3 max 112.004 9 250.542 13 302.477 14 916.485 20 4465.671 9 2410.155 9 206 min -106.342 8 -354.347 -305.388 9 -1 3.786 9' -4645.682 1 -14774,561 12 207 4 max 7.289 1 1 .008 9 .007 10 0 1 .018 13 .151 9 08 min. 4&86 13 0. 12 -. 01 1_1 0 1 -.127 10 - 14 1 209 5 max 0 1 1 .008 9 .007 10 0 1 0 1 1 0 1 1 min 0 1 Q, 1 -.001 13 0 1 ` 0 2111 M22A 1 max 301.569 1 0 1 0 1 14.696 20 0 1 0 1 212 80.87 1 0 -67.188 9" 1` 0 1 213 2 max 299.025 1 0 1 1 0 1 14.696 20 0 1 0 1 214 -' nrim 179.243 13 0 1' 1 - 6 T, 88 9 0_L 01' 215 3 max 296.482 1 0 1 0 1 14.696 20 0 1 0 1 '216 min 177.608 13 0 - 1 7 1 9 0 1` 0 1 217 4 max 1293.939 1 0 1 0 1 14.696 20 0 1 1 0 1 218 min 1175.973ja 0 1 0 1 7.1 8 0 1 0 1 219 5 max 1291.395 1 0 1 0 1 14.696 20 0 1 0 1 min 174.33811 1 0' 1 718 9 0 1-: 0 1t 221 M23A 1 max -421.372 13 3.412 1 0 1 84.401 23 0 1 0 1 222 min - 19.01 1 19 .1 0 ,. 1 -145.582 8 0 1 0 223 2 max -419.737 13 1.706 1 0 1 84.401 23 0 1 -20.303 13 224 min 71s.as7 1 1.0 7 1 0 1 " -146 582 "8 0 1 _ -31r.582 225 3 max -418.102 13 0 1 0 1 84.401 23 0 1 -27.071 13 226 min -713s23 1 0' 0 . 1 -146.582 '8 0 1 1{2.11 1 227 4 max 416.466 13 -1.097 401 0 1 84.401 23 0 1 20.303 13 RISA-31D Version 13.0.1 [f:\... \... \... \...\4C installation [2017]\FP12 - Antenna Mounts.r3d] Page 8 hI- Company �1q; Designer � Job Number Model Name APX Engineering Group, LLC M. Phillips 17-0107.37 FP12 - Antenna Mount Analysis Envelope Member Section Forces (Continued) May 23, 2017 Checked By:_ Memher Sac AsialOhl I r v Shaarflhl I C 7 Shaarflhl I C Tnrnnwflh-inl I C v-v Mnm._ I C 7-7 Momenlrlh-inl 1 C 2284° 1 min -711.38 - -1.70 1. 0 t= -14 582 8 c 0;TIR-31.5N82. 1 229 5 max -414.831 13 -2.193 12 0 1 84.401 23 0 1 230 min 5-708.836 1 -3.41 1 0 1 -146582 8 0 1231 M24 1 max 488.778 1 0 1 0 1 9.968 20 0 1 min 27-&8 6 131._-d0 < -1:.-r:56.50 z, 9 :Z 0,.233 2 max 486.235 1 0 1 0 1 9.968 20 0 1 34 ': min 272.1711 0 1 0 1 ;' - 0 1 235 3 max 483.691 1 0 1 0 1 9.968 20 0 1 36 min 270.536'1 13 1 ! - 1 56 504 0 t: 1 . 237 4 max 481.148 1 0 1 0 1 9.968 20 0 1 0 1 min = . 0 ' 13 T 1 0 1 1 ' =56 50 `. 0 1- 1 239 5 max 478.604 1 0 1 0 1 1 9.968 201 0 1 0 1 40 min 267.266 1 0 1Y -5 .504 9 0 1 241 M25 1 max -261.161 13 3.412 -L 1 0 1 112.971 141 0 1 0 1 42 '' imin =456.,255 1: 2.19 0 -12 3 '9 1 : ` 1 243 2 max -259.626 13 1.706 1 0 1 112.971 14 0 1 -20.303 22 44 " min -453. 112 '1 1:0 7 1 . - 3'9 1 ` 31C 245 3 max -257.891 13 0 1 0 1 112.971 14 0 1 -27.07 22 246 min :=451.16& 1. 0 " 1 . 1" ° -12 :92 8 =- 1 �2.11 1 247 4 max -256.256 13 -1.097 13 0 1 112.971 14 0 1 -20.303 22 248 ,' min 448•s25 `" 1:706 1 1 -123'92 8 .: 0 1 t 31582 249 5 max -254.621 13 -2.193 13 0 1 112.971 14 0 1 0 1 250 min-446,081 1 -3.412 1 0 1 _-123'.922 8 ,_ 0 1l_ 0_ 1 _ 251 M26 1 max 192.017 1 0 1 0 1 1 9.888 20 0 1 1 0 1 min7 173= 1 1 1 -1 2M 0 1:' 253 2 max 188.257 19 0 1 0 1 9.888 20 0 1 0 1 254 1 1 min 84.504` 120 0 1 -112.05 9 0 1 < ° 0. 1 255 3 max 184.699 19 0 -L 1 0 1 9.888 20 0 1 0 1 56 min '81.836 1121 0 * 1 _0 1 14 9 " 0, 257 4 max 181.141 19 0 1 0 1 9.888 20 0 1 0 1 258 min .167 JZ 0 1 "'0 1 -112.05 9 0 1' 0 1 259 5 max 177.583 19 0 1 0 1 9.888 20 0 1 0 1 260 min -76.49 12. 1 0 1 t e -112-05 9 261 M27 1 max 581.482 9 0 1 0 1 114.638 12 0 1 1 0 1 262 min 78.049. 12, 0 1 0 1 -161'_184 0 1' 0 1 263 2 max 579.302 9 0 1 0 1 114.638 12 1 0 1 0 1 264 14 min'76.414 12 0 1 0 1 161i184 9 0 A � 0. 1' 265 3 max 577.122 9 1 0 1 0 1 114.638 121 0 1 0 1 266'=: min .-74.779"12 0°' `1- '.`0 _ 1 `-1611184 9 ' <` 0 1 t 0 267 4 max 574.942 9 0 1 0 1 114.638 12 0 1 0 1 8 min 73.143 "12 0_ 1 0 1 _- 1.1 4 1 0 1 269 5 max 572.762 9 0 1 0 1 114.638 12 0 1 0 1 270. mm::71.50=-12.. 4; 1 "r 0 �1 -18 1 9 "=0 -i, -�0 e'I 271 M28s 1 max -188.847 12 3.412 1 0 1 49.75 12 0 1 0 1 272 min -1388A61 '' 3 3 1 ' 2_ 7 10 0 1 1 273 2 max -187.212 12 1.706 1 0 1 49.75 12 0 1 -20.303 23 4 s mi -1385s8t ,9 - 1.0 7 23 0 b,-9 .347 9 .1 = -3 5 2 1 275 3 max -185.577 12 0 1 0 1 49.75 12 0 1 -27.071 23 276 in -1383.801 1 1 -92 347 10 0 1`- -42 11 1 ' 277 4 max -183.942 12 A.097 113 0 1 1 49.75 12 0 1 -20.303 23 7< i`-1381.621 9 -1 6 1 0 1 .3 7 10 .:: 0 1'' S 2 279 5 max -182.306 12 -2.193 13 0 1 49.75 12 0 1 0 1 280 min =1379.441 9 -3.412 1 0 1 ` -922 7 10 0 1 0 1 281 M29 1 max 939.73 9 0 1 0 1 31.745 20 0 1 1 0 1 2821 min 160.986 j-z 0 1 1: -76155 9 0 1 0 1 283 2 max 937.549 9 0 1 0 1 31.745 20 0 1 0 1 4 L, 1'5 .3 .' I 7 0 RISA-3D Version 13.0.1 [T:\... \... \... \... \4C installation [2017]1FP12 - Antenna Mounts.r3d] Page 9 WI-RS_ Company Designer CA, Job Number - Model Name APX Engineering Group, LLC M. Phillips 17-0107.37 FP12 - Antenna Mount Analysis May 23, 2017 Checked By:_ Envelope Member Section Forces(Continued)Member Section Forces (Continued) Mamhar Rpn Axialnhl I C v Rh..rnh1 I r v RhparrIhl I r Tnrnuonh_inl I r. v_v Mnm 1 r v Mnmantrih_inl 1 r 285 3 max 935.369 9 0 1 1 0 1 31.745 20 0 1 0 1 286 min 157.716 12 0 1 0 1 -76.15 9 0 L 0 -1 287 4 max 933.189 9 0 1 0 1 31.745 20 0 1 0 1 288 Min ll 8 1 0 1 0 1 -76.155 0 1 0 1 289 5 max 931.009 9 0 1 0 1 31.745 20 0 1 0 1 min 154. 446 12 : 1 1 -76.155 9. 0 .1 291 M30 1 max -172.428 12 3.412 1 0 1 136.271 12 0 1 0 1 292 i-905.959 9 2.193 23 0 1 .. -1' 7 0 0 0 1 293 2 max 1 -170.793 112 1.706 1 0 1 1 136.271 1121 0 1 1 -20.303 23 294 min -903.779 9 1.097 23 0 1 -169.737 1101 0 1,: 1 1 295 3 max -169.157 12R245.849 1 0 1 136.271 12 0 1 -27.07 23 296 minl-901.598 91 0 1 -1 9.7 10 0 1 42:11 1 297 4 max -167.522 1212 0 1 136.271 12 0 1 -20.303 23 9 min` -899.418 1 -169.737 ° 10 1 1. 1 .. 299 5 max -165.887 1212 0 1 136.271 12 0 1 0 1 0min -89Z238 '9 1- 0 69.737 0 0 1 0' 1 301 M31 1 max 538.67 9 8 608.946 9 474.366 23 0 1 0 1 302 min -95.761 12;L3 -782.57 8 -676.658 8 0 1 0303 2 max 535.112 9 8 608.946 9 474.366 23 6242.307 g 1869.893 13 304 - min -98.43 12 -182,411 13 -782.57 .8 -676 6 8 8 -8022 12s 8 -2520.196` 8 305 3 max 531.554 9 245.849 8 608.946 9 474.366 23 12484.614 9 3739.787 13 306. min -101.098 12 =182;411'1 -7 .57 8 -616.658 S -16044.2_,8 -5040.392 8 307 4 max 304.065 9 462.626 9 1886.65 8 494.646 23 15015.933 9 4742.382 9 308 min 2 - 8 -1464.826' 9 95.357 -19340.0. - 2480 6 8.- 309 5 max .146.64 300.507 9 462.626 9 1886.65 8 494.646 23 0 1 0 1 310 min.143.972 20 '-609.51 8 -t464:826 -695 357 8. 0 1 0 1 311 M32 1 max 2814.247 8 17.714 1 0 1 280.516 9 0 1 0 1 ' 1 min-2173.777 13'! 11.38 2 1 -204. 7 12 0 <1 0 1 313 2 max 2813.509 8 8.857 1 0 1 280.516 9 0 1 -187.692 23 314 in -2174-33 13 23 0 1 ° - 41 7 12 91,.965' 1 315 3 max 2812.772 81 0 1 280.516 9 0 1 -250.255 23 316 min =2176.049 9 1.-204.167 12 1 8: 9 317 4 max 2812.149 1222 0 1 280.516 9 0 1 -187.692 23 318 in -2175.787 '9 K70.841, 1 0 1 20 1 7 12 0 1 291:965 1 319 5 max 2811.596 12 22 0 1 280.516 9 0 1 0 1 320 min-217ti:524 1 1 204.167 "12 1 1 321 M34 1 max 133.102 8 14 80.951 14 -408.983 13 1214.334 9 .002 8 2 min -133.102 9 1 -78.01 "1 -637 56 1 -1198.096 8 -:002 1 323 2 max 133.102 8 1 45.54 14 1 80.951 14 -408.983 13 1155.865 9 53.13 1 324 in -183.102 9 ''-70.841 1 -78.01 ''1 7 6 1 4197 504 34.151, 1 325 3 max 133.102 8 45.54 14 80.951 14 -408.983 13 1097.395 9 106.261 1 326 Min -133.102 9 jQ,84f1 -78.01 " 13 7' 1 -1196.91 - 14 327 4 max 133.102 8 -45.54 14 80.951 14 -408.983 13 1038.926 9 159.391 1 328 min -133.102 q.`-7 . 4 01 ` 13 14 329 5 max 133.102 8 -45.54 14 80.951 14 -408.983 13 980.456 9 212.521 1 330 min-133.102 '9 -70. 41' -7 3 .-637.56 1 -11195.728 8 136.619 14 331 M36 1 max 80.948 10 -45.397 13 132.077 9 0 1 .005 17 .001 21 33 min - 0.961 "9 1 -70.84 ` 12 0 1 - 00 12 0 19 _333 2 max 80.948 10 -45.397 -1-133.12 13 132.077 9 0 1 297.175 9 159.39 1 4 min -80.96 -7 . 9 -133.1 1 0 -299.527 2 102,143 1' 335 3 max 80.948 10 -45.397 13 132.077 9 0 1 594.347 9 318.78 1 33 min' -80 96 7 . 4' 1 -133.1212 1 -599047 12 204.286 13 337 4 max 80.948 10 45.397 13 132.077 9 0 1 891.52 9 478.17 1 38 min -80.9 -7 .8 -133.12 12 1< -898.568 :-12 306 28 13 339 5 max 80.948 10 -45.397 13 132.077 9 0 1 1188.692 9 637.561 1 40 min -80.961 70 84 1 -133.12 12 1 -119&.089 12 0 57 13 341 M37 .1 max 63.2 14 -48.6 23 122.167 9 0 1 .002 13 0 1 RISA-3D Version 13.0.1 [T:\... \... \... \... \4C installation [2017]\FP12 - Antenna Mounts.r3d] Page 10 Company ■ ., Designer �Q ■-` Job Number Model Name APX Engineering Group, LLC M. Phillips 17-0107.37 FP12 -Antenna Mount Analysis Envelope Member Section Forces (Continued) May 23, 2017 Checked By:_ Member Sec Axialnbl LC v Shearnbl LC z Shearnbl LC Tor ue b-in LC v-v Mom... LC z-z Moment Ib-in LC 342 in -63.202 ' 9 -75.6 1 --122.,fd 12 0' �; 1 e: -.004" 12< 0 I"5 1 3431 1 2 max 63.2 14 -48.6 23 122.167 9 0 1 274.874 9 170.1 1 344 min -63.202 9 -M6 1 -122.4 12 0 1 "-275A04 12 109.35 12 345 3 max 63.2 14 -48.6 23 122.167 9 0 1 549.75 9 340.2 1 .346 r =� min`63202'=9s 75.6 "7 122: "`12 0 "` 1"' 550.e04 12:` 2183 12L 347 4 max 63.2 14 -48.6 23 122.167 9 0 1 824.627 9 510.3 1 348 - min .202 ' 9 ' - 55.6 ' 1 -122.4 12 0 1 + -826.204 12 328.05 23 349 5 max 63.2 14 -48.6 23 122.167 9 0 1 1099.504 9 680.4 1 350 rni !-63.202 9 -75 6 1 -M.4 12 0 1 -1101.604 12 437.4 23 351 M40 1 max 58.88 10 -54 123 130.823 9 0 1 .002 16 0 23 352 _ -°- min -58M '9 -84 4 1 - 1^ 12 0 1 .1 -002 12 `0' "F 353 2 max 58.88 10 -54 23 130.823 9 0 1 294.352 9 189.001 1 354 min Z8.88 9 -84 1 -1 04.:1 <29a.841 12 121.5 12. 355 3 max 58.88 10 -54 23 130.823 9 0 1 588.704 9 378.001 1 356 in "w &88 ° 9 -84 12, 1 -589 681; 12,' 243 12 357 4 max 58.88 10 -54 23 130.823 9 0 1 883.056 9 567.001 1 358 i - 8.'88 9 4 11 -131.04' 12 0 1 -884.521 12 364.5 12 359 5 max 58.88 10 -54 23 130.823 9 1 0 1 1177.408 g 756.001 1 1 360 in -58.88 -84 1 -131.0 12. 0sF 1 i 1479.36" 1 ' 48 =23 361 M39 1 max 122.391 8 -48.6 15 63.2 14 -437.4 12 1099.499 9 .001 17 '362 ' in -122:375, 5-601 '1 =6366 13 80.4 1 11o1so412 - 10 363 2 max 122.391 8 -48.6 15 63.2 14 -437.4 12 1051.753 9 56.7 1 364' min 5122-375 -7 - 1 1 -63.666'13 -680A 1 -11a1-16212` 36,451 1 365 3 max 122.391 8 48.6 15 63.2 14 -437.4 12 1004.008 g 113.401 1 366 i -122.375` g 75:601 ''1 ° 3:6 6' 1 =6 4 1 . -1100719 12, 2.901 14 ° 367 4 max 122.391 8 -48.6 15 63.2 14 -437.4 12 956.263 9 170.102 1 36 min -122-375 '-7 . 1., 3. 13 - .4 1 -1100.27$ 1 9: 51 •14 369 5 max 122.391 8 -48.6 15 63.2 14 -437.4 12 908.518 9 226.802 1 370 _ min -I 375 . y -601 -1 ` -63:866 '13 680A 1 -1o99.a37 - 145.801 74. 371 M40A 1 max 131.027 9 -54 14 59.377 13 756.001 1 1177.41 9 .003 1 372 '_'" min,.A31.027 8; 84 1 7 1 6 2.A1796366 a -.001 1 373 2 max 131.027 9 -54 14 59.377 13 756.001 1 1221.936 9 63.003 1 7 -131027 8 -84 1 - ° 79. 10 _4 1 '1t79.e32 40.5 _ k . t 375 3 max 131.027 9 -54 14 59.377 13 756.001 1 1266.461 g 126.003 1 376 min -131.027 8 -84 ' 1 -58.879` 10 486 12-1180.301 1ZI 81 15 ' 377 4 max 131.027 9 -54 14 59.377 13 756.001 1 1310.987 g 189.003 1 378 - min .A31.027 . _8 -58-879 :10 :486 12 -1180.774 12 121: 15- 379 5 max 131.027 9 -54 14 59.377 13 756.001 1 1355.513 13 252.003 1 3$0 min =13t_027 8: -84 °'; 1 = 8-879'10 :486. 12 1181.247 12 162 �15 381 M40B 1 max 133.118 13a-454 82.68 13 637.562 1 1188.694 g 003 1 2 _ min -133A18 80.951: 14' 0 .572 ` 13'-1198.091; 12, -- 23 ° 383 2 max 133.118 13 82.68 13 637.562 1 1260.703 9 53.134 1 in .=133.118 9 408 572 . 1 -1198.546 8 ` 34155 1385 3 max 133.118 13 82.68 13 637.562 1 1312.711 9 106.265 1 8 _ nii -133.118 8 r-70. 1 `1 -80: 51- 14 408.572 _11s9:012 15'' 387 4 max 133.118 13 -45.54 15 82.68 13 637.562 1 1374.719 9 159.396 1 8min.=133118 .8 4 . 1 �' ` 4 408.572 13 -1199.477 8�^ 389 5 max 133.118 13 -45.54 1513 637.562 1 1436.727 g 212.527 1 390 min .-133-118 8 -70.841 ''1 14 40 7 1199.9a3 8 136. 1 5 391 M40C 1 max 80.963 10 -45.442 13 9 0 1 .004 21 0 6 392 min ' 7 9 -7 . 4 1 . 5-M951 01 1 001 . 10 "17 393 2 max 80.963 10 -45.442 13 9 01 303.581 9 159.39 1 in 80: 7 7 18 Of 1- 9 .52 8 102:245 1395 3 max 80.963 10 -45.442 13 9 0 1 607.159 9 318.78 1 396 min '-80.978 9 77 .8 1 -133.12t'8 . 1 1-§9-9.042 8` 204.4 1 1 397 4 max 80.963 10 -45.442 13 134.923 9 0 1 910.737 9 478.17 1 39 in `= . 78 9 ._ -7 _84 _1. -133.121 O,i 1 i-898.564JL 306,737 13: RISA-3D Version 13.0.1 [T:\... \... \... \... \4C installation [2017DFP12 -Antenna Mounts.r3d] Page 11 Company APX Engineering Group, LLC May 23, 2017 p■ a: Designer M. Phillips Job Number 17-0107.37 Checked By:_ Model Name FP12-Antenna Mount Analysis Envelope Member Section Forces (Continued) Envelope Joint Reactions Joint X Ilbl LC Y llbl LC Z TIM LC MX Ilb-inl LC MY Ilb-in'! LC MZ rlh-inl LC 1 TOP max 1516.278 13 1556.727 1 12024.655113 0 1 0 1 0 1 2 ., . min -1984.337 ".. 35.8 7 . 23 -3027961 11 a 0 -JL 0 0 `9- 3 BOTTOM max 1417.098 9 654.628 19 2627.466 9 0 1 0 1 0 1 in -1171.771 12 62.524 '12 4 2:864 20 c 0 1 0 9 0 T 5 N17 max 441.824 8 201.907 8 1281.906 8 0 1 0 1 0 1 min -331.54_ 1 -142.466 23 -9 3.54 90 0 1 0_' 1 7 N18 max 401.335 12 45.756 8 1308.536 8 0 —:L 1 0 1 0 1 8 min -305.364 9-21.852 13 --19t2:5zs , 9 0 i 0 1 0 1 9 N19 max 20.905 8 111.762 8 16.934 9 0 1 0 1 0 1 90 min :-1 .221 2 �-82.503 23 -19 351 12 0 0 1 0 1 11 N20 max 34.671 12 71.608 19 19.073 12 0 1 0 1 0 1 12 min -26591 19 -92. 83 112 -15.205 1191 0 1 0 1 0 1 13 Totals: max 2201.732 13 1100.3921 1 2403.191 9 14 min 22Q1.712 8 '7 7395 13 -2403,19 14 RISA-31D Version 13.0.1 [TA ... \... \... 1... \4C installation [2017]\FP12 - Antenna Mounts.r3d] Page 12 Connection Calculations In Accordance With AISC LRFD 14th Edition APX Engineering Group, LLC 3400 Lakeside Drive, #525, Miramar, FL 33027 AT& FP12 [FA# 10070076] 17-0107.3 M. Phillios. Mav 201 U-Bolts at Tower Legs ASTM A307, 1/2" 0 Tu = 3,750 Ibs (MAX Tension Reaction per RISA-3D, Factored) N = 4 (Numbers of Bolts in Tension) Tma. = T,, / N (MAX Tension per Bolt) 938 Ibs per Bolt Vn = 2693 Ibs (MAX Shear Reaction per RISA-31), Factored) n = 4 (Numbers of Bolts in Shear) VMax = VG / n (MAX Shear per Bolt) 673 Ibs per Bolt �Tn = 6,627 Ibs (Bolt Design Tensile Strength, AISC Eq. J3-1) �Vn = 3,976 Ibs (Bolt Design Shear Strength, AISC Eq. J3-1) fn, = 3,428 psi (Bolt Required Shear Stress, AISC J3.7) Fnt = 1.31=nt - (Fnt/r Fnv)fry > Fnt = 45,000 psi (Modified Nominal Tensile Stress, AISC Eq. J3-3a) = 50,882 psi (Thus, Fat Governs) ORn = 6,627 Ibs (Bolt Available Tensile Strength, AISC Eq. J3-2) TMax 5 �Rn OK 14.1% Stressed Combined Bolts at Standoff Connections to Tower Leg Brackets ASTM A325-N, 3/4" 0 Tu = 750 Ibs (MAX Tension Reaction per RISA-3D, Factored) N = 1 (Numbers of Bolts in Tension) TMas = Tv / N (MAX Tension per Bolt) = 750 Ibs per Bolt V = 5j250 Ibs (MAX Shear Reaction per RISA-3D, Factored) n = 1' (Numbers of Bolts in Shear) VM;ix = V / n (MAX Shear per Bolt) = 5,250 Ibs per Bolt �Tn = 29,821 Ibs (Bolt Design Tensile Strength, AISC Eq. J3-1) �Vn = 17,892 Ibs (Bolt Design Shear Strength, AISC Eq. J3-1) f, = 11,884 psi (Bolt Required Shear Stress, AISC J3.7) Fnt = 1.3Fnt - (Fnt/�Fnv)fn, > Fnt = 90,000 psi (Modified Nominal Tensile Stress, AISC Eq. J3-3a) = 90,592 psi (Thus, Fnt Governs) �Rn = 29,821 Ibs (Bolt Available Tensile Strength, AISC Eq. J3-2) Page 1 of 2 Supporting Member Bolts (TYP.) T IH V TMaz < �Rn OK 2.5% Stressed Combined Connection Calculations (Continued) �_' S" In Accordance With AISC LRFD 14th Edition AT&T APX Engineering Group, LLC FP12 [FA# 10070076117-0107 37 .. 3400 Lakeside Drive. #525. Miramar, FL 33027 M. Phillips, Mav 2017 aaz >„ai Bolts at Standoff Bracing Members ASTM A307, 1/2" 0 Ta = 3,500` Ibs (MAX Tension Reaction per RISA-3D, Factored) N = ] (Numbers of Bolts in Tension) TMax = T,, / N (MAX Tension per Bolt) = 3,500 Ibs per Bolt V = 1,750 Ibs (MAX Shear Reaction per RISA-3D, Factored) n = 1 (Numbers of Bolts in Shear) VMax=Va/n (MAX Shear per Bolt) = 1,750 Ibs per Bolt �Tn = 6,627 Ibs (Bolt Design Tensile Strength, AISC Eq. J3-1) OVn = 3,976 Ibs (Bolt Design Shear Strength, AISC Eq. J3-1) fn, = 8,913 psi (Bolt Required Shear Stress, AISC J3.7) Font = 1.3Fnt - (FnV/ Fnv)fni <_ Fnt = 45,000 psi (Modified Nominal Tensile Stress, AISC Eq. J3-3a) = 38,694 psi ORn = 5,698 Ibs (Bolt Available Tensile Strength, AISC Eq. J3-2) TMax S �Rn OK 61.4% Stressed Combined U-Bolts at Standoff Connections to Mount Face Members ASTM A307, 1/2" 0 Ta = 4,250. Ibs (MAX Tension Reaction per RISA-3D, Factored) N = 4 (Numbers of Bolts in Tension) TMax = Tn / N (MAX Tension per Bolt) 313 Ibs per Bolt Va = 2,500, Ibs (MAX Shear Reaction per RISA-3D, Factored) n = 4 (Numbers of Bolts in Shear) VMax = V. / n (MAX Shear per Bolt) = 625 Ibs per Bolt �Tn = 6,627 Ibs (Bolt Design Tensile Strength, AISC Eq. J3-1) �Vn = 3,976 Ibs (Bolt Design Shear Strength, AISC Eq. J3-1) fir, = 3,183 psi (Bolt Required Shear Stress, AISC J3.7) Font = 1.3Fnt - (Fnt/�Fnv)f, > Fnt = 45,000 psi (Modified Nominal Tensile Stress, AISC Eq. J373a) = 51,426 psi (Thus, Fnt Governs) �Rn = 6,627 Ibs (Bolt Available Tensile Strength, AISC Eq. J3-2) Page 2 of 2 'Gmetic Sk,t. Supporting Member Bolts (TYP.) T V TMax 5 4.7% Stressed Combined