C05 Attachment 17 031005L050501-Barillas Lookout-20230906-SAR-V9.pdf

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Barillas Peak & Encino Vista Lookout Tower Restoration, Santa Fe NF
Solicitation number
127EAX26Q0069
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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

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STRUCTURAL ANALYSIS

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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

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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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