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Report (28) COR NE CORE DNE SO6EOcondONSULLTINGeS51�D. U S A Seattle,Washington 9010.4 Mount Modification Report AT&T — LTE 6C / 5G NR / 4TXRX / 4TX4RX March 13,2019 Site Name TIGARD Site Number PR35 FA# 10094146 PTN # 3898A0K0JB/9898A0K0J1/3898A0K0J0/3898AOKOGY/ 3898A0K0GY Pace# MRWOR037102/MRWOR036935/MRWOR036933/ MRWOR037046/MRWOR037107 Client Velocitel Proposed Carrier AT&T 6975 SOUTHWEST SANDBERG ROAD Site Location TIGARD, OR 97223 45.4215360° N NAD83 122.747378° W NAD83 Structure Type Ballast Frame Structural Usage Ratio 99.1% Overall Result Pass-See Required Recommendations Below Notes Install a minimum of(64) 16x8x8 CMU Blocks between (6)trays per ballast frame.Total CMU weight per ballast tray must be 2048 pounds. Upon reviewing the results of this analysis, it is our opinion that the antenna supporting structure does meet the specified IBC/ASCE/TIA code and minimum design requirements with the modification installed. The modified structure is therefore deemed adequate to support the existing and proposed loading as listed in this report. PRQ,i 6-7`c IN( sio 972PE �i1a/�0 111, 2 -OA/AI T ov RENEWS:fr./or 2°2/ John t. Liiu Oregon Professional Engineer `' "' www.coreoneconsulting.com r r March 13, 2019 Page 1 2 Summary of Contents Introduction Opening Statement Project Description Criteria Conclusion Calculations Appendix A Design Tables & Resources Used Assumptions and Limitations Our structural calculations are completed assuming all information provided to CORE ONE CONSULTING USA is accurate and applicable to this site. For the purposes of calculations, we assume an overall structure condition of"like new" and all members and connections to be free of corrosion and/or structural defects. The structure owner and/or contractor shall verify the structure's condition prior to installation of any proposed equipment. If actual conditions differ from those described in this report CORE ONE CONSULTING USA should be notified immediately to complete a revised evaluation. Our evaluation is completed using standard TIA, AISC, ACI, and ASCE methods and procedures. Our structural results are proprietary and should not be used by others as their own. CORE ONE CONSULTING USA is not responsible for decisions made by others that are or are not based on our supplied assumptions and conclusions. This report is an evaluation of the proposed carriers mount structure only and does not reflect adequacy of the existing rooftop, other mounts, or coax mounting attachments. These elements are assumed to be adequate for the purposes of this analysis and are assumed to have been installed per their manufacturer requirements. (�` Core One Consulting USA t, OR1E E Phone: (778) 805-2166 ❑ N L_l I T I N r' USA www.coreoneconsulting.com March 13, 2019 Page 13 INTRODUCTION At the request of AT&T, CORE ONE CONSULTING USA has performed a Post Modification Mount analysis on the existing antenna mount supporting structure. All supporting documents have been obtained from the client and are assumed to be accurate and applicable to this site. The mount was analyzed using Risa3D version 17.0.2. Supporting Documentation RFDS AT&T RFDS ID:2013032 V1.00, dated 11/13/18 Photos FDH Velocitel Site#PR35, 02/28/19 Previous Analysis Core One Consulting USA Site#PR35, Dated 03/01/19 Analysis Code Requirements Wind Speed 93 mph (3-Second Gust, V,asd)/120 mph (3-Second Gust, Vult) Wind Speed w/ice 30 mph (3-Second Gust) w/ 1" Ice TIA Revision ANSI/TIA-222-G/ASCE 7-10 Adopted IBC 2015 IBC Structure Class II Exposure Category B Topographic Category 1 Calculated Crest Height 0 Site Class D-Stiff Soil Spectral Response Ss=0.975g, S1=0.422 g CONCLUSION Upon reviewing the results of this analysis, it is our opinion that the antenna supporting structure does meet the specified IBC/ASCE/TIA code and minimum design requirements with the modification installed. The modified structure is therefore deemed adequate to support the existing and proposed loading as listed in this report. Alexander Bazeley Structural Engineering Lead I Core One Consulting USA 2875 W Ray Road, Suite 6, Chandler, AZ 85224 (0) 1+(855) 708-2195 1 (M) (518) 892-0471 Alex.bazeley@coreoneconsultants.com 1 info@coreoneconsulting.com Core One Consulting USA F.17:40 COREONE Phone: (778) 805-2166 N r N S A www.coreoneconsulting.com March 13, 2019 Page 14 Existing and Reserved Loading Configuration Mount Rad. Vert. Mount CL(ft) HT(ft) 0/S Qty. Appurtenance Type Carrier (ft) 2 Powerwave P65-17-XLH-RR 1 Kathrein 80010766 3 CCI DPA-65R-BUUUU-H8 3 Kathrein 80010765 2 Powerwave LGP 21401 4 Andrew ETB19GB-12UB 44.0 44.0 0.0 3 Alcatel Lucent 2x40W-07L Ballast AT&T 3 Alcatel Lucent RRH2x60-1900A-4R 3 Alcatel Lucent RRH2x60-850 3 Alcatel Lucent RRH2x40-AWS+RDEM 3 Alcatel Lucent RRH4x25-WCS-4R 3 Raycap FC12-PC6-10E 9 Raycap DC2-48-60-0-9E Equipment to be removed Mount Rad. Vert. Mount CL(ft) HT(ft) 0/S Qty. Appurtenance Type Carrier (ft) 2 Powerwave P65-17-XLH-RR 1 Kathrein 80010766 3 Kathrein 80010765 2 Powerwave LGP 21401 44.0 44.0 0.0 4 Andrew ETB19GB-12UB -- AT&T 3 Alcatel Lucent 2x40W-07L 3 Alcatel Lucent RRH2x60-1900A-4R 3 Alcatel Lucent RRH2x60-850 3 Alcatel Lucent RRH2x40-AWS+RDEM Core One Consulting USA OO R EE Phone: (778) 805-2166 ,, F I N LJ S A www.coreoneconsulting.com March 13, 2019 Page 15 Proposed Loading Configuration Mount Rad. Vert. Mount CL(ft) HT(ft) 0/S Qty. Appurtenance Carrier (ft) Type 6 ACE XXQLH-654L4H8-iVT 3 Nokia B12/B14 Airscale Dualband RRH 44.0 44.0 0.0 3 Nokia AirScale Dual RRH 4T4R B25/66 -- AT&T 3 Nokia AirScale Dual RRH 4T4R B5 160W AHCA Final Loading Configuration Mount Rad. Vert. Mount CL (ft) HT (ft) O/S Qty. Appurtenance Carrier (ft) Type 6 ACE XXQLH-654L4H8-iVT* 3 CCI DPA-65R-BUUUU-H8 3 Nokia B12/B14 Airscale Dualband RRH 3 Nokia AirScale Dual RRH 4T4R B25/66 44.0 44.0 0.03 Nokia AirScale Dual RRH 4T4R B5 Ballast AT&T 160W AHCA 3 Alcatel Lucent RRH4x25-WCS-4R 3 Raycap FC12-PC6-10E 9. Raycap DC2-48-60-0-9E *3'Separation from another antenna Structure Usages Summary Pipe 49.3% Pass Ballast 72.4% Pass Overturning 99.1% Pass RATING= 99.1% Pass Core One Consulting USA cJ R ED _ Phone: (778) 805-2166 N i LJ S A www.coreoneconsulting.com t r Site Name PR35 Client Velocitel Carrier AT&T Date 3/1/2019 Wind Loading Inputs: Design Wind Velocity: 120 ultimate 3-second gust Exposure Category: B Adopted Building Code: ASCE 7-10 Antenna Load Standard: ASCE 7-10 Wind Centerline(ft): 44.00 ft qz= 27.32 Ice Wind 30 Cf= 1.20 Ice Thickness 1 Gh= 1.00 Fst_Ice(psf) 3.95 Fst(psf)= 32.78 Fp= I 0.35 Wind Force Seismic Force Appurtenance Name Total Quantity Weight(lbs) F-Norm(lbs) F-Perp(lbs) F-Norm(lbs) F-Perp(lbs) ACE_XXQLH-654L4H8-IVT 3 94.8 468.3 217.6 32.8 32.8 ACE_XXQLH-654L4H8-IVT 3 94.8 468.3 217.6 32.8 32.8 CCI ANTENNAS_DPA-65R-BUUUU-H8 3 69.0 348.2 204.1 23.9 23.9 Airscale Dual 4T4R B25/66_ 3 86.0 100.6 63.9 29,8 29.8 Airscale Dual 4T4R B12/14_ 3 101.4 100.6 63.9 35.1 35.1 Airscale Dual RRH 4T4R B5 160 W AHCA 3 36.9 35,4 18.2 12.8 12.8 ALCATEL LUCENT_RRH4X25-WCS-4R 3 91.0 104.8 91.1 31.5 31.5 RAYCAP_FC12-PC6-10E 3 20.4 57.3 23.4 7.0 7,0 RAYCAP_DC2-48-60-0-9E 9 16,0 25.4 15.4 5.5 5.5 March 1, 2019 Seismic Loads Latitude and longitude were determined from existing as-builts, AT&T records, and confirmed using GoogleEarth. Design spectral acceleration parameters were optained using NSHMP Hazard,a program by USGS for determining seismic values within the continental US. Input data and program output are provided at the end of this report. Latitude: 45.421536 Longitude: -122.74738 Ss= 0.975 g Site Class: D Fa= 1.11 Occupancy Category: II SMS= 1.082 Importance Factor, I: 1.00 Sos= 0.722 Seismic Design Catagory: D S1= 0.422 g Amplification Factor, ap: 1.0 F"= 1.58 Response Factor, Rp: 2.5 SMi= 0.666 z= 44.0 ft Sol= 0.444 h = 44.0 ft Telecommunication cabinets and radio equipment are non-structural components to be designed under the provisions of ASCE 7-10 chapter 13. (ASCE 7-10 13.3-3) Fp,m;n = 0.3SDSIpWp = 0.216 wP (ASCE 7-10 13.3-1) F = 0.4aPSDSWP / z\ P / 1+2— = 0.346 wP RP h i Use Fp = 0.346 wp �Ip (ASCE 7-10 13.3-2) Fp max = 1.6SDSIPWp = 1.154 wP Core One Consulting USA COREONEPhone: (778)805-2166 i ti . _ . + C USA www.coreoneconsulting.com Y 7;> Z '� �X ,/, ' .... :-Air ,";--/ db.,. 11, 4..m iiik CORE ONE CONSULTIN... APB PR32 Feb 28, 2019 at 6:17 PM PR35.r3d • Z X Prior to any modification contractor must install two additional rails for 16"x8"x8" Hollow CMU's. I • Install Site Pro 1 MAT 18 under proposed rails Roam CORE ONE CONSULTIN... [Proposed Modification APB PR32 Mar 18, 2019 at 11:19 AM PR35.r3d Z x : ? z ^ < i > ° iiip .„,_..._-_, » \ y \ \ ^ �^ . . \ « . � -43 ---- -- \ . . . �w\ m. � �_ : .�?� © . . +w© � �« 1 ; x . _ may ! :y. . « » _ ...... » ^i ` Evenly distribute (q ]&\8"x" ' Hollow Concrete Masonry Units between (6) trays. .4.01.1.00*, CORE ONE CONSUL w. Final Configuration APB PR32 Mar 18, 2019m41d9AM PR35.r3d X OP I.V10 2_404 Envelope Only Solution CORE ONE CONSULTIN... Final Configuration APB PR32 Mar 18, 2019 at 11:24 AM PR35.r3d Section Sets EP2.n L2x2x4 2 X N a Ago d .r, QUO 07�r, 44 .401411 Envelope Only Solution CORE ONE CONSULTIN... Final Configuration APB PR32 Mar 18, 2019 at 11:24 AM PR35.r3d Material Sets I A36 Gr. A55B3 Gr.6 Z X m M q m ..G,.e tii 0 CO 0 i Pdik• fir.tis \ cic p310 . '!/ `;a k. sl., giil rW.,; 44C00 � 6GC'G36 i,k -' A�.3 1X30 P36Gt36 Envelope Only Solution CORE ONE CONSULTIN... Final Configuration APB PR32 Mar 18, 2019 at 11:24 AM PR35.r3d Y Code Check (Env) •' No Calc >1.0 Z x .90-1.0 .75-.90 .50-.75 0.-.50 v a)v 05 � a) 40 .,,, s. 5.444 ice/ •''� •'4 ...e.„/„0„ - Adolio3,11 '.r. 110. 1 11 ,r _. 11 P. iiiiiillidinii. Member Code Checks Displayed(Enveloped) Envelope Only Solution CORE ONE CONSULTIN... Final Configuration APB PR32 Mar 18, 2019 at 11:24 AM PR35.r3d Y Shear Check (Env) -' No Calc >1.0 Z X .90-1.0 75-.90 .50-.75 0.-.50 co coj r=-) r 9J. sP.0,,, t.,i0400 0,',or: . _,1-0,',- ,,,,b,-ok... ‘‘. - _4 ...., A.% 0,,,,,,, „ , - 4 ,.,,..... .”. .0 ...A.... ,.. J"„ J . . _ . . _... ._ Member Shear Checks Displayed(Enveloped) Envelope Only Solution CORE ONE CONSULTIN... Final Configuration APB PR32 Mar 18, 2019 at 11:25 AM PR35.r3d Y Z X a 10 vill011.- 64,. 2 0>*S- N a J ;Piii,N 400,0 ,...,w .,.& ...4.4.10 _, „..0 ,,-- , ,JJ ' J�� Envelope Only Solution CORE ONE CONSULTIN... Final Configuration APB PR32 Mar 18, 2019 at 11:25 AM PR35.r3d I z x 4 \ 4 NOoNSII ,60:4'. 0001 -4- 1:01 0...,di i i Ail I PP)11%,lit..:#..,,a,. 7... 001111.117.0- ,01:-.0111P.-'-'-' ."4" .. 4,:.:.40, Ill ..... -*From 7.100.0.110010.100 0 Member Length(in)Displayed Envelope Only Solution CORE ONE CONSULTIN... Final Configuration APB PR32 Mar 18, 2019 at 11:25 AM PR35.r3d 4 4 A Z X ____ __________ -47.41b 1 -34.51b -161. -911. -47.41b -47.41. 011 187.41. .414 s 44140, 0„410-rv-- ,.. ,A.,>.,6, Alt rolw, ,,,,r4 ,...1•0000fr J 41r All Loads:BLC 1,Self Weight Envelope Only Solution CORE ONE CONSULTIN... Final Configuration APB PR32 Mar 18, 2019 at 11:28 AM PR35.r3d Z X •{ r '�'a3 4ya ato; ,� ♦ e ,Q .;` cq. i.a • • .'�sr32.78ps � • a Ve:. .a o .4";. 00o. a.: '♦ .yr '. .. _, .. z.....:.a .i r.':._.i ai--.:ivicicc'iili� Loads:BLC 2,Wind Load AZI 000 Envelope Only Solution CORE ONE CONSULTIN... Final Configuration APB PR32 Mar 18, 2019 at 11:28 AM PR35.r3d 1 Y .1% Z x -6 61b ••• .. -61.231b .,,N. r r vo,, :K., ,t::,-4e ti r}� r, ''.......4%‘111S404144410:- ...;:::::v***,:::'...t:V.:**:::',,Z1.4:::•1::.:::.:.:::411:4:11:.}...4:::4: moi .°'r � •• .4•/,.: Ib ..i . s;.' >,ti.,?i•,r ., ,F�yF�.:: �' j�. epi, .,..y,.+. r Avy fir.n ',. AIL ?l,F -32.78psf Loads:BLC 3,Wind Load AZI 090 Envelope Only Solution CORE ONE CONSULTIN... Final Configuration APB PR32 Mar 18, 2019 at 11:28 AM PR35.r3d ..-41,.... Z x -13.91b -4.28lb/f� -10.7971b -4.281b/ft -18.0231., -4.281b/ft -4.281b/ft 1111-. .1431., 13.91b �i -4.28Ib -13.91,/ a �1�I1111''\Ci Pq. *a b/ft4`0bI 8.2241., -10.797 oe}0100/ e ¢K 10, .851b/ft A. ;�_ .Sl a N�, 110,t,0001 -11��l �� 1.. Loads:BLC 4,Ice Weight Envelope Only Solution CORE ONE CONSULTIN... Final Configuration APB PR32 Mar 18, 2019 at 11:28 AM PR35.r3d Y :q4. Z X • i :>y r's. r 0 7siri ii � Rn a° �W. r , 6r a.. r •u .4, riaa F* . -J Loads:BLC 5,Wind+Ice Load AZI 000 Envelope Only Solution CORE ONE CONSULTIN... Final Configuration APB PR32 Mar 18, 2019 at 11:28 AM PR35.r3d AY Z x -1*41ba1 Hca '• -121.3lb .�'•,'+.`"•+` ,.s 2.1: •• • .a,. g FgY • o` r` :"..ii...:••••..",,,,,":•.•::- �,�� ✓sem ' ;�.` ,.,ilta::::•\;.;a4.8.14;.:44,44.:-:"...:1. k AN 4,11111), 4k4:::7-..,:a",;s9.';',,t1,-'•%.*...0.0.."4-$.1....t.t4,14%.4...v..4sia„.4%,?: 4 40 :•:•:•,...,............,::::::„.„,:::::,„:.::,.::„... A. i:;1�a,faaK,�,�:.•.. ;a• -3.95psf �.. Loads:BLC 6,Wind+Ice Load AZI 090 Envelope Only.Solution CORE ONE CONSULTIN... Final Configuration APB PR32 Mar 18, 2019 at 11:29 AM PR35.r3d CORE €�, , ,, Company : CORE ONE CONSULTING USA Mar 18, 2019 /Iii: , Designer : APB 11:46 AM U S A Job Number Checked By. Model Name : PR32 Member Primary Data Label I Joint J Joint K Joint Rotate(deg) Section/Shape Type Design List Material Design Rules 1 M1N9 N22 P2.0 I Beam Single Angle A53 Gr. B T .ical .2 M2 i _N71A N20i 45.0 Beam 'Single Angle A53 Gr. B : .;cal 3 M3 N27 N28 P2.0 Beam Single Angle A53 Gr. B T ..cal 4 M4 N25 N26 P2.0 Beam ySingle Angle jA53 Gr. B ?`, s*.cal 5 , M5 N23 N24 P2.0 Beam Single Angle A53 Gr. B T ideal 6 MP1 N31 N29 P2.0 Beam ISinfgle Angle A53 Gr. B T •`" -I 7 MP2 N34 N32 P2.0 Beam Single Angle IA53 Gr. B T .ical 8 MP3 N37 N35 j P2.0 Beam Single Angle A53 Gr. B Typical 9 I MP4 N40 N38 P2.0 Beam Single An le A53 Gr. B Typical 10 i M10 1 � N43 l N41 ; -[ P2.0 Beam Single Angle A53 Gr. B T 11 M11 N44 N42 P2.0 Beam Single Angle A53 Gr. B T .cal 12 M12 N71A L N9 L2x2x4 Beam ISingle Angle A36 Gr.36 T , r 4 13 M13 N8 N10 270 L2x2x4 Beam Single Angle A36 Gr.36 Typical 14 M14 N11 [ N13 L2x2x4 Beam SingleAng le A36 cx.36 ' Typical 15 M15 N12 N14 270 L2x2x4 Beam Single Angle A36 Gr.36 Typical 16 M16 N15 N17 L2x2x4 Beam Single Angle A36 Gr.36 Typical 17 M17 N18 N16 L2x2x4 Beam Single Angle,.A36 Gr.36 , Typical 18 M18 N19 N21 L L2x2x4 Beam Single Angle,. A36 Gr.36 Typical 19 M19 N20 N22 270 L2x2x4 Beam Single Angle A36 Gr 36 Typical 20 ! M20 N45 N47 1 I L2x2x4 Beam Single Angle A36 Gr 36 Typical 21 M21 N46 N48270 L2x2x4 Beam Single Angle A36 Gr.36 1 Typical 22 M22 N49 I N51 I L2x2x4 Beam Single Angle,A36 Gr.36 Typical 23 M23 f N52 I N50 L2x2x4 Beam Single An_gle A36 Gr.36 Typical -i Hot Rolled Steel Section Sets Label I Shape Type Design List Material Design Rules A[n2] lyy[in4] Izz[in4] J[in4] 1 P2.0 PIPE 2.0 r Beam Single Angle A53 Gr. B Typical 1.02 .627 .627 1.25 2 jl L2x2x4 I L2x2x4 ( ;_Beam Single Angle A36 Gr.36 Typical .944 .346 1 .346 .021 Hot Rolled Steel Design Parameters Label Shape Length[in] Lbyy[in] r Lbzz[i[ Lcomp top[in]Lcom_gbot[in]L-torqu... yy Kzz Cb Function 1 M1 P2.0 144 Lbyy 1 Lateral 2 P2 144 ' Lbyy 1 I Lateral 3 M3 P2.0 144 Lbyy Lateral I'' 4 M4 P2.0 127.562 1 Lbyy Lateral 5 M5 P2.0 127.562 Lbyy Lateral 6 MP1 - P2.0 � 144. Lbyy Lateral 7 MP2 P2.0 144 LbyyLateral 8 MP3 P2.0 144 Lbyy l - Lateral 9 MP4 P2.0 144 .0 M10Lbyy P2.0 1.70.937 Lbyy_ Lateral 11 M11 P2.0 70.937 Lbyy Lateral 12 M12 L2x2x4 84 .001 .001 .001 .001 .001 Lateral13 M13 L2x2x4 84 .001 .001 .001 .001 .001 Lateral 14 M14 L2x2x4 84 { .001 .001 .001 .001 .001 Lateral 15 M15 L2x2x4 84 I .001 .001 .001 .001 .001 Lateral 16 L M16 L2x2x4_-_ 84 .001 > .001 .001 .001 .001 Lateral 17 M17 L2x2x4 84 .001 .001 .001 .001 .001 Lateral RISA-3D Version 17.0.2 [C:\...\...\Desktop\Projects\2019\February\To Do\PR35\Mod\PR35.r3d] Page 1 CORE(--)N1-...-7- Company : CORE ONE CONSULTING USA Mar 18,2019 - L.- Designer : APB , 11:46 AM U s A Job Number : Checked By Model Name : PR32 Hot Rolled Steel Design Parameters (Continued) Label Shape Length[in] Lbyy[ril Lbzzlin] Lcomp top[inl,Lcomp botfin L-torgu... Kyy Kzz Cb Function 18 M18 L L2x2x4 1 84 .001 ' .001 .001I .001 001. , Lateral 19 M19 I L2x2x4 84 .001 .001 .001 .001 ' .001 Lateral _, 20 M20 1 L2x2x4 84 .001 .001 .001 .001 .001 Lateral 21 M21 L2x2x4 , 84 .001 .001 .001 .001 .001 Lateral 22 M22 L2x2x4 84 .001 .001 .001 1 .001 .001 1 Lateral 23 M23 L2x2x4 84 _I .001 .001 .001 , .001 .001 t Lateral Material Takeoff Material Size _______ Pieces Length[in] Weight[LB1 1 Hot Rolled Steel 2 A36 Gr.36 L2x2x4 2 1-2 1008 269.8 3 A53 Gr. B PIPE 2.0 11 1405 406.4 LA ± Total HR Steel - 1 ' 2V-', 2413 676.2 Basic Load Cases BLC Description Category X GravityY Gravity Z Gravity Joint Point Distribu...Area(M... SurfacflateNV all) 1 Self Weight 1 DL -1 r 1 4 2 Wind Load AZI 000, WLZ 14 1 3 Wind Load AZI 090 WLX I 14 1 I 4 Ice Weight OL1 ' 14 ' 23 5 Wind+ Ice Load... OL2 14 1 1 6 Wind+Ice Load... OL3 14 1 7 I Service Live 1 LL 8 IBLC 2 Transient... None - 1 11 i 1 9 BLC 3 Transient... None 20 10 BLC 5 Transient... None I 11 [ 11 BLC 6 Transient... None 20 , Load Combinations Description S...P...S...B...Fa..B...Fa..B...Fa..B...Fa..B...Fa..B..,Fa..B..Fa..B..Fa..B...Fa..B...Fa... ' 1 1.0D WEISE 1 1 I f 1 2 1D+0.6W AZI 000 - iiiiill- 1 - .61 3 1D +0.6W AZI 030 Y..y DL 1 ... .52 ... .3 4 1D +0.6W AZI 060 Y.•Y al_ 1 ,... .3 ... .52 5 1D +0.6W AZI 090 y..y DL 1 , 6 1D+0.6W AZI 120 Y.•Y IL 1 ... -.3... .52 7 1D +0.6W AZI 150 Y...y DL 1 ... -.52'... 3 • 8 1D+0.6W AZI 180 Y,.y DLII... -.6 j L 1 9 1D +0.6W AZI 210 r_••Y DL 1 ... .52... -.3 1 , 1 10 1D +0.6VV AZI 240 Y..y !bi.. 1 ... ,3... .52 . _ 11 1D +0.6W AZI 270 Y...y DL 1 ••• -.8 1 1 12 1D+0.6W AZI 300 Y..y DL 1 ... .3 ... .52 7 13 1D +0.6W AZI 330 'Y..y DL 1 ... .52 ... -.3 I 14 0.6D + 0.6W AZ1000 Y4Y Li.6 ••• .6 L ' 15 0.6D + 0.6W AZI 030 Y..Y DL .6 ... .52 ... .3 I •1 16 , 0.6D + 0.6W AZI 060 IY.•Y ,r4:4,.- .3 ..• * , V. 177 0.6D + 0.6W AZI 090 y.i y DL .6 ••• .6 I RISA-3D Version 17.0.2 [C:\...\...\Desktop\Projects\2019\February\To Do\PR35\M od\PR35.r3d] Page 2 • Company : CORECAM ,iiiki � --- Designer CORE ONE CONSULTING USA Mar 18 019 U S A Job Number Checked By. Model Name : PR32 Load Combinations (Continued) Description S..P...S_...B...Fa..B...Fa..B...Fa..B...Fa..B...Fa..B...Fa..B...Fa..B..Fa..B...Fa..B...Fa... 18 0.6D+0.6W AZI 120 Y..�Y IL 61... -.31_.. .52 + 19 0.6D + 0.6W AZI 150 Y..Y DL .6 ... -.52... .3 20 0.6D+ 0.6W AZ1 180 Y...y IL ,6 .,. _.6 21 0.6D+ 0.6W AZI 210 Y..Y 22 0.6D + 0.6W AZI 240 -- Y..y DL .6 .._ 3... .52 1 1 is 23 0.6D+ 0.6W AZI 270 Y..y DL •g 6 24 0.6D+ 0.6W AZI 300 ®Y DL .6 ,.. 3 ... -.52 F 25 0.6D + 0.6W AZI 330 Y..Y DL ,6 ... 52 ... - 26 1 1D+1Di - Y..Y IL 1 0. 1 3 27 1D + 1Di + 1Wi AZ!000 Y..Y DL 1 0.. 1 1 28 - 1D + 1Di + 1WiAZ1030 Y..Y DL 1 0:: 1 ... .8.....1.5 29 1D+ 1Di + 1Wi AZI 060 Y..Y DL 1 0.. 1 ... .5 ... .8...; 30 1D + 1 Di+ 1 W i Z 1090 Y..Y' DL 1 0... 1 ... 1 L. 1 31 1D+1Di + 1WiAZI 120 Y...Y DL 1 0.. 1 .. -.5 . .8... 1 32 1D+ 1Di+ 1WiAZI 150 Y...Y IL 1 0.. 1 . ... .5 33 1D+1Di + 1WiZ1180 Y..,Y DLl 1 'O_.11 Z ... - 1. ... -. < ( 1 34 1D+ 1Di+ 1Wi I210 Y•••Y L 1 0•. 1 5 35 1D + 1Di + 1WiAZI240 Y. y DL 1 0.. 1 ... 5 - 36 1D+ 1Di+ 1Wi AZI 270 Y..}Y. 1 0..� 1 .. -1 1- -1 } 37 10 + 1Di + 1WiAZI300 Y. Y DL 1 0.. 1 5 ' 38 Y D 1 . 1 10+ 1Di + 1WiZ1330 Y.rY L 1 0.4 8 .... -.5C I 1 L I 39 1D + 1.5L+ 1WL (0 mphAZ1 000 Y.- DL LL 1.5 .. 1 40 l 1D+ 1.5L+ 1WL(30mpjZ1030 Y:..YI NL 1LL15 .. .18 1.. r 7 1- + 41 1 1D + 1.5L+ 1 WL( 5 30 mph)AZI 060 Y••Y �L 1 LL 1 5 ••• .5 ... 8... 42 1D+ 1.5L+ 1WL(30 mp 30mph)AZI 090 Y.•Y L 1 LL 1.5 .. 43 1D + 1.5L+ 1WL(30 mph)AZI 120 Y..Y 1DL 1 LL 1.5 ... .5i... .8. 44 1 D+ 1.5L+ 1WL(30 mph)Z1150 Y..Y 01_11 LL 1.5 .... ... ,5 1 I l f mph)AZI 180 Y..Y 1 LL 46 1D+ 1.5L+ 1WL 30 mph)AZI 210 Y•• DL 1.5. .. -1 ' 47 1D + 1.5L+ 1WL( 0 mp )ZI 240 Y..Y DL 1 LL 1.5 ... (3mph)_AZI Y 1 LL 5, 48 1D+ 1.5L+ 1WL 30 mh AZI 270 Y•• IL 15 .. _1, 7 1 49 10 + 1.5L+ 1WL(30 mph)AZI 300 Y.! f 1 P ) Y DL1 LL 15 .5 - 1_- 50 1D+ 1.5L+ 1WL(30 mph)AZI 330 Y...Y L. 1 LL 1.5... :8 ....1 .5 fi 1 51 ( 52 1.0+0.2Sds D+ 1 E AZI 030 Y.•Y 1 E... 1 X53 (1.0+0.2Sds)D + 1E AZI 060 Y..y DL 1...:E._ 5�E...8... 1 (1.0+0.2Sds)D54 55 1 E AZI 120 Y.., f 1 56 ( ) 090Y .L+ SIE...8... Y DL11 E .. { till (1.0+0.2Sds)D 1 E AZI 150 1Y:.Y �oL 1 E.:.-... E.. ,51 I_ 57 (1.0+0.2Sds)D + 1 E AZI 180 Y..Y 1DL 1....'E...,-1 58 (1.0+0.2Sds)D + 1E AZI 210 59 (1.0+0.2Sds)D + 1E AZI 240 Y•.Y DL 1 .••E... 5 E -.. .' 60 I E -1 1 61 AlX1.0+0.2Sds D + 1E AZI 300 Y..Y DL11 ...E... .5 E -....I 62 (1.0+0.2Sds)D + 1 E AZI 330_..- YM, DL El....,IE...,.8...E.._•5� 630 6-0.2Sds)D + 1 E AZI 000 Y...y DL.4...E 64 0.6-0.2Sds)D+;1 E AZ1 030 LY..Y L 4 IE....8...IE..1.5 1 65 + .-( Y DL 4 E E...8... 67 ---0.6-0.2Sds D + 1 E AZI 120 Y..'Y �L 4 E . 1 t Sds D + 1 E AZI 060 Y• J - I J + ID 66 0.6-0.2Sds D+ 1 E AZI 090 1Y...Y !DL a...�E..._ 5 E...8..� _ 68 (0.6-0.2Sds)D+ 1E Z1 150 Y..Y` -DLI 4 IE IE.,.5 C f l 69 (0.6-0.2Sds)D + 1 E AZI 180 Y..,Y DL14...IE..,-1 L RISA-3D Version 17.0.2 [C:\...\...\Desktop\Projects\2019\February\To Do\PR35\Mod\PR35.r3d] Page 3 mr" CORE IN12-- Company ,, Desigpanenry r. ACPOBRE ONE CONSULTING USA Mar 18, 2019 • ,1,,,,,., 11:46 AM u s A Job Number . Checked By Model Name : PR32 Load Combinations (Continued) Description S .P .S .B..Fa..B .Fa..B. Fa B Fa. B. Fa.B .Fa B. Fa B ..Fa B. Fa.B .Fa. . 70 A0.6-0.2Sds)D 4' 1E AZI 210 tr.VT DL.4...E...-.... E..-.5f 71 (0.6-0.2Sds)D + 1 E AZI 240 i - 72 /9.6-0.2Sds)D+ IEAZI 270 Y..)1 IL.4.-- E.-1 1 73 (0.6-0.2Sds)D+ lE AZI 300 74 j9.6-0.2Sds)D+ 1E AZI 330 Iy..y IL.4..E....8...E5 JJ I I - I I21 Joint Coordinates and Temperatures Label ) 11•1] Y[in] Z[in] Temp[F] Detach From Dup... 1 N69A 198 154 -43 T 0 I 2 N70A 198 154 120.3125 0 3 N71A 24 0 96.3125 0 4 N72A -54 154 120.3125 0 5 N73A 198 0 -43 0 6 N74A 198 0 120.3125 0 7 N75 -54 0 120.3125 0 8 N8 42 0 i 9E3125 0 9 N9 24 0 12.3125 0 10 N10 42 i 0 12.3125 0 11 N11 75 0 96.3125 0 12 N12 L 93 0 96.3125 0 13 N13 I 75 0 12.3125 0 14 N14 93 0 123125 0 15 N15 99 0 96.3125 0 16 N16 T 117 0 9E3125 0 17 N17 99 0 12.3125 0 18 N18 117 0 12.3125 0 19 N19 150 0 96.3125 0 20 - N20 J 168 0 96.3125 0 21 N21 150 0 12.3125 0 22 N22 168 0 12.3125 0 23 N23 138 96 96.3125 0 24 N24 1 138 0 12.3125 0 25 N25 54 96 96.3125 0 26 I N26 54 I 0 12.3125 0 _ 27 N27 24 96 96.3125 0 28± N28 168 96 - 96.3125 0 29 N29 27 0 96.3125 0 30 N30 27 96 96.3125 0 31 N31 27 144 96.3125 0 32 N32 73 0 96.3125 i 0 33 N33 73 96 96.3125 0 34 i N34 73 144 f 96.3125 0 35 N35 119 0 96.3125 0 36 N36 119 96 9E3125 0 37 N37 119 144 96.3125 0 38 N38 165 0 1- 96.3125 0 39 N39 165 96 96.3125 0 40 N40 165 144 96.3125 0 41 N41 73 60 96.3125 0 42 i N42 119 60 96.3125 0 RISA-3D Version 17.0.2 [C:\...\...\Desktop\Projects\2019\February\To Do\PR35\Mod\PR35.r3d] Page 4 I CORE a Company : CORE ONE CONSULTING USA Mar 18,2019 Designer APB 11:46 AM U S A Job Number Checked By. Model Name : PR32 Joint Coordinates and Temperatures (Continued) Label X[n] YJ]n] Z[in] Temp[F] Detach From Diap . 43 N43 27 6 96.3125 0 44 N44 165 6 96.3125 ! 0 I 45 N45 53 0 96.3125 0 46 N46 71 0 96.3125 0 47 N47 53 0 12.3125 0 F48 N48 71 0 12.3125 0 49 N49 121 0_--- 96.3125 I- --0 50 N50 139 0 96.3125 0 51 N51 121 0 12.3125 0 52 N52 139 0 12.3125 0 Joint Boundary Conditions Joint Label X[k/ink YLk/in] Z[k/inL X Rot.jk-ft/rad] Y Rot.[k-ft/rad] Z Rot.jk-ft/rad] 1 1 N69A 2 N70A 3 N71A Reaction Reaction Reaction 4 _L N72A 5 N73A 6 N74A 7 N75 8 N8 Reaction Reaction Reaction 9 N9 Reaction Reaction Reaction 10 N10 Reaction Reaction Reaction 11 N11 Reaction Reaction Reaction 12N12 Reaction Reaction Reaction 13 N13 Reaction Reaction Reaction 14 N14 Reaction Reaction Reaction i 15 N15 Reaction Reaction Reaction 16 N - 16 Reaction Reaction –__Reaction 17 N17 Reaction Reaction Reaction 18 N18 Reaction Reaction Reaction 1 19 N19 Reaction Reaction Reaction 20 N20 Reaction Reaction Reaction 21 N21 Reaction Reaction Reaction 22 N22 Reaction } _Reaction � Reaction 23 1 N23 24 N24 - 25 -__ N25 26 - N26 - - 27 N27 28 N28 L 29 N29 30 N30 _ - 31 N31 32 N32 33 N33 34 N34 - 35 N35 36 N36 37 N37 RISA-3D Version 17.0.2 [C:\...\...\Desktop\Projects\2019\February\To Do\PR35\Mod\PR35.r3d] Page 5 , . Company : CORE ONE CONSULTING USA Mar 18,2019 11:46 AM i L.J, -A JDoebsTuemrber : APB Checked By Model Name : PR32 Joint Boundary Conditions (Continued) Joint Label X tkkli Y[k/in] Z[k/in] X Rot.[k-ft/radj Y Rotrk-ft/radi Z Rot.[k-ft/rad] 38 N38 39 N39 40 N40 1_ 41 N41 42 N42 -I 43J N43 I 44 N44 II 45 N45 Reaction Reaction Reaction 46 N46 Reaction Reaction Reaction 47 N47 Reaction Reaction Reaction 48 N48 Reaction Reaction Reaction 1 49 N49 Reaction Reaction Reaction 50 ' N50 Reaction Reaction Reaction 51 N51 Reaction Reaction Reaction 52 N52 Reaction Reaction Reaction Member Distributed Loads (BLC 4:Ice Weight) Member Label Direction Start MagnitudelVft,F,psf] End Magnitude[113/1..Start Location[in,%J_End Locaton[in,%1 '- .1 M1 Y -4.28 -4.28 0 %100 1 2 _L M2 Y -428 -4.28 0 %100 3 M3 V -4.28 -4.28 0 %100 4 M4 Y -4.28 -4.28 0 %100 5 M5 Y -4.28 -4.28 0 %100 6 MP1 Y T. -4.28 -4.28 r 0 %100 1 1 7 MP2 Y -4.28 -4.28 0 %100 1 8 MP3 Y -4.28 -4.28 0 I %100 9 MP4 Y - -} -4.28 -4.28 0 %100 10 M10 Y -4.28 -4.28 0 %100 11 M11 Y -4.28 -4.28 0 %100 12 M12 Y -4.85 -4.85 0 %100 13 M13 Y -4.85 -4.85 0 %100 14 M14 Y -4.85 -4.85 0 %100 15 M15 Y -4.85 -4.85 0 %100 16 M16 Y -4.85 -4.85 0 %100 17 M17 Y -4.85 -4.85 0 %100 18 M18 Y -4.85 -4.85 0 %100 19 M19 Y -4.85 -4.85 0 %100 20 M20 Y -4.85 -4.85 0 %100 21 M21 Y -4.85 -4.85 0 %100 22 M22 Y -4.85 -4.e 0 %100 23 M23 Y -4.85 -4.85 0 %100 Member Distributed Loads (BLC 8:BLC 2 Transient Area Loads) Member Label Direction Start MAgnituderlb/ft,F,psf] End Magnitudep/f..Start Location[in,N End Locaton[in,%1_ 1 M1 I Z -6.488 -6.488 0 144 2 M2 L Z -6.488 -6.488 0 144 3 M3 Z -6.488 -6.488 0 144 4 M4 ' Z -4.882 -4.882 0 127.562 5 M5 Z -4.882 -4.882 0 1_ 127.562 I 6 MP1 Z , -6.488 -6.488 0 I 144 _1 RISA-3D Version 17.0.2 [CA...\...1Desktop\Projects\2019\February\To Do\PR35\Mod\PR35.r3d] Page 6 / 1: CORC V Company : CORE ONE CONSULTING USA Mar 18,2019 C Designer APB 11:46 AM USA Job Number : Checked By. Model Name : PR32 Member Distributed Loads (BLC 8:BLC 2 Transient Area Loads) (Continued) Member Label Direction Start Magnitude[Ib/ft,F,psfL End Magnitude[lbf..Start Location[in,%] End Location[in%] 7 MP2 Z -6.488 -6.488 0 144 8 --- MP3 [ Z -6.488 -6.488 0 144 9 MP4 Z -6.488 -6.488 0 144 10 M10 Z -6.488 -6.488 0 70.937 11 _,- M11 Z -__ -6.488 -6.488 0 1 70.937 Member Distributed Loads (BLC 9:BLC 3 Transient Area Loads) Member Label Direction Start Magnitude[Ib/ft,F,pst] End Magnitudellb/F..StartLocation[in,%o] End Location[in,%] 1 M4 X -6.488 -6.488 0 1 127.562 2 M5 - _- -_ X i__- -6.488_. I -6.488 0.__ 127.562 ---' 3 MP1 X -6.488 -6.488 0 144 4 MP2 X -6.488 -6.488 0 144 5 MP3 X -6.488 -6.488 0 144 6 MP4 X -6.488 -6.488 ' _ -0 1.4.4 7 M10 X -4.939 -4.939 0 70.937 8 M11 X -4.939 -4.939 0 70.937 9 M12 X -5.463 -5.463 0 84 10 M13 X I -5.463 -5.463, 0 1 84 11 M14 X -5.463 -5.463 0 84 11 12 M15 X -5.463 -5.463`' 0 1 84 13 M16 X -5.463 -5.463 0 84 14 M17 X -5.463 -5.463 . _L 0 84 15 16 M18 X -5.463 -5.463 0 84 M19 X -5.463 -5.463 0 84 17 M20 X -5.463 -5.463 0 84 18 L M21 X -5.463 -5.463 0 i 84 - 19 M22 X -5.463 -5A63 0 1 84 20 L M23 X -5.463 -5.463 j 0 84 1 Member Distributed Loads (BLC 10 :BLC 5 Transient Area Loads) Member Label Direction Start Magnitude[lb/ft,F,psfl End MagnitudeLlb/F..Start Location[in,%o End Locationfin%] 1 M1 Z -.782 -.782 0 144 2 ;M2 Z -.782 I .782 0 144 3 M3 Z -.782 -.782 0 144 4 M4 j Z L -.588_' -.588 0 127.562 5 M5 Z -.588 I -.588 0 127.562 1 6 MP1 j Z -.782 -.782 0 T 144 7 MP2 Z -.782 -.782 _ 0 144 8 MP3 Z -.782 - -.782 j 0 144 - 9 MP4 Z -.782 -.782 I 0 144 10 M10 Z - ,-.782 - -. -.782 70.937 -.- 11 M11 Z -.782 -.782 0 70.937 Member Distributed Loads (BLC 11 :BLC 6 Transient Area Loads) Member Label Direction Start Magnitu[lb/ft,F,psf] End Ma_g itude[lb/f..Start Locationjn,%o] End Location[in,%] 1 M4 X -.782 -.782 0 127.562 2 M5 i_ -.782 0 1 127.562 _ X -.782 3 MP1 X I -.782 -.782 0_ I 144 4 MP2 X -.782 -.782 i 0 1 144 5 MP3 X -.782 -.782 0 144 RISA-3D Version 17.0.2 [C:\...\...\Desktop\Projects\2019\February\To Do\PR35\Mod\PR35.r3d] Page 7 Tik,4 C 0 R E(" 1C: 1 Company : CORE ONE CONSULTING USA Mar 18,2019 Designer APB 11:46 AM u s A Job Number Checked By. Model Name : PR32 Member Distributed Loads (BLC 11 :BLC 6 Transient Area Loads) (Continued) Member Label Direction Start Ma_gnitudejlb/ft,F,psf] End Magnitudejjb/f..Start Locationfin,°/1 End Locationjin,%1l 6 MP4 X -.782 -.782 0 144 1 7M10 X -.595 -.595 0 i 70.937 8 M11 X -.595 -.595 0 l -_70.937 9 M12 X -.658 -.658 0 - 84 10 M13 X -.658 -.658 0 84 11 M14 X -.658 -.658 0 84 12 M15 j X -.658 -.658 0 84 13 M16 X -.658 -.658 0 84 14 M17 X -.658 -.658 84 15 M18 X -.658 -.658 0 84 16— M19 X -.658 -.658 0 84 17 M20 X -.658 -.658 0 84 18. M21 X r -.658 -.658 - 0 84 19 M22 X -.658 -.658 084 20 M23 - X -.658 1- -.658 0 84 Member Area Loads (BLC 2: Wind Load AZI 000) Joint A Joint B Joint C Joint D Direction Distribution Magnitude[psf] 1 N75 N74A 1 N70A N72A Z Open Structure -32.78 Member Area Loads (BLC 3: Wind Load AZI 090) Joint A Joint B Joint C Joint D Direction Distribution Magnitude[psf] 1 N74A N73A j N69A N70A X Open Structure -32.78 Member Area Loads (BLC 5: Wind+Ice Load AZI 000) Joint A _ Joint B Joint C Joint D Direction Distribution Magnitude s 1 N75 J N74A j N70A N72A Z 1-Open Structure 1 -3.95 Member Area Loads (BLC 6: Wind+Ice Load AZI 090) Joint A Joint B Joint C Joint D Direction Distribution Magnitude[psf[ 1 N74A N73A N69A 1 N70A X Open Structure 1 -3.95 Member Point Loads (BLC 1 : Self Weight) Member Label Direction M_gnitude[Ib,k-ft] Location[in,% 1 MP1 Y -47.4 6 2 MP4 1( -47.4 6 3 ' MP2 Y -34.5 6 4 MP4 Y -43 54 5 MP4 Y -50.7 54 6 MP1 Y -8 54 7 MP2 Y -45.5 54 8lMP1 ( Y I -47.4 102 9MP4 Y -47.4 102 10,- -- MP2 --- - - Y - - _ -34.5_ 1--__ --- 102 11 MP4 Y -43 54 MP4 Y -50.7 54 13 MP1 Y -8 54 RISA-3D Version 17.0.2 [C:\...\...\Desktop\Projects\2019\February\To Do\PR35\Mod\PR35.r3d] Page 8 Co CORE ,— Des gner CORE ONE CONSULTING USA Mar 11:46 AM 19 ., u S A Job Number : Checked By. Model Name : PR32 Member Point Loads (BLC 1 : Self Weight) (Continued) Member Labe I Direction Magnitude[Ib,k-ft] Location[in,%] 14 1 MP2 Y -455_ 54 I Member Point Loads (BLC 2: Wind Load AZ/000) Member Label Direction Magnitude[Ib,k-ft] Location[in,%] 1 MP1 Z -140.503 6 2 MP4 Z -140.503 _.._ 6 3 MP2 Z -104.454 6 4 ) MP4 Z -30.183 54 5 - MP4 Z -30.183 54 6 MPI Z -10.523 54 7 MP2 Z -31.429 54 8 MP1 Z - -140.503 102 9 MP4 Z .1.40.503 102 10 I MP2 Z 104:454 102 11 MP4 Z -30.183 54 12 MP4 Z -30.183 54 13 MP1 Z -10.523 54 14 MP2 Z -31.429 54 Member Point Loads (BLC 3: Wind LoadAZ/090) Member Label Direction Magnitude[Ib,k-ft] Location[in,%]_ 1 MP1 X -65.286 6 2 MP4 X _-65,286 6 - --- 6 3 T _MP2 X -61.23 6 4 MP4 X 19.157 54 5 MP4 X -19.157 54 6 - MP1 X —_ - -5.88.---- 54 - -27.344 7 MP2 X 54-- 8 MP1 X i 65.286 102 9 MP4 X -65.286 102 10 MP2 I X -61.23 102 11 T MP4 X -19.157 54 L 12 MP4 X -19.157 54 13 MPI X -5.88 54 14 MP2 X )- -27.344 54 J Member Point Loads (BLC 4: Ice Weight) Member Label Direction Magnitude[Ib,k-ft] LocationLn,%o] L 1 MP1 Y -13.9 6 7 2 MP4 _ . . Y -- - -13.9 _ "'"-'4' 6 . 3 MP2 Y -10.797 6 4 MP4 Y -12.056 54 5 MP4 Y -12.056 54 6 MP1 Y -9.012 54 7 MP2 Y -11.571 54 8 I MP1 Y -13.9 102 9 MP4 Y -13.9 102 10 MP2 Y -10.797 102 11 MP4 Y -12.056 54 12 MP4 Y -12.056 1 - 54 RISA-3D Version 17.0.2 [C:\...\...\Desktop\Projects\2019\February\To Do\PR35\Mod\PR35.r3d] Page 9 I. vORE[ -�� ' m Designer : APBEONE CONSULTING USA Mar18, 2019 11:�� AM U S A Job Number : Checked By. Model Name : PR32 Member Point Loads (BLC 4: Ice Weight) (Continued) Member Label Direction Magnitude[L3,k-ft] Location[in,%] 13 MP1 1 Y -9.012 54 14 MP2 1 Y -11.571 I, 54 Member Point Loads (BLC 5: Wind+ Ice Load AZI 000) Member Label Direction Magnitude fjb,k ft] Location[in,O ] 1 MP1 Z -28.224 6 1 2 MP4 Z -28.224 6 3 MP2 Z -20.982 6 4 MP4 Z -6.063 54 5 MP4 Z -6.063 54 6 MPI Z -2.135 54 7 MP2 Z -6.313 54 8_ MP1 1 Z -28.224 - - - i - — 102 9 - MP4 Z -28.224 102 10 MP2 Z -20.982 102 11 MP4 Z -6.063 54 12 MP4 Z -6.063 54 13 MP1 Z -2.135 54 MP2 L14 ! Z -6.313 - -- � 54 Member Point Loads (BLC 6: Wind+ Ice Load AZI 090) Member Label Direction Magnitude[Ib,k-ft] Location[in,%] 1 MP1 X -13.114 6 2 -__ MP4 X -13.114 6 3 MP2 X -12.3 6 4 MP4 X 7 -3.848 54 5 MP4 X -3.848 54 6 MP1 X -1.095 54 7 MP2 X -5.493 54 i 8 - - MP1 - X -13.114 -- _ - 102 9 MP4 X ! -13.114 102 10 MP2 X -12.3 102 1 11 MP4 X -3.848 54 12 L MP4 X -3.848 54 13 MP1 X -1.095 54 14 MP2 X `5.493_ I 54 Envelope Joint Displacements Joint X[in] LC Y[in] LC Z[in] LC X Rotation ILC Y Rotation [...LC Z Rotation[...LC 1 N69A max 0 74 0 741 0 74 0 741 0 74 0 74 2 0 1 0 0 1 0 r1 74 0 74 11_- Amin 0 � 1 0 1 3 N70A max 0 74 0 0 74 0 74 0 74 4 min 0 1 0 1 0 1 0 1 0 1 0 1 5 N71A max' 6 min 0 14i 0 14 0 14 -3.54e-03 39 -1.45e-04 39 56e-04 45 4e-04 42 . -4.824e-04 48 78 N72A max0 1 0 1 0 1 0 1 74 74 74 74 0 1 0 1 04 i 4 9 N73A max 0 74 0 74 0 74 0 74 0 74 0 74 10 min 1 0 1 0 1 1 0 , 1 RISA-3D Version 17.0.2 [C:\...\...\Desktop\Projects\2019\February\To Do\PR35\Mod\PR35.r3d] Page 10 . . Com an : CORE ONE CONSULTING USA Mar 18,2019 ORES �� . . Designer : APB Mar .,..... U S A Job Number Checked By. Model Name : PR32 Envelope Joint Displacements (Continued) Joint X[n] LC Y[in] LC Z[in] LC X Rotation L LC Y Rotation j,.LC Z Rotation[...LC 11 N74A max 0 74 [ 0 74 0 174 1 0 74 0 74 j 0 74 12 min 0 1 0 1 0 1 0 1 0 1 0 1 13 N75 max 0 74 0 74 0 74 0 74 0 74 0 74 14 ' min 0 1 0 1 0 1 0 1 0 1 0 1 15 N8 max 0 74 0 74 0 74 3.631e-03 45 5.8e-05 39 2.1e-04 48 16 min 0 , 1.3 17 N9 max.__. 0 74 '-- 0 -_-! 1 0 1 -3.3185-o3 39 -5.818e-05 45 -1.3975-04 42 0 74 0 74 1.911e-03 27 2.426e-05 49 2.846e-05 44 18 min 0__ 1 0 1 0 1 3.631e-04 25 2.409e-05 43_ -3.57e-05 50 19 N10 max 0 74 0 74 0 74 1.911e-03 27 4.64e-05 43 7.045e-05 50 20 min 0 1 L 0 1 j 0 1 3.631e-04 25 -4.676e-05 49 -6.644e-05 44 21 N11 max 0 74 0 74 0 74 2.29e-03 45 1.167e-05 45 7.161e-05 47 22 min 0 1 0 1 0 1 -1.979e-03 39 -1.105e-05 4 39 -4.97.5-05 41 23 24 N12 max 0 1 0 1 01 74 4._T- 74 -1.07e-03 45 3.092e-07 39 7.574e-06 41 762e-03 39 -4.201e-07 45 9.347e-06 47 25 N13 max 0 74 0 74 0 74 1.897e-03 27 2.142e-06 50 4.457e-07 44 26 ; min 0 1 0 1 0 1 3.318e-04 14 1 -2.138e-06_44 -2.183e-06 38 27 N14 max 0 74 0 74 0 74 1.884e-03 27 2.012e-061 452.356e-06; 38 28 min 0 1 0 1 0 .__ 1` 2.957e-04 14 -2.013e-06 39 4.889e-07 19 29 N15 max 30 �'mm 0 74 0 0 1 0 _ 74 ' 0 74 1.996e-03 45 2.527e-07 46 9.502e-06 43 1 01 9e-03 31 N16 j max 0 74 0 74 0 � 74 1.7� 39 -1.6715-07�40 -9.65e-06 49 76e 03( _ .._- 45 9.741 e-06 1 39 6.35e-05 49 32 ! min 0 1 0 I 1 0 1 -1.471e-03 39 -1.036e-05 45 -7.034e-05 43 33 N17 1 max 0 74 0 74 ! 0 74 1.88e-03 27 '2 017e-06 39 -4.738e-07 21 34 min 0 1 0 1 0 1 2.836e-04 14 -2.015e-06 45 -2.361e-06 27 35 N18 'max 0 74 0 74 0 74 1.867e-03 27 2.152e-06 46 2.393e-06 40 36 [ mm 0 1 0 1 0 1 2.475e-04 14 -2.162e-06 6 N 19 0925 04 48 -6.483e-07 46 37 max 0 74 0 74 0 74 4.092e-03 45 8.7995 05 4 38 - min0 [ 1 0 1 0 1 3.784e-03 39 -8.726e-05 39 -2.51e-04 42 39 N20 max 0 74 0 , 74 0 74 5.225e-03 45 2219e-04 39 6.274e-04 42 40 I min 0 1 1 0 11 ---- 0 1 -4.915e-03 39 -2.242e-04 45 -1.3030-04148 41 N21 max 0 174 0 74 0 74 1.852e-03 27 4.722e-05 41 7.705e-05 46 42 min 0 i 1 0 1 0 1 2.053e-04 14 -4.66e-05 47 -8-141e-05 40 43 N22 max 0 74 0 74 0 74 1.852e-03_27 12.419e-05 47 4.093e-05 40 44 1 min 0 1 0 - 1 1 0 �1 2.053e-04-14 -2.448e-05 141 -3.33e-05 46 45 N23 max .206 48 .05 39 .071 45 2.297e-03 45 8.966e-03 39 1.317e-03' 50 46 min -.205 42 -.055 45 -.066 39 -3.132e-03 � � I39 -9 1295.-03 45 -1.4675-03 44 47 N24 max 0 47 0 46 ' 0 46 1.8525-03 27 2.032e-04 47 3.551e-04 40 48 r -3.484e-04 49 N25 max .206 48 .051 39 .073 45 3.302e-03 45 6.349e-03 45 1.38e-03 46 50 min -.205. 42 -.056 450 -.067 0 _ 40 2.053e-04 14 -6.208e-03 .�-032.06e-04 41 -1.��� 46 39 4.145 03 39 _.:.39 40_. 51 _ N26 max 0 49 0 44 0 44 1.911e-03 27 2.036e-04 49 2.975e-04'1 44 1 52 mm 0 433.631e-041 25 1-2.02e-04 431-3.03e-04 50 53 N27 max 206 48 .007 46 _0 50 0 50383 45 7.434e-03 4 45 1 1 133e-02 45 12.8245-033 40 ...I � 54 j min -.205 42 -.008 l 40 .373 39 -7.821e-03 39 1.119e-02 139 -2.992e-03 46 55 N28 1 max .206 48 .006 44 .494 45 7.082e-03 45 1.505e-02 39 2.989e-03 44 56 'min -.205 i 42 -.009 50 -.483 '39 -7.462e-03 391-1.523e-02 45 -2.921e-03 50 57 N29 max 0 48 0 42 0 39 4.268e-03 45 1.94e-04 45 5. 1 6e-0 48 08 42 58 mm 0 42 -.001 48 0 45 -3.954e-03 -1.935e-04 59 N30 max .206 48 0 39 .349 45 7.434e-03 45 1.133e-02 45 2.823e-03 40 60 min -.205 42 -.002 45 -.34 39 -7.821e-03 39; -1.1195-02 39 -2.992e-03 46 61 N31 max .434 47 0 39 1.023 45 1.669e-02 451.133e-02, 45 6.324e-03, 41 62 min -.424 41 1 -.002 45 -1.032 39 1.708e-02 39 -1.119e-02 39 -6.49e-03i 47 RISA-3D Version 17.0.2 [C:\...\...\Desktop\Projects\2019\February\To Do\PR35\Mod\PR35.r3d] Page 11 a5ed [pugEzdd\pov\i\gcHd\op onfueruqed\61..onspe[wd\dop1soth \-•\'0] OLI. uopJaA GC-VS1H PL 0 17L , 0 '1;11- 0 09 9L98 99 Z9179 Z17 I ZZV61 1XeW 6N S I 41 0 I. 0 4 1 0 6£ 6£Z.98- Z17 464'60Z- 917 1899604-ulw 17 VL 0 VL 1 0 17L 0 9t E9998 817 Z2.6EC Z17 I 99604 Xeal 9N 9 1 4 0 1. 1 0 4 0 9t '11796994- St 90179ZL- St V98.1-Lt-u!wr Z ,tL 0 17L 0 17L 0 6C 6LC191. 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Company : CORE ONE CONSULTING USA Mar 18,2019 • ORE ...... 1, ,;. Designer : APB �� AM u S A Job Number : Che 11: k d By. Model Name : PR32 Envelope Joint Reactions(Continued) Joint X[lbl LC Y�IbL LC Z_[1131 LC MX[Iftj LC MY[k-ftl LC MZ[kt LC 48 2.683 19 1 -8.642 44 0 1 I 0 1 1 0 1 7 IN 10 max 19.122 T 42 130.658 � 44 71.158 43 0 74 0 74 0 74 8 min -19.122 48 99.77 50 -71.763 49 0 1 ! 0 1 0 1 9 N11 1 max 10.898 47 * 395.191 45 80.926 1 45 0 74 0 74 0 174 1110 N12 lmax 19.122` I 41 -123.9031 39 -77.164 39 0 1 0 1 0 1 42 1 40.548 42 3.603 39 0 74 0 74 0 74 12 min -19.122 48 -18.649 , 48 -3.48 1 45 0 1 0 j 1 0 1 13 N13 max 19.122 42 111.028 44 60.995 43 0 741 0 74 0 74 14 min -19.122 1 48 -83.272 1 50 -61.502 49 0 1 0 1 1 0 1 15 N14 ma)4 19.122 42 35.949 37 6.49 1 39 0 74 0 16 min,-19.122 48 6.855 63. 1 -6.489 45 0 1 1 01 1 0 1 17 N15 max 19.122 42 46.189 48 4.33839 0 74 0 74 0 174 18L mink-19.122i 48 -15.837 1 42 -4.21 ( 45 0 1 0 1 T 0 1 19 N16 max 21.248 1 49 1 320.332 46 1111.2191 45 0 74 0 74 0 74 20 Amin -21.998 43 -214.485 40 1-108.064 39 0 1 0 1 1 1 0 1 21 N17 max 19.122 42 35.965 29 6.504 39 0 74 0 74 0 74 22 min 1-19.122 1 48 6.856 63 -6.501 145 I 0 , 1 0 1 0 1 23 N18 max 19.122 42 126.347 46 61.288 47 0 1741 0 74 1 0 [74 24 'mini-19.1221 48 T -98.978 1 40 -62.174 41 1 0 1 0 1 0 1 25 N 19 max 106.814 42 393.044 42 130.935 45 0 74 0 74 0 74 26 min,-106.351 48 -165.201 48 -129.82 39 - 0 L1 � 0 1 1 0 ; 1 27 N20 max 457.583 42 1123.692 48 203.6488 39 0 74 0 1 74 0 174 28 min-455.269, 48 -544.898 42 j-202.6931 45 0 1 1 0 1 19.122 42 148.651 46 71.492 47 0 74 0 74 0 1 29 N21 max 74 30 min -19.122 ' 48 1 -118.126 40 +-72.539 ' 41 0 1 0 1 0 ['1 31 N22 max 19.122 42 35.084 28 8.809 40 0 741 0 74 0 74 32 min -19.122 48 1.825 21 J -8.743 * 46 0 1 �_ 0 ___ 1 1 i 0 1 33 N45 Imax 19.122 42 80.291 42 39.852 39 0 74 0 74 0 174, 34 min -19.122.48 -90.298 48 -40.06 1 45 0 1 0 1 0 1 1 35 N46 max 10.898 47 775.24 47 '123.706 39 0 74 0 74 0 74 36 Imini-10.4061 41 -494.523 41 -129.773 45 0 ' 1 0 T 1 0 1 37 N47 max 68.441 42812.225 39 689.054 39 0 74 0 74 0 74 38 1 min -68.756 48 T -744.33 145 1-686.697. 45 0 1 0 1 0 1 39 N48 max 22.023 42 192.905 50 121.101 49 0 74 0 74 0 74 40ml 21.2481 49 763.496 43 1 411 N49 maxx 105.986 39 0 74 0 74 1 0 74_' r42 ,min -21.9.98 43 -629.153 49 T-112.092 45 j 0 1 0 1 1 0 1 1 1 1_43 N50 1max 19.122 42 6. 4.18 48 55.157 39 0 74 0 74 0 74 44mini-19.122 48 -104.203 42 -55.617 , 45 0 1 0 1 0 ' 1 1 46 min 22 006 48 -190.225 46 -120.736 47 f_ 0 1 0 1 0 1 45 N51 max 47 N52 max 70.199 41 795.869 39 676.636. 39 0 74 0 74 22.035 42 221.94 40 122.358 41 0 74 0 0 74 0 74 74 48 min 1-71.747 47 , -730.086 45 -675.831 45 0 1 0 1 0 1 ' 49 Totals: max 1493.328142 2304.311 38 1701.028 39 50 ±min{-1493.3281 48 1 574.319 63 -1701.028 451 f 1 Envelope RISC 15th(360-16):ASD Steel Code Checks . 121377.2 _1 245 1 1.245 Member Shape Code... L 114 LC Shear..266 11Loc 14 in D454544.89ir LC Pnc/om ...Pnt/om[I..!vin Cb E� 1 M3 PIPE 2.0 .724 /o... Mnzz/o... 2 � lr [ L H1-1b1, L 2 1 MP4 i PIPE 2.0 .507 144_b48 .202 48 L 0454544.89121377.2 1.245 1.245 2...1.1-11-la RISA-3D Version 17.0.2 [C:\...\...\Desktop\Projects\2019\February\To Do\PR35\Mod\PR35.r3d] Page 13 l�. CORE[ 1I Company : CORE ONE CONSULTING USA Mar 18, 2019 �i Designer APB 11:46 AM �� U s A Job Number Checked By. Model Name : PR32 Envelope AISC 15th(360-16):ASD Steel Code Checks(Continued) Member Shape Code... Loc[int LC Shear...Loc[in]Dr LC Pnc/om ...Pnt/om[I..lvinyy/o... Mnzz/o... Cb Eqn 3 MP1 PIPE 2.0 .493 1-48 45 1 .160 138 464544.89213772... 1.245 1.245 '2���H1-1 b' 4 MP3 PIPE 2.0 .492 48 [ 43 .072 84 44 4544.89 21377.2... 1.245 1.245 3....H1-1b 5 MP2 PIPE 2.0 .490 48 46 .070 84 46 4544.8921377.2... 1.245 1.245 3....H1-1b 6 .-_ M2 PIPE 2.0 .271 141 48 .208 141 X474544.89 21377.2... 1.245___1.245 4-1-11-1 b 7 M_5 } PIPE 2.0 .243 0 39 .071 _ 0 45 5791.719 21377.2... 1.245 1.245 2....H1-lb 8 M4 PIPE"2.0 .219 0 39 .053 0 45 5791.719 21377.2... 1.245 1.245 2....H1-1 b 9 _ M12 L2x2x4 .113 42 30 .005 0 y 3520349.7...20349.7... .46 1.049 1 H2-1 10-__ M14 L2x2x4 .11.3 42 30 .004 0 3520349.7...20349.7... .46 1.049- 1 H2-1 11 M16 L2x2x4 113 42 30 1 .004 0 20349.7...20349.7... ..46 1.049 1 H2-1 46 1.049 1 H2-1 12 M17 L2x2x4 .113 42 36 0 � ® .004 20349.7...203497.. 13 M18 L2x2x4 I .113 42 30 .005 0 y 3120349.7...20349.7... .46 1.049 1 H2-1 14 M20 L2x2x4 .113 42 30 .004 0 3220349.7...20349.7... .46 1.049 1 H2-1 15 M22 J L2x2x4 .113 42 30 .004 0 y 27120349.7...20349.7... .46__- 1.049 1 H2-1 16 M23 L2x2x4 .113 42 '36 .005 0 y 3420349.7...20349.7... .46 1.049 1 H2-1 17 M13 L2x2x4 .113 42 36 .005 0 z 3520349.7...20349.7... .46 1.049 1 1 H2-1 18 M15 L2x2x4 .113 42 36 .Ofl4 0 z 3520349.7H20349:7-7... .46 1.049 1 H2-1 19 ' M19 L2x2x4 .113 42 36 .005 0 z 3120349.7...20349.7... .46 1.049 1 H2-1 20 M21 L2x2x4 .11113. 42 36 .004 0 3720349.7..X20349.7... ,46 1.049. 1 H2-1 3 21 M1 PIPE 2.0 114 46 .154 30 394544.8921377.2... 1.245 1.245 2....H1-1b 22 M10 PIPE 2.0 .050 0 42 .046 0 4514060.2...121377.2...i 1.245 1.245 [1-..H1-1b*, 23i M11 PIPE 2.0 .048 0 j 48 j .052 0 4514060.2...21377.2... 1.245 1.245 t1.•.H1-1 b*, RISA-3D Version 17.0.2 [C:\...\...\Desktop\Projects\2019\February\To Do\PR35\Mod\PR35.r3d] Page 14 Project#: PR35 Date: 3/13/2019 Site: Tigard By: APB Wind Loading Inputs: Design Wind Velocity: 93 mph (nominal 3-second gust) Wind Centerline: 44 ft Rooftop height: 36 ft Wind Force Risk Category: II Exposure Category: B qz (psf) Gh FST(psf) Adopted Building Code: 2015 IBC 27.32 1.00 32.78 Antenna Load Standard: TIA-222-G Analysis/Design Analysis Loading Data Unfactored Horizontal Antenna Load (AL): 975.7 lb - Height from roof to center of antenna (H): 8.0 ft Overall Frame Bearing Width: 12.0 ft Overall Frame Bearing Length: 7.0 ft " Frame Weight: 1139.3 lb Friction Coefficient 0.6 W Distance Tray 1: 3.5 ft Tray 1 Paver Type 1: 16x8x8 Hollow CMU Tray 1#Paver Type 1: 64 Tray 1 Paver Type 2: 16x8x2 Hollow CMU Tray 1# Paver Type 2: 0 Applied Overturning Moment: 12489.0 lb-ft Overtuning Moment Resistance: 12603.4 lb-ft Overturning Usage: 99.1 Total Weight: 3824.8 lb Sliding 2294.9 lb Slide Check 68.0 Overall Usage CORE � � Core One Consulting USA Phone: (778) 805 2166 �' S A www.coreoneconsulting.com March 13, 2019 Page 1 6 APPENDIX A Design Tables & Resources Core One Consulting USA COREL1NE Phone: (778) 805-2166 IJRA www.coreoneconsulting.com V - 3/1/2019 ATC Hazards by Location CtTC Hazards by Location Search Information Coordinates: 45.421536,-122.747378 Vancouver ze 239 ft Elevation: 239 ft Tillamook Hillsboro° land o State Forest �eav�r[t�n Gresharn Timestamp: 2019-03-01T21:36:55.313Z 15'3 Mt.Hs Hazard Type: Seismic National Reference ASCE7-10 Document: Q o gle Mapdata©2019 Google Risk Category: II Site Class: D MCER Horizontal Response Spectrum Design Horizontal Response Spectrum Sa(g) Sa(g) 1.00 0.80 0.60 0.60 0.40 0.40 0.20 0.20 0.00 0.00 • 0 5 10 15 Period(s) 0 5 10 15 Period(s) Basic Parameters Name Value Description SS 0.975 MCER ground motion(period=0.2s) Si 0.422 MCER ground motion(period=1.0s) SMS 1.082 Site-modified spectral acceleration value SMI 0.666 Site-modified spectral acceleration value SDS 0.721 Numeric seismic design value at 0.2s SA SDI 0.444 Numeric seismic design value at 1.0s SA Additional Information Name Value Description SDC D Seismic design category Fa 1.11 Site amplification factor at 0.2s Fv 1.578 Site amplification factor at 1.0s CRs 0.898 Coefficient of risk(0.2s) https://hazards.atcouncil.org/#/seismic?lat=45.421536&ing=-122.747378&address= 1/2 r r 3/1/2019 ATC Hazards by Location CR1 0.871 Coefficient of risk(1.0s) PGA 0.426 MCEG peak ground acceleration FPGA 1.074 Site amplification factor at PGA PGAM 0.457 Site modified peak ground acceleration TL 16 Long-period transition period(s) SsRT 0.975 Probabilistic risk-targeted ground motion(0.2s) SsUH 1.085 Factored uniform-hazard spectral acceleration(2%probability of exceedance in 50 years) SsD 2.509 Factored deterministic acceleration value(0.2s) S1 RT 0.422 Probabilistic risk-targeted ground motion(1.0s) Si UH 0.484 Factored uniform-hazard spectral acceleration(2%probability of exceedance in 50 years) S1D 0.812 Factored deterministic acceleration value(1.0s) PGAd 0.921 Factored deterministic acceleration value(PGA) The results indicated here DO NOT reflect any state or local amendments to the values or any delineation lines made during the building code adoption process. Users should confirm any output obtained from this tool with the local Authority Having Jurisdiction before proceeding with design. Disclaimer Hazard loads are provided by the U.S.Geological Survey Seismic Design Web Services. While the information presented on this website is believed to be correct,ATC and its sponsors and contributors assume no responsibility or liability for its accuracy.The material presented in the report should not be used or relied upon for any specific application without competent examination and verification of its accuracy,suitability and applicability by engineers or other licensed professionals.ATC does not intend that the use of this information replace the sound judgment of such competent professionals,having experience and knowledge in the field of practice,nor to substitute for the standard of care required of such professionals in interpreting and applying the results of the report provided by this website. Users of the information from this website assume all liability arising from such use.Use of the output of this website does not imply approval by the governing building code bodies responsible for building code approval and interpretation for the building site described by latitude/longitude location in the report. https://hazards.atcouncil.org/#/seismic?lot=45.421536&Ing=-122.747378&address= 2/2