C05 Attachment 17 031005L050501-Barillas Lookout-20230906-SAR-V9.pdf
PDF 2 MB Posted
- Solicitation number
- 127EAX26Q0069
- Issued by
-
Department of Agriculture Forest Service
About this file
This is a Feasibility Structural Analysis Report for a 54.4-foot self-support tower located near Santa Fe County, New Mexico, prepared by the Federal Aviation Administration (FAA) Structural Support Branch for the U.S. Forest Service (USFS). The analysis examines the structural adequacy of the existing tower supporting technology and appurtenances under current site-specific environmental loading conditions in accordance with ANSI/TIA-222-H and ASCE-7-22 design standards. The tower was modeled as a cantilever structure with five sections made of equal angle leg members, subject to wind loads of 105 mph basic wind speed and ice loads of 0.22 inches nominal thickness combined with 45 mph wind at the 9,202-foot elevation with 580-foot crest height. The structural analysis yielded a tower rating of 49.9% for existing physical conditions and current equipment configuration, indicating the tower structure passes all strength capacity requirements with controlling leg (T5) utilization at 49.9%. The analysis included service-level deflection calculations, foundation and soil capacity checks (not performed due to lack of design data), and comprehensive member capacity evaluations using finite element modeling via TNX Tower software. The report notes that all information not formally collected was derived from past experience and standard industry practice, and recommends verification of appurtenance functional performance and re-checking of plumb and twist in short intervals. An additional analysis scenario was run showing the tower would pass with two added antennas at the highest available position, though this does not justify proceeding with modifications without updated structural analysis.
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FAA Structural Support 8201 S. MacArthur Boulevard
Oklahoma City, OK 73169
Barrillas Lookout Tower
Page
Project
STRUCTURAL ANALYSIS
For
USFS
By
FAA-AJW-L500
Structural Analysis Report | REV 1.1
FEASIBILITY STRUCTURAL ANALYSIS REPORT
OF
EXISTING STRUCTURE, TECHNOLOGY & OTHER ASSETS
FOR
U.S Forest Service
Tower Location
Region 03, Forest 10
New Mexico – Barillas Lookout Santa Fe County, California
Latitude: 35°34'7.75"N, Longitude: 105°28'24.13"W
Report Date
Jul-2024
Analysis and Report by:
Mohanad Ashor, EIT Civil Engineer
FAA Mike Moroney Air Logistics Center Oklahoma City, Oklahoma
Report Checked by:
Eric Trujillo Civil Engineer
FAA Mike Moroney Air Logistics Center Oklahoma City, Oklahoma
Project
STRUCTURAL ANALYSIS
For
USFS
Table of Contents Table of Contents Executive Summary Detailed Analysis Report Results Appendix A - Detailed Analysis Graphics Appendix B – TNX Output Report
Project
STRUCTURAL ANALYSIS
For
USFS
Executive Summary
The analyzed tower is approximately 54.4 feet Self Support Tower constructed of 5 sections supporting existing technology and other assets attached at multiple heights on the tower. The tower is located near Santa Fe County, New Mexico and supports operational and functional capacity of the sector. Tower has been identified for an update of the tower capacity. A full tower assessment has not been completed only the tower mapping and equipment inventory have been analyzed with current field notes which constitute the basis of the tower model and analysis.
All information not collected to complete the structural analysis will be derived from past experience, standard industry practice and other available information. Information not provided for incorporation into the structural analysis report will constitute a limiting factor for the operational (or functional) capacity of the tower structure.
Completion of a structural analysis does not constitute a verification of the operational degradation of existing technology, appurtenances, and other assets due to potential increases in deflection tilt or twist of the tower structure.
This information was used to determine the tower rating and safe load capacity for the tower in accordance with the provisions contained in ANSI/TIA-222, “Structural Standard for Antenna Supporting Structures and Antennas”. The tower was modeled with the currently recorded existing loading under the site-specific environmental loading for Santa Fe County, California using a Type II Structure in a Class 2 Topography and Class C Exposure on a 9202 FT elevation and 580 FT crest.
The Structural Analysis Report shows the Tower Rating of 49.9% (TIA-222-H, ASCE-7-22) for the existing physical condition of the tower and existing load configuration of attached assets and appurtenances. A tower rating exceeding 100% shows that a tower cannot accommodate the existing technology and other assets under the 222-H design standards.
For all future tower modifications, it is recommended that the tower regardless of rating receive an updated analysis to determine possible effects of the modification on the structure and existing equipment. This should be completed prior to modifications to include the addition or removal of equipment and/or structural components.
Tower Utilization with Current Configuration of Equipment/Structure 49.9% Notes:
o All other tower members are at or below the currently identified member with the highest utilization.
Modifications to the tower can both change the member with the highest utilization and greatly increase the percentage of utilization.
o See section capacity table for specific member information.
Tower Utilization with Updated Configuration of Equipment/Structure PASS Notes:
o Upon US Forest Service request, an additional structural analysis was run with two added antennas, (TeleWave ANT150F2) located at the highest available position. Results should be utilized to inform on the addition of new equipment to the tower, but not as justification to move forward with additions or modifications to the existing tower configuration. All additions or modifications should still receive a structural analysis to confirm the towers’ ability to accept the proposed modifications and/or equipment.
o Structural analysis results are generated on an assumed tower structural integrity of 95% of perfect condition with no known damaged.
Project
STRUCTURAL ANALYSIS
For
USFS
Detailed Analysis Report
Objective
Determine overall structural system adequacy for the existing load scenarios defined for the tower site.
Study Scope
FAA-AJW-L500 Structural Support Branch has completed a tower mapping and review of the current tower structure to do discrepancies with tower geometry among USFS service providers.
The analysis performed represents the estimated tower capacity and utilization to determine an overall Rating and Pass/Fail result for the adequacy of the tower structure. The tower was not analyzed to determine an acceptable level of twist, sway and deflection for microwave emitting dishes attached (existing) to the tower structure. Nor was the foundation and soil analyzed to determine safe load carrying capacity and utilization. The report for the tower at the above referenced site utilizes details and information from government furnished or collected information to construct the existing tower structure and site conditions. Government furnished or collected information has been referenced from tower mapping field notes and pictures. All information not provided or collected to complete the structural system analysis was derived from past experience, standard industry practice and other available information used from other comparable USFS Programs.
Applicable Codes, Standards and References
Project
STRUCTURAL ANALYSIS
For
USFS
Basis of Design
The tower is a Self Support-type structure made up of 5 sections up to top of the structure. Each section is made of a Equal Angle leg section. The tower’s current condition information and tower data was not formally recorded but can be seen from onsite photography and field notes collected during the tower mapping. The location, asset inventory and physical condition were noted and used to create the original structural analysis mode.
Data Document(s) Tower FAA Tower Mapping 2023 Loading FAA Tower Mapping 2023 Soil N/A Foundation N/A
Criteria, Assumptions and Input
Assumptions
The current documents do not identify enough information or data to provide all of the required input to complete the structural analysis of the tower. The following assumptions were required to complete the structural model;
1. Tower Locality Input (Reference Previous sections)
2. Tower sections rigidly connected at all connection and joints
3. Tower Coatings modeled through tower weight increases
4. Tower and Foundation were installed according to and within manufacturer specifications
5. Tower and Foundations were maintained in accordance with manufacturers specifications
6. Tower and Foundation are in good working order and condition
7. Appurtenances, mounts and technology installed in accordance with man. specifications
8. Appurtenances, mounts and technology able to withstand loading
9. Elevation reference center of antennas and attachment points for mounts.
10. Weights and surface areas of mounts, hardware, feedlines and other incidental assets are included in the weight and surface areas of the appurtenance and attachment unless otherwise modeled
Project
STRUCTURAL ANALYSIS
For
USFS
Limitations
1. Model may not accurately reflect designed tower and foundation due to construction eccentricities from craftsmanship and quality of materials incorporated into construction.
2. Model may not accurately reflect designed or constructed tower due to the maintenance and rehabilitation of the tower during the service life.
3. Model may not accurately affect actual condition of tower from exposure to non-static loading (i.e. dynamic loads or cyclical loads)
4. Model does not characterize or calculate factored loads on appurtenances, mounts and technology attached to tower for capacity results.
Input
The tower was loaded and modeled under existing loading and geometry noted in tower mapping and photography from 2023.
Analysis Method and Modeling
A three-dimensional finite element model of the tower in each scenario was created using TNX Tower® Version 8.2.4.3 (Tower Numeric Inc.). The model was used based on government furnished and collected information and the loading scenarios requested by USFS. The model was analyzed as a cantilever structure subject to wind and ice loads applied to all attached assets and appurtenances such as antennas, mounts, lightening protection, etc. normalized for site specific conditions. No additional environmental loads or miscellaneous construction eccentric loading was considered.
The tower was analyzed for linear first order effects to determine a failing elements and corresponding load capacities. Load capacities and failing elements are identified after the model is analyzed and calculated for the resulting forces, moments and stresses. Additional analysis is conducted to estimate non-linear and second order effects on the tower. The effect of displacement on the member forces (P-Δ effects) is included to identify potential overstressing or local buckling.
After completion of the linear and non-linear idealization of the model a comparison is made of the calculated member stresses with the allowable values set forth in the design standard. All elements and members that exceed the allowable stresses are identified as failing elements. The highest utilized member load capacity governed the overall rating for the tower.
Project
STRUCTURAL ANALYSIS
For
USFS
Results
The structural tower analysis yielded the following results:
Tower Strength Capacity Results Load Scenario Controlling Section &
Member Tower Rating
PASS / FAIL
Existing Leg (T5) 49.9% PASS
Tower Service Results Load Scenario Tilt - (DEG) Twist - (DEG) PASS / FAIL
ACTUAL ALLOWED ACTUAL ALLOWED
Existing 0 0 0 0 PASS
0.500744 0.190875 0.0040524 0.318125 PASS
0.430847 0.528263 0.0148713 0.562313 PASS
0.441135 0.842888 0.0206329 0.524375 PASS
Foundation Capacity Results Load Scenario Bending (KFT) Shear (K) PASS / FAIL
ACTUAL ALLOWED ACTUAL ALLOWED
Existing NOT CHECKED. FOUNDATION DESIGN NOT PROVIDED.
Soil Capacity Results Load Scenario Overturning (KFT) Bearing (KSF) PASS / FAIL
ACTUAL ALLOWED ACTUAL ALLOWED
Existing NOT CHECKED. GEOTECHNICAL INVESTIAGATION NOT PROVIDED.
Project
STRUCTURAL ANALYSIS
For
USFS
Conclusions
The structural system analysis produced the following conclusions:
• Tower Strength Capacity Results Pass
• Tower Service Results Pass
• Foundation Capacity Results Not Checked
• Soil Capacity Results Not Checked
Recommendations
The following items are recommended
1.) Verify the functional and operational performance of appurtenances and attachments.
2.) Re-check of Plump and Twist in short terms.
Project
STRUCTURAL ANALYSIS
For
USFS
Appendix A - Detailed Analysis Graphics
Project
STRUCTURAL ANALYSIS
For
USFS
Project
STRUCTURAL ANALYSIS
For
USFS
Project
STRUCTURAL ANALYSIS
For
USFS
Project
STRUCTURAL ANALYSIS
For
USFS
Appendix B – TNX Output Report
Tower Input Data
The main tower is a 4x free standing tower with an overall height of 54.40 ft above the ground line.
The base of the tower is set at an elevation of 0.00 ft above the ground line.
The face width of the tower is 13.33 ft at the top and 22.50 ft at the base.
This tower is designed using the TIA-222-H standard.
The following design criteria apply:
1. Tower is located in Santa Fe County, New Mexico.
2. Tower base elevation above sea level: 9202.00 ft.
3. Basic wind speed of 105 mph.
4. Risk Category II.
5. Exposure Category C.
6. Simplified Topographic Factor Procedure for wind speed-up calculations is used.
7. Topographic Category: 2.
8. Crest Height: 580.00 ft.
9. Nominal ice thickness of 0.2200 in.
10. Ice thickness is considered to increase with height.
11. Ice density of 56 pcf.
12. A wind speed of 45 mph is used in combination with ice.
13. Temperature drop of 50 °F.
14. Deflections calculated using a wind speed of 60 mph.
15. Weld together tower sections have flange connections..
16. Connections use galvanized A325 bolts, nuts and locking devices. Installation per TIA/EIA-222 and AISC
Specifications..
17. Tower members are ''hot dipped'' galvanized in accordance with ASTM A123 and ASTM A153 Standards..
18. Welds are fabricated with ER-70S-6 electrodes..
19. A non-linear (P-delta) analysis was used.
20. Pressures are calculated at each section.
21. Stress ratio used in tower member design is 1.
22. Local bending stresses due to climbing loads, feed line supports, and appurtenance mounts are not considered.
Options
Consider Moments - Legs Assume Legs Pinned √ Calculate Redundant Bracing Forces Consider Moments - Horizontals √ Assume Rigid Index Plate Ignore Redundant Members in FEA Consider Moments - Diagonals √ Use Clear Spans For Wind Area SR Leg Bolts Resist Compression Use Moment Magnification √ Use Clear Spans For KL/r √ All Leg Panels Have Same Allowable √ Use Code Stress Ratios Retension Guys To Initial Tension Offset Girt At Foundation √ Use Code Safety Factors - Guys √ Bypass Mast Stability Checks √ Consider Feed Line Torque Escalate Ice √ Use Azimuth Dish Coefficients √ Include Angle Block Shear Check Always Use Max Kz √ Project Wind Area of Appurtenances Use TIA-222-H Bracing Resist. Exemption Use Special Wind Profile √ Alternative Appurt. EPA Calculation Use TIA-222-H Tension Splice Exemption √ Include Bolts In Member Capacity Autocalc Torque Arm Areas Poles Leg Bolts Are At Top Of Section Add IBC .6D+W Combination Include Shear-Torsion Interaction √ Secondary Horizontal Braces Leg √ Sort Capacity Reports By Component Always Use Sub-Critical Flow Use Diamond Inner Bracing (4 Sided) √ Triangulate Diamond Inner Bracing Use Top Mounted Sockets √ SR Members Have Cut Ends Treat Feed Line Bundles As Cylinder Pole Without Linear Attachments √ SR Members Are Concentric Ignore KL/ry For 60 Deg. Angle Legs Pole With Shroud Or No Appurtenances Distribute Leg Loads As Uniform Use ASCE 10 X-Brace Ly Rules Outside and Inside Corner Radii Are Known
Project
STRUCTURAL ANALYSIS
For
USFS
Leg C Leg D
Fa ce
A
Face B
Face D
Square Tower
Face C
Wind 0
Wind 90
Wind
Leg A Leg B
Z
X
Tower Section Geometry
Tower Section
Elevation ft
Assembly Database
Description Section Width
Number of
Sections
Length
T1 54.40-44.40 13.33 1 10.00 T2 44.40-34.40 15.02 1 10.00 T3 34.40-23.80 16.70 1 10.60 T4 23.80-12.50 18.49 1 11.30 T5 12.50-0.00 20.39 1 12.50
Tower Section Geometry (cont’d)
Diagonal Spacing
Bracing Type
Has K Brace
End Panels
Has Horizontals
Top Girt Offset in
Bottom Girt Offset
T1 54.40-44.40 10.00 K1 Down No Yes 0.0000 0.0000 T2 44.40-34.40 10.00 K1 Down No Yes 0.0000 0.0000 T3 34.40-23.80 10.60 K1 Down No Yes 0.0000 0.0000 T4 23.80-12.50 11.30 K1 Down No Yes 0.0000 0.0000 T5 12.50-0.00 12.50 K1 Down No Yes 0.0000 0.0000
Project
STRUCTURAL ANALYSIS
For
USFS
ft
Leg Type
Size
Grade
T1 54.40-44.40 Equal Angle L3x3x1/4 A572-50 (50 ksi)
Double Angle 2L2 1/2x2x3/16 A572-50 (50 ksi)
T2 44.40-34.40 Equal Angle L3x3x1/4 A572-50 (50 ksi)
Double Angle 2L2 1/2x2x3/16 A572-50 (50 ksi)
T3 34.40-23.80 Equal Angle L3 1/2x3 1/2x1/4 A572-50 (50 ksi)
Double Angle 2L2 1/2x2x3/16 A572-50 (50 ksi)
T4 23.80-12.50 Equal Angle L4x4x1/4 A572-50 (50 ksi)
Double Angle 2L3x2 1/2x1/4 A572-50 (50 ksi)
T5 12.50-0.00 Equal Angle L4x4x1/4 A572-50 (50 ksi)
Double Angle 2L3 1/2x3x1/4 A572-50 (50 ksi)
No.
of
Mid Girts
Mid Girt
Horizontal
T1 54.40-44.40 None Flat Bar A36 (36 ksi)
Double Angle 2L3 1/2x3x1/4 A572-50 (50 ksi)
T2 44.40-34.40 None Flat Bar A36 (36 ksi)
Double Angle 2L3 1/2x3x1/4 A572-50 (50 ksi)
T3 34.40-23.80 None Flat Bar A36 (36 ksi)
Double Angle 2L3 1/2x3x1/4 A572-50 (50 ksi)
T4 23.80-12.50 None Flat Bar A36 (36 ksi)
Double Angle 2L3 1/2x3x1/4 A572-50 (50 ksi)
T5 12.50-0.00 None Flat Bar A36 (36 ksi)
Double Angle 2L4x3x1/4 A572-50 (50 ksi)
Redundant Bracing Grade
K Factor
T1 54.40- 44.40
A36 (36 ksi) A36 (36 ksi)
Horizontal (1) Diagonal (1)
Double Angle Double Equal Angle
2L2 1/2x2x1/4 2L2 1/2x2 1/2x1/4
T2 44.40- 34.40
A36 (36 ksi) A36 (36 ksi)
Horizontal (1) Diagonal (1)
Double Angle Double Equal Angle
2L2 1/2x2x1/4 2L2 1/2x2 1/2x1/4
T3 34.40- 23.80
A36 (36 ksi) A36 (36 ksi)
Horizontal (1) Diagonal (1)
Double Angle Double Equal Angle
2L2 1/2x2x1/4 2L2 1/2x2 1/2x1/4
T4 23.80- 12.50
A36 (36 ksi) A36 (36 ksi)
Horizontal (1) Diagonal (1)
Double Angle Double Equal Angle
2L2 1/2x2x1/4 2L2 1/2x2 1/2x1/4
T5 12.50-0.00 A36 (36 ksi) A36 (36 ksi)
Horizontal (1) Diagonal (1)
Double Angle Double Equal Angle
2L2 1/2x2x1/4 2L2 1/2x2 1/2x1/4
Project
STRUCTURAL ANALYSIS
For
USFS
Gusset Area
(per face) ft2
Gusset Thickness
Gusset Grade Adjust. Factor Af
Adjust.
Factor
Ar
Weight Mult.
Double Angle Stitch Bolt Spacing
Diagonals in
Double Angle Stitch Bolt Spacing
Horizontals in
Double Angle Stitch Bolt Spacing
Redundants in
T1 54.40-44.40 0.00 0.0000 A36 (36 ksi)
1.05 1 1.05 36.0000 36.0000 36.0000
T2 44.40-34.40 0.00 0.0000 A36 (36 ksi)
1.05 1 1.05 36.0000 36.0000 36.0000
T3 34.40-23.80 0.00 0.0000 A36 (36 ksi)
1.05 1 1.05 36.0000 36.0000 36.0000
T4 23.80-12.50 0.00 0.0000 A36 (36 ksi)
1.05 1 1.05 36.0000 36.0000 36.0000
T5 12.50-0.00 0.00 0.0000 A36 (36 ksi)
1.05 1 1.05 36.0000 36.0000 36.0000
K Factors1
Calc K
Single Angles
Calc K
Solid Rounds
Legs X Brace Diags
X Y
K Brace Diags
X Y
Single Diags
Y
Girts
Horiz.
Sec.
Horiz.
Inner Brace
T1 54.40- 44.40
Yes No 1 1
T2 44.40- 34.40
Yes No 1 1
T3 34.40- 23.80
Yes No 1 1
T4 23.80- 12.50
Yes No 1 1
T5 12.50-0.00 Yes No 1 1
1Note: K factors are applied to member segment lengths. K-braces without inner supporting members will have the K factor in the out-of-plane direction applied to the overall length.
ft
Leg Diagonal Top Girt Bottom Girt Mid Girt Long Horizontal Short Horizontal
Net Width Deduct
U
Net Width Deduct
Net
Deduct
Deduct
Deduct
Deduct
T1 54.40-44.40 0.0000 1 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 T2 44.40-34.40 0.0000 1 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 T3 34.40-23.80 0.0000 1 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 T4 23.80-12.50 0.0000 1 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 T5 12.50-0.00 0.0000 1 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75
Project
STRUCTURAL ANALYSIS
For
USFS
ft
Redundant Horizontal
Redundant Diagonal
Redundant Sub- Diagonal
Redundant Sub- Horizontal
Redundant Vertical Redundant Hip Redundant Hip Diagonal
Net Width Deduct
Deduct
Deduct
Deduct
Deduct
T1 54.40-44.40 0.0000 0.75 (1) 0.0000 0.75 (1)
0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 (1) 0.0000 0.75 (1)
0.0000 0.75 (2) 0.0000 0.75 (2)
0.0000 0.75 (2) 0.0000 0.75 (2)
0.0000 0.75 (3) 0.0000 0.75 (3)
0.0000 0.75 (3) 0.0000 0.75 (3)
0.0000 0.75 (4) 0.0000 0.75 (4)
0.0000 0.75 (4) 0.0000 0.75 (4)
T2 44.40-34.40 0.0000 0.75 (1) 0.0000 0.75 (1)
0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 (1) 0.0000 0.75 (1)
0.0000 0.75 (2) 0.0000 0.75 (2)
0.0000 0.75 (2) 0.0000 0.75 (2)
0.0000 0.75 (3) 0.0000 0.75 (3)
0.0000 0.75 (3) 0.0000 0.75 (3)
0.0000 0.75 (4) 0.0000 0.75 (4)
0.0000 0.75 (4) 0.0000 0.75 (4)
T3 34.40-23.80 0.0000 0.75 (1) 0.0000 0.75 (1)
0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 (1) 0.0000 0.75 (1)
0.0000 0.75 (2) 0.0000 0.75 (2)
0.0000 0.75 (2) 0.0000 0.75 (2)
0.0000 0.75 (3) 0.0000 0.75 (3)
0.0000 0.75 (3) 0.0000 0.75 (3)
0.0000 0.75 (4) 0.0000 0.75 (4)
0.0000 0.75 (4) 0.0000 0.75 (4)
T4 23.80-12.50 0.0000 0.75 (1) 0.0000 0.75 (1)
0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 (1) 0.0000 0.75 (1)
0.0000 0.75 (2) 0.0000 0.75 (2)
0.0000 0.75 (2) 0.0000 0.75 (2)
0.0000 0.75 (3) 0.0000 0.75 (3)
0.0000 0.75 (3) 0.0000 0.75 (3)
0.0000 0.75 (4) 0.0000 0.75 (4)
0.0000 0.75 (4) 0.0000 0.75 (4)
T5 12.50-0.00 0.0000 0.75 (1) 0.0000 0.75 (1)
0.0000 0.75 0.0000 0.75 0.0000 0.75 0.0000 0.75 (1) 0.0000 0.75 (1)
0.0000 0.75 (2) 0.0000 0.75 (2)
0.0000 0.75 (2) 0.0000 0.75 (2)
0.0000 0.75 (3) 0.0000 0.75 (3)
0.0000 0.75 (3) 0.0000 0.75 (3)
0.0000 0.75 (4) 0.0000 0.75 (4)
0.0000 0.75 (4) 0.0000 0.75 (4)
Project
STRUCTURAL ANALYSIS
For
USFS
ft
Leg Connection
Type
Leg Diagonal Top Girt Bottom Girt Mid Girt Long Horizontal Short Horizontal
Bolt Size in
No. Bolt Size in
No. Bolt Size in
No. Bolt Size in
No. Bolt Size in
No. Bolt Size in
No. Bolt Size in
No.
T1 54.40-44.40 Sleeve SS 0.7500 A325N
12 0.7500 A325N
3 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 0.7500 A325N
3 0.6250 A325N
T2 44.40-34.40 Sleeve SS 0.7500 A325N
12 0.7500 A325N
3 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 0.7500 A325N
3 0.6250 A325N
T3 34.40-23.80 Sleeve SS 0.7500 A325N
12 0.7500 A325N
3 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 0.7500 A325N
3 0.6250 A325N
T4 23.80-12.50 Sleeve SS 0.7500 A325N
12 0.7500 A325N
3 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 0.7500 A325N
3 0.6250 A325N
T5 12.50-0.00 Flange 0.8750 A325N
0 0.7500 A325N
3 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 0.7500 A325N
3 0.6250 A325N ft
Redundant Horizontal
Redundant Diagonal
Redundant Sub- Diagonal
Redundant Sub- Horizontal
Redundant Vertical Redundant Hip Redundant Hip Diagonal
Bolt Size
Bolt Size
T1 54.40-44.40 0.7500
1 (1) 0.7500 A325N
1 (1) 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 (1) 0.6250 A325N
0 (1)
0.7500 A325N
1 (2) 0.7500 A325N
1 (2) 0.6250 A325N
0 (2) 0.6250 A325N
0 (2)
0.7500 A325N
1 (3) 0.7500 A325N
1 (3) 0.6250 A325N
0 (3) 0.6250 A325N
0 (3)
0.7500 A325N
1 (4) 0.7500 A325N
1 (4) 0.6250 A325N
0 (4) 0.6250 A325N
0 (4)
T2 44.40-34.40 0.7500 A325N
1 (1) 0.7500 A325N
1 (1) 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 (1) 0.6250 A325N
0 (1)
0.7500 A325N
1 (2) 0.7500 A325N
1 (2) 0.6250 A325N
0 (2) 0.6250 A325N
0 (2)
0.7500 A325N
1 (3) 0.7500 A325N
1 (3) 0.6250 A325N
0 (3) 0.6250 A325N
0 (3)
0.7500 A325N
1 (4) 0.7500 A325N
1 (4) 0.6250 A325N
0 (4) 0.6250 A325N
0 (4)
T3 34.40-23.80 0.7500 A325N
1 (1) 0.7500 A325N
1 (1) 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 (1) 0.6250 A325N
0 (1)
0.7500 A325N
1 (2) 0.7500 A325N
1 (2) 0.6250 A325N
0 (2) 0.6250 A325N
0 (2)
0.7500 A325N
1 (3) 0.7500 A325N
1 (3) 0.6250 A325N
0 (3) 0.6250 A325N
0 (3)
0.7500 A325N
1 (4) 0.7500 A325N
1 (4) 0.6250 A325N
0 (4) 0.6250 A325N
0 (4)
T4 23.80-12.50 0.7500 A325N
1 (1) 0.7500 A325N
1 (1) 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 (1) 0.6250 A325N
0 (1)
0.7500 A325N
1 (2) 0.7500 A325N
1 (2) 0.6250 A325N
0 (2) 0.6250 A325N
0 (2)
0.7500 A325N
1 (3) 0.7500 A325N
1 (3) 0.6250 A325N
0 (3) 0.6250 A325N
0 (3)
0.7500 A325N
1 (4) 0.7500 A325N
1 (4) 0.6250 A325N
0 (4) 0.6250
0 (4)
Project
STRUCTURAL ANALYSIS
For
USFS
Elevation ft
Redundant Horizontal
Redundant Diagonal
Redundant Sub- Diagonal
Redundant Sub- Horizontal
Redundant Vertical Redundant Hip Redundant Hip Diagonal
Bolt Size
T5 12.50-0.00 0.7500
1 (1) 0.7500 A325N
1 (1) 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 0.6250 A325N
0 (1) 0.6250
0 (1)
0.7500
1 (2) 0.7500 A325N
1 (2) 0.6250 A325N
0 (2) 0.6250
0 (2)
1 (3) 0.7500 A325N
1 (3) 0.6250 A325N
0 (3) 0.6250
0 (3)
1 (4) 0.7500 A325N
1 (4) 0.6250 A325N
0 (4) 0.6250
0 (4)
Feed Line/Linear Appurtenances - Entered As Area
Description Face or
Leg
Allow Shield
Exclude From
Torque Calculation
Component
Placement
Total
CAAA
ft2/ft
Weight plf stair bovine A No No CaAa (In Face)
12.50 - 0.00 1 No Ice 1/2'' Ice
1.00 1.11
35.00 38.67 stair bovine C No No CaAa (In Face)
23.00 - 12.50 1 No Ice 1/2'' Ice
1.00 1.11
35.00 38.67 stair bovine A No No CaAa (In Face)
34.50 - 23.00 1 No Ice 1/2'' Ice
1.00 1.11
35.00 38.67 stair bovine C No No CaAa (In Face)
44.50 - 34.50 1 No Ice 1/2'' Ice
1.00 1.11
35.00 38.67 stair bovine A No No CaAa (In Face)
54.40 - 44.50 1 No Ice 1/2'' Ice
1.00 1.11
35.00 38.67
Feed Line/Linear Appurtenances Section Areas
Section
Tower Elevation
Face AR
AF
In Face ft2
CAAA
Out Face lb T1 54.40-44.40 A
B C D
0.000 0.000 0.000 0.000
0.000 0.000 0.000 0.000
9.900 0.000 0.100 0.000
0.000 0.000 0.000 0.000
346.50 0.00 3.50 0.00
T2 44.40-34.40 A B C D
0.000 0.000 0.000 0.000
0.000 0.000 0.000 0.000
0.100 0.000 9.900 0.000
0.000 0.000 0.000 0.000
3.50 0.00
346.50 0.00
T3 34.40-23.80 A 0.000 0.000 10.600 0.000 371.00
Project
STRUCTURAL ANALYSIS
For
USFS
Section
Tower Elevation
Face AR
In Face ft2
CAAA
Out Face
B C D
0.000 0.000 0.000
0.000 0.000 0.000
0.000 0.000 0.000
0.000 0.000 0.000
0.00 0.00 0.00
T4 23.80-12.50 A B C D
0.000 0.000 0.000 0.000
0.000 0.000 0.000 0.000
0.800 0.000
10.500 0.000
0.000 0.000 0.000 0.000
28.00 0.00
367.50 0.00
T5 12.50-0.00 A B C D
0.000 0.000 0.000 0.000
0.000 0.000 0.000 0.000
12.500 0.000 0.000 0.000
0.000 0.000 0.000 0.000
437.50 0.00
Feed Line/Linear Appurtenances Section Areas - With Ice
Section
Tower Elevation ft
Face or
Leg
Ice Thickness
AR
In Face ft2
CAAA
Out Face
T1 54.40-44.40 A
B C D
0.288 0.000 0.000 0.000 0.000
0.000 0.000 0.000 0.000
10.533 0.000 0.106 0.000
0.000 0.000 0.000 0.000
367.44 0.00 3.71 0.00
T2 44.40-34.40 A B C D
0.283 0.000 0.000 0.000 0.000
0.000 0.000 0.000 0.000
0.106 0.000
10.522 0.000
0.000 0.000 0.000 0.000
3.71 0.00
367.06 0.00
T3 34.40-23.80 A B C D
0.275 0.000 0.000 0.000 0.000
0.000 0.000 0.000 0.000
11.249 0.000 0.000 0.000
0.000 0.000 0.000 0.000
392.45 0.00 0.00 0.00
T4 23.80-12.50 A B C D
0.264 0.000 0.000 0.000 0.000
0.000 0.000 0.000 0.000
0.847 0.000
11.116 0.000
0.000 0.000 0.000 0.000
29.55 0.00
387.87 0.00
T5 12.50-0.00 A B C D
0.239 0.000 0.000 0.000 0.000
0.000 0.000 0.000 0.000
13.163 0.000 0.000 0.000
0.000 0.000 0.000 0.000
459.41 0.00
Feed Line Center of Pressure
Section Elevation
CPX
CPZ
CPX
Ice in
CPZ
Ice in
T1 54.40-44.40 -11.6948 0.0000 -11.6262 0.0000 T2 44.40-34.40 12.3704 0.0000 12.2812 0.0000 T3 34.40-23.80 -13.1679 0.0000 -13.0928 0.0000 T4 23.80-12.50 11.4475 0.0000 11.4385 0.0000 T5 12.50-0.00 -13.5889 0.0000 -13.6178 0.0000
Project
STRUCTURAL ANALYSIS
For
USFS
Shielding Factor Ka
Feed Line Record No.
Description Feed Line Segment Elev.
Ka No Ice
Ka Ice
T1 4 stair bovine 44.40 - 44.50 1.0000 1.0000 T1 5 stair bovine 44.50 - 54.40 1.0000 1.0000 T2 3 stair bovine 34.40 - 34.50 1.0000 1.0000 T2 4 stair bovine 34.50 - 44.40 1.0000 1.0000 T3 3 stair bovine 23.80 - 34.40 1.0000 1.0000 T4 2 stair bovine 12.50 - 23.00 1.0000 1.0000 T4 3 stair bovine 23.00 - 23.80 1.0000 1.0000 T5 1 stair bovine 0.00 - 12.50 1.0000 1.0000
Discrete Tower Loads or
Leg
Offset Type
Offsets:
Horz
Lateral Vert ft ft ft
Azimuth Adjustment
Front
Side platform full steel 24'x24' C None 0.0000 54.20 No Ice 1/2'' Ice
7.20 8.82
7.20 8.82
17500.00 20262.80
Cabin 13'x13' C None 0.0000 58.60 No Ice 1/2'' Ice
144.00 145.49
144.00 145.49
10650.00 12613.53
Mounting Pipe - 1.75'' x 3' A From Face 0.00 0.00 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' A From Face 0.00 6.70 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' A From Face 0.00 -6.70 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' A From Face 0.00 12.00 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' A From Face 0.00 -12.00 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' B From Face 0.00 0.00 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' B From Face 0.00 6.70 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' B From Face 0.00 -6.70 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' B From Face 0.00 12.00 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' B From Face 0.00 0.0000 54.00 No Ice 0.48 0.48 8.50
Project
STRUCTURAL ANALYSIS
For
USFS
or
Leg
Offset Type
Offsets:
Horz
Lateral Vert ft ft ft
Azimuth Adjustment
Front
Side
-12.00 1.50
1/2'' Ice 0.67 0.67 12.82
Mounting Pipe - 1.75'' x 3' C From Face 0.00 0.00 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' C From Face 0.00 6.70 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' C From Face 0.00 -6.70 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' C From Face 0.00 12.00 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' C From Face 0.00 -12.00 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' D From Face 0.00 0.00 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' D From Face 0.00 6.70 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' D From Face 0.00 -6.70 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' D From Face 0.00 12.00 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe - 1.75'' x 3' D From Face 0.00 -12.00 1.50
0.0000 54.00 No Ice 1/2'' Ice
0.48 0.67
0.48 0.67
8.50 12.82
Mounting Pipe Horizontal - 2'' Dia x 24' L
A From Face 0.00 0.00 3.00
0.0000 54.00 No Ice 1/2'' Ice
4.80 6.41
0.03 0.06
130.00 176.96
Mounting Pipe Horizontal - 2'' Dia x 24' L
B From Face 0.00 0.00 3.00
0.0000 54.00 No Ice 1/2'' Ice
4.80 6.41
0.03 0.06
130.00 176.96
Mounting Pipe Horizontal - 2'' Dia x 24' L
C From Face 0.00 0.00 3.00
0.0000 54.00 No Ice 1/2'' Ice
4.80 6.41
0.03 0.06
130.00 176.96
Mounting Pipe Horizontal - 2'' Dia x 24' L
D From Face 0.00 0.00 3.00
0.0000 54.00 No Ice 1/2'' Ice
4.80 6.41
0.03 0.06
130.00 176.96
10' 2-Bay Dipole B From
Centroid- Face
7.00 7.00 14.00
0.0000 54.00 No Ice 1/2'' Ice
3.00 4.50
3.00 4.50
28.00 50.00
10' 2-Bay Dipole D From Centroid-
Face
7.00 7.00 14.00
0.0000 54.00 No Ice 1/2'' Ice
3.00 4.50
3.00 4.50
28.00 50.00
Project
STRUCTURAL ANALYSIS
For
USFS
Tower Pressures - No Ice
GH = 0.850
z
KZ
qz psf
AG
F a c e
Aleg
In
Face ft2
CAAA
Out Face ft2 T1 54.40-44.40 49.40 1.091 36 143.179 A
B C D
18.521 18.521 18.521 18.521
0.000 0.000 0.000 0.000
5.035 27.19 27.19 27.19 27.19
9.900 0.000 0.100 0.000
0.000 0.000 0.000 0.000
T2 44.40-34.40 39.40 1.04 35 160.030 A B C D
19.562 19.562 19.562 19.562
0.000 0.000 0.000 0.000
5.035 25.74 25.74 25.74 25.74
0.100 0.000 9.900 0.000
0.000 0.000 0.000 0.000
T3 34.40-23.80 29.10 0.976 33 188.238 A B C D
22.128 22.128 22.128 22.128
0.000 0.000 0.000 0.000
6.227 28.14 28.14 28.14 28.14
10.600 0.000 0.000 0.000
0.000 0.000 0.000 0.000
T4 23.80-12.50 18.15 0.884 30 221.777 A B C D
26.302 26.302 26.302 26.302
0.000 0.000 0.000 0.000
7.587 28.84 28.84 28.84 28.84
0.800 0.000
10.500 0.000
0.000 0.000 0.000 0.000
T5 12.50-0.00 6.25 0.85 30 270.395 A B C D
31.432 31.432 31.432 31.432
0.000 0.000 0.000 0.000
8.392 26.70 26.70 26.70 26.70
12.500 0.000 0.000 0.000
0.000 0.000 0.000
Tower Pressure - With Ice tZ a c
Face ft2
CAAA
Out Face ft2 T1 54.40-44.40 49.40 1.091 7 0.2879 143.660 A
B C D
18.521 18.521 18.521 18.521
3.619 3.619 3.619 3.619
6.002 27.11 27.11 27.11 27.11
10.533 0.000 0.106 0.000
0.000 0.000 0.000 0.000
T2 44.40-34.40 39.40 1.04 6 0.2827 160.503 A B C D
19.562 19.562 19.562 19.562
3.745 3.745 3.745 3.745
5.984 25.68 25.68 25.68 25.68
0.106 0.000
10.522 0.000
0.000 0.000 0.000 0.000
T3 34.40-23.80 29.10 0.976 6 0.2755 188.727 A B C D
22.128 22.128 22.128 22.128
3.951 3.951 3.951 3.951
7.207 27.64 27.64 27.64 27.64
11.249 0.000 0.000 0.000
0.000 0.000 0.000 0.000
T4 23.80-12.50 18.15 0.884 6 0.2640 222.276 A B C D
26.302 26.302 26.302 26.302
4.107 4.107 4.107 4.107
8.588 28.24 28.24 28.24 28.24
0.847 0.000
11.116 0.000
0.000 0.000 0.000 0.000
T5 12.50-0.00 6.25 0.85 5 0.2386 270.894 A B C
31.432 31.432 31.432
4.106 4.106 4.106
9.393 26.43 26.43 26.43
13.163 0.000 0.000
0.000
Project
STRUCTURAL ANALYSIS
For
USFS
tZ a c
Face ft2
CAAA
Out Face
D 31.432 4.106 26.43 0.000 0.000
Tower Pressure - Service a c
Face ft2
CAAA
Out Face ft2 T1 54.40-44.40 49.40 1.091 12 143.179 A
B C D
18.521 18.521 18.521 18.521
0.000 0.000 0.000 0.000
5.035 27.19 27.19 27.19 27.19
9.900 0.000 0.100 0.000
0.000 0.000 0.000 0.000
T2 44.40-34.40 39.40 1.04 11 160.030 A B C D
19.562 19.562 19.562 19.562
0.000 0.000 0.000 0.000
5.035 25.74 25.74 25.74 25.74
0.100 0.000 9.900 0.000
0.000 0.000 0.000 0.000
T3 34.40-23.80 29.10 0.976 11 188.238 A B C D
22.128 22.128 22.128 22.128
0.000 0.000 0.000 0.000
6.227 28.14 28.14 28.14 28.14
10.600 0.000 0.000 0.000
0.000 0.000 0.000 0.000
T4 23.80-12.50 18.15 0.884 10 221.777 A B C D
26.302 26.302 26.302 26.302
0.000 0.000 0.000 0.000
7.587 28.84 28.84 28.84 28.84
0.800 0.000
10.500 0.000
0.000 0.000 0.000 0.000
T5 12.50-0.00 6.25 0.85 10 270.395 A B C D
31.432 31.432 31.432 31.432
0.000 0.000 0.000 0.000
8.392 26.70 26.70 26.70 26.70
12.500 0.000 0.000 0.000
0.000 0.000
Tower Forces - No Ice - Wind Normal To Face
Add
Self a c e CF
DF
DR
AE
w
Ctrl.
Face
T1 54.40- 44.40
350.00 1981.66 A B C D
0.129 0.129 0.129 0.129
3.304 3.304 3.304 3.304
36 1
18.521 18.521 18.521 18.521
2182.22 218.22 D
T2 44.40- 34.40
350.00 2122.01 A B C D
0.122 0.122 0.122 0.122
3.339 3.339 3.339 3.339
35 1
19.562 19.562 19.562 19.562
2228.05 222.80 D
T3 34.40- 23.80
371.00 2353.75 A B C D
0.118 0.118 0.118 0.118
3.362 3.362 3.362 3.362
33 1
22.128 22.128 22.128 22.128
2389.10 225.39 D
T4 23.80- 12.50
395.50 3048.32 A B
0.119 0.119
3.357 3.357
30 1
26.302 26.302
2569.50 227.39 D
Project
STRUCTURAL ANALYSIS
For
USFS
a c
Face
C D
0.119 0.119
3.357 3.357
26.302 26.302
T5 12.50-0.00 437.50 3680.07 A B C D
0.116 0.116 0.116 0.116
3.368 3.368 3.368 3.368
30 1
31.432 31.432 31.432 31.432
2982.73 238.62 D
Sum Weight: 1904.00 13185.81 OTM 330388.18 lb-ft
12351.60
Tower Forces - No Ice - Wind 45 To Face a c
Face
T1 54.40- 44.40
350.00 1981.66 A B C D
0.129 0.129 0.129 0.129
3.304 3.304 3.304 3.304
36 1.097 1.097 1.097 1.097
1.097 1.097 1.097 1.097
20.317 20.317 20.317 20.317
2364.19 236.42 D
T2 44.40- 34.40
350.00 2122.01 A B C D
0.122 0.122 0.122 0.122
3.339 3.339 3.339 3.339
35 1.092 1.092 1.092 1.092
1.092 1.092 1.092 1.092
21.356 21.356 21.356 21.356
2405.19 240.52 D
T3 34.40- 23.80
371.00 2353.75 A B C D
0.118 0.118 0.118 0.118
3.362 3.362 3.362 3.362
33 1.088 1.088 1.088 1.088
1.088 1.088 1.088 1.088
24.079 24.079 24.079 24.079
2573.46 242.78 D
T4 23.80- 12.50
395.50 3048.32 A B C D
0.119 0.119 0.119 0.119
3.357 3.357 3.357 3.357
30 1.089 1.089 1.089 1.089
1.089 1.089 1.089 1.089
28.642 28.642 28.642 28.642
2772.12 245.32 D
T5 12.50-0.00 437.50 3680.07 A B C D
0.116 0.116 0.116 0.116
3.368 3.368 3.368 3.368
30 1.087 1.087 1.087 1.087
1.087 1.087 1.087 1.087
34.172 34.172 34.172 34.172
3215.31 257.22 D
Sum Weight: 1904.00 13185.81 OTM 356853.07
13330.28
Tower Forces - With Ice - Wind Normal To Face a c
Face
T1 54.40- 44.40
371.15 2505.07 A B C D
0.154 0.154 0.154 0.154
3.186 3.186 3.186 3.186
7 1
20.576 20.576 20.576 20.576
428.98 42.90 D
Project
STRUCTURAL ANALYSIS
For
USFS
a c
Face
T2 44.40- 34.40
370.77 2669.37 A B C D
0.145 0.145 0.145 0.145
3.228 3.228 3.228 3.228
6 1
21.686 21.686 21.686 21.686
438.10 43.81 D
T3 34.40- 23.80
392.45 2944.21 A B C D
0.138 0.138 0.138 0.138
3.261 3.261 3.261 3.261
6 1
24.366 24.366 24.366 24.366
468.35 44.18 D
T4 23.80- 12.50
417.42 3713.30 A B C D
0.137 0.137 0.137 0.137
3.268 3.268 3.268 3.268
6 1
28.628 28.628 28.628 28.628
500.04 44.25 D
T5 12.50-0.00 459.41 4404.06 A B C D
0.131 0.131 0.131 0.131
3.295 3.295 3.295 3.295
5 1
33.756 33.756 33.756 33.756
575.68 46.05 D
Sum Weight: 2011.19 16236.01 OTM 64755.55
2411.15
Tower Forces - With Ice - Wind 45 To Face a c
Face
T1 54.40- 44.40
371.15 2505.07 A B C D
0.154 0.154 0.154 0.154
3.186 3.186 3.186 3.186
7 1.116 1.116 1.116 1.116
1.116 1.116 1.116 1.116
22.954 22.954 22.954 22.954
471.64 47.16 D
T2 44.40- 34.40
370.77 2669.37 A B C D
0.145 0.145 0.145 0.145
3.228 3.228 3.228 3.228
6 1.109 1.109 1.109 1.109
1.109 1.109 1.109 1.109
24.048 24.048 24.048 24.048
479.53 47.95 D
T3 34.40- 23.80
392.45 2944.21 A B C D
0.138 0.138 0.138 0.138
3.261 3.261 3.261 3.261
6 1.104 1.104 1.104 1.104
1.104 1.104 1.104 1.104
26.891 26.891 26.891 26.891
510.87 48.20 D
T4 23.80- 12.50
417.42 3713.30 A B C D
0.137 0.137 0.137 0.137
3.268 3.268 3.268 3.268
6 1.103 1.103 1.103 1.103
1.103 1.103 1.103 1.103
31.565 31.565 31.565 31.565
545.52 48.28 D
T5 12.50-0.00 459.41 4404.06 A B C D
0.131 0.131 0.131 0.131
3.295 3.295 3.295 3.295
5 1.098 1.098 1.098 1.098
1.098 1.098 1.098 1.098
37.077 37.077 37.077 37.077
626.32 50.11 D
Sum Weight: 2011.19 16236.01 OTM 70874.47
2633.89
Project
STRUCTURAL ANALYSIS
For
USFS
Tower Forces - Service - Wind Normal To Face a c
Face
T1 54.40- 44.40
350.00 1981.66 A B C D
0.129 0.129 0.129 0.129
3.304 3.304 3.304 3.304
12 1
18.521 18.521 18.521 18.521
712.56 71.26 D
T2 44.40- 34.40
350.00 2122.01 A B C D
0.122 0.122 0.122 0.122
3.339 3.339 3.339 3.339
11 1
19.562 19.562 19.562 19.562
727.53 72.75 D
T3 34.40- 23.80
371.00 2353.75 A B C D
0.118 0.118 0.118 0.118
3.362 3.362 3.362 3.362
11 1
22.128 22.128 22.128 22.128
780.11 73.60 D
T4 23.80- 12.50
395.50 3048.32 A B C D
0.119 0.119 0.119 0.119
3.357 3.357 3.357 3.357
10 1
26.302 26.302 26.302 26.302
839.02 74.25 D
T5 12.50-0.00 437.50 3680.07 A B C D
0.116 0.116 0.116 0.116
3.368 3.368 3.368 3.368
10 1
31.432 31.432 31.432 31.432
973.95 77.92 D
Sum Weight: 1904.00 13185.81 OTM 107881.86
4033.17
Tower Forces - Service - Wind 45 To Face a c
Face
T1 54.40- 44.40
350.00 1981.66 A B C D
0.129 0.129 0.129 0.129
3.304 3.304 3.304 3.304
12 1.097 1.097 1.097 1.097
1.097 1.097 1.097 1.097
20.317 20.317 20.317 20.317
771.98 77.20 D
T2 44.40- 34.40
350.00 2122.01 A B C D
0.122 0.122 0.122 0.122
3.339 3.339 3.339 3.339
11 1.092 1.092 1.092 1.092
1.092 1.092 1.092 1.092
21.356 21.356 21.356 21.356
785.37 78.54 D
T3 34.40- 23.80
371.00 2353.75 A B C D
0.118 0.118 0.118 0.118
3.362 3.362 3.362 3.362
11 1.088 1.088 1.088 1.088
1.088 1.088 1.088 1.088
24.079 24.079 24.079 24.079
840.31 79.27 D
T4 23.80- 12.50
395.50 3048.32 A B C D
0.119 0.119 0.119 0.119
3.357 3.357 3.357 3.357
10 1.089 1.089 1.089 1.089
1.089 1.089 1.089 1.089
28.642 28.642 28.642 28.642
905.18 80.10 D
T5 12.50-0.00 437.50 3680.07 A B C D
0.116 0.116 0.116 0.116
3.368 3.368 3.368 3.368
10 1.087 1.087 1.087 1.087
1.087 1.087 1.087 1.087
34.172 34.172 34.172 34.172
1049.90 83.99 D
Sum Weight: 1904.00 13185.81 OTM 116523.45 4352.74
Project
STRUCTURAL ANALYSIS
For
USFS
a c
Face
Force Totals
Load Case
Vertical Forces
Sum of Forces
X lb
Sum of Forces
Z lb
Sum of Overturning Moments, Mx lb-ft
Sum of Overturning Moments, Mz
Sum of Torques
Leg Weight 1336.89 Bracing Weight 11848.92 Total Member Self-Weight 13185.81 0.00 4341.64 Total Weight 43985.81 0.00 4341.64 Wind 0 deg - No Ice 0.00 -17896.98 -654755.74 4341.64 -3378.01 Wind 45 deg - No Ice 13347.10 -13347.10 -481695.72 -477354.08 -2388.61 Wind 90 deg - No Ice 17896.98 0.00 0.00 -650414.10 0.00 Member Ice 3050.19 Total Weight Ice 50085.49 0.00 4566.57 Wind 0 deg - Ice 0.00 -3473.97 -126947.50 4566.57 -654.90 Wind 45 deg - Ice 2613.97 -2613.97 -94092.16 -89525.60 -463.09 Wind 90 deg - Ice 3473.97 0.00 0.00 -122380.93 0.00 Total Weight 43985.81 0.00 4341.64 Wind 0 deg - Service 0.00 -5843.91 -213797.79 0.00 -1103.02 Wind 45 deg - Service 4358.24 -4358.24 -157288.40 -157288.40 -779.96 Wind 90 deg - Service 5843.91 0.00 0.00 -213797.79 0.00
Load Combinations
Comb.
No.
Description
1 Dead Only 2 1.2 Dead+1.0 Wind 0 deg - No Ice 3 0.9 Dead+1.0 Wind 0 deg - No Ice 4 1.2 Dead+1.0 Wind 45 deg - No Ice 5 0.9 Dead+1.0 Wind 45 deg - No Ice 6 1.2 Dead+1.0 Wind 90 deg - No Ice 7 0.9 Dead+1.0 Wind 90 deg - No Ice 8 1.2 Dead+1.0 Ice+1.0 Temp 9 1.2 Dead+1.0 Wind 0 deg+1.0 Ice+1.0 Temp 10 1.2 Dead+1.0 Wind 45 deg+1.0 Ice+1.0 Temp 11 1.2 Dead+1.0 Wind 90 deg+1.0 Ice+1.0 Temp 12 Dead+Wind 0 deg - Service 13 Dead+Wind 45 deg - Service 14 Dead+Wind 90 deg - Service
Project
STRUCTURAL ANALYSIS
For
USFS
Maximum Member Forces
Elevation ft Component
Type Condition Gov.
Load
Axial
Major Axis Moment lb-ft
Minor Axis Moment lb-ft T1 54.4 - 44.4 Leg Max Tension 1 0.00 0.00 0.00
Max. Compression 9 -10130.92 37.11 26.55 Max. Mx 2 -8240.62 -179.69 0.55 Max. My 6 -8240.65 11.80 -177.11 Max. Vy 2 698.82 0.01 0.00 Max. Vx 6 691.59 -0.00 0.01 Diagonal Max Tension 3 2330.16 13.12 14.85 Max. Compression 2 -2584.72 0.00 0.00 Max. Mx 10 191.05 31.24 28.05 Max. My 11 -621.94 8.08 -29.79 Max. Vy 10 18.13 0.00 0.00 Max. Vx 11 -7.08 0.00 0.00 Top Girt Max Tension 3 805.33 -138.65 -47.03 Max. Compression 2 -2163.89 -184.75 -63.33 Max. Mx 9 -851.65 -209.81 -76.73 Max. My 11 -837.28 -206.66 -77.38 Max. Vy 9 -84.56 -209.81 -76.73 Max. Vx 9 -16.02 0.00 0.00 Redund Horz 1
Bracing Max Tension 3 94.88 0.00 0.00
Max. Compression 2 -144.37 0.00 0.00 Max. Mx 9 -29.19 15.21 0.00 Max. My 9 -9.15 0.00 -1.28 Max. Vy 9 -18.26 0.00 0.00 Max. Vx 9 1.54 0.00 0.00 Redund Diag 1
Bracing Max Tension 2 201.09 0.00 0.00
Max. Compression 3 -59.28 0.00 0.00 Max. Mx 9 106.00 25.41 0.00 Max. My 9 123.01 0.00 4.25 Max. Vy 9 -17.52 0.00 0.00 Max. Vx 9 2.93 0.00 0.00
T2 44.4 - 34.4 Leg Max Tension 1 0.00 0.00 0.00 Max. Compression 4 -13505.51 31.82 33.14 Max. Mx 4 -9707.04 106.24 -19.98 Max. My 4 -9732.76 -21.01 107.44 Max. Vy 6 -53.48 92.54 6.24 Max. Vx 2 -63.71 5.53 93.42 Diagonal Max Tension 3 2711.75 0.00 0.00 Max. Compression 2 -3038.11 0.00 0.00 Max. Mx 9 -212.49 31.72 31.59 Max. My 9 -761.46 2.28 -33.07 Max. Vy 9 18.84 0.00 0.00 Max. Vx 9 -7.48 0.00 0.00 Horizontal Max Tension 3 1781.96 -141.16 -56.79 Max. Compression 2 -1795.34 -188.23 -75.74 Max. Mx 9 -0.52 -219.47 -91.80 Max. My 9 -7.97 -209.40 -92.09 Max. Vy 9 -88.85 -219.47 -91.80 Max. Vx 11 17.29 0.00 0.00 Redund Horz 1
Bracing Max Tension 2 83.05 0.00 0.00
Max. Compression 3 -61.85 0.00 0.00 Max. Mx 9 15.38 19.24 0.00 Max. My 9 25.87 0.00 -1.62
Project
STRUCTURAL ANALYSIS
For
USFS
No.
Elevation ft
Component Type
Condition Gov.
Load
Moment lb-ft
Minor Axis Moment lb-ft Max. Vy 9 -20.50 0.00 0.00 Max. Vx 9 1.73 0.00 0.00 Redund Diag 1
Bracing Max Tension 2 132.05 0.00 0.00
Max. Compression 3 -38.13 0.00 0.00 Max. Mx 9 82.83 30.11 0.00 Max. My 9 93.50 0.00 4.56 Max. Vy 9 -19.99 0.00 0.00 Max. Vx 9 3.03 0.00 0.00
T3 34.4 - 23.8 Leg Max Tension 1 0.00 0.00 0.00 Max. Compression 4 -17274.17 -87.20 -103.47 Max. Mx 4 -10619.42 162.01 -47.94 Max. My 4 -10402.29 -45.90 157.73 Max. Vy 4 -80.78 162.01 -47.94 Max. Vx 6 -70.69 -11.81 127.98 Diagonal Max Tension 3 3234.46 -5.59 17.12 Max. Compression 2 -3609.53 0.00 0.00 Max. Mx 9 -218.93 31.93 36.88 Max. My 2 -3572.71 -2.22 -42.89 Max. Vy 9 -21.74 -11.59 37.00 Max. Vx 11 -8.18 0.00 0.00 Horizontal Max Tension 2 2184.47 -190.53 -92.36 Max. Compression 3 -2168.26 -142.89 -69.29 Max. Mx 9 18.99 -225.47 -111.32 Max. My 9 8.91 -212.21 -111.60 Max. Vy 9 -93.03 -225.47 -111.32 Max. Vx 9 18.93 0.00 0.00 Redund Horz 1
Bracing Max Tension 4 110.05 0.00 0.00
Max. Compression 5 -68.55 0.00 0.00 Max. Mx 10 31.64 23.69 0.00 Max. My 9 33.76 0.00 -2.00 Max. Vy 10 -22.69 0.00 0.00 Max. Vx 9 1.91 0.00 0.00 Redund Diag 1
Bracing Max Tension 4 147.69 0.00 0.00
Max. Compression 5 -50.00 0.00 0.00 Max. Mx 9 91.52 36.17 0.00 Max. My 9 104.51 0.00 5.27 Max. Vy 9 22.27 0.00 0.00 Max. Vx 9 -3.25 0.00 0.00
T4 23.8 - 12.5 Leg Max Tension 5 1967.89 15.40 32.52 Max. Compression 4 -21950.87 71.16 68.76 Max. Mx 4 -11406.29 175.26 -52.54 Max. My 4 -11431.98 -51.19 171.10 Max. Vy 4 -74.42 175.26 -52.54 Max. Vx 4 -84.94 -51.19 171.10 Diagonal Max Tension 3 3749.37 0.00 0.00 Max. Compression 2 -4200.40 0.00 0.00 Max. Mx 4 -3146.46 66.77 52.32 Max. My 9 -1041.29 -10.33 -56.07 Max. Vy 10 -36.32 -19.33 53.02 Max. Vx 11 11.64 0.00 0.00 Horizontal Max Tension 3 2568.78 -152.92 -103.39 Max. Compression 2 -2587.30 -203.91 -137.87 Max. Mx 2 19.20 -243.39 -137.03 Max. My 11 -10.52 -227.81 -162.01 Max. Vy 9 -98.89 -242.94 -161.77 Max. Vx 11 23.65 0.00 0.00
Project
STRUCTURAL ANALYSIS
For
USFS
No.
Elevation ft
Component Type
Condition Gov.
Load
Moment lb-ft
Minor Axis Moment lb-ft Redund Horz 1
Bracing Max Tension 4 113.12 0.00 0.00
Max. Compression 5 -74.22 0.00 0.00 Max. Mx 10 23.88 28.82 0.00 Max. My 9 33.44 0.00 -2.43 Max. Vy 10 -24.94 0.00 0.00 Max. Vx 9 2.10 0.00 0.00 Redund Diag 1
Bracing Max Tension 4 185.49 0.00 0.00
Max. Compression 5 -37.47 0.00 0.00 Max. Mx 9 123.04 43.20 0.00 Max. My 9 140.02 0.00 6.12 Max. Vy 9 -24.60 0.00 0.00 Max. Vx 9 -3.49 0.00 0.00
T5 12.5 - 0 Leg Max Tension 5 5393.30 37.67 34.64 Max. Compression 4 -27171.86 -126.75 -147.21 Max. Mx 4 -12409.25 175.24 -52.63 Max. My 4 -12412.68 -51.23 171.07 Max. Vy 4 77.71 175.24 -52.63 Max. Vx 4 75.80 -126.75 -147.21 Diagonal Max Tension 3 4375.46 -41.44 41.15 Max. Compression 2 -4933.97 0.00 0.00 Max. Mx 4 -3651.80 116.88 69.67 Max. My 11 -1198.83 -0.86 -74.68 Max. Vy 4 -46.66 -76.19 -56.76 Max. Vx 11 14.43 0.00 0.00 Horizontal Max Tension 3 2992.58 -207.20 -141.51 Max. Compression 3 -2999.98 -207.20 -141.51 Max. Mx 2 28.81 -348.51 -187.80 Max. My 10 438.07 -211.50 -218.91 Max. Vy 9 108.91 -235.43 -218.84 Max. Vx 10 28.72 0.00 0.00 Redund Horz 1
Bracing Max Tension 3 114.34 0.00 0.00
Max. Compression 3 -115.56 0.00 0.00 Max. Mx 9 17.80 34.51 0.00 Max. My 10 29.72 0.00 -2.91 Max. Vy 9 -27.08 0.00 0.00 Max. Vx 10 -2.28 0.00 0.00 Redund Diag 1
Bracing Max Tension 4 251.09 0.00 0.00
Max. Compression 5 -30.06 0.00 0.00 Max. Mx 10 151.85 51.86 0.00 Max. My 9 182.98 0.00 7.37 Max. Vy 10 -26.73 0.00 0.00 Max. Vx 9 -3.80 0.00 0.00
Maximum Reactions
Location Condition Gov.
Comb.
Vertical lb
Horizontal, X lb
Horizontal, Z lb
Leg D Max. Vert 8 14841.51 1424.37 -1428.94 Max. Hx 8 14841.51 1424.37 -1428.94 Max. Hz 3 -3434.19 -151.63 3553.86 Min. Vert 5 -9707.44 -3197.78 3247.62
Project
STRUCTURAL ANALYSIS
For
USFS
Location Condition Gov.
Load
Comb.
Vertical lb
Horizontal, X lb
Horizontal, Z lb
Min. Hx 7 -3434.13 -3519.59 185.92 Min. Hz 8 14841.51 1424.37 -1428.94
Leg C Max. Vert 6 26502.31 -5747.54 -2415.94 Max. Hx 3 -3607.84 226.71 3485.30 Max. Hz 3 -3607.84 226.71 3485.30 Min. Vert 3 -3607.84 226.71 3485.30 Min. Hx 6 26502.31 -5747.54 -2415.94 Min. Hz 6 26502.31 -5747.54 -2415.94
Leg B Max. Vert 4 32766.16 -5474.77 5417.35 Max. Hx 1 10899.91 -1061.79 1058.17 Max. Hz 2 26502.24 -2457.84 5705.68 Min. Vert 1 10899.91 -1061.79 1058.17 Min. Hx 6 26502.30 -5747.54 2415.94 Min. Hz 1 10899.91 -1061.79 1058.17
Leg A Max. Vert 2 26734.10 2382.75 5789.42 Max. Hx 2 26734.10 2382.75 5789.42 Max. Hz 2 26734.10 2382.75 5789.42 Min. Vert 7 -3434.12 -3519.59 -185.92 Min. Hx 7 -3434.12 -3519.59 -185.92 Min. Hz 7 -3434.12 -3519.59 -185.92
Tower Mast Reaction Summary
Combination
Vertical
Shearx
Shearz
Overturning Moment, Mx lb-ft
Overturning Moment, Mz
Torque
Dead Only 43985.81 0.00 -0.00 -0.00 4344.32 0.00
1.2 Dead+1.0 Wind 0 deg - No
Ice
52782.97 -0.00 -17896.98 -604009.23 5213.98 -3378.57
0.9 Dead+1.0 Wind 0 deg - No
Ice
39587.23 -0.00 -17896.98 -603802.09 3909.73 -3378.41
1.2 Dead+1.0 Wind 45 deg - No
Ice
52782.97 13347.10 -13347.10 -443070.75 -437856.74 -2389.03
0.9 Dead+1.0 Wind 45 deg - No
Ice
39587.23 13347.10 -13347.10 -442916.65 -439004.94 -2389.29
1.2 Dead+1.0 Wind 90 deg - No
Ice
52782.97 17896.98 -0.00 0.00 -598795.38 -0.01
0.9 Dead+1.0 Wind 90 deg - No
Ice
39587.23 17896.98 -0.00 0.00 -599892.05 -0.01
1.2 Dead+1.0 Ice+1.0 Temp 58882.65 0.00 -0.00 0.00 5438.06 0.00
1.2 Dead+1.0 Wind 0 deg+1.0
Ice+1.0 Temp
58882.65 -0.00 -3473.97 -116968.18 5438.06 -654.90
1.2 Dead+1.0 Wind 45 deg+1.0
Ice+1.0 Temp
58882.65 2613.97 -2613.97 -86414.06 -80976.01 -463.09
1.2 Dead+1.0 Wind 90 deg+1.0
Ice+1.0 Temp
58882.65 3473.97 -0.00 -0.00 -111530.12 0.00
Dead+Wind 0 deg - Service 43985.81 -0.00 -5843.91 -197182.35 4344.34 -1103.17 Dead+Wind 45 deg - Service 43985.81 4358.24 -4358.24 -144646.13 -140302.15 -779.96 Dead+Wind 90 deg - Service 43985.81 5843.91 -0.00 -0.00 -192838.02 -0.00
Project
STRUCTURAL ANALYSIS
For
USFS
Solution Summary
Sum of Applied Forces Sum of Reactions % Error PX lb
PY
lb
PZ
lb
PX
lb
PY
lb
PZ
lb
1 0.00 -43985.81 0.00 -0.00 43985.81 0.00 0.000% 2 0.00 -52782.97 -17896.98 0.00 52782.97 17896.98 0.000% 3 0.00 -39587.23 -17896.98 0.00 39587.23 17896.98 0.000% 4 13347.10 -52782.97 -13347.10 -13347.10 52782.97 13347.10 0.000% 5 13347.10 -39587.23 -13347.10 -13347.10 39587.23 13347.10 0.000% 6 17896.98 -52782.97 0.00 -17896.98 52782.97 0.00 0.000% 7 17896.98 -39587.23 0.00 -17896.98 39587.23 0.00 0.000% 8 0.00 -58882.65 0.00 -0.00 58882.65 0.00 0.000% 9 0.00 -58882.65 -3473.97 0.00 58882.65 3473.97 0.000% 10 2613.97 -58882.65 -2613.97 -2613.97 58882.65 2613.97 0.000% 11 3473.97 -58882.65 0.00 -3473.97 58882.65 0.00 0.000% 12 0.00 -43985.81 -5843.91 0.00 43985.81 5843.91 0.000% 13 4358.24 -43985.81 -4358.24 -4358.24 43985.81 4358.24 0.000% 14 5843.91 -43985.81 0.00 -5843.91 43985.81 0.00 0.000%
Non-Linear Convergence Results
Combination
Converged? Number of Cycles
Displacement Tolerance
Force Tolerance
1 Yes 4 0.00000001 0.00000001 2 Yes 4 0.00000001 0.00000001 3 Yes 4 0.00000001 0.00000001 4 Yes 4 0.00000001 0.00001842 5 Yes 4 0.00000001 0.00000001 6 Yes 4 0.00000001 0.00000001 7 Yes 4 0.00000001 0.00000001 8 Yes 4 0.00000001 0.00000001 9 Yes 4 0.00000001 0.00000001 10 Yes 4 0.00000001 0.00000001 11 Yes 4 0.00000001 0.00000001 12 Yes 4 0.00000001 0.00000001 13 Yes 4 0.00000001 0.00000001 14 Yes 4 0.00000001 0.00000001
Maximum Tower Deflections - Service Wind
Horz.
Deflection in
Gov.
Load
Comb.
Tilt
Twist
T1 54.4 - 44.4 0.093 13 0.0103 0.0002 T2 44.4 - 34.4 0.068 13 0.0101 0.0001 T3 34.4 - 23.8 0.044 13 0.0088 0.0001 T4 23.8 - 12.5 0.022 13 0.0068 0.0000 T5 12.5 - 0 0.006 13 0.0040 0.0000
Project
STRUCTURAL ANALYSIS
For
USFS
Critical Deflections and Radius of Curvature - Service Wind
Appurtenance Gov.
Load
Deflection
Tilt
Twist
Radius of Curvature ft
58.60 Cabin 13'x13' 13 0.093 0.0103 0.0002 Inf
54.20 platform full steel 24'x24' 13 0.093 0.0103 0.0002 Inf
54.00 Mounting Pipe - 1.75'' x 3' 13 0.092 0.0103 0.0002 Inf
Maximum Tower Deflections - Design Wind
Horz.
Deflection in
Gov.
Load
Comb.
Tilt
Twist
T1 54.4 - 44.4 0.287 4 0.0319 0.0005 T2 44.4 - 34.4 0.208 4 0.0311 0.0003 T3 34.4 - 23.8 0.135 4 0.0271 0.0002 T4 23.8 - 12.5 0.067 4 0.0209 0.0001 T5 12.5 - 0 0.020 4 0.0124 0.0001
Critical Deflections and Radius of Curvature - Design Wind
Appurtenance Gov.
Load
Deflection
Tilt
Twist
Radius of Curvature ft
58.60 Cabin 13'x13' 4 0.287 0.0319 0.0005 343860
54.20 platform full steel 24'x24' 4 0.286 0.0319 0.0005 343860
54.00 Mounting Pipe - 1.75'' x 3' 4 0.284 0.0319 0.0005 343860
Bolt Design Data
Component Type
Bolt
Of
Bolts
Maximum Load per Bolt lb
Allowable Load per Bolt lb
Ratio Load
Allowable
Allowable Ratio
Criteria
T1 54.4 Leg A325N 0.7500 12 1688.49 19880.40 0.085 1 Bolt SS
Diagonal A325N 0.7500 3 776.72 16757.80 0.046 1 Member Block Shear
Redund Horz 1 Bracing
A325N 0.7500 1 160.92 23925.00 0.007 1 Member Block Shear
Redund Diag 1 Bracing
A325N 0.7500 1 201.09 23925.00 0.008 1 Member Block Shear
T2 44.4 Leg A325N 0.7500 12 2250.92 19880.40 0.113 1 Bolt SS
Diagonal A325N 0.7500 3 903.92 16757.80 0.054 1 Member Block Shear
Horizontal A325N 0.7500 3 593.99 25390.60 0.023 1 Member Block Shear
Project
STRUCTURAL ANALYSIS
For
USFS
Component Type
Bolt
Of
Bolts
Maximum Load per Bolt lb
Allowable Load per Bolt lb
Ratio Load
Allowable
Allowable Ratio
Criteria
Redund Horz 1 Bracing
A325N 0.7500 1 214.53 23925.00 0.009 1 Member Block Shear
Redund Diag 1 Bracing
A325N 0.7500 1 172.10 23925.00 0.007 1 Member Block Shear
T3 34.4 Leg A325N 0.7500 12 2879.03…
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