Concourse B Preconditioned Air Equipment Replacement Denver
Transcription
Concourse B Preconditioned Air Equipment Replacement Denver
Concourse B Preconditioned Air Equipment Replacement for Denver International Airport Design Analysis Report Issued for Construction August 29, 2014 Prepared by: B&McD Project: 65967 Concourse B Preconditioned Air Equipment Replacement for Denver International Airport Design Analysis Report Issued for Construction August 29, 2014 Prepared by: Burns & McDonnell Engineering Co. B&McD Project: 65967 August 29, 2014 Mr. Lee Walinchus, PE Project Manager DIA, Planning and Development Division AOB, 7th Floor 8500 Pena Blvd. Denver, CO 80249-6340 Concourse B – PCA Equipment Replacement IFC Submittal - B&McD Project: 65967 Dear Mr. Walinchus, We have completed the design documents for the Concourse B PCA Equipment Replacement project, which will replace the existing point of use (POU) pre-condition air system with in-kind but larger POU units delivering air to aircraft parked at each gate (except the Regional Jet Concourses) of Concourse B. We have prepared this submittal with the intent of presenting solutions to issues identified in course of our design efforts and to provide solutions to any new issues associated with the project. The results of this effort are summarized in this report. The report includes the results of our analysis, our opinion of probable cost and a Design Analysis Report. We trust this submittal meets with your intentions and we thank you for giving us this opportunity to be of service to the City Sincerely, Aurom Mahobian, PE Project Manager BURNS & McDONNELL 9785 Maroon Circle • Suite 400 • Centennial, CO 80112-2692 Tel: 303 721-9292 • Fax: 303 721-0563 • www.burnsmcd.com Table of Contents 1.0 A. B. C. D. E. F. G. H. I. J. FORWARD ...........................................................................................................2 Certification of Compliance ...................................................................................2 Program Statement...............................................................................................2 Diagrams ..............................................................................................................2 Interviews and Meetings .......................................................................................2 Description of Services .........................................................................................2 Limits of Consultant Work .....................................................................................3 Project Limits ........................................................................................................3 Design and Construction Schedule ....................................................................... 3 Summary of Actions..............................................................................................4 Bid and Procurement Packaging........................................................................... 4 2.0 A. B. C. D. E. F. G. H. I. J. K. L. M. N. O. P. Q. R. S. T. U. V. DESIGN REQUIREMENTS ..................................................................................5 General Description ..............................................................................................5 Design Criteria ......................................................................................................5 Design Alternatives ...............................................................................................3 Planning Study .....................................................................................................3 Statistical Summary ..............................................................................................4 Major Components ...............................................................................................4 Code Analysis.......................................................................................................5 Life Safety, Security and Communications Systems ............................................. 5 Systems Load Requirements ...............................................................................5 Design Alternatives ...............................................................................................5 Costs and Budgets ...............................................................................................5 Value Engineering ................................................................................................5 Operations and Maintenance Criteria (O&M) ..................................................... 5 List of Equipment and Long Lead Items ................................................................ 5 Critical Construction/RFP Activities ....................................................................... 5 Independent Testing Laboratory Report................................................................ 5 Contract Data Submittal Report (CSDR) ............................................................... 5 Cut Sheets............................................................................................................5 Soils Report ..........................................................................................................5 FM Global Property Loss Prevention .................................................................... 6 DIA Environmental Review ...................................................................................6 Leadership in Energy & Environmental Design (LEED) ........................................ 6 3.0 A. B. C. CALCULATIONS .................................................................................................7 Structural Calculations ..........................................................................................7 Mechanical Calculations .......................................................................................7 Electrical Calculations...........................................................................................7 4.0 APPENDIX ...........................................................................................................8 TOC DESIGN ANALYSIS REPORT CONCOURSE B – PRECONDITIONED AIR EQUIPMENT REPLACEMENT 1.0 FORWARD A. Certification of Compliance To the best of our knowledge and understanding all drawings that Burns & McDonnell has prepared as part of this project conform to DIA design standards. B. Program Statement Replace existing Preconditioned Air (PCA) units with new units at each gate in Concourse B, not including the Regional Jet Facility. The new units were initially intended to be glycol type units served from a new central plant. However, direction has been provided by DIA staff that the new units are to be selfcontained direct expansion (DX) units, which are similar to the existing units and are referred to as Point of Use (POU) units. C. Diagrams Logic diagrams, decision matrices or space planning, functional diagrams were not prepared or are needed for this project. D. Interviews and Meetings Several project meetings have taken place on this project. Additionally, there have been a significant number of phone conversations, electronic communication and site visits to discuss issues of plant capacity, gate operations, physical limitations, system operation and general construction sequencing issues. Other meetings, site visits and discussions will continue to take place during design to review and resolve issues. The significant issues that this project faces that have surfaced during interviews and meetings include: 1) Adequacy of the power supply. 2) Attachment of the new, larger units to the passenger boarding bridges (PBB). 3) Scheduling of allowable gates outages. E. Description of Services 1. Initial Project Scope of Work The Initial Scope of Work, based on the original Authorization, required that the design team address the following project elements: a. Determine the required capacity of the new PCA Central Plant. b. Determine a location for the plant. c. Develop a general arrangement of the equipment that will be located in the new plant. 2. Revised Project Scope of Work After the Schematic Design submittal, DIA requested an Interim Report be prepared, the intent of which was to evaluate options for the replacement of the units. Options for the replacement included the replacement of the units Page 2 with units of similar type (DX cooling units) referred to as Point of Use (POU) units as well as the glycol based central plant system. Although the recommendation in the Interim Report was to continue on the course of the glycol based, central plant system, DIA staff provided direction to proceed on the basis that the existing POU units will be replaced with DX POU units but of a larger capacity than indicated in the report. The revised Scope of Work during the Schematic Phase was to provide 45 ton units at each gate, except for gates that serve wide body aircraft which are to receive 60 ton units. The scope for this Final Design effort was identical to the scope developed at the end of the Schematic Design Phase. However, the preparation of Technical Memorandum 1 and resultant direction from DIA resulted in a modification of the scope to change to 90 ton units at the wide body gates. After the 60% Submittal, the scope was revised once again to eliminate the following gates from the project: B30/B32, B34/B36, B38/B40, B39, and B42A/B42B. These were the gates intended to receive the 90 ton units. The project was issued for IFC, but placed on hold due to funding deficiencies. The project scope has now been revised again to install 90 ton units at the gates where B787 aircraft will park. The existing 60 ton units that were installed during the Japan Services project are not maintaining the cooling loads properly and UAL has asked that they be upsized. The 100% Resubmittal has revised the scope to include gates B30/32B, B34/B36B, B38/B40B, and B42A/B42B. For these “double” gates that have an A and a B bridge, the B gates will receive new 90 ton units, and the existing 60 ton unit from the B gates will be preserved and reinstalled at gates B52, B53, B55, and B60. The existing 60 ton units at the A gates will remain. The issues for this revised Scope of Work include the following: a. Determine the effect of the larger capacity units on the electrical system. b. Develop the preferred location of the new air handling units on the PBB. F. Limits of Consultant Work The design efforts of this project are limited to the designs needed to install equipment, provide additional power to the new units, remove and replace air handling units on the passenger boarding bridges. G. Project Limits The construction activities associated with this project will have an effect on the ramp operations of Concourse B. Construction will occur on the ramp adjacent to the building. H. Design and Construction Schedule The proposed schedule is included in Appendix D of this report. Page 3 I. Summary of Actions We do not anticipate need for any special or unusual permitting. However, we do anticipate disruption of ramp aircraft operations and as a result coordination with DIA Operations will be necessary. J. Bid and Procurement Packaging Special bid packaging and procurement could be considered for this project. One approach would be to prepare a separate bid package for the air handling units and a separate bid package for the installation of the new units. However, then DIA would have to take responsibility for receipt and storage of the units. The preferred approach is to have the installing contractor take on responsibility for coordinating with the unit supplier for delivery and necessary and unique installation items. Page 4 2.0 DESIGN REQUIREMENTS A. General Description The purpose of this project is to install replacement air handling units at all of the Passenger Boarding Bridges (PBB) on Concourse B, not including those in the Regional Jet Facility and gates B19, B30/B32A, B34/B36A, B38/B40A, B39 and B42A/B42B. The new units will be similar in operation and components, but larger in capacity than the existing units. At gates B30/32A, B34/B36A, B38/B40A and B42A/B42B, the existing 60 ton units from the A gates will remain, and the existing 60 ton units on the B gates will be removed (to be used at other gates) and replaced with 90 ton units. Gates B30/32, B34/36, B38/40, and B42 are all “double gates” meaning that they are capable of supporting a B747 aircraft. Only a 747 will require the use of both bridges at the same time. Each PBB on these gates is currently equipped with two 60 ton PCA units. This is effective for every aircraft that uses these gates except for the B787 as this aircraft requires a load that is greater than the 60 ton unit can provide. Unlike the B747, the 787 has only one PCA connection, making it impossible to use both 60 ton units at these gates at the same time. As such the double gates must be equipped with one 90 ton unit each. The 90 ton unit must have 2 PCA outlets so that a 747 can be properly cooled. When a 787 is using one of these gates, however, the 90 ton unit must divert all of its output to one hose. Because each outlet is supplied by the same blower, diverting the air to one hose will cause a larger pressure drop. The 90 ton unit will be equipped with 4 settings for regional jets, narrow-body, wide-body and jumbo aircraft. B. Design Criteria The following criteria will affect the design of the replacement of the existing point of use (POU) PCA system with similar, larger capacity units: 1. Unit Capacity Increase: The existing POU units at the existing PBB will be replaced with larger capacity units in the following schedule: Gate Number B15 B16 B17 B18 B20 B21 B22 B23 B24 B25 Existing Unit (tons) 20 20 20 20 20 20 20 20 20 20 Page 5 New Unit (tons) 45 60 45 45 45 60 45 45 45 45 B26 B27 B28 B29 B30/B32A B30/B32B B31 B33 B34/B36A B34/B36B B35 (Non-Functional) B37 B38/B40A B38/B40B B41 B42A B42B B43 B44 B45 B46 B47 B48 B49 B50 (Non-Functional) B51 (Non-Functional) B52 B53 B54 B55 B56 B58 B60 20 20 20 20 60 60 20 20 60 60 20 20 60 60 20 60 60 20 20 20 20 20 20 20 20 20 20 20 20 20 20 20 20 45 45 45 45 N/A 90 45 45 N/A 90 45 45 N/A 90 60 N/A 90 60 60 45 45 45 45 45 45 45 60 60 45 60 60 45 60 Note that the new 60 ton units at gates B52, B53, B55, and B60 are the relocated units from gates B30/32B, B34/B36B, B38/B40B, and B42B. 2. Electrical System Effects: The existing electrical distribution for the Preconditioned Air (PCA) units in Concourse B includes a local 480VAC panelboard (GXXAH) at each gate, with a 480V-208Y/120VAC transformer feeding an existing 208Y/120VAC panelboard. The existing 480VAC gate panelboards are fed out of existing gate 1600 Amp distribution panelboards located in the core electrical rooms. Page 6 The 1600 Amp distribution panelboards are fed from the existing baggage distribution main switchgear via a fully rated 1600 Amp low voltage power circuit breaker. The electrical scope of work for the PCA upgrade includes demolishing the existing units including the raceway, cable and overcurrent protection in the local gate 480VAC panelboard. The installation of the new PCA units includes providing and installing new overcurrent protection in the local gate 480VAC panelboard with new cable and raceway from the existing panelboard to the new unit. The new units to be installed shall be three different sizes: • The 45 ton units shall have a new 150 Amp 3 pole circuit breaker installed in the panelboard with (3 #1/0 & #6G) 2”C routed to the new unit. • The new 60 ton units shall have a new 200 Amp 3 pole circuit breaker installed in the panelboard with (3 #3/0 & #6G) 2”C routed to the new unit. • The new 90 ton units shall have a new 300 Amp 3 pole circuit breaker installed in the panelboard with (3 #350 & #4G) 3”C routed to the new unit. Existing raceway shall be reused if space allows. The new PCAs will be powered from the existing GXXAH panels. These panels will feed either an existing control panel or new 3 pole disconnect. A 3 pole breaker inside the control panel will be replaced. The control panel (MCP) shall feed the PCA unit. The PCA unit will feed a new controls station located next to the unit. The following gates shall need new control panels (MCP): B21, B33, B45, B46, B47, B48, B49, B50, B52, B53, B54, B55, B56, B60. The new PCA upgrade will increase the existing load, therefore when at full load, the system will be at maximum capacity at each gate panel and at each of the existing 1600 Amp distribution panelboards. The following design assumptions have been made: • Gates with both 60 and 90 ton units cannot run at the same time. Panelboards that power both 60 ton and a 90 ton units, demand factors have been set to 0 for the 60 ton and 0.85 for 90 ton unit. • All subpanels are MLO, therefore the 1600A breaker in SWBD feeding the subpanel can be loaded to 100% • 3,000A main circuit breakers in SWBDs are 100% rated. 3. Structural Evaluation of Existing Passenger Boarding Bridges: A Structural analysis has been performed to determine if the existing Passenger Boarding Bridges can support the new, larger POU units at each gate. Preliminary structural analysis calculations of the existing jet bridge framing indicates that no retrofits or supplemental support will be needed other than the manufacturer's standard mounting assemblies. This analysis is included in section 3.0 of this report. 4. Condensate Disposal: Page 2 Several methods of condensate disposal have been reviewed for the new POU units. The different methods include: 1) Pump the condensate to the nearest area drain 2) Drain the condensate directly to the ramp 3) Drain the condensate to the discharge of the condenser fan The current project direction is to order the POU units with an internal condensate pump and hose that is piped directly to the discharge side of the condenser fan on the unit’s exterior, which will then evaporate the condensate. This approach has been compared to the restrictions on condensate disposal in the 2009 International Mechanical Code along with the 2011 Denver Amendments, and is fully compliant with the codes. 5. MD80 Aircraft: According to the PCA unit manufacturer, any gates that service an MD80 aircraft must be provided with a special hose extension on the respective PCA unit due to the odd location of the MD80 duct connection. Currently, there are no MD80 aircraft in the aircraft mix at Concourse B. However, if this changes at any point, DIA will have to make the necessary provisions to service that aircraft with the appropriate hose. C. PCA Unit Location Determination The Aircraft fleet mix at each gate was evaluated to determine the minimum aircraft size at each gate. The minimum aircraft size determines if the PCA unit needs to be bridge-mounted or stand-mounted, because if the aircraft’s door sill height is too low, a bridge-mounted unit might hit the apron or pose a safety issue for ramp workers. Each gate was evaluated and the units were identified on the drawings as either bridge-mounted or stand-mounted. D. Design Alternatives Early in the Schematic Design Phase of the project, analyses of several design alternatives were performed to address several technical and operational issues associated with the project. These analyses are summarized in the following list as a reference of work completed previously: 1. 2. 3. 4. 5. 6. Peak Load Determination Plant Equipment Capacity Plant Location Glycol Type Air Handling Unit (AHU) Mounting at PBB Distribution Pipe Route in Basement Based on direction from DIA, the project consists of replacement of the POU units with similar types of units. E. Planning Study An Interim Report was prepared with the expressed intent of providing an estimate of capital costs, operational costs and maintenance costs. The study was prepared at the conclusion of the Schematic Design Phase to provide verification of least cost scenarios. Page 3 F. Statistical Summary No statistical summary was required for this design. G. Major Components All components for this project are categorical systems of the City. Page 4 H. Code Analysis No code analysis of this installation is required as no exiting or egress facilities are affected. I. Life Safety, Security and Communications Systems None of these systems will be affected or impacted by construction of this project. J. Systems Load Requirements The project will have an effect on the overall building electrical system and no effect on the natural gas system. Because of the larger heating coil in the new units, the peak electrical demand for the Concourse will likely increase. However, the actual increase is difficult to estimate as the peak load will be a function of diversity of the units in operation. Electrical Load calculations have been performed and are displayed on the drawings. K. Design Alternatives Design alternatives as part of the bid package are not anticipated. L. Costs and Budgets A cost estimate has been prepared and is included in Appendix B of this report. M. Value Engineering No formal value engineering analysis has been performed as part of this project. N. Operations and Maintenance Criteria (O&M) No special maintenance criteria pertain to this project. O. List of Equipment and Long Lead Items The new DX POU units will be the longest lead items for this project. Depending on the desire of DIA to have the units operating, it may be possible to schedule the installation contractor with the initial delivery of the units. P. Critical Construction/RFP Activities This project has not been designated as a design-build project. Q. Independent Testing Laboratory Report No independent testing is expected. R. Contract Data Submittal Report (CSDR) This project has not been designated as a design-build project and therefore no CSDR is required. S. Cut Sheets Cut sheets for the new POU unit cut sheet have been included in Appendix C of this report. T. Soils Report This project does not involve any new foundations or sub-surface work. Therefore, we believe no new soils report is required. Page 5 U. FM Global Property Loss Prevention No Loss Prevention Data Sheets are available for this project. V. DIA Environmental Review The Environmental Planning Checklist will be prepared and submitted by the Environmental Department of DIA. W. Leadership in Energy & Environmental Design (LEED) LEED is not required for this project. Page 6 3.0 CALCULATIONS A. Structural Calculations The manufacturer of some of the existing PBB does not exist any longer. Therefore a structural analysis was performed on the PBBs to verify suitability for replacing the existing PCA units with larger/heavier units. Those calculations follow. B. Mechanical Calculations Mechanical calculations that were used to determine the required size of the units needed at each gate were performed and presented to DIA in Technical Memorandum 1. TM 1 is attached to this report separately and in its entirety. As a result, no mechanical calculations are provided in this section. Since the presentation of TM 1, the scope of the project has been revised to include 90 ton units at gates that need to accommodate B787 aircraft. The mechanical calculation for this aircraft has been provided by the PCA unit manufacturer. C. Electrical Calculations Electrical calculations that are needed to secure a permit from the Denver Building Department are shown on the drawings, so that, no additional supporting calculations are required and as a result none are provided in this section of the report. Page 7 San Engineering LLC Civil and Structural Engineering PCA AIR DIA PCA Replacement IFC STRUCTURAL CALCULATIONS Submittal Date: August 28,2014 Prepared for: Prepared by: Burns & McDonnell Engineering Aurom Mahobian, AP 9785 Maroon Cir Suite 400 Centennial, CO 80112 303-474-2267 San Engineering, LLC John J. Migliaccio, PE 6099 S. Windermere St. Littleton, CO 80120 (303) 503.2593 San Engineering LL Civil and Structural Engineering Colfax Station Calculations Index Description Page Station Structure Assumptions and Loading Criteria 3 Wind Analysis 4 Angle Leg Bending 6 Loads to Drive Column 6 Decking Spec 5 SAP Analysis of Jetway 7-59 PCA Unit Specs 60-62 Client: Burns & McDonnell Job No: Project: Subject: PCA Air Assumptions Date: Sheet No: San Engineering LLC Civil and Structural Engineering 08/28/14 of: Calculation Assumptions Jetway Framing • • • • Field inspection revealed jetway is supported on simply supported L5x5xl/2 spanning 25 '-0" max. The walls, floor and roof are framed with metal roof deck. Conservative assumption of 1.5B22 metal roof deck is used for design, (see roof deck following) Metal roof deck welded to L5x5xl/2 at 36" oc. Worst case loading is 90 Ton unit (weight = 7950 lb) at midspan. (see 90 ton unit specifications following. Loading • PCA Unit weight conservatively applied as Live Load = 7950 lb /4 = 2 kip • Snow Load = 30 psf • Passenger Live Load in Jetway =100 psf Wind 100 mph exposure C 1=1.0 Simplified procedure Ps = OCztIps30 Assume curved roof <15 degrees slope See enercalc output MFRWS Walls Zone A 77.0 psf Zone B -39.7 psf Zone C 50.8 psf Zone D -23.7 psf MFRWS Roof Zone E -92.5 psf Zone F -52.3 psf Zone G -64.4 psf Zone H-40.1 psf Use 77 psf for wind loading Project Title: Engineer: Project Descr: Title Block Line 1 You can change this area using the "Settings" menu item and then using the "Printing & Colfax Station I-225 Light Rail bky Project ID: Title Block" selection. Title Block Line 6 Printed: 29 JUL 2014, 3:18PM f ASCE 7-05 Simplified Procedure Wind Loads File: E:\Seagale Backup\EDUARDO-PC\CVT(MProjecls\DIA PCA AIRWia pea air.ec6 • ENERCALC, INC. 1983-2012, Build:6.12.11.1, Ver:6.12.4.30 | Licensee : San Engineering LLC 1 Lie. # : KW-06009192 Description : dia pea air Analytical Values Calculations per ASCE V: Basic Wind Speed per Sect 6.5.4 & Figure 1 100.0 mph Roof Slope Angle 0 to 5 degrees 7-05 All Buildings and other structures except those listed as Category I, III, and IV Occupancy per Table 1-1 1.00 Importance Factor per Sect. 6.5.5, & Table 6-1 Exposure Category per 6.5.6.3, .4 & .5 Mean Roof height Lambda : per Figure 6.2, Pg 40 Effective Wind Area of Component & Cladding Roof pitch for cladding pressure User specified minimum design pressure Topographic Factor Kzt per 6.5.7.2 Exposure C 20.0 ft 1.21 10.0 ftA2 0 to 7 degrees 10.0 psf 4.00 Net design pressure from table 1609.9.2.1(2)&(3) interpolated by area Design Wind Pressures Minimum Additional Load Case per 6.4.2.1.1 = 10 PSF on entire vertical plane Horizontal Pressures Zone: A = 76.96 psf Zone: C = 50.82 psf Zone: B = -39.69 psf Zone: D = -23.72 psf Vertical Pressures.. Zone: E = Zone: -92.44 psf Zone: G = -64.37 psf = -52.27 psf Zone: H = -40.66 psf Eoh = -129.23 psf Zone: Goh = -101.16 psf F Overhangs... Zone: Component & Cladding Design Wind Pressures Minimum Additional Load Case per 6.4.2.1.1 = 10 PSF on entire vertical plane Design Wind Pressure = Lambda * Kzt * Importance * Ps30 per ASCE 7-05 6.4.2.1 Eq 6-1 Roof Zone 1: Roof Zone 2: Positive: 35.332 psf Negative: -87.120 psf Positive: Negative: Roof Zone 3: Positive: Negative: Wall Zone 4: Wall Zone 5: 35.332 psf -146.168 psf 35.332 psf -219.736 psf Positive: 87.120 psf Negative: -94.380 psf Positive: Negative: 87.120 psf -116.644 psf Roof Overhang Zone 2: -31.339 psf Roof Overhang Zone 3: -51.667 psf J VULCRAFT 1.5 B, Bl, BA, BIA, BSV Maximum Sheet Length 42'-0 Extra charge for lengths under 6'-0 ICC ER-3415 FM Global Approved2 V '• \_, "W Interlocking side lap is not drawn to show actual detail. -30" OR 36* SECTION PROPERTIES Section Properties Deck type Design thickness in. W psf 'P in4/ft in3/ft in4/ft in3/ft B24 0.0239 1.46 0.107 0.120 0.135 0.131 : 2634 60 B22 0.0295 1.78 0.155 0.186 0.183 0.192 1818 33 Sp sfl v9 ry ksi lbs/ft B20 0.0358 2.14 0.201 0.234 0.222 0.247 2193 33 B19 0.0418 2.49 0.246 0.277 0.260 0.289 2546 33 B18 0.0474 2.82 0.289 0.318 0.295 0.327 2870 33 B16 0.0598 3.54 0.373 0.408 0.373 0.411 3578 33 ACOUSTICAL INFORMATION Deck Type 1.5BA, 1.5BIA 1 In 125 .11 Absorption Coefficient 2000 250 500 1000 1.02 0.61 .18 .66 4000 0.33 Noise Reduction Coefficient1 0.60 Type B (wide rib) deck provides excellent structural load carrying capacity per pound of steel utilized, and its nestable design eliminates the need for die-set ends. 1" or more rigid insulationis required for Type B deck. Acoustical deck (Type BA, BIA) is particularly suitable in structures such as auditoriums, schools, and theatres where sound control is desirable. Acoustic perforations are locatedin the vertical webs where the load carrying properties are negligibly affected (less than 5%). Source: Riverbank Acoustical Laboratories. Test was conducted with 1,50 pcf fiberglass batts and 2 inch polyisocyanurate foam insulation for the SDI. Inert, non-organic glass fiber soundabsorbing batts are placedin the rib openings to absorb up to 60% of the sound striking the deck. VERTICAL LOADS FOR TYPE 1.5B No. of Spans 1 2 3 Notes: Deck Tvne B24 B22 B20 B19 B18 B16 B24 B22 B20 B19 B18 B16 B24 B22 B20 B19 B18 B16 Max. SDI Const. SDan 4'-8 5'-7 6'-5 7-1 7'-8 8'-8 5'-10 6-11 7'-9 8-5 9'-1 10-3 5'-10 6'-11 7'-9 8'-5 9'-1 10'-3 5-0 115/56 98/81 123/105 146/129 168/152 215/196 124/153 100/213 128/267 150/320 169/369 213/471 154/120 124/167 159/209 186 / 250 210 / 289 264/369 5-6 95/42 81/61 102/79 121 / 97 138/114 178/147 103/115 83/160 106/201 124 / 240 140 / 277 176/354 128/90 103/126 132/157 154/188 174/217 219/277 Batts are field installed andmay require separation, Allowable Total (PSF) / Load Causino Deflection of L/240 or 1inch (PSF) Span (ft.-in.) ctr to ctr of suonorts 9-0 6-0 6-6 7-0 7-6 8-0 8-6 35/10 80/32 68/26 59/20 51/17 45/14 40/11 38/20 30/14 68/47 58/37 50/30 44/24 34/17 86/61 73/48 63/38 55/31 48/26 43/21 38/18 101/75 65/38 57/31 51/26 45/22 86/59 74/47 52/26 116/88 99/69 85/55 74/45 65/37 58/31 149/113 127/89 96/58 84/48 74/40 66/34 110/71 39/26 86/88 74/70 64/56 56/45 49/37 43/31 59/97 51/78 45/63 39/52 35/43 31/37 70/124 45/54 40/46 89/155 76 /122 66/97 57/79 51/65 104/185 89/145 77/116 67/95 59/78 52/65 47/55 59/75 53/63 118/213 101/168 87/134 76/109 67/90 110/172 95/140 84/115 74/96 66/81 149 / 273 127/214 54/24 48/21 92/55 79/44 69/35 61/29 108/69 64/61 56/50 49/41 43/34 39/29 87/97 74/76 111/121 95/95 82/76 72/62 63/51 56/43 50/36 130/145 96/91 74/61 65/51 58/43 111/114 84/74 66/50 147/167 126/132 108/105 95/86 83/71 74/59 93/75 83/63 185/214 158/168 136/135 119/109 105/90 1. Minimum exterior bearing length required is 1.50 inches. Minimum interior bearing length required is 3.00 inches. If these minimum lengths are not provided, web crippling must be checked. 2. FM Global approved numbers and spans available on page 21. 9-6 32/8 27/12 34/15 40/19 46/22 60/29 35/22 28/31 36/39 42/47 48/54 60/69 43/17 35/24 45/31 52/37 59/42 74/54 10-0 29/7 25/10 31/13 36/16 42/19 54/24 31/19 25/27 32/33 38/40 43/46 54/59 39/15 31/21 40/26 47/31 54/36 67/46 Client: Burns & McDonnell Job No: Project: Subject: PCA Air Assumptions Date: Sheet No: SL^T^SanEngineering u.c Civil and Structural Engineering 08/28/14 of: L5x5xl/2 Horizontal leg Bending • The PCA Air units hang from the horizontal leg of the L5x5xl/2 angles. • Ms = Pe = 2 kips * 2 1/2" = 5 kip-in • Mn / Q = Fy*t2*b / (4 * Q) = 36 ksi * 0.52 * 5" / (4 *1.67) = 6.76 k-in > Ms ok Check Loads to Drive Column Live Load: Snow Load: Dead Load: Total Load: • • • LL = 100 psf * 25'-0" *772= SL = 30 psf * 25'-0" *772= DL = 60 psf * 25'-0" * 772= 8.75 K 2.7 K 5.4 K 16.9 K Max possible load from new unit = 7950 lb (90 ton) - 4850 (60 ton unit) = 3100 lb (if centered over drive column) Additional Load to each wheel unit = 3100 lb / 2 = 1.55 K Percent increase = 1.55 k / 16.9 K = 9% Thus the midspan location would be the critical location because the additional load would result in maximum local bending stresses on the jet bridge box-truss structure chords spanning between Rotunda and Drive Column. The increase in loading at the support locations will be less than 10% compared to existing conditions. Therefore it can be safely concluded that the controlling condition will be the jet bridge box truss structure. Client: Burns & McDonnell Job No: Project: Subject: PCA Air Assumptions Date: Sheet No: San Engineering LLC Civil ami Structural Engineering 08/28/14 of: SAP Model SAP2000 Plus Version 15.2.1 was used to analyze the jetway. The jetway consists of L5x5xl/2 angles at all for comers and roof decking spanning between the angles. The roof decking has been modeled as flat shell elements with t = 0.2" (conservative). The PCA AIR unit weight has been applied to the jetway at the center to induce the largest moments on the angles. A snow load of 30 psf has been applied to the roof. Wind pressure of 77 psf has been added to the full height of the structure. The max interaction ration for the L5x5xl/2 is 0.170 (see SAP output following) SAP2000 SAP2000 v15.2.1 - File:Jet way sap model_V11_V12 7-29 - 3-D View - Kip, in, F Units 7/29/14 15:35:18 SAP2000 SAP2000 v15.2.1 - File:Jet way sap model_V11_V12 7-29 - Frame Span Loads (Live) (As Defined) - lb, ft, F Units 7/29/14 15:54:01 SAP2000 SAP2000 V15.2.1 - File:Jet way sap model_V11_V12 7-29 - Frame Span Loads (SNOW) (As Defined) - lb, ft, F Units 7/29/14 15:54:35 SAP2000 SAP2000 v15.2.1 - File:Jet way sap model_V11_V12 7-29 - Frame Span Loads (WIND) (As Defined) - lb, ft, F Units 7/29/14 15:54:53 SAP2000 7/29/14 15:55:34 0.00 0.50 0.70 0.90 SAP2000 v15.2.1 - File:Jet way sap model_V11_V12 7-29 - Steel Design Sections (AISC-LRFD99) - Kip, in, F Units 1.00 SAP2000 SAP2000 V15.2.1 - File:Jetway sap model_V11_V12 7-29-3-D View-Kip, in, F Units 7/29/14 15:56:15 •SAP2ooo >:34 ' FHe:Jet Ways apm0de/__Vlt '^Sr^ws SAP2000 7/29/14 15:56:55 7/29/14 15:57:25 SAP2000 V15.2.1 - FtlerJet way sap modeT vYl_V12 7-2g: Oeformed Shape (UDSTL2) -KipTn, F Units SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Jet way sap model__V11_V12 7-29,sdb Table: Area Section Assignments Table: Area Section Assignments Area Section MatProp 5 deck Default 8 deck 11 deck Default Default 14 17 20 deck Default deck deck Default 23 26 29 deck deck deck 30 33 deck 36 39 42 45 48 51 54 55 58 61 64 67 70 73 76 79 80 84 87 90 93 97 100 103 106 Default Default Default Default Default Default Default Default deck deck deck Default Default Default Default deck deck deck deck deck deck Default Default deck deck Default Default deck deck Default Default deck deck Default Default Default Default deck deck deck deck Default Default Default deck deck deck Default Default Default deck deck deck Default Default Default deck Table: Frame Loads - Distributed, Part 1 of 3 Table: Frame Loads - Distributed, Part 1 of 3 Frame LoarlPat CoordSys Type Dir DistTypc RelDistA • 1 GLOBAL Force GLOBAL Force Gravity Gravity RelDist 2 Live Live 0.0000 0.0000 6 Live GLOBAL Force Gravity RelDist 7 8 Live GLOBAL GLOBAL Force Force Gravity Gravity RelDist GLOBAL GLOBAL Force Force Gravity Gravity 9 10 Live Live Live RelDist RelDist RelDist RelDist 0.0000 0.0000 0.0000 0.0000 0.0000 Page 1 of 43 Jet way sap model_V11_V12 7-29.sdb Table: SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Frame Loads - Distributed, Part 1 of 3 RelDistA Frame LoadPat CoordSys Type Dir DistType 11 12 13 Live GLOBAL GLOBAL Force Force Force Gravity RelDist Gravity RelDist 0.0000 0.0000 Gravity RelDist 0.0000 14 15 Live Live Live GLOBAL Force Gravity Gravity Gravity RelDist RelDist RelDist 0.0000 GLOBAL Force Force Gravity Gravity RelDist RelDist 0.0000 Gravity RelDist 0.0000 0.0000 Gravity RelDist 0.0000 Gravity Gravity RelDist RelDist 0.0000 Gravity RelDist 0.0000 0.0000 0.0000 16 Live Live GLOBAL GLOBAL 17 18 Live GLOBAL Force Live 19 20 Live GLOBAL GLOBAL Force Force GLOBAL Force Force 21 22 23 24 25 26 27 28 29 29 29 29 29 32 32 32 32 Live Live Live Force Force Live Live Live GLOBAL GLOBAL Force Force Gravity Gravity RelDist RelDist Live Live Live GLOBAL GLOBAL GLOBAL Force Force Gravity RelDist Gravity Gravity RelDist RelDist Live Live GLOBAL GLOBAL GLOBAL Gravity RelDist Y RelDist RelDist Live Live WIND Live Live 32 Live Live WIND 35 35 Live Live 35 35 Live 35 38 38 38 GLOBAL GLOBAL GLOBAL Live WIND Live Live Live GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL Force Force Force Force Force Force Force Force Y Y Y Gravity 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 RelDist 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 RelDist RelDist Force Force Y RelDist RelDist RelDist Force Force Y Gravity RelDist RelDist Force Y RelDist Force Force Force Y Y Y Gravity RelDist RelDist RelDist Y Y RelDist RelDist Force Force Force Y Y Gravity RelDist RelDist RelDist Force Force RelDist Force Y Y Y Force Force Y Gravity Force Force Force Y Y 0.0000 0.0000 RelDist 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 38 38 Live WIND 41 Live GLOBAL GLOBAL 41 41 Live GLOBAL GLOBAL 41 Live Live 41 WIND GLOBAL GLOBAL 44 44 Live Live GLOBAL GLOBAL Force Y RelDist 44 Live Force Force Y RelDist RelDist 0.0000 Live GLOBAL GLOBAL WIND GLOBAL Force RelDist 0.0000 Live Live GLOBAL Force Force Y Gravity RelDist RelDist 0.0000 0.0000 RelDist RelDist 0.0000 RelDist 0.0000 RelDist 0.0000 44 44 47 47 47 47 47 50 Y Y Live GLOBAL GLOBAL Force Y Live GLOBAL Force Y WIND GLOBAL GLOBAL Force Force Y Gravity Live 0.0000 RelDist 0.0000 0.0000 RelDist 0.0000 RelDist RelDist 0.0000 0.0000 0.0000 0.0000 0.0000 Page 2 of 43 SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Loads - Distributed, Part 1 of 3 Frame LoadPat CoordSys Type Dir DistType 50 Live Y Y GLOBAL RelDist RelDist 0.0000 Live Force Force Force 0.0000 Live GLOBAL GLOBAL RelDist 50 50 50 WIND Live GLOBAL Force Force Y Gravity Live GLOBAL GLOBAL Force Y Force Y Force Force Live GLOBAL GLOBAL GLOBAL Y Y Gravity Live Live GLOBAL GLOBAL Live 53 53 53 53 53 54 54 54 Live Live WIND GLOBAL 54 54 WIND GLOBAL GLOBAL 54 Live GLOBAL 54 55 SNOW Live Live GLOBAL GLOBAL Live GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL 55 55 55 55 55 55 56 56 56 56 56 56 56 57 57 57 57 57 57 57 58 58 58 58 58 58 58 59 59 59 Live WIND Live SNOW Live Live GLOBAL Force Force Force Force Force Force Force Force Force Force Force Force Force Force Force Live Live GLOBAL GLOBAL GLOBAL GLOBAL WIND Live GLOBAL GLOBAL SNOW GLOBAL Force Force Force Force Live Live Live Live WIND GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL Live SNOW Force Force Y RelDist 0.0000 Gravity Gravity RelDist RelDist 0.0000 0.0000 Y Y Y Y Gravity Gravity Gravity RelDist RelDist RelDist RelDist 0.0000 0.0000 RelDist RelDist 0.0000 Y Y Y RelDist RelDist RelDist RelDist 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 Y Gravity Gravity RelDist RelDist RelDist Force Force Gravity 0.0000 0.0000 Force Y RelDist RelDist RelDist Force Force Y Y Gravity RelDist 0.0000 0.0000 RelDist 0.0000 0.0000 RelDist RelDist 0.0000 0.0000 RelDist 0.0000 0.0000 Force Force Y Y GLOBAL GLOBAL Force Force Y Y GLOBAL Force GLOBAL GLOBAL Force Force Y Gravity Live GLOBAL Force Live GLOBAL GLOBAL Force GLOBAL Force Force Force RelDist RelDist 0.0000 0.0000 0.0000 Gravity RelDist RelDist 0.0000 0.0000 Y Y RelDist RelDist Y RelDist 0.0000 0.0000 0.0000 Y Gravity RelDist RelDist RelDist 0.0000 0.0000 0.0000 RelDist 0.0000 RelDist 0.0000 0.0000 Gravity 59 WIND GLOBAL 59 Live Force 59 60 SNOW GLOBAL GLOBAL GLOBAL Force Gravity Gravity GLOBAL GLOBAL Force Force Y Y Force RelDist RelDist 0.0000 0.0000 RelDist 59 Live 0.0000 0.0000 0.0000 RelDist Live Live 60 60 RelDist RelDist 0.0000 Force Live Live 0.0000 0.0000 RelDist RelDist Y Y Y Gravity Force Live SNOW 0.0000 RelDist RelDist 0.0000 Gravity Gravity Live WIND 0.0000 RelDist RelDist RelDist RelDist Y GLOBAL GLOBAL GLOBAL Live Live Live RelDistA RelDist Page 3 of 43 Jet way sap model_V11_V12 7-29.sdb Table: rame 60 60 60 60 61 61 SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Frame Loads - Distributed, Part 1 of 3 DistType RelDistA LoadPat CoordSys Type Dir Live GLOBAL Force Force Y RelDist 0.0000 Y Gravity Gravity RelDist 0.0000 0.0000 WIND Live GLOBAL GLOBAL SNOW Live Live GLOBAL GLOBAL GLOBAL GLOBAL Force RelDist RelDist RelDist 0.0000 Gravity Force Y RelDist Force Force Y Y RelDist 0.0000 0.0000 Force Y Gravity Gravity RelDist RelDist 0.0000 0.0000 RelDist RelDist RelDist 0.0000 0.0000 Force Force 0.0000 61 Live 61 Live 61 61 61 WIND Live GLOBAL GLOBAL GLOBAL SNOW GLOBAL Live GLOBAL Force Force Live Live Live GLOBAL GLOBAL Force Force Y Y RelDist 0.0000 RelDist GLOBAL Y GLOBAL GLOBAL RelDist RelDist 0.0000 0.0000 WIND Live SNOW Force Force Live Live GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL 62 62 62 62 62 62 62 63 63 63 63 63 63 63 64 64 64 64 64 64 64 65 65 65 65 Live Live WIND Live SNOW Live Live GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL Force Force Force Force Force Force Force Force Force Force Force Force Live SNOW GLOBAL GLOBAL GLOBAL Force Force Force GLOBAL GLOBAL GLOBAL Force Force Force Force Gravity Gravity Y Y Y Force Force Gravity Force Force Gravity Live SNOW 66 66 66 Live Live GLOBAL GLOBAL Live GLOBAL Force 66 66 Live WIND GLOBAL GLOBAL Force Force 66 Live GLOBAL 66 SNOW 67 65 Y Y Gravity GLOBAL GLOBAL GLOBAL 65 65 Y Y Y Gravity Y Y Y Gravity GLOBAL GLOBAL Live WIND Gravity Y Gravity Gravity GLOBAL Live Live Y Gravity Gravity Force Force Force Live Live WIND Live Gravity Y Y Y 0.0000 0.0000 RelDist RelDist 0.0000 0.0000 RelDist 0.0000 RelDist RelDist 0.0000 0.0000 RelDist RelDist RelDist 0.0000 0.0000 0.0000 0.0000 RelDist RelDist RelDist RelDist RelDist RelDist 0.0000 0.0000 0.0000 0.0000 0.0000 RelDist RelDist RelDist RelDist RelDist 0.0000 RelDist RelDist 0.0000 RelDist RelDist RelDist RelDist RelDist RelDist 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 RelDist 0.0000 Force Y Gravity RelDist GLOBAL Force Gravity RelDist 0.0000 0.0000 Live GLOBAL Live Y RelDist RelDist 0.0000 67 Force Force Gravity 67 67 Live Live GLOBAL GLOBAL Force Y RelDist 0.0000 Y RelDist 67 WIND GLOBAL Live GLOBAL Y Gravity RelDist 67 Force Force Force 0.0000 0.0000 0.0000 SNOW GLOBAL GLOBAL Force Force 67 68 Live GLOBAL Gravity RelDist RelDist Gravity RelDist 0.0000 0.0000 0.0000 Page 4 of 43 SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Loads - Distributed, Part 1 of 3 Frame LoadPat CoordSys Type Dir DistType 68 68 Live GLOBAL Force 0.0000 GLOBAL Force Force Y Y Y RelDist Live Live RelDist RelDist 0.0000 0.0000 WIND Live GLOBAL GLOBAL 0.0000 0.0000 GLOBAL Y Gravity Gravity RelDist RelDist SNOW Live Force Force RelDist Force Force Gravity RelDist 0.0000 0.0000 Live GLOBAL GLOBAL GLOBAL Force Y Y RelDist RelDist 0.0000 Live Live WIND GLOBAL GLOBAL Live GLOBAL Y Y Gravity RelDist RelDist RelDist 0.0000 0.0000 69 Force Force Force 69 71 71 SNOW GLOBAL Gravity RelDist 0.0000 Live Live GLOBAL GLOBAL Force Force Gravity Force Y RelDist RelDist 0.0000 0.0000 71 71 71 Live GLOBAL GLOBAL GLOBAL Force Force 0.0000 0.0000 0.0000 71 71 Live SNOW GLOBAL Y Y Y Gravity RelDist Live WIND 72 72 Live 68 68 68 68 69 69 69 69 69 72 72 72 72 72 Live Live Live WIND 73 73 73 Live SNOW Live Live Live 73 73 Live WIND 73 Live 73 74 SNOW Live 74 Live 74 74 Live Live 74 GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL Force Force Force Force Force Gravity Gravity Force Force Force Y Y Y Force Force Y Gravity Gravity Force Force Force Force GLOBAL GLOBAL Force Force Force GLOBAL GLOBAL GLOBAL Force Force Force RelDist RelDist RelDist RelDist RelDist RelDist RelDist RelDist RelDist Gravity RelDist RelDist RelDist Y Y Y RelDist RelDist RelDist Y Gravity Gravity RelDist RelDist RelDist RelDist Gravity RelDistA 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 Y Y RelDist RelDist RelDist Y Gravity RelDist RelDist Force Force Gravity GLOBAL Force Y RelDist RelDist RelDist Live GLOBAL GLOBAL Force Force Y Y RelDist Live WIND Y Gravity Gravity RelDist RelDist RelDist 0.0000 Gravity Y RelDist 0.0000 RelDist 0.0000 0.0000 GLOBAL Force WIND GLOBAL GLOBAL Force Force 74 Live GLOBAL Force 74 75 SNOW Live GLOBAL GLOBAL 75 Live 75 75 Y Gravity RelDist 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 75 Live GLOBAL GLOBAL 75 SNOW GLOBAL Force Force Force 76 76 Live GLOBAL Force Live Live GLOBAL Force Force Force Y RelDist Y RelDist RelDist 0.0000 Y Gravity RelDist 0.0000 75 76 Live GLOBAL GLOBAL 76 76 WIND GLOBAL Force Live GLOBAL Force 76 0.0000 0.0000 Page 5 of 43 SAP2000 v15.2.1 - License #OX23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Loads - Distributed, Part 1 of 3 Frame LoadPat CoordSys Type Dir DistType 76 SNOW Live GLOBAL GLOBAL Gravity Gravity RelDist 0.0000 GLOBAL RelDist RelDist 0.0000 Live Live Force Force Force WIND GLOBAL GLOBAL Y Y Force Live SNOW GLOBAL GLOBAL RelDist Live GLOBAL GLOBAL Y Gravity Gravity Gravity RelDist RelDist RelDist 0.0000 Live Force Force 0.0000 0.0000 0.0000 77 77 77 77 77 77 77 78 78 78 78 Live Live Live 78 WIND 78 78 79 79 79 GLOBAL Live GLOBAL GLOBAL Force Force Force Live Live 80 80 80 81 81 SNOW Live 81 SNOW Live Live SNOW Live 83 83 84 84 84 85 85 85 86 Force Live SNOW Live Live 82 83 Force Force Force 79 82 82 Force GLOBAL GLOBAL GLOBAL Live WIND Live SNOW 79 79 79 GLOBAL Live Live SNOW Live Live SNOW Live Live SNOW Live GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL Force Force Force Force Force Force Force Force Force Force Force Force Force Force Force Force Y RelDist RelDist Y Y RelDist RelDist Y Y Gravity RelDist RelDistA 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 RelDist RelDist RelDist 0.0000 RelDist RelDist RelDist 0.0000 0.0000 RelDist RelDist RelDist 0.0000 0.0000 0.0000 Gravity Gravity RelDist RelDist 0.0000 Gravity RelDist RelDist Gravity Gravity Y Y Y Y Gravity 0.0000 0.0000 0.0000 0.0000 0.0000 RelDist RelDist 0.0000 0.0000 0.0000 Gravity Gravity RelDist RelDist RelDist 0.0000 0.0000 0.0000 Gravity Gravity Gravity RelDist RelDist RelDist 0.0000 0.0000 Gravity Gravity Gravity RelDist Gravity Gravity Gravity RelDist Gravity Gravity Gravity RelDist RelDist RelDist 0.0000 0.0000 Gravity Gravity Gravity Gravity GLOBAL GLOBAL GLOBAL Force Force GLOBAL GLOBAL GLOBAL Force Force GLOBAL GLOBAL GLOBAL Force Force GLOBAL GLOBAL GLOBAL Force Force GLOBAL GLOBAL Gravity RelDist 0.0000 Gravity GLOBAL Force Force Force Gravity RelDist RelDist 0.0000 0.0000 Force Force Force Force RelDist RelDist RelDist RelDist 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 86 Live SNOW 87 87 Live Live 87 SNOW GLOBAL Force 88 88 Live Live GLOBAL GLOBAL Force Gravity Gravity RelDist RelDist 0.0000 RelDist 0.0000 SNOW GLOBAL Force Force Gravity 88 89 89 Gravity RelDist Live GLOBAL GLOBAL Force Gravity 0.0000 0.0000 Force 89 SNOW Live Live GLOBAL Force Gravity Gravity RelDist RelDist GLOBAL GLOBAL Force Force 86 90 90 Live 0.0000 0.0000 RelDist 0.0000 Gravity RelDist Gravity RelDist 0.0000 0.0000 Page 6 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Loads - Distributed, Part 1 of 3 Frame LoadPat CoordSys Type Dir DistType 90 91 91 SNOW GLOBAL Force Live Live Force Gravity Gravity RelDist RelDist RelDist SNOW Live Live Force Force Gravity 91 GLOBAL GLOBAL GLOBAL Gravity GLOBAL Force Force Force Gravity Gravity RelDist RelDist Gravity RelDist RelDist RelDist 92 92 GLOBAL 92 93 93 SNOW GLOBAL Live GLOBAL GLOBAL Force Gravity Force 93 94 SNOW Live Force Force 94 Live GLOBAL GLOBAL GLOBAL Gravity Gravity Gravity 94 SNOW Live Live GLOBAL Force GLOBAL GLOBAL Force Force GLOBAL 96 96 SNOW Live Live Force Force Force 96 97 SNOW Live 97 Live 97 98 98 SNOW Live Live GLOBAL GLOBAL GLOBAL GLOBAL 98 99 99 SNOW Live Live 99 100 100 SNOW Live Live 100 SNOW 101 101 Live Live 101 102 102 102 SNOW Live 95 95 95 Live GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL Live GLOBAL SNOW Live Live GLOBAL GLOBAL 103 104 104 SNOW Live GLOBAL GLOBAL Live 104 SNOW GLOBAL GLOBAL 103 103 Force Force Force Force Force Force Force Force Force Force Force Force Force Gravity Gravity Gravity Gravity Gravity RelDist RelDist RelDist RelDist RelDist RelDist RelDist RelDist RelDist RelDist RelDist Gravity Gravity RelDist RelDist Gravity Gravity RelDist RelDist Gravity Gravity RelDist RelDist Gravity RelDist RelDist RelDist RelDist Force Force Gravity Gravity Gravity RelDist RelDist Force Force Gravity Gravity RelDist RelDist Force Gravity RelDist Force Force Gravity Gravity RelDist RelDist Force Gravity RelDist Force Gravity Gravity RelDist RelDist Gravity RelDist Gravity RelDist Force Force Force Force 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 RelDist Gravity Gravity Gravity Gravity Gravity Gravity Gravity RelDistA RelDist Table: Frame Loads - Distributed, Part 2 of 3 Frame Table: Frame Loads - Distributed, Part 2 of 3 RelDistB AbsDistA AbsDistB FOverLA in Kip/in Kip/in 12.000 0.0292 0.0292 12.000 0.0292 0.0292 12.000 0.0292 12.000 0.0292 0.0292 0.0292 LoadPat jjajgl 1 2 6 7 in Live Live Live Live 1.0000 1.0000 1.0000 1.0000 o.ooo" 0.000 0.000 0.000 FOverLB Page 7 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame 8 9 10 11 12 13 14 15 LoadPat Frame Loads - Distributed, Part 2 of 3 RelDistB AbsDistA AbsDistB FOverLA in in Kip/in FOverLB Kip/in 12.000 12.000 0.0292 0.0292 CK0292 0.0292 12.000 12.000 0.0292 0.0292 0.0292 12.000 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 Live Live Live 1.0000 0.000 1.0000 1.0000 0.000 Live Live 1.0000 1.0000 0.000 0.000 Live 1.0000 0.000 12.000 Live 1.0000 1.0000 0.000 12.000 0.000 0.000 12.000 12.000 12.000 12.000 12.000 0.000 16 Live Live 17 18 Live Live 1.0000 1.0000 Live Live Live 1.0000 0.000 0.000 0.000 1.0000 0.000 12.000 0.0292 0.0292 0.0292 1.0000 1.0000 0.000 12.000 12.000 0.0292 1.0000 1.0000 1.0000 0.000 0.000 0.000 12.000 1.0000 1.0000 0.000 12.000 12.000 12.000 12.000 0.0292 0.0292 0.0292 0.0292 12.000 12.000 0.0125 0.0196 -0.0321 0.0321 19 20 21 22 23 24 25 26 Live Live Live Live Live Live Live 1.0000 0.000 12.000 12.000 1.0000 0.000 0.000 Live Live 1.0000 1.0000 1.0000 0.000 0.000 0.000 Live WIND 1.0000 1.0000 12.000 12.000 1.0000 1.0000 1.0000 1.0000 0.000 0.000 32 32 35 Live Live Live Live 0.000 0.000 0.000 WIND Live 1.0000 35 35 Live Live 0.000 0.000 0.000 0.000 36.000 36.000 36.000 36.000 35 35 Live WIND 38 Live 38 38 Live Live 38 Live 38 WIND 41 41 Live 27 28 29 29 29 29 29 32 32 32 Live 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 41 41 Live Live Live 41 WIND 1.0000 1.0000 1.0000 1.0000 44 44 Live Live 44 Live 1.0000 44 Live WIND Live 1.0000 44 47 47 47 Live Live 1.0000 1.0000 1.0000 1.0000 1.0000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 36.000 36.000 36.000 36.000 36.000 36.000 36.000 36.000 36.000 36.000 36.000 36.000 36.000 0.0292 0.0292 0.0292 0.0292 0.0292 0.0125 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0292 0.0125 0.0196 -0.0321 0.0321 0.0292 0.0196 -0.0321 0.0125 0.0196 -0.0321 0.0321 0.0292 0.0321 0.0292 0.0125 0.0196 -0.0321 0.0125 0.0321 0.0292 0.0125 0.0196 -0.0321 0.0321 0.0196 -0.0321 0.0321 0.0292 0.0125 0.0196 0.0292 -0.0321 0.0321 0.0292 0.0125 0.0196 0.0125 0.0196 0.000 36.000 36.000 -0.0321 -0.0321 0.000 36.000 0.0321 0.0321 0.000 0.000 36.000 36.000 0.0292 0.0125 0.000 0.000 36.000 36.000 0.0196 -0.0321 -0.0321 0.000 36.000 0.0321 0.0321 0.000 0.000 36.000 36.000 36.000 0.0292 0.0292 0.0125 0.0196 0.0125 0.0196 0.000 0.000 0.000 0.0292 0.0125 0.0196 Page 8 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model V11 V12 7-29.sdb Frame Table: Frame Loads - Distributed, Part 2 of 3 AbsDistB AbsDistA RelDistB FOverLA in in Kip/in Kip/in 36.000 36.000 36.000 -0.0321 -0.0321 0.0321 LoadPat FOverLB 47 Live 1.0000 47 50 WIND Live 1.0000 1.0000 0.000 0.000 0.000 50 1.0000 1.0000 0.000 0.000 36.000 0.0125 0.0292 0.0125 50 50 Live Live Live 36.000 0.000 36.000 0.0196 -0.0321 -0.0321 50 WIND 1.0000 1.0000 0.000 53 Live Live 1.0000 1.0000 0.000 0.000 36.000 36.000 Live Live 1.0000 1.0000 0.000 WIND 1.0000 1.0000 54 Live Live Live 54 54 Live WIND 1.0000 53 53 53 53 54 54 1.0000 1.0000 54 Live 1.0000 1.0000 54 55 55 55 SNOW Live 1.0000 1.0000 Live Live 1.0000 55 55 55 55 56 Live WIND 1.0000 1.0000 1.0000 1.0000 36.000 0.0321 0.0292 0.0321 0.0292 0.0125 0.0196 0.0321 0.0292 0.0125 36.000 36.000 0.0196 0.0196 -0.0321 0.000 0.000 36.000 0.0321 -0.0321 0.0321 12.000 12.000 12.000 0.0088 0.0125 0.0196 0.0088 0.000 0.000 0.000 0.000 0.000 0.000 0.000 12.000 12.000 -0.0321 0.0321 12.000 12.000 -0.0321 0.0321 -0.0088 0.0088 0.000 0.000 0.000 0.000 12.000 12.000 12.000 12.000 0.000 12.000 12.000 0.000 12.000 -0.0088 0.0088 0.0088 0.0125 0.0196 -0.0321 0.0321 0.0125 0.0196 0.0088 0.0125 0.0196 -0.0321 0.0321 -0.0088 0.0088 12.000 12.000 -0.0088 0.0088 0.0088 0.0125 12.000 12.000 0.0196 -0.0321 0.000 0.000 0.000 12.000 12.000 12.000 -0.0088 0.0088 0.0196 -0.0321 0.0321 -0.0088 1.0000 1.0000 0.000 0.000 Live 1.0000 0.000 12.000 12.000 12.000 57 57 Live WIND 1.0000 1.0000 0.000 0.000 57 Live 0.000 57 58 SNOW Live 1.0000 1.0000 1.0000 12.000 12.000 12.000 58 Live 1.0000 0.000 0.000 0.000 58 Live 1.0000 58 Live WIND 1.0000 1.0000 0.000 0.000 Live 1.0000 0.000 58 SNOW Live 1.0000 1.0000 0.000 59 59 Live Live Live SNOW Live 0.000 0.000 Live Live Live 1.0000 1.0000 1.0000 1.0000 1.0000 WIND 1.0000 56 Live SNOW 1.0000 1.0000 57 57 Live Live 57 56 56 56 56 56 58 58 59 59 59 59 59 Live WIND Live SNOW 0.000 0.000 0.000 0.000 0.0088 0.0125 0.0088 0.0088 0.0125 0.0196 0.0196 -0.0321 -0.0321 0.0321 -0.0088 0.0321 -0.0088 12.000 12.000 12.000 0.0088 0.0088 0.0088 0.0125 12.000 0.0196 12.000 12.000 -0.0321 0.0321 0.0125 0.0196 -0.0321 12.000 12.000 -0.0088 0.0088 0.0088 -0.0088 0.0125 0.0196 -0.0321 0.0125 0.0196 -0.0321 0.000 0.000 12.000 1.0000 1.0000 0.000 12.000 0.000 1.0000 0.000 12.000 12.000 1.0000 1.0000 0.000 0.000 1.0000 0.0321 0.0088 0.0125 12.000 12.000 12.000 0.0088 0.0321 0.0088 0.0088 0.0321 0.0321 -0.0088 0.0088 -0.0088 0.0088 Page 9 of 43 SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Loads - Distributed, Part 2 of 3 Frame LoadPat AbsDistB FOverLA in in Kip/in Kip/in 0.000 0.000 0.000 12.000 12.000 12.000 0.0088 0.0088 0.0125 0.0196 0.0125 1.0000 1.0000 0.000 12.000 0.000 12.000 -0.0321 0.0321 1.0000 0.000 12.000 -0.0088 0.000 0.000 0.000 12.000 12.000 12.000 0.0088 0.0125 12.000 12.000 12.000 0.0196 -0.0321 0.0321 -0.0321 0.0321 12.000 12.000 -0.0088 -0.0088 0.0088 12.000 0.0088 0.0125 0.0088 0.0088 1.0000 60 60 Live Live 60 60 Live Live 60 60 WIND Live 60 61 61 SNOW Live 1.0000 1.0000 Live 1.0000 61 Live 61 61 Live WIND 1.0000 1.0000 1.0000 0.000 0.000 0.000 61 Live 1.0000 0.000 61 SNOW Live 1.0000 1.0000 0.000 0.000 1.0000 0.000 62 62 Live Live Live WIND 1.0000 1.0000 0.000 0.000 1.0000 62 62 Live SNOW 1.0000 1.0000 0.000 0.000 63 Live Live 1.0000 1.0000 Live 1.0000 1.0000 1.0000 1.0000 62 62 62 63 63 63 63 63 63 64 64 64 64 64 64 Live WIND Live SNOW Live Live Live Live WIND Live 1.0000 1.0000 1.0000 1.0000 1.0000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 -0.0088 0.0088 12.000 12.000 12.000 12.000 12.000 12.000 12.000 0.000 0.000 0.000 12.000 12.000 12.000 1.0000 1.0000 1.0000 0.000 0.000 0.000 12.000 0.000 0.000 0.000 12.000 65 Live Live 1.0000 1.0000 1.0000 65 65 WIND 1.0000 Live 65 SNOW Live Live 1.0000 1.0000 0.000 0.000 0.000 1.0000 1.0000 66 12.000 12.000 12.000 1.0000 1.0000 SNOW Live 65 0.0196 -0.0321 12.000 12.000 1.0000 12.000 12.000 0.0088 0.0125 0.0196 -0.0321 0.0321 -0.0088 0.0088 0.0088 0.0125 0.0196 -0.0321 0.0321 -0.0088 0.0088 0.0321 -0.0088 0.0088 0.0088 0.0125 0.0196 0.0125 0.0196 -0.0321 0.0321 -0.0088 0.0088 0.0088 0.0125 0.0196 -0.0321 0.0321 -0.0088 0.0088 0.0088 0.0125 0.0196 -0.0321 0.0321 -0.0088 0.0088 0.0088 0.0125 0.0196 -0.0321 12.000 0.0196 -0.0321 0.0321 12.000 12.000 -0.0088 0.0088 0.000 12.000 0.0088 0.0125 12.000 12.000 1.0000 0.000 0.000 12.000 12.000 66 66 66 Live WIND 1.0000 1.0000 0.000 0.000 12.000 12.000 Live 1.0000 0.000 12.000 66 67 SNOW 1.0000 0.000 12.000 Live 1.0000 0.000 67 67 Live Live 1.0000 1.0000 0.000 0.000 12.000 12.000 67 67 Live WIND 1.0000 0.000 0.000 1.0000 0.0321 0.0196 -0.0321 0.0088 0.0125 Live 66 66 0.0088 12.000 12.000 12.000 0.000 0.000 64 65 65 Live FOverLB AbsDistA RelDistB 0.0088 0.0088 0.0196 0.0125 0.0196 -0.0321 -0.0321 0.0321 -0.0088 0.0321 -0.0088 0.0088 0.0088 0.0088 0.0125 0.0125 0.0196 12.000 0.0196 -0.0321 12.000 0.0321 12.000 0.0321 -0.0088 0.0088 -0.0321 0.0321 Page 10 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Loads - Distributed, Part 2 of 3 Frame LoadPal 67 Live 67 68 68 SNOW Live Live 68 RelDistB 1.0000 1.0000 AbsDistA AbsDistB 11181111811l!(lll|l!®o!© 12.000 0.000 0.000 0.000 12.000 12.000 0.000 Live 1.0000 1.0000 68 Live 1.0000 0.000 12.000 12.000 12.000 68 68 68 WIND 1.0000 Live SNOW 1.0000 1.0000 0.000 0.000 Live Live Live 1.0000 69 69 69 69 69 Live WIND Live 69 SNOW 69 71 71 Live Live 71 71 71 Live Live WIND 71 71 72 Live SNOW Live 72 72 Live Live 72 Live WIND 72 72 72 73 73 73 73 73 73 73 74 74 74 74 74 Live SNOW Live Live Live Live WIND 1.0000 1.0000 1.0000 1.0000 0.000 0.000 12.000 12.000 12.000 0.000 0.000 12.000 12.000 1.0000 1.0000 0.000 0.000 0.000 0.000 0.0196 -0.0321 12.000 12.000 12.000 12.000 -0.0088 0.0088 0.0088 0.000 0.000 0.000 12.000 0.0125 12.000 12.000 0.0196 -0.0321 -0.0088 0.0088 0.0088 0.0125 0.0196 0.000 0.000 0.000 12.000 12.000 12.000 12.000 0.0321 -0.0088 0.0088 0.0088 12.000 12.000 0.0125 0.0196 -0.0321 0.0321 0.000 0.000 0.000 12.000 12.000 0.000 12.000 12.000 WIND Live 1.0000 0.0321 -0.0088 0.0196 -0.0321 0.0321 12.000 12.000 1.0000 1.0000 -0.0321 0.0321 -0.0088 0.0088 0.0125 0.000 0.000 0.000 1.0000 -0.0321 0.0088 1.0000 1.0000 Live Live Live 0.0125 0.0196 0.0088 0.000 0.000 0.000 1.0000 1.0000 0.0088 0.0088 0.0088 0.0125 0.000 1.0000 1.0000 1.0000 1.0000 0.0196 -0.0321 0.0321 -0.0088 0.0088 0.0125 0.0196 12.000 12.000 12.000 0.0125 -0.0321 12.000 12.000 12.000 0.0088 0.0196 0.000 0.000 0.000 0.000 0.000 Live SNOW Live 0.0088 0.0088 0.0125 0.0321 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 -0.0088 0.0088 -0.0088 0.0088 0.000 0.000 1.0000 Kip/in -0.0088 12.000 12.000 0.000 FOverLB Kip/in 12.000 1.0000 1.0000 1.0000 1.0000 1.0000 FOverLA 0.000 0.000 12.000 12.000 12.000 0.0321 -0.0321 0.0321 -0.0088 0.0088 0.0088 0.0125 0.0196 -0.0321 0.0321 -0.0088 0.0088 0.0088 -0.0088 0.0125 0.0196 -0.0321 0.0125 0.0321 -0.0088 0.0088 0.0088 0.0196 -0.0321 0.0321 -0.0088 0.000 12.000 SNOW 1.0000 1.0000 0.000 0.0088 0.0088 Live 1.0000 0.000 12.000 12.000 0.0088 Live 1.0000 12.000 0.0125 0.0088 0.0125 1.0000 12.000 75 Live Live 0.000 0.000 0.000 12.000 0.0196 -0.0321 -0.0321 75 WIND 1.0000 1.0000 0.000 0.0321 Live 1.0000 0.000 12.000 12.000 0.0321 75 -0.0088 75 76 SNOW 1.0000 12.000 0.0088 Live Live Live 1.0000 0.000 0.000 -0.0088 0.0088 12.000 0.000 12.000 0.000 12.000 0.0088 0.0125 0.0196 74 74 75 75 75 76 76 1.0000 1.0000 0.0196 0.0088 0.0125 0.0196 Page 11 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame 76 76 76 76 77 77 77 Frame Loads - Distributed, Part 2 of 3 AbsDistA AbsDistB in in 1.0000 0.000 12.000 1.0000 1.0000 1.0000 0.000 12.000 12.000 Live Live 1.0000 0.000 0.000 Live Live 1.0000 LoadPat Live WIND Live SNOW RelDistB 1.0000 0.000 0.000 0.000 0.000 FOverLA Kip/in FOverLB -0.0321 0.0321 -0.0321 0.0321 -0.0088 -0.0088 12.000 0.0088 12.000 12.000 12.000 0.0088 0.0125 0.0088 0.0088 12.000 0.0196 -0.0321 1.0000 1.0000 0.000 12.000 Live SNOW Live 1.0000 0.000 1.0000 1.0000 0.000 0.000 12.000 12.000 Live Live 1.0000 0.000 12.000 78 78 78 78 Live WIND Live 1.0000 1.0000 0.000 0.000 12.000 12.000 1.0000 12.000 78 79 79 79 SNOW Live Live Live 0.000 0.000 0.000 0.000 0.000 0.000 12.000 12.000 0.0088 0.0125 12.000 79 79 Live WIND 1.0000 1.0000 1.0000 1.0000 0.000 Live SNOW 1.0000 1.0000 0.000 0.000 0.0196 -0.0321 0.0321 79 1.0000 1.0000 0.000 0.000 0.000 0.000 12.000 12.000 12.000 12.000 12.000 77 77 77 77 78 78 79 80 80 WIND Live Live 81 SNOW Live Live 81 82 82 SNOW Live Live 82 SNOW Live 80 81 83 83 83 84 84 Live SNOW Live Live 84 SNOW 85 Live Live 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 SNOW 1.0000 1.0000 0.000 0.000 Live Live 1.0000 1.0000 0.000 0.000 86 87 SNOW 1.0000 Live 87 Live 1.0000 1.0000 0.000 0.000 87 SNOW Live Live 1.0000 1.0000 85 85 86 86 88 88 88 89 89 SNOW Live Live Kip/in 12.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 0.0321 -0.0088 0.0125 0.0196 -0.0321 0.0321 -0.0088 0.0088 0.0088 0.0125 0.0088 0.0088 0.0196 0.0196 -0.0321 0.0321 -0.0321 0.0321 -0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0125 -0.0088 0.0088 0.0088 0.0125 0.0196 -0.0321 0.0321 -0.0088 0.0088 0.0088 -0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 -0.0088 12.000 12.000 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 12.000 0.0088 12.000 0.0088 -0.0088 0.0088 0.0088 12.000 12.000 12.000 12.000 12.000 12.000 0.0088 0.0088 -0.0088 0.0088 12.000 0.0088 0.0088 0.000 12.000 -0.0088 1.0000 0.000 12.000 0.0088 -0.0088 0.0088 1.0000 0.000 0.000 12.000 12.000 0.0088 -0.0088 -0.0088 0.000 12.000 0.0088 0.0088 0.000 0.000 12.000 0.0088 -0.0088 0.0088 -0.0088 1.0000 1.0000 12.000 0.0088 0.0088 Page 12 of 43 SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Loads - Distributed, Part 2 of 3 Frame LoadPat 89 90 90 SNOW 90 91 SNOW Live Live Live RelDistB AbsDistA AbsDistB in in 1.0000 1.0000 1.0000 1.0000 0.000 12.000 0.000 0.000 0.000 12.000 0.000 12.000 12.000 12.000 91 Live 1.0000 1.0000 91 SNOW Live Live 1.0000 1.0000 1.0000 0.000 0.000 0.000 12.000 SNOW Live 1.0000 0.000 0.000 0.000 12.000 12.000 Live 1.0000 1.0000 SNOW 1.0000 0.000 12.000 Live Live 1.0000 0.000 0.000 SNOW 1.0000 1.0000 0.000 12.000 12.000 12.000 0.000 0.000 12.000 12.000 Live 0.000 0.000 0.000 12.000 1.0000 1.0000 SNOW Live Live 1.0000 1.0000 1.0000 0.000 0.000 0.000 12.000 12.000 SNOW Live 1.0000 1.0000 1.0000 0.000 0.000 1.0000 1.0000 99 SNOW Live Live 99 100 100 SNOW Live Live 100 101 101 SNOW Live Live 1.0000 1.0000 1.0000 1.0000 0.000 0.000 0.000 0.000 12.000 12.000 12.000 12.000 12.000 101 102 102 SNOW Live Live 102 103 103 SNOW Live Live 103 104 SNOW 104 Live SNOW 92 92 92 93 93 93 94 94 94 95 95 95 Live Live SNOW Live 96 96 96 97 97 97 98 98 Live 98 99 104 Live 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 1.0000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 12.000 FOverLA Kip/in FOverLB Kip/in 0.0088 0.0088 0.0088 0.0088 -0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 0.0088 -0.0088 -0.0088 0.0088 0.0088 -0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 0.0088 0.0088 -0.0088 -0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 0.0088 0.0088 -0.0088 0.0088 0.0088 -0.0088 -0.0088 12.000 12.000 0.0088 0.0088 0.0088 0.0088 -0.0088 -0.0088 12.000 12.000 0.0088 0.0088 0.0088 0.0088 12.000 12.000 -0.0088 -0.0088 0.0088 12.000 12.000 12.000 12.000 0.0088 0.0088 0.0088 Table: Frame Loads - Distributed, Part 3 of 3 Table: Frame Loads - Distributed, Part 3 of 3 Page 13 of 43 Jet way sap model_V11_V12 7-29.sdb Table: Frame Loads - Distributed, Part 3 of 3 Frame LoadPat 2 6 Live 7 8 9 GUID Live Live Live 10 Live Live 11 12 13 Live Live Live 14 15 16 Live Live Live 17 18 Live Live 19 Live 20 21 Live Live 22 Live 23 24 25 Live Live Live 26 27 28 Live Live 29 29 Live Live Live 29 29 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Live 29 32 Live WIND Live 32 32 32 32 Live Live Live WIND 35 35 35 Live Live Live 35 35 Live WIND 38 38 38 Live Live Live 38 38 Live WIND 41 Live 41 41 41 Live Live Live 41 WIND 44 Live 44 44 Live Live 44 44 Live WIND Page 14 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Loads - Distributed, Part 3 of 3 Frame LoadPat 47 47 47 Live Live 47 47 50 50 50 Live Live WIND Live Live Live 50 Live 50 53 WIND 53 53 53 53 54 54 54 Live Live Live Live WIND Live Live Live 54 54 54 Live WIND 54 55 SNOW Live 55 Live 55 55 55 Live Live WIND Live SNOW 55 55 56 Live 56 56 56 Live Live Live Live 56 WIND 56 56 Live SNOW 57 Live 57 57 Live Live 57 57 57 WIND 57 58 58 Live Live SNOW Live Live 58 58 Live Live 58 WIND 58 Live 58 59 SNOW Live 59 Live 59 Live Live 59 GUID Page 15 of 43 Jet way sap model_V11_V12 7-29.sdb Table: Frame Loads - Distributed, Part 3 of 3 Frame LoadPat 59 WIND Live 59 59 60 60 60 60 60 60 60 Live Live Live Live WIND Live SNOW Live Live 61 Live 61 61 61 61 62 62 62 62 62 Live WIND Live SNOW Live Live Live Live WIND 62 62 63 63 Live SNOW 63 63 63 63 Live Live WIND 63 SNOW Live 64 64 64 64 64 Live Live Live Live Live Live WIND 64 Live 64 65 SNOW 65 Live Live 65 65 Live 65 WIND Live 65 65 66 Live SNOW Live 66 Live 66 Live Live WIND 66 66 66 66 67 67 GUID SNOW 61 61 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Live SNOW Live Live Page 16 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Loads - Distributed, Part 3 of 3 Frame LoadPat 67 67 67 Live 67 Live WIND 67 68 Live SNOW Live 68 Live 68 Live 68 Live 68 68 68 WIND Live 69 69 SNOW 69 Live Live Live 69 69 Live WIND 69 69 71 71 SNOW Live 71 71 71 Live Live WIND 71 71 72 SNOW Live 72 72 72 72 72 72 GUID Live Live Live Live Live Live WIND Live SNOW 73 73 73 Live Live 73 73 73 Live WIND 73 74 74 SNOW Live Live Live Live 74 Live 74 74 Live WIND 74 74 SNOW 75 Live 75 75 Live Live 75 75 WIND 75 75 SNOW Live Live Live Page 17 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Loads - Distributed, Part 3 of 3 Frame LoadPat 76 Live 76 76 76 76 76 Live Live Live WIND Live 76 77 77 SNOW Live 77 77 Live 77 77 77 78 78 78 78 78 78 78 Live Live WIND Live SNOW Live Live Live Live WIND Live SNOW 79 79 79 Live Live 79 79 79 Live WIND Live SNOW Live 79 80 80 80 81 81 81 GUID Live Live SNOW Live Live SNOW 82 82 Live Live 82 SNOW 83 83 Live Live 83 84 84 SNOW Live 84 Live SNOW 85 85 Live Live 85 86 86 SNOW 86 SNOW 87 Live 87 87 Live SNOW 88 88 Live Live Live Live Page 18 of 43 Jet way sap model_V11_V12 7-29.sdb SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Table: Frame Loads - Distributed, Part 3 of 3 Frame LoadPat 88 89 SNOW Live 89 Live 89 90 90 SNOW Live 90 91 SNOW Live Live 91 Live 91 SNOW Live 92 92 92 Live SNOW 93 Live 93 93 94 Live SNOW Live 94 94 95 95 Live SNOW 95 96 SNOW Live Live Live 96 Live 96 97 SNOW Live Live 97 97 98 98 SNOW Live 98 99 SNOW Live 99 Live SNOW 99 100 100 Live Live Live 100 SNOW 101 101 Live Live 101 102 SNOW Live 102 Live 102 103 103 SNOW Live Live 103 SNOW 104 Live Live 104 104 GUID SNOW Page 19 of 43 Jet way sap model_V11_V12 7-29.sdb SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Table: Frame Section Assignments Table: Frame Section Assignments Frame SectionType AutoSelect AnalSect DesignSect MatProp 1 2 6 Angle N.A. Default N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 Angle L5X5X1/2 Angle Default Default Angle Angle L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 7 8 N.A. N.A. L5X5X1/2 L5X5X1/2 Default 9 10 Angle N.A. N.A. L5X5X1/2 Default Default 11 Angle Angle Angle N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 Default L5X5X1/2 L5X5X1/2 Default Default L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Default Default Default L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Default Default Default L5X5X1/2 L5X5X1/2 L5X5X1/2 Default Default Default 12 13 14 15 16 17 18 19 20 21 Angle Angle Angle Angle Angle Angle N.A. N.A. N.A. N.A. N.A. N.A. N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 N.A. N.A. 22 23 Angle Angle Angle Angle Angle 24 Angle 25 26 Angle Angle N.A. N.A. N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 27 28 29 32 Angle Angle Angle N.A. N.A. N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Angle Angle Angle N.A. N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Angle Angle N.A. N.A. N.A. L5X5X1/2 N.A. N.A. N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 N.A. L5X5X1/2 L5X5X1/2 35 38 41 44 47 50 53 54 Angle 55 56 Angle Angle 57 58 59 Angle Angle Angle 60 Angle Angle Angle N.A. N.A. N.A. N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Angle N.A. N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 61 62 Angle Angle N.A. N.A. L5X5X1/2 63 Angle N.A. L5X5X1/2 L5X5X1/2 64 Angle 65 66 Angle N.A. N.A. L5X5X1/2 L5X5X1/2 N.A. L5X5X1/2 67 Angle Angle N.A. L5X5X1/2 68 Angle 69 Angle L5X5X1/2 L5X5X1/2 71 72 Angle N.A. N.A. N.A. N.A. N.A. 73 Angle Angle N.A. N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Default Default Default Default Default Default Default Default Default Default Default Default Default Default Default Default Default Default Default Default Default Default Default Default Default L5X5X1/2 Default L5X5X1/2 L5X5X1/2 L5X5X1/2 Default L5X5X1/2 L5X5X1/2 Default Default L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Default L5X5X1/2 Default Default Default Default Default Page 20 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Section Assignments Frame SectionType AutoSelect AnalSect DesignSect MatProp 74 75 Angle N.A. N.A. L5X5X1/2 N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Default Default N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Default N.A. N.A. L5X5X1/2 L5X5X1/2 Default Default N.A. N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Default N.A. N.A. L5X5X1/2 L5X5X1/2 Default L5X5X1/2 N.A. N.A. N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Default Default N.A. N.A. N.A. L5X5X1/2 L5X5X1/2 L5X5X1/2 Default Default Default 76 77 78 79 Angle Angle Angle Angle 80 Angle Angle 81 82 Angle Angle 83 Angle Angle 84 85 86 87 Angle Angle Angle 88 Angle 89 90 Angle 91 92 93 94 95 96 97 98 99 100 101 102 103 104 Angle Angle Angle Angle Angle Angle Angle Angle Angle Angle Angle Angle Angle Angle Angle N.A. N.A. N.A. N.A. N.A. N.A. N.A. N.A. N.A. N.A. N.A. N.A. N.A. N.A. N.A. L5X5X1/2 L5X5X1/2 Default Default Default L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Default Default Default L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Default Default Default L5X5X1/2 L5X5X1/2 L5X5X1/2 Default Default L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Default Default L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Default Default L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Default Default Default Default L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Table: Frame Section Properties 01 - General, Part 1 of 7 Table: Frame Section Properties 01 - General, Part 1 of 7 SectionName Material Shape t2 s in L5X5X1/2 W10X112 W10X12 W10X49 W10X68 W10X88 W12X136 W12X14 W12X16 W12X19 tw | inj 5.0000 5.0000 0.5000 0.5000 I/Wide Flange I/Wide Flange 11.4000 9.8700 1.2500 0.2100 0.7550 I/Wide Flange 9.9800 10.4000 3.9600 10.0000 0.5600 0.3400 I/Wide Flange 10.4000 10.8000 13.4000 0.7700 0.9900 0.4700 0.6050 STEEL I/Wide Flange lA/Vide Flange 10.1000 10.3000 12.4000 1.2500 0.7900 STEEL I/Wide Flange 3.9700 0.2250 STEEL STEEL I/Wide Flange 11.9000 12.0000 3.9900 0.2650 0.2000 0.2200 I/Wide Flange 12.2000 4.0100 STEEL 14.4000 12.7000 12.0000 0.3500 1.7400 1.0600 STEEL STEEL STEEL STEEL STEEL STEEL Angle W12X190 W12X65 STEEL I/Wide Flange I/Wide Flange W12X96 STEEL I/Wide Flange W14X109 W14X132 STEEL STEEL W14X159 STEEL I/Wide Flange I/Wide Flange lA/Vide Flange 12.1000 12.7000 14.3000 14.7000 15.0000 0.1900 0.2350 0.6050 0.3900 12.2000 0.9000 14.6000 14.7000 15.6000 0.8600 0.5500 0.5250 1.0300 1.1900 0.7450 0.6450 Page 21 of 43 Jet way sap model_V11_V12 7-29.sdb SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Table: Frame Section Properties 01 - General, Part 1 of 7 SectionName Material Shape t3 in t2 tf tw in in 15.8000 1.5600 0.3350 1.8900 in 0.9800 1.1800 2.2600 1.4100 1.6600 1.8800 STEEL I/Wide Flange STEEL STEEL I/Wide Flange I/Wide Flange 15.7000 13.7000 16.4000 W14X311 W14X370 W14X426 STEEL I/Wide Flange I/Wide Flange 17.1000 17.9000 16.2000 16.5000 18.7000 16.7000 W14X90 W16X26 STEEL STEEL I/Wide Flange I/Wide Flange 2.6600 3.0400 14.0000 I/Wide Flange 14.5000 5.5000 0.7100 0.3450 W16X31 STEEL I/Wide Flange 15.7000 15.9000 5.5300 0.4400 0.4400 0.2500 0.2750 W18X119 STEEL STEEL STEEL I/Wide Flange I/Wide Flange 19.0000 17.7000 11.3000 6.0000 I/Wide Flange 0.6550 0.3000 0.3150 STEEL STEEL STEEL I/Wide Flange 17.9000 18.1000 1.0600 0.4250 0.5250 7.5300 0.6300 0.7500 0.3900 0.6800 0.4250 STEEL STEEL STEEL I/Wide Flange 0.8700 0.4500 0.5350 0.3500 I/Wide Flange I/Wide Flange STEEL I/Wide Flange I/Wide Flange 12.8000 12.9000 0.5350 0.9800 0.8500 0.9600 0.3800 STEEL STEEL 12.9000 13.0000 1.0900 1.2200 12.9000 13.0000 13.2000 13.5000 1.3400 0.6500 0.7050 0.7500 0.8700 W14X211 W14X22 W14X257 W18X35 W18X40 W18X55 W18X65 W18X76 W18X97 W21X44 W21X50 W24X103 W24X117 W24X131 W24X146 W24X162 W24X176 W24X207 W24X250 W24X335 W24X55 W24X62 STEEL STEEL STEEL STEEL STEEL STEEL STEEL STEEL STEEL I/Wide Flange I/Wide Flange I/Wide Flange I/Wide Flange I/Wide I/Wide I/Wide l/Wlde Flange Flange Flange Flange I/Wide Flange I/Wide Flange I/Wide Flange I/Wide Flange 18.4000 18.2000 18.6000 20.7000 20.8000 24.5000 24.3000 24.5000 24.7000 25.0000 25.2000 25.7000 26.3000 27.5000 23.6000 23.7000 23.7000 W24X68 STEEL STEEL W24X76 W27X84 W27X94 STEEL STEEL STEEL I/Wide Flange I/Wide Flange I/Wide Flange 23.9000 26.7000 26.9000 W30X108 STEEL STEEL STEEL STEEL I/Wide Flange I/Wide Flange 29.8000 30.0000 I/Wide Flange 30.7000 I/Wide Flange I/Wide Flange 30.4000 30.7000 I/Wide Flange W30X116 W30X148 W30X173 5.0000 16.0000 6.0200 7.5900 11.0000 11.1000 6.5000 6.5300 9.0000 7.0100 7.0400 8.9700 8.9900 9.9600 9.9900 1.5700 1.8900 2.4800 0.2300 0.4500 0.5500 0.5500 0.6050 1.0400 1.3800 0.5050 0.5900 0.5850 0.3950 0.4300 0.6800 0.6400 0.7450 0.4400 0.4600 0.4900 0.5450 0.7600 0.4150 10.5000 10.5000 10.5000 0.8500 1.1800 15.0000 1.0700 29.7000 15.0000 10.5000 1.1900 0.6700 32.9000 33.1000 35.6000 11.5000 0.7400 11.5000 12.0000 0.8550 0.7900 0.5800 12.0000 0.9400 1.2600 1.3600 0.6250 0.7650 0.5650 0.6500 0.6550 0.7100 0.5200 0.5500 W33X118 STEEL STEEL STEEL W33X130 STEEL I/Wide Flange I/Wide Flange W36X135 STEEL I/Wide Flange W36X150 W36X194 W36X210 STEEL STEEL I/Wide Flange STEEL 12.2000 W36X230 W36X260 I/Wide Flange I/Wide Flange 36.7000 STEEL STEEL STEEL 35.9000 1.2600 0.7600 I/Wide Flange 36.3000 16.5000 16.6000 1.4400 I/Wide Flange 36.7000 7.8900 16.7000 1.6800 0.8400 0.9450 3.9400 I/Wide Flange I/Wide Flange I/Wide Flange 6.5000 0.2050 0.4000 0.1700 7.9300 8.0000 0.4350 0.2850 8.2500 8.0000 8.0700 0.5600 I/Wide Flange I/Wide Flange 8.7500 9.0000 8.2200 8.2800 0.8100 0.9350 0.3600 0.5100 0.5700 W30X191 W30X99 W36X300 W8X10 W8X24 W8X31 W8X40 W8X58 W8X67 STEEL STEEL STEEL STEEL STEEL STEEL I/Wide Flange I/Wide Flange 35.9000 36.5000 12.1000 0.6000 0.8300 0.2450 Page 22 of 43 SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Section Properties 01 - General, Part 2 of 7 Table; SectionNnme t2b in Frame Section Properties 01 - General, Part 2 of 7 Area TorsConst I33 I22 in in2 iri4 in4 in4 in4 0.42 15.10 5.470E-02 11.30 11.30 6.66 716.00 53.80 236.00 0.00 2.18 272.00 394.00 534.00 93.40 134.00 0.00 0.00 0.00 1240.00 398.00 88.60 103.00 2.36 2.82 W10X112 W10X12 10.4000 1.2500 4.75 32.90 3.9600 0.2100 3.54 W10X49 10.0000 10.1000 0.5600 14.40 20.00 10.3000 0.9900 1.2500 0.2250 L5X5X1/2 W10X68 W10X88 W12X136 W12X14 W12X16 12.4000 3.9700 3.9900 4.0100 W12X19 W12X190 W12X65 12.7000 12.0000 W12X96 W14X109 W14X132 12.2000 14.6000 14.7000 W14X159 W14X211 W14X22 15.6000 W14X257 16.0000 16.2000 W14X311 W14X370 W14X426 W14X90 W16X26 W16X31 W18X119 W18X35 W18X40 W18X55 W18X65 W18X76 W18X97 W21X44 W21X50 W24X103 15.8000 5.0000 16.5000 16.7000 14.5000 5.5000 5.5300 11.3000 6.0000 6.0200 7.5300 7.5900 11.0000 11.1000 6.5000 6.5300 W24X117 9.0000 12.8000 W24X131 12.9000 W24X146 W24X162 12.9000 123 tfb 0.7700 7.53 39.90 4.16 18.50 7.040E-02 0.10 4.71 1.7400 0.6050 0.9000 55.80 0.8600 1.0300 1.1900 1.5600 32.00 38.80 2.2600 2.6600 3.0400 0.7100 0.3450 0.4400 1.0600 0.4250 0.5250 0.6300 0.7500 0.6800 0.8700 0.4500 0.5350 0.9800 0.8500 3.56 25.90 0.2650 0.3500 0.3350 1.8900 1.39 5.57 19.10 28.20 0.18 48.80 2.18 6.85 7.12 12.30 179.00 130.00 3.76 589.00 174.00 0.00 270.00 447.00 548.00 0.00 0.00 748.00 1030.00 7.00 0.00 0.00 0.00 0.00 0.00 533.00 833.00 1240.00 1530.00 1900.00 6.49 75.60 91.40 109.00 79.10 136.00 222.00 3400.00 4330.00 5440.00 1290.00 1610.00 125.00 26.50 7.68 331.00 6600.00 999.00 301.00 9.13 35.10 10.30 0.46 10.60 0.51 375.00 2190.00 2360.00 362.00 9.59 12.40 11.80 16.20 19.10 0.81 1.66 2.73 612.00 890.00 22.30 28.50 13.00 2.83 5.86 0.77 14.70 1.14 30.30 34.40 7.07 6.72 4.06 0.26 0.00 0.00 0.00 1890.00 19.70 44.60 0.21 46.70 62.00 0.00 0.00 2660.00 199.00 510.00 1070.00 1330.00 1990.00 253.00 15.30 19.10 44.90 54.80 152.00 1750.00 843.00 984.00 201.00 20.70 3000.00 3540.00 4020.00 119.00 297.00 24.90 340.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 38.50 9.50 43.00 47.70 13.40 18.50 4580.00 391.00 5170.00 1.3400 1.5700 51.70 60.70 5680.00 443.00 479.00 0.00 1.8900 73.50 23.90 38.30 66.60 0.00 0.00 98.40 16.30 152.00 1.24 11900.00 578.00 724.00 1030.00 18.30 1.77 29.10 34.50 0.00 0.5900 0.5850 1360.00 1560.00 20.10 0.00 0.6800 22.40 82.50 0.6400 W27X94 9.9900 0.7450 24.80 27.70 1830.00 2100.00 2850.00 70.40 8.9900 9.9600 1.87 2.68 4.03 W30X108 W30X116 10.5000 0.7600 0.8500 31.70 4.99 3270.00 4470.00 0.00 0.00 0.00 34.20 6.43 4930.00 0.9600 1.0900 1.2200 W24X176 13.0000 12.9000 W24X207 W24X250 13.0000 13.2000 W24X335 13.5000 2.4800 7.0100 7.0400 0.5050 W24X55 W24X62 W24X68 W24X76 W27X84 8.9700 10.5000 2.81 6820.00 8490.00 106.00 124.00 146.00 164.00 0.00 0.00 0.00 0.00 0.00 Page 23 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: SectionName Frame Section Properties 01 - General, Part 2 of 7 tfb Area TorsConst I33 I22 in in 1.1800 in2 in4 in4 in4 in4 43.50 51.00 14.50 15.60 6680.00 227.00 598.00 56.30 29.10 21.00 3.77 34.70 38.30 5.30 9200.00 3990.00 5900.00 0.00 0.00 0.00 39.70 44.20 7.00 W30X148 10.5000 W30X173 15.0000 15.0000 1.0700 10.5000 0.6700 0.7400 W30X191 W30X99 W33X118 W33X130 123 t2b 11.5000 11.5000 1.1900 0.8550 W36X135 W36X150 12.0000 0.7900 12.0000 W36X194 12.1000 0.9400 1.2600 W36X210 W36X230 12.2000 16.5000 W36X260 16.6000 W36X300 7.37 57.00 10.10 22.20 8230.00 6710.00 7800.00 9040.00 12100.00 1.3600 1.2600 1.4400 61.80 28.00 67.60 76.50 28.60 41.50 1.6800 88.30 W8X10 16.7000 3.9400 0.2050 W8X24 W8X31 W8X40 W8X58 6.5000 8.0000 8.0700 8.2200 0.4000 0.4350 2.96 7.08 64.20 4.260E-02 0.35 110.00 146.00 228.00 W8X67 8.2800 0.54 1.12 3.33 5.05 0.5600 0.8100 0.9350 9.12 11.70 17.10 19.70 13200.00 15000.00 673.00 128.00 187.00 218.00 225.00 270.00 375.00 411.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 0.00 20300.00 940.00 1090.00 1300.00 30.80 82.70 2.09 18.30 0.00 0.00 0.00 17300.00 272.00 37.10 49.10 75.10 88.60 0.00 0.00 0.00 0.00 0.00 Table: Frame Section Properties 01 - General, Part 3 of 7 Table: Frame Section Properties 01 - General, Part 3 of 7 AS3 in2 S33 S22 Z33 in2 in3 in3 in3 L5X5X1/2 2.50 2.50 3.16 3.16 5.68 W10X112 W10X12 8.61 1.88 147.00 12.60 3.39 125.61 10.90 54.51 75.77 98.89 45.38 W10X49 W10X68 W10X88 W12X136 21.67 1.39 9.33 12.96 SectionName AS2 4.89 6.53 10.59 17.00 25.83 1.10 18.68 26.53 34.76 185.07 64.19 14.89 17.17 1.19 1.41 1.88 92.76 2.38 1.49 2.64 2.87 1.76 2.34 15.26 4.72 6.99 36.83 12.10 262.50 88.10 18.30 131.18 7.51 20.93 9.48 11.18 25.24 30.94 173.43 208.16 253.33 95.90 W14X211 W14X22 W14X257 15.39 3.15 41.08 2.79 50.40 338.85 130.38 2.80 W14X311 24.11 29.71 61.02 506.43 73.15 607.82 W14X426 W14X90 35.16 84.61 6.16 W16X26 3.92 W16X31 4.37 12.44 5.31 5.64 5.27 W12X14 W12X16 W12X19 W12X190 W12X65 W12X96 W14X109 W14X132 W14X159 W14X370 W18X119 W18X35 W18X40 19.35 21.31 29.00 44.26 61.23 60.40 85.30 113.00 214.00 17.40 20.10 24.70 311.00 96.80 147.00 192.00 Z22 in3 5.68 69.20 1.74 28.30 40.10 53.10 98.00 1.90 2.26 R33 lllillll! 1.5424 4.6651 3.8984 4.3461 4.4385 4.5407 5.5747 4.6150 4.6764 2.98 143.00 44.10 67.50 4.8311 92.70 6.2249 6.2796 5.8199 5.2826 5.4350 234.00 287.00 390.00 113.00 146.00 198.00 6.3785 33.20 4.39 5.5374 161.25 487.00 246.00 603.00 304.00 6.7062 6.8829 705.88 198.77 241.21 282.63 736.00 869.00 370.00 434.00 7.2664 17.16 3.16 142.71 38.34 49.93 3.49 157.00 75.60 6.1399 44.20 4.06 47.17 4.48 54.00 5.48 7.03 6.2604 6.4089 19.96 230.53 57.63 68.38 44.78 5.10 262.00 66.50 78.40 69.10 8.06 7.8989 4.25 9.95 7.2017 29.05 414.63 74.56 6.35 6.5501 7.0646 7.0367 Page 24 of 43 Jet way sap model_V11V12 7-29.sdb Table: ectionName _____ AS2 in2 74)6 SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Frame Section Properties 01 - General, Part 3 of 7 AS3 in2 S33 S22 Z33 Z22 in3 in3 in3 in3 R33 in 7.91 9.49 98.34 11.93 14.44 27.64 112.00 18.50 ~ 7.4120 133.00 163.00 22.50 W18X65 8.28 W18X76 7.74 9.95 7.24 12.47 116.30 146.15 16.09 4.88 188.17 81.45 36.22 211.00 55.30 7.4847 7.7228 7.8360 6.37 7.90 13.48 5.82 94.62 7.63 95.40 110.00 10.20 12.20 8.1816 14.70 18.13 244.90 291.36 26.44 46.41 280.00 327.00 20.64 23.43 26.43 328.16 370.00 370.85 413.60 52.71 60.62 68.15 41.50 71.40 81.50 93.20 28.81 34.02 450.79 74.26 418.00 468.00 511.00 10.1443 10.2184 10.3204 105.00 115.00 10.4108 10.4816 530.74 88.92 10.5998 645.63 171.00 55.80 865.45 115.25 109.70 152.59 606.00 744.00 137.00 41.58 1020.00 238.00 10.7476 10.9970 8.30 9.80 135.00 154.00 9.1343 15.70 177.00 200.00 244.00 278.00 13.40 15.80 24.50 28.60 33.20 38.80 9.6825 10.7200 10.8651 11.8747 12.0063 12.3921 W18X97 W21X44 W21X50 W24X103 W24X117 W24X131 W24X146 W24X162 W24X176 W24X207 W24X250 W24X335 W24X55 W24X62 W24X68 13.36 14.82 16.06 17.63 18.90 22.36 27.35 37.95 9.32 10.19 9.84 W24X76 W27X84 W27X94 10.52 12.28 W30X108 16.24 16.95 19.95 19.91 W30X116 W30X148 W30X173 W30X191 W30X99 W33X118 W33X130 W36X135 W36X150 W36X194 W36X210 W36X230 W36X260 W36X300 13.18 21.80 15.44 18.09 19.20 21.36 22.44 27.92 30.46 27.28 30.49 34.68 W8X10 W8X24 W8X31 W8X40 1.34 W8X58 W8X67 4.46 5.13 1.94 2.28 2.97 5.90 6.92 131.65 8.75 10.19 154.43 175.73 10.62 12.40 13.30 14.88 213.48 243.12 20.65 26.75 29.75 11.73 435.18 541.45 599.35 268.69 14.18 16.39 358.66 405.44 300.00 328.67 18.35 21.29 24.82 42.20 9.9504 9.2329 9.5417 27.81 31.24 43.24 500.00 43.90 49.20 68.00 79.73 89.73 24.38 607.00 675.00 312.00 123.00 138.00 38.60 12.7032 32.52 415.00 467.00 509.00 51.30 70.90 97.70 13.0395 13.2362 14.0169 14.3012 346.00 378.00 59.50 59.70 15.80 438.20 37.91 37.50 18.80 25.41 27.65 503.62 663.01 719.35 45.00 61.98 67.38 581.00 767.00 833.00 34.65 39.84 46.76 835.65 953.17 1106.27 1080.00 1260.00 1.35 4.33 5.80 7.81 20.86 27.50 113.94 131.33 155.69 1.06 8.87 176.00 204.00 241.00 1.66 5.63 9.27 23.10 30.40 8.57 14.10 7.53 11.10 12.90 35.39 12.17 18.27 21.40 39.80 18.50 27.90 32.70 52.11 60.44 8.0527 943.00 59.80 70.10 107.00 12.7832 11.7095 14.5699 14.6148 14.8961 15.0381 15.1624 3.2257 3.4177 3.4730 3.5325 3.6515 3.7158 Table: Frame Section Properties 01 - General, Part 4 of 7 Table: SectionName R22 Frame Section Properties 01 - General, Part 4 of 7 Color ConcCol ConcBe.im EccV2 in in L5X5X1/2 1.5424 0.0000 W10X112 2.6783 0.0000 W10X12 W10X49 0.7847 2.5468 0.0000 0.0000 W10X68 2.5884 0.0000 TotalWt TotalMass Kip Kip-s2/in No No No No Red Cyan 1.616 0.000 0.0042 No No 0.000 0.0000 No No No No White Gray8Dark 0.000 0.000 0.0000 Blue 0.0000 0.0000 Page 25 of 43 Jet way sap model_V11_V12 7-29.sdb SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Table: Frame Section Properties 01 - General, Part 4 of 7 SectionName R22 EccV2 Musm 0.0000 0.0000 ConcCol ConcBeam Color TotalWt Kip TotalMass No No No No No No Green Blue 0.000 0.000 Red Magenta 0.000 0.0000 0.0000 0.0000 Kip-s2/in W12X14 2.6289 3.1583 0.7532 0.0000 No W12X16 0.7738 0.0000 No W12X19 0.8216 Yellow 0.000 0.000 0.0000 0.0000 3.2489 No No No W12X190 W12X65 W12X96 0.0000 0.0000 No Green 0.000 0.0000 3.0183 3.0943 3.7375 0.0000 No No 0.000 0.0000 0.0000 0.0000 No No No No White Gray8Dark 0.000 Magenta 0.0000 0.0000 3.7582 4.0021 0.0000 0.0000 No No W14X211 4.0759 0.0000 No No No No 0.000 0.000 White Gray8Dark W14X22 W14X257 1.0385 4.1308 Cyan 4.1970 No No No No W14X311 0.0000 0.0000 0.0000 No No W14X370 W14X426 4.2728 W14X90 No No No No 4.3451 3.6960 0.0000 0.0000 0.0000 Blue Green Cyan W16X26 W16X31 1.1175 1.1654 0.0000 0.0000 No No W18X119 W18X35 2.6848 0.0000 No No No No 1.2188 1.2723 1.6648 0.0000 0.0000 0.0000 No No 1.6938 2.6108 2.6557 0.0000 0.0000 0.0000 No No No No W21X44 W21X50 W24X103 1.2619 1.3015 1.9818 0.0000 0.0000 0.0000 No No No W24X117 W24X131 2.9383 0.0000 No W24X146 2.9717 3.0155 0.0000 0.0000 No No W24X162 W24X176 W24X207 3.0475 3,0438 3.0858 0.0000 0.0000 No No 0.0000 No W24X250 W24X335 3.1385 3.2353 1.3361 0.0000 0.0000 No No 0.0000 No 0.0000 0.0000 No W10X88 W12X136 W14X109 W14X132 W14X159 W18X40 W18X55 W18X65 W18X76 W18X97 W24X55 W24X62 W24X68 1.3730 No No Yellow Red Red Magenta Yellow Gray8Dark No No No Green Cyan No No Magenta Yellow No White Blue No No No No No No No No No No No No No No No No Red Green White Gray8Dark Blue 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 Red Magenta 0.000 0.000 0.000 0.000 Yellow White Cyan 0.000 0.000 0.000 0.0000 0.0000 Red Magenta 0.000 0.000 Yellow Gray8Dark 0.000 0.0000 0.0000 0.0000 Blue Cyan 0.000 0.000 Red Magenta 0.000 0.000 Green Cyan 0.0000 0.0000 0.0000 0.0000 W24X76 1.8715 1,9191 0.0000 No No W27X84 2.0674 0.0000 No W27X94 W30X108 2.1158 0.0000 0.0000 No No No W30X116 0.0000 No No W30X148 W30X173 2.1898 2.2844 0.0000 No 3.4243 0.0000 No No No Yellow 0.000 W30X191 3.4574 White 0.000 2.0973 No No No W30X99 W33X118 0.0000 0.0000 No 0.0000 No No Green Gray8Dark 0.000 0.000 0.0000 W33X130 2.3214 2.3858 0.0000 No Blue 0.000 0.0000 W36X135 W36X150 2.3807 0.0000 No 2.4716 0.0000 No No No No Green Cyan 0.000 0.000 0.0000 0.0000 2.1461 No 0.000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 0.0000 Page 26 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Section Properties 01 - General, Part 4 of 7 ConcBeam Color ConcCol EccV2 R22 SectionName in W36X194 2.5649 0.0000 W36X210 W36X230 2.5789 3.7290 0.0000 W36X260 3.7747 3.8370 0.8403 W36X300 W8X10 W8X24 W8X31 W8X40 W8X58 W8X67 1.6077 0.0000 0.0000 No 0.0000 0.0000 0.0000 No No 2.0169 2.0486 0.0000 2.0957 0,0000 0.0000 2.1207 No No 0.0000 No No No No No No Red TotalWt TotalMass Kip Kip-s2/in 0.000 0.000 0.000 0.0000 0.0000 0.000 0.0000 0.0000 0.0000 No No No Magenta No No White Gray8Dark No Blue 0.000 0.000 No Green Cyan 0.000 0.000 Red 0.000 0.0000 0.0000 0.0000 Magenta Yellow 0.000 0.000 0.0000 0.0000 Yellow No No No No 0.0000 Table: Frame Section Properties 01 - General, Part 5 of 7 Table: SectionName FromFile L5X5X1/2 W10X112 Yes Yes W10X12 W10X49 W10X68 W10X88 Yes Yes Yes Yes Frame Section Properties 01 - General, Part 5 of 7 AMod A2Mod A3Mod JMod l2Mod l3Mod 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 W12X14 W12X16 Yes Yes Yes W12X19 W12X190 Yes Yes 1.000000 1.000000 W12X65 W12X96 W14X109 W14X132 Yes Yes 1.000000 W14X159 W14X211 W14X22 Yes Yes Yes W14X257 W14X311 W14X370 Yes Yes Yes W14X426 W14X90 W16X26 Yes Yes Yes W16X31 W18X119 Yes Yes 1.000000 1.000000 W18X35 Yes 1.000000 W18X40 Yes Yes 1.000000 W12X136 Yes Yes 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 W18X65 W18X76 Yes 1.000000 1.000000 1.000000 1.000000 Yes 1.000000 1.000000 1.000000 1.000000 1.000000 W18X97 Yes 1.000000 1.000000 Yes Yes 1.000000 1.000000 1.000000 1.000000 W21X44 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 Yes 1.000000 1.000000 1.000000 1.000000 Yes 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 W18X55 W21X50 W24X103 W24X117 1.000000 1.000000 1.000000 1.000000 1.000000 Page 27 of 43 SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Section Properties 01 - General, Part 5 of 7 AMod A2Mod A3Mod JMod l2Mod l3Mod Yes Yes Yes 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 W24X176 W24X207 Yes 1.000000 1.000000 1.000000 1.000000 Yes 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 W24X250 Yes 1.000000 1.000000 1.000000 1.000000 1.000000 Yes Yes Yes 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 W24X335 1.000000 1.000000 1.000000 1.000000 1.000000 Yes Yes Yes 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 Yes Yes 1.000000 1.000000 1.000000 1.000000 Yes 1.000000 1.000000 1.000000 Yes Yes 1.000000 1.000000 Yes 1.000000 1.000000 SectionName FromFile W24X131 W24X146 W24X162 W24X55 W24X62 W24X68 W24X76 W27X84 W27X94 W30X108 W30X116 W30X148 W30X173 W30X191 W30X99 W33X118 Yes Yes 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 Yes Yes Yes 1.000000 1.000000 1.000000 W36X300 W8X10 W8X24 Yes 1.000000 1.000000 W8X58 W8X67 1.000000 1.000000 1.000000 1.000000 W36X210 W36X230 W36X260 Yes Yes Yes Yes 1.000000 1.000000 1.000000 1.000000 1.000000 Yes Yes Yes Yes W8X31 W8X40 1.000000 1.000000 1.000000 1.000000 1.000000 W33X130 W36X135 W36X150 W36X194 Yes Yes 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 1.000000 Table: Frame Section Properties 01 - General, Part 6 of 7 Table: Frame Section Properties 01 - General, Part 6 of 7 MMod WMod ScctlnFilc FileNamc L5X5X1/2 1.000000 1.000000 L5X5X1/2 c:\program files\computers and structures\sap2000 10 demo\aisc.pro W10X112 1.000000 1.000000 W10X112 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W10X12 1.000000 1.000000 W10X12 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W10X49 1.000000 1.000000 W10X49 W10X68 1.000000 1.000000 W10X68 C:\Program FilesVComputers and Structures\SAP2000 10 Demo\Sections8.pro C:\Program FilesVComputers and Structures\SAP2000 10 Demo\Sections8.pro SectionName GUID Page 28 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: SectionName Frame Section Properties 01 - General, Part 6 of 7 MMod WMod SectlnFile FileName W10X88 1.000000 1.000000 W10X88 C:\PrograrnFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W12X136 1.000000 1.000000 W12X136 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W12X14 1.000000 1.000000 W12X14 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W12X16 1.000000 1.000000 W12X16 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W12X19 1.000000 1.000000 W12X19 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W12X190 1.000000 1.000000 W12X190 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W12X65 1.000000 1.000000 W12X65 W12X96 1.000000 1.000000 W12X96 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W14X109 1.000000 1.000000 W14X109 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W14X132 1.000000 1.000000 W14X132 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W14X159 1,000000 1.000000 W14X159 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sectlons8.pro W14X211 1.000000 1.000000 W14X211 W14X22 1.000000 1.000000 W14X22 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W14X257 1.000000 1.000000 W14X257 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W14X311 1.000000 1.000000 W14X311 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W14X370 1.000000 1.000000 W14X370 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W14X426 1.000000 1.000000 W14X426 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W14X90 1.000000 1.000000 W14X90 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W16X26 1.000000 1.000000 W16X26 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W16X31 1.000000 1.000000 W16X31 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro GUID Page 29 of 43 SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Section Properties 01 - General, Part 6 of 7 MMod WMod SectlnFile FileName W18X119 1.000000 1.000000 W18X119 W18X35 1.000000 1.000000 W18X35 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W18X40 1.000000 1.000000 W18X40 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W18X55 1.000000 1.000000 W18X55 W18X65 1.000000 1.000000 W18X65 W18X76 1.000000 1.000000 W18X76 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W18X97 1.000000 1.000000 W18X97 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sectlons8.pro W21X44 1.000000 1.000000 W21X44 W21X50 1.000000 1.000000 W21X50 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W24X103 1.000000 1.000000 W24X103 W24X117 1.000000 1.000000 W24X117 W24X131 1.000000 1.000000 W24X131 W24X146 1.000000 1.000000 W24X146 W24X162 1.000000 1.000000 W24X162 W24X176 1.000000 1.000000 W24X176 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W24X207 1.000000 1.000000 W24X207 W24X250 1.000000 1.000000 W24X250 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W24X335 1.000000 1.000000 W24X335 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W24X55 1.000000 1.000000 W24X55 W24X62 1.000000 1.000000 W24X62 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro SectionName GUID C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro Page 30 of 43 SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Section Properties 01 - General, Part 6 of 7 SectionName MMod WMod SectlnFile FileName W24X68 1.000000 1.000000 W24X68 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W24X76 1.000000 1.000000 W24X76 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W27X84 1.000000 1.000000 W27X84 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W27X94 1.000000 1.000000 W27X94 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W30X108 1.000000 1.000000 W30X108 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W30X116 1.000000 1.000000 W30X116 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W30X148 1.000000 1.000000 W30X148 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W30X173 1.000000 1.000000 W30X173 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sectlons8.pro W30X191 1.000000 1.000000 W30X191 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W30X99 1.000000 1.000000 W30X99 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W33X118 1.000000 1.000000 W33X118 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W33X130 1.000000 1.000000 W33X130 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W36X135 1.000000 1.000000 W36X135 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W36X150 1.000000 1.000000 W36X150 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W36X194 1.000000 1.000000 W36X194 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W36X210 1.000000 1.000000 W36X210 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W36X230 1.000000 1.000000 W36X230 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W36X260 1.000000 1.000000 W36X260 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W36X300 1.000000 1.000000 W36X300 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W8X10 1.000000 1.000000 W8X10 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro GUID Page 31 of 43 Jet way sap model_V11_V12 7-29.sdb SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Table: SectionName Frame Section Properties 01 - General, Part 6 of 7 MMod WMod SectlnFile FileName W8X24 1.000000 1.000000 W8X24 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W8X31 1.000000 1.000000 W8X31 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro W8X40 1.000000 1.000000 W8X40 C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro W8X58 1.000000 1.000000 W8X58 W8X67 1.000000 1.000000 W8X67 C:\ProgramFiles\Computersand Structures\SAP2000 10 Demo\Sections8.pro C:\Program Files\Computers and Structures\SAP2000 10 Demo\Sections8.pro GUID Table: Frame Section Properties 01 - General, Part 7 of 7 Table: Frame Section Properties 01 - General, Part 7 of 7 SectionName Notes | L5X5X1/2 W10X112 W10X12 W10X49 W10X68 W10X88 W12X136 W12X14 W12X16 W12X19 W12X190 W12X65 W12X96 W14X109 W14X132 W14X159 W14X211 W14X22 W14X257 W14X311 W14X370 W14X426 W14X90 W16X26 W16X31 W18X119 W18X35 W18X40 W18X55 W18X65 W18X76 W18X97 W21X44 W21X50 Page 32 of 43 SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Frame Section Properties 01 - General, Part 7 of7 SectionName Notes W24X103 W24X117 W24X131 W24X146 W24X162 W24X176 W24X207 W24X250 W24X335 W24X55 W24X62 W24X68 W24X76 W27X84 W27X94 W30X108 W30X116 W30X148 W30X173 W30X191 W30X99 W33X118 W33X130 W36X135 W36X150 W36X194 W36X210 W36X230 W36X260 W36X300 W8X10 W8X24 W8X31 W8X40 W8X58 W8X67 Table: Joint Coordinates, Part 1 of 2 Table: Joint Coordinates, Part 1 of 2 Joint CoordSys CcordTypo SpccialJt XorR in in 3 4 GLOBAL GLOBAL Cartesian 0.000 0.000 Cartesian 300.000 2.939E-15 5 GLOBAL Cartesian 0.000 83.000 6 GLOBAL 7 8 GLOBAL Cartesian Cartesian 300.000 0.000 83.000 0.000 Cartesian Cartesian 300.000 2.939E-15 9 GLOBAL GLOBAL 0.000 83.000 10 GLOBAL Cartesian 300.000 83.000 11 12 GLOBAL GLOBAL Cartesian Cartesian 12.000 24.000 13 GLOBAL Cartesian 36.000 0.000 0.000 0.000 GlobalX in 0.000 0.000 0.000 0.000 Yes 0.000 Yes No 300.000 0.000 No 300.000 120.000 No 0.000 120.000 120.000 120.000 No No No 300.000 0.000 0.000 Yes Yes 0.000 Yes 0.000 300.000 12.000 24.000 36.000 Page 33 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Joint Coordinates, Part 1 of 2 Joint CoordSys 14 15 GLOBAL 16 GLOBAL GLOBAL 17 18 19 GLOBAL GLOBAL GLOBAL GLOBAL CoordType Cartesian Cartesian Cartesian 108.000 0.000 120.000 132.000 144.000 0.000 0.000 0.000 0.000 Yes 0.000 0.000 Yes Yes 132.000 156.000 168.000 0.000 0.000 0.000 Yes 156.000 168.000 180.000 0.000 0.000 0.000 192.000 0.000 0.000 Yes 192.000 204.000 216.000 0.000 0.000 0.000 Yes Yes 204.000 216.000 228.000 0.000 0.000 0.000 0.000 Yes 228.000 0.000 0.000 0.000 Yes Yes 240.000 252.000 Yes Yes Yes 264.000 0.000 0.000 120.000 120.000 120.000 Yes Yes Yes 12.000 24.000 120.000 120.000 120.000 Yes 120.000 120.000 Yes Yes Yes 24 25 GLOBAL GLOBAL 26 GLOBAL 27 GLOBAL GLOBAL Cartesian Cartesian Cartesian Cartesian Cartesian Cartesian 32 33 34 GLOBAL Cartesian Cartesian GLOBAL GLOBAL Cartesian Cartesian 83 84 85 86 GLOBAL GLOBAL GLOBAL GLOBAL Cartesian Cartesian 92 GLOBAL GLOBAL 93 94 GLOBAL GLOBAL 95 96 GLOBAL GLOBAL 97 GLOBAL 98 GLOBAL 99 100 GLOBAL GLOBAL 101 102 GLOBAL 103 GLOBAL GLOBAL Yes Yes 108.000 120.000 144.000 180.000 0.000 0.000 Cartesian 288.000 12.000 24.000 36.000 0.000 0.000 0.000 0.000 Cartesian Cartesian 48.000 60.000 0.000 0.000 Cartesian Cartesian Cartesian Cartesian 72.000 84.000 0.000 0.000 96.000 108.000 0.000 0.000 Cartesian Cartesian Cartesian 120.000 132.000 144.000 0.000 0.000 0.000 Cartesian Cartesian Cartesian 156.000 168.000 180.000 0.000 0.000 0.000 Cartesian Cartesian 192.000 204.000 216.000 0.000 228.000 240.000 252.000 0.000 120.000 120.000 120.000 0.000 0.000 120.000 120.000 Yes Yes 264.000 0.000 276.000 288.000 0.000 0.000 120.000 120.000 Yes Yes 252.000 264.000 276.000 120.000 Yes 288.000 12.000 24.000 36.000 83.000 83.000 0.000 Yes Yes Yes 12.000 24.000 83.000 0.000 0.000 36.000 48.000 83.000 0.000 Yes 48.000 83.000 83.000 0.000 Yes 0.000 Yes 60.000 72.000 83.000 0.000 0.000 Yes Yes 96.000 83.000 0.000 Yes 108.000 Cartesian Cartesian Cartesian Cartesian Cartesian Cartesian Cartesian 107 GLOBAL GLOBAL 108 GLOBAL Cartesian 109 GLOBAL 110 111 GLOBAL Cartesian Cartesian 105 106 240.000 252.000 0.000 Yes 264.000 276.000 GLOBAL GLOBAL 104 84.000 96.000 Cartesian Cartesian 89 90 91 72.000 Yes Cartesian GLOBAL GLOBAL GLOBAL GLOBAL Yes Yes 0.000 0.000 GLOBAL 87 88 48.000 60.000 0.000 Cartesian 31 0.000 0.000 in Yes Yes 96.000 GLOBAL GLOBAL GLOBAL 0.000 GlobalX 0.000 GLOBAL GLOBAL SpecialJt 0.000 22 23 28 z in 84.000 21 29 30 fsiifisili in IJlllllliirKllll 48.000 0.000 60.000 0.000 72.000 0.000 Cartesian Cartesian Cartesian Cartesian 20 XorR Cartesian Cartesian 60.000 112 113 114 GLOBAL GLOBAL Cartesian GLOBAL Cartesian 72.000 84.000 GLOBAL 115 GLOBAL Cartesian Cartesian 96.000 108.000 0.000 0.000 83.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes 276.000 288.000 36.000 48.000 60.000 72.000 84.000 96.000 108.000 120.000 132.000 144.000 156.000 168.000 180.000 192.000 204.000 216.000 228.000 240.000 84.000 Page 34 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Joint CoordSys Joint Coordinates, Part 1 of 2 CoordType XorR in 116 117 118 GLOBAL GLOBAL GLOBAL Cartesian 120.000 132.000 144.000 Cartesian Cartesian mmmsm Y 83.000 0.000 83.000 0.000 0.000 83.000 Cartesian Cartesian 156.000 83.000 168.000 Cartesian 180.000 83.000 83.000 GLOBAL GLOBAL Cartesian Cartesian Cartesian 192.000 204.000 GLOBAL GLOBAL Cartesian Cartesian GLOBAL Cartesian 128 129 130 GLOBAL GLOBAL Cartesian 131 GLOBAL GLOBAL 119 120 GLOBAL 121 GLOBAL GLOBAL 122 123 124 125 126 127 132 133 134 135 136 137 138 139 140 141 142 143 144 145 146 147 148 149 150 151 152 153 154 GLOBAL GLOBAL Cartesian GLOBAL Cartesian Cartesian GLOBAL GLOBAL Cartesian Cartesian GLOBAL GLOBAL Cartesian Cartesian Cartesian Cartesian GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL GLOBAL Cartesian Cartesian Cartesian Cartesian Cartesian Cartesian GLOBAL Cartesian Cartesian Cartesian GLOBAL GLOBAL GLOBAL Cartesian Cartesian Cartesian GLOBAL GLOBAL GLOBAL Cartesian Cartesian Cartesian GLOBAL GLOBAL SpecialJt GlobalX Yus Yes 120.000 132.000 Yes 144.000 Yes 156.000 Yes 168.000 180.000 in 0.000 0.000 0.000 Yes Yes Yes 192.000 83.000 83.000 83.000 0.000 228.000 240.000 252.000 83.000 83.000 83.000 0.000 0.000 0.000 264.000 276.000 83.000 0.000 Yes 83.000 0.000 83.000 12.000 24.000 83.000 83.000 0.000 120.000 Yes Yes 276.000 288.000 Yes 12.000 24.000 36.000 83.000 48.000 60.000 72.000 216.000 Cartesian Cartesian Z in 0.000 0.000 216.000 228.000 Yes 240.000 252.000 264.000 Yes 120.000 120.000 Yes Yes 83.000 83.000 83.000 120.000 Yes Yes 84.000 96.000 108.000 83.000 83.000 83.000 120.000 120.000 120.000 120.000 132.000 144.000 83.000 83.000 83.000 120.000 156.000 83.000 168.000 180.000 83.000 83.000 192.000 204.000 216.000 228.000 83.000 83.000 83.000 83.000 240.000 252.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 204.000 Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes 120.000 120.000 120.000 Yes Yes 120.000 120.000 120.000 Yes Yes 264.000 83.000 83.000 83.000 276.000 288.000 83.000 83.000 120.000 120.000 Yes Yes Yes Yes 288.000 36.000 48.000 60.000 72.000 84.000 96.000 108.000 120.000 132.000 144.000 156.000 168.000 180.000 192.000 204.000 216.000 228.000 240.000 252.000 264.000 276.000 288.000 Table: Joint Coordinates, Part 2 of 2 Table: Joint Joint Coordinates, Part 2 of 2 GlobnIY GlobnIZ 3 4 0.000 2.939E-15 0.000 5 83.000 6 83.000 0.000 7 8 0.000 120.000 2.939E-15 83.000 83.000 120.000 120.000 9 10 GUID 0.000 0.000 120.000 Page 35 of 43 Jet way sap model_V11_V12 7-29.sdb Table: Joint Joint Coordinates, Part 2 of 2 GlobalY GlobalZ in in 0.000 13 0.000 0.000 0.000 14 0.000 15 16 0.000 0.000 0.000 0.000 0.000 17 18 0.000 0.000 0.000 0.000 0.000 0.000 11 12 19 20 0.000 0.000 0.000 0.000 22 23 0.000 0.000 0.000 0.000 0.000 0.000 24 0.000 0.000 0.000 0.000 0.000 0.000 0.000 21 25 26 27 0.000 28 0.000 0.000 29 30 0.000 0.000 31 32 0.000 0.000 0.000 0.000 0.000 0.000 0.000 85 86 87 88 0.000 0.000 0.000 120.000 120.000 120.000 0.000 0.000 0.000 120.000 89 0.000 90 91 0.000 0.000 120.000 120.000 92 93 0.000 0.000 0.000 120.000 120.000 120.000 120.000 97 0.000 0.000 0.000 98 0.000 99 100 0.000 0.000 120.000 120.000 101 0.000 120.000 102 0.000 103 104 0.000 120.000 120.000 0.000 0.000 120.000 106 0.000 120.000 107 83.000 108 109 83.000 0.000 0.000 83.000 83.000 0.000 111 83.000 0.000 112 83.000 0.000 33 34 83 84 94 95 96 105 110 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 0.000 0.000 0.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 0.000 Page 36 of 43 SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Joint Joint Coordinates, Part 2 of 2 GlobalY in 113 114 115 83.000 83.000 83.000 83.000 GlobalZ in 0.000 0.000 0.000 117 118 83.000 0.000 0.000 83.000 0.000 119 120 121 83.000 0.000 83.000 83.000 0.000 122 83.000 123 83.000 83.000 116 124 125 126 127 128 129 130 83.000 83.000 83.000 83.000 83.000 83.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 120.000 120.000 133 134 83.000 83.000 83.000 83.000 135 136 83.000 83.000 120.000 120.000 120.000 120.000 137 138 139 140 83.000 83.000 120.000 120.000 83.000 83.000 120.000 141 142 83.000 83.000 83.000 83.000 131 132 143 144 145 146 147 148 149 150 151 152 153 154 83.000 83.000 83.000 83.000 83.000 83.000 83.000 83.000 83.000 83.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 120.000 Table: Joint Loads - Force, Part 1 of 2 Table: ' Joint LoadPat CoordSys is Live 27 114 123 Live Live Live Joint Loads - Force, Part 1 of 2 F1 Kip F2 Kip F3 Kip f.11 Kip-in M2 Kip-in , GLOBAL 0.000 0.000 -2.000 0.000 0.000 GLOBAL GLOBAL GLOBAL 0.000 0.000 0.000 0.000 0.000 0.000 -2.000 -2.000 -2.000 0.000 0.000 0.000 0.000 0.000 0.000 Page 37 of 43 Jet way sap model_V11_V12 7-29.sdb Table: Joint Loads - Force, Part 2 of 2 Table: Joint SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Joint Loads - Force, Part 2 of 2 LoadPat M3 GUID Kip-in 18 Live 0.000 27 114 Live Live 0.000 0.000 123 Live 0.000 Table: Joint Reactions Table: Joint Reactions oint 3 3 3 3 3 3 3 3 3 3 3 3 4 4 4 4 4 4 OutputCase CaseType UDSTL1 UDSTL2 UDSTL3 Combination UDSTL4 UDSTL5 UDSTL6 Combination UDSTL7 UDSTL8 UDSTL9 Combination Combination Combination Combination Combination Combination Combination UDSTL10 UDSTL11 UDSTL12 Combination UDSTL1 UDSTL2 UDSTL3 UDSTL4 Combination Combination UDSTL5 UDSTL6 Combination Combination Combination Combination Combination Combination Combination 4 4 4 UDSTL7 4 4 4 UDSTL10 UDSTL11 Combination Combination Combination Combination UDSTL12 UDSTL1 Combination Combination UDSTL2 Combination UDSTL3 Combination Combination 5 5 5 5 5 5 5 UDSTL8 UDSTL9 UDSTL4 UDSTL5 UDSTL6 UDSTL7 Combination Combination Combination F3 Kip F1 F2 Kip Kip 0.393 5.234 -0.032 0.807 -0.408 -8.129 7.598 -0.028 11.360 2.352 -8.511 15.306 0.337 0.337 -5.618 6.291 -11.656 12.161 0.281 3.341 -0.393 -5.234 8.554 -15.349 -0.337 -0.337 5.639 -6.312 11.699 -0.028 -3.960 3.904 -7.885 7.843 -0.023 -0.261 -0.073 -0.997 -8.455 7.162 -0.063 -0.063 -3.967 3.842 -7.855 -12.204 -0.281 7.761 -0.052 -3.341 -0.636 0.032 0.393 5.234 15.883 0.408 -7.259 -9.089 0.337 7.790 0.028 0.337 6.580 0.028 -3.734 3.790 12.367 0.692 0.692 M1 M2 M3 Kip- n Kip-in Kip-in -1.168E-06 -1.679E-05 254.193 0.000 0.000 0.000 0.000 0.000 0.000 -254.193 -1.001E-06 -1.001E-06 0.000 0.000 0.000 0.000 127.096 -127.096 5.527 0.577 7.244 -254.193 -8.343E-07 -1.070E-05 0.807 10.922 2.078 -1.506E-06 -2.077E-05 254.192 12.093 -254.192 -1.291E-06 -1.291E-06 0.000 0.000 127.096 0.000 0.000 0.000 0.000 0.692 0.692 -1.812 3.196 -4.488 254.193 -127.096 254.192 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 -254.192 -1.076E-06 -1.325E-05 1.168E-06 0.000 0.000 0.000 11.360 12.367 2.352 1.679E-05 0.000 254.193 0.000 0.000 0.692 0.692 1.001E-06 1.001E-06 0.000 0.000 0.000 0.000 0.000 0.000 3.196 127.096 0.000 0.000 -1.812 -127.096 254.193 0.000 0.000 0.000 -254.193 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 0.000 -254.193 5 5 UDSTL8 UDSTL9 Combination -5.906 12.738 -7.504 5.527 UDSTL10 Combination -12.233 7.545 5 UDSTL11 5 UDSTL12 Combination Combination -4.488 0.577 0.261 0.073 7.244 8.343E-07 1.070E-05 0.807 1.506E-06 2.077E-05 254.192 0.023 0.000 0.000 0.000 0.000 0.000 0.000 0.000 5.527 0.577 6.970 0.807 Combination 5 0.000 0.000 -1.812 3.196 -4.488 6 UDSTL1 Combination 0.281 3.341 -0.393 6 6 UDSTL2 UDSTL3 Combination Combination -5.234 -15.926 0.997 10.922 -6.957 6 UDSTL4 9.132 8.250 6 UDSTL5 Combination Combination 12.093 2.078 -0.337 0.063 0.692 0.000 0.000 0.000 -254.192 0.000 0.000 0.000 0.000 0.000 1.291E-06 0.000 0.000 Page 38 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Joint OutputCase CaseType Joint Reactions F1 F2 F3 Kip Kip Kip M1 Kip-in M2 M3 Kip-in Kip-in 0.692 3.196 -1.812 1.291E-06 127.096 -127.096 0.000 0.000 0.000 0.000 0.000 0.000 6 UDSTL6 Combination -0.337 6 6 UDSTL7 Combination Combination -6.601 5.928 0.063 -3.739 3.864 6 6 Combination Combination -12.781 -7.557 5.527 254.192 0.000 12.276 7.651 Combination -0.281 0.000 0.000 0.000 0.000 0.000 6 UDSTL12 Combination -3.341 0.052 0.636 -4.488 0.577 -254.192 6 UDSTL9 UDSTL10 UDSTL11 0.000 0.000 UDSTL8 6.970 1.076E-06 1.325E-05 Table: Load Case Definitions, Part 1 of 2 Table: Load Case Definitions, Part 1 of 2 Case Type InitialCond DEAD MODAL LinStatic LinModal Zero Zero Zero Zero Zero Live WIND SNOW LinStatic LinStatic LinStatic ModalCase BaseCase DesTypeOpt DesignType DesActOpt Prog Det Prog Det Prog Det Prog Det Prog Det DEAD Prog Det OTHER LIVE WIND Prog Det LIVE Prog Det Prog Det Prog Det Table: Load Case Definitions, Part 2 of 2 Table: Load Case Definitions, Part 2 of 2 Case DesignAct AutoType RunCase CaseStatus DEAD Non-Compos ite None Yes Finished MODAL Live Other Short-Term Composite None None No Yes Finished WIND Short-Term Composite None Yes Finished SNOW Short-Term Composite None Yes Finished GUID Notes Not Run Table: Material Properties 01 - General Table: Material Properties 01 - General Material Type SymType TempDepen ••taiMi Color A416Gr270 Tendon Uniaxial No Yellow ALUM Aluminum isotropic No Yellow CLDFRM ColdFormed Isotropic No White CONC Concrete Isotropic No Magenta OTHER REBAR Other Rebar isotropic Uniaxial No No Gray8Dark STEEL Steel Isotropic No Red Blue GUID ASTM A416 Grade 270 added 7/24/2014 9:52:46 AM Aluminum Alloy 6061 T6 added 7/24/2014 9:52:46 AM ASTM A653 SQ Grade 50 added 7/24/2014 9:52:46 AM Normalweight fc = 4 ksi added 7/24/2014 9:52:46 AM Material added 7/24/2014 9:52:46 AM ASTM A615 Grade 60 added 7/24/2014 9:52:46 AM ASTM A36 added 7/24/2014 9:52:46 AM Page 39 of 43 Jet way sap model_V11_V12 7-29.sdb SAP2000 v15.2.1 - License #0X23E80 30 July 2014 Table: Material Properties 03a - Steel Data Table: Material STEEL Material Properties 03a - Steel Data Fy Fu EffFy EffFu Kip/in2 Kip/in2 Kip/in2 Kip/in2 36.000 58.000 54.000 63.800 SSCurveOpt SSHysType User Defined Kinematic Table: Project Information Table: Project Information Item Data Company Name Client Name Project Name Project Number Model Name Model Description Revision Number Frame Type Engineer Checker Supervisor Issue Code Design Code Table: Steel Design 1 - Summary Data - AISC-LRFD99, Part 1 of 2 Frame 1 2 6 7 8 9 10 11 12 13 Table: Steel Design 1 - Summary Data - AISC-LRFD99, Part 1 of 2 Ratio DesignType Status DcsignScct L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 Beam Beam Beam Beam Beam Beam 0.175760 Beam Beam No Messages No Messages 0.158819 0.088265 PMM PMM Beam No Messages No Messages 0.080470 PMM 0.028924 PMM No Messages 0.057148 No Messages 0.047734 0.034814 PMM PMM PMM 16 L5X5X1/2 Beam Beam 17 18 L5X5X1/2 Beam 21 L5X5X1/2 22 23 L5X5X1/2 24 L5X5X1/2 L5X5X1/2 25 26 L5X5X1/2 L5X5X1/2 PMM PMM PMM PMM PMM PMM L5X5X1/2 L5X5X1/2 PMM PMM 0.039774 0.082522 15 20 0.192876 0.192876 0.191159 0.095565 No Messages No Messages No Messages 14 L5X5X1/2 L5X5X1/2 No Messages No Messages No Messages 0.347916 Beam Beam L5X5X1/2 L5X5X1/2 19 No Messages No Messages RatioType Beam No Messages Beam Beam No Messages No Messages 0.071100 PMM 0.155676 PMM Beam Beam No Messages 0.155676 PMM No Messages Beam No Messages 0.156236 0.085189 PMM PMM Beam Beam No Messages No Messages No Messages 0.073494 PMM 0.111078 0.175494 PMM PMM Beam Page 40 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Steel Design 1 - Summary Data - AISC-LRFD99, Part 1 of 2 Frame DesignSect DesignType Status 27 28 29 L5X5X1/2 Beam L5X5X1/2 L5X5X1/2 Beam Beam Beam No Messages No Messages 0.160048 0.103529 PMM PMM No Messages 0.342703 PMM No Messages 0.201314 0.148794 0.175760 PMM PMM PMM 0.084206 0.082523 PMM PMM 0.156236 0.162912 PMM 0.169958 0.229016 0.229668 PMM 32 35 38 41 44 47 50 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 L5X5X1/2 L5X5X1/2 L5X5X1/2 Beam No Messages Beam L5X5X1/2 L5X5X1/2 Beam No Messages No Messages L5X5X1/2 Beam Beam L5X5X1/2 L5X5X1/2 L5X5X1/2 Beam Beam Beam L5X5X1/2 L5X5X1/2 L5X5X1/2 Beam Beam Beam No Messages No Messages No Messages 0.193241 L5X5X1/2 L5X5X1/2 L5X5X1/2 Beam Beam Beam No Messages 0.105926 0.055469 L5X5X1/2 L5X5X1/2 L5X5X1/2 Beam Beam Beam L5X5X1/2 L5X5X1/2 Beam Beam Beam L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 71 72 73 L5X5X1/2 L5X5X1/2 74 75 76 L5X5X1/2 L5X5X1/2 L5X5X1/2 77 78 L5X5X1/2 79 80 81 82 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 83 84 85 L5X5X1/2 86 87 L5X5X1/2 L5X5X1/2 L5X5X1/2 88 89 No Messages No Messages No Messages Ratio L5X5X1/2 L5X5X1/2 L5X5X1/2 L5X5X1/2 No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages 0.135964 0.099886 0.063358 0.052302 0.065486 0.075892 PMM PMM PMM PMM PMM PMM PMM PMM PMM PMM PMM PMM PMM Beam Beam No Messages No Messages No Messages No Messages Beam Beam No Messages No Messages 0.072140 Beam Beam Beam No Messages No Messages 0.041658 0.074688 PMM PMM PMM No Messages No Messages 0.075912 0.100619 PMM PMM Beam Beam Beam Beam 0.042156 0.077028 0.072398 0.047307 0.066240 RatioType PMM PMM PMM PMM No Messages 0.133037 PMM No Messages No Messages PMM PMM PMM PMM Beam Beam Beam No Messages 0.100371 0.100371 0.103224 No Messages No Messages 0.233521 0.240533 Beam Beam No Messages 0.181501 PMM PMM No Messages No Messages 0.124618 0.057045 PMM PMM No Messages 0.055469 PMM No Messages 0.079525 Beam No Messages PMM PMM Beam No Messages No Messages 0.040074 0.035972 Beam Beam Beam Beam No Messages 0.035471 0.039827 PMM PMM PMM PMM 91 92 L5X5X1/2 Beam Beam No Messages 0.045096 L5X5X1/2 Beam No Messages 0.048209 PMM 93 Beam 94 L5X5X1/2 L5X5X1/2 No Messages No Messages 95 L5X5X1/2 No Messages PMM PMM PMM 96 97 L5X5X1/2 Beam Beam 0.045249 0.039104 0.031180 L5X5X1/2 Beam No Messages No Messages 0.051928 0.047407 PMM PMM 90 Beam Page 41 of 43 SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Jet way sap model_V11_V12 7-29.sdb Table: Steel Design 1 - Summary Data - AISC-LRFD99, Part 1 of 2 Frame DesignSect DesignType Status Ratio RatioType 98 99 L5X5X1/2 L5X5X1/2 Beam Beam No Messages No Messages 0.040731 0.050392 PMM PMM 100 L5X5X1/2 Beam No Messages 0.096132 PMM 101 102 L5X5X1/2 L5X5X1/2 Beam Beam No Messages No Messages 0.154104 0.095208 PMM PMM 103 L5X5X1/2 Beam No Messages 0.097263 PMM 104 L5X5X1/2 Beam No Messages 0.103224 PMM Table: Steel Design 1 - Summary Data - AISC-LRFD99, Part 2 of 2 Table: Frame Combo Steel Design 1 - Summary Data - AISC-LRFD99, Part 2 of 2 Location ErrMsg WarnMsg No Messages No Messages in 1 2 6 7 8 9 10 11 12 13 14 15 16 12.000 No Messages 12.000 No Messages No Messages No Messages UDSTL2 0.000 0.000 0.000 UDSTL4 UDSTL4 12.000 12.000 UDSTL2 UDSTL2 UDSTL2 UDSTL2 0.000 0.000 UDSTL3 UDSTL3 UDSTL3 UDSTL3 UDSTL3 UDSTL2 12.000 0.000 12.000 12.000 0.000 0.000 17 18 19 20 UDSTL2 UDSTL3 UDSTL2 UDSTL2 21 22 UDSTL2 UDSTL2 UDSTL4 0.000 12.000 UDSTL3 UDSTL3 UDSTL3 12.000 12.000 UDSTL3 UDSTL3 UDSTL4 0.000 0.000 23 24 25 26 27 28 29 32 35 38 41 44 UDSTL4 UDSTL4 UDSTL2 UDSTL4 UDSTL4 12.000 12.000 0.000 0.000 12.000 12.000 0.000 0.000 0.000 36.000 36.000 No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages 36.000 53 UDSTL4 UDSTL4 12.000 No Messages 54 UDSTL2 12.000 No Messages 55 56 UDSTL2 UDSTL4 0.000 0.000 No Messages No Messages 57 58 UDSTL4 UDSTL4 0.000 0.000 59 UDSTL2 12.000 No Messages No Messages No Messages UDSTL2 No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages 47 50 No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages Page 42 of 43 Jet way sap model_V11_V12 7-29.sdb Table: Frame Combo SAP2000 V15.2.1 - License #0X23E80 30 July 2014 Steel Design 1 - Summary Data - AISC-LRFD99, Part 2 of 2 ErrMsg WarnMsg 12.000 No Messages No Messages 0.000 No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages Location in 62 UDSTL4 UDSTL3 UDSTL4 63 UDSTL4 64 65 UDSTL4 66 67 UDSTL4 UDSTL4 UDSTL4 12.000 0.000 UDSTL4 UDSTL4 12.000 60 61 68 69 71 72 73 UDSTL2 UDSTL4 74 UDSTL4 UDSTL4 75 UDSTL4 76 77 UDSTL2 UDSTL4 78 79 80 81 82 0.000 12.000 0.000 12.000 12.000 0.000 0.000 12.000 0.000 12.000 No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages UDSTL4 12.000 12.000 0.000 UDSTL2 UDSTL3 UDSTL3 12.000 12.000 0.000 UDSTL3 UDSTL3 0.000 0.000 No Messages No Messages No Messages No Messages UDSTL2 0.000 UDSTL2 UDSTL2 UDSTL2 12.000 12.000 0.000 0.000 No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages Messages Messages Messages Messages No Messages No Messages No Messages No Messages No Messages No Messages 12.000 12.000 12.000 12.000 0.000 No Messages No Messages No Messages No Messages No Messages No Messages No Messages UDSTL2 0.000 UDSTL2 UDSTL3 12.000 0.000 No Messages No Messages UDSTL3 0.000 UDSTL3 UDSTL2 0.000 0.000 100 101 102 UDSTL3 12.000 UDSTL3 UDSTL3 12.000 103 104 UDSTL2 UDSTL2 83 84 85 86 87 88 UDSTL2 89 90 UDSTL3 UDSTL2 91 92 UDSTL2 UDSTL2 UDSTL2 93 94 95 96 97 98 99 0.000 12.000 12.000 No No No No No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages No Messages Page 43 of 43 mm mm WM \€m W) N* €*?€ 00 mAni wl SPECIFICATIONS: LENGTH: 150in (381cm) WIDTH: 87.75in (223cm) HEIGHT: 62in (157cm) WEIGHT: 7950lbs (3606kg) DESIGN AMBIENT COOL: 100°F(38°C)DB/76°F(24°C)WB DESIGN AMBIENT HEAT: -10°F(-23°C)/50%RH OUTLET TEMP. @ UNIT: 32°F (0°C) -38°F (3°C) COOLING: ] mm ml mA mA HEATING: COOLING CAPACITY: HEATING CAPACITY: AIR FLOW COOL: AIR FLOW HEAT: STATIC PRESSURE: POWER REQUIRED: 102.77 23.61 STANDARD COLOR: REFRIGERANT: 100°F (38°C) - 160°F (71°C) 90 TONS 160kW 500ppm (3.78kg/s) 330ppm (2.49kg/s) 35 inH20 (8.718 kPA) @ END OF THE DUCT 480 V A.C. 60 Hz, 3 Phase 300 amp RAL9003 41OA 2X0 14.00 OUTLET O O CN NO 150.00 UNLESS OTHERWISE SPECIFIED: DATE DIMENSIONS ARE ININCHES TOLERANCES: ANGULAR: • £ DEG TWO PLACE DECIMAL -.015 THREE PLACE DECIMAL -.005 FOUR PLACE DECIMALS -.0005 SPRING 4/25/13 THIRD ANGLE PROJECTION PROPRIETARY AND CONFIDENTIAL SIZE J DWG. NO. B DO NOT SCALE DRAWING SPECIALIST; TWIST INC 90 TON PCA PCA090480WH PCS.REQ'D. THE INFORMATION CONTAINED INTHIS DRAWING IS THESOLE PROPERTY OF TWIST INC.. ANY REPRODUCTION IN PARTOR AS AWHOLE WITHOUT THE WRITTEN PERMISSIONOF TWIST INC. IS PROHIBITED. TWIST INC. JAMESTOWN. OHIO. U.S.A. TITLE: PCA090480WH | REV ' A SHEET 1 OF 1 SCALE: 1:30 WEIGHT: 1 SPECIFICATIONS: LENGTH: WIDTH: HEIGHT: WEIGHT: DESIGN AMBIENT COOL: DESIGN AMBIENT HEAT: OUTLET TEMP. @ UNIT: COOLING: HEATING: COOLING CAPACITY: HEATING CAPACITY: AIR FLOW COOL: AIR FLOW HEAT: STATIC PRESSURE: POWER REQUIRED: STANDARD COLOR: REFRIGERANT: 114in (290cm) 87.75in (223cm) 59in (150cm) 4850lbs (2200kg) 100°F(38°C)DB/76°F(24°C)WB -10°F(-23°C)/50%RH 32°F (0°C) - 38°F (3°C) 100°F (38°C) - 160°F (71°C) 60 TONS @ 60 Hz POWER 120kW 325ppm (2.46kg/s) 215ppm (1.63kg/s) 30 inH20 (7.473 kPA) @ END OF UNIT 480 V A.C. 60 Hz, 3 Phase 200 amp RAL9003 41OA TWIST AERO UNLESS OTHERWISE SPECIFIED: DIMENSIONS ARE IN INCHES TOLERANCES: ANGULAR: i.5 DEG TWO PLACE DECIMAL ±.015 THREE PLACE DECIMAL ±.005 FOUR PUCE DECIMALS ±03005 JAMESTOWN, OHIO. U.S.A. TITLE: TWIST INC 60 TON PCA PCA060480WH THIRD ANGLE PROJECTION PCS. REQ'D. PROPRIETARY AND CONFIDENTIAL THE INFORMATION CONTAIN® INTHIS DRAWING IS THE SOLE PROPERTY OF TWIST INC.. ANY REPRODUCTION IN PART OR AS AWHOLE WITHOUTTHE WRITTEN PERMISSION OF TWIST INC. IS PROHIBITED. SIZE B DO NOT SCALE DRAWING DWG. NO. REV PCA060480WH SCALE: 1:30 WEIGHT: A SHEET 1 OF 1 SPECIFICATIONS: LQ N. r\ CO m m m LENGTH: WIDTH: HEIGHT: WEIGHT: DESIGN AMBIENT COOL: DESIGN AMBIENT HEAT: OUTLET TEMP. @ UNIT: COOLING: HEATING: COOLING CAPACITY: HEATING CAPACITY: AIR FLOW COOL: AIR FLOW HEAT: STATIC PRESSURE: a POWER REQUIRED: M STANDARD COLOR: REFRIGERANT: 98.77 114in (290cm) 87.75in (223cm) 59in (150cm) 4500lbs (2041kg) 100°F(38°C)DB/76°F(24°C)WB -10°F(-23°C)/50% RH 32°F (0°C) - 38°F (3°C) 100°F (38°C) - 160°F (71°C) 45 TONS @ 60 Hz POWER 80kW 275ppm (2.08kg/s) 165ppm (1.25kg/s) 25 inH20 (6.227 kPA) @ END OF UNIT 480 V A.C. 60 Hz, 3 Phase 150 amp RAL9003 41OA 7.62 HZ ] o p CN to 114.00 TWIST AERO UNLESS OTHERWISE SPECIFIED: " DIMENSIONS ARE IN INCHES TOLERANCES: - ANGULAR: • .5 DEG TWO PLACE DECIMAL t.015 . THREE PLACE DECIMAL =.005 FOUR PLACE DECIMALS =.0005 JAMESTOWN. OHIO. U.S.A. TITLE: TWIST INC 45 TON PCA PCA045480WH THIRD ANGLE PROJECTION -^7 - PCS. REQ'D. | "I SIZE PROPRIETARY AND CONFIDENTIAL THE INFORMATION CONTAINS) INTHIS DRAWING IS THE SOLE PROPERTY OF TWISTINC.. ANY REPRODUCTION IN PART ORAS A WHOLE WITHOUTTHE WRITTEN PERMISSION OF TWIST INC. IS PROHIBIT®. 6 B 3 2 REV PCA045480WH SCALE: 1:30[WEIGHT: DO NOT SCALE DRAWING 4 DWG. NO. A SHEET! OF 1 AIRCRAFT COOLING AND HEATING LOADS A-321-100 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type Denver, Colorado 0.83 A-321-100 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct 8,739 Btuh o # of Passengers 152 Temperature Rise due to Duct 4.2 F % Full 100 % Req'd Coil Leaving Air Temp o 31 F # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply 7 o 92 F o 60 F Air System Resistance: External Static Pressure 11 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 o 901 Btuh/ F o 75 F o 35 F Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower 4 in. w.c. 24 in. w.c. Fan Brake Horsepower, bhp Blower Heat, Qblower Temperature Rise due to Blower Coil Entering Air Temperature 13 bhp 33,732 Btuh o 19 F o 111 F Conduction Load, Qconduction 27,931 Btuh Unit Entering Air Enthalpy, hOA Passenger Load, Qpassenger 36,570 Btuh Unit Leaving Air Enthalpy, hLA 28.4 Btu/lba 10.4 Btu/lba Aircraft Solar Load Aircraft Max Electrical Load Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft 13,148 11,440 50 5,720 83,369 Enthalpy Difference, h 18.0 Btu/lba Unit Supply Air Flow, m Static Pressure Requirements Fan Efficiency Btuh Btuh % Btuh Btuh 145 lba/min 11 in. w.c. 55 % Air Load, Qair (not including blower) 156,317 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Total Net Tons POU Unit Correction Estimated POU Unit Tons 190,049 16 82 19 Btuh Tons % Tons HEATING LOAD ESTIMATE Cabin Temperature o 75 F o Conduction Load, Qconduction Outdoor Temperature -5 F Heat Capacity Req'd, Q CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct Supply Air Temperature, Tsupply 72,080 Btuh 186,102 Btuh 2o 0.56 Btuh/ft F 16,072 Btuh o 126 F TOTAL PCA UNIT HEATING LOAD Density of Air Heating Air Flow Rate 3 0.062 lbm/ft 99 lbm/min Total Heat Capacity Req'd, Q total 202,174 Btuh Total Heat Capacity Req'd, Q total 59.26 kW AIRCRAFT COOLING AND HEATING LOADS B-737-500 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type Denver, Colorado 0.83 B-737-500 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct 8,739 Btuh o # of Passengers 135 Temperature Rise due to Duct 4.6 F % Full 100 % Req'd Coil Leaving Air Temp o 30 F # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply 7 o 92 F o 60 F Air System Resistance: External Static Pressure 11 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 o 978 Btuh/ F o 75 F o 35 F Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower 4 in. w.c. 24 in. w.c. Fan Brake Horsepower, bhp Blower Heat, Qblower Temperature Rise due to Blower Coil Entering Air Temperature 12 bhp 30,830 Btuh o 19 F o 111 F Conduction Load, Qconduction 30,318 Btuh Unit Entering Air Enthalpy, hOA Passenger Load, Qpassenger 32,660 Btuh Unit Leaving Air Enthalpy, hLA 28.4 Btu/lba 10.4 Btu/lba Aircraft Solar Load Aircraft Max Electrical Load Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft 7,741 10,955 50 5,478 76,197 Enthalpy Difference, h 18.0 Btu/lba Unit Supply Air Flow, m Static Pressure Requirements Fan Efficiency Btuh Btuh % Btuh Btuh 132 lba/min 11 in. w.c. 55 % Air Load, Qair (not including blower) 142,868 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Total Net Tons POU Unit Correction Estimated POU Unit Tons 173,698 14 82 18 Btuh Tons % Tons HEATING LOAD ESTIMATE Cabin Temperature o 75 F o Conduction Load, Qconduction Outdoor Temperature -5 F Heat Capacity Req'd, Q CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct Supply Air Temperature, Tsupply 78,240 Btuh 180,071 Btuh 2o 0.56 Btuh/ft F 17,413 Btuh o 136 F TOTAL PCA UNIT HEATING LOAD Density of Air Heating Air Flow Rate 3 0.062 lbm/ft 88 lbm/min Total Heat Capacity Req'd, Q total 197,484 Btuh Total Heat Capacity Req'd, Q total 57.88 kW AIRCRAFT COOLING AND HEATING LOADS B-747-400 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type Denver, Colorado 0.83 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct B-747-400 8,739 Btuh o # of Passengers 499 Temperature Rise due to Duct 1.3 F % Full 100 % Req'd Coil Leaving Air Temp o 34 F # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA 21 Air System Resistance: o 92 F o 60 F External Static Pressure 25 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower o 2,975 Btuh/ F Fan Brake Horsepower, bhp Blower Heat, Qblower Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply Conduction Load, Qconduction Passenger Load, Qpassenger o 75 F o 35 F 92,225 Btuh Unit Entering Air Enthalpy, hOA 28.4 Btu/lba 119,600 Btuh Unit Leaving Air Enthalpy, hLA 10.4 Btu/lba Enthalpy Difference, h 18.0 Btu/lba Aircraft Max Electrical Load 75,000 Btuh 50 % Air Load, Qair (not including blower) 519,984 Btuh 37,500 Btuh 277,325 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Unit Supply Air Flow, m o 123 F 28,000 Btuh Aircraft Electrical Load Aircraft Load, Qaircraft 70 bhp 177,665 Btuh o 31 F Coil Entering Air Temperature Aircraft Solar Load Percent of Max Electrical Load Temperature Rise due to Blower 4 in. w.c. 38 in. w.c. 481 lba/min 697,649 Btuh Total Net Tons 58 Tons Static Pressure Requirements 25 in. w.c. POU Unit Correction 82 % Fan Efficiency 55 % Estimated POU Unit Tons 71 Tons o 75 F Conduction Load, Qconduction 238,000 Btuh Outdoor Temperature -5 F Heat Capacity Req'd, Q 610,902 Btuh CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct HEATING LOAD ESTIMATE Cabin Temperature Supply Air Temperature, Tsupply Density of Air Heating Air Flow Rate o 2o 0.56 Btuh/ft F 16,132 Btuh o 126 F 3 0.062 lbm/ft 324 lbm/min TOTAL PCA UNIT HEATING LOAD Total Heat Capacity Req'd, Q total Total Heat Capacity Req'd, Q total DEN PCA Htg-Clg loads-V2-AM-BLB.xlsx 627,034 Btuh 183.78 kW AIRCRAFT COOLING AND HEATING LOADS B-757-200 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type Denver, Colorado 0.83 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct B-757-200 8,739 Btuh o # of Passengers 201 Temperature Rise due to Duct 4.4 F % Full 100 % Req'd Coil Leaving Air Temp o 31 F # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA 7 o 92 F o 60 F Air System Resistance: External Static Pressure 10 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower o 605 Btuh/ F Fan Brake Horsepower, bhp Blower Heat, Qblower Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply o 75 F o 35 F Temperature Rise due to Blower 4 in. w.c. 23 in. w.c. 12 bhp 30,987 Btuh o 18 F o Coil Entering Air Temperature 110 F Conduction Load, Qconduction 18,755 Btuh Unit Entering Air Enthalpy, hOA 28.4 Btu/lba Passenger Load, Qpassenger 47,840 Btuh Unit Leaving Air Enthalpy, hLA 10.4 Btu/lba Enthalpy Difference, h 18.0 Btu/lba Aircraft Solar Load 8,520 Btuh Aircraft Max Electrical Load 9,600 Btuh Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft 50 % Air Load, Qair (not including blower) 4,800 Btuh 79,915 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Unit Supply Air Flow, m 149,841 Btuh 139 lba/min 180,828 Btuh Total Net Tons 15 Tons Static Pressure Requirements 10 in. w.c. POU Unit Correction 82 % Fan Efficiency 55 % Estimated POU Unit Tons 18 Tons o 75 F Conduction Load, Qconduction 48,400 Btuh HEATING LOAD ESTIMATE Cabin Temperature o Outdoor Temperature -5 F Heat Capacity Req'd, Q CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct Supply Air Temperature, Tsupply Density of Air Heating Air Flow Rate 197,561 Btuh 2o 0.56 Btuh/ft F 13,042 Btuh o 101 F 3 0.062 lbm/ft 129 lbm/min TOTAL PCA UNIT HEATING LOAD Total Heat Capacity Req'd, Q total Total Heat Capacity Req'd, Q total DEN PCA Htg-Clg loads-V2-AM-BLB.xlsx 210,603 Btuh 61.73 kW AIRCRAFT COOLING AND HEATING LOADS B-767-300 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type Denver, Colorado 0.83 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct B-767-300 8,739 Btuh o # of Passengers 269 Temperature Rise due to Duct 2.7 F % Full 100 % Req'd Coil Leaving Air Temp o 32 F # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA 9 o 92 F o 60 F Air System Resistance: External Static Pressure 23 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower o 882 Btuh/ F Fan Brake Horsepower, bhp Blower Heat, Qblower Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply o 75 F o 35 F Temperature Rise due to Blower 4 in. w.c. 36 in. w.c. 31 bhp 77,814 Btuh o 29 F o Coil Entering Air Temperature 121 F Conduction Load, Qconduction 27,342 Btuh Unit Entering Air Enthalpy, hOA 28.4 Btu/lba Passenger Load, Qpassenger 63,940 Btuh Unit Leaving Air Enthalpy, hLA 10.4 Btu/lba Aircraft Solar Load 12,840 Btuh Enthalpy Difference, h 18.0 Btu/lba Aircraft Max Electrical Load 48,180 Btuh Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft 50 % Air Load, Qair (not including blower) 24,090 Btuh 128,212 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Unit Supply Air Flow, m 240,398 Btuh 223 lba/min 318,212 Btuh Total Net Tons 27 Tons Static Pressure Requirements 23 in. w.c. POU Unit Correction 82 % Fan Efficiency 55 % Estimated POU Unit Tons 32 Tons o 75 F Conduction Load, Qconduction 70,560 Btuh HEATING LOAD ESTIMATE Cabin Temperature o Outdoor Temperature -5 F Heat Capacity Req'd, Q CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct Supply Air Temperature, Tsupply Density of Air Heating Air Flow Rate 269,919 Btuh 2o 0.56 Btuh/ft F 13,332 Btuh o 103 F 3 0.062 lbm/ft 173 lbm/min TOTAL PCA UNIT HEATING LOAD Total Heat Capacity Req'd, Q total Total Heat Capacity Req'd, Q total DEN PCA Htg-Clg loads-V2-AM-BLB.xlsx 283,252 Btuh 83.02 kW AIRCRAFT COOLING AND HEATING LOADS B-777-200 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type Denver, Colorado 0.83 B-777-200 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct 8,739 Btuh o # of Passengers 375 Temperature Rise due to Duct 1.8 F % Full 100 % Req'd Coil Leaving Air Temp o 33 F # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply 16 Air System Resistance: o 92 F o 60 F External Static Pressure 25 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 o 1,800 Btuh/ F o 75 F o 35 F Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower 4 in. w.c. 38 in. w.c. Fan Brake Horsepower, bhp Blower Heat, Qblower Temperature Rise due to Blower Coil Entering Air Temperature 48 bhp 123,310 Btuh o 31 F o 123 F Conduction Load, Qconduction 55,800 Btuh Unit Entering Air Enthalpy, hOA Passenger Load, Qpassenger 89,930 Btuh Unit Leaving Air Enthalpy, hLA 28.4 Btu/lba 10.4 Btu/lba Enthalpy Difference, h 18.0 Btu/lba Aircraft Solar Load Aircraft Max Electrical Load Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft Unit Supply Air Flow, m Static Pressure Requirements Fan Efficiency 28,000 37,500 50 18,750 192,480 Btuh Btuh % Btuh Btuh 334 lba/min 25 in. w.c. 55 % Air Load, Qair (not including blower) 360,900 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Total Net Tons POU Unit Correction Estimated POU Unit Tons 484,210 40 82 49 Conduction Load, Qconduction 144,000 Btuh 424,394 Btuh Btuh Tons % Tons HEATING LOAD ESTIMATE Cabin Temperature o 75 F o Outdoor Temperature -5 F Heat Capacity Req'd, Q CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct Supply Air Temperature, Tsupply 2o 0.56 Btuh/ft F 14,904 Btuh o 116 F TOTAL PCA UNIT HEATING LOAD Density of Air Heating Air Flow Rate 3 0.062 lbm/ft 243 lbm/min Total Heat Capacity Req'd, Q total 439,298 Btuh Total Heat Capacity Req'd, Q total 128.76 kW Twist, Inc.. Aircraft Heat Load Calculations Air Craft Air Flow Required At Design Conditions CUSTOMER: LOCATION: DATE: FILE : RFQ: DIA THREE PHASE POWER: 480 VAC 60 Hz VOLTS: HERTZ: 34 °CDB 16 °CWB DESIGN AMBIENT TEMPERATURE: 93 °FDB 61 °FWB R-410A REFRIGERANT DESIRED CABIN TEMPERATURE: SUPPLY AIR TEMPERATURE: (at aircraft connection) TEMPERATURE DIFFERENCE: 24 °C 75 °F 4 °C 40 °F 10 °C 18 °F B-787-8 AIRCRAFT MODEL: LOAD ESTIMATE: Heat Transmission Delta T 18 x Btu/Hr/°F 809 People Sensible Load # of People 284 x Btu/Hr/Person 275 = 78100 Btu/Hr Btu/Hr/°F 22000 = 22000 Btu/Hr Btu/Hr 68000 = 68000 Btu/Hr Solar Load 1 Electric Load 100 % = 14557 Btu/Hr Total Load 182657 Btu/Hr Air Flow Required: Total Load 182657 / (.24 x 60) Cabin Temp. - Supply Temp. x 35 From Aircraft Curves, Static Pressure Required Recommended Unit Size DIA 787-8-1.xls = = 362 lb./min 33 in. of H2O PCA075 8/20/2014 Confidential Prepared By Bob Woo Page 1 AIRCRAFT COOLING AND HEATING LOADS EMB-145 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type # of Passengers % Full # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA Denver, Colorado 0.83 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct EMB-145 50 100 % 4 o 92 F o 60 F 8,739 Btuh 9.6 F Req'd Coil Leaving Air Temp o 25 F Air System Resistance: External Static Pressure 5 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower o 133 Btuh/ F Fan Brake Horsepower, bhp Blower Heat, Qblower Cabin Temperature, Tcabin o Temperature Rise due to Duct o 75 F o Temperature Rise due to Blower 4 in. w.c. 18 in. w.c. 4 bhp 11,089 Btuh o 14 F o 35 F Coil Entering Air Temperature 106 F 4,123 Btuh Unit Entering Air Enthalpy, hOA 28.4 Btu/lba Passenger Load, Qpassenger 12,420 Btuh Unit Leaving Air Enthalpy, hLA 10.4 Btu/lba Aircraft Solar Load 14,600 Btuh Enthalpy Difference, h 18.0 Btu/lba Aircraft Max Electrical Load 10,800 Btuh Supply Air Temp@Aircraft, Tsupply Conduction Load, Qconduction Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft 50 % Air Load, Qair (not including blower) 5,400 Btuh 36,543 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Unit Supply Air Flow, m Static Pressure Requirements Fan Efficiency 68,518 Btuh 63 lba/min 5 in. w.c. Total Net Tons POU Unit Correction 79,607 Btuh 7 Tons 82 % 55 % Estimated POU Unit Tons 8 Tons o 75 F Conduction Load, Qconduction 10,640 Btuh Outdoor Temperature -5 F Heat Capacity Req'd, Q 49,364 Btuh CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct 12,553 Btuh Supply Air Temperature, Tsupply o 97 F TOTAL PCA UNIT HEATING LOAD Total Heat Capacity Req'd, Q total 61,917 Btuh HEATING LOAD ESTIMATE Cabin Temperature Density of Air Heating Air Flow Rate o 3 0.062 lbm/ft 34 lbm/min Total Heat Capacity Req'd, Q total DEN PCA Htg-Clg loads-V2-AM-BLB.xlsx 2o 0.56 Btuh/ft F 18.15 kW AIRCRAFT COOLING AND HEATING LOADS MD-11 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type Denver, Colorado 0.83 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct MD-11 8,739 Btuh o # of Passengers 270 Temperature Rise due to Duct 2.7 F % Full 100 % Req'd Coil Leaving Air Temp o 32 F # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply 13 Air System Resistance: o 92 F o 60 F External Static Pressure 25 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 o 973 Btuh/ F o 75 F o 35 F Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower 4 in. w.c. 38 in. w.c. Fan Brake Horsepower, bhp Blower Heat, Qblower Temperature Rise due to Blower Coil Entering Air Temperature 33 bhp 83,445 Btuh o 31 F o 123 F Conduction Load, Qconduction 30,163 Btuh Unit Entering Air Enthalpy, hOA Passenger Load, Qpassenger 65,090 Btuh Unit Leaving Air Enthalpy, hLA 28.4 Btu/lba 10.4 Btu/lba Enthalpy Difference, h 18.0 Btu/lba Aircraft Solar Load Aircraft Max Electrical Load Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft Unit Supply Air Flow, m Static Pressure Requirements Fan Efficiency 16,000 38,000 50 19,000 130,253 Btuh Btuh % Btuh Btuh 226 lba/min 25 in. w.c. 55 % Air Load, Qair (not including blower) 244,224 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Total Net Tons POU Unit Correction Estimated POU Unit Tons 327,669 27 82 33 Btuh Tons % Tons HEATING LOAD ESTIMATE Cabin Temperature o 75 F o Conduction Load, Qconduction Outdoor Temperature -5 F Heat Capacity Req'd, Q CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct Supply Air Temperature, Tsupply 77,840 Btuh 280,785 Btuh 2o 0.56 Btuh/ft F 13,624 Btuh o 106 F TOTAL PCA UNIT HEATING LOAD Density of Air Heating Air Flow Rate 3 0.062 lbm/ft 176 lbm/min Total Heat Capacity Req'd, Q total 294,409 Btuh Total Heat Capacity Req'd, Q total 86.29 kW AIRCRAFT COOLING AND HEATING LOADS B-727-200 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type Denver, Colorado 0.83 B-727-200 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct 8,739 Btuh o # of Passengers 148 Temperature Rise due to Duct 4.7 F % Full 100 % Req'd Coil Leaving Air Temp o 30 F # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply 7 o 92 F o 60 F Air System Resistance: External Static Pressure 12 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 o 875 Btuh/ F o 75 F o 35 F Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower 4 in. w.c. 25 in. w.c. Fan Brake Horsepower, bhp Blower Heat, Qblower Temperature Rise due to Blower Coil Entering Air Temperature 12 bhp 31,570 Btuh o 20 F o 112 F Conduction Load, Qconduction 27,125 Btuh Unit Entering Air Enthalpy, hOA Passenger Load, Qpassenger 35,650 Btuh Unit Leaving Air Enthalpy, hLA 28.4 Btu/lba 10.4 Btu/lba Aircraft Solar Load Aircraft Max Electrical Load Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft 7,730 8,800 50 4,400 74,905 Enthalpy Difference, h 18.0 Btu/lba Unit Supply Air Flow, m Static Pressure Requirements Fan Efficiency Btuh Btuh % Btuh Btuh 130 lba/min 12 in. w.c. 55 % Air Load, Qair (not including blower) 140,447 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Total Net Tons POU Unit Correction Estimated POU Unit Tons 172,017 14 82 17 Btuh Tons % Tons HEATING LOAD ESTIMATE Cabin Temperature o 75 F o Conduction Load, Qconduction Outdoor Temperature -5 F Heat Capacity Req'd, Q CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct Supply Air Temperature, Tsupply 70,000 Btuh 181,154 Btuh 2o 0.56 Btuh/ft F 16,048 Btuh o 125 F TOTAL PCA UNIT HEATING LOAD Density of Air Heating Air Flow Rate 3 0.062 lbm/ft 96 lbm/min Total Heat Capacity Req'd, Q total 197,202 Btuh Total Heat Capacity Req'd, Q total 57.80 kW AIRCRAFT COOLING AND HEATING LOADS B-737-300 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type Denver, Colorado 0.83 B-737-300 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct 8,739 Btuh o # of Passengers 126 Temperature Rise due to Duct 6.0 F % Full 100 % Req'd Coil Leaving Air Temp o 29 F # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply 7 o 92 F o 60 F Air System Resistance: External Static Pressure 10 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 o 640 Btuh/ F o 75 F o 35 F Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower 4 in. w.c. 23 in. w.c. Fan Brake Horsepower, bhp Blower Heat, Qblower Temperature Rise due to Blower Coil Entering Air Temperature 9 bhp 22,770 Btuh o 18 F o 110 F Conduction Load, Qconduction 19,840 Btuh Unit Entering Air Enthalpy, hOA Passenger Load, Qpassenger 30,590 Btuh Unit Leaving Air Enthalpy, hLA 28.4 Btu/lba 10.4 Btu/lba Aircraft Solar Load Aircraft Max Electrical Load Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft 4,800 6,984 50 3,492 58,722 Enthalpy Difference, h 18.0 Btu/lba Unit Supply Air Flow, m Static Pressure Requirements Fan Efficiency Btuh Btuh % Btuh Btuh 102 lba/min 10 in. w.c. 55 % Air Load, Qair (not including blower) 110,104 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Total Net Tons POU Unit Correction Estimated POU Unit Tons 132,873 11 82 14 Btuh Tons % Tons HEATING LOAD ESTIMATE Cabin Temperature o 75 F o Conduction Load, Qconduction Outdoor Temperature -5 F Heat Capacity Req'd, Q CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct Supply Air Temperature, Tsupply 51,200 Btuh 146,577 Btuh 2o 0.56 Btuh/ft F 15,133 Btuh o 118 F TOTAL PCA UNIT HEATING LOAD Density of Air Heating Air Flow Rate 3 0.062 lbm/ft 83 lbm/min Total Heat Capacity Req'd, Q total 161,710 Btuh Total Heat Capacity Req'd, Q total 47.40 kW AIRCRAFT COOLING AND HEATING LOADS DC-10 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type Denver, Colorado 0.83 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct DC-10 8,739 Btuh o # of Passengers 270 Temperature Rise due to Duct 2.7 F % Full 100 % Req'd Coil Leaving Air Temp o 32 F # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply 13 Air System Resistance: o 92 F o 60 F External Static Pressure 25 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 o 973 Btuh/ F o 75 F o 35 F Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower 4 in. w.c. 38 in. w.c. Fan Brake Horsepower, bhp Blower Heat, Qblower Temperature Rise due to Blower Coil Entering Air Temperature 33 bhp 83,445 Btuh o 31 F o 123 F Conduction Load, Qconduction 30,163 Btuh Unit Entering Air Enthalpy, hOA Passenger Load, Qpassenger 65,090 Btuh Unit Leaving Air Enthalpy, hLA 28.4 Btu/lba 10.4 Btu/lba Enthalpy Difference, h 18.0 Btu/lba Aircraft Solar Load Aircraft Max Electrical Load Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft Unit Supply Air Flow, m Static Pressure Requirements Fan Efficiency 16,000 38,000 50 19,000 130,253 Btuh Btuh % Btuh Btuh 226 lba/min 25 in. w.c. 55 % Air Load, Qair (not including blower) 244,224 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Total Net Tons POU Unit Correction Estimated POU Unit Tons 327,669 27 82 33 Btuh Tons % Tons HEATING LOAD ESTIMATE Cabin Temperature o 75 F o Conduction Load, Qconduction Outdoor Temperature -5 F Heat Capacity Req'd, Q CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct Supply Air Temperature, Tsupply 77,840 Btuh 280,785 Btuh 2o 0.56 Btuh/ft F 13,624 Btuh o 106 F TOTAL PCA UNIT HEATING LOAD Density of Air Heating Air Flow Rate 3 0.062 lbm/ft 176 lbm/min Total Heat Capacity Req'd, Q total 294,409 Btuh Total Heat Capacity Req'd, Q total 86.29 kW AIRCRAFT COOLING AND HEATING LOADS EMB-170 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type # of Passengers % Full # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply Denver, Colorado 0.83 EMB-170 45 100 % 3 o 92 F o 60 F Duct Diameter 14 in. Duct Length 60 ft. o 11.8 F Req'd Coil Leaving Air Temp o 23 F Air System Resistance: External Static Pressure 5 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. 14 F o 106 F o 75 F o 35 F 8,739 Btuh Temperature Rise due to Duct o o 0.24 Btu/lb F 1 o 45 Btuh/ F 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower 4 in. w.c. 18 in. w.c. Fan Brake Horsepower, bhp Blower Heat, Qblower Temperature Rise due to Blower Coil Entering Air Temperature 4 bhp 9,008 Btuh o 14 F o 106 F 1,395 Btuh Unit Entering Air Enthalpy, hOA Passenger Load, Qpassenger 11,040 Btuh Unit Leaving Air Enthalpy, hLA 28.4 Btu/lba 10.4 Btu/lba Aircraft Solar Load Aircraft Max Electrical Load Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft 14,600 5,300 50 2,650 29,685 Enthalpy Difference, h 18.0 Btu/lba Conduction Load, Qconduction Unit Supply Air Flow, m Static Pressure Requirements Fan Efficiency Btuh Btuh % Btuh Btuh Air Load, Qair (not including blower) 55,659 Btuh 52 lba/min 5 in. w.c. 55 % TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Total Net Tons POU Unit Correction Estimated POU Unit Tons 64,668 5 82 7 o 75 F Conduction Load, Qconduction Btuh Tons % Tons HEATING LOAD ESTIMATE Cabin Temperature o 3,600 Btuh Outdoor Temperature -5 F Heat Capacity Req'd, Q 38,022 Btuh CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct 2o 0.56 Btuh/ft F 10,877 Btuh Supply Air Temperature, Tsupply o 83 F TOTAL PCA UNIT HEATING LOAD Density of Air Heating Air Flow Rate 3 0.062 lbm/ft 30 lbm/min Total Heat Capacity Req'd, Q total 48,899 Btuh Total Heat Capacity Req'd, Q total 14.33 kW AIRCRAFT COOLING AND HEATING LOADS MD-80 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type Denver, Colorado 0.83 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct MD-80 8,739 Btuh o # of Passengers 150 Temperature Rise due to Duct 5.1 F % Full 100 % Req'd Coil Leaving Air Temp o 30 F # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA 7 o 92 F o 60 F Air System Resistance: External Static Pressure 15 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower o 679 Btuh/ F Fan Brake Horsepower, bhp Blower Heat, Qblower Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply o 75 F o 35 F Temperature Rise due to Blower 4 in. w.c. 28 in. w.c. 13 bhp 32,330 Btuh o 22 F o Coil Entering Air Temperature 114 F Conduction Load, Qconduction 21,049 Btuh Unit Entering Air Enthalpy, hOA 28.4 Btu/lba Passenger Load, Qpassenger 36,110 Btuh Unit Leaving Air Enthalpy, hLA 10.4 Btu/lba Enthalpy Difference, h 18.0 Btu/lba Aircraft Solar Load Aircraft Max Electrical Load Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft 5,880 Btuh 10,900 Btuh 50 % Air Load, Qair (not including blower) 5,450 Btuh 68,489 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Unit Supply Air Flow, m 128,417 Btuh 119 lba/min 160,747 Btuh Total Net Tons 13 Tons Static Pressure Requirements 15 in. w.c. POU Unit Correction 82 % Fan Efficiency 55 % Estimated POU Unit Tons 16 Tons o 75 F Conduction Load, Qconduction 54,320 Btuh HEATING LOAD ESTIMATE Cabin Temperature o Outdoor Temperature -5 F Heat Capacity Req'd, Q CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct Supply Air Temperature, Tsupply Density of Air Heating Air Flow Rate 166,908 Btuh 2o 0.56 Btuh/ft F 14,598 Btuh o 114 F 3 0.062 lbm/ft 98 lbm/min TOTAL PCA UNIT HEATING LOAD Total Heat Capacity Req'd, Q total Total Heat Capacity Req'd, Q total DEN PCA Htg-Clg loads-V2-AM-BLB.xlsx 181,506 Btuh 53.20 kW AIRCRAFT COOLING AND COOLING LOADS A-330-300 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type Denver, Colorado 0.83 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct A-330-300 8,739 Btuh o # of Passengers 335 Temperature Rise due to Duct 1.8 F % Full 100 % Req'd Coil Leaving Air Temp o 33 F # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA 13 Air System Resistance: o 92 F o 60 F External Static Pressure 11 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower o 2,884 Btuh/ F Fan Brake Horsepower, bhp Blower Heat, Qblower Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply o 75 F o 35 F Temperature Rise due to Blower 4 in. w.c. 24 in. w.c. 31 bhp 78,508 Btuh o 19 F o Coil Entering Air Temperature 111 F Conduction Load, Qconduction 89,404 Btuh Unit Entering Air Enthalpy, hOA 28.4 Btu/lba Passenger Load, Qpassenger 80,040 Btuh Unit Leaving Air Enthalpy, hLA 10.4 Btu/lba Aircraft Solar Load 13,148 Btuh Enthalpy Difference, h 18.0 Btu/lba Aircraft Max Electrical Load 22,881 Btuh Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft 50 % Air Load, Qair (not including blower) 11,440 Btuh 194,032 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Unit Supply Air Flow, m 363,810 Btuh 337 lba/min 442,318 Btuh Total Net Tons 37 Tons Static Pressure Requirements 11 in. w.c. POU Unit Correction 82 % Fan Efficiency 55 % Estimated POU Unit Tons 45 Tons o 75 F Conduction Load, Qconduction 230,720 Btuh Outdoor Temperature -5 F Heat Capacity Req'd, Q 480,278 Btuh CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct HEATING LOAD ESTIMATE Cabin Temperature Supply Air Temperature, Tsupply Density of Air Heating Air Flow Rate o 2o 0.56 Btuh/ft F 18,951 Btuh o 149 F 3 0.062 lbm/ft 217 lbm/min TOTAL PCA UNIT HEATING LOAD Total Heat Capacity Req'd, Q total Total Heat Capacity Req'd, Q total DEN PCA Htg-Clg loads-V2-AM-BLB.xlsx 499,229 Btuh 146.32 kW AIRCRAFT COOLING AND HEATING LOADS B-777-300 Project Name DIA - Concourse B - PCA Replacement Project Number 65967 Date 19-Aug-14 COOLING LOAD ESTIMATE Project Location Altitude Correction Factor Aircraft Type Denver, Colorado 0.83 Duct Diameter 14 in. Duct Length 60 ft. 2o 0.56 Btuh/ft F Duct U-Value Duct Heat Gain, Qduct B-777-300 8,739 Btuh o # of Passengers 386 Temperature Rise due to Duct 1.7 F % Full 100 % Req'd Coil Leaving Air Temp o 33 F # of Crew Dry Bulb Temperature, Tdb Wet Bulb Temperature, Twb Aircraft Skin Temp Corr ΔT Aircraft Skin Temperature (TDB+ΔT) Specific Heat of Air, Cp Cloud Cover Factor, CCF UA 16 Air System Resistance: o 92 F o 60 F External Static Pressure 25 in. w.c. Duct (1) 14" x 60 feet 2 in. w.c. o 14 F o 106 F o 0.24 Btu/lb F 1 Coupling 4 in. w.c. Evaporator Coil 2 in. w.c. Air Filter 1 in. w.c. Internal Resistance Total SP Required by Blower o 1,800 Btuh/ F Fan Brake Horsepower, bhp Blower Heat, Qblower Cabin Temperature, Tcabin Supply Air Temp@Aircraft, Tsupply o 75 F o 35 F Temperature Rise due to Blower 4 in. w.c. 38 in. w.c. 51 bhp 130,088 Btuh o 31 F o Coil Entering Air Temperature 123 F Conduction Load, Qconduction 55,800 Btuh Unit Entering Air Enthalpy, hOA 28.4 Btu/lba Passenger Load, Qpassenger 92,460 Btuh Unit Leaving Air Enthalpy, hLA 10.4 Btu/lba Aircraft Solar Load 27,300 Btuh Enthalpy Difference, h 18.0 Btu/lba Aircraft Max Electrical Load 55,000 Btuh Percent of Max Electrical Load Aircraft Electrical Load Aircraft Load, Qaircraft 50 % Air Load, Qair (not including blower) 27,500 Btuh 203,060 Btuh TOTAL PCA UNIT COOLING LOAD Total Load, Qtotal (Qair +Qblower) Unit Supply Air Flow, m 380,738 Btuh 353 lba/min 510,825 Btuh Total Net Tons 43 Tons Static Pressure Requirements 25 in. w.c. POU Unit Correction 82 % Fan Efficiency 55 % Estimated POU Unit Tons 52 Tons o 75 F Conduction Load, Qconduction 144,000 Btuh Outdoor Temperature -5 F Heat Capacity Req'd, Q 432,282 Btuh CFM/Person Required 10 cfm Duct U-Value Duct Losses, Qduct HEATING LOAD ESTIMATE Cabin Temperature Supply Air Temperature, Tsupply Density of Air Heating Air Flow Rate o 2o 0.56 Btuh/ft F 14,766 Btuh o 115 F 3 0.062 lbm/ft 250 lbm/min TOTAL PCA UNIT HEATING LOAD Total Heat Capacity Req'd, Q total Total Heat Capacity Req'd, Q total DEN PCA Htg-Clg loads-V2-AM-BLB.xlsx 447,048 Btuh 131.03 kW 4.0 APPENDIX A. Technical Memorandums B. Opinion of Probable Cost C. Product Data D. Project Schedule Page 7 Appendix A – Technical Memorandums Techn nical Memoran M ndum 1..0 Date: February 10 0, 2012 Re: Concourse B PCA Unit Replacement R Sizes S Discussion The purpo ose of this Technical Mem morandum is to o discuss the pprocess used for determiniing the sizes oof the new Pre-C Conditioned Air A (PCA) Un nits on the Co oncourse B Paassenger Boarrding Bridgess (PBB) and too provide co onfirmation of o the size of the t units to bee installed at each gate. Thhe existing briidges are currrently served by y 20 ton and 45 ton Air-a-P Plane PCA units. Analysis A. Outdo oor Design Co onditions The following fo wass obtained from m the DIA Design Manuall 4 Summ mer Design Conditions: 92 2 °F / 59 ° F WB W Winteer Design Con nditions: -5 ° F B. Aircraaft Cooling Load L Calculatiions The PCA P air handlling unit will be sized to maintain m a 75 °°F (+/- 2 degrrees) cabin temperature foor both heating h and co ooling for thee largest aircraft type incluuded in the gaate aircraft mix for each gate. The following fo load d conditions were w assumed d when calcullating the cooling load for the different aircraaft. 10 00% full passsenger load an nd crew for th he largest airccraft to be coooled. 230 Btuuh per personn was ussed for the sensible heat paassenger load d calculations.. The T solar load calculated ussing 100% briight sunshinee conditions. 50 0% of the airccraft electricaal load. Because B the air handling un nit will be mounted near thhe rotunda collumn, a telesccoping air ducct will bee utilized to deliver d air acrross the bridgee to the flexibble hose connnection near thhe bridge lift co olumn. The heat h gain/loss through the telescoping t dduct and flexibble hose was calculated at about 5 ºF for both su ummer and winter w conditio ons. The airrflow requiredd to cool the aaircraft was caalculated usin ng the 35ºF teemperature at the connectioon to the aircrraft. For heatting the airfloow is baased on the nu umber of passengers and the air temperrature at the cconnection to the aircraft w was deetermined to be b about 107 ºF. Actual A aircraftt static pressurre drops weree obtained froom curves pubblished by thee aircraft manufacturers m . Blower horrsepower requ uirements werre calculated uusing the suppply air quantiity an nd the overalll static pressu ure requirement. Blower hheat gain was added to the aircraft load aand aiir enthalpy load (outside aiir to cabin) ass the overall ttotal coil loadd for the air haandling unit. February y 10, 2012 Page 2 The T following table summaarizes the peak k aircraft loadd for the varioous aircraft inn the design m mix fo or Concourse B. Attached to t this memorandum are thhe individual load calculattions for eachh type off aircraft. Table 1.1 – Aircraftt Cooling and d Heating Looads Aircraftt Type A-321-100 B-737-50 00 B-747-40 00 B-757-20 00 B-767-30 00 B-777-20 00 EMB-17 70 MD-11 Un nit Cooling Lo oad (Tons) 19 18 71 18 32 49 7 33 Unit Heatiing Load (MB BH) 202 197 627 211 283 439 49 294 The T calculated d loads above were revieweed by a PCA uunit manufaccturer and werre determinedd to bee consistent with w industry norms. C. Replaacement Unitss 1. Manufactu urer DIA has reequested the use u of one maanufacturer, F FCX systems for the replaccement PCA uunits throughoutt the Concourrse. This willl decrease thee amount of sppare parts reqquired to be kkept on site and d will enable maintenance m staff to becom me familiar w with one type of equipmentt. As opposed to o the existing equipment, FCX F replacem ment parts aree readily availlable. 2. Sizes The availaable nominal sizes s for the FCX F units (inn tons of cooliing) are: 20, 330, 45, 60, 755, 90, 120, and 150. In order to t prevent deccrease in capaacity due to thhe high altitudde and ambient temperaturres in Denverr, FCX sizes the blowers acccordingly to ensure the PC CA units are capable off performing at a their nomin nal rating at thhe site conditiions. These bblowers also hhave Variable Frequency F Driives (VFD) which w allows ccapacity adjusstment for diffferent aircrafft sizes. 3. Operation Each new PCA unit is typically t prov vided with an individual puush-button staation with butttons for differen nt sized aircraaft. The aircraaft sizes are cclassified as fo follows: RJ – Regional Jet, NB – Narrow Body, B WB – Wide Body, JB J – Jumbo B Body. When aan aircraft pullls into the gaate, the ground d crew will pu ush the approp priate button for that aircraaft. The PCA unit VFD wiill then ramp up or down to t a pre-determ mined speed tto adequatelyy meet the coooling load of tthat aircraft. February y 10, 2012 Page 3 D. Special Requiremeents 1. Jumbo Gattes Gates that serve JB – Ju umbo Body aiircraft can be handled in tw wo different w ways. These ggates each have two PBBs. The table abov ve indicates thhat the calculaated cooling lload for a B-7747 is 71 tons. Th he two option ns for these gaates are to eithher install a 990 ton unit onn one of the bridges, orr one 60 ton unit u on each of o the two briddges. Below iis a comparisoon of these tw wo options: a. On ne 90 ton unitt: Half the amo ount of equipment requiredd Less availab ble cooling Cannot servee an RJ – nom minal capacityy is too large As only one PBB has a PCA unit all aiircraft that woould be conneected to the P PCA unit must co onnect to that bridge. wo 60 ton uniits: b. Tw Capability to o park an RJ, NB, WB, or JB. 120 tons of available a cooling PCA unit on n each PBB will w give airlinnes more flexiibility Bridge farthest from the aircraft a air co nnection willl require a lonnger duct Multiple duccts at ramp level posing a ppotential safeety hazard More equipm ment required d, therefore hiigher installedd and maintennance costs Conclusio ons The resultts of our analy ysis provide confirmation c of the directioon given by D DIA to select one manufaccturer, FCX Systtems, and two o nominal sizees (45 & 60 to ons) to be useed on the repllacement PCA A units througghout Concourse B. All gatees capable of serving s a B-7 767, B-777 orr MD-11 aircrraft will requiire a 60 ton unnit. All other gates will req quire a 45 ton unit. Any gates that servee B-747 aircraaft have two P PBBs and willl get one 60 ton n unit for each h bridge. Appendix B - Opinion of Probable Cost PROJECT CLIENTDenver International Airport PROJECT DESC: Concourse B - PCA Replacement PROJECT #: OVERALL PROJECT SUMMARY EST LEVEL: IFC ESTIMATE DUE DATE: 8/29/2014 LEAD ESTIMATOR: A. Mahobian 65967 DESCRIPTION MH LABOR COST MATERIAL COST EQUIP. & SUBCON. EQUIPMENT RENT COST TOTAL COST PCA Equipment POU Air Handling Equipment 4,822,356 6,683,800 Installation Contract Architecture Civil/Site Work Structural 3,290 269,049 194,063 74,841 645,600 Mechanical/Piping 21,600 2,293,681 65,189 325,944 3,382,900 Electrical 12,693 1,534,205 1,846,313 INSTALLATION CONTRACT SUB-TOTAL 37,583 4,096,935 2,105,565 4,056,700 400,785 ROCIP (15% of Install TIC) 8,085,200 1,212,780 PROJECT TOTAL 37,583 4,096,935 6,927,921 400,785 15,981,780 NOTE: TOTAL COSTS INCLUDE ESCALATION AND GENERAL CONDITIONS Concourse B - PCA - IFC - Cost Estimate - 082914.xls Printed 9/3/2014 12:06 PM BURNS & McDONNELL ESTIMATE PAGE 1 PROJECT CLIENTDenver International Airport PROJECT DESC: Concourse B - PCA Replacement PROJECT # : 65967 SUMMARY PCA Equipment DESCRIPTION MH P1 POU Air Handling Equipment ESTIMATE TOTALS LABOR COST MATERIAL COST SUBCON COST EQUIPMENT RENT COST TOTAL COST 4,822,356 4,822,356 $4,822,356 $4,822,356 4,822,356 SUBTOTAL GENERAL CONDITIONS 20.00% 964,471 5,786,828 5.00% 289,341 6,076,169 607,617 6,683,786 SUBTOTAL FEE SUBTOTAL SHIPPING 10.00% TOTAL Concourse B - PCA - IFC - Cost Estimate - 082914.xls EST LEVEL: IFC ESTIMATE DUE DATE: 8/29/2014 ESTIMATOR: A. Mahobian Printed 9/3/2014 12:06 PM BURNS & McDONNELL ESTIMATE PAGE 2 PROJECT CLIENTDenver International Airport PROJECT DESC: Concourse B - PCA Replacement PROJECT # : 65967 SUMMARY EST LEVEL: IFC ESTIMATE DUE DATE: 8/29/2014 ESTIMATOR: A. Mahobian PCA Equipment DESCRIPTION MH LABOR COST MATERIAL COST SUBCON COST EQUIPMENT RENT COST MARK-UP SETTINGS 1.15000 1.15000 NA NA NA 1.15000 SUBTOTALS SALES TAX 1.08000 NA NA NA 1.08000 NA NA 1.15000 1.08000 SUBTOTALS FIELD OVERHEAD 1.07000 NA 1.07000 1.08000 1.07000 NA NA 1.24200 1.07000 SUBTOTALS HOME OFFICE COSTS 1.00000 1.07000 1.00000 1.15560 1.00000 NA NA 1.32894 1.00000 SUBTOTALS SUB-CONTR. PROFIT 1.00000 1.07000 1.00000 1.15560 1.00000 NA NA 1.32894 1.00000 SUBTOTALS BOND 1.00000 1.07000 1.00000 1.15560 1.00000 NA 1.00000 1.32894 1.00000 SUBTOTALS ESCALATION TO MID 2017 1.00000 1.07000 1.00000 1.15560 1.00000 1.00000 1.00000 1.32894 1.00000 SUBTOTALS CONTINGENCY 1.15000 1.07000 1.15000 1.15560 1.15000 1.00000 1.15000 1.32894 1.15000 CTP SUBTOTAL MARKUP MULTIPLIERS G . C. O & P ON S/C WORK 1.10000 1.23050 1.10000 1.32894 1.10000 1.15000 1.10000 1.52828 1.10000 1.35355 1.46183 1.26500 1.68111 WORKING CONDIT. FACTOR TOTAL MARKUP MULTIPLIERS 1.15000 TOTAL COST INFORMATION ABOUT THE MARKUPS : "WORKING CONDITIONS FACTOR" = ADJUSTMENT FACTOR FOR UNUSUALLY DIFFICULT WORK ENVIRONMENT SUCH AS CONGESTED/CLOSE QUARTERS, HIGH ALTITUDE WORK LOCATIONS, POOR PRODUCTIVITY HISTORY, OWNER OCCUPATION OF FACILITY WHILE WORK IS IN PROGRESS, ETC. "SALES TAX" = USUALLY APPLIED ONLY TO MATERIAL AND EQUIPMENT COSTS. INCLUDES CITY, COUNTY AND STATE SALES TAX FOR THE PROJECT LOCATION. "FIELD OVERHEAD" = INCLUDES SUPERVISION, TEMPORARY UTILITIES/FACILITIES, SMALL TOOLS AND CONSUMABLES, TRUCKS, TRAILERS, ETC., MOBILIZATION AND GENERAL CONDITIONS ITEMS. THE PERCENTAGE USED IS APPLIED ACROSS THE BOARD ON LABOR, MATERIAL AND EQUIPMENT. "HOME OFFICE COSTS" = Concourse B - PCA - IFC - Cost Estimate - 082914.xls INCLUDES ESTIMATING, PURCHASING, AND OTHER ADMINISTRATIVE COSTS. Printed 9/3/2014 12:06 PM BURNS & McDONNELL ESTIMATE PAGE 3 ESTIMATE DETAIL PCA Equipment PROJECT CLIENT: Denver International Airport PROJECT DESC: Concourse B - PCA Replacement PROJECT # 65967 DESCRIPTION COSTS & RATES SHOWN BELOW INCLUDE ALL MARKUPS (SEE SETTINGS PAGE) QTY. UNIT LABOR U MH MH RATE $/MH MATERIAL TTL COST UNIT COST SUBCONTRACT TTL COST UNIT COST TTL COST EST LEVEL: IFC ESTIMATE DATE: 8/29/2014 ESTIMATOR: A. Mahobian EQUIPMENT RENT UNIT COST TTL COST UNIT COST TOTAL COST POU Air Handling Equipment Air Handling Units - 45 tons 25 EA 101.52 94202.04 2,355,051 Air Handling Units - 60 tons 5 EA 101.52 110241.29 94202.04 2,355,051 551,206 110241.29 551,206 Air Handling Units - 90 tons 5 EA 101.52 138874.23 694,371 138874.23 694,371 1. Standard Mounting Brackets 26 EA 1337.58 34,777 1337.58 34,777 2. Hose Supports, 2 Per Unit 3. 20' x 14'' Starter Hose with Scuff Strip, Wire Reinforce. Entrance Cuff: Hook Velcro 4. 20' x 14'' Hose Section of Layflat, Spiral Wound, insulated. (3) Sections Required per Gate. 70 EA 423.93 29,675 423.93 29,675 35 EA 733.84 25,684 733.84 25,684 105 EA 777.70 81,658 777.70 81,658 5. 14'' x 8'' Reducer with Scuff Strip and wire Reinforced 35 EA 308.45 10,796 308.45 10,796 6. 8'' Aircraft Coupler 35 EA 752.84 26,350 752.84 26,350 7. Remote Box - two button/mode with 75' cable 35 EA 1162.16 40,676 1162.16 40,676 8. Temperature Probe 9. 2 Section, Heavy Duty, Stainless Steel, Single Hose Trolley System for 60 Ton AHU 35 EA 475.10 16,628 475.10 16,628 30 EA 10963.76 328,913 10963.76 328,913 10. Dual Tube 4.0'' ID. Includes Mounting Brackets 35 EA 12311.57 430,905 12311.57 430,905 11. UL Certification 35 EA 730.92 25,582 730.92 25,582 12. Operations & Maintenance Manuals 13. 3 Section, Heavy duty, Stainless Stell, Double Hose Trolley for 90T units 6 EA 328.91 1,973 328.91 1,973 5 EA 33622.18 168,111 33622.18 168,111 Flex connections and Accessories (included in Unit Costs above) Accessories Cost includes: TOTALS Concourse B - PCA - IFC - Cost Estimate - 082914.xls 4,822,356 Printed 9/3/2014 12:06 PM BURNS & McDONNELL ESTIMATE 4,822,356 PAGE 4 PROJECT CLIENT Denver International Airport PROJECT DESC: Concourse B - PCA Replacement PROJECT # : 65967 SUMMARY Structural DESCRIPTION MH P1 EST LEVEL: IFC ESTIMATE DUE DATE: 8/29/2014 ESTIMATOR: A. Mahobian Miscellaneous Equipment Support and Hangers ESTIMATE TOTALS LABOR COST MATERIAL COST SUBCON COST EQUIPMENT RENT COST TOTAL COST 3,290 269,049 194,063 74,841 537,953 3,290 $269,049 $194,063 $74,841 $537,953 SUBTOTAL GENERAL CONDITIONS 20.00% $ SUBTOTAL FEE $ SUBTOTAL ENGINEERING $ TOTAL - BASE BID Concourse B - PCA - IFC - Cost Estimate - 082914.xls Printed 9/3/2014 12:06 PM BURNS & McDONNELL ESTIMATE $537,953 107,591 645,544 645,544 645,544 PAGE 5 SUMMARY PROJECT CLIENT Denver International Airport PROJECT DESC: Concourse B - PCA Replacement PROJECT # : EST LEVEL: IFC ESTIMATE DUE DATE: 8/29/2014 Structural 65967 DESCRIPTION MH ESTIMATOR: A. Mahobian LABOR COST MATERIAL COST SUBCON COST EQUIPMENT RENT COST NA NA NA NA NA NA 2.00000 NA 1.08000 TOTAL COST MARK-UP SETTINGS WORKING CONDIT. FACTOR 2.00000 2.00000 SUBTOTALS SALES TAX 1.08000 NA SUBTOTALS NA FIELD OVERHEAD 1.07000 SUBTOTALS HOME OFFICE COSTS 1.02000 SUBTOTALS SUB-CONTR. PROFIT 1.07000 SUBTOTALS BOND 1.01500 SUBTOTALS ESCALATION TO MID 2017 1.03000 SUBTOTALS CONTINGENCY 1.20000 CTP SUBTOTAL MARKUP MULTIPLIERS G . C. O & P ON S/C WORK 1.10000 TOTAL MARKUP MULTIPLIERS 2.00000 1.08000 2.00000 1.08000 NA 2.16000 1.07000 1.07000 NA 1.07000 1.07000 1.15560 NA 2.31120 1.02000 1.02000 NA 1.02000 1.09140 1.17871 NA 2.35742 1.07000 1.07000 NA 1.07000 1.16780 1.26122 NA 2.52244 1.01500 1.01500 1.01500 1.01500 1.18531 1.28014 1.01500 2.56028 1.03000 1.03000 1.03000 1.03000 1.22087 1.31854 1.04545 2.63709 1.20000 1.20000 1.20000 1.20000 1.46505 1.58225 1.25454 3.16451 1.10000 1.10000 1.10000 1.10000 1.61155 1.74048 1.37999 3.48096 INFORMATION ABOUT THE MARKUPS : "WORKING CONDITIONS FACTOR" = ADJUSTMENT FACTOR FOR UNUSUALLY DIFFICULT WORK ENVIRONMENT SUCH AS CONGESTED/CLOSE QUARTERS, HIGH ALTITUDE WORK LOCATIONS, POOR PRODUCTIVITY HISTORY, OWNER OCCUPATION OF FACILITY WHILE WORK IS IN PROGRESS, ETC. "SALES TAX" = "FIELD OVERHEAD" = USUALLY APPLIED ONLY TO MATERIAL AND EQUIPMENT COSTS. INCLUDES CITY, COUNTY AND STATE SALES TAX FOR THE PROJECT LOCATION. INCLUDES SUPERVISION, TEMPORARY UTILITIES/FACILITIES, SMALL TOOLS AND CONSUMABLES, TRUCKS, TRAILERS, ETC., MOBILIZATION AND GENERAL CONDITIONS ITEMS. THE PERCENTAGE USED IS APPLIED ACROSS THE BOARD ON LABOR, MATERIAL AND EQUIPMENT. "HOME OFFICE COSTS" = Concourse B - PCA - IFC - Cost Estimate - 082914.xls INCLUDES ESTIMATING, PURCHASING, AND OTHER ADMINISTRATIVE COSTS. Printed 9/3/2014 12:06 PM BURNS & McDONNELL ESTIMATE PAGE 6 ESTIMATE DETAIL Structural PROJECT CLIENT: Denver International Airport PROJECT DESC: Concourse B - PCA Replacement 65967 PROJECT # DESCRIPTION COSTS & RATES SHOWN BELOW INCLUDE ALL MARKUPS (SEE SETTINGS PAGE) QTY. UNIT LABOR U MH MH RATE $/MH MATERIAL TTL COST UNIT COST TTL COST SUBCONTRACT UNIT COST TTL COST EST LEVEL: IFC ESTIMATE DATE: 8/29/2014 ESTIMATOR: A. Mahobian EQUIPMENT RENT UNIT COST TTL COST UNIT COST TOTAL COST Miscellaneous Equipment Support and Hangers Minor Demolition Gate/Bridge Demolition Support Steel Additons @ 500 lbs per gate Bollards for Stand-Mounted Units 35 EA 80 2,800 80.58 225,618 1740.48 60,917 21500 LBS 0.02 430 88.64 38,113 5.22 112,261 60 EA 1 60 88.64 5,318 348.10 20,886 TOTALS Concourse B - PCA - IFC - Cost Estimate - 082914.xls 3,290 Printed 9/3/2014 12:06 PM 269,049 BURNS & McDONNELL ESTIMATE 194,063 3.48 74,841 74,841 8186.70 286,534 10.48 225,215 436.73 26,204 537,953 PAGE 7 PROJECT CLIENT Denver International Airport PROJECT DESC: Concourse B - PCA Replacement PROJECT # : 65967 SUMMARY Mechanical/Piping DESCRIPTION MH P1 Equipment, Demolition and Installation P3 Pipe, Valves and Fittings ESTIMATE TOTALS EQUIPMENT RENT COST TOTAL COST 325,944 2,684,814 21,600 $2,293,681 $65,189 $325,944 $2,684,814 20.00% SUBTOTAL 5.00% TOTAL - BASE BID Printed 9/3/2014 12:06 PM SUBCON COST 65,189 FEE Concourse B - PCA - IFC - Cost Estimate - 082914.xls MATERIAL COST 2,293,681 SUBTOTAL ITA LABOR COST 21,600 SUBTOTAL GENERAL CONDITIONS EST LEVEL: IFC ESTIMATE DUE DATE: 8/29/2014 ESTIMATOR: A. Mahobian BURNS & McDONNELL ESTIMATE $2,684,814 536,963 $ 3,221,777 $ 3,221,777 161,089 $ 3,382,866 PAGE 8 PROJECT CLIENT: PROJECT DESC: PROJECT # ESTIMATE DETAIL Mechanical/Piping Denver International Airport Concourse B - PCA Replacement 65967 DESCRIPTION EST LEVEL: IFC ESTIMATE DUE DATE: 8/29/2014 ESTIMATOR: A. Mahobian COSTS BELOW ARE MARKED UP (SEE SETTINGS PAGE) QTY. UNIT LABOR U MH MH RATE $/MH MATERIAL TTL COST UNIT COST TTL COST SUBCONTRACT UNIT COST TTL COST EQUIPMENT RENT UNIT COST TTL COST UNIT COST TOTAL COST Equipment, Demolition and Installation Demolition Existing Unit Demolition 40 EA 100 4,000 75.45 301,800 1629.72 65,189 4074.30 162,972 13249.03 529,961 4074.30 162,972 Installation Air Handling Units 40 EA 200 8,000 113.18 905,400 26709.31 1,068,373 Flex connections and Accessories 40 EA 200 8,000 113.18 905,400 22635.01 905,400 Ductwork 40 EA 40 1,600 113.18 181,080 4527.00 181,080 TOTALS Concourse B - PCA - IFC - Cost Estimate - 082914.xls 21,600 Printed 9/3/2014 12:06 PM 2,293,681 BURNS & McDONNELL ESTIMATE 65,189 325,944 2,684,814 PAGE 9 PROJECT CLIENT Denver International Airport PROJECT DESC: Concourse B - PCA Replacement PROJECT # : 65967 SUMMARY EST LEVEL: IFC ESTIMATE DUE DATE: 8/29/2014 ESTIMATOR: A. Mahobian Electrical DESCRIPTION MH LABOR COST P1 DEMO 789 95,412 P2 GATE PANELBOARD TO MCP 4,420 534,181 P3 MCP TO PCA 6,559 P4 GENERAL 925 12,693 $1,534,205 ESTIMATE TOTALS SUBTOTAL GENERAL CONDITIONS 20.00% SUBTOTAL FEE SUBTOTAL ENGINEERING TOTAL - BASE BID Concourse B - PCA - IFC - Cost Estimate - 082914.xls Printed 9/3/2014 12:06 PM BURNS & McDONNELL ESTIMATE MATERIAL COST SUBCON COST EQUIPMENT RENT COST TOTAL COST 95,412 533,400 1,067,581 792,811 751,173 1,543,984 111,802 561,739 673,541 $1,846,313 $3,380,518 $3,380,518 676,104 $ 4,056,621 $ 4,056,621 $ 4,056,621 PAGE 10 PROJECT CLIENT: PROJECT DESC: PROJECT # ESTIMATE DETAIL Electrical Denver International Airport Concourse B - PCA Replacement 65967 DESCRIPTION EST LEVEL: IFC ESTIMATE DUE DATE: 8/29/2014 ESTIMATOR: A. Mahobian COSTS BELOW ARE MARKED UP (SEE SETTINGS PAGE) QTY. UNIT LABOR U MH MH RATE $/MH MATERIAL TTL COST UNIT COST TTL COST SUBCONTRACT UNIT COST TTL COST EQUIPMENT RENT UNIT COST TTL COST UNIT COST TOTAL COST DEMO Demolish circuit breaker in panelboard 40 EA 3 120 120.87 14,504 362.60 14,504 Demolish local circuit breaker in local disconnect panel 26 EA 3.2 83 120.87 10,056 386.77 10,056 Demolish local disconnect 14 EA 3.2 45 120.87 5,415 386.77 5,415 Demolish cable from gate panelboard to local disconnect/panel 186 CLF 0.964 179 120.87 21,672 116.52 21,672 Demolish conduit from gate panelboard to local disconnect/panel 62 LF 0.106 7 120.87 794 12.81 794 Demolish cable from local disconnect/panel to pca 80 CLF 4.444 356 120.87 42,970 537.13 42,970 TOTALS Concourse B - PCA - IFC - Cost Estimate - 082914.xls 789 Printed 9/3/2014 12:06 PM 95,412 BURNS & McDONNELL ESTIMATE 95,412 PAGE 11 PROJECT CLIENT: PROJECT DESC: PROJECT # ESTIMATE DETAIL Electrical Denver International Airport Concourse B - PCA Replacement 65967 DESCRIPTION EST LEVEL: IFC ESTIMATE DUE DATE: 8/29/2014 ESTIMATOR: A. Mahobian COSTS BELOW ARE MARKED UP (SEE SETTINGS PAGE) QTY. UNIT LABOR U MH MH RATE $/MH MATERIAL TTL COST UNIT COST SUBCONTRACT TTL COST UNIT COST TTL COST EQUIPMENT RENT UNIT COST TTL COST UNIT COST TOTAL COST GATE PANELBOARD TO MCP New 3-1/C #2/0 116.25 CLF 13.2 1,535 120.87 185,470 471.67 54,832 2067.11 240,301 New 3-1/C #4/0 45 CLF 7.272 327 120.87 39,552 739.70 33,287 1618.65 72,839 New 3-1/C #400 22.5 CLF 9.412 212 120.87 25,596 1401.09 31,524 2538.68 57,120 New #4 Cu Gnd 52.5 CLF 3.018 158 120.87 19,151 150.55 7,904 515.33 27,055 New #6 Cu Gnd 60 CLF 2.462 148 120.87 17,854 95.73 5,744 393.30 23,598 4650 LF 0.246 1,144 120.87 138,259 9.57 44,513 39.31 182,772 LF 0.5 New 150A 3P Circuit Breaker 30 EA 4.572 137 120.87 16,578 5134.41 154,032 5687.01 170,610 New 200A 3P Circuit Breaker 5 EA 4.572 23 120.87 2,763 5134.41 25,672 5687.01 28,435 New 300A 3P Circuit Breaker 5 EA 6.4 32 120.87 3,868 6439.77 32,199 7213.32 36,067 New Control Panel with 60A Circuit Breaker for Gate and Xfrmer 16 EA 44 704 120.87 85,090 8980.87 143,694 14299.00 228,784 2" GRC 3" GRC 120.87 22.63 60A 3P circuit breaker for Gate 20 ft of 500 KCMIL 15 A 2p Circuit Breaker 480-120/240 5 Kva Transformer 3 20A 1P circuit breakers 30"H x 24"W x 12"D Nema 4X enclosure Reconnection of all existing equipment TOTALS Concourse B - PCA - IFC - Cost Estimate - 082914.xls 4,420 Printed 9/3/2014 12:06 PM 534,181 BURNS & McDONNELL ESTIMATE 533,400 1,067,581 PAGE 12 PROJECT CLIENT: PROJECT DESC: PROJECT # ESTIMATE DETAIL Electrical Denver International Airport Concourse B - PCA Replacement 65967 DESCRIPTION EST LEVEL: IFC ESTIMATE DUE DATE: 8/29/2014 ESTIMATOR: A. Mahobian COSTS BELOW ARE MARKED UP (SEE SETTINGS PAGE) QTY. UNIT LABOR U MH MH RATE $/MH MATERIAL TTL COST UNIT COST TTL COST SUBCONTRACT UNIT COST TTL COST EQUIPMENT RENT UNIT COST TTL COST UNIT COST TOTAL COST MCP TO PCA New 200A 3P NF Disconnect EA 13.334 New 150A 3P CIRCUIT BREAKER IN LOCAL DISCONNECT PNL 14 EA 4.572 64 120.87 120.87 7,736 5134.41 1575.13 71,882 5687.01 79,618 New 200A 3P CIRCUIT BREAKER IN LOCAL DISCONNECT PNL 5 EA 4.572 23 120.87 2,763 5134.41 25,672 5687.01 28,435 New 300A 3P CIRCUIT BREAKER IN LOCAL DISCONNECT PNL 5 EA 6.4 32 120.87 3,868 6439.77 32,199 7213.32 36,067 New 1-3/C #2/0 & #6 GND, AIRCRAFT JET BRIDGE CABLE 60 CLF 17.68 1,061 120.87 128,215 3045.84 182,750 5182.76 310,966 New 1-3/C #4/0 & #6 GND, AIRCRAFT JET BRIDGE CABLE 10 CLF 23.312 233 120.87 28,176 4777.61 47,776 7595.26 75,953 New 1-3/C #400 & #4 GND, AIRCRAFT JET BRIDGE CABLE 10 CLF 36.54 365 120.87 44,165 11241.75 112,418 15658.22 156,582 INSTALLING LOCAL CONTROL STATION 35 EA 6 210 120.87 25,382 725.20 25,382 New 1-6/C #14, AIRCRAFT JET BRIDGE CABLE 800 CLF 5.714 4,571 120.87 552,505 1038.73 830,982 TOTALS Concourse B - PCA - IFC - Cost Estimate - 082914.xls 6,559 Printed 9/3/2014 12:06 PM 792,811 BURNS & McDONNELL ESTIMATE 348.10 278,477 751,173 1,543,984 PAGE 13 PROJECT CLIENT: PROJECT DESC: PROJECT # ESTIMATE DETAIL Electrical Denver International Airport Concourse B - PCA Replacement 65967 DESCRIPTION EST LEVEL: IFC ESTIMATE DUE DATE: 8/29/2014 ESTIMATOR: A. Mahobian COSTS BELOW ARE MARKED UP (SEE SETTINGS PAGE) QTY. UNIT LABOR U MH MH RATE $/MH MATERIAL TTL COST UNIT COST SUBCONTRACT TTL COST UNIT COST TTL COST EQUIPMENT RENT UNIT COST TTL COST UNIT COST TOTAL COST GENERAL Misc Electrical Controls & Instrumentation Reprogramming System 1 LS 645 Pts 1 645 1 LS 240 240 TOTALS Concourse B - PCA - IFC - Cost Estimate - 082914.xls 40 40 925 Printed 9/3/2014 12:06 PM 120.87 4,835 435.12 435 120.87 77,959 870.24 561,304 120.87 29,008 111,802 BURNS & McDONNELL ESTIMATE 561,739 5269.78 5,270 991.11 639,263 29007.98 29,008 673,541 PAGE 14 Appendix C – Product Data DAS-CI-50-US Series TAD Telescoping Air Duct Cavotec INET has a proud history of being at the forefront of new technology applications to increase efficiency for practical fixed pre-conditioned air and 400Hz ground power systems. General information As part of Cavotec INET’s PCA System, Cavotec INET’s Series TAD Telescoping Air Duct assembly is designed to transport cold or hot preconditioned air (pc air) across the telescoping sections of an apron-drive passenger boarding bridge. With thousands of gates in service world-wide since 1984, these units have demonstrated an extremely high level of reliability and maintenance-free long life. The duct is fully insulated, flame-proof and smoke retardant, with significant air losses and pressure drop. TAD with PCA basket hose The TAD is comprised of sections of fiberglass and internal insulating urethane foam. The complete TAD assembly as shipped includes the telescoping duct sections, seals, bearings, mounting clamps and bridge mounting brackets. Units may be mounted either on the top, side or underneath the boarding bridge. They are available in either 2-tunnel or 3-tunnel versions. Cavotec INET custom-configures the assemblies to fit the unique models by any of the many passenger bridge companies worldwide, as determined by detailed coordination during the project. They are typically supplied in a finish to match or complement the bridge color scheme. The TAD is a Cavotec INET innovation covered by patent in the US and several other countries. High insulation properties STANDARD FEATURES • Light-weight fiberglass three layers • Allows mounting of AHU with no weight on bridge • Internal urethane foam insulation between fiberglass • Pressure rating exceeds all pc air requirement • Efficient insulation: no condensation • Air seals allow insignificant air leakage • ETL, UL, and CSA Standards • No maintenance required for 10 years Integration onto the PBB • • • • Greater than 20-year life for ducts/bearings 2-tunnel or 3-tunnel models available Side or under-bridge mounting Cavote INET custom configurations for any boarding bridge • Custom colors to match boarding bridge finish General design notes The Cavotec INET TAD is covered under US and several international patents and is installed at over 3,000 gates world wide. The TAD assembly is comprised of either 2 or 3 sections which fit into one another, allowing it to expand or contract together with the boarding bridge to which it is mated. The TAD presents a smoothwalled, well insulated path for the air flow, with minimum pressure drop and heat gain, and with no condensation at design temperatures with supply air to -50°C. It is made in sections of 14”/16”/18” for 3-tunnel models. It is normally supplied with all mounting clamps to be attached to points on the bridge as coordinated with the bridge factory. Materials/methods/specifications - Series Tad Outer and inner duct layers are hand laid-up plies of fiberglass cloth impregnated and treated with fire-proof and smoke-retardant resin. Between the inner and outer fiberglass layers is 1/4 inch thickness of urethane foam insulation. Self-centering bearings are teflon-derivative solid, all around 20-yr life. Seals have minimum 10-yr life, of alimorphic solid foam, 4 per section. Overall assembly is proven and tested flame-proof and not to produce smoke or any toxic fumes at prolonged fire and super-heated air, in accordance with LUL and CSA standards, tested by MT Labs. Maximum Pressure: Maximum Airflow: Internal Air Temp: Ambient Temp: Temp rises @37°C amb, 440 lb/min: Air loss: Weight Estimates (depends on configuration): Diameter: Insulation K-factor, BTU/hr/degF/ft2 1200mm H20 280 kg/min -20°C to +90°C -30°C to +55°C 0.5°C <0.5% new, 1% @ 5 years about 220 kg for 3-tunnel 18” (457mm) outer duct 16” (406)mm) 2nd duct 14” (355mm) inner* - insulation layer: K=0.5 - overall assembly, effective K=0.31 Important Note: The application data shown on this data sheet depicts a basic unit for standard design ambient conditions with the most common outlet air delivery conf igurations. Other performance models may be selected by the factory to optimize operating conditions for a given aircraft mix, climate, altitude, and installation factors. It is suggested that this data be used as an initial guide only, pending analysis of full system operating requirements by Cavotec INET application engineering staff. *If needed Illustrations 2-tunnel TAD at DFW International Airport, one of 48 installed in 1987. Notice air handler mounted to bridge rotunda column, with no weight transferred to any of the bridge sections. Bridge and tire life are not at all impaired. Duct is mounted to side of bridge to allow full use of underbridge area for vehicle traffic. Seals have been replaced in 2000, after 13 years of operation. Bearings and ducts are original. 2-tunnel TAD at Brussels International Airport, one of 53 installed bewteen 1992 and 2002. Notice that in this case the TAD is mounted to the underside of the bridge, since the glass-walled bridges made esthetic appearance from inside the bridge an important consideration, and no traffic was expected below the bridge. In this case, the AHU is ground-mounted due to architectural considerations. Bridge life is not affected by the pc air system. In addition to specific PCA distribution systems, Cavote INET engineers and manufacture a wide range of PCA mobile and fix AHU (Point of Use or Central System) - please contact us for any inquiry. 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(ÿ)"(8)!ÿ*!ÿ8(1W1$*))*!(#ÿ'G1>C1ÿ !"#$"%%ÿ,!(*,(ÿ+!W)/*(+!-ÿ%"*:"ÿX);+0"U / 08%"ÿ(ÿ !"#$"%%)08,(ÿ/ 0"% R L=")"ÿ+:ÿ! ÿ)"(8)!ÿW)ÿ)"X*+)1*!01)"(8)!ÿ:")1 E" +*%ÿ!8/F") ;+,"ÿ*;*+%*F%"ÿW)ÿ*!#ÿWÿ(="ÿTV1DO3ÿ)ÿ <8)/F ")ÿWÿ(="ÿ0"W",( TV1POOÿ:")+":ÿX)08,(: <*(8)"ÿWÿ0"W",( f^]f\[\ÿZÿ ^^_][^ÿ\[] ÿÿÿ !"#$"%%ÿ'!(")!*(+!*%ÿ'!, !"#$"%%ÿ.+/+("01 !"#$"%%ÿ.+/+(2" 3456ÿ7 89%*:ÿ7)+;"ÿ< )(= >6ÿ7#!*/+,ÿ7)+;" ? %0"!ÿ@*%%"#AÿB<ÿÿ66CDD E,*)F )89=AÿG!(*)+ÿÿB3@ÿCH4 ,8:(/")-= !"#$"%%-,/ IÿJ-E-ÿK"9+:(")"0ÿL)*0"/*)M NÿDOOPÿ !"#$"%%ÿ'!(")!*(+!*%ÿ'!,461QQ6>RO3ÿÿÿÿÿÿÿÿÿÿS-H-ÿÿÿÿÿÿÿÿÿÿO51OQÿ 8 7 5 6 4 2 3 1 D 87.75 D C C 7.62 16.86 98.77 14.00 OUTLET B 26.22 59.00 B 26.61 114.00 UNLESS OTHERWISE SPECIFIED: DIMENSIONS ARE IN INCHES TOLERANCES: ANGULAR: .5 DEG TWO PLACE DECIMAL .015 THREE PLACE DECIMAL .005 FOUR PLACE DECIMALS .0005 A PCS. REQ'D. MATERIAL PROPRIETARY AND CONFIDENTIAL THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF TWIST INC.. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT THE WRITTEN PERMISSION OF TWIST INC. IS PROHIBITED. 8 7 6 5 USED ON NEXT ASSY APPLICATION 4 HEAT TREAT DRAWN NAME DATE JRK 4/9/13 TWIST AERO JAMESTOWN, OHIO. U.S.A. TITLE: CHECKED THIRD ANGLE PROJECTION - SIZE DWG. NO. COMMENTS: - B 2 A REV PCA045480WH A SHEET 1 OF 1 SCALE: 1:30 WEIGHT: DO NOT SCALE DRAWING 3 TWIST INC 45 TON PCA PCA045480WH 1 8 7 5 6 4 2 3 1 D 87.75 D C C 7.62 16.86 98.77 14.00 OUTLET B 26.22 59.00 B 26.61 114.00 UNLESS OTHERWISE SPECIFIED: DIMENSIONS ARE IN INCHES TOLERANCES: ANGULAR: .5 DEG TWO PLACE DECIMAL .015 THREE PLACE DECIMAL .005 FOUR PLACE DECIMALS .0005 A PCS. REQ'D. MATERIAL PROPRIETARY AND CONFIDENTIAL THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF TWIST INC.. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT THE WRITTEN PERMISSION OF TWIST INC. IS PROHIBITED. 8 7 6 5 USED ON NEXT ASSY APPLICATION 4 HEAT TREAT DRAWN NAME DATE JRK 4/9/13 TWIST AERO JAMESTOWN, OHIO. U.S.A. TITLE: CHECKED THIRD ANGLE PROJECTION - SIZE DWG. NO. COMMENTS: - B 2 A REV PCA060480WH A SHEET 1 OF 1 SCALE: 1:30 WEIGHT: DO NOT SCALE DRAWING 3 TWIST INC 60 TON PCA PCA060480WH 1 8 5 6 7 4 2 3 1 D 87.75 D C C 23.61 16.73 102.77 2X B 26.70 62.00 B 14.00 OUTLET 21.93 42.93 150.00 UNLESS OTHERWISE SPECIFIED: DIMENSIONS ARE IN INCHES TOLERANCES: ANGULAR: .5 DEG TWO PLACE DECIMAL .015 THREE PLACE DECIMAL .005 FOUR PLACE DECIMALS .0005 A PCS. REQ'D. MATERIAL PROPRIETARY AND CONFIDENTIAL THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF TWIST INC.. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT THE WRITTEN PERMISSION OF TWIST INC. IS PROHIBITED. 8 7 6 5 USED ON NEXT ASSY APPLICATION 4 HEAT TREAT DRAWN NAME DATE JRK 6/25/13 SPRING TWIST INC 90 TON PCA PCA090480WH THIRD ANGLE PROJECTION SIZE DWG. NO. COMMENTS: B - PCA090480WH 2 A REV A SHEET 1 OF 1 SCALE: 1:30 WEIGHT: DO NOT SCALE DRAWING 3 SPECIALIST TITLE: CHECKED - TWIST INC. JAMESTOWN, OHIO. U.S.A. 1 PRODUCT SHEET: RAMPTECH High Performance Non-Metallic PCA Adapters The RAMPTECH PCA adapters are the best adapters ever made. They are built for safety. Built for the airport. Built to last. Safety first. Metal adapters can get crushed or as they drag along the ground, get sharp, dangerous edges. These sharp edges can be dangerous to personnel. The sharp edges can damage the hose as well. RAMPTECH PCA patented plastic adapters resist getting crushed and eliminates the sharp edges. Sage Parts offers high performance RAMPTECH PCA adapters in all sizes for every need, including 8-inch x 8-inch, 8-inch x 12-inch, 8-inch x 14-inch, and 45-degree swivel adapters. BETTER. BY DESIGN. RAMPTECH PCA adapters are setting a new standard for quality. With their patented non-metallic design, RAMPTECH PCA adapters MB828 MB845 are specifically engineered to outperform other brands by resisting corrosion that can compromise the performance of metallic adapters. RAMPTECH PCA adaptors are made of high-density, high-impact polyethylene for exceptional durability, even in the most demanding airport environments. Withstands hot and cold temperature extremes Provides a consistently airtight fit Will not shake loose due to vibrations or air blasts All stainless steel clamps and hardware Fits any aircraft and any locking configuration Ergonomic handles for easy latching Resistant to chemicals and UV rays Never needs paint, will not dent Replaceable parts, including the AC mating gasket Sage Parts 30 Hub Drive, Melville, NY 11747 +1.877.SAGE.877 | +1.631.501.1300 Tel +1.631.501.1619 Fax [email protected] Anticipating needs, meeting demands. Reducing cost. www.sageparts.com PRODUCT SHEET: RAMPTECH BridgeCool Double Insulated, Wire-Reinforced PCA Duct OUTER SHELL The 16 oz./yd.² (542 g/m²) opaque, high-polish white PVC/polyester outer shell is designed to shield pre-conditioned air from the heating effects of the sun’s rays. The outer shell features mold and mildew inhibitors and is UV stabilized for protection against harmful sun degradation. MADE IN THE USA 16 oz. High-Polish White PVC/Polyester Outer Shell Temptrol Outer Radiant Heat Barrier and Insulation Layer SBP Inner Insulation Layer 11 oz. Inner Liner Designed specifically for fixed Jet Bridge applications Cool your Jet Bridges more efficiently with our newly introduced double insulated BridgeCool Ducting BridgeCool is made with a unique 4-ply construction featuring an outer layer of white Black-Out material designed to block the suns UV rays. This UV resistant outer layer Helps the BridgeCool product outlast the competition even in the harshest of environments. The double insulation layers act as a radiant heat barrier that keeps both the heat out and the cool in. The duct is supported by two helixes of wire re-enforcement, helping BridgeCool ducting to retain is shape. These enhanced design features allow you’re A/C units to operate more efficiently with greater cost effectively. The unique composition of the products used in manufacturing this product offer a greater life, thus reducing the total cost of ownership. OUTER INSULATION LAYER The outer insulation layer is a patented polypropylene fabric that is metalized on one side for superb radiant heat insulation. Its unique construction allows the material to flex without cracking or flaking. The material is also designed to inhibit growth of fungi and bacteria. INNER INSULATION LAYER The inner insulation layer consists of stitch-bonded polyester insulation similar to the high performance material found in cold weather clothing and camping products. INNER LINER The inner sleeve is made of VentaTex® 11-1812 high strength material, an 11 oz./yd.² (373 g/m²), threeply PVC fabric manufactured by ABC Industries, Inc. VentaTex® 11-1812 is specially designed to eliminate delamination commonly found in other inner liners. It is constructed by compressing high-tenacity, high-density polyester yarn between PVC films. Sage Parts 30 Hub Drive, Melville, NY 11747 +1.877.SAGE.877 | +1.631.501.1300 Tel +1.631.501.1619 Fax [email protected] Anticipating needs, meeting demands. Reducing cost. www.sageparts.com PRODUCT SHEET: RAMPTECH BridgeCool Double Insulated, Wire-Reinforced PCA Duct MADE IN THE USA Specifications: RAMPTECH BridgeCool Double Insulated, Wire-Reinforced PCA Duct TEMPERATURE -20° to 180° F (-29° to 82° C) DIAMETER 8”, 10”, 12”, & 14” (200 mm, 254mm, 300 mm, 350 mm) LENGTH Per Customer Specification COLOR High-Polish White OPTIONAL ENDS Soft Cuff , sized per application requirement Accessories: Reducers 12 to 8, 14 to 8 Elbows 45 and 90 Degree 8,12 and 14” Reducing Elbows All Configurations Starter Sections Machine Connection to Duct Transition Sections To convert from one style end to another Sage Parts 30 Hub Drive, Melville, NY 11747 +1.877.SAGE.877 | +1.631.501.1300 Tel +1.631.501.1619 Fax [email protected] Anticipating needs, meeting demands. Reducing cost. www.sageparts.com PRODUCT SHEET: RAMPTECH PREMIUM PCA LAYFLAT DUCTING Above. And beyond. MADE IN THE USA There simply is no better PCA layflat ducting available on the market today. RAMPTECH® Premium PCA layflat ducting from Sage Parts features the finest engineering... assuring the highest level of performance for the most demanding positive pressure applications. OUTER SHELL Heat-sealed (welded) design, high resistance to external abrasion and ultra-durable overall construction combine with flexibility to deliver everything you want in a top quality PCA layflat ducting product that meets UL94VTM-O standards. But that’s not all. Unique spiral construction enables the addition of a military-spec scuff strip that protects the entire duct – reducing fatigue and resulting in incredibly long service life. Other vital advantages include an extended inner liner, and elastic seals at connection points to minimize air loss, as well as excellent UV stabilization, and mold and mildew inhibitors. INSULATION LAYER The outer shell is comprised of VentaTex® 20XHDMW 3-ply, 20 ounce/ square yard (678 g/m²) high-strength PVC fabric and black wearstrip that meets military specifications. To improve abrasion resistance, nine millimeters of high-density molecular weight PVC is added to the external wear surface. The custom laminate is produced by compressing high strength, multi-denier, uni-directional Ripstop polyester yarns between PVC films. Finished material thickness is 0.029 inches (0.737 mm). The middle layer consists of stitch-bonded polyester insulation similar to the high performance material found in cold weather clothing and camping products. INNER LINER The inner sleeve is made of VentaTex® 11-1812 high-strength material, and 11 ounce/square yard (373 g/m²), 3-ply PVC fabric VentaTex® 11-1812 is specially designed to eliminate delamination, which is commonly found in other inner liners. It is constructed by compressing high tenacity, high density polyester yarn between PVC films. Finished material thickness is 0.017 inches (0.432 mm). Sage Parts 30 Hub Drive, Melville, NY 11747 +1.877.SAGE.877 | +1.631.501.1300 Tel +1.631.501.1619 Fax [email protected] www.sageparts.com PRODUCT SHEET: RAMPTECH PREMIUM PCA LAYFLAT DUCTING MADE IN THE USA SPECIFICATIONS: RAMPTECH PREMIUM LAYFLAT TEMPERATURE -20° to +180° F (-29° to +82° C) DIAMETER 8 in, 12 in, and 14 in (203.2 mm, 304.8 mm, 355.6 mm) Other diameters available upon request LENGTH 10 ft, 20 ft, 25 ft, 50 ft (3.04 m, 6.09 m, 7.62 m, 15.24 m) Custom lengths available upon request WEARSTRIP Heavy-Duty Military Specification, Abrasion Resistant COLOR Yellow with black wearstrip OPTIONAL ENDS Fold Over Velcro® Cuff, Soft Cuff, or Zipper Cuff ACCESSORIES AVAILABLE Reducers Diameters of 12 to 8 inches 14 to 8 inches Elbows Diameters of 8, 12, and 14 inches Angles of 45 and 90 degrees Starter Sections Diameters of 8, 12, and 14 inches Lengths at 3, 5, and 8 feet Custom available upon request Transition Sections Diameters of 12 and 14 inches Cuff combinations are Zipper to Velcro, Velcro to Zipper, Soft Cuff to Velcro, and Soft Cuff to Zipper Reducing Elbows 14 to 8 inches at 90 degrees 14 to 8 inches at 45 degrees Wye 8x8x8 inches 12x12x12 inches of any cuff combination Clamps 8 inch - Part Number 501197 12 inch - Part Number 501198 14 inch - Part Number 501199 Sage Parts 30 Hub Drive, Melville, NY 11747 +1.877.SAGE.877 | +1.631.501.1300 Tel +1.631.501.1619 Fax [email protected] www.sageparts.com PRODUCT SHEET: RAMPTECH SPIRAL REINFORCED INSULATED DUCTING Stronger, smarter. Better. When it comes to ducting for pre-conditioned air (positive pressure) applications, strength is imperative. And so is smart engineering. RAMPTECH® spiral reinforced insulated ducting from Sage Parts is intelligently designed in and out – built to perform better than any other brand. All three layers of RAMPTECH® spiral reinforced insulated ducting...outer layer, insulation layer and inner layer...are constructed of the finest materials to provide incomparable durability no matter how challenging the ramp demands are. Plus, welded construction and flame resistance combine with top-notch UV stabilization and mold and mildew inhibitors to elevate performance and durability even higher. MADE IN THE USA OUTER SHELL The outer shell is comprised of VentaTex® 20XHDMW 3-ply, 20 ounce/ square yard (678 g/m²) high strength PVC fabric and black wearstrip that meets military specifications. To improve abrasion resistance, nine millimeters of high density molecular weight PVC is added to the external wear surface. The custom laminate is produced by compressing highstrength, multi- denier, uni-directional Ripstop polyester yarns between PVC films. Finished material thickness is .029 inches (0.737 mm). INSULATION LAYER The middle layer consists of stitch-bonded polyester insulation similar to the high performance material found in cold weather clothing and camping products. INNER LINER The inner sleeve is made of VentaTex®11-1812 high strength material, and 11 ounce/square yard (373 g/m²), 3-ply PVC fabric VentaTex®11-1812 is specially designed to eliminate delamination commonly found in other inner liners. It is constructed by compressing high tenacity, high density polyester yarn between PVC films. Finished material thickness is 0.017 inches (0.432 mm). Sage Parts 30 Hub Drive, Melville, NY 11747 +1.877.SAGE.877 | +1.631.501.1300 Tel +1.631.501.1619 Fax [email protected] www.sageparts.com PRODUCT SHEET: RAMPTECH SPIRAL REINFORCED INSULATED DUCTING MADE IN THE USA Specifications: RAMPTECH SPIRAL REINFORCED INSULATED DUCTING TEMPERATURE -20° to 180° F (-29° to 82° C) STANDARD PITCH 4”, 6” WIRE Hard-Drawn Steel DIAMETERS 8”, 12” & 14” (203.2 mm, 304.8 mm, 355.6 mm) Other diameters available upon request. COLOR Yellow WEARSTRIP Heavy-Duty Black (Military Spec) OPTIONAL ENDS Fold Over Velcro® Cuff, Soft Cuff, or Zipper Cuff Accessories: Reducers 12 to 8 14 to 8 Elbows 45 and 90 Degree 8,12 and 14” Reducing Elbows All Configurations Starter Sections Machine Connection to Duct Transition Sections To convert from one style end to another Sage Parts 30 Hub Drive, Melville, NY 11747 +1.877.SAGE.877 | +1.631.501.1300 Tel +1.631.501.1619 Fax [email protected] www.sageparts.com PRODUCT SHEET: RAMPTECH ULTRALYTE™ PCA LAYFLAT DUCTING MADE IN THE USA Lightweight construction. Heavy-duty performance. It’s the best of both worlds. RAMPTECH® UltraLyteTM PCA layflat ducting from Sage Parts revolutionizes PCA ducting design by combining super lightweight convenience with unsurpassed performance to tackle any and all rigors the aviation industry can throw at it. Reinforced seams are lockstitched with high-strength polyester thread. The result? No unraveling. And three-ply fabric prevents wicking and will not degrade when exposed to Skydrol or other ramp chemicals, providing outstanding durability. It all adds up to longer service life, extensive cost savings and strong return on investment over the product lifecycle. OUTER SHELL The high-strength yellow ballistic nylon outer shell is urethane coated for much better abrasion resistance than any lightweight PCA ducting available today. The fabric is resistant to the usual degrading effects of Glycol Alcohol or Skydrol exposure. Additionally, the outer shell is UV stabilized for protection against harmful sun degradation. INSULATION LAYER The middle layer is a patented polypropylene fabric that is metalized on one side for superb radiant heat insulation. Its unique construction allows the material to flex without cracking or flaking. The material is also designed to inhibit growth of fungi and bacteria. INNER LINER The high-strength inner liner consists of a tightly woven, rip-resistant, urethane-coated nylon material, which is designed to withstand the heavy wear associated with the airline industry. Sage Parts 30 Hub Drive, Melville, NY 11747 +1.877.SAGE.877 | +1.631.501.1300 Tel +1.631.501.1619 Fax [email protected] www.sageparts.com PRODUCT SHEET: RAMPTECH ULTRALYTE™ PCA LAYFLAT DUCTING MADE IN THE USA Specifications: RAMPTECH ULTRALYTE™ Layflat MATERIAL WEIGHT Outer Shell: 9.3 oz/yd² (315 g/m²) Inner: 5.9 oz/yd² (200 g/m²) TEMPERATURE -20° to +180° F (-29° to +82° C) TRAPEZOID TEAR Outer Shell: Warp=110 lb/in² (77,338 kg/m²) | Fill=70 lb/in² (49,215 kg/m²) Inner Liner: Warp=85 lb/in² (59,761 kg/m²) | Fill 30 lb/in² (21,092 kg/m²) ABRADE TO FAILURE Outer Shell: 2,125 Cycles DIAMETER 8 in, 12 in, and 14 in +/- 1/4 in (203.2mm, 304.8 mm, 355.6 mm) LENGTH 10 ft, 15 ft, 20 ft, 25ft, 30 ft (3.04 m, 4.57 m, 6.09 m, 7.62 m, 9.14 m) COLOR Yellow (other colors available upon request) OPTIONAL ENDS Fold Over Velcro® Cuff, Soft Cuff, or Zipper Cuff ACCESSORIES AVAILABLE Reducers Diameters of 12 to 8 inches 14 to 8 inches Elbows Diameters of 8, 12, and 14 inches Angles of 45 and 90 degrees Starter Sections Diameters of 8, 12, and 14 inches Lengths at 3, 5, and 8 feet Custom available upon request Transition Sections Diameters of 12 and 14 inches Cuff combinations are Zipper to Velcro, Velcro to Zipper, Soft Cuff to Velcro, and Soft Cuff to Zipper Reducing Elbows 14 to 8 inches at 90 degrees 14 to 8 inches at 45 degrees Wye 8x8x8 inches 12x12x12 inches of any cuff combination Clamps 8 inch - Part Number 501197 12 inch - Part Number 501198 14 inch - Part Number 501199 Sage Parts 30 Hub Drive, Melville, NY 11747 +1.877.SAGE.877 | +1.631.501.1300 Tel +1.631.501.1619 Fax [email protected] www.sageparts.com REVISION TABLE DESCRIPTION INITIAL DESIGN - NOT FOR RELEASE - REV + - DATE - APPROVED - TELESCOPING AIR DUCT (TAD TUBE) PASSENGER BOARDING BRIDGE FLEXIBLE TRANSITION HOSE LOWER OR UPPER BRIDGE EDGE MOUNTING AVAILIBLE (LOWER SHOWN) OUTLET TO CONNECT TO HOSE STORAGE DEVICE. STAND MOUNTED PCA UNLESS OTHERWISE SPECIFIED: DIMENSIONS ARE IN INCHES TOLERANCES: ANGULAR: .5 DEG TWO PLACE DECIMAL .015 THREE PLACE DECIMAL .005 FOUR PLACE DECIMAL .0005 PROPRIETARY AND CONFIDENTIAL 4 CHECKED 3 TWIST INC. DATE SES 7/29/14 - - JAMESTOWN, OHIO. U.S.A. TITLE: THIRD ANGLE PROJECTION MATERIAL THE INFORMATION CONTAINED IN THIS Material DRAWING IS THE SOLE PROPERTY OF TWIST INC. HEAT TREAT ANY REPRODUCTION IN PART OR AS A WHOLE Heat Treat WITHOUT THE WRITTEN PERMISSION OF TWIST INC. IS PROHIBITED. DO NOT SCALE DRAWING 5 NAME DRAWN SIZE COMMENTS: A TWIST INC SAMPLE TAD-TUBE INSTALLATION REV DWG. FMC NO. BRIDGE LAYOUT 3T - TUNNEL PRJ. NO. PRX-XXXXXX + SCALE: 1:150WEIGHT: Weight SHEET 1 OF 2 2 1 UNLESS OTHERWISE SPECIFIED: DIMENSIONS ARE IN INCHES TOLERANCES: ANGULAR: .5 DEG TWO PLACE DECIMAL .015 THREE PLACE DECIMAL .005 FOUR PLACE DECIMAL .0005 PCS. REQ'D. PROPRIETARY AND CONFIDENTIAL THE INFORMATION CONTAINED IN THIS DRAWING IS THE SOLE PROPERTY OF TWIST INC.. ANY REPRODUCTION IN PART OR AS A WHOLE WITHOUT THE WRITTEN PERMISSION OF TWIST INC. IS PROHIBITED. MATERIAL HEAT TREAT NEXT ASSY USED ON APPLICATION 5 4 _______ DRAWN NAME DATE SES 7/29/14 TWIST INC. SPECIALIST JAMESTOWN, OHIO. U.S.A. TITLE: CHECKED TWIST INC SAMPLE TAD-TUBE INSTALLATION THIRD ANGLE PROJECTION COMMENTS: _______ SIZE DWG. NO. REV A + FMC BRIDGE LAYOUT 3T - TUNNEL _______ SHEET 2 OF 2 SCALE: 1:200WEIGHT: Weight1304212.743 DO NOT SCALE DRAWING 3 SPRING 2 1 2.07 AIR DELIVERY EQUIPMENT Telescoping Rigid Insulated Air Duct (TAD) - For Transporting Preconditioned Air Across the Sections of 3-Tunnel Passenger Loading Bridges: 1. General: The telescoping air duct shall be a complete assembly of rigid insulated tubing sections, air seals or gaskets, guide bearings, brackets and other mounting and alignment devices. It shall be designed to extend and retract during the full range of motion of a telescoping passenger loading bridge to which it is attached. It shall be extensively proven in service to withstand thousands of bridge motion cycles while carrying air at the specified conditions from a fixed-mounted air handler at the terminal end of a loading bridge to a connection of flexible duct at the aircraft-end of the bridge. 2. Manufacturer Experience: The telescoping air duct shall be the regular product of a company who has designed, manufactured, and installed no less than 300 units that are currently in service as specified herein, with at least 100 currently-installed units of this same design in continuous service on passenger loading bridges for a minimum of 10 years. The full-retract and full-extend lengths shall be as required to install on the loading bridges as defined in the bid documents or other bridge definition documents. 3. Ratings: The TAD shall be rated to carry pressurized air at up to 1,000 mm column of H2O at temperatures between -5°C and +65°C. In order to accommodate the required airflows within acceptable pressure drop limits, the inner diameter of the smallest section of duct shall be at least 350mm. In addition, the construction shall allow extension and retraction of the duct assembly while mounted on the bridge, for a minimum of 50,000 full cycles or ten years, without requiring inspection or any scheduled maintenance. This shall be proven in practice by a minimum of 100 previously-installed units. 4. Materials and Construction: Telescoping air duct shall be rigid cross-bridge, shall be foam core fiber glass with minimum 1/8" inner and outer fiberglass layer for rigid construction. Polyurethane insulation core shall be flame retardant. Fireproof and smoke proof, as tested and demonstrated according to approved NFPA procedures, with records of such successful testing on existing products previously installed to be submitted as requested by the Owner. Telescoping section shall have Teflon bearings and foam seals to minimize air leaks. Seals shall be provided as necessary to limit air leakage during operation to less than 1% under the above rated air pressure conditions. The number of telescoping sections shall match the number of tunnels of the passenger loading bridge at each gate. Provide no hindrance or resistance to bridge retraction or extension in excess of 50kg of force opposing the bridge motion. Cause no limitation of bridge retraction or extension limits be reason of its mounting method beyond a small amount which may be approved by the Owner. The telescoping air duct shall be of the type and design proven at similar airport installations at a minimum of 100 gates. Furnish telescoping duct with all brackets and supports as recommended by the manufacturer's installation requirements (where required). TAD to be designed to maximize airflow and minimize heat gains when utilizing subfreezing air flow. 5. Mounting: Each telescoping duct assembly shall be provided with a full set of mounting clamps and brackets to attach to the bridge in a manner as coordinated with the bridge manufacturer during the project design process. It is the responsibility of the PLB manufacturer to mount TAD brackets under the supervision of the PCA supplier. 6. Shipping: Each telescoping duct assembly shall be shipped complete, as an assembly, with all two or three sections retracted into one another. Each assembly shall be marked on the outside of its wrapping with bridge or gate number ID, along with its mounting bracket kit, as established during the project coordination process. 7. Drawings and coordination: The manufacturer shall provide mounting installation guide and adequate information to the coordination process with the bridge manufacturer. Following complete coordination, the manufacturer shall provide full set of installation drawings and process description, matched gate-by-gate for each appropriate bridge. WEB-201, WEB-600, CP-201 and CP-600 Series Controllers INSTALLATION INSTRUCTIONS BEFORE INSTALLATION 1. 2. 3. 4. Unpack the controller. Inspect contents of the package for damaged or missing components. Check the equipment and report any damage to a Honeywell representative at once and return any damaged components for immediate repair or replacement. See RETURNING A DEFECTIVE UNIT section. Read all of these instructions and ensure they are understood. Included in this Package GENERAL This document covers the mounting and wiring of the Honeywell WEB-201, CP-201, WEB-600 and CP-600 Series Controllers. It is assumed that the installer is a trained engineer, technician, or service person, and is fully qualified to install control systems. Instructions in this document apply to the following products. Please read this entire document before beginning the installation procedures. NOTE: Not covered in this document is the Niagara AX™ software installation and configuration required for a fully functioning unit. This includes setting host IP address and password, serial port configuration, and other parameters. Refer to the Niagara AX Install and Setup Guide for this information. In addition, the mounting and wiring of expansion options are covered in separate documents. See sections EXPANSION OPTIONS and RELATED DOCUMENTATION. WEB-201 The power module, purchased separately, can be one of the following: — NPB-PWR-H (formerly WEB-NPB-PWR): 24 Vac or 24 Vdc input, DIN-mount capable, with grounding wire, — NPB-PWR-UN-H 90-263 Vac input, DIN-mount capable, with grounding wire, or — NPB-WPM-US external wall-mount power adapter (input 90-254 Vac, 50-60 Hz, output: 15 Vdc, 1 A) Materials and Tools Required The following tools and supplies are required for installation: Product Description Model Included in this package you should find the following items: • One base controller • INSTALLATION INSTRUCTIONS, form no. 95-7722. • Hardware package containing one grounding wire with quick-disconnect 0.187 in. (4.75 mm) female connector. • One power module (if ordered), which is required for operation. Description WEB-201 Basic Unit Controller CP-201 CP-201 Basic Unit Controller WEB-600 WEB-600 Basic Unit Controller CP-600 CP-600 Basic Unit Controller • DIN rail, type NS35/7.5 (1.4 IN. X 0.3 in. [35 mm x 7.5 mm]) recommended for any installation that includes DIN rail power supply and/or optional I/O modules. NOTE: Length of DIN rail is determined by the number of optional DIN-mounted options. Refer to Fig. 2 for more details. • If using a DIN rail power supply, one of the following: 95-7722-05 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS — UL listed, Class 2, 24 Vac transformer, rated at a minimum of 8.5 VA to 20 VA (approximate range of controller alone, to fully-expanded unit with 4 additional I/O-16 modules and other option boards). A dedicated transformer is required (cannot power additional equipment). — 24 Vdc power supply, capable of supplying at least 1 A (24 W). • Suitable screws and screwdriver for mounting DIN rail, or if DIN rail not used, for mounting bases of controller, DIN rail power supply (if used), and any I/O modules (if used). • #2 Phillips screwdriver: used to install and remove optional communications modules. • Small flat-blade screwdriver: used for mounting or removing the controller from DIN rail, also for making wiring connections to RS-485 connector, and LON® and I/O connectors (if used). SAFETY INSTRUCTIONS NOTES REGARDING DEVICE DESCRIPTION These instructions include indications for use and mounting of the device. In case of questions that cannot be answered with these instructions, please consult the product supplier or manufacturer. It is the responsibility of the equipment installer to ensure that all federal, state and local codes are followed. SAFETY INSTRUCTIONS • Keep these Installation Instructions for industrial safety and the prevention of accidents. • The information in these instructions must be read and understood by every person using this device. • The following items share warnings of a general nature relating to the installation and start-up of the controller. • Be sure to heed these warnings to prevent personal injury or equipment damage. WARNING • Depending on power module used, the circuit powering the controller is 90–263Vac at 50/60 Hz (if using NPB-PWR-UN-H), 24Vac at 50/60 Hz or 24Vdc (if using NPB-PWR-H), or from 100–240Vac at 50/60 Hz (if using NPB-WPM-US). • Disconnect power before installation or servicing to prevent electrical shock or equipment damage. Make all connections in accordance with national and local electrical codes. Use copper conductors only. • To reduce the risk of fire or electrical shock, install in a controlled environment relatively free of contaminants. • This device is only intended for use as a monitoring and control device. To prevent data loss or equipment damage, do not use for any other purpose. Static Discharge Precautions CAUTION • Work in a static free area. • Discharge any static electricity you may have accumulated. Discharge static electricity by touching a known securely grounded object. • Do not handle the printed circuit board (PCB) without proper protection against static discharge. Use a wrist strap when handling PCBs. The wrist strap clamp is to be secured to earth ground. MOUNTING Mount the controller in a location that allows clearance for wiring, servicing and module removal. Additional mounting information applies as follows: • Environmental Requirements • Physical Mounting Environmental Requirements The following are the environmental requirements for the mounting locations of the controller. • This product is intended for indoor use only. Do not expose the unit to ambient conditions outside of the range of 32° to 122° F (0° to 50° C) and relative humidity outside the range of 5% to 95% noncondensing (pollution degree 1). • If mounting inside an enclosure, that enclosure should be designed to keep the unit within its required operating range considering a 20-watt dissipation by the controller. This is especially important if the controller is mounted inside an enclosure with other heat producing equipment. • Do not mount the unit: — in an area where excessive moisture, corrosive fumes, or explosive vapors are present. — where vibration or shock is likely to occur. — in a location subject to electrical noise. This includes the proximity of large electrical contractors, electrical machinery, welding equipment, and spark igniters. Physical Mounting The following information applies to physically mounting the unit: • The unit may be mounted in any orientation. It is not necessary to remove the cover before mounting. • Mounting on a 1.4 in. (35 mm) wide DIN rail is recommended. The unit base has a molded DIN rail slot and locking clip, as does the 24 Vac power module (DIN rail power supply) and both types of I/O expansion modules. Mounting on a DIN rail ensures accurate alignment of connectors between all modules. • If DIN rail mounting is impractical, use screws in mounting tabs on the controller, then in any end-connected accessory. Tab dimensions are shown in Fig. 1. Static charges produce voltages high enough to damage electronic components. The microprocessors and associated circuitry within a controller are sensitive to static discharge. Follow these precautions when installing, servicing or operating the system: 95-7722—05 2 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS 1/64 (4 MM) 6-23/32 (171 MM) CONTROLLER 3-3/4 (95 MM) 4 (102 MM) 2-1/2 (64 MM) CONTROLLER ADDITIONAL IO ADDITIONAL IO OR DIN POWER SUPPLY IO OR DIN POWER SUPPLY 3-1/4 (83 MM) 3-1/4 (83 MM) 3-31/64 (89 MM) DISTANCE BETWEEN CENTER OF TABS FROM ONE UNIT TO ANOTHER UNIT. 2-1/2 (64 MM) NOTE: ELECTRONIC AND PRINTED VERSIONS OF THIS GUIDE MAY NOT SHOW THE DIMENSIONS TO SCALE. VERIFY ALL MEASUREMENTS DRILLING. DIN MOUNTING IS RECOMMENDED OVER TAB MOUNTING. SEE FIGURE 2 ON PAGE 4. M23696 Fig. 1. Tab Mounting Dimensions. Procedure 1 provides step by step DIN rail mounting instructions for the controller. NOTE: Mount the controller prior to mounting any accessory items (24 V power module, I/O modules). Procedure 1. Din Rail Mount. Step 1 Securely install the DIN rail using at least two screws, near both ends of the rail. Step 2 Position the controller in the rail, tilting to hook DIN rail tabs over one edge of the DIN rail (Fig. 2). Step 3 Use a screwdriver to pry down the plastic locking clip, and push down and in on the controller, to force the locking clip to snap over the edge of the DIN rail. Step 4 To prevent the controller from sliding on the DIN rail, secure with clips provided by the DIN rail vendor, or place a screw in one of the 4 mounting tabs in the base. Step 5 Mount any accessory item onto the DIN rail in the same manner. Step 6 Slide the accessory along the DIN rail to connect its 20-position plug into the controller. Step 7 Repeat this for all accessories, until all are mounted on the DIN rail and firmly connected to each other. Step 8 To keep this assembly from sliding on the DIN rail, secure the last accessory with clips provided by the DIN rail vendor, or place a screw in one of the mounting tabs in the base of the last accessory. 3 95-7722—05 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS MOUNTING ON DIN RAIL M23265 UP TO FOUR (4) MODULES ARE SUPPORTED 7-1/8 (181 MM) REMOVING FROM DIN RAIL IO-16 6-3/8 (162 MM) 2.-3/64 (91 MM) IO-16 (1) IO-16 (2) IO-16 (3) IO-16 (4) POWER 4-7/64 (181 MM) M23266 M23697 10-11/32 (263 MM) 13-37/64 (345 MM) 16-13/16 (427 MM) 20-3/64 (509 MM) 23-17/64 (591 MM) NOTE: IF INSTALLING IO-16 MODULES AND USING THE DIN POWER SUPPLY MODULE, DIN POWER SUPPLY MODULE INSTALLS AT THE END OF THE CHAIN Fig. 2. Controller Accessory Mounting details. Removing and Replacing the Cover Remove the cover to connect the battery (new unit) or to replace the battery, and to install any option boards. The cover snaps onto the base with 4 plastic tabs (two on each end). To remove the cover, press in the 4 tabs on both ends of the unit, and lift the cover off. NOTE: If accessory modules are plugged into the controller, it may be necessary to slide them away from the unit to get to the cover tabs. To replace the cover, orient it so the cutout area for common ports is correct, then push inward to snap in place. EXPANSION OPTIONS The controller provides for field-installable expansions with two kinds of options: • Option cards - Install on connectors inside the base unit. See Option Cards section. • Accessory modules - To “chain” onto the controller’s 20-pin connector. See Accessory Modules section. Option Cards The controller has two option slots for custom option cards, designed for use with the controller. Each slot has a 30-pin connector on the Base Board (Refer to Fig. 3). WARNING Power to the controller must be OFF when installing or removing option cards, or damage will occur! Be very careful to plug an option card into its connector properly (pins aligned). BOARD LAYOUT Figure 3 shows the location of LEDs, option slots, and other features of the controller with cover removed. For a side view of the communications ports and other features (Refer to Fig. 5). 95-7722—05 Option cards typically provide additional communications features, such as the following available models listed in Table 1. 4 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS Table 1. Controller Option Cards. Model Description Notes NPB-LON FTT-10A LON Up to 2 LON option cards may be installed.a • If one LON option, it operates as LON1, regardless of slot. (LONWORKS®) adapter • If two LON options, LON1 is Option slot 1, LON2 is Option slot 2. with a 2-position removable screw-terminal connector plug. NPB-MDM 56kbps Auto-dial/Autoanswer Modem with one RJ-11 connector for phone line. Maximum of one. Does not have its own universal asynchronous receivertransmitter (UART). Must be installed in Option Slot 1, where it operates as COM1. This disables the RS-232 base serial port (DB-9 connector) on the controller during normal operation. NOTE: If an NPB-MDM is installed, and the “mode jumper” (see Fig. 3) is put in “Serial Shell” position, the controller base RS-232 port becomes active immediately following a reboot. This allows an RS-232 connection to the “serial shell” for debugging purposes. To re-enable the modem, you must put the mode jumper back in the “Normal” position, and reboot again. NPB-2XRS485 Dual, optically-isolated, RS-485 adapter with two 3-position removable screw-terminal connector plugs. NPB-RS232 Single port RS-232 One or twoa 232 option cards may be installed, with COM assignments as: adapter, with a DB-9M • If one 232 option in Option slot 1, port is COM3. Port is COM3 if connector. Uses its own installed in Option slot 2 also, unless NPB-485 option is in option slot 1. on-board UART. Supports In this case only, 232 port is COM5. baud rates up to 115200. • If two 232 options, ports are COM3 for Option slot 1, and COM4 for Option slot 2. NOTE: Niagara AX 3.2.11 or higher needed in the controller. a Only One or twoa 485 option cards may be installed, with COM assignments as: If one 485 option in Option slot 1, ports are COM3 and COM4. COM3 and COM4 if installed in Option slot 2 also, unless NPB-232 option is in slot 1. In this case only, 485 ports are COM4 and COM5. • If two 485 options, ports are COM3 and COM4 for Option slot 1, and COM5 and COM6 for Option slot 2. one NPB option card is recommended for use on WEB-201 and CP-201 controllers. OPTION SLOT 2 BATTERY BRACKET (ON TOP OF OPTION CARDS, IF ANY) SERIAL PORT LEDS ON BOTTOM BOARD, REMOVE COVER TO SEE: COM1 STATUS LEDS (VISIBLE WITH COVER ON): COM2 LAN2 LAN1 BEAT STATUS 20 PIN CONNECTOR (I/O AND POWER MODULES) BATTERY CONNECTOR OPTION SLOT CONNECTORS MODE JUMPER (FOR SERIAL SHELL ACCESS) OPTION SLOT 1 SECONDARY ETHERNET PRIMARY (RJ-45) LAN2 RS-232 (DB-9) ETHERNET (TOP BOARD) COM1 (RJ-45) LAN1 (TOP BOARD) EARTH GROUND USB PORT SPADE LUG (TOP BOARD) WEB-600 AND CP-600 ONLY RS-485 (3-POSITION) COM2 (BOTTOM BOARD) BARREL POWER CONNECTOR FOR WALL MOUNTED POWER MODULE (NPB-WPM-US) M27171 Fig. 3. Controller Board Layout details. 5 95-7722—05 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS Mounting Option Cards For complete details, see the INSTALLATION INSTRUCTIONS document that accompany the specific option card. The following procedure provides a basic set of steps for mounting an option card: Procedure 2. Mounting Controller Option Cards. Step 1 Remove power from the controller - see WARNING, Option Cards section. Step 2 Remove the cover. See Removing and Replacing the Cover section. Step 3 Remove the battery and bracket assembly by taking out the 4 screws holding it in place, setting the screws aside for later. Unplug the battery from the connector on the controller. Step 4 Remove the blanking end plate for the slot the option card is being installed into. (Retain the blanking plate in case the option card must be removed at a later date). Step 5 Carefully insert the pins of the option card into the socket of the appropriate option card slot. The mounting holes on the option board should line up with the standoffs on the base board. If they do not, the connector is not properly aligned. Press until the option card is completely seated. Step 6 Place the custom end plate that came with the option card over the connector(s) of the option card. Step 7 Plug the battery connector plug into the battery connector on the controller. Step 8 Set the battery and bracket assembly back over the option card slots, with the mounting holes aligned with the standoffs. Step 9 Place the 4 screws through the battery bracket, end plates, and into the standoffs on the controller base board. Hand tighten these screws. Step 10 Replace the cover. Accessory Modules WARNING The controller has a 20-pin, right angle, Euro-DIN connector that accepts custom-built accessory modules. The connector provides power and signal lines to any connected modules, and is located on the end of the controller opposite to the option cards. • Power to the controller must be OFF when inserting or unplugging accessory modules. Wait for all LED activity to stop (all LEDs to be off). • Also, do not connect live voltages to the inputs or outputs of an I/O module (IO-16 or IO-34) while it is in an “un-powered state” before plugging the module into a controller. Otherwise, damage to the I/O module and/or the controller may result! Each accessory module has a DIN-mount base and provides two 20-pin connectors that allow a “chain” of multiple accessories (see Procedure 1). Table 2 lists the currently available accessory modules. Table 2. Accessory Modules. Model NPB-PWR-H Description DIN-mountable, 24 V isolated power module, used to power controller from a dedicated, external, Class-2, 24 Vac transformer or a 24 Vdc power supply. Notes • Wiring is covered in this document, see Fig. 4. • Only one NPB-PWR-H per controller. • Do not install if using NPB-WPM-US. NPB-PWR-UN-H DIN-mountable, Universal 90-263 Vac input, 15Vdc output, 30W power supply to power controller. • Only one NPB-PWR-UN-H per controller. • Do not install if using NPB-WPM-US or NPB-PWR-H. • Wiring is covered in this document, Refer to “NPB-PWR-UN-H,” page 8. IO-16-H DIN-mountable, 16 points WEB-IO module, used to provide I/O ports as noted. Provides the following I/O points: • 8 - Universal Inputs (UIs). • 4 - Digital Outputs (DOs), SPST-relay type. • 4 - Analog Outputs, 0-10 Vdc type. Up to 4 (maximum) IO-16-H accessory modules are supported. IO-34-H Din-mountable, combined 34 points I/O with 24 V isolated power module, used to provide I/O points as well as power controller from a dedicated, external, Class-2, 24 Vac transformer or a 24 Vdc power supply. Only one IO-34-H per controller provides the following I/O points: • 16 - Universal Inputs (UIs). • 10 - Digital Outputs (DOs), SPST-relay type. • 8 - Analog Outputs, 0-10 Vdc type. Up to 2 additional IO-16-H modules can be used. Do not power the IO-34-H, if using NPB-WPM-US. 95-7722—05 6 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS WIRING Refer to Fig. 3 to locate connectors and other components on the controller. Make connections to the controller in the following order. 1. Install any option boards (LON, RS-485, or modem) in option slots 1 and 2. See Mounting Option Cards section for a general procedure. For complete details, refer to the specific INSTALLATION INSTRUCTIONS guide that shipped with the option board. 2. Connect the supplied earth grounding wires (with spade connectors) from the earth ground lug on the controller and any accessory modules (if used) to a nearby earth grounding point. See GROUNDING section for details. 3. Prepare power wiring (leave the unit powered off). See Power Wiring section for details. 4. Connect communications cables. See Communications Wiring section for ports available on the controller base unit. For ports on any installed option board (LON, RS-485, modem), see the specific Installation Instructions for any additional details. 5. If I/O accessory modules are installed, connect the I/O wiring. Refer to the appropriate Installation Instructions for complete details. 6. Connect the backup battery to the controller battery connector, and apply power to the unit. See POWER UP AND INITIAL CHECKOUT section. • NPB-PWR-H (24 Vac-powered in-line module). • NPB-PWR-UN-H universal 90-263 Vac powered in-line module. NPB-WPM-US (Wall Wort Power Supply) CAUTION Do not plug the barrel connector plug from the NPB-WPM-US into the controller until all other mounting and wiring is completed. See POWER UP AND INITIAL CHECKOUT section. The NPB-WPM-US power modules are self-contained, isolated, switching power supplies designed to plug into a standard building power receptacle of appropriate voltage. To supply power to the controller, plug the barrel connector plug from the NPB-WPM-US into the barrel power connector on the controller base board (See Fig. 3). NPB-PWR-H (DIN Rail Power Supply) Using the NPB-PWR-H module allows the controller to be powered (and if installed, IO-16-H modules) from a dedicated Class 2, 24 Vac transformer, or from a 24 Vdc power supply. If installing IO-16-H modules, the NPB-PWR-H installs as the last (end) module in the chain (Refer to Fig. 2). CAUTION Grounding An earth ground spade lug 0.187 in. (4.75 mm) is provided on the base of the controller for connection to earth ground. For maximum protection from electrostatic discharge or other forms of EMI, connect the supplied earth grounding wire to this lug and a nearby earth ground (See Fig. 4). Keep this wire as short as possible. Connect the earth ground spade lug of each accessory module to ground in the same manner. Power Wiring The controller must be powered by an approved 15 Vdc power source. This can be either an external wall mount AC adapter (NPB-WPM-US), the DIN-mount 24 Vac or 24 Vdc powered module (NPB-PWR-H) or the 90-263 Vac (NPB-PWR-UN-H). The controller does not include an on/ off switch. To apply power: — — — If NPB-WPM-US, plug in the power connector to the controller. If NPB-PWR-H, plug in the 2-position power connector. If NPB-PWR-UN-H, energize the AC circuit (90-263 Vac) wired to that module. Do not plug 24 V power into the NPB-PWR-H (reinsert connector plug) until all other mounting and wiring is completed. See POWER UP AND INITIAL CHECKOUT section. NOTE: If powering from a 24 V transformer, do not power any other equipment with it because conducted noise problems may result. Do not ground either side of the transformer’s 24 V secondary. Power consumption depends on installed accessories and option boards, and may vary from: • Controller with NPB-PWR-H module alone: approximately 8.5 VA (AC) or 8.5 W (DC). • Controller with NPB-PWR-H and 4 IO-16-H modules, plus option boards: up to 20 VA (AC) or 20 W (DC). Located at the bottom of the controller with NPB-PWR-H module is a 2-position power connector and an earth ground spade lug as shown in Fig. 4. NPB-PWR-H (COVER SHOWN REMOVED) EARTH GROUND CAUTION 24 VDC POWER SUPPLY (POLARITY NOT CRITICAL) NEITHER SIDE TIED TO EARTH DEDICATED 24 VAC TRANSFORMER NEITHER SIDE OF SECONDARY TIED TO EARTH GROUND Do not connect both the NPB-WPM-US and NPB-PWR-H/NPB-PWR-UN-H supplies at the same time, or equipment damage may result. LINE VOLTAGE (MAINS) If desired, use the wall mount power supply in your office (to initially commission the controller), and then install the controller at the job using a DIN rail power supply. The following sections provide more details: • NPB-WPM-US (Wall Power Modules). 24 VDC OR – 24 VDC + M23698A Fig. 4. NPB-PWR-H Module Wiring Connections. 7 95-7722—05 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS Connect the supplied earth ground wire to a nearby earth ground point. Unplug the power connector plug from the module and make connections to it as shown in Fig. 4. NPB-PWR-UN-H The NPB-PWR-UN-H module lets you power the controller (and if installed, IO-16-H modules) from AC line power, with a universal input range from 90-263 Vac. If installing IO-16-H modules, the NPB-PWR-UN-H installs as the last (end) module in the chain (Refer to Fig. 2). WARNING • A 120Vac or 240Vac circuit powers the NPB-PWR-UN-H. Disconnect power to this circuit before installation to prevent electrical shock of equipment damage. • Make all connections in accordance with national and local electrical codes. Use copper conductors only. • Do not exceed the 30W capacity of NPB-PWR-UN-H by the powered devices. Power input connections are made to the terminals on the circuit board (cover removal is required). An earth ground connection must be made to the grounding lug using the supplied earth wire (See Fig. 5). REMOVE COVER SIX-PIN CONNECTOR NOT USED CONTROLLER OR LAST IO-16 Communications Wiring Connect communication wiring to the controller using ports on the bottom of the unit (Fig. 6), which include: • Ethernet • Serial NOTE: Prior to connecting cables, provide strain relief for them to prevent damage to the controller. Ethernet Two female 10/100-Mbit Ethernet connections are provided on the controller. These are RJ-45 connectors labeled LAN2 and LAN1. Use a standard Ethernet patch cable for connecting to a hub or Ethernet switch. An activity LED for each Ethernet port is visible, and are labeled “LAN2” and “LAN1” on the cover. The factory-default IP address for LAN1 on a controller is 192.168.1.12n, where the last numeral n in the address matches the controller's serial number, and subnet mask is 255.255.255.0. By default, LAN2 on a controller is disabled. Refer to the Niagara AX Install and Startup Guide for details on changing IP address. NOTE: Typically, only LAN1 (primary port) is used, unless there is a specific application for isolating a driver’s network traffic to a separate LAN, using LAN2. Do not use LAN2 as the primary port. The packing slip accompanying the controller will provide the “factory-shipped” IP settings for both LAN1 and LAN2. Refer to the INSTALLATION INSTRUCTIONS guide for details on changing IP address. AC INPUT L N 120 OR 240 VAC 50-60 HZ SINGLE PHASE LINE EARTH GROUND NEUTRAL NOTES: THE SIX-PIN CONNECTOR OF THE NPB-PWR-UN-H IS NOT USED WITH A WEB-201 OR WEB-600 SERIES CONTROLLER. THE SIX PIN CONNECTOR IS DESIGNED FOR USE WITH THE WEBS-AX SECURITY CONTROLLER (SEC-H-201) AND ASSOCIATED SECURITY MODULES, AND ONLY WITH THE VARIATION OF THIS POWER SUPPLY THAT ARE INTEGRAL IN A WEB-AX SECURITY ENCLOSURE. M27033 Fig. 5. 95-7722—05 8 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS BATTERY IN BRACKET (ON TOP OF OPTION CARDS, IF ANY) PRIMARY ETHERNET (RJ-45) LAN 1 ETHERNET (RJ-45) LAN 2 USB PORT (FUTURE USE) WEB-600 AND CP-600 ONLY 20 PIN CONNECTOR (I/O AND POWER MODULES) BATTERY CONNECTOR EARTH GROUND SPADE LUG OPTION SLOT AREA (SLOT #1 THIS SIDE) RS-232 (DB-9) COM1 RS-485 (3-POS.) COM2 BARREL POWER CONNECTOR FOR NPB-WPM-US M27172 Fig. 6. Controller Bottom Side (cover removed). Serial There are two serial ports on the base unit. Each has a UART capable of operating up to 115, 200 baud. At the bottom of the board (refer to Fig. 5), the left port is an RS232 port using a DB-9 plug (male) connector. To the right of this is a two-wire with shield, isolated RS-485 port, using a screw-terminal connector plug. NOTE: A green “receive” LED and yellow “transmit” LED are provided for each serial port. These LEDs are located on the bottom board, on the opposite side of the serial connectors (refer to Fig. 3). These LEDs are labeled on the board (COM1, COM2) and are not visible with the cover on. RS-232 An RS-232 serial port using a male DB-9 connector always operates as COM1. Standard DB-9 serial cable may be used with this port. The controller is a serial data terminal equipment (DTE) device; another DTE device (PC, for example) requires a “null modem” cable. If connecting the controller to a data communications equipment (DCE) device (modem, for example), a straight-through cable is used. Table 3 provides standard serial DB-9 pinouts. NOTE: If a modem option card (NPB-MDM) is installed, this port becomes disabled - except if rebooted with the mode jumper (refer to Fig. 3) in the “Serial Shell” position. RS-485 An RS-485, optically isolated port, uses a 3-position, screw terminal connector and always operates as COM2. Wire to this connector with shielded 18 - 22 AWG (0.8 mm2 - 0.3 mm2) wiring (refer to the TIA/EIA-485 standard). As shown in Table 3, the screw terminals (from left-to-right) are shield, plus (+), and minus (-). USB (WEB-600 and CP-600 only) A single USB port is on the top board. NOTE: The USB port is for future use. Table 3. Serial Port (RS-485) Pinouts. Base RS-232 DB-9 Port (COM1) Pinouts References DB-9 Plug (male) Base RS-485 Port (COM2) Signal DB-9 Plug Pin DCD Data carried defect 1 RXD Receive data 2 TXD Transmit data 3 DTR Data terminal ready 4 GND Ground 5 DSR Data set ready 6 RTS Request to send 7 CTS Clear to send 8 not used Pinouts 3-position connector (male) 9 POWER UP AND INITIAL CHECKOUT Ensure power wiring to the controller is ready - see the Power Wiring section. Refer to Fig. 3 for the location of the controller battery connector, status LEDs, and barrel power connector (for NPB-WPM-US only). Refer to Fig. 4 for location of the power connector on the NPB-PWR-H module. 9 95-7722—05 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS After all mounting and wiring procedures are completed, perform the following procedure: Procedure 3. Initial power and checkout If after applying power, the STATUS LED goes out, or if the BEAT LED comes on (steady) and stays lit longer then two minutes, refer to the Using Status LEDs section. Step 1 Connect the Backup Battery. Battery Step 2 Apply Power. Step 3 Check the Status LEDs. The controller is provided with a custom 10-cell NiMH battery pack mounted to the unit (under the cover). This battery allows the controller to continue operation through very short power bumps (a few seconds in duration). If a longer power outage occurs, the battery provides enough run time to backup data and then shutdown. Typically, this is one minute. Shutdown occurs automatically after data is backed up to on-board flash memory. Connect the Backup Battery With the cover removed from the controller, (See REMOVING AND REPLACING THE COVER section), locate the red and black wires coming from the backup battery with the 2-position connector plug. Insert the plug into the battery connector on the bottom board (below option slot 2 area), as shown in Fig. 7. BATTERY ASSEMBLY The controller charges the battery during normal operation until fully charged. Typically, the charge operation completes within 18 hours. Following a power outage, the battery is charged again as necessary. The power and battery circuitry is monitored by a station running on the controller (via the Power Monitor Service). Station alarms are generated whenever primary power is lost or if the battery is uncharged or unable to hold sufficient charge. The battery should be replaced approximately every three years or more often if the unit is in a high temperature environment. BATTERY CONNECTOR M29292 Fig. 7. Backup battery connector on bottom board. The connector is keyed - it cannot be inserted incorrectly. The red (positive) connections should be the furthest from the two 30-pin option board connectors. For more battery details, see the Battery section. Apply Power CAUTION Do not connect both the NPB-WPM-US and NPB-PWR-H supplies at the same time, or equipment damage may result, or a power outage may go unrecognized. Apply power to the controller by plugging in the power plug into either the controller (if wall mount AC adapter NPB-WPM-US) or the 24 V-powered NPB-PWR-H module. If powering using the line-voltage input NPBPWR-UN-H power supply module, energize the 90–263 Vac circuit wired to the NPB-PWR-UN-H module. Check the Status LEDs When power is applied, the green LED labeled “STATUS” will light. This indicates that the system is OK and that power is applied. Once the controller boots, the yellow “BEAT” (heartbeat) LED will begin blinking, with a typical rate of approximately 1 Hz. Blinking should begin within 30 seconds after power is applied. 95-7722—05 NOTE: A NiMH battery characteristic is to lose charge if not left in charge mode (trickle charge). Leaving the battery unconnected, or the unit powered off will cause the battery to fully discharge in a matter of weeks. In the case of a new controller the battery is shipped completely discharged. Therefore, allow at least 18 hours for the battery to charge if it has not been in a powered unit. For more information on the use and replacement of the battery, refer to the Required Battery Maintenance section. USING STATUS LEDS The controller includes several LEDs that can help determine the status of the unit. They are located in two places: the top of the controller (visible through the cover), and on the bottom board (visible only with cover removed). From left-to-right, these LEDs include: • Ethernet Ports • Heartbeat • Status • Serial Ports Refer to Fig. 3 for the exact locations of status LEDs on the controller. Ethernet Ports Each Ethernet port (“LAN2”, “LAN1”) has one green LED, visible on the top cover. A “LANx” LED indicates activity on that port as follows: • Off - No Ethernet link is made. • On - Ethernet link is present, but no activity on the LAN. • Blinking - Ethernet link is present with data activity on the LAN. 10 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS Heartbeat The “BEAT” LED is located to the right of the Ethernet status LEDs, and is yellow. Under normal operation, this LED should blink about once per second. If the heartbeat LED stays on constantly, does not light, or blinks very fast (more than once per second), contact your Honeywell representative for technical support. During boot-up, the heartbeat LED blinks in a 90% on — 10% off pattern. Do not remove power during this time, or data loss may result (I/O module’s firmware upgrade may be in progress). • New Replacement Units • Replacing the Controller Base Assembly • Returning a Defective Unit Cleaning If dust or metal filings are present inside the unit, clean with vacuum or compressed air. Otherwise, no cleaning inside the unit is required. Optionally, if the cover becomes dirty, wipe it with a damp cloth and mild detergent. Required Battery Maintenance Status The “STATUS” LED is located to the right of the heartbeat (“BEAT”) LED, and is green. This LED provides a CPU machine status check and should remain lit whenever the controller is powered. If the STATUS LED does not light while power is applied, contact your Honeywell representative for technical support. Serial Ports LEDs for the two serial ports are located on the controller’s bottom board (visible only with cover removed), on the opposite side of the RS-232 and RS485 ports (see Fig. 3). Labels “COM1” and “COM2” correspond to the software configuration of the COM ports. LEDs show the transmit and receive activity for the serial ports and optional modem. NOTE: The cover must be removed to view the serial port LEDs. See Removing and Replacing the Cover section. • The yellow transmit LED indicates that the controller is sending data out the serial port over a communications line to a connected device. • The green receive LED indicates that the controller is receiving data from a connected device. These LEDs provide a fixed on-time when data is detected on the port. If these LEDs are on constantly, this indicates a problem with the communications channel such as a shorted wire or reversed wiring. Battery life expectancy is a function of discharge cycles (the number of discharges and their depth) and the ambient temperature of the battery during normal operation. In most applications, the battery should see relatively few discharges. Therefore, ambient temperature has more to do with determining the life expectancy of the battery then does any other factor. If the controller is installed in a conditioned space, the battery should provide dependable service for approximately three years (average). In an environment where the operating temperature is 122° F (50° C) or higher, the life expectancy of the battery is approximately one year. The NiMH battery in the controller is fully discharged when factory shipped. Additionally, NiMH batteries lose charge over time if not kept trickle-charged (for more details, see the Battery section). Therefore even a new unit (or replacement battery) will require up to 18 hours of powered operation before it is fully charged and can provide reliable backup power. The controller monitors the battery and periodically loads the battery to test its ability to maintain battery-backed functions. Investigate any battery trouble message and check the battery connections to the unit. Replace the battery as required. To order a new battery, see the Standard Replacement Parts section. Replacing the Battery CAUTION MAINTENANCE Use only battery packs approved for use with the controller. This section provides information on the following topics: • Cleaning • Required Battery Maintenance • Replacement Parts • Non Replacement Parts • Standard Replacement Parts A replacement battery is a complete assembly comprised of a battery pack pre-attached to a battery bracket (Refer to Fig. 6). To replace the battery proceed as follows: Procedure 4. Replacing the Battery. Step 1 Backup controller’s configuration to your PC using the appropriate Niagara-AX software tool (for example, WEBStation-AX). Step 2 Remove power from the controller. Step 3 Remove the cover. See Removing and Replacing Cover section. Step 4 Remove the old battery and bracket assembly by taking out the 4 screws holding it in place, setting the screws aside for later. Unplug the battery from the connector on the controller. Step 5 Plug the battery connector plug of the replacement battery into the battery connector on the controller. Step 6 Set the replacement battery/bracket assembly back over the option card slots, with the mounting holes aligned with the standoffs. Step 7 Place the 4 screws through the battery bracket, option cards blanking plates, and into the standoffs on the controller base board. Hand tighten these screws. Step 8 Replace the cover. Step 9 Restore power and verify normal operation. 11 95-7722—05 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS Replacement Parts Servicing the controllers may call for replacement parts. There are three categories of parts: • Non-replacement Parts • Standard Replacement Parts • New Replacement Units Non-replacement Parts Other than the parts listed in the replacement parts sections, there are no serviceable components on the base assembly. Memory Any addition, modification, or replacement of memory components requires software configuration and is not a field upgrade. Fuse The controller contains a non-user replaceable fuse, soldered on the circuit board. This fuse provides protection from internal shorts or connection to incorrect power supplies. If the fuse circuitry is suspect, contact the regional Honeywell office for technical support. See the RETURNING A DEFECTIVE UNIT section. NOTE: Screws used for the controller are standard no. 6-32 x 3/8 in (9.5 mm) types, which may be obtained locally if lost. New Replacement Units To replace a faulty unit, order and install a new controller. NOTE: These products do not have special “field replacement units”, or FRU’s, with separate part numbers. If the faulty unit is still in warranty, credit may be received by returning it to Tridium. Be sure to contact Tridium for a return authorization (RA) number before shipping an item for return credit. See RETURNING A DEFECTIVE UNIT section for details. NOTE: Before ordering a new controller, it is strongly recommended that your normal technical support resource is contacted to eliminate the possibility of a software issue or misconfiguration problem. Replacing the Base Assembly Standard Replacement Parts CAUTION Standard replacement parts are listed in Table 4 and can be ordered directly from Tridium without restriction. Standard replacement parts cannot be returned for credit and should be disposed of in an appropriate manner. Before handling circuit boards, discharge any accumulated static by touching the metal surface of the Base Assembly. For details, see the Static Discharge Precautions section. Table 4. Standard Replacement Parts. Part Number Description 10499 NiMH Battery Pack (with battery bracket) see Replacing the Battery section. 10027 RS-485 connector plug, 3-position. 95-7722—05 12 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS To replace the Base Assembly in the field, proceed as follows: Procedure 5. Replacing a Base Assembly. Step 1 Using the appropriate Niagara software tool, backup the station database to PC. Step 2 Remove power to the controller. The unit should power down automatically. Step 3 Record positions of all communications and other wiring cables going to the controller, as well as all installed accessory modules. If necessary, label connectors and accessory modules to avoid mis-connection later (after controller is replaced). NOTES: — — The software that runs on the unit expects the terminal positions to be the same to collect data from or to control the attached devices. If using I/O modules, and any I/O points have voltage, turn the devices off or disconnect power to them. Step 4 Unplug all Ethernet, serial, LON, modem, and I/O connectors from the controller and any installed accessory modules if applicable. Step 5 Unplug the earth ground wires to the controller grounding lug and any installed accessory modules. Step 6 If the controller has installed accessory modules, remove them, starting with the end module. Modules may be secured by screws in mounting tabs or clipped to DIN rail, or a combination of both methods. For details on DIN rail mounting (including removal), see Fig. 2. NOTE: If DIN rail mounting was used, often it is possible to remove any screws or clips that secure each module (possibly just the last module) and then slide each module (individually) away from the unit until the controller can be removed from the DIN rail. Step 7 Remove any screws or DIN rail clips securing the controller, removing it from its mounting. Step 8 Remove the cover from the old controller (see Removing and Replacing the Cover section). Record the position of installed option boards, if any. Transfigure the boards to the replacement controller. Step 9 Remove the option boards from the old controller and install them into the replacement controller, if applicable. See Mounting Option Cards section for more details. Step 10 Mount the replacement controller as it was previously, using the same DIN rail location and/or screws. Step 11 Reconnect/remount any removed accessory modules, being careful to replace in the same order, using the same DIN rail location and/or screws. Secure all accessory modules as done previously. Step 12 Reconnect the earth ground wires to the controller grounding lug and any installed accessory modules. Step 13 Reconnect any Ethernet, serial, modem and I/O connectors to the controller and any installed accessory modules. Step 14 If using I/O modules, with voltage to any of the I/O points, turn the devices back on or reconnect power to them. Step 15 Restore power to the controller. It should boot up as a new unit (see Check the Status LEDs section. Step 16 Using the Niagara AX platform tools, re-commission the controller and install the saved station database. For more details, see the JACE Niagara AX Install and Startup Guide. 13 95-7722—05 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS RETURNING A DEFECTIVE UNIT NOTES: If the defective unit is under warranty, follow return instructions provided in this section. If the unit is out of warranty, discard the unit. — Do not return an out-of-warranty controller to Tridium. — There is no “return for repair-and-return” service available for any of these products. For proper credit on an in-warranty unit, ship the defective unit to Tridium within 30 days. Prior to returning the unit, contact one of the following Tridium offices to obtain a return authorization (RA) number and other instructions. Please provide: • Product model • Serial Number • Nature of the defect United States Phone: 804-254-7086, ext. 11 Return to: Tridium, Inc. 2256 Dabney Road, Suite C Richmond, VA 23230 Attn: Return Department RA# ____________ Asia / Pacific Phone: +65 6887 5154 Fax: +65 6887 5342 Mobile: +65 9665 6024 Return to: Tridium Asia Pacific Pte Ltd Email for technical support: 101 Cecil Street, [email protected] #10-11, Tong Eng Building, Singapore 069533 Attn: Mr Lim Hoon Chiat, Engineering Manager RA# ____________ Sales: (Australia): Phone: +617 5539 1211 Fax: +617 5597 2334 (Japan): Phone: +81 044 829 1750 95-7722—05 14 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS RELATED DOCUMENTATION For more information on configuring and using WEB-201, 600, CP-201, 600 Series Controllers, consult the following literature: • IO-16-H Installation Instructions, literature no. 95-7723. • IO-34-H Installation Instructions, literature no. 95-7724. • Niagara AX Ndio Guide. • Niagara AX User Guide. • JACE Niagara AX Install and Startup Guide. CERTIFICATIONS Federal Communications Commission (FCC) This equipment generates, uses, and can radiate radio frequency energy, and if not installed and used in accordance with the instruction manual, may cause interference with radio communications. It has been tested and found to comply with the limits for a Class A computing device pursuant to Subpart J of Part 15 of FCC Rules, which are designed to provide reasonable protection against such interference when operated in a commercial environment. Operation of this equipment in a residential area may cause interference, in which case, users, at their own expense, will be required to take whatever measures may be required to correct the interference. Any unauthorized modification of this equipment may result in the revocation of the owner’s authority to continue its operation. Canadian Department of Communications (DOC) This Class A digital apparatus meets all requirements of the Canadian Interference-Causing Equipment Regulations. LON®, LONWORKS® and Echelon® are registered trademarks of Echelon Corporation. JACE® and Niagara Framework® are registered trademarks, and Niagara AX™ is a trademark of Honeywell International Inc. 15 95-7722—05 WEB-201, WEB-600, CP-201 AND CP-600 SERIES CONTROLLERS Automation and Control Solutions Honeywell International Inc. Honeywell Limited-Honeywell Limitée 1985 Douglas Drive North 35 Dynamic Drive Golden Valley, MN 55422 Toronto, Ontario M1V 4Z9 customer.honeywell.com ® U.S. Registered Trademark © 2008 Honeywell International Inc. 95-7722—05 J.I. Rev. 02-08 Appendix D - Project Schedule ID Task Name 1 Notice to Proceed 2 Kick Off Meeting/Site Visit 3 60% Submittal Duration Start 0 days Fri 6/1/12 Finish Predecessors Fri 6/1/12 1 day Wed 6/20/12 37 days Thu 6/21/12 Fri 8/10/12 Fri 7/20/12 2 CCD Wed 6/20/12 1FS+13 days 4 Engineering Analysis 22 days Thu 6/21/12 5 Drawing Production 12 days Thu 7/5/12 6 Specification Preparation 5 days Mon 7/23/12 Fri 7/27/12 4 7 Estimate Preparation 2 days Mon 7/23/12 Tue 7/24/12 4 8 Design Analysis Report 3 days Wed 7/25/12 Fri 7/27/12 7 9 60% Submittal to DIA 0 days Fri 7/27/12 DIA Review 10 days Mon 7/30/12 Fri 8/10/12 9 Fri 7/27/12 5,6,7,8 11 90% Submittal 170 days Mon 8/13/12 Fri 4/5/13 20 days Mon 8/13/12 Engineering Analysis 13 Drawing Production 7 days Mon 8/20/12 Tue 8/28/12 12SS+5 days 14 Specification Preparation 2 days Mon 9/10/12 Tue 9/11/12 12 15 Estimate Preparation 2 days Mon 9/10/12 Tue 9/11/12 12 16 Design Analysis Report 1 day Wed 9/12/12 Wed 9/12/12 15 17 90% Submittal to DIA Wed 9/12/12 13,14,15,16 18 DIA Review Fri 9/7/12 10 0 days Wed 9/12/12 147 days Thu 9/13/12 Fri 4/5/13 17 29 days Mon 4/8/13 Thu 5/16/13 18 5 days Mon 4/8/13 10 days Mon 4/15/13 Fri 4/26/13 20 2 days Mon 4/29/13 Tue 4/30/13 21 20 Unit Location Confirmation 21 Drawing Production 22 Specification Preparation 23 Estimate Preparation 1 day Wed 5/1/13 Wed 5/1/13 22 24 Design Analysis 1 day Thu 5/2/13 Thu 5/2/13 23 25 100% Submittal to DIA 0 days Thu 5/2/13 Thu 5/2/13 24 26 DIA Review 10 days Fri 5/3/13 Thu 5/16/13 24 136 days Fri 5/17/13 Fri 11/22/13 Issue for Construction Submittal 28 Engineering Analysis 3 days Fri 5/17/13 Tue 5/21/13 26 29 Drawing Production 133 days Wed 5/22/13 Fri 11/22/13 28 30 Specification Preparation 133 days Wed 5/22/13 Fri 11/22/13 32 IFC Submittal to DIA 100% Resubmittal 33 Engineering Analysis 34 Drawing Production 35 0 days Fri 11/22/13 Fri 11/22/13 30 17 days Thu 7/10/14 Fri 8/1/14 Thu 7/17/14 6 days Thu 7/10/14 12 days Thu 7/17/14 Fri 8/1/14 Specification Preparation 8 days Thu 7/17/14 Mon 7/28/14 36 Estimate Preparation 5 days Mon 7/21/14 Fri 7/25/14 37 Design Analysis 5 days Mon 7/28/14 Fri 8/1/14 38 100% Resubmittal to DIA 0 days Fri 8/1/14 Fri 8/1/14 39 DIA Review 5 days Mon 8/4/14 40 IFC Resubmittal 11 days Mon 8/11/14 Mon 8/25/14 Wed 8/13/14 Comment Review & Response 3 days Mon 8/11/14 42 Drawing Production 8 days Thu 8/14/14 Mon 8/25/14 41 43 Specification Preparation 5 days Thu 8/14/14 Wed 8/20/14 44 Estimate Preparation 2 days Wed 8/20/14 Thu 8/21/14 45 Design Analysis 2 days Fri 8/22/14 Mon 8/25/14 0 days Mon 8/25/14 Mon 8/25/14 47 IFC Resubmittal to DIA Construction Phase 48 Building Department Permit Set 49 Contractor Bid Award 50 Construction Project: Concourse B PCA Replaceme Date: Wed 7/16/14 817 days 5/2 11/22 8/1 Fri 8/8/14 38 41 46 9/12 Fri 4/12/13 27 31 BMcD 7/27 12 100% Submittal BMcD '12May 13, Jun 17, 'Jul 22, '1Aug 26, 'Sep 30, 'Nov 4, '1Dec 9, '1Jan 13, 'Feb 17, 'Mar 24, 'Apr 28, '1Jun 2, '13 Jul 7, '13Aug 11, 'Sep 15, 'Oct 20, 'Nov 24, 'Dec 29, 'Feb 2, '1Mar 9, '1Apr 13, '1May 18, Jun 22, 'Jul 27, '1Aug 31, 'Oct 5, '14Nov 9, '1Dec 14, 'Jan 18, 'Feb 22, 'Mar 29, 'May 3, '1Jun 7, '15 Jul 12, '1Aug 16, 'Sep 20, 'Oct 25, '1Nov 29, 'Jan 3, '16 Feb 7, '1Mar 13, 'Apr 17, ' May 22, Jun 26, 'Jul 31, '1Sep 4, '1Oct 9, '16Nov 13, 'Dec 18, 'Jan 22, 'Feb 26, 'Apr 2, '17May 7, '1Jun 11, 'Jul 16, '1Aug 20, 'Sep 24, 'Oct 3 18 2 17 2 17 1 16 31 15 30 15 30 14 29 14 29 13 28 12 27 14 29 13 28 13 28 12 27 12 27 11 26 10 25 10 25 9 24 9 24 8 23 7 22 9 24 8 23 8 23 7 22 7 22 6 21 5 20 5 20 4 19 4 19 3 18 2 17 4 19 3 18 3 18 2 17 2 17 1 16 31 15 30 15 30 14 29 14 29 13 28 12 27 13 28 12 27 12 27 11 26 11 26 10 25 9 24 9 24 8 23 8 23 7 22 6 21 8 23 7 22 7 22 6 21 6 21 5 20 4 19 4 19 3 6/1 Fri 7/20/12 4SS+10 days 10 19 Resource Names 8/25 Tue 8/26/14 Wed 10/11/17 30 days Tue 8/26/14 Mon 10/6/14 46 90 days Thu 10/2/14 Wed 2/4/15 700 days Thu 2/5/15 Wed 10/11/17 49 Task Milestone Project Summary External Milestone Inactive Milestone Manual Task Manual Summary Rollup Start-only Progress Split Summary External Tasks Inactive Task Inactive Summary Duration-only Manual Summary Finish-only Deadline Page 1