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T-Mobile Rooftop Cellular InstallationDecision Small Project Review - SRA-21-14 Address of Project: 217 ESSEX STREET Meeting Date:August 11, 2021 Members Present:David Guarino, Cynthia Nina-Soto, Dean Rubin Members Absent:Grace Napolitano, Russ Vickers Decision:To approve the project as presented and conditioned herein. Referenced Plans and Documents: - Application prepared by Timothy Greene, TerraSearch LLC, 157 Riverside Drive, Norwell, MA 02061, submitted on July 22, 2021. DRB Recommendation Staff Comments dated 7/30/21. Conditions of Approval: - Consistency with Approved Design/Plans: Should the applicant determine that the project may not be completed as presented and conditioned herein, he/she/they shall return to the SRA to review proposed modifications prior to making any changes in the field. - Color of Infrastructure: The applicant shall paint all of the components, including but not limited to, antennas, support structures, cables, and brackets, a dark slate gray. Findings: - Consistency with Design Standards and Guidelines: This project is consistent with the design guidelines and standards. Blending of Infrastructure: The dark color for the infrastructure so that it 'disappears' from view; the lighter colors tend to stand out and have greater visual impact. Signature of the SRA: By the signature below, I certify that this recommendation accurately reflects the actions of the Salem Redevelopment Authority Board. Tom Daniel, AICP, Executive Director Date Signed: July 22, 2021 SRA-21-14 8/26/2021 1/2 Design Review Board Recommendation Small Project Review - SRA-21-14 Address of Project: 217 ESSEX STREET Meeting Date:August 25, 2021 Members Present:Paul Durand, Chair, Helen Sides, David Jaquith, Glenn Kennedy, Catherine Miller, Marc Perras Members Absent:J. Michael Sullivan Decision:To recommend approval of the project as presented with the proposed conditions. Referenced Plans and Documents: - Application prepared by Timothy Greene, TerraSearch LLC, 157 Riverside Drive, Norwell, MA 02061, submitted on July 22, 2021. Conditions of Approval: - Consistency with Approved Design/Plans: Should the applicant determine that the project may not be completed as presented and conditioned herein, he/she/they shall return to the DRB to review proposed modifications prior to making any changes in the field. - Color of Infrastructure: The applicant shall paint all of the components, including but not limited to, antennas, support structures, cables, and brackets, a dark slate gray. Findings: - Consistency with Design Standards and Guidelines: This project is consistent with the design guidelines and standards. Blending of Infrastructure: The Board chose a dark color for the infrastructure so that it 'disappears' from view; the lighter colors tend to stand out and have greater visual impact. Signature of the DRB: By the signature below, I certify that this recommendation accurately reflects the actions of the Design Review Board. Paul Durand, Chair Date Signed: July 22, 2021 SRA-21-14 8/26/2021 2/2 7/22/2021 OpenGov https://salemma.viewpointcloud.io/#/explore/records/290797/printable?act=false&app=true&att=false&emp=false&int=false&loc=true&sec=1011778%2…1/2 07/22/2021 City of Salem, MA SRA-21-14 SRA-Urban Renewal Area - Small Project Review Additional Applicant Info Project Information Status: Active Date Created: Jul 22, 2021 Applicant Timothy Greene tgreene@terrasearchllc.com 157 RIVERSIDE DR. NORWELL, MA 02061 617-877-2950 Location 217 ESSEX STREET SALEM, MA 01970 Owner: ESSEX STREET LOFTS, LLC 732 EAST BROADWAY SOUTH BOSTON, MA 02127 Owner T Mobile Northeast Who is the point of contact for this application? Timothy Greene Owner Email Address tgreene@terrasearchllc.com Owner Phone Number 617-877-2950 Project Name/Title T Mobile / Sprint Upgrades Project Description Replacement of antennas and upgrade of equipment at existing wireless facility located on site. Removal of 3 microwave dishes. Removal of 6 Remote Radio Units. Modification of antenna mounts Existing Structure's Square Footage 0 Proposed Structure's Square Footage 0 7/22/2021 OpenGov https://salemma.viewpointcloud.io/#/explore/records/290797/printable?act=false&app=true&att=false&emp=false&int=false&loc=true&sec=1011778%2…2/2 Signature DRB Recommendation SRA Decision Entry Section Estimated time schedule for completing project 3 weeks Will your project include a proposal for Public Art? No Do you have a plan in place for Public Art at this location? No Digital Signature Timothy Greene 07/13/2021 THIS STUDY DOES NOT CLAIM IN ANY WAYTO SHOW THE ONLY AREAS OF VISIBILITY.IT IS MEANT TO SHOW A BROADREPRESENTATION OF AREAS WHERE THEPROPOSED INSTALLATION MAY BE VISIBLEBASED UPON THE BEST INFORMATION FORTOPOGRAPHY AND VEGETATIONLOCATIONS AVAILABLE TO DATE.SITE TYPE: ROOFTOPDATE: 07/15/2021DRAWN BY:AMSCALE: N.T.S.REV: 045 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-558615 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-2893T-MOBILENORTHEAST LLCPAGE 1 OF 11Prepared For:T-MOBILESite Name:4BSS362A217 ESSEX STREETSALEM, MA 01970 #THIS STUDY DOES NOT CLAIM IN ANY WAYTO SHOW THE ONLY AREAS OF VISIBILITY.IT IS MEANT TO SHOW A BROADREPRESENTATION OF AREAS WHERE THEPROPOSED INSTALLATION MAY BE VISIBLEBASED UPON THE BEST INFORMATION FORTOPOGRAPHY AND VEGETATIONLOCATIONS AVAILABLE TO DATE.SITE TYPE: ROOFTOPDATE: 07/15/2021DRAWN BY:AMSCALE: N.T.S.REV: 045 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-558615 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-2893T-MOBILENORTHEAST LLCPAGE 2 OF 11234SITE51 THIS STUDY DOES NOT CLAIM IN ANY WAYTO SHOW THE ONLY AREAS OF VISIBILITY.IT IS MEANT TO SHOW A BROADREPRESENTATION OF AREAS WHERE THEPROPOSED INSTALLATION MAY BE VISIBLEBASED UPON THE BEST INFORMATION FORTOPOGRAPHY AND VEGETATIONLOCATIONS AVAILABLE TO DATE.SITE TYPE: ROOFTOPDATE: 07/15/2021DRAWN BY:AMSCALE: N.T.S.REV: 045 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-558615 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-2893T-MOBILENORTHEAST LLCPAGE 3 OF 11 THIS STUDY DOES NOT CLAIM IN ANY WAYTO SHOW THE ONLY AREAS OF VISIBILITY.IT IS MEANT TO SHOW A BROADREPRESENTATION OF AREAS WHERE THEPROPOSED INSTALLATION MAY BE VISIBLEBASED UPON THE BEST INFORMATION FORTOPOGRAPHY AND VEGETATIONLOCATIONS AVAILABLE TO DATE.SITE TYPE: ROOFTOPDATE: 07/15/2021DRAWN BY:AMSCALE: N.T.S.REV: 045 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-558615 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-2893T-MOBILENORTHEAST LLCPAGE 4 OF 11 THIS STUDY DOES NOT CLAIM IN ANY WAYTO SHOW THE ONLY AREAS OF VISIBILITY.IT IS MEANT TO SHOW A BROADREPRESENTATION OF AREAS WHERE THEPROPOSED INSTALLATION MAY BE VISIBLEBASED UPON THE BEST INFORMATION FORTOPOGRAPHY AND VEGETATIONLOCATIONS AVAILABLE TO DATE.SITE TYPE: ROOFTOPDATE: 07/15/2021DRAWN BY:AMSCALE: N.T.S.REV: 045 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-558615 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-2893T-MOBILENORTHEAST LLCPAGE 5 OF 11 THIS STUDY DOES NOT CLAIM IN ANY WAYTO SHOW THE ONLY AREAS OF VISIBILITY.IT IS MEANT TO SHOW A BROADREPRESENTATION OF AREAS WHERE THEPROPOSED INSTALLATION MAY BE VISIBLEBASED UPON THE BEST INFORMATION FORTOPOGRAPHY AND VEGETATIONLOCATIONS AVAILABLE TO DATE.SITE TYPE: ROOFTOPDATE: 07/15/2021DRAWN BY:AMSCALE: N.T.S.REV: 045 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-558615 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-2893T-MOBILENORTHEAST LLCPAGE 6 OF 11 THIS STUDY DOES NOT CLAIM IN ANY WAYTO SHOW THE ONLY AREAS OF VISIBILITY.IT IS MEANT TO SHOW A BROADREPRESENTATION OF AREAS WHERE THEPROPOSED INSTALLATION MAY BE VISIBLEBASED UPON THE BEST INFORMATION FORTOPOGRAPHY AND VEGETATIONLOCATIONS AVAILABLE TO DATE.SITE TYPE: ROOFTOPDATE: 07/15/2021DRAWN BY:AMSCALE: N.T.S.REV: 045 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-558615 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-2893T-MOBILENORTHEAST LLCPAGE 7 OF 11 THIS STUDY DOES NOT CLAIM IN ANY WAYTO SHOW THE ONLY AREAS OF VISIBILITY.IT IS MEANT TO SHOW A BROADREPRESENTATION OF AREAS WHERE THEPROPOSED INSTALLATION MAY BE VISIBLEBASED UPON THE BEST INFORMATION FORTOPOGRAPHY AND VEGETATIONLOCATIONS AVAILABLE TO DATE.SITE TYPE: ROOFTOPDATE: 07/15/2021DRAWN BY:AMSCALE: N.T.S.REV: 045 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-558615 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-2893T-MOBILENORTHEAST LLCPAGE 8 OF 11 THIS STUDY DOES NOT CLAIM IN ANY WAYTO SHOW THE ONLY AREAS OF VISIBILITY.IT IS MEANT TO SHOW A BROADREPRESENTATION OF AREAS WHERE THEPROPOSED INSTALLATION MAY BE VISIBLEBASED UPON THE BEST INFORMATION FORTOPOGRAPHY AND VEGETATIONLOCATIONS AVAILABLE TO DATE.SITE TYPE: ROOFTOPDATE: 07/15/2021DRAWN BY:AMSCALE: N.T.S.REV: 045 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-558615 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-2893T-MOBILENORTHEAST LLCPAGE 9 OF 11 THIS STUDY DOES NOT CLAIM IN ANY WAYTO SHOW THE ONLY AREAS OF VISIBILITY.IT IS MEANT TO SHOW A BROADREPRESENTATION OF AREAS WHERE THEPROPOSED INSTALLATION MAY BE VISIBLEBASED UPON THE BEST INFORMATION FORTOPOGRAPHY AND VEGETATIONLOCATIONS AVAILABLE TO DATE.SITE TYPE: ROOFTOPDATE: 07/15/2021DRAWN BY:AMSCALE: N.T.S.REV: 045 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-558615 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-2893T-MOBILENORTHEAST LLCPAGE 10 OF 11 THIS STUDY DOES NOT CLAIM IN ANY WAYTO SHOW THE ONLY AREAS OF VISIBILITY.IT IS MEANT TO SHOW A BROADREPRESENTATION OF AREAS WHERE THEPROPOSED INSTALLATION MAY BE VISIBLEBASED UPON THE BEST INFORMATION FORTOPOGRAPHY AND VEGETATIONLOCATIONS AVAILABLE TO DATE.SITE TYPE: ROOFTOPDATE: 07/15/2021DRAWN BY:AMSCALE: N.T.S.REV: 045 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-558615 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-2893T-MOBILENORTHEAST LLCPAGE 11 OF 11 T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’T-1SHEETNO.DESCRIPTIONREV.LOCATIONSPECIAL RESTRICTIONSPROJECTSITESITE NAME: 4BSS362A_BS23XC362_217 ESSEX ST_RT217 ESSEX STREETSALEM, MA 01970ESSEX COUNTYSITE NUMBER: 4BSS362ARF DESIGN GUIDELINE: 67D5A997DB INDOOR72 HOURSUNDERGROUND SERVICE ALERT T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’GN-1GROUNDING NOTESGENERAL NOTES T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’SN-1STRUCTURAL NOTES:NOTES:MASSACHUSETTS AMENDMENTS TO THE IBC(REFERENCE 780 CMR):’SPECIAL INSPECTION CHECKLISTBEFORE CONSTRUCTION REQUIREDENGINEER OF RECORD APPROVEDSHOP DRAWINGS 1 REQUIREDMATERIAL SPECIFICATIONS REPORT 2 REQUIREDPACKING SLIPS 3DURING CONSTRUCTION REQUIREDSTEEL INSPECTIONS45AFTER CONSTRUCTION REQUIREDMODIFICATION INSPECTOR REDLINEOR RECORD DRAWINGS 6 REQUIREDPHOTOGRAPHSREQUIRED INSPECTIONS AND SITE REVIEW DOCUMENT AS ACONDITION OF THE BUILDING PERMIT THE FOLLOWINGINSPECTIONS AND SITE REVIEWS IDENTIFIED BY THE BUILDINGOFFICIAL ARE REQUIRED FOR WORK PER THE9TH EDITION OF THE MASSACHUSETTS STATE BUILDING CODE,780 CMR, SECTION 110 AND CHAPTER 17REQUIRED SITE REVIEW AND DOCUMENTATION FOR PORTIONS OR PHASESCONSTRUCTION 1,6,7SITE REVIEW AND DOCUMENTATIONXSITE REVIEW ANDDOCUMENTATIONXSTRUCTURAL FRAME -WALL/FLOOR/ROOFXSPECIAL INSPECTIONS (SECTION1704):XSPECIAL INSPECTIONS (REFERENCE IBC CHAPTER 17):NOTES: T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’A-1ROOFTOP PLANNOTE:EXISTING EQUIPMENT PLANPROPOSED EQUIPMENT PLANSTRUCTURAL NOTES: T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’A-2NOTE:EXISTING ANTENNA PLANNOTE:PROPOSED ANTENNA PLANSTRUCTURAL NOTES: T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’A-3ELEVATIONNOTE:STRUCTURAL NOTES: T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’A-4L600 ANTENNA DETAILRADIO DETAILAIR32 ANTENNA DETAILL25+N25 ANTENNA DETAILSITE SUPPORT CABINET DETAILBATTERY CABINET DETAILNOTE:RADIO DETAILPROPOSED PURCELL CABINET T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’A-5PROPOSED L600 + L700ANTENNA MOUNTING DETAIL(ALPHA SECTOR)NOTE:PROPOSED L600 + L700ANTENNA MOUNTING DETAIL(GAMMA SECTOR)PROPOSED L600 + L700ANTENNA MOUNTING DETAIL(BETA SECTOR)STRUCTURAL NOTES: T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’A-6NOTE:PROPOSED L600 + L700ANTENNA MOUNTING DETAIL(BETA SECTOR)PROPOSED L600 + L700ANTENNA MOUNTING DETAIL(ALPHA SECTOR)PROPOSED L25+N25ANTENNA MOUNTING DETAILSTRUCTURAL NOTES: T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’S-1BETA/GAMMA SECTORCHIMNEY ELEVATIONBETA/GAMMA SECTORCHIMNEY CONNECTION PLANBETA/GAMMA SECTORCHIMNEY CONNECTION PLANBETA/GAMMA SECTORCHIMNEY CONNECTION PLANSTRUCTURAL NOTES:MOUNT NOTE: T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’S-2BETA SECTOR CHIMNEYCONNECTION PLANBETA SECTOR CHIMNEYCONNECTION DETAILBETA SECTOR CHIMNEYCONNECTION PLANSTRUCTURAL NOTES: T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’S-3ALPHA & GAMMA SECTORCHIMNEY CONNECTION PLANALPHA & GAMMA SECTOR ELEVATIONSTRUCTURAL NOTES: T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’S-4ALPHA & GAMMA SECTOR ELEVATIONALPHA SECTOR ANTENNACONNECTION DETAILALPHA SECTOR ANTENNACONNECTION DETAILSTRUCTURAL NOTES: T-MOBILENORTHEAST LLC15 COMMERCE WAY, SUITE BNORTON, MA 02766OFFICE: (508) 286-2700FAX: (508) 286-289345 BEECHWOOD DRIVETEL: (978) 557-5553N. ANDOVER, MA 01845FAX: (978) 336-5586’G-1TOWER TOP CABLE GROUNDING DETAILELECTRICAL & GROUNDING NOTESELECTRICAL LEGENDGROUNDING RISER DIAGRAMTYPICAL GROUND BARCONNECTION DETAILONE LINE POWER DIAGRAM p: 978.557.5553 f: 978.336.5586 a: 45 Beechwood Drive, N. Andover, MA 01845 March 4, 2021 SAI Communications 12 Industrial Way Salem NH, 03079 RE: Site Number: 4BSS362A Site Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Site Address: 217 Essex Street Salem, MA 01970 To Whom It May Concern: Hudson Design Group LLC (HDG) has been authorized by SAI Communications to perform a mount analysis on the existing and proposed T-Mobile antenna/RRH mounts to determine their capability of supporting the following additional loading:  (3) AIR6449 B41 Antennas (33.1”x20.5”x8.5” – Wt. = 103 lbs. /each)  (3) AIR 32 B66A B2A Antennas (56.6”x12.9”x8.7” – Wt. = 133 lbs. /each)  APXVAALL24_43-U-NA20 Antennas (95.9”x24.0”x8.5” – Wt. = 150 lbs. /each)  (3) 4415 RRH’s (14.9”x13.2”x5.4” – Wt. = 44 lbs. /each)  (3) 4449 B71+B85 RRH’s (17.9”x13.2”x9.5” – Wt. = 71 lbs. /each) *Proposed equipment shown in bold. No original structural design documents or fabrication drawings were available for the existing mounts. HDG conducted an on-site visual survey of the above site on September 2, 2020. Page 2 of 5 Re: 4BSS362A March 4, 2021 p: 978.557.5553 f: 978.336.5586 a: 45 Beechwood Drive, N. Andover, MA 01845 Mount Analysis Methods:  This analysis was conducted in accordance with EIA/TIA-222-H, Structural Standards for Steel Antenna Towers and Antenna Supporting Structures, the International Building Code 2015, and the Massachusetts State Building Code, 9th edition, and AT&T Mount Technical Directive – R13.  HDG considers this mount to be asymmetrical and has applied wind loads in 30 degree increments all around the mount. Per TIA-222-H and Chapter 16 of the Massachusetts State Building Code, 9th edition, the max basic wind speed for this site is equal to 127 mph with a max basic wind speed with ice of 50 mph and a max ice thickness of 1.0 in. An escalated ice thickness of 1.10 in was used for this analysis.  HDG considers this site to be exposure category B; tower is located in an urban/suburban or wooded area with numerous closely spaced obstructions.  HDG considers this site to be topographic category 1; tower is located on flat terrain or the bottom of a hill or ridge.  HDG considers this site to have a spectral response acceleration parameter at short periods, S S, of 0.240 and a spectral response acceleration parameter at a period of 1 second, S1, of 0.073. Based on our evaluation, we have determined that the existing and proposed mounts ARE NOT CAPABLE of supporting the proposed installation. Component Controlling Load Case Stress Ratio Pass/Fail Chimney Mount Rating 1 LC7 69% PASS Penthouse Mount Rating (Worst Case) 4 LC7 145% FAIL Based on our evaluation, we have determined that the existing connections ARE NOT CAPABLE of supporting the proposed installation.  Refer to Structural Analysis by HDG for modification recommendations. Anchor Stress Ratio Pass/Fail Chimney Connection (Worst Case) 3/4" Epoxy Anchors 172% FAIL Penthouse Connection (Worst Case) 1/2" Epoxy Anchors 305% FAIL Reference Documents:  Previous HDG Construction Drawings dated December 15, 2011. Page 4 of 5 Re: 4BSS362A March 4, 2021 p: 978.557.5553 f: 978.336.5586 a: 45 Beechwood Drive, N. Andover, MA 01845 FIELD PHOTOS: Page 5 of 5 Re: 4BSS362A March 4, 2021 p: 978.557.5553 f: 978.336.5586 a: 45 Beechwood Drive, N. Andover, MA 01845 Wind & Ice Calculations Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC 2.6.5.2 Velocity Pressure Coeff: Kz= 2.01 (z/zg) 2/α z= 88 (ft) zg=1200 (ft) Kz=0.953 α= 7.0 Kzmin ≤ Kz ≤ 2.01 Table 2-4 Exposure Zg α Kzmin Kc B 1200 ft 7.0 0.70 0.9 C 900 ft 9.5 0.85 1.0 D 700 ft 11.5 1.03 1.1 2.6.6.2 Topographic Factor: Table 2-5 Topo. Category Kt f 2 0.43 1.25 3 0.53 2.0 4 0.72 1.5 Kzt= [1+(Kc Kt/Kh)]2 Kh= e (f*z/H) Kzt=1 Kh=1 Kc=0.9 (from Table 2-4) (If Category 1 then K zt =1.0)Kt=0 (from Table 2-5) f=0 (from Table 2-5) Category=1 z=88 zs=20 (Mean elevation of base of structure above sea level) H= 0 (Ht. of the crest above surrounding terrain) Kzt=1.00 (from 2.6.6.2.1) Ke=1.00 (from 2.6.8) 2.6.10 Design Ice Thickness Max Ice Thickness =ti = 1.00 in Importance Factor = I= 1.0 (from Table 2-3) Kiz =1.10 (from Sec. 2.6.10) tiz= ti*I*Kiz*(Kzt)0.35 tiz = 1.10 in Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC 2.6.9 Gust Effect Factor 2.6.9.1 Self Supporting Lattice Structures Gh = 1.0 Latticed Structures > 600 ft Gh = 0.85 Latticed Structures 450 ft or less Gh = 0.85 + 0.15 [h/150 - 3.0]h= ht. of structure h= 68 Gh=0.85 2.6.9.2 Guyed Masts Gh=0.85 2.6.9.3 Pole Structures Gh=1.1 2.6.9 Appurtenances Gh=1.0 2.6.9.4 Structures Supported on Other Structures (Cantilivered tubular or latticed spines, pole, structures on buildings (ht. : width ratio > 5) Gh=1.35 Gh= 1.00 2.6.11.2 Design Wind Force on Appurtenances F=qz*Gh*(EPA)A qz= 0.00256*Kz*Kzt*Ks*Ke*Kd*Vmax 2 Kz=0.953 (from 2.6.5.2) Kzt=1.0 (from 2.6.6.2.1) Ks=1.0 (from 2.6.7) qz=33.42 Ke=1.00 (from 2.6.8) qz (ice)=5.18 Kd=0.85 (from Table 2-2) qz (30)=1.86 Vmax=127 mph (Ultimate Wind Speed) Vmax (ice)=50 mph V30=30 mph Table 2-2 Structure Type Wind Direction Probability Factor, Kd Latticed structures with triangular, square or rectangular cross sections 0.85 Tubular pole structures supporting antennas enclosed within a cylindrical shroud 1.00 Tubular pole structures, latticed structures with other cross sections, appurtenances 0.95 Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Determine Ca: Table 2-9 Round C < 39 (Subcritical) 39 ≤ C ≤ 78 (Transitional) C > 78 (Supercritical) Ice Thickness =1.10 in Angle =0 (deg)Equivalent Angle =180 (deg) Appurtenances Height Width Depth Flat Area Aspect Ratio Ca Force (lbs)Force (lbs) (w/ Ice) Force (lbs) (30 mph) AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.61 1.20 189 35 11 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 4.39 1.28 218 41 12 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 4.00 1.27 676 117 38 4415 RRH 14.9 13.2 5.4 1.37 1.13 1.20 55 11 3 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.36 1.20 66 13 4 3" Pipe 3.5 12.0 0.29 0.29 1.20 12 3 1 2" Pipe 2.4 12.0 0.20 0.20 1.20 8 3 0 Note: Linear interpolation may be used for aspect ratios other than those shown. Flat Aspect Ratio is the overall length/width ratio in the plane normal to the wind direction. (Aspect ratio is independent of the spacing between support points of a linear appurtenance, 1.2 0.7 4.14/(C0.485) 0.5 3.66/(C0.415) 46.8/(C .1.0) 1.4 0.8 0.6 0.6 1.2 Aspect Ratio ≤ 2.5 Aspect Ratio = 7 Aspect Ratio ≥ 25 Force Coefficients (Ca) for Appurtenances Member Type Ca Ca Ca 2.0 Square/Rectangular HSS 1.2 - 2.8(rs) ≥ 0.85 1.4 - 4.0(rs) ≥ 0.90 2.0 - 6.0(rs) ≥ 1.25 Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Angle =30 (deg) Ice Thickness =1.10 in.Equivalent Angle =210 (deg) WIND LOADS WITH NO ICE: Appurtenances Height Width Depth Flat Area (normal) Flat Area (side) Aspect Ratio (normal) Aspect Ratio (side) Ca (normal)Ca (side) Force (lbs) (normal) Force (lbs) (side) Force (lbs) (angle) AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 189 82 162 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 218 157 203 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 676 292 580 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 55 23 47 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 66 47 61 WIND LOADS WITH ICE: AIR6449 B41 Antennas 35.3 22.7 10.7 5.57 2.62 1.55 3.30 1.20 1.24 35 17 30 AIR 32 B66A B2A Antennas 58.8 15.1 10.9 6.17 4.45 3.89 5.39 1.26 1.33 40 31 38 APXVAALL24_43-U-NA20 Antennas 98.1 26.2 10.7 17.85 7.29 3.74 9.16 1.26 1.47 116 56 101 4415 RRH 17.1 15.4 7.6 1.83 0.90 1.11 2.25 1.20 1.20 11 6 10 4449 B71+B85 RRH 20.1 15.4 11.7 2.15 1.63 1.31 1.72 1.20 1.20 13 10 13 WIND LOADS AT 30 MPH: AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 11 5 9 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 12 9 11 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 38 16 32 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 3 1 3 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 4 3 3 WIND LOADS Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Angle =60 (deg) Ice Thickness =1.10 in.Equivalent Angle =240 (deg) WIND LOADS WITH NO ICE: Appurtenances Height Width Depth Flat Area (normal) Flat Area (side) Aspect Ratio (normal) Aspect Ratio (side) Ca (normal) Ca (side) Force (lbs) (normal) Force (lbs) (side) Force (lbs) (angle) AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 189 82 109 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 218 157 172 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 676 292 388 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 55 23 31 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 66 47 52 WIND LOADS WITH ICE: AIR6449 B41 Antennas 35.3 22.7 10.7 5.57 2.62 1.55 3.30 1.20 1.24 35 17 21 AIR 32 B66A B2A Antennas 58.8 15.1 10.9 6.17 4.45 3.89 5.39 1.26 1.33 40 31 33 APXVAALL24_43-U-NA20 Antennas 98.1 26.2 10.7 17.85 7.29 3.74 9.16 1.26 1.47 116 56 71 4415 RRH 17.1 15.4 7.6 1.83 0.90 1.11 2.25 1.20 1.20 11 6 7 4449 B71+B85 RRH 20.1 15.4 11.7 2.15 1.63 1.31 1.72 1.20 1.20 13 10 11 WIND LOADS AT 30 MPH: AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 11 5 6 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 12 9 10 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 38 16 22 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 3 1 2 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 4 3 3 WIND LOADS Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Angle =90 (deg) Ice Thickness =1.10 in.Equivalent Angle =270 (deg) WIND LOADS WITH NO ICE: Appurtenances Height Width Depth Flat Area (normal) Flat Area (side) Aspect Ratio (normal) Aspect Ratio (side) Ca (normal) Ca (side) Force (lbs) (normal) Force (lbs) (side) Force (lbs) (angle) AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 189 82 82 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 218 157 157 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 676 292 292 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 55 23 23 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 66 47 47 WIND LOADS WITH ICE: AIR6449 B41 Antennas 35.3 22.7 10.7 5.57 2.62 1.55 3.30 1.20 1.24 35 17 17 AIR 32 B66A B2A Antennas 58.8 15.1 10.9 6.17 4.45 3.89 5.39 1.26 1.33 40 31 31 APXVAALL24_43-U-NA20 Antennas 98.1 26.2 10.7 17.85 7.29 3.74 9.16 1.26 1.47 116 56 56 4415 RRH 17.1 15.4 7.6 1.83 0.90 1.11 2.25 1.20 1.20 11 6 6 4449 B71+B85 RRH 20.1 15.4 11.7 2.15 1.63 1.31 1.72 1.20 1.20 13 10 10 WIND LOADS AT 30 MPH: AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 11 5 5 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 12 9 9 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 38 16 16 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 3 1 1 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 4 3 3 WIND LOADS Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Angle =120 (deg) Ice Thickness =1.10 in.Equivalent Angle =300 (deg) WIND LOADS WITH NO ICE: Appurtenances Height Width Depth Flat Area (normal) Flat Area (side) Aspect Ratio (normal) Aspect Ratio (side) Ca (normal) Ca (side) Force (lbs) (normal) Force (lbs) (side) Force (lbs) (angle) AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 189 82 109 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 218 157 172 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 676 292 388 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 55 23 31 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 66 47 52 WIND LOADS WITH ICE: AIR6449 B41 Antennas 35.3 22.7 10.7 5.57 2.62 1.55 3.30 1.20 1.24 35 17 21 AIR 32 B66A B2A Antennas 58.8 15.1 10.9 6.17 4.45 3.89 5.39 1.26 1.33 40 31 33 APXVAALL24_43-U-NA20 Antennas 98.1 26.2 10.7 17.85 7.29 3.74 9.16 1.26 1.47 116 56 71 4415 RRH 17.1 15.4 7.6 1.83 0.90 1.11 2.25 1.20 1.20 11 6 7 4449 B71+B85 RRH 20.1 15.4 11.7 2.15 1.63 1.31 1.72 1.20 1.20 13 10 11 WIND LOADS AT 30 MPH: AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 11 5 6 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 12 9 10 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 38 16 22 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 3 1 2 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 4 3 3 WIND LOADS Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Angle =150 (deg) Ice Thickness =1.10 in.Equivalent Angle =330 (deg) WIND LOADS WITH NO ICE: Appurtenances Height Width Depth Flat Area (normal) Flat Area (side) Aspect Ratio (normal) Aspect Ratio (side) Ca (normal) Ca (side) Force (lbs) (normal) Force (lbs) (side) Force (lbs) (angle) AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 189 82 162 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 218 157 203 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 676 292 580 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 55 23 47 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 66 47 61 WIND LOADS WITH ICE: AIR6449 B41 Antennas 35.3 22.7 10.7 5.57 2.62 1.55 3.30 1.20 1.24 35 17 30 AIR 32 B66A B2A Antennas 58.8 15.1 10.9 6.17 4.45 3.89 5.39 1.26 1.33 40 31 38 APXVAALL24_43-U-NA20 Antennas 98.1 26.2 10.7 17.85 7.29 3.74 9.16 1.26 1.47 116 56 101 4415 RRH 17.1 15.4 7.6 1.83 0.90 1.11 2.25 1.20 1.20 11 6 10 4449 B71+B85 RRH 20.1 15.4 11.7 2.15 1.63 1.31 1.72 1.20 1.20 13 10 13 WIND LOADS AT 30 MPH: AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 11 5 9 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 12 9 11 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 38 16 32 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 3 1 3 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 4 3 3 WIND LOADS Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Thickness of ice:1.10 in. Density of ice:56 pcf AIR6449 B41 Antennas AIR 32 B66A B2A Antennas Weight of ice based on total radial SF area: Weight of ice based on total radial SF area: Height (in): 33.1 Height (in): 56.6 Width (in): 20.5 Width (in): 12.9 Depth (in): 8.5 Depth (in): 8.7 Total weight of ice on object: 86 lbs Total weight of ice on object: 106 lbs Weight of object: 103.0 lbs Weight of object: 133.0 lbs Combined weight of ice and object: 189 lbs Combined weight of ice and object: 239 lbs APXVAALL24_43-U-NA20 Antennas 4415 RRH Weight of ice based on total radial SF area: Weight of ice based on total radial SF area: Height (in): 95.9 Height (in): 14.9 Width (in): 24.0 Width (in): 13.2 Depth (in): 8.5 Depth (in): 5.4 Total weight of ice on object: 285 lbs Total weight of ice on object: 26 lbs Weight of object: 150.0 lbs Weight of object: 44.0 lbs Combined weight of ice and object: 435 lbs Combined weight of ice and object: 70 lbs 4449 B71+B85 RRH 3" Pipe Weight of ice based on total radial SF area: Per foot weight of ice: Height (in): 17.9 diameter (in): 3.5 Width (in): 13.2 Per foot weight of ice on object: 6 plf Depth (in): 9.5 Total weight of ice on object: 35 lbs Weight of object: 71.0 lbs Combined weight of ice and object: 106 lbs 2" Pipe Per foot weight of ice: diameter (in): 3.5 Per foot weight of ice on object: 6 plf ICE WEIGHT CALCULATIONS Penthouse Antenna Mount Calculations (Existing Conditions) Current Date: 3/4/2021 4:51 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Chimney Mount.retx Current Date: 3/4/2021 4:51 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Chimney Mount.retx Current Date: 3/4/2021 4:51 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Chimney Mount.retx Current Date: 3/4/2021 4:51 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Chimney Mount.retx Current Date: 3/4/2021 4:51 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Chimney Mount.retx Load data ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ GLOSSARY Comb : Indicates if load condition is a load combination Load Conditions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition Description Comb.Category ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- D Dead Load No DL Wo Wind Load (NO ICE)No WIND W30 WL 30deg No WIND W60 WL 60deg No WIND W90 WL 90deg No WIND W120 WL 120deg No WIND W150 WL 150deg No WIND Di Ice Load No LL WI0 WL ICE 0deg No WIND WI30 WL ICE 30deg No WIND WI60 WL ICE 60deg No WIND WI90 WL ICE 90deg No WIND WI120 WL ICE 120deg No WIND WI150 WL ICE 150deg No WIND ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Distributed force on members ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition Member Dir1 Val1 Val2 Dist1 %Dist2 % [Kip/ft][Kip/ft][ft][ft] ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Wo 1 z -0.012 -0.012 20.00 Yes 100.00 Yes 19 z -0.012 -0.012 35.00 Yes 100.00 Yes 20 z -0.012 -0.012 35.00 Yes 100.00 Yes W30 1 z -0.012 -0.012 20.00 Yes 100.00 Yes 19 z -0.012 -0.012 35.00 Yes 100.00 Yes 20 z -0.012 -0.012 35.00 Yes 100.00 Yes W60 1 x -0.012 -0.012 20.00 Yes 100.00 Yes 19 x -0.012 -0.012 35.00 Yes 100.00 Yes 20 x -0.012 -0.012 35.00 Yes 100.00 Yes W90 1 x -0.012 -0.012 20.00 Yes 100.00 Yes 19 x -0.012 -0.012 35.00 Yes 100.00 Yes 20 x -0.012 -0.012 35.00 Yes 100.00 Yes W120 1 x -0.012 -0.012 20.00 Yes 100.00 Yes 19 x -0.012 -0.012 35.00 Yes 100.00 Yes Page1 20 x -0.012 -0.012 35.00 Yes 100.00 Yes W150 1 z 0.012 0.012 20.00 Yes 100.00 Yes 19 z 0.012 0.012 35.00 Yes 100.00 Yes 20 z 0.012 0.012 35.00 Yes 100.00 Yes Di 1 y -0.006 -0.006 0.00 No 100.00 Yes 19 y -0.006 -0.006 0.00 No 100.00 Yes 20 y -0.006 -0.006 0.00 No 100.00 Yes ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Concentrated forces on members ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition Member Dir1 Value1 Dist1 % [Kip][ft] -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- D 1 y -0.052 1.00 No y -0.052 3.00 No 19 y -0.067 1.75 No y -0.067 5.25 No 20 y -0.067 1.75 No y -0.067 5.25 No Wo 1 z -0.095 1.00 No z -0.095 3.00 No 19 z -0.109 1.75 No z -0.109 5.25 No 20 z -0.109 1.75 No z -0.109 5.25 No W30 1 3 -0.081 1.00 No 3 -0.081 3.00 No 19 3 -0.102 1.75 No 3 -0.102 5.25 No 20 3 -0.102 1.75 No 3 -0.102 5.25 No W60 1 3 -0.055 1.00 No 3 -0.055 3.00 No 19 3 -0.086 1.75 No 3 -0.086 5.25 No 20 3 -0.086 1.75 No 3 -0.086 5.25 No W90 1 x -0.041 1.00 No x -0.041 3.00 No 19 x -0.079 1.75 No x -0.079 5.25 No 20 x -0.079 1.75 No x -0.079 5.25 No W120 1 2 -0.055 1.00 No 2 -0.055 3.00 No 19 2 -0.086 1.75 No 2 -0.086 5.25 No 20 2 -0.086 1.75 No 2 -0.086 5.25 No W150 1 2 -0.081 1.00 No 2 -0.081 3.00 No Page2 19 2 -0.102 1.75 No 2 -0.102 5.25 No 20 2 -0.102 1.75 No 2 -0.102 5.25 No Di 1 y -0.043 1.00 No y -0.043 3.00 No 19 y -0.053 1.75 No y -0.053 5.25 No 20 y -0.053 1.75 No y -0.053 5.25 No WI0 1 z -0.018 1.00 No z -0.018 3.00 No 19 z -0.021 1.75 No z -0.021 5.25 No 20 z -0.021 1.75 No z -0.021 5.25 No WI30 1 3 -0.015 1.00 No 3 -0.015 3.00 No 19 3 -0.019 1.75 No 3 -0.019 5.25 No 20 3 -0.019 1.75 No 3 -0.019 5.25 No WI60 1 3 -0.011 1.00 No 3 -0.011 3.00 No 19 3 -0.017 1.75 No 3 -0.017 5.25 No 20 3 -0.017 1.75 No 3 -0.017 5.25 No WI90 1 x -0.009 1.00 No x -0.009 3.00 No 19 x -0.016 1.75 No x -0.016 5.25 No 20 x -0.016 1.75 No x -0.016 5.25 No WI120 1 2 -0.011 1.00 No 2 -0.011 3.00 No 19 2 -0.017 1.75 No 2 -0.017 5.25 No 20 2 -0.017 1.75 No 2 -0.017 5.25 No WI150 1 2 -0.015 1.00 No 2 -0.015 3.00 No 19 2 -0.019 1.75 No 2 -0.019 5.25 No 20 2 -0.019 1.75 No 2 -0.019 5.25 No -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Self weight multipliers for load conditions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Self weight multiplier Condition Description Comb.MultX MultY MultZ ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ D Dead Load No 0.00 -1.00 0.00 Wo Wind Load (NO ICE)No 0.00 0.00 0.00 W30 WL 30deg No 0.00 0.00 0.00 W60 WL 60deg No 0.00 0.00 0.00 Page3 W90 WL 90deg No 0.00 0.00 0.00 W120 WL 120deg No 0.00 0.00 0.00 W150 WL 150deg No 0.00 0.00 0.00 Di Ice Load No 0.00 0.00 0.00 WI0 WL ICE 0deg No 0.00 0.00 0.00 WI30 WL ICE 30deg No 0.00 0.00 0.00 WI60 WL ICE 60deg No 0.00 0.00 0.00 WI90 WL ICE 90deg No 0.00 0.00 0.00 WI120 WL ICE 120deg No 0.00 0.00 0.00 WI150 WL ICE 150deg No 0.00 0.00 0.00 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Earthquake (Dynamic analysis only) ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition a/g Ang.Damp. [Deg][%] -------------------------------------------------------------------------------------------------------------------------------------------------------- D 0.00 0.00 0.00 Wo 0.00 0.00 0.00 W30 0.00 0.00 0.00 W60 0.00 0.00 0.00 W90 0.00 0.00 0.00 W120 0.00 0.00 0.00 W150 0.00 0.00 0.00 Di 0.00 0.00 0.00 WI0 0.00 0.00 0.00 WI30 0.00 0.00 0.00 WI60 0.00 0.00 0.00 WI90 0.00 0.00 0.00 WI120 0.00 0.00 0.00 WI150 0.00 0.00 0.00 -------------------------------------------------------------------------------------------------------------------------------------------------------- Page4 Current Date: 3/4/2021 4:51 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Chimney Mount.retx Steel Code Check ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Report: Summary - Group by member Load conditions to be included in design : LC1=1.2D+Wo LC2=1.2D+W30 LC3=1.2D+W60 LC4=1.2D+W90 LC5=1.2D+W120 LC6=1.2D+W150 LC7=1.2D-Wo LC8=1.2D-W30 LC9=1.2D-W60 LC10=1.2D-W90 LC11=1.2D-W120 LC12=1.2D-W150 LC13=0.9D+Wo LC14=0.9D+W30 LC15=0.9D+W60 LC16=0.9D+W90 LC17=0.9D+W120 LC18=0.9D+W150 LC19=0.9D-Wo LC20=0.9D-W30 LC21=0.9D-W60 LC22=0.9D-W90 LC23=0.9D-W120 LC24=0.9D-W150 LC25=1.2D+Di+WI0 LC26=1.2D+Di+WI30 LC27=1.2D+Di+WI60 LC28=1.2D+Di+WI90 LC29=1.2D+Di+WI120 LC30=1.2D+Di+WI150 LC31=1.2D+Di-WI0 LC32=1.2D+Di-WI30 LC33=1.2D+Di-WI60 LC34=1.2D+Di-WI90 LC35=1.2D+Di-WI120 LC36=1.2D+Di-WI150 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Description Section Member Ctrl Eq.Ratio Status Reference ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ PIPE 3x0.216 1 LC7 at 68.75%0.69 OK 19 LC1 at 68.75%0.62 OK 20 LC7 at 68.75%0.62 OK ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ WT 6X11 2 LC1 at 75.00%0.15 OK 3 LC7 at 75.00%0.15 OK 6 LC19 at 0.00%0.09 OK 7 LC2 at 21.88%0.07 OK 8 LC6 at 100.00%0.07 OK 9 LC2 at 77.08%0.08 OK 10 LC24 at 0.00%0.02 OK 11 LC7 at 0.00%0.02 OK Page1 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Page2 Current Date: 3/4/2021 4:51 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Chimney Mount.retx Geometry data ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ GLOSSARY Cb22, Cb33 : Moment gradient coefficients Cm22, Cm33 : Coefficients applied to bending term in interaction formula d0 : Tapered member section depth at J end of member DJX : Rigid end offset distance measured from J node in axis X DJY : Rigid end offset distance measured from J node in axis Y DJZ : Rigid end offset distance measured from J node in axis Z DKX : Rigid end offset distance measured from K node in axis X DKY : Rigid end offset distance measured from K node in axis Y DKZ : Rigid end offset distance measured from K node in axis Z dL : Tapered member section depth at K end of member Ig factor : Inertia reduction factor (Effective Inertia/Gross Inertia) for reinforced concrete members K22 : Effective length factor about axis 2 K33 : Effective length factor about axis 3 L22 : Member length for calculation of axial capacity L33 : Member length for calculation of axial capacity LB pos : Lateral unbraced length of the compression flange in the positive side of local axis 2 LB neg : Lateral unbraced length of the compression flange in the negative side of local axis 2 RX : Rotation about X RY : Rotation about Y RZ : Rotation about Z TO : 1 = Tension only member 0 = Normal member TX : Translation in X TY : Translation in Y TZ : Translation in Z Nodes ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Node X Y Z Rigid Floor [ft][ft][ft] ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 1 3.00 0.00 0.50 0 2 3.00 19.50 0.50 0 3 3.00 1.00 0.00 0 4 3.00 5.83 0.00 0 5 0.00 1.00 0.00 0 6 0.00 5.83 0.00 0 7 3.33 1.00 0.00 0 8 3.33 5.83 0.00 0 9 3.00 5.83 0.50 0 10 3.00 1.00 0.50 0 12 2.50 5.83 0.00 0 13 0.75 5.83 0.00 0 14 2.50 1.00 0.00 0 15 0.75 1.00 0.00 0 16 0.00 5.83 -3.33 0 17 0.00 1.00 -3.33 0 18 3.33 5.83 -3.33 0 19 3.33 1.00 -3.33 0 22 0.00 5.83 -0.75 0 23 0.00 1.00 -0.75 0 24 0.00 5.83 -2.58 0 Page1 25 0.00 1.00 -2.58 0 28 0.75 5.83 -3.33 0 29 0.75 1.00 -3.33 0 30 2.58 5.83 -3.33 0 31 2.58 1.00 -3.33 0 40 -0.50 5.83 -0.50 0 41 -0.50 1.00 -0.50 0 44 -0.40 5.83 -3.70 0 45 -0.40 1.00 -3.70 0 47 -0.50 19.50 -0.50 0 48 -0.40 19.50 -3.70 0 50 -0.50 0.00 -0.50 0 51 -0.40 0.00 -3.70 0 59 0.00 1.00 -0.50 0 60 0.00 5.83 -0.50 0 ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Restraints ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Node TX TY TZ RX RY RZ ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 12 1 1 1 0 0 0 13 1 1 1 0 0 0 14 1 1 1 0 0 0 15 1 1 1 0 0 0 22 1 1 1 0 0 0 23 1 1 1 0 0 0 24 1 1 1 0 0 0 25 1 1 1 0 0 0 28 1 1 1 0 0 0 29 1 1 1 0 0 0 30 1 1 1 0 0 0 31 1 1 1 0 0 0 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Members ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Member NJ NK Description Section Material d0 dL Ig factor [in][in] ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 1 2 1 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 2 6 8 WT 6X11 A36 0.00 0.00 0.00 3 5 7 WT 6X11 A36 0.00 0.00 0.00 6 16 6 WT 6X11 A36 0.00 0.00 0.00 7 17 5 WT 6X11 A36 0.00 0.00 0.00 8 18 16 WT 6X11 A36 0.00 0.00 0.00 9 19 17 WT 6X11 A36 0.00 0.00 0.00 10 8 18 WT 6X11 A36 0.00 0.00 0.00 11 7 19 WT 6X11 A36 0.00 0.00 0.00 19 48 51 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 20 47 50 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Page2 Orientation of local axes ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Member Rotation Axes23 NX NY NZ [Deg] ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 1 315.00 0 0.00 0.00 0.00 2 270.00 0 0.00 0.00 0.00 3 270.00 0 0.00 0.00 0.00 6 270.00 0 0.00 0.00 0.00 7 270.00 0 0.00 0.00 0.00 8 270.00 0 0.00 0.00 0.00 9 270.00 0 0.00 0.00 0.00 10 270.00 0 0.00 0.00 0.00 11 270.00 0 0.00 0.00 0.00 19 315.00 0 0.00 0.00 0.00 20 315.00 0 0.00 0.00 0.00 ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Page3 Current Date: 3/4/2021 4:52 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Chimney Mount.retx Current Date: 3/4/2021 4:52 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Chimney Mount.retx Analysis result Reactions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Direction of positive forces and moments Forces [Kip] Moments [Kip*ft] Node FX FY FZ MX MY MZ ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Condition LC1=1.2D+Wo 24 0.13657 -0.43396 0.94712 0.00000 0.00000 0.00000 28 -0.15553 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____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Note.-lc is the controlling load condition Direction of positive forces and moments Page11 Envelope of nodal reactions for : LC1=1.2D+Wo LC2=1.2D+W30 LC3=1.2D+W60 LC4=1.2D+W90 LC5=1.2D+W120 LC6=1.2D+W150 LC7=1.2D-Wo LC8=1.2D-W30 LC9=1.2D-W60 LC10=1.2D-W90 LC11=1.2D-W120 LC12=1.2D-W150 LC13=0.9D+Wo LC14=0.9D+W30 LC15=0.9D+W60 LC16=0.9D+W90 LC17=0.9D+W120 LC18=0.9D+W150 LC19=0.9D-Wo LC20=0.9D-W30 LC21=0.9D-W60 LC22=0.9D-W90 LC23=0.9D-W120 LC24=0.9D-W150 LC25=1.2D+Di+WI0 LC26=1.2D+Di+WI30 LC27=1.2D+Di+WI60 LC28=1.2D+Di+WI90 LC29=1.2D+Di+WI120 LC30=1.2D+Di+WI150 LC31=1.2D+Di-WI0 LC32=1.2D+Di-WI30 LC33=1.2D+Di-WI60 LC34=1.2D+Di-WI90 LC35=1.2D+Di-WI120 LC36=1.2D+Di-WI150 Forces Moments Node Fx lc Fy lc Fz lc Mx lc My lc Mz lc [Kip][Kip][Kip][Kip*ft][Kip*ft][Kip*ft] -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 24 Max 0.155 LC12 0.708 LC7 0.947 LC1 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.152 LC6 -0.465 LC13 -0.918 LC19 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 28 Max 0.720 LC4 0.688 LC10 0.257 LC6 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.689 LC22 -0.433 LC16 -0.248 LC24 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 30 Max 0.057 LC24 0.100 LC2 0.302 LC24 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.059 LC6 -0.095 LC20 -0.317 LC6 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 13 Max 0.380 LC2 0.945 LC7 0.174 LC6 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.364 LC20 -0.946 LC1 -0.164 LC24 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 12 Max 0.545 LC5 2.020 LC1 0.739 LC13 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.552 LC11 -1.603 LC19 -0.779 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 22 Max 0.536 LC6 1.225 LC12 0.851 LC1 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.495 LC24 -0.966 LC18 -0.861 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 25 Max 0.061 LC6 0.725 LC1 0.465 LC19 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.064 LC12 -0.486 LC19 -0.494 LC1 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 29 Max 0.332 LC24 0.661 LC2 0.111 LC24 0.00000 LC1 0.00000 LC1 0.00000 LC1 Page12 Min -0.364 LC6 -0.412 LC20 -0.120 LC6 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 31 Max 0.033 LC6 0.150 LC8 0.187 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.031 LC24 -0.142 LC14 -0.171 LC13 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 23 Max 0.260 LC24 1.164 LC6 0.464 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.301 LC6 -0.909 LC24 -0.454 LC1 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 15 Max 0.165 LC20 0.746 LC1 0.086 LC13 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.181 LC2 -0.750 LC7 -0.096 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 14 Max 0.290 LC12 1.997 LC7 0.463 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.282 LC6 -1.580 LC13 -0.423 LC13 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Page13 Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC CHECK EPOXY ANCHOR CONNECTION CAPACITY → EXISTING ANCHORS AT PENTHOUSE MOUNT Reference:Hilti North American Product Technical Guide, 19th Edition Epoxy Type =HIT-HY20 (Assumed) Anchor Diameter =1/2 in. (HAS-E Threaded Rod) Embedment Depth = 6 in. (Assumed) Allowable Loads (lbs) Tensile Load 745 Shear Load 930 TENSILE FORCES Reaction F =1966 lbs. (See Bentley Output) SHEAR FORCES Reactions in X direction:965 lbs. (See Bentley Output) Reactions in Y direction:3076 lbs. (See Bentley Output) Resultant:3224 lbs. No. of Supports =1 No. of Anchors / Support =2 Tension Design Load / Anchor = ft=983.00 lbs.>745 lbs.Therefore, NOT OK ! Shear Design Load / Anchor= fv=1611.91 lbs.>930 lbs.Therefore, NOT OK ! CHECK COMBINED TENSION AND SHEAR ft / FT +fv / FV ≤1.0 1.319 + 1.733 =3.053 >1.0 Therefore, NOT OK ! 1 1 930 Spacing Reduct. Factor Edge Reduct. Factor Reduced Loads (lbs) 1 1 745 Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC CHECK CONNECTION CAPACITY (Worst Case) - ANCHORS AT PENTHOUSE MOUNT Reference:AISC Steel Construction Manual 14th Edition (ASD) Bolt Type =A36 1/2"Threaded Rod Allowable Tensile Load = FTall =4271 lbs. Allowable Shear Load = FVall=2562 lbs. TENSILE FORCES Reaction F =1966 lbs.(See Bentley Output) SHEAR FORCES Reactions in X direction:1305 lbs.(See Bentley Output) Reactions in Y direction:3448 lbs.(See Bentley Output) Resultant:3687 lbs. No. of Supports =1 No. of Bolts / Support =2 Tension Design Load /Bolts = ft=983.00 lbs.<4271 lbs.Therefore, OK ! Shear Design Load / Bolts= fv=1843.35 lbs.<2562 lbs.Therefore, OK ! CHECK COMBINED TENSION AND SHEAR ft / FT +fv / FV ≤1.0 0.230 + 0.719 =0.950 <1.0 Therefore, OK ! Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC CHECK EPOXY ANCHOR CONNECTION CAPACITY → PROPOSED ANCHORS AT PENTHOUSE MOUNT Reference:Hilti North American Product Technical Guide, 19th Edition Epoxy Type =HIT-HY 270 Anchor Diameter =3/4 in. (HAS Threaded Rod) Embedment Depth = 8 in. Allowable Loads (lbs) Tensile Load 1575 Shear Load 1985 TENSILE FORCES Reaction F =1966 lbs. (See Bentley Output) SHEAR FORCES Reactions in X direction:965 lbs. (See Bentley Output) Reactions in Y direction:3076 lbs. (See Bentley Output) Resultant:3224 lbs. No. of Supports =1 No. of Anchors / Support =2 Tension Design Load / Anchor = ft=983.00 lbs.<1575 lbs.Therefore, OK ! Shear Design Load / Anchor= fv=1611.91 lbs.<1985 lbs.Therefore, OK ! CHECK COMBINED TENSION AND SHEAR ft / FT +fv / FV ≤1.0 0.624 + 0.812 =1.436 >1.0 Therefore, NOT OK ! Spacing Reduct. Factor 1 1 Edge Reduct. Factor 1 1 Conc. Thickness Reduct. Factor 1 1 Reduced Loads (lbs) 1575 1985 Chimney Antenna Mount Calculations (Existing Conditions) Current Date: 3/4/2021 4:54 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Penthouse Mount.retx Current Date: 3/4/2021 4:54 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Penthouse Mount.retx Current Date: 3/4/2021 4:54 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Penthouse Mount.retx Current Date: 3/4/2021 4:54 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Penthouse Mount.retx Current Date: 3/4/2021 4:54 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Penthouse Mount.retx Load data ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ GLOSSARY Comb : Indicates if load condition is a load combination Load Conditions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition Description Comb.Category ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- D Dead Load No DL Wo Wind Load (NO ICE)No WIND W30 WL 30deg No WIND W60 WL 60deg No WIND W90 WL 90deg No WIND W120 WL 120deg No WIND W150 WL 150deg No WIND Di Ice Load No LL WI0 WL ICE 0deg No WIND WI30 WL ICE 30deg No WIND WI60 WL ICE 60deg No WIND WI90 WL ICE 90deg No WIND WI120 WL ICE 120deg No WIND WI150 WL ICE 150deg No WIND ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Distributed force on members ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition Member Dir1 Val1 Val2 Dist1 %Dist2 % [Kip/ft][Kip/ft][ft][ft] ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Wo 5 z -0.012 -0.012 35.00 Yes 100.00 Yes 8 z -0.012 -0.012 20.00 Yes 100.00 Yes W30 5 z -0.012 -0.012 35.00 Yes 100.00 Yes 8 z -0.012 -0.012 20.00 Yes 100.00 Yes W60 4 x -0.012 -0.012 0.00 No 100.00 Yes 3 x -0.012 -0.012 0.00 No 100.00 Yes 5 x -0.012 -0.012 0.00 No 100.00 Yes 8 x -0.012 -0.012 0.00 No 100.00 Yes W90 4 x -0.012 -0.012 0.00 No 100.00 Yes 3 x -0.012 -0.012 0.00 No 100.00 Yes 5 x -0.012 -0.012 0.00 No 100.00 Yes 8 x -0.012 -0.012 0.00 No 100.00 Yes W120 4 x -0.012 -0.012 0.00 No 100.00 Yes 3 x -0.012 -0.012 0.00 No 100.00 Yes Page1 5 x -0.012 -0.012 0.00 No 100.00 Yes 8 x -0.012 -0.012 0.00 No 100.00 Yes W150 5 z 0.012 0.012 35.00 Yes 100.00 Yes 8 z 0.012 0.012 20.00 Yes 100.00 Yes Di 4 y -0.006 -0.006 0.00 No 100.00 Yes 3 y -0.006 -0.006 0.00 No 100.00 Yes 5 y -0.006 -0.006 0.00 No 100.00 Yes 8 y -0.006 -0.006 0.00 No 100.00 Yes ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Concentrated forces on members ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition Member Dir1 Value1 Dist1 % [Kip][ft] -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- D 4 y -0.075 1.50 No y -0.075 8.50 No y -0.044 12.50 No y -0.071 16.50 No 3 y -0.075 1.50 No y -0.075 8.50 No y -0.044 12.50 No y -0.071 16.50 No 5 y -0.067 1.75 No y -0.067 5.25 No 8 y -0.052 1.00 No y -0.052 3.00 No Wo 4 z -0.338 1.50 No z -0.338 8.50 No z -0.055 12.50 No z -0.066 16.50 No 3 z -0.338 1.50 No z -0.338 8.50 No z -0.055 12.50 No z -0.066 16.50 No 5 z -0.109 1.75 No z -0.109 5.25 No 8 z -0.095 1.00 No z -0.095 3.00 No W30 4 3 -0.29 1.50 No 3 -0.29 8.50 No 3 -0.047 12.50 No 3 -0.061 16.50 No 3 3 -0.29 1.50 No 3 -0.29 8.50 No 3 -0.047 12.50 No 3 -0.061 16.50 No 5 3 -0.102 1.75 No 3 -0.102 5.25 No 8 3 -0.081 1.00 No 3 -0.081 3.00 No W60 4 3 -0.194 1.50 No Page2 3 -0.194 8.50 No 3 -0.031 12.50 No 3 -0.052 16.50 No 3 3 -0.194 1.50 No 3 -0.194 8.50 No 3 -0.031 12.50 No 3 -0.052 16.50 No 5 3 -0.086 1.75 No 3 -0.086 5.25 No 8 3 -0.055 1.00 No 3 -0.055 3.00 No W90 4 x -0.146 1.50 No x -0.146 8.50 No x -0.023 12.50 No x -0.047 16.50 No 3 x -0.146 1.50 No x -0.146 8.50 No x -0.023 12.50 No x -0.047 16.50 No 5 x -0.079 1.75 No x -0.079 5.25 No 8 x -0.041 1.00 No x -0.041 3.00 No W120 4 2 -0.194 1.50 No 2 -0.194 8.50 No 2 -0.031 12.50 No 2 -0.052 16.50 No 3 2 -0.194 1.50 No 2 -0.194 8.50 No 2 -0.031 12.50 No 2 -0.052 16.50 No 5 2 -0.086 1.75 No 2 -0.086 5.25 No 8 2 -0.055 1.00 No 2 -0.055 3.00 No W150 4 2 -0.29 1.50 No 2 -0.29 8.50 No 2 -0.047 12.50 No 2 -0.061 16.50 No 3 2 -0.29 1.50 No 2 -0.29 8.50 No 2 -0.047 12.50 No 2 -0.061 16.50 No 5 2 -0.102 1.75 No 2 -0.102 5.25 No 8 2 -0.081 1.00 No 2 -0.081 3.00 No Di 4 y -0.143 1.50 No y -0.143 8.50 No y -0.026 12.50 No y -0.035 16.50 No 3 y -0.143 1.50 No y -0.143 8.50 No y -0.026 12.50 No y -0.035 16.50 No 5 y -0.053 1.75 No y -0.053 5.25 No 8 y -0.043 1.00 No y -0.043 3.00 No WI0 4 z -0.059 1.50 No Page3 z -0.059 8.50 No z -0.011 12.50 No z -0.013 16.50 No 3 z -0.059 1.50 No z -0.059 8.50 No z -0.011 12.50 No z -0.013 16.50 No 5 z -0.021 1.75 No z -0.021 5.25 No 8 z -0.018 1.00 No z -0.018 3.00 No WI30 4 3 -0.051 1.50 No 3 -0.051 8.50 No 3 -0.01 12.50 No 3 -0.013 16.50 No 3 3 -0.051 1.50 No 3 -0.051 8.50 No 3 -0.01 12.50 No 3 -0.013 16.50 No 5 3 -0.019 1.75 No 3 -0.019 5.25 No 8 3 -0.015 1.00 No 3 -0.015 3.00 No WI60 4 3 -0.036 1.50 No 3 -0.036 8.50 No 3 -0.007 12.50 No 3 -0.011 16.50 No 3 3 -0.036 1.50 No 3 -0.036 8.50 No 3 -0.007 12.50 No 3 -0.011 16.50 No 5 3 -0.017 1.75 No 3 -0.017 5.25 No 8 3 -0.011 1.00 No 3 -0.011 3.00 No WI90 4 x -0.028 1.50 No x -0.028 8.50 No x -0.006 12.50 No x -0.01 16.50 No 3 x -0.028 1.50 No x -0.028 8.50 No x -0.006 12.50 No x -0.01 16.50 No 5 x -0.016 1.75 No x -0.016 5.25 No 8 x -0.009 1.00 No x -0.009 3.00 No WI120 4 2 -0.036 1.50 No 2 -0.036 8.50 No 2 -0.007 12.50 No 2 -0.011 16.50 No 3 2 -0.036 1.50 No 2 -0.036 8.50 No 2 -0.007 12.50 No 2 -0.011 16.50 No 5 2 -0.017 1.75 No 2 -0.017 5.25 No 8 2 -0.011 1.00 No 2 -0.011 3.00 No WI150 4 2 -0.051 1.50 No Page4 2 -0.051 8.50 No 2 -0.01 12.50 No 2 -0.013 16.50 No 3 2 -0.051 1.50 No 2 -0.051 8.50 No 2 -0.01 12.50 No 2 -0.013 16.50 No 5 2 -0.019 1.75 No 2 -0.019 5.25 No 8 2 -0.015 1.00 No 2 -0.015 3.00 No -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Self weight multipliers for load conditions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Self weight multiplier Condition Description Comb.MultX MultY MultZ ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ D Dead Load No 0.00 -1.00 0.00 Wo Wind Load (NO ICE)No 0.00 0.00 0.00 W30 WL 30deg No 0.00 0.00 0.00 W60 WL 60deg No 0.00 0.00 0.00 W90 WL 90deg No 0.00 0.00 0.00 W120 WL 120deg No 0.00 0.00 0.00 W150 WL 150deg No 0.00 0.00 0.00 Di Ice Load No 0.00 0.00 0.00 WI0 WL ICE 0deg No 0.00 0.00 0.00 WI30 WL ICE 30deg No 0.00 0.00 0.00 WI60 WL ICE 60deg No 0.00 0.00 0.00 WI90 WL ICE 90deg No 0.00 0.00 0.00 WI120 WL ICE 120deg No 0.00 0.00 0.00 WI150 WL ICE 150deg No 0.00 0.00 0.00 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Earthquake (Dynamic analysis only) ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition a/g Ang.Damp. [Deg][%] -------------------------------------------------------------------------------------------------------------------------------------------------------- D 0.00 0.00 0.00 Wo 0.00 0.00 0.00 W30 0.00 0.00 0.00 W60 0.00 0.00 0.00 W90 0.00 0.00 0.00 W120 0.00 0.00 0.00 W150 0.00 0.00 0.00 Di 0.00 0.00 0.00 WI0 0.00 0.00 0.00 WI30 0.00 0.00 0.00 WI60 0.00 0.00 0.00 WI90 0.00 0.00 0.00 WI120 0.00 0.00 0.00 WI150 0.00 0.00 0.00 -------------------------------------------------------------------------------------------------------------------------------------------------------- Page5 Page6 Current Date: 3/4/2021 4:55 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Penthouse Mount.retx Steel Code Check ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Report: Summary - Group by member Load conditions to be included in design : LC1=1.2D+Wo LC2=1.2D+W30 LC3=1.2D+W60 LC4=1.2D+W90 LC5=1.2D+W120 LC6=1.2D+W150 LC7=1.2D-Wo LC8=1.2D-W30 LC9=1.2D-W60 LC10=1.2D-W90 LC11=1.2D-W120 LC12=1.2D-W150 LC13=0.9D+Wo LC14=0.9D+W30 LC15=0.9D+W60 LC16=0.9D+W90 LC17=0.9D+W120 LC18=0.9D+W150 LC19=0.9D-Wo LC20=0.9D-W30 LC21=0.9D-W60 LC22=0.9D-W90 LC23=0.9D-W120 LC24=0.9D-W150 LC25=1.2D+Di+WI0 LC26=1.2D+Di+WI30 LC27=1.2D+Di+WI60 LC28=1.2D+Di+WI90 LC29=1.2D+Di+WI120 LC30=1.2D+Di+WI150 LC31=1.2D+Di-WI0 LC32=1.2D+Di-WI30 LC33=1.2D+Di-WI60 LC34=1.2D+Di-WI90 LC35=1.2D+Di-WI120 LC36=1.2D+Di-WI150 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Description Section Member Ctrl Eq.Ratio Status Reference ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ PIPE 3x0.216 4 LC7 at 68.75%1.45 N.G. 3 LC7 at 60.42%1.16 N.G. 5 LC10 at 68.75%0.68 OK 8 LC7 at 68.75%0.69 OK ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Page1 Current Date: 3/4/2021 4:55 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Penthouse Mount.retx Geometry data ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ GLOSSARY Cb22, Cb33 : Moment gradient coefficients Cm22, Cm33 : Coefficients applied to bending term in interaction formula d0 : Tapered member section depth at J end of member DJX : Rigid end offset distance measured from J node in axis X DJY : Rigid end offset distance measured from J node in axis Y DJZ : Rigid end offset distance measured from J node in axis Z DKX : Rigid end offset distance measured from K node in axis X DKY : Rigid end offset distance measured from K node in axis Y DKZ : Rigid end offset distance measured from K node in axis Z dL : Tapered member section depth at K end of member Ig factor : Inertia reduction factor (Effective Inertia/Gross Inertia) for reinforced concrete members K22 : Effective length factor about axis 2 K33 : Effective length factor about axis 3 L22 : Member length for calculation of axial capacity L33 : Member length for calculation of axial capacity LB pos : Lateral unbraced length of the compression flange in the positive side of local axis 2 LB neg : Lateral unbraced length of the compression flange in the negative side of local axis 2 RX : Rotation about X RY : Rotation about Y RZ : Rotation about Z TO : 1 = Tension only member 0 = Normal member TX : Translation in X TY : Translation in Y TZ : Translation in Z Nodes ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Node X Y Z Rigid Floor [ft][ft][ft] ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 2 0.00 1.00 0.00 0 4 0.00 1.00 0.50 0 5 0.00 19.50 0.50 0 6 0.00 0.00 0.50 0 15 5.00 5.83 0.00 0 16 5.00 1.00 0.00 0 17 5.00 5.83 0.50 0 18 5.00 1.00 0.50 0 19 5.00 19.50 0.50 0 20 5.00 0.00 0.50 0 21 15.00 5.83 0.00 0 22 15.00 1.00 0.00 0 23 15.00 5.83 0.50 0 24 15.00 1.00 0.50 0 25 15.00 19.50 0.50 0 26 15.00 0.00 0.50 0 27 10.00 5.83 0.00 0 28 10.00 1.00 0.00 0 29 10.00 5.83 0.50 0 30 10.00 1.00 0.50 0 31 10.00 19.50 0.50 0 Page1 32 10.00 0.00 0.50 0 3 0.00 7.50 0.50 0 1 0.00 7.50 0.00 0 ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Restraints ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Node TX TY TZ RX RY RZ ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 2 1 1 1 0 1 0 15 1 1 1 0 1 0 16 1 1 1 0 1 0 21 1 1 1 0 1 0 22 1 1 1 0 1 0 27 1 1 1 0 1 0 28 1 1 1 0 1 0 1 1 1 1 0 1 0 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Members ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Member NJ NK Description Section Material d0 dL Ig factor [in][in] ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 4 19 20 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 3 5 6 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 5 31 32 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 8 25 26 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Orientation of local axes ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Member Rotation Axes23 NX NY NZ [Deg] ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 4 315.00 0 0.00 0.00 0.00 3 315.00 0 0.00 0.00 0.00 5 315.00 0 0.00 0.00 0.00 8 315.00 0 0.00 0.00 0.00 ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Page2 Current Date: 3/4/2021 4:55 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Penthouse Mount.retx Current Date: 3/4/2021 4:55 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\MSA\4BSS362A - Penthouse Mount.retx Analysis result Reactions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Direction of positive forces and moments Forces [Kip] Moments [Kip*ft] Node FX FY FZ MX MY MZ ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Condition LC1=1.2D+Wo 1 0.00000 3.07592 1.44841 0.00000 0.00000 0.00000 15 0.00000 3.44811 1.95942 0.00000 0.00000 0.00000 27 0.00000 1.51630 0.82140 0.00000 0.00000 0.00000 21 0.00000 1.65672 0.89352 0.00000 0.00000 0.00000 2 0.00000 -2.58612 -0.65141 0.00000 0.00000 0.00000 16 0.00000 -2.95830 -1.16242 0.00000 0.00000 0.00000 28 0.00000 -1.18369 -0.45130 0.00000 0.00000 0.00000 22 0.00000 -1.36011 -0.51632 0.00000 0.00000 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 0.00000 1.60883 2.34130 0.00000 0.00000 0.00000 Condition LC2=1.2D+W30 1 0.90341 1.96452 0.86475 0.00000 0.35709 0.00000 15 1.22209 2.18965 1.16995 0.00000 0.45359 0.00000 27 0.45520 1.10518 0.58907 0.00000 0.16584 0.00000 21 0.39775 1.17437 0.63197 0.00000 0.14399 0.00000 2 -0.41692 -1.47471 -0.37826 0.00000 -0.11333 0.00000 16 -0.73560 -1.69984 -0.68346 0.00000 -0.20941 0.00000 28 -0.31095 -0.77257 -0.29272 0.00000 -0.09355 0.00000 22 -0.28320 -0.87776 -0.33021 0.00000 -0.08655 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 1.23178 1.60883 1.57108 0.00000 0.61768 0.00000 Condition LC3=1.2D+W60 1 0.92373 1.39091 0.56820 0.00000 0.37000 0.00000 15 1.24939 1.54247 0.76881 0.00000 0.46913 0.00000 27 0.81277 0.84788 0.34897 0.00000 0.30395 0.00000 21 0.69868 0.64876 0.23922 0.00000 0.26174 0.00000 2 -0.35668 -0.90110 -0.23516 0.00000 -0.08613 0.00000 16 -0.68234 -1.05267 -0.43577 0.00000 -0.18499 0.00000 28 -0.45714 -0.51527 -0.22735 0.00000 -0.12595 0.00000 22 -0.38690 -0.35216 -0.16144 0.00000 -0.10574 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 1.80150 1.60883 0.86550 0.00000 0.90200 0.00000 Page1 Condition LC4=1.2D+W90 1 0.96498 0.24794 -0.03747 0.00000 0.38648 0.00000 15 1.30525 0.24802 -0.05042 0.00000 0.48990 0.00000 27 0.92767 0.16889 -0.03412 0.00000 0.34564 0.00000 21 0.71338 0.15055 -0.03038 0.00000 0.26697 0.00000 2 -0.36898 0.24187 0.03747 0.00000 -0.08851 0.00000 16 -0.70925 0.24179 0.05042 0.00000 -0.19195 0.00000 28 -0.53567 0.16371 0.03412 0.00000 -0.14966 0.00000 22 -0.39738 0.14606 0.03038 0.00000 -0.10899 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 1.90000 1.60883 0.00000 0.00000 0.94989 0.00000 Condition LC5=1.2D+W120 1 0.92399 -0.89978 -0.64304 0.00000 0.36952 0.00000 15 1.24990 -1.04947 -0.86952 0.00000 0.46835 0.00000 27 0.81294 -0.51097 -0.41718 0.00000 0.30372 0.00000 21 0.69879 -0.34814 -0.29997 0.00000 0.26161 0.00000 2 -0.35694 1.38959 0.30999 0.00000 -0.08638 0.00000 16 -0.68285 1.53928 0.53648 0.00000 -0.18554 0.00000 28 -0.45732 0.84358 0.29556 0.00000 -0.12614 0.00000 22 -0.38701 0.64475 0.22219 0.00000 -0.10586 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 1.80150 1.60883 -0.86550 0.00000 0.89929 0.00000 Condition LC6=1.2D+W150 1 0.90381 -1.47941 -0.93946 0.00000 0.35641 0.00000 15 1.22287 -1.70049 -1.27049 0.00000 0.45249 0.00000 27 0.45535 -0.76898 -0.65723 0.00000 0.16564 0.00000 21 0.39789 -0.87519 -0.69263 0.00000 0.14381 0.00000 2 -0.41732 1.96922 0.45297 0.00000 -0.11373 0.00000 16 -0.73638 2.19029 0.78400 0.00000 -0.21027 0.00000 28 -0.31110 1.10158 0.36088 0.00000 -0.09371 0.00000 22 -0.28334 1.17179 0.39088 0.00000 -0.08671 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 1.23178 1.60883 -1.57108 0.00000 0.61392 0.00000 Condition LC7=1.2D-Wo 1 0.00000 -2.60941 -1.52273 0.00000 0.00000 0.00000 15 0.00000 -2.97083 -2.05946 0.00000 0.00000 0.00000 27 0.00000 -1.18186 -0.88948 0.00000 0.00000 0.00000 21 0.00000 -1.35986 -0.95410 0.00000 0.00000 0.00000 2 0.00000 3.09922 0.72573 0.00000 0.00000 0.00000 16 0.00000 3.46063 1.26246 0.00000 0.00000 0.00000 28 0.00000 1.51446 0.51938 0.00000 0.00000 0.00000 22 0.00000 1.65646 0.57690 0.00000 0.00000 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 0.00000 1.60883 -2.34130 0.00000 0.00000 0.00000 Condition LC8=1.2D-W30 1 -0.90381 -1.47941 -0.93946 0.00000 -0.35641 0.00000 15 -1.22287 -1.70049 -1.27049 0.00000 -0.45249 0.00000 27 -0.45535 -0.76898 -0.65723 0.00000 -0.16564 0.00000 21 -0.39789 -0.87519 -0.69263 0.00000 -0.14381 0.00000 2 0.41732 1.96922 0.45297 0.00000 0.11373 0.00000 16 0.73638 2.19029 0.78400 0.00000 0.21027 0.00000 28 0.31110 1.10158 0.36088 0.00000 0.09371 0.00000 22 0.28334 1.17179 0.39088 0.00000 0.08671 0.00000 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------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM -0.22486 2.49483 0.22486 0.00000 -0.11246 0.00000 Envelope for nodal reactions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Note.-lc is the controlling load condition Direction of positive forces and moments Envelope of nodal reactions for : LC1=1.2D+Wo LC2=1.2D+W30 LC3=1.2D+W60 LC4=1.2D+W90 LC5=1.2D+W120 LC6=1.2D+W150 LC7=1.2D-Wo Page8 LC8=1.2D-W30 LC9=1.2D-W60 LC10=1.2D-W90 LC11=1.2D-W120 LC12=1.2D-W150 LC13=0.9D+Wo LC14=0.9D+W30 LC15=0.9D+W60 LC16=0.9D+W90 LC17=0.9D+W120 LC18=0.9D+W150 LC19=0.9D-Wo LC20=0.9D-W30 LC21=0.9D-W60 LC22=0.9D-W90 LC23=0.9D-W120 LC24=0.9D-W150 LC25=1.2D+Di+WI0 LC26=1.2D+Di+WI30 LC27=1.2D+Di+WI60 LC28=1.2D+Di+WI90 LC29=1.2D+Di+WI120 LC30=1.2D+Di+WI150 LC31=1.2D+Di-WI0 LC32=1.2D+Di-WI30 LC33=1.2D+Di-WI60 LC34=1.2D+Di-WI90 LC35=1.2D+Di-WI120 LC36=1.2D+Di-WI150 Forces Moments Node Fx lc Fy lc Fz lc Mx lc My lc Mz lc [Kip][Kip][Kip][Kip*ft][Kip*ft][Kip*ft] -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 1 Max 0.965 LC4 3.076 LC1 1.455 LC13 0.00000 LC1 0.38648 LC4 0.00000 LC1 Min -0.965 LC10 -2.661 LC19 -1.523 LC7 0.00000 LC1 -0.38648 LC10 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 15 Max 1.305 LC4 3.448 LC1 1.966 LC13 0.00000 LC1 0.48990 LC4 0.00000 LC1 Min -1.305 LC10 -3.017 LC19 -2.059 LC7 0.00000 LC1 -0.48990 LC10 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 27 Max 0.928 LC4 1.516 LC1 0.827 LC13 0.00000 LC1 0.34564 LC4 0.00000 LC1 Min -0.928 LC10 -1.217 LC19 -0.889 LC7 0.00000 LC1 -0.34564 LC10 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 21 Max 0.713 LC4 1.657 LC1 0.898 LC13 0.00000 LC1 0.26697 LC4 0.00000 LC1 Min -0.713 LC10 -1.390 LC19 -0.954 LC7 0.00000 LC1 -0.26697 LC10 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 2 Max 0.417 LC8 3.099 LC7 0.726 LC7 0.00000 LC1 0.11373 LC8 0.00000 LC1 Min -0.417 LC6 -2.636 LC13 -0.658 LC13 0.00000 LC1 -0.11373 LC6 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 16 Max 0.736 LC8 3.461 LC7 1.262 LC7 0.00000 LC1 0.21027 LC8 0.00000 LC1 Min -0.736 LC6 -3.003 LC13 -1.169 LC13 0.00000 LC1 -0.21027 LC6 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 28 Max 0.536 LC10 1.514 LC7 0.519 LC7 0.00000 LC1 0.14966 LC10 0.00000 LC1 Min -0.536 LC4 -1.218 LC13 -0.457 LC13 0.00000 LC1 -0.14966 LC4 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 22 Max 0.397 LC10 1.656 LC7 0.577 LC7 0.00000 LC1 0.10899 LC10 0.00000 LC1 Min -0.397 LC4 -1.389 LC13 -0.521 LC13 0.00000 LC1 -0.10899 LC4 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Page9 Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC CHECK EPOXY ANCHOR CONNECTION CAPACITY → EXISTING ANCHORS AT CHIMNEY MOUNT Reference:Hilti North American Product Technical Guide, 19th Edition Epoxy Type =HIT-HY20 (Assumed) Anchor Diameter =3/4 in.(HAS-E Threaded Rod) Embedment Depth = 8 in.(Assumed) Allowable Loads (lbs) Tensile Load 1400 Shear Load 1800 TENSILE FORCES Reaction F =779 lbs.(See Bentley Output) SHEAR FORCES Reactions in X direction:552 lbs.(See Bentley Output) Reactions in Y direction:2020 lbs.(See Bentley Output) Resultant:2094 lbs. No. of Supports =1 No. of Anchors / Support =1 Tension Design Load / Anchor = ft=779.00 lbs.<1400 lbs.Therefore, OK ! Shear Design Load / Anchor= fv=2094.06 lbs.>1800 lbs.Therefore, NOT OK ! CHECK COMBINED TENSION AND SHEAR ft / FT +fv / FV ≤1.0 0.556 + 1.163 =1.720 >1.0 Therefore, NOT OK ! 1 1 1800 Spacing Reduct. Factor Edge Reduct. Factor Reduced Loads (lbs) 1 1 1400 Reference Documents SCOPE OF WORK: Hudson Design Group LLC (HDG) has been authorized by T-Mobile to conduct a structural evaluation of the structure supporting the proposed equipment located in the areas depicted in the latest HDG construction drawings. This report represents this office’s findings, conclusions and recommendations pertaining to the support of T-Mobile’s proposed antennas listed below. This office conducted an on-site visual survey of the above site on September 2, 2020. Attendees included Edvin Broka (HDG – Lead Designer). The following documents were used for our reference: HDG Mount Structural Analysis dated March 3, 2021. Previous HDG Construction Drawings dated December 15, 2011. Previous HDG Structural Analysis dated November 14, 2011. CONCLUSION SUMMARY: Based on our evaluation, we have determined that the existing structure IS CAPABLE of supporting the proposed equipment loading. HDG recommends not installing any additional load on the existing chimney structure. HDG considers the structure marginally passing and does not recommend installing any additional, larger, or heavier equipment. Based on our evaluation, we have determined that the modified connections ARE CAPABLE of supporting the proposed equipment loading with the following modifications: Reinforce the existing and proposed pipe masts at the existing chimney with 2” std. (2.38” O.D.) pipe braces (total of 6). See latest HDG Construction Drawings for locations and details. Install new steel (total of 4) secured to the face of the existing chimney with new epoxy anchors (total of 8). See latest HDG Construction Drawings for locations and details. Reinforce the existing and proposed pipe masts at the existing penthouse with 2” std. (2.38” O.D.) pipe braces (total of 8). See latest HDG Construction Drawings for locations and details. Anchor Type Stress Ratio Pass/Fail Chimney Connection (Modified) 3/4" Epoxy Anchors 97% PASS Penthouse Connection (Modified) 3/4” Epoxy Anchors 94% PASS Based on our evaluation, we have determined that the modified mounts ARE CAPABLE of supporting the proposed equipment loading. Member Controlling Load Case Stress Ratio Pass/Fail Chimney Mount (Modified) 31 LC7 58% PASS Penthouse Mount (Modified) 4 LC10 98% PASS APPURTENANCE CONFIGURATION: Appurtenances Dimensions Weight **Elevation Mount (3) AIR6449 B41 Antennas 33.1”x20.5”x8.5” 103 lbs 88’-0” Pipe Mast (3) AIR 32 B66A B2A Antennas 56.6”x12.9”x8.7” 133 lbs 87’-0” Pipe Mast (3) APXVAALL24_43-U- NA20 Antennas 95.9”x24.0”x8.5” 150 lbs 86’-0” Pipe Mast (3) 4415 RRH’s 14.9”x13.2”x5.4” 44 lbs -- Pipe Mast (3) 4449 B71+B85 RRH’s 17.9”x13.2”x9.5” 71 lbs -- Pipe Mast (1) 6160 Cabinet 63.0”x25.6”x33.5” 1500 lbs -- Equipment Room (1) B160 Cabinet 63.0”x26.0”x34.0” 2000 lbs -- Equipment Room (1) SFX17-2822 Cabinet 37.0”x28.2”x18.0” 500 lbs -- Equipment Room * Proposed equipment shown in bold. ** Elevation to antenna centerline. DESIGN CRITERIA: International Building Code (IBC) 2015 with Massachusetts State Building Code 9 th Edition, and ASCE 7-10 (Minimum Design Loads for Buildings and Other Structures). Wind Reference Wind Speed: 127 mph (780 CMR Table 1604.11) Exposure Category: B (ASCE 7-10 Chapter 26) Risk Category: II (ASCE 7-10 Table 1.5-1) Snow Ground Snow, Pg: 50 (780 CMR Table 1604.11) Importance Factor (Is): 1.0 (ASCE 7-10 Table 1.5-2) Exposure Factor (Ce): 1.0 (Partially Exposed, Table 7-2) Thermal Factor (Ct): 1.0 (ASCE 7-10 Table 7-3) Flat Roof Snow Load: 35 psf (ASCE 7-10 Equation 7.3-1) Min. Flat Roof Snow Load: 30 psf (780 CMR Table 1604.11) EIA/TIA-222-H Structural Standards for Steel Antenna Towers and Antenna Supporting Structures Wind City/Town: Salem County: Essex Wind Load: 120 mph (TIA-222-H Figure B-2) Ice Design Ice Thickness (ti): 1.0 in (TIA-222-H Figure B-9) Structure Class: II (TIA-222-H Table 2-1) Importance Factor (Ii): 1.0 (TIA-222-H Table 2-3) Factored Thickness of Radial Ice (tiz): 1.10 in (TIA-222-H Sec. 2.6.10) EXISTING PENTHOUSE WALL CONSTRUCTION: The existing penthouse wall construction consists of masonry brick and wood framing. ANTENNA/RRH SUPPORT RECOMMENDATIONS:  The proposed antennas and RRH’s are proposed to be mounted on new and existing pipe masts installed on new and existing angle mounts secured to the existing penthouse with new and existing thru-bolts and/or epoxy anchors. Reference the latest set of HDG Construction Drawings for details and locations.  The proposed antennas and RRH’s are proposed to be mounted on new and existing pipe masts installed on new and existing angle mounts secured to the existing chimney with epoxy anchors. EQUIPMENT RECOMMENDATIONS: The Verizon equipment is proposed to be installed in the existing equipment room located in the basement of the existing building. Limitations and Assumptions: 1. Reference the latest HDG construction drawings for all the equipment locations and details. 2. All detail requirements will be designed and furnished in the construction drawings. 3. All structural members and their connections are assumed to be in good condition and are free from defects with no deterioration to its member capacities. 4. HDG is not responsible for any modifications completed prior to and hereafter which HDG was not directly involved. 5. All antennas, coax cables and waveguide cables are assumed to be properly installed and supported as per the manufacturer requirements. 6. If field conditions differ from what is assumed in this report, then the engineer of record is to be notified as soon as possible. FIELD PHOTOS: Photo 1: Sample photo illustrating the proposed location of the Alpha sector. Photo 2: Sample photo illustrating the proposed locations of the Beta and Gamma sectors at the existing penthouse. FIELD PHOTOS (CONT.): Photo 3: Sample photo illustrating the proposed locations of the Beta and Gamma sectors at the existing chimney. Photo 4: Sample photo illustrating existing wall constructions within the penthouse. FIELD PHOTOS (CONT.): Photo 5: Sample photo illustrating existing framing within the penthouse. Photo 6: Sample photo illustrating the existing equipment cabinets (to be removed). Wind & Ice Calculations Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC 2.6.5.2 Velocity Pressure Coeff: Kz= 2.01 (z/zg) 2/α z= 88 (ft) zg=1200 (ft) Kz=0.953 α= 7.0 Kzmin ≤ Kz ≤ 2.01 Table 2-4 Exposure Zg α Kzmin Kc B 1200 ft 7.0 0.70 0.9 C 900 ft 9.5 0.85 1.0 D 700 ft 11.5 1.03 1.1 2.6.6.2 Topographic Factor: Table 2-5 Topo. Category Kt f 2 0.43 1.25 3 0.53 2.0 4 0.72 1.5 Kzt= [1+(Kc Kt/Kh)]2 Kh= e (f*z/H) Kzt=1 Kh=1 Kc=0.9 (from Table 2-4) (If Category 1 then K zt =1.0)Kt=0 (from Table 2-5) f=0 (from Table 2-5) Category=1 z=88 zs=20 (Mean elevation of base of structure above sea level) H= 0 (Ht. of the crest above surrounding terrain) Kzt=1.00 (from 2.6.6.2.1) Ke=1.00 (from 2.6.8) 2.6.10 Design Ice Thickness Max Ice Thickness =ti = 1.00 in Importance Factor = I= 1.0 (from Table 2-3) Kiz =1.10 (from Sec. 2.6.10) tiz= ti*I*Kiz*(Kzt)0.35 tiz = 1.10 in Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC 2.6.9 Gust Effect Factor 2.6.9.1 Self Supporting Lattice Structures Gh = 1.0 Latticed Structures > 600 ft Gh = 0.85 Latticed Structures 450 ft or less Gh = 0.85 + 0.15 [h/150 - 3.0]h= ht. of structure h= 68 Gh=0.85 2.6.9.2 Guyed Masts Gh=0.85 2.6.9.3 Pole Structures Gh=1.1 2.6.9 Appurtenances Gh=1.0 2.6.9.4 Structures Supported on Other Structures (Cantilivered tubular or latticed spines, pole, structures on buildings (ht. : width ratio > 5) Gh=1.35 Gh= 1.00 2.6.11.2 Design Wind Force on Appurtenances F=qz*Gh*(EPA)A qz= 0.00256*Kz*Kzt*Ks*Ke*Kd*Vmax 2 Kz=0.953 (from 2.6.5.2) Kzt=1.0 (from 2.6.6.2.1) Ks=1.0 (from 2.6.7) qz=33.42 Ke=1.00 (from 2.6.8) qz (ice)=5.18 Kd=0.85 (from Table 2-2) qz (30)=1.86 Vmax=127 mph (Ultimate Wind Speed) Vmax (ice)=50 mph V30=30 mph Table 2-2 Structure Type Wind Direction Probability Factor, Kd Latticed structures with triangular, square or rectangular cross sections 0.85 Tubular pole structures supporting antennas enclosed within a cylindrical shroud 1.00 Tubular pole structures, latticed structures with other cross sections, appurtenances 0.95 Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Determine Ca: Table 2-9 Round C < 39 (Subcritical) 39 ≤ C ≤ 78 (Transitional) C > 78 (Supercritical) Ice Thickness =1.10 in Angle =0 (deg)Equivalent Angle =180 (deg) Appurtenances Height Width Depth Flat Area Aspect Ratio Ca Force (lbs)Force (lbs) (w/ Ice) Force (lbs) (30 mph) AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.61 1.20 189 35 11 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 4.39 1.28 218 41 12 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 4.00 1.27 676 117 38 4415 RRH 14.9 13.2 5.4 1.37 1.13 1.20 55 11 3 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.36 1.20 66 13 4 3" Pipe 3.5 12.0 0.29 0.29 1.20 12 3 1 2" Pipe 2.4 12.0 0.20 0.20 1.20 8 3 0 Note: Linear interpolation may be used for aspect ratios other than those shown. Flat Aspect Ratio is the overall length/width ratio in the plane normal to the wind direction. (Aspect ratio is independent of the spacing between support points of a linear appurtenance, 1.2 0.7 4.14/(C0.485) 0.5 3.66/(C0.415) 46.8/(C .1.0) 1.4 0.8 0.6 0.6 1.2 Aspect Ratio ≤ 2.5 Aspect Ratio = 7 Aspect Ratio ≥ 25 Force Coefficients (Ca) for Appurtenances Member Type Ca Ca Ca 2.0 Square/Rectangular HSS 1.2 - 2.8(rs) ≥ 0.85 1.4 - 4.0(rs) ≥ 0.90 2.0 - 6.0(rs) ≥ 1.25 Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Angle =30 (deg) Ice Thickness =1.10 in.Equivalent Angle =210 (deg) WIND LOADS WITH NO ICE: Appurtenances Height Width Depth Flat Area (normal) Flat Area (side) Aspect Ratio (normal) Aspect Ratio (side) Ca (normal)Ca (side) Force (lbs) (normal) Force (lbs) (side) Force (lbs) (angle) AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 189 82 162 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 218 157 203 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 676 292 580 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 55 23 47 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 66 47 61 WIND LOADS WITH ICE: AIR6449 B41 Antennas 35.3 22.7 10.7 5.57 2.62 1.55 3.30 1.20 1.24 35 17 30 AIR 32 B66A B2A Antennas 58.8 15.1 10.9 6.17 4.45 3.89 5.39 1.26 1.33 40 31 38 APXVAALL24_43-U-NA20 Antennas 98.1 26.2 10.7 17.85 7.29 3.74 9.16 1.26 1.47 116 56 101 4415 RRH 17.1 15.4 7.6 1.83 0.90 1.11 2.25 1.20 1.20 11 6 10 4449 B71+B85 RRH 20.1 15.4 11.7 2.15 1.63 1.31 1.72 1.20 1.20 13 10 13 WIND LOADS AT 30 MPH: AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 11 5 9 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 12 9 11 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 38 16 32 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 3 1 3 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 4 3 3 WIND LOADS Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Angle =60 (deg) Ice Thickness =1.10 in.Equivalent Angle =240 (deg) WIND LOADS WITH NO ICE: Appurtenances Height Width Depth Flat Area (normal) Flat Area (side) Aspect Ratio (normal) Aspect Ratio (side) Ca (normal) Ca (side) Force (lbs) (normal) Force (lbs) (side) Force (lbs) (angle) AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 189 82 109 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 218 157 172 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 676 292 388 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 55 23 31 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 66 47 52 WIND LOADS WITH ICE: AIR6449 B41 Antennas 35.3 22.7 10.7 5.57 2.62 1.55 3.30 1.20 1.24 35 17 21 AIR 32 B66A B2A Antennas 58.8 15.1 10.9 6.17 4.45 3.89 5.39 1.26 1.33 40 31 33 APXVAALL24_43-U-NA20 Antennas 98.1 26.2 10.7 17.85 7.29 3.74 9.16 1.26 1.47 116 56 71 4415 RRH 17.1 15.4 7.6 1.83 0.90 1.11 2.25 1.20 1.20 11 6 7 4449 B71+B85 RRH 20.1 15.4 11.7 2.15 1.63 1.31 1.72 1.20 1.20 13 10 11 WIND LOADS AT 30 MPH: AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 11 5 6 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 12 9 10 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 38 16 22 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 3 1 2 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 4 3 3 WIND LOADS Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Angle =90 (deg) Ice Thickness =1.10 in.Equivalent Angle =270 (deg) WIND LOADS WITH NO ICE: Appurtenances Height Width Depth Flat Area (normal) Flat Area (side) Aspect Ratio (normal) Aspect Ratio (side) Ca (normal) Ca (side) Force (lbs) (normal) Force (lbs) (side) Force (lbs) (angle) AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 189 82 82 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 218 157 157 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 676 292 292 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 55 23 23 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 66 47 47 WIND LOADS WITH ICE: AIR6449 B41 Antennas 35.3 22.7 10.7 5.57 2.62 1.55 3.30 1.20 1.24 35 17 17 AIR 32 B66A B2A Antennas 58.8 15.1 10.9 6.17 4.45 3.89 5.39 1.26 1.33 40 31 31 APXVAALL24_43-U-NA20 Antennas 98.1 26.2 10.7 17.85 7.29 3.74 9.16 1.26 1.47 116 56 56 4415 RRH 17.1 15.4 7.6 1.83 0.90 1.11 2.25 1.20 1.20 11 6 6 4449 B71+B85 RRH 20.1 15.4 11.7 2.15 1.63 1.31 1.72 1.20 1.20 13 10 10 WIND LOADS AT 30 MPH: AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 11 5 5 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 12 9 9 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 38 16 16 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 3 1 1 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 4 3 3 WIND LOADS Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Angle =120 (deg) Ice Thickness =1.10 in.Equivalent Angle =300 (deg) WIND LOADS WITH NO ICE: Appurtenances Height Width Depth Flat Area (normal) Flat Area (side) Aspect Ratio (normal) Aspect Ratio (side) Ca (normal) Ca (side) Force (lbs) (normal) Force (lbs) (side) Force (lbs) (angle) AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 189 82 109 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 218 157 172 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 676 292 388 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 55 23 31 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 66 47 52 WIND LOADS WITH ICE: AIR6449 B41 Antennas 35.3 22.7 10.7 5.57 2.62 1.55 3.30 1.20 1.24 35 17 21 AIR 32 B66A B2A Antennas 58.8 15.1 10.9 6.17 4.45 3.89 5.39 1.26 1.33 40 31 33 APXVAALL24_43-U-NA20 Antennas 98.1 26.2 10.7 17.85 7.29 3.74 9.16 1.26 1.47 116 56 71 4415 RRH 17.1 15.4 7.6 1.83 0.90 1.11 2.25 1.20 1.20 11 6 7 4449 B71+B85 RRH 20.1 15.4 11.7 2.15 1.63 1.31 1.72 1.20 1.20 13 10 11 WIND LOADS AT 30 MPH: AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 11 5 6 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 12 9 10 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 38 16 22 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 3 1 2 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 4 3 3 WIND LOADS Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Angle =150 (deg) Ice Thickness =1.10 in.Equivalent Angle =330 (deg) WIND LOADS WITH NO ICE: Appurtenances Height Width Depth Flat Area (normal) Flat Area (side) Aspect Ratio (normal) Aspect Ratio (side) Ca (normal) Ca (side) Force (lbs) (normal) Force (lbs) (side) Force (lbs) (angle) AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 189 82 162 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 218 157 203 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 676 292 580 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 55 23 47 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 66 47 61 WIND LOADS WITH ICE: AIR6449 B41 Antennas 35.3 22.7 10.7 5.57 2.62 1.55 3.30 1.20 1.24 35 17 30 AIR 32 B66A B2A Antennas 58.8 15.1 10.9 6.17 4.45 3.89 5.39 1.26 1.33 40 31 38 APXVAALL24_43-U-NA20 Antennas 98.1 26.2 10.7 17.85 7.29 3.74 9.16 1.26 1.47 116 56 101 4415 RRH 17.1 15.4 7.6 1.83 0.90 1.11 2.25 1.20 1.20 11 6 10 4449 B71+B85 RRH 20.1 15.4 11.7 2.15 1.63 1.31 1.72 1.20 1.20 13 10 13 WIND LOADS AT 30 MPH: AIR6449 B41 Antennas 33.1 20.5 8.5 4.71 1.95 1.61 3.89 1.20 1.26 11 5 9 AIR 32 B66A B2A Antennas 56.6 12.9 8.7 5.07 3.42 4.39 6.51 1.28 1.38 12 9 11 APXVAALL24_43-U-NA20 Antennas 95.9 24.0 8.5 15.98 5.66 4.00 11.28 1.27 1.54 38 16 32 4415 RRH 14.9 13.2 5.4 1.37 0.56 1.13 2.76 1.20 1.21 3 1 3 4449 B71+B85 RRH 17.9 13.2 9.5 1.64 1.18 1.36 1.88 1.20 1.20 4 3 3 WIND LOADS Date: 3/4/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC Thickness of ice:1.10 in. Density of ice:56 pcf AIR6449 B41 Antennas AIR 32 B66A B2A Antennas Weight of ice based on total radial SF area: Weight of ice based on total radial SF area: Height (in): 33.1 Height (in): 56.6 Width (in): 20.5 Width (in): 12.9 Depth (in): 8.5 Depth (in): 8.7 Total weight of ice on object: 86 lbs Total weight of ice on object: 106 lbs Weight of object: 103.0 lbs Weight of object: 133.0 lbs Combined weight of ice and object: 189 lbs Combined weight of ice and object: 239 lbs APXVAALL24_43-U-NA20 Antennas 4415 RRH Weight of ice based on total radial SF area: Weight of ice based on total radial SF area: Height (in): 95.9 Height (in): 14.9 Width (in): 24.0 Width (in): 13.2 Depth (in): 8.5 Depth (in): 5.4 Total weight of ice on object: 285 lbs Total weight of ice on object: 26 lbs Weight of object: 150.0 lbs Weight of object: 44.0 lbs Combined weight of ice and object: 435 lbs Combined weight of ice and object: 70 lbs 4449 B71+B85 RRH 3" Pipe Weight of ice based on total radial SF area: Per foot weight of ice: Height (in): 17.9 diameter (in): 3.5 Width (in): 13.2 Per foot weight of ice on object: 6 plf Depth (in): 9.5 Total weight of ice on object: 35 lbs Weight of object: 71.0 lbs Combined weight of ice and object: 106 lbs 2" Pipe Per foot weight of ice: diameter (in): 3.5 Per foot weight of ice on object: 6 plf ICE WEIGHT CALCULATIONS Penthouse Mount Calculations (Modified Conditions) Current Date: 3/4/2021 4:49 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Penthouse Mount (Mod).retx Current Date: 3/4/2021 4:49 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Penthouse Mount (Mod).retx Current Date: 3/4/2021 4:49 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Penthouse Mount (Mod).retx Current Date: 3/4/2021 4:49 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Penthouse Mount (Mod).retx Load data ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ GLOSSARY Comb : Indicates if load condition is a load combination Load Conditions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition Description Comb.Category ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- LC1 1.2D+Wo Yes LC2 1.2D+W30 Yes LC3 1.2D+W60 Yes LC4 1.2D+W90 Yes LC5 1.2D+W120 Yes LC6 1.2D+W150 Yes LC7 1.2D-Wo Yes LC8 1.2D-W30 Yes LC9 1.2D-W60 Yes LC10 1.2D-W90 Yes LC11 1.2D-W120 Yes LC12 1.2D-W150 Yes LC13 0.9D+Wo Yes LC14 0.9D+W30 Yes LC15 0.9D+W60 Yes LC16 0.9D+W90 Yes LC17 0.9D+W120 Yes LC18 0.9D+W150 Yes LC19 0.9D-Wo Yes LC20 0.9D-W30 Yes LC21 0.9D-W60 Yes LC22 0.9D-W90 Yes LC23 0.9D-W120 Yes LC24 0.9D-W150 Yes LC25 1.2D+Di+WI0 Yes LC26 1.2D+Di+WI30 Yes LC27 1.2D+Di+WI60 Yes LC28 1.2D+Di+WI90 Yes LC29 1.2D+Di+WI120 Yes LC30 1.2D+Di+WI150 Yes LC31 1.2D+Di-WI0 Yes LC32 1.2D+Di-WI30 Yes LC33 1.2D+Di-WI60 Yes LC34 1.2D+Di-WI90 Yes LC35 1.2D+Di-WI120 Yes LC36 1.2D+Di-WI150 Yes ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Self weight multipliers for load conditions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Page1 Self weight multiplier Condition Description Comb.MultX MultY MultZ ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ LC1 1.2D+Wo Yes 0.00 0.00 0.00 LC2 1.2D+W30 Yes 0.00 0.00 0.00 LC3 1.2D+W60 Yes 0.00 0.00 0.00 LC4 1.2D+W90 Yes 0.00 0.00 0.00 LC5 1.2D+W120 Yes 0.00 0.00 0.00 LC6 1.2D+W150 Yes 0.00 0.00 0.00 LC7 1.2D-Wo Yes 0.00 0.00 0.00 LC8 1.2D-W30 Yes 0.00 0.00 0.00 LC9 1.2D-W60 Yes 0.00 0.00 0.00 LC10 1.2D-W90 Yes 0.00 0.00 0.00 LC11 1.2D-W120 Yes 0.00 0.00 0.00 LC12 1.2D-W150 Yes 0.00 0.00 0.00 LC13 0.9D+Wo Yes 0.00 0.00 0.00 LC14 0.9D+W30 Yes 0.00 0.00 0.00 LC15 0.9D+W60 Yes 0.00 0.00 0.00 LC16 0.9D+W90 Yes 0.00 0.00 0.00 LC17 0.9D+W120 Yes 0.00 0.00 0.00 LC18 0.9D+W150 Yes 0.00 0.00 0.00 LC19 0.9D-Wo Yes 0.00 0.00 0.00 LC20 0.9D-W30 Yes 0.00 0.00 0.00 LC21 0.9D-W60 Yes 0.00 0.00 0.00 LC22 0.9D-W90 Yes 0.00 0.00 0.00 LC23 0.9D-W120 Yes 0.00 0.00 0.00 LC24 0.9D-W150 Yes 0.00 0.00 0.00 LC25 1.2D+Di+WI0 Yes 0.00 0.00 0.00 LC26 1.2D+Di+WI30 Yes 0.00 0.00 0.00 LC27 1.2D+Di+WI60 Yes 0.00 0.00 0.00 LC28 1.2D+Di+WI90 Yes 0.00 0.00 0.00 LC29 1.2D+Di+WI120 Yes 0.00 0.00 0.00 LC30 1.2D+Di+WI150 Yes 0.00 0.00 0.00 LC31 1.2D+Di-WI0 Yes 0.00 0.00 0.00 LC32 1.2D+Di-WI30 Yes 0.00 0.00 0.00 LC33 1.2D+Di-WI60 Yes 0.00 0.00 0.00 LC34 1.2D+Di-WI90 Yes 0.00 0.00 0.00 LC35 1.2D+Di-WI120 Yes 0.00 0.00 0.00 LC36 1.2D+Di-WI150 Yes 0.00 0.00 0.00 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Earthquake (Dynamic analysis only) ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition a/g Ang.Damp. [Deg][%] -------------------------------------------------------------------------------------------------------------------------------------------------------- LC1 0.00 0.00 0.00 LC2 0.00 0.00 0.00 LC3 0.00 0.00 0.00 LC4 0.00 0.00 0.00 LC5 0.00 0.00 0.00 LC6 0.00 0.00 0.00 LC7 0.00 0.00 0.00 LC8 0.00 0.00 0.00 LC9 0.00 0.00 0.00 LC10 0.00 0.00 0.00 LC11 0.00 0.00 0.00 LC12 0.00 0.00 0.00 LC13 0.00 0.00 0.00 LC14 0.00 0.00 0.00 Page2 LC15 0.00 0.00 0.00 LC16 0.00 0.00 0.00 LC17 0.00 0.00 0.00 LC18 0.00 0.00 0.00 LC19 0.00 0.00 0.00 LC20 0.00 0.00 0.00 LC21 0.00 0.00 0.00 LC22 0.00 0.00 0.00 LC23 0.00 0.00 0.00 LC24 0.00 0.00 0.00 LC25 0.00 0.00 0.00 LC26 0.00 0.00 0.00 LC27 0.00 0.00 0.00 LC28 0.00 0.00 0.00 LC29 0.00 0.00 0.00 LC30 0.00 0.00 0.00 LC31 0.00 0.00 0.00 LC32 0.00 0.00 0.00 LC33 0.00 0.00 0.00 LC34 0.00 0.00 0.00 LC35 0.00 0.00 0.00 LC36 0.00 0.00 0.00 -------------------------------------------------------------------------------------------------------------------------------------------------------- Page3 Current Date: 3/4/2021 4:49 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Penthouse Mount (Mod).retx Steel Code Check ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Report: Summary - Group by member Load conditions to be included in design : LC1=1.2D+Wo LC2=1.2D+W30 LC3=1.2D+W60 LC4=1.2D+W90 LC5=1.2D+W120 LC6=1.2D+W150 LC7=1.2D-Wo LC8=1.2D-W30 LC9=1.2D-W60 LC10=1.2D-W90 LC11=1.2D-W120 LC12=1.2D-W150 LC13=0.9D+Wo LC14=0.9D+W30 LC15=0.9D+W60 LC16=0.9D+W90 LC17=0.9D+W120 LC18=0.9D+W150 LC19=0.9D-Wo LC20=0.9D-W30 LC21=0.9D-W60 LC22=0.9D-W90 LC23=0.9D-W120 LC24=0.9D-W150 LC25=1.2D+Di+WI0 LC26=1.2D+Di+WI30 LC27=1.2D+Di+WI60 LC28=1.2D+Di+WI90 LC29=1.2D+Di+WI120 LC30=1.2D+Di+WI150 LC31=1.2D+Di-WI0 LC32=1.2D+Di-WI30 LC33=1.2D+Di-WI60 LC34=1.2D+Di-WI90 LC35=1.2D+Di-WI120 LC36=1.2D+Di-WI150 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Description Section Member Ctrl Eq.Ratio Status Reference ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ PIPE 2x0.154 20 LC1 at 50.00%0.01 OK 21 LC1 at 50.00%0.03 OK 22 LC7 at 100.00%0.12 OK 23 LC7 at 0.00%0.11 OK 24 LC11 at 50.00%0.09 OK 25 LC3 at 50.00%0.08 OK 26 LC1 at 50.00%0.02 OK 27 LC12 at 50.00%0.02 OK ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ PIPE 3x0.216 4 LC10 at 61.61%0.98 OK 3 LC4 at 61.46%0.98 OK 5 LC10 at 68.75%0.68 OK Page1 8 LC7 at 68.75%0.69 OK 16 LC11 at 69.79%0.84 OK 17 LC11 at 70.54%0.84 OK ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Page2 Current Date: 3/4/2021 4:49 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Penthouse Mount (Mod).retx Geometry data ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ GLOSSARY Cb22, Cb33 : Moment gradient coefficients Cm22, Cm33 : Coefficients applied to bending term in interaction formula d0 : Tapered member section depth at J end of member DJX : Rigid end offset distance measured from J node in axis X DJY : Rigid end offset distance measured from J node in axis Y DJZ : Rigid end offset distance measured from J node in axis Z DKX : Rigid end offset distance measured from K node in axis X DKY : Rigid end offset distance measured from K node in axis Y DKZ : Rigid end offset distance measured from K node in axis Z dL : Tapered member section depth at K end of member Ig factor : Inertia reduction factor (Effective Inertia/Gross Inertia) for reinforced concrete members K22 : Effective length factor about axis 2 K33 : Effective length factor about axis 3 L22 : Member length for calculation of axial capacity L33 : Member length for calculation of axial capacity LB pos : Lateral unbraced length of the compression flange in the positive side of local axis 2 LB neg : Lateral unbraced length of the compression flange in the negative side of local axis 2 RX : Rotation about X RY : Rotation about Y RZ : Rotation about Z TO : 1 = Tension only member 0 = Normal member TX : Translation in X TY : Translation in Y TZ : Translation in Z Nodes ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Node X Y Z Rigid Floor [ft][ft][ft] ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 1 1.17 7.50 0.00 0 2 1.17 1.00 0.00 0 3 1.17 7.50 0.50 0 4 1.17 1.00 0.50 0 5 1.17 19.50 0.50 0 6 1.17 0.00 0.50 0 15 5.00 7.50 0.00 0 16 5.00 1.00 0.00 0 17 5.00 7.50 0.50 0 18 5.00 1.00 0.50 0 19 5.00 19.50 0.50 0 20 5.00 0.00 0.50 0 21 15.00 5.83 0.00 0 22 15.00 1.00 0.00 0 23 15.00 5.83 0.50 0 24 15.00 1.00 0.50 0 25 15.00 19.50 0.50 0 26 15.00 0.00 0.50 0 27 10.00 5.83 0.00 0 28 10.00 1.00 0.00 0 29 10.00 5.83 0.50 0 Page1 30 10.00 1.00 0.50 0 31 10.00 19.50 0.50 0 32 10.00 0.00 0.50 0 33 0.00 5.83 -7.00 0 34 0.00 1.00 -7.00 0 35 0.00 5.83 -7.50 0 36 0.00 1.00 -7.50 0 37 0.00 19.50 -7.50 0 38 0.00 0.00 -7.50 0 39 5.00 5.83 -7.00 0 40 5.00 1.00 -7.00 0 41 5.00 5.83 -7.50 0 42 5.00 1.00 -7.50 0 43 5.00 19.50 -7.50 0 44 5.00 0.00 -7.50 0 45 1.17 12.00 0.50 0 46 5.00 17.00 -7.50 0 47 5.00 12.50 0.50 0 48 0.00 17.50 -7.50 0 49 1.17 18.00 0.50 0 50 5.00 18.00 0.50 0 51 0.00 18.00 -7.50 0 52 5.00 18.00 -7.50 0 53 5.00 12.00 -7.50 0 54 0.00 12.50 -7.50 0 55 5.00 17.50 0.50 0 56 1.17 17.00 0.50 0 57 5.00 12.00 0.50 0 58 0.00 12.00 -7.50 0 ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Restraints ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Node TX TY TZ RX RY RZ ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 1 1 1 1 0 1 0 2 1 1 1 0 1 0 15 1 1 1 0 1 0 16 1 1 1 0 1 0 21 1 1 1 0 1 0 22 1 1 1 0 1 0 27 1 1 1 0 1 0 28 1 1 1 0 1 0 33 1 1 1 0 1 0 34 1 1 1 0 1 0 39 1 1 1 0 1 0 40 1 1 1 0 1 0 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Members ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Page2 Member NJ NK Description Section Material d0 dL Ig factor [in][in] ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 4 19 20 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 3 5 6 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 5 31 32 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 8 25 26 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 16 43 44 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 17 37 38 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 20 49 50 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 21 51 52 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 22 48 47 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 23 45 46 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 24 55 53 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 25 56 54 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 26 45 57 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 27 58 53 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Orientation of local axes ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Member Rotation Axes23 NX NY NZ [Deg] ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 4 315.00 0 0.00 0.00 0.00 3 315.00 0 0.00 0.00 0.00 5 315.00 0 0.00 0.00 0.00 8 315.00 0 0.00 0.00 0.00 16 315.00 0 0.00 0.00 0.00 17 315.00 0 0.00 0.00 0.00 ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Hinges ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Node-J Node-K Member M33 M22 V3 V2 M33 M22 V3 V2 TOR AXL Axial rigidity ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 20 1 1 0 0 1 1 0 0 0 0 Full 21 1 1 0 0 1 1 0 0 0 0 Full 22 1 1 0 0 1 1 0 0 0 0 Full 23 1 1 0 0 1 1 0 0 0 0 Full 24 1 1 0 0 1 1 0 0 0 0 Full 25 1 1 0 0 1 1 0 0 0 0 Full 26 1 1 0 0 1 1 0 0 0 0 Full 27 1 1 0 0 1 1 0 0 0 0 Full ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Page3 Current Date: 3/4/2021 4:48 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Penthouse Mount (Mod).retx Current Date: 3/4/2021 4:48 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Penthouse Mount (Mod).retx Analysis result Reactions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Direction of positive forces and moments Forces [Kip] Moments [Kip*ft] Node FX FY FZ MX MY MZ ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Condition LC1=1.2D+Wo 1 -0.01736 1.14198 1.33764 0.00000 -0.02184 0.00000 2 0.02807 -1.48264 -0.32976 0.00000 0.00413 0.00000 15 -0.06905 0.93229 1.20388 0.00000 -0.02282 0.00000 16 0.03326 -1.33478 -0.28916 0.00000 0.01103 0.00000 21 0.00000 1.65672 0.89352 0.00000 0.00000 0.00000 22 0.00000 -1.36011 -0.51632 0.00000 0.00000 0.00000 27 0.00000 1.51630 0.82140 0.00000 0.00000 0.00000 28 0.00000 -1.18369 -0.45130 0.00000 0.00000 0.00000 33 -0.01507 -0.45535 1.34567 0.00000 -0.00391 0.00000 34 0.03986 1.85034 -0.56954 0.00000 -0.01885 0.00000 39 -0.04581 -0.17305 1.24227 0.00000 0.03385 0.00000 40 0.04611 1.71368 -0.50477 0.00000 -0.00685 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 0.00000 2.82168 4.18354 0.00000 -0.02527 0.00000 Condition LC2=1.2D+W30 1 1.04160 0.23857 0.47415 0.00000 0.43105 0.00000 2 -0.45178 -0.24198 -0.04123 0.00000 -0.11132 0.00000 15 1.00614 1.03263 1.05207 0.00000 0.43292 0.00000 16 -0.44877 -1.18631 -0.27422 0.00000 -0.10583 0.00000 21 0.39775 1.17437 0.63197 0.00000 0.14399 0.00000 22 -0.28320 -0.87776 -0.33021 0.00000 -0.08655 0.00000 27 0.45520 1.10518 0.58907 0.00000 0.16584 0.00000 28 -0.31095 -0.77257 -0.29272 0.00000 -0.09355 0.00000 33 0.92002 0.36538 0.63698 0.00000 -0.37596 0.00000 34 -0.51383 0.88765 -0.21941 0.00000 0.12591 0.00000 39 0.90221 -0.42222 1.04107 0.00000 -0.35341 0.00000 40 -0.50962 1.51877 -0.47522 0.00000 0.13294 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 2.20476 2.82168 2.79229 0.00000 0.30604 0.00000 Page1 Condition LC3=1.2D+W60 1 1.24148 -0.10294 0.04340 0.00000 0.51817 0.00000 2 -0.49197 0.34416 0.09279 0.00000 -0.11230 0.00000 15 1.21912 0.89471 0.76291 0.00000 0.52096 0.00000 16 -0.49058 -0.80690 -0.19219 0.00000 -0.10844 0.00000 21 0.69868 0.64876 0.23922 0.00000 0.26174 0.00000 22 -0.38690 -0.35216 -0.16144 0.00000 -0.10574 0.00000 27 0.81277 0.84788 0.34897 0.00000 0.30395 0.00000 28 -0.45714 -0.51527 -0.22735 0.00000 -0.12595 0.00000 33 1.13473 0.65227 0.26742 0.00000 -0.45923 0.00000 34 -0.58683 0.39722 -0.05013 0.00000 0.13960 0.00000 39 1.12892 -0.37242 0.78156 0.00000 -0.44784 0.00000 40 -0.58465 1.18636 -0.37358 0.00000 0.14348 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 3.23763 2.82168 1.53159 0.00000 0.52839 0.00000 Condition LC4=1.2D+W90 1 1.28375 -0.43135 -0.48292 0.00000 0.54135 0.00000 2 -0.51649 1.00513 0.22675 0.00000 -0.11693 0.00000 15 1.28075 0.69302 0.32108 0.00000 0.54481 0.00000 16 -0.51726 -0.25982 -0.08717 0.00000 -0.11562 0.00000 21 0.71338 0.15055 -0.03038 0.00000 0.26697 0.00000 22 -0.39738 0.14606 0.03038 0.00000 -0.10899 0.00000 27 0.92767 0.16889 -0.03412 0.00000 0.34564 0.00000 28 -0.53567 0.16371 0.03412 0.00000 -0.14966 0.00000 33 1.19687 0.95597 -0.24492 0.00000 -0.48126 0.00000 34 -0.62278 -0.21272 0.14613 0.00000 0.15023 0.00000 39 1.20409 -0.22158 0.33784 0.00000 -0.48448 0.00000 40 -0.62290 0.66380 -0.21680 0.00000 0.14956 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 3.39404 2.82168 0.00000 0.00000 0.54163 0.00000 Condition LC5=1.2D+W120 1 1.23211 -0.70873 -0.97620 0.00000 0.52412 0.00000 2 -0.51231 1.61380 0.34730 0.00000 -0.11696 0.00000 15 1.24795 0.46306 -0.14435 0.00000 0.52776 0.00000 16 -0.51504 0.32385 0.02658 0.00000 -0.11826 0.00000 21 0.69879 -0.34814 -0.29997 0.00000 0.26161 0.00000 22 -0.38701 0.64475 0.22219 0.00000 -0.10586 0.00000 27 0.81294 -0.51097 -0.41718 0.00000 0.30372 0.00000 28 -0.45732 0.84358 0.29556 0.00000 -0.12614 0.00000 33 1.17219 1.21202 -0.73816 0.00000 -0.46761 0.00000 34 -0.62194 -0.78909 0.32838 0.00000 0.15353 0.00000 39 1.19164 -0.03546 -0.12723 0.00000 -0.48505 0.00000 40 -0.62437 0.11304 -0.04851 0.00000 0.14841 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 3.23763 2.82168 -1.53159 0.00000 0.49929 0.00000 Condition LC6=1.2D+W150 1 1.02525 -0.87202 -1.29235 0.00000 0.44111 0.00000 2 -0.48466 2.01447 0.43421 0.00000 -0.11857 0.00000 15 1.05589 0.22261 -0.52029 0.00000 0.44532 0.00000 16 -0.48870 0.83514 0.14031 0.00000 -0.12163 0.00000 21 0.39789 -0.87519 -0.69263 0.00000 0.14381 0.00000 22 -0.28334 1.17179 0.39088 0.00000 -0.08671 0.00000 27 0.45535 -0.76898 -0.65723 0.00000 0.16564 0.00000 28 -0.31110 1.10158 0.36088 0.00000 -0.09371 0.00000 33 0.98493 1.32703 -1.03408 0.00000 -0.39011 0.00000 34 -0.57703 -1.15630 0.44630 0.00000 0.15108 0.00000 39 1.01129 0.14783 -0.46493 0.00000 -0.41742 0.00000 Page2 40 -0.58102 -0.32629 0.09664 0.00000 0.14269 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 2.20476 2.82168 -2.79229 0.00000 0.26149 0.00000 Condition LC7=1.2D-Wo 1 0.01311 -0.55123 -1.39392 0.00000 0.01938 0.00000 2 -0.02822 1.98809 0.40286 0.00000 -0.00474 0.00000 15 0.06446 -0.33692 -1.25800 0.00000 0.02138 0.00000 16 -0.03338 1.83683 0.36178 0.00000 -0.01119 0.00000 21 0.00000 -1.35986 -0.95410 0.00000 0.00000 0.00000 22 0.00000 1.65646 0.57690 0.00000 0.00000 0.00000 27 0.00000 -1.18186 -0.88948 0.00000 0.00000 0.00000 28 0.00000 1.51446 0.51938 0.00000 0.00000 0.00000 33 0.02076 1.04170 -1.26490 0.00000 0.00127 0.00000 34 -0.04109 -1.34019 0.46928 0.00000 0.01871 0.00000 39 0.05161 0.75665 -1.15692 0.00000 -0.03601 0.00000 40 -0.04724 -1.20245 0.40357 0.00000 0.00697 0.00000 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------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 0.00000 4.71398 -0.64600 0.00000 0.00419 0.00000 Condition LC32=1.2D+Di-WI30 1 -0.18301 0.56527 -0.12148 0.00000 -0.07633 0.00000 2 0.07975 0.48481 0.06820 0.00000 0.01946 0.00000 15 -0.17638 0.41558 -0.23218 0.00000 -0.07551 0.00000 16 0.07907 0.66655 0.11275 0.00000 0.01885 0.00000 21 -0.07423 0.05708 -0.11335 0.00000 -0.02683 0.00000 22 0.05302 0.32553 0.09214 0.00000 0.01623 0.00000 27 -0.08544 0.07128 -0.13033 0.00000 -0.03108 0.00000 28 0.05857 0.36733 0.10346 0.00000 0.01766 0.00000 33 -0.17163 0.50169 -0.00702 0.00000 0.06982 0.00000 34 0.09398 0.36398 -0.06853 0.00000 -0.02294 0.00000 39 -0.16875 0.65311 -0.08629 0.00000 0.06675 0.00000 40 0.09341 0.24177 -0.01900 0.00000 -0.02384 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM -0.40164 4.71398 -0.40164 0.00000 -0.04777 0.00000 Condition LC33=1.2D+Di-WI60 1 -0.12932 0.55685 -0.10240 0.00000 -0.05410 0.00000 2 0.05524 0.46896 0.06601 0.00000 0.01324 0.00000 15 -0.12476 0.45139 -0.18109 0.00000 -0.05338 0.00000 16 0.05477 0.59832 0.09767 0.00000 0.01288 0.00000 21 -0.05444 0.09368 -0.09361 0.00000 -0.01968 0.00000 22 0.03888 0.28893 0.07806 0.00000 0.01190 0.00000 27 -0.07645 0.08723 -0.12137 0.00000 -0.02781 0.00000 28 0.05240 0.35137 0.09733 0.00000 0.01580 0.00000 33 -0.12167 0.50868 0.01842 0.00000 0.04949 0.00000 34 0.06563 0.38992 -0.07523 0.00000 -0.01588 0.00000 39 -0.11968 0.61569 -0.03789 0.00000 0.04746 0.00000 40 0.06523 0.30294 -0.04005 0.00000 -0.01647 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM -0.29416 4.71398 -0.29416 0.00000 -0.03655 0.00000 Condition LC34=1.2D+Di-WI90 1 -0.14498 0.61934 -0.00235 0.00000 -0.06179 0.00000 2 0.06209 0.34495 0.04121 0.00000 0.01445 0.00000 15 -0.14383 0.48736 -0.09878 0.00000 -0.06112 0.00000 16 0.06197 0.49806 0.07903 0.00000 0.01455 0.00000 21 -0.06299 0.19432 -0.03933 0.00000 -0.02277 0.00000 22 0.04499 0.18829 0.03933 0.00000 0.01377 0.00000 27 -0.10175 0.22283 -0.04515 0.00000 -0.03702 0.00000 28 0.06975 0.21577 0.04515 0.00000 0.02102 0.00000 33 -0.13601 0.45039 0.11542 0.00000 0.05466 0.00000 34 0.07440 0.50453 -0.11189 0.00000 -0.01847 0.00000 39 -0.13607 0.58934 0.04573 0.00000 0.05520 0.00000 Page10 40 0.07442 0.39878 -0.06838 0.00000 -0.01822 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM -0.33800 4.71398 0.00000 0.00000 -0.04574 0.00000 Condition LC35=1.2D+Di-WI120 1 -0.13237 0.66626 0.08815 0.00000 -0.05739 0.00000 2 0.05945 0.23715 0.02048 0.00000 0.01390 0.00000 15 -0.13491 0.53174 -0.00889 0.00000 -0.05681 0.00000 16 0.05969 0.38696 0.05775 0.00000 0.01449 0.00000 21 -0.05443 0.29493 0.01495 0.00000 -0.01968 0.00000 22 0.03888 0.08767 0.00061 0.00000 0.01190 0.00000 27 -0.07644 0.35840 0.03106 0.00000 -0.02782 0.00000 28 0.05240 0.08021 -0.00702 0.00000 0.01579 0.00000 33 -0.12338 0.40621 0.20614 0.00000 0.04883 0.00000 34 0.07102 0.60913 -0.14435 0.00000 -0.01845 0.00000 39 -0.12552 0.55187 0.13556 0.00000 0.05194 0.00000 40 0.07146 0.50345 -0.10029 0.00000 -0.01739 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM -0.29416 4.71398 0.29416 0.00000 -0.04069 0.00000 Condition LC36=1.2D+Di-WI150 1 -0.18761 0.72300 0.14736 0.00000 -0.08112 0.00000 2 0.08574 0.15366 0.00125 0.00000 0.02038 0.00000 15 -0.19104 0.53236 0.01081 0.00000 -0.08049 0.00000 16 0.08606 0.36403 0.05368 0.00000 0.02111 0.00000 21 -0.07423 0.33152 0.03468 0.00000 -0.02684 0.00000 22 0.05301 0.05109 -0.01347 0.00000 0.01623 0.00000 27 -0.08543 0.37434 0.04003 0.00000 -0.03109 0.00000 28 0.05856 0.06426 -0.01316 0.00000 0.01765 0.00000 33 -0.17373 0.35443 0.25737 0.00000 0.06874 0.00000 34 0.10153 0.67669 -0.16852 0.00000 -0.02657 0.00000 39 -0.17665 0.56043 0.15810 0.00000 0.07296 0.00000 40 0.10215 0.52816 -0.10649 0.00000 -0.02515 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM -0.40164 4.71398 0.40164 0.00000 -0.05419 0.00000 Envelope for nodal reactions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Note.-lc is the controlling load condition Direction of positive forces and moments Page11 Envelope of nodal reactions for : LC1=1.2D+Wo LC2=1.2D+W30 LC3=1.2D+W60 LC4=1.2D+W90 LC5=1.2D+W120 LC6=1.2D+W150 LC7=1.2D-Wo LC8=1.2D-W30 LC9=1.2D-W60 LC10=1.2D-W90 LC11=1.2D-W120 LC12=1.2D-W150 LC13=0.9D+Wo LC14=0.9D+W30 LC15=0.9D+W60 LC16=0.9D+W90 LC17=0.9D+W120 LC18=0.9D+W150 LC19=0.9D-Wo LC20=0.9D-W30 LC21=0.9D-W60 LC22=0.9D-W90 LC23=0.9D-W120 LC24=0.9D-W150 LC25=1.2D+Di+WI0 LC26=1.2D+Di+WI30 LC27=1.2D+Di+WI60 LC28=1.2D+Di+WI90 LC29=1.2D+Di+WI120 LC30=1.2D+Di+WI150 LC31=1.2D+Di-WI0 LC32=1.2D+Di-WI30 LC33=1.2D+Di-WI60 LC34=1.2D+Di-WI90 LC35=1.2D+Di-WI120 LC36=1.2D+Di-WI150 Forces Moments Node Fx lc Fy lc Fz lc Mx lc My lc Mz lc [Kip][Kip][Kip][Kip*ft][Kip*ft][Kip*ft] -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 1 Max 1.284 LC4 1.451 LC12 1.345 LC13 0.00000 LC1 0.54135 LC4 0.00000 LC1 Min -1.289 LC10 -0.943 LC18 -1.394 LC7 0.00000 LC1 -0.54458 LC10 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 2 Max 0.518 LC10 2.014 LC6 0.434 LC6 0.00000 LC1 0.11676 LC10 0.00000 LC1 Min -0.516 LC4 -1.550 LC24 -0.366 LC24 0.00000 LC1 -0.11857 LC6 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 15 Max 1.281 LC4 1.033 LC2 1.212 LC13 0.00000 LC1 0.54481 LC4 0.00000 LC1 Min -1.267 LC10 -0.524 LC20 -1.258 LC7 0.00000 LC1 -0.53850 LC10 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 16 Max 0.514 LC10 1.837 LC7 0.362 LC7 0.00000 LC1 0.11968 LC12 0.00000 LC1 Min -0.517 LC4 -1.396 LC13 -0.298 LC13 0.00000 LC1 -0.12163 LC6 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 21 Max 0.713 LC4 1.657 LC1 0.898 LC13 0.00000 LC1 0.26697 LC4 0.00000 LC1 Min -0.713 LC10 -1.390 LC19 -0.954 LC7 0.00000 LC1 -0.26697 LC10 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 22 Max 0.397 LC10 1.656 LC7 0.577 LC7 0.00000 LC1 0.10899 LC10 0.00000 LC1 Min -0.397 LC4 -1.389 LC13 -0.521 LC13 0.00000 LC1 -0.10899 LC4 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 27 Max 0.928 LC4 1.516 LC1 0.827 LC13 0.00000 LC1 0.34564 LC4 0.00000 LC1 Min -0.928 LC10 -1.217 LC19 -0.889 LC7 0.00000 LC1 -0.34564 LC10 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 28 Max 0.536 LC10 1.514 LC7 0.519 LC7 0.00000 LC1 0.14966 LC10 0.00000 LC1 Page12 Min -0.536 LC4 -1.218 LC13 -0.457 LC13 0.00000 LC1 -0.14966 LC4 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 33 Max 1.197 LC4 1.327 LC6 1.346 LC1 0.00000 LC1 0.48462 LC10 0.00000 LC1 Min -1.206 LC10 -0.795 LC24 -1.276 LC19 0.00000 LC1 -0.48126 LC4 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 34 Max 0.623 LC10 1.850 LC1 0.481 LC19 0.00000 LC1 0.15353 LC5 0.00000 LC1 Min -0.623 LC4 -1.402 LC19 -0.570 LC1 0.00000 LC1 -0.15288 LC11 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 39 Max 1.204 LC4 1.024 LC8 1.242 LC1 0.00000 LC1 0.48412 LC10 0.00000 LC1 Min -1.202 LC10 -0.494 LC14 -1.168 LC19 0.00000 LC1 -0.48505 LC5 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 40 Max 0.624 LC10 1.714 LC1 0.416 LC19 0.00000 LC1 0.14956 LC4 0.00000 LC1 Min -0.624 LC5 -1.265 LC19 -0.505 LC1 0.00000 LC1 -0.14993 LC10 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Page13 Date: 3/5/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC CHECK EPOXY ANCHOR CONNECTION CAPACITY → EXISTING ANCHORS AT MODIFIED PENTHOUSE MOUNT Reference:Hilti North American Product Technical Guide, 19th Edition Epoxy Type =HIT-HY20 (Assumed) Anchor Diameter =3/4 in.(HAS-E Threaded Rod) Embedment Depth = 8 in.(Assumed) Allowable Loads (lbs) Tensile Load 1400 Shear Load 1800 TENSILE FORCES Reaction F =1222 lbs.(See Bentley Output) SHEAR FORCES Reactions in X direction:1065 lbs.(See Bentley Output) Reactions in Y direction:1451 lbs.(See Bentley Output) Resultant:1800 lbs. No. of Supports =1 No. of Anchors / Support =2 Tension Design Load / Anchor = ft=611.00 lbs.<1400 lbs.Therefore, OK ! Shear Design Load / Anchor= fv=899.95 lbs.<1800 lbs.Therefore, OK ! CHECK COMBINED TENSION AND SHEAR ft / FT +fv / FV ≤1.0 0.436 + 0.500 =0.936 <1.0 Therefore, OK ! 1 1 1800 Spacing Reduct. Factor Edge Reduct. Factor Reduced Loads (lbs) 1 1 1400 Date: 3/5/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC CHECK CONNECTION CAPACITY (Worst Case) - ANCHORS AT MODIFIED PENTHOUSE MOUNT Reference:AISC Steel Construction Manual 14th Edition (ASD) Bolt Type =A36 1/2"Threaded Rod Allowable Tensile Load = FTall =4271 lbs. Allowable Shear Load = FVall=2562 lbs. TENSILE FORCES Reaction F =1346 lbs.(See Bentley Output) SHEAR FORCES Reactions in X direction:1206 lbs.(See Bentley Output) Reactions in Y direction:1327 lbs.(See Bentley Output) Resultant:1793 lbs. No. of Supports =1 No. of Bolts / Support =2 Tension Design Load /Bolts = ft=673.00 lbs.<4271 lbs.Therefore, OK ! Shear Design Load / Bolts= fv=896.57 lbs.<2562 lbs.Therefore, OK ! CHECK COMBINED TENSION AND SHEAR ft / FT +fv / FV ≤1.0 0.158 + 0.350 =0.507 <1.0 Therefore, OK ! Date: 3/5/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC CHECK EPOXY ANCHOR CONNECTION CAPACITY → PROPOSED ANCHORS AT MODIFIED PENTHOUSE MOUNT Reference:Hilti North American Product Technical Guide, 19th Edition Epoxy Type =HIT-HY 270 Anchor Diameter =3/4 in. (HAS Threaded Rod) Embedment Depth = 8 in. Allowable Loads (lbs) Tensile Load 1575 Shear Load 1985 TENSILE FORCES Reaction F =1394 lbs. (See Bentley Output) SHEAR FORCES Reactions in X direction:1289 lbs. (See Bentley Output) Reactions in Y direction:1451 lbs. (See Bentley Output) Resultant:1941 lbs. No. of Supports =1 No. of Anchors / Support =2 Tension Design Load / Anchor = ft=697.00 lbs.<1575 lbs.Therefore, OK ! Shear Design Load / Anchor= fv=970.43 lbs.<1985 lbs.Therefore, OK ! CHECK COMBINED TENSION AND SHEAR ft / FT +fv / FV ≤1.0 0.443 + 0.489 =0.931 <1.0 Therefore, OK ! 1 1 1 1985 Spacing Reduct. Factor Edge Reduct. Factor Conc. Thickness Reduct. Factor Reduced Loads (lbs) 1 1 1 1575 Chimney Mount Calculations (Modified Conditions) Current Date: 3/9/2021 5:04 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Chimney Mount (Mod).retx Current Date: 3/9/2021 5:04 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Chimney Mount (Mod).retx Current Date: 3/9/2021 5:04 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Chimney Mount (Mod).retx Current Date: 3/9/2021 5:04 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Chimney Mount (Mod).retx Load data ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ GLOSSARY Comb : Indicates if load condition is a load combination Load Conditions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition Description Comb.Category ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- D Dead Load No DL Wo Wind Load (NO ICE)No WIND W30 WL 30deg No WIND W60 WL 60deg No WIND W90 WL 90deg No WIND W120 WL 120deg No WIND W150 WL 150deg No WIND Di Ice Load No LL WI0 WL ICE 0deg No WIND WI30 WL ICE 30deg No WIND WI60 WL ICE 60deg No WIND WI90 WL ICE 90deg No WIND WI120 WL ICE 120deg No WIND WI150 WL ICE 150deg No WIND ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Distributed force on members ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition Member Dir1 Val1 Val2 Dist1 %Dist2 % [Kip/ft][Kip/ft][ft][ft] ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Wo 1 z -0.012 -0.012 20.00 Yes 100.00 Yes 20 z -0.012 -0.012 35.00 Yes 100.00 Yes 22 z -0.008 -0.008 0.00 No 100.00 Yes 23 z -0.008 -0.008 0.00 No 100.00 Yes 32 z -0.008 -0.008 0.00 No 100.00 Yes 33 z -0.008 -0.008 0.00 No 100.00 Yes W30 1 z -0.012 -0.012 20.00 Yes 100.00 Yes 20 z -0.012 -0.012 35.00 Yes 100.00 Yes 22 z -0.008 -0.008 0.00 No 100.00 Yes 23 z -0.008 -0.008 0.00 No 100.00 Yes 32 z -0.008 -0.008 0.00 No 100.00 Yes 33 z -0.008 -0.008 0.00 No 100.00 Yes W60 1 x -0.012 -0.012 20.00 Yes 100.00 Yes 19 x -0.012 -0.012 35.00 Yes 68.00 Yes Page1 20 x -0.012 -0.012 35.00 Yes 68.00 Yes 21 x -0.008 -0.008 0.00 No 100.00 Yes 22 x -0.008 -0.008 0.00 No 100.00 Yes 23 x -0.008 -0.008 0.00 No 100.00 Yes 31 x -0.008 -0.008 0.00 No 100.00 Yes 32 x -0.008 -0.008 0.00 No 100.00 Yes 33 x -0.008 -0.008 0.00 No 100.00 Yes W90 1 x -0.012 -0.012 20.00 Yes 100.00 Yes 19 x -0.012 -0.012 35.00 Yes 68.00 Yes 20 x -0.012 -0.012 35.00 Yes 68.00 Yes 21 x -0.008 -0.008 0.00 No 100.00 Yes 22 x -0.008 -0.008 0.00 No 100.00 Yes 23 x -0.008 -0.008 0.00 No 100.00 Yes 31 x -0.008 -0.008 0.00 No 100.00 Yes 32 x -0.008 -0.008 0.00 No 100.00 Yes 33 x -0.008 -0.008 0.00 No 100.00 Yes W120 1 x -0.012 -0.012 20.00 Yes 100.00 Yes 19 x -0.012 -0.012 35.00 Yes 68.00 Yes 20 x -0.012 -0.012 35.00 Yes 68.00 Yes 21 x -0.008 -0.008 0.00 No 100.00 Yes 22 x -0.008 -0.008 0.00 No 100.00 Yes 31 x -0.008 -0.008 0.00 No 100.00 Yes 32 x -0.008 -0.008 0.00 No 100.00 Yes W150 1 z 0.012 0.012 20.00 Yes 100.00 Yes 19 z 0.012 0.012 35.00 Yes 100.00 Yes 22 z 0.008 0.008 0.00 No 100.00 Yes 23 z 0.008 0.008 0.00 No 100.00 Yes 32 z 0.008 0.008 0.00 No 100.00 Yes 33 z 0.008 0.008 0.00 No 100.00 Yes Di 1 y -0.006 -0.006 0.00 No 100.00 Yes 19 y -0.006 -0.006 0.00 No 100.00 Yes 20 y -0.006 -0.006 0.00 No 100.00 Yes 21 y -0.006 -0.006 0.00 No 100.00 Yes 22 y -0.006 -0.006 0.00 No 100.00 Yes 23 y -0.006 -0.006 0.00 No 100.00 Yes 31 y -0.006 -0.006 0.00 No 100.00 Yes 32 y -0.006 -0.006 0.00 No 100.00 Yes 33 y -0.006 -0.006 0.00 No 100.00 Yes ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Concentrated forces on members ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition Member Dir1 Value1 Dist1 % [Kip][ft] -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- D 1 y -0.052 1.00 No y -0.052 3.00 No 19 y -0.067 1.75 No y -0.067 5.25 No 20 y -0.067 1.75 No y -0.067 5.25 No Wo 1 z -0.095 1.00 No Page2 z -0.095 3.00 No 19 z -0.109 1.75 No z -0.109 5.25 No 20 z -0.109 1.75 No z -0.109 5.25 No W30 1 3 -0.081 1.00 No 3 -0.081 3.00 No 19 3 -0.102 1.75 No 3 -0.102 5.25 No 20 3 -0.102 1.75 No 3 -0.102 5.25 No W60 1 3 -0.055 1.00 No 3 -0.055 3.00 No 19 3 -0.086 1.75 No 3 -0.086 5.25 No 20 3 -0.086 1.75 No 3 -0.086 5.25 No W90 1 x -0.041 1.00 No x -0.041 3.00 No 19 x -0.079 1.75 No x -0.079 5.25 No 20 x -0.079 1.75 No x -0.079 5.25 No W120 1 2 -0.055 1.00 No 2 -0.055 3.00 No 19 2 -0.086 1.75 No 2 -0.086 5.25 No 20 2 -0.086 1.75 No 2 -0.086 5.25 No W150 1 2 -0.081 1.00 No 2 -0.081 3.00 No 19 2 -0.102 1.75 No 2 -0.102 5.25 No 20 2 -0.102 1.75 No 2 -0.102 5.25 No Di 1 y -0.043 1.00 No y -0.043 3.00 No 19 y -0.053 1.75 No y -0.053 5.25 No 20 y -0.053 1.75 No y -0.053 5.25 No WI0 1 z -0.018 1.00 No z -0.018 3.00 No 19 z -0.021 1.75 No z -0.021 5.25 No 20 z -0.021 1.75 No z -0.021 5.25 No WI30 1 3 -0.015 1.00 No 3 -0.015 3.00 No 19 3 -0.019 1.75 No 3 -0.019 5.25 No 20 3 -0.019 1.75 No 3 -0.019 5.25 No WI60 1 3 -0.011 1.00 No 3 -0.011 3.00 No 19 3 -0.017 1.75 No 3 -0.017 5.25 No 20 3 -0.017 1.75 No 3 -0.017 5.25 No WI90 1 x -0.009 1.00 No Page3 x -0.009 3.00 No 19 x -0.016 1.75 No x -0.016 5.25 No 20 x -0.016 1.75 No x -0.016 5.25 No WI120 1 2 -0.011 1.00 No 2 -0.011 3.00 No 19 2 -0.017 1.75 No 2 -0.017 5.25 No 20 2 -0.017 1.75 No 2 -0.017 5.25 No WI150 1 2 -0.015 1.00 No 2 -0.015 3.00 No 19 2 -0.019 1.75 No 2 -0.019 5.25 No 20 2 -0.019 1.75 No 2 -0.019 5.25 No -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Self weight multipliers for load conditions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Self weight multiplier Condition Description Comb.MultX MultY MultZ ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ D Dead Load No 0.00 -1.00 0.00 Wo Wind Load (NO ICE)No 0.00 0.00 0.00 W30 WL 30deg No 0.00 0.00 0.00 W60 WL 60deg No 0.00 0.00 0.00 W90 WL 90deg No 0.00 0.00 0.00 W120 WL 120deg No 0.00 0.00 0.00 W150 WL 150deg No 0.00 0.00 0.00 Di Ice Load No 0.00 0.00 0.00 WI0 WL ICE 0deg No 0.00 0.00 0.00 WI30 WL ICE 30deg No 0.00 0.00 0.00 WI60 WL ICE 60deg No 0.00 0.00 0.00 WI90 WL ICE 90deg No 0.00 0.00 0.00 WI120 WL ICE 120deg No 0.00 0.00 0.00 WI150 WL ICE 150deg No 0.00 0.00 0.00 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Earthquake (Dynamic analysis only) ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Condition a/g Ang.Damp. [Deg][%] -------------------------------------------------------------------------------------------------------------------------------------------------------- D 0.00 0.00 0.00 Wo 0.00 0.00 0.00 W30 0.00 0.00 0.00 W60 0.00 0.00 0.00 W90 0.00 0.00 0.00 W120 0.00 0.00 0.00 W150 0.00 0.00 0.00 Di 0.00 0.00 0.00 WI0 0.00 0.00 0.00 WI30 0.00 0.00 0.00 Page4 WI60 0.00 0.00 0.00 WI90 0.00 0.00 0.00 WI120 0.00 0.00 0.00 WI150 0.00 0.00 0.00 -------------------------------------------------------------------------------------------------------------------------------------------------------- Page5 Current Date: 3/9/2021 5:04 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Chimney Mount (Mod).retx Steel Code Check ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Report: Summary - Group by member Load conditions to be included in design : LC1=1.2D+Wo LC2=1.2D+W30 LC3=1.2D+W60 LC4=1.2D+W90 LC5=1.2D+W120 LC6=1.2D+W150 LC7=1.2D-Wo LC8=1.2D-W30 LC9=1.2D-W60 LC10=1.2D-W90 LC11=1.2D-W120 LC12=1.2D-W150 LC13=0.9D+Wo LC14=0.9D+W30 LC15=0.9D+W60 LC16=0.9D+W90 LC17=0.9D+W120 LC18=0.9D+W150 LC19=0.9D-Wo LC20=0.9D-W30 LC21=0.9D-W60 LC22=0.9D-W90 LC23=0.9D-W120 LC24=0.9D-W150 LC25=1.2D+Di+WI0 LC26=1.2D+Di+WI30 LC27=1.2D+Di+WI60 LC28=1.2D+Di+WI90 LC29=1.2D+Di+WI120 LC30=1.2D+Di+WI150 LC31=1.2D+Di-WI0 LC32=1.2D+Di-WI30 LC33=1.2D+Di-WI60 LC34=1.2D+Di-WI90 LC35=1.2D+Di-WI120 LC36=1.2D+Di-WI150 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Description Section Member Ctrl Eq.Ratio Status Reference ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ PIPE 2x0.154 21 LC7 at 0.00%0.49 OK 22 LC2 at 0.00%0.23 OK 23 LC4 at 100.00%0.35 OK 31 LC7 at 0.00%0.58 OK 32 LC8 at 100.00%0.28 OK 33 LC4 at 100.00%0.43 OK ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ PIPE 3x0.216 1 LC7 at 69.79%0.32 OK 19 LC1 at 69.79%0.35 OK 20 LC7 at 69.79%0.34 OK ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ WT 6X11 2 LC12 at 75.00%0.08 OK Page1 3 LC9 at 75.00%0.04 OK 6 LC1 at 21.88%0.06 OK 7 LC1 at 21.88%0.07 OK 8 LC1 at 77.08%0.05 OK 9 LC1 at 77.08%0.06 OK 10 LC12 at 0.00%0.02 OK 11 LC9 at 0.00%0.01 OK 24 LC8 at 75.00%0.04 OK 26 LC1 at 21.88%0.08 OK 27 LC1 at 77.08%0.07 OK 28 LC8 at 22.92%0.03 OK ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Page2 Current Date: 3/9/2021 5:05 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Chimney Mount (Mod).retx Geometry data ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ GLOSSARY Cb22, Cb33 : Moment gradient coefficients Cm22, Cm33 : Coefficients applied to bending term in interaction formula d0 : Tapered member section depth at J end of member DJX : Rigid end offset distance measured from J node in axis X DJY : Rigid end offset distance measured from J node in axis Y DJZ : Rigid end offset distance measured from J node in axis Z DKX : Rigid end offset distance measured from K node in axis X DKY : Rigid end offset distance measured from K node in axis Y DKZ : Rigid end offset distance measured from K node in axis Z dL : Tapered member section depth at K end of member Ig factor : Inertia reduction factor (Effective Inertia/Gross Inertia) for reinforced concrete members K22 : Effective length factor about axis 2 K33 : Effective length factor about axis 3 L22 : Member length for calculation of axial capacity L33 : Member length for calculation of axial capacity LB pos : Lateral unbraced length of the compression flange in the positive side of local axis 2 LB neg : Lateral unbraced length of the compression flange in the negative side of local axis 2 RX : Rotation about X RY : Rotation about Y RZ : Rotation about Z TO : 1 = Tension only member 0 = Normal member TX : Translation in X TY : Translation in Y TZ : Translation in Z Nodes ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Node X Y Z Rigid Floor [ft][ft][ft] ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 1 3.00 0.00 0.50 0 2 3.00 19.50 0.50 0 3 3.00 1.00 0.00 0 4 3.00 5.83 0.00 0 5 0.00 1.00 0.00 0 6 0.00 5.83 0.00 0 7 3.33 1.00 0.00 0 8 3.33 5.83 0.00 0 9 3.00 5.83 0.50 0 10 3.00 1.00 0.50 0 12 2.50 5.83 0.00 0 13 0.75 5.83 0.00 0 14 2.50 1.00 0.00 0 15 0.75 1.00 0.00 0 16 0.00 5.83 -3.33 0 17 0.00 1.00 -3.33 0 18 3.33 5.83 -3.33 0 19 3.33 1.00 -3.33 0 22 0.00 5.83 -0.75 0 23 0.00 1.00 -0.75 0 24 0.00 5.83 -2.58 0 Page1 25 0.00 1.00 -2.58 0 28 0.75 5.83 -3.33 0 29 0.75 1.00 -3.33 0 30 2.58 5.83 -3.33 0 31 2.58 1.00 -3.33 0 40 -0.50 5.83 -0.50 0 41 -0.50 1.00 -0.50 0 44 -0.40 5.83 -3.70 0 45 -0.40 1.00 -3.70 0 47 -0.50 19.50 -0.50 0 48 -0.40 19.50 -3.70 0 50 -0.50 0.00 -0.50 0 51 -0.40 0.00 -3.70 0 52 3.00 18.00 0.50 0 53 -0.50 18.00 -0.50 0 54 -0.40 18.00 -3.70 0 59 0.00 1.00 -0.50 0 60 0.00 5.83 -0.50 0 61 3.00 3.33 0.00 0 62 0.00 3.33 0.00 0 63 3.33 3.33 0.00 0 64 3.00 3.33 0.50 0 65 2.50 3.33 0.00 0 66 0.75 3.33 0.00 0 67 0.00 3.33 -3.33 0 68 3.33 3.33 -3.33 0 69 0.00 3.33 -0.75 0 70 0.00 3.33 -2.58 0 71 0.75 3.33 -3.33 0 72 2.58 3.33 -3.33 0 73 -0.50 3.33 -0.50 0 74 -0.40 3.33 -3.70 0 75 0.00 3.33 -0.50 0 76 3.00 10.00 0.50 0 77 -0.50 10.00 -0.50 0 78 -0.40 10.00 -3.70 0 79 3.33 3.33 -2.58 0 80 3.33 3.33 -0.75 0 ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Restraints ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Node TX TY TZ RX RY RZ ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 12 1 1 1 0 0 0 13 1 1 1 0 0 0 14 1 1 1 0 0 0 15 1 1 1 0 0 0 22 1 1 1 0 0 0 23 1 1 1 0 0 0 24 1 1 1 0 0 0 25 1 1 1 0 0 0 28 1 1 1 0 0 0 29 1 1 1 0 0 0 30 1 1 1 0 0 0 31 1 1 1 0 0 0 65 1 1 1 0 0 0 Page2 66 1 1 1 0 0 0 69 1 1 1 0 0 0 70 1 1 1 0 0 0 71 1 1 1 0 0 0 72 1 1 1 0 0 0 79 1 1 1 0 0 0 80 1 1 1 0 0 0 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Members ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Member NJ NK Description Section Material d0 dL Ig factor [in][in] ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ 1 2 1 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 2 6 8 WT 6X11 A36 0.00 0.00 0.00 3 5 7 WT 6X11 A36 0.00 0.00 0.00 6 16 6 WT 6X11 A36 0.00 0.00 0.00 7 17 5 WT 6X11 A36 0.00 0.00 0.00 8 18 16 WT 6X11 A36 0.00 0.00 0.00 9 19 17 WT 6X11 A36 0.00 0.00 0.00 10 8 18 WT 6X11 A36 0.00 0.00 0.00 11 7 19 WT 6X11 A36 0.00 0.00 0.00 19 48 51 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 20 47 50 PIPE 3x0.216 A53 GrB 0.00 0.00 0.00 21 53 54 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 22 54 52 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 23 52 53 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 24 62 63 WT 6X11 A36 0.00 0.00 0.00 26 67 62 WT 6X11 A36 0.00 0.00 0.00 27 68 67 WT 6X11 A36 0.00 0.00 0.00 28 63 68 WT 6X11 A36 0.00 0.00 0.00 31 77 78 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 32 78 76 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 33 76 77 PIPE 2x0.154 A53 GrB 0.00 0.00 0.00 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Orientation of local axes ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Member Rotation Axes23 NX NY NZ [Deg] ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 1 315.00 0 0.00 0.00 0.00 2 270.00 0 0.00 0.00 0.00 3 270.00 0 0.00 0.00 0.00 6 270.00 0 0.00 0.00 0.00 7 270.00 0 0.00 0.00 0.00 8 270.00 0 0.00 0.00 0.00 9 270.00 0 0.00 0.00 0.00 10 270.00 0 0.00 0.00 0.00 11 270.00 0 0.00 0.00 0.00 19 315.00 0 0.00 0.00 0.00 20 315.00 0 0.00 0.00 0.00 24 270.00 0 0.00 0.00 0.00 26 270.00 0 0.00 0.00 0.00 27 270.00 0 0.00 0.00 0.00 Page3 28 270.00 0 0.00 0.00 0.00 ---------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Page4 Current Date: 3/9/2021 5:07 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Chimney Mount (Mod).retx Current Date: 3/9/2021 5:07 PM Units system: English File name: Z:\Shared\Work2.0\STRUCTURAL DEPARTMENT\ANALYSIS SOFTWARE\RAM Elements\RAM Projects\T-MOBILE\MA\4BSS362A\SA\4BSS362A - Chimney Mount (Mod).retx Analysis result Reactions ____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Direction of positive forces and moments Forces [Kip] Moments [Kip*ft] Node FX FY FZ MX MY MZ ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ Condition LC1=1.2D+Wo 24 0.13211 0.40256 0.98554 0.00000 0.00000 0.00000 28 -0.06566 0.44256 -0.13263 0.00000 0.00000 0.00000 30 0.05653 -0.08042 0.31208 0.00000 0.00000 0.00000 22 -0.36633 -0.31022 0.85492 0.00000 0.00000 0.00000 13 0.17616 -0.23746 -0.16488 0.00000 0.00000 0.00000 12 -0.14640 0.65182 0.68204 0.00000 0.00000 0.00000 80 0.03021 -0.12714 -0.35612 0.00000 0.00000 0.00000 79 -0.00167 0.18403 -0.00480 0.00000 0.00000 0.00000 71 0.14060 0.59973 0.03932 0.00000 0.00000 0.00000 72 0.00051 -0.29298 0.01463 0.00000 0.00000 0.00000 70 -0.08625 0.71789 -0.58373 0.00000 0.00000 0.00000 66 -0.11470 0.13376 0.03202 0.00000 0.00000 0.00000 69 0.20553 -0.72585 -0.50918 0.00000 0.00000 0.00000 65 0.08546 -0.19826 -0.23136 0.00000 0.00000 0.00000 31 0.00664 -0.09755 0.03974 0.00000 0.00000 0.00000 29 -0.09451 0.43815 -0.02067 0.00000 0.00000 0.00000 25 -0.01845 0.59860 -0.03027 0.00000 0.00000 0.00000 23 0.03905 -0.55132 0.09098 0.00000 0.00000 0.00000 15 0.04201 0.07547 -0.01502 0.00000 0.00000 0.00000 14 -0.02084 -0.02089 0.07309 0.00000 0.00000 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 0.00000 1.60248 1.07570 0.00000 0.00000 0.00000 Condition LC2=1.2D+W30 24 0.04520 0.28972 0.59220 0.00000 0.00000 0.00000 28 0.37945 0.19906 -0.00049 0.00000 0.00000 0.00000 30 0.02760 -0.02449 0.17519 0.00000 0.00000 0.00000 22 0.11071 -0.16768 0.52895 0.00000 0.00000 0.00000 13 0.25255 -0.03815 -0.08402 0.00000 0.00000 0.00000 12 0.31989 0.21063 0.60444 0.00000 0.00000 0.00000 80 0.02006 -0.15106 -0.14902 0.00000 0.00000 0.00000 79 0.00396 0.18370 -0.00306 0.00000 0.00000 0.00000 71 -0.22945 0.51071 -0.02417 0.00000 0.00000 0.00000 72 -0.00133 -0.24506 0.00928 0.00000 0.00000 0.00000 70 -0.03671 0.48910 -0.33435 0.00000 0.00000 0.00000 66 -0.15905 0.24984 0.00779 0.00000 0.00000 0.00000 69 -0.06727 -0.02700 -0.28943 0.00000 0.00000 0.00000 Page1 65 -0.23002 -0.41390 -0.23240 0.00000 0.00000 0.00000 31 0.00140 -0.05769 0.00820 0.00000 0.00000 0.00000 29 -0.03085 0.33552 -0.00213 0.00000 0.00000 0.00000 25 -0.01172 0.41418 -0.02969 0.00000 0.00000 0.00000 23 -0.01974 -0.07709 0.06871 0.00000 0.00000 0.00000 15 0.01093 0.18651 -0.00278 0.00000 0.00000 0.00000 14 0.01743 -0.26438 0.00952 0.00000 0.00000 0.00000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------ SUM 0.40305 1.60248 0.85275 0.00000 0.00000 0.00000 Condition LC3=1.2D+W60 24 -0.01382 0.21959 0.21934 0.00000 0.00000 0.00000 28 0.58362 0.05904 0.09717 0.00000 0.00000 0.00000 30 -0.00972 0.00939 -0.01951 0.00000 0.00000 0.00000 22 0.43444 -0.12127 0.17488 0.00000 0.00000 0.00000 13 0.27049 0.07960 0.01898 0.00000 0.00000 0.00000 12 0.64302 -0.04444 0.33836 0.00000 0.00000 0.00000 80 0.00609 -0.09599 0.00350 0.00000 0.00000 0.00000 79 0.00634 0.13886 -0.00137 0.00000 0.00000 0.00000 71 -0.38273 0.38987 -0.05717 0.00000 0.00000 0.00000 72 -0.00209 -0.17301 0.00413 0.00000 0.00000 0.00000 70 0.00609 0.29570 -0.11505 0.00000 0.00000 0.00000 66 -0.16583 0.25357 -0.00995 0.00000 0.00000 0.00000 69 -0.23113 0.36422 -0.12278 0.00000 0.00000 0.00000 65 -0.36005 -0.36779 -0.16215 0.00000 0.00000 0.00000 31 -0.00534 -0.02358 -0.02773 0.00000 0.00000 0.00000 29 -0.00004 0.23947 0.00959 0.00000 0.00000 0.00000 25 -0.00312 0.26081 -0.02876 0.00000 0.00000 0.00000 23 -0.03673 0.19028 0.01870 0.00000 0.00000 0.00000 15 -0.01260 0.19419 0.01188 0.00000 0.00000 0.00000 14 0.07016 -0.26603 -0.03105 0.00000 0.00000 0.00000 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30 -0.04283 0.09470 -0.20451 0.00000 0.00000 0.00000 22 0.71184 0.26475 -0.45654 0.00000 0.00000 0.00000 13 0.11870 0.24770 0.12178 0.00000 0.00000 0.00000 12 0.69388 -0.35369 -0.12509 0.00000 0.00000 0.00000 80 -0.01341 0.05571 0.26283 0.00000 0.00000 0.00000 79 0.00719 0.00537 0.00244 0.00000 0.00000 0.00000 71 -0.52628 0.00905 -0.08736 0.00000 0.00000 0.00000 72 -0.00234 0.04447 -0.00749 0.00000 0.00000 0.00000 70 0.06699 -0.19638 0.34786 0.00000 0.00000 0.00000 66 -0.06538 0.17585 -0.03148 0.00000 0.00000 0.00000 69 -0.37481 1.03168 0.30482 0.00000 0.00000 0.00000 65 -0.40234 -0.12398 0.00039 0.00000 0.00000 0.00000 31 -0.00663 0.07361 -0.03602 0.00000 0.00000 0.00000 29 0.07108 -0.03978 0.02268 0.00000 0.00000 0.00000 25 0.00534 -0.14573 -0.01905 0.00000 0.00000 0.00000 23 -0.09435 0.71844 -0.02646 0.00000 0.00000 0.00000 15 -0.05131 0.13541 0.01204 0.00000 0.00000 0.00000 14 0.08354 -0.11467 -0.04709 0.00000 0.00000 0.00000 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-0.05943 0.11602 -0.32978 0.00000 0.00000 0.00000 22 0.40155 0.53889 -0.85143 0.00000 0.00000 0.00000 13 -0.15474 0.24321 0.17517 0.00000 0.00000 0.00000 12 0.15440 -0.28762 -0.71779 0.00000 0.00000 0.00000 80 -0.02991 0.27324 0.35215 0.00000 0.00000 0.00000 79 0.00185 -0.15701 0.00487 0.00000 0.00000 0.00000 71 -0.13275 -0.34306 -0.03813 0.00000 0.00000 0.00000 72 -0.00057 0.24736 -0.01486 0.00000 0.00000 0.00000 70 0.08700 -0.50240 0.59159 0.00000 0.00000 0.00000 Page3 66 0.11784 -0.06641 -0.03139 0.00000 0.00000 0.00000 69 -0.19993 0.95740 0.50607 0.00000 0.00000 0.00000 65 -0.09546 0.45018 0.22488 0.00000 0.00000 0.00000 31 -0.00386 0.13856 -0.02043 0.00000 0.00000 0.00000 29 0.05376 -0.23994 0.00906 0.00000 0.00000 0.00000 25 0.01492 -0.39519 -0.00510 0.00000 0.00000 0.00000 23 -0.09034 0.75583 -0.07966 0.00000 0.00000 0.00000 15 -0.06077 -0.06868 0.00317 0.00000 0.00000 0.00000 14 0.02863 0.35809 -0.02223 0.00000 0.00000 0.00000 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0.00701 0.02629 0.00275 0.00000 0.00000 0.00000 22 -0.39557 0.35100 -0.18473 0.00000 0.00000 0.00000 13 -0.25588 -0.07418 -0.00932 0.00000 0.00000 0.00000 12 -0.63272 0.41088 -0.37104 0.00000 0.00000 0.00000 80 -0.00562 0.24204 -0.00922 0.00000 0.00000 0.00000 79 -0.00621 -0.11177 0.00145 0.00000 0.00000 0.00000 71 0.38839 -0.13329 0.05789 0.00000 0.00000 0.00000 72 0.00205 0.12733 -0.00438 0.00000 0.00000 0.00000 70 -0.00492 -0.07944 0.12398 0.00000 0.00000 0.00000 66 0.16843 -0.18644 0.01089 0.00000 0.00000 0.00000 69 0.23871 -0.13442 0.12037 0.00000 0.00000 0.00000 65 0.35207 0.61988 0.15498 0.00000 0.00000 0.00000 31 0.00819 0.06456 0.04740 0.00000 0.00000 0.00000 29 -0.04036 -0.04114 -0.02128 0.00000 0.00000 0.00000 25 -0.00030 -0.05724 -0.00688 0.00000 0.00000 0.00000 23 -0.01390 0.01357 -0.00722 0.00000 0.00000 0.00000 15 -0.00685 -0.18763 -0.02382 0.00000 0.00000 0.00000 14 -0.06280 0.60374 0.08224 0.00000 0.00000 0.00000 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____________________________________________________________________________________________________________________________________________________________________________________________________________________________________________________ Note.-lc is the controlling load condition Direction of positive forces and moments Envelope of nodal reactions for : LC1=1.2D+Wo LC2=1.2D+W30 LC3=1.2D+W60 LC4=1.2D+W90 LC5=1.2D+W120 LC6=1.2D+W150 LC7=1.2D-Wo LC8=1.2D-W30 LC9=1.2D-W60 LC10=1.2D-W90 LC11=1.2D-W120 LC12=1.2D-W150 LC13=0.9D+Wo LC14=0.9D+W30 LC15=0.9D+W60 LC16=0.9D+W90 LC17=0.9D+W120 LC18=0.9D+W150 LC19=0.9D-Wo LC20=0.9D-W30 LC21=0.9D-W60 LC22=0.9D-W90 LC23=0.9D-W120 LC24=0.9D-W150 LC25=1.2D+Di+WI0 LC26=1.2D+Di+WI30 LC27=1.2D+Di+WI60 LC28=1.2D+Di+WI90 LC29=1.2D+Di+WI120 LC30=1.2D+Di+WI150 LC31=1.2D+Di-WI0 LC32=1.2D+Di-WI30 LC33=1.2D+Di-WI60 LC34=1.2D+Di-WI90 LC35=1.2D+Di-WI120 LC36=1.2D+Di-WI150 Page16 Forces Moments Node Fx lc Fy lc Fz lc Mx lc My lc Mz lc [Kip][Kip][Kip][Kip*ft][Kip*ft][Kip*ft] -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 24 Max 0.158 LC12 0.403 LC1 0.986 LC1 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.159 LC18 -0.213 LC19 -0.977 LC19 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 28 Max 0.754 LC4 0.482 LC12 0.212 LC5 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.722 LC22 -0.296 LC18 -0.201 LC23 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 30 Max 0.058 LC24 0.116 LC7 0.314 LC13 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.061 LC6 -0.085 LC13 -0.330 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 22 Max 0.712 LC5 0.539 LC7 0.855 LC13 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.688 LC23 -0.338 LC13 -0.851 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 13 Max 0.270 LC3 0.317 LC6 0.175 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.258 LC21 -0.311 LC24 -0.166 LC13 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 12 Max 0.754 LC4 0.852 LC12 0.686 LC13 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.741 LC10 -0.532 LC18 -0.718 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 80 Max 0.030 LC1 0.297 LC8 0.365 LC18 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.030 LC19 -0.169 LC14 -0.369 LC12 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 79 Max 0.008 LC4 0.184 LC1 0.005 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.008 LC22 -0.160 LC19 -0.005 LC13 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 71 Max 0.533 LC11 0.600 LC1 0.088 LC11 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.526 LC5 -0.375 LC19 -0.087 LC5 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 72 Max 0.003 LC22 0.253 LC19 0.015 LC13 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.003 LC4 -0.293 LC1 -0.015 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 70 Max 0.087 LC7 0.718 LC1 0.592 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.086 LC13 -0.529 LC19 -0.584 LC13 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 66 Max 0.168 LC9 0.254 LC3 0.039 LC12 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.166 LC15 -0.195 LC21 -0.038 LC18 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 69 Max 0.382 LC11 1.168 LC6 0.506 LC7 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.375 LC17 -0.966 LC24 -0.509 LC1 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 65 Max 0.431 LC22 0.666 LC8 0.226 LC20 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.439 LC4 -0.445 LC14 -0.232 LC2 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 31 Max 0.010 LC12 0.139 LC7 0.061 LC12 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.008 LC18 -0.102 LC13 -0.043 LC18 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 29 Max 0.085 LC18 0.438 LC1 0.026 LC18 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.121 LC12 -0.264 LC19 -0.036 LC12 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 25 Max 0.015 LC19 0.599 LC1 0.014 LC24 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.018 LC1 -0.420 LC19 -0.046 LC6 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 23 Max 0.071 LC24 0.848 LC6 0.091 LC1 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.116 LC6 -0.669 LC24 -0.081 LC19 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 15 Max 0.044 LC13 0.194 LC3 0.015 LC16 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.061 LC7 -0.188 LC21 -0.026 LC10 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- 14 Max 0.084 LC5 0.604 LC9 0.124 LC12 0.00000 LC1 0.00000 LC1 0.00000 LC1 Min -0.077 LC23 -0.308 LC15 -0.080 LC18 0.00000 LC1 0.00000 LC1 0.00000 LC1 -------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------------- Page17 Date: 3/9/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC CHECK EPOXY ANCHOR CONNECTION CAPACITY → EXISTING ANCHORS AT MODIFIED CHIMNEY MOUNT Reference:Hilti North American Product Technical Guide, 19th Edition Epoxy Type =HIT-HY20 (Assumed) Anchor Diameter =3/4 in.(HAS-E Threaded Rod) Embedment Depth = 8 in.(Assumed) Allowable Loads (lbs) Tensile Load 1400 Shear Load 1800 TENSILE FORCES Reaction F =985 lbs.(See Bentley Output) SHEAR FORCES Reactions in X direction:132 lbs.(See Bentley Output) Reactions in Y direction:403 lbs.(See Bentley Output) Resultant:424 lbs. No. of Supports =1 No. of Anchors / Support =1 Tension Design Load / Anchor = ft=985.00 lbs.<1400 lbs.Therefore, OK ! Shear Design Load / Anchor= fv=424.07 lbs.<1800 lbs.Therefore, OK ! CHECK COMBINED TENSION AND SHEAR ft / FT +fv / FV ≤1.0 0.704 + 0.236 =0.939 <1.0 Therefore, OK ! 1 1 1800 Spacing Reduct. Factor Edge Reduct. Factor Reduced Loads (lbs) 1 1 1400 Date: 3/9/2021 Project Name: 4BSS362A_BS23XC362_217 ESSEX ST_RT Project No.: 4BSS362A Designed By: CL Checked By: MSC CHECK EPOXY ANCHOR CONNECTION CAPACITY → PROPOSED ANCHORS AT MODIFIED CHIMNEY MOUNT Reference:Hilti North American Product Technical Guide, 19th Edition Epoxy Type =HIT-HY 270 Anchor Diameter =3/4 in. (HAS Threaded Rod) Embedment Depth = 8 in. Allowable Loads (lbs) Tensile Load 1575 Shear Load 1985 TENSILE FORCES Reaction F =509 lbs. (See Bentley Output) SHEAR FORCES Reactions in X direction:382 lbs. (See Bentley Output) Reactions in Y direction:1168 lbs. (See Bentley Output) Resultant:1229 lbs. No. of Supports =1 No. of Anchors / Support =1 Tension Design Load / Anchor = ft=509.00 lbs.<1575 lbs.Therefore, OK ! Shear Design Load / Anchor= fv=1228.88 lbs.<1985 lbs.Therefore, OK ! CHECK COMBINED TENSION AND SHEAR ft / FT +fv / FV ≤1.0 0.323 + 0.619 =0.942 <1.0 Therefore, OK ! 1 1 1 1985 Spacing Reduct. Factor Edge Reduct. Factor Conc. Thickness Reduct. Factor Reduced Loads (lbs) 1 1 1 1575 Reference Documents