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.
For further information please visit www.cavotec.com
Disclaimer: specifications are subject to change without notice
www.cavotec.com
06!"ÿ0#$%&'6%&$%&ÿ()*%+,
012345543061ÿ012389
30612
Mÿ4B1434ÿ=ÿ5ÿ>?;@A;ÿ43ÿ4DÿIÿ32ÿ<ÿ
SK;TUVÿÿSK;WUUÿ56Cÿ:79ÿTÿ1615ÿ
>?;VW;ÿ432ÿ5ÿ2ÿIÿ329ÿ6ÿ<71ÿÿ66ÿ=ÿ
@TÿO>29ÿV]ÿDÿ36<3629ÿ5ÿVWÿ58ÿ36<36ÿ<1562C
`.a68.ÿ012345543061
-.
1
.
8
4
5
/012ÿ3456ÿ72ÿ60ÿ43561589ÿ:11589ÿ5ÿ15161ÿ
266;3<ÿ=ÿ>?;@A;ÿB<5215ÿ43Cÿ>6ÿ22342ÿ606ÿ
D3ÿÿ5ÿ58159ÿ6051159ÿÿ271ÿ<25ÿ:0ÿ12ÿ
<=4158ÿH56ÿ2D264ÿ1526615ÿ32158ÿ60ÿE18ÿ
F4:G Cÿ2ÿÿ6012ÿ561ÿ3456ÿI=ÿ
I8155158ÿ60ÿ1526615ÿ<32C
/012ÿ3456ÿ2ÿ56ÿ12322ÿ2=6:ÿ1526615ÿÿ
26615ÿ5=183615CÿFÿ4ÿ15=4615ÿ5ÿ602ÿ
6<129ÿ=ÿ6ÿ60ÿ34562ÿ126ÿ15ÿ60ÿJKLM/KNÿ
N?OPKE/M/>?Eÿ2615C
bc O5<Gÿ60ÿ>?;@A;ÿ4<6ÿN16ÿKB<5215ÿ
P3C
dc >52<6ÿ56562ÿ=ÿ60ÿ<G8ÿ=ÿ48ÿÿ
4122158ÿ4<5562C
ec 0Gÿ60ÿf31<456ÿ5ÿ<6ÿ5Dÿ48ÿ6ÿÿ
5D:ÿ<256617ÿ6ÿ5ÿ5ÿ635ÿ5Dÿ
48ÿ4<5562ÿ=ÿ14416ÿ<1ÿÿ
<456Cÿ[ÿJK/OJE>EgÿMÿNKFK/>^Kÿ
OE>/ÿ2615C
hc Jÿÿ=ÿ602ÿ152636152ÿ5ÿ523ÿ60Dÿÿ
3526C
0>5#i3+%*,ÿ15*ÿ6ÿ0j1#2ÿÿ<&kjGlÿ8QmÿDin3ÿm20o,3ÿ=15ÿ60ÿ=:158ÿ
1642p
q ?5ÿ>?;@A;ÿ439ÿ:160ÿ835158ÿ:1ÿ07158ÿÿ
f31G;12556ÿUCV]rÿ15CÿZACrsÿ44\ÿ=4ÿ
556C
q >?;@A;ÿ>E[/MLLM/>?Eÿ>E[/JO/>?E[9ÿ1663ÿ
5Cÿts;rrTAC
q ?5ÿVs;<21615ÿ6415ÿ<38ÿ5ÿ60ÿVT;<21615ÿ
6415ÿ<3829ÿ=ÿ>_?ÿ:1158C
q ?5ÿT;<21615ÿ6415ÿ<389ÿ=ÿTAÿ^ÿ<:C
/0ÿ5D:ÿ>?;@A;ÿ12ÿÿ4<6ÿ16ÿ>?ÿ43ÿ=ÿ q [1B65ÿAtt;04ÿ21262ÿ=ÿA;TUÿ4Mÿ15<362C
3B11Dÿ4516158ÿ5ÿ56ÿ:05ÿ32ÿ:160ÿÿSK; (m&
,ujm+lÿm#*ÿ3))+lÿ8,v%ju,*
TUVÿÿSK;WUUÿ212ÿ56ÿÿ60ÿ56ÿ
ÿ=:158ÿ62ÿ5ÿ23<<12ÿÿf31ÿ=ÿ
<6=42ÿ2ÿ1561=1ÿ15ÿ601ÿ2<617ÿ6ÿ2062Cÿ /0
1526615p
/012ÿ<615ÿB<52ÿ60ÿ56ÿ5ÿ1615ÿ@Aÿ
2316Iÿ<:ÿ239ÿ2ÿ5ÿ=ÿ60ÿ=:158p
81;56ÿ<1562Cÿ>53ÿÿVWÿ35172ÿ15<3629ÿ q Mÿ
w OLÿ1269ÿ22ÿT9ÿTAÿ^ÿ652=49ÿ6ÿÿ
VUÿ=4ÿXMYÿZ[[/\ÿDÿ36<362ÿ5ÿ]ÿ58ÿZ768ÿ
4151434ÿ=ÿ]Csÿ^Mÿ6ÿTUÿ^MÿZ<<B146ÿ58ÿ
5D\ÿ36<362Cÿ/012ÿ86DÿB<52ÿ60ÿ56ÿ
=ÿSK;TUVÿÿSK;WUUÿ:160ÿ>?;@A;ÿ59ÿ6ÿ
4516158ÿ5ÿ56ÿ<I11612ÿ:160ÿ=269ÿ1I9ÿ
=3D;B<5ÿ3516ÿ:160ÿTÿ1615ÿ>?;VW;ÿ
16ÿ15<362ÿ5ÿ36<362ÿ=ÿ4516158ÿ<:9ÿ
432ÿ5ÿ60ÿ<615ÿI2\CÿMÿxyxz{|}yxÿ
64<639ÿ034116Dÿ5ÿ26632Cÿ>5ÿ16159ÿ60ÿ
652=4ÿ12ÿf31ÿZ556ÿ<:ÿ1615ÿ
>?;@A;ÿ<712ÿ<:ÿ6ÿ60ÿ660ÿ56ÿ32158ÿ
1<456\C
160ÿ5ÿB65D;23<<1ÿTAÿ^ÿ652=4ÿÿTAÿ^ÿ w TAfÿ3^
ÿ<:ÿ23<<D9ÿ<Iÿ=ÿ23<<D158ÿ6ÿ
<:ÿ23<<DC
26ÿVÿMÿZTAÿS\C
Eÿ19ÿ6D<ÿE[@s_rCsÿZ@sÿ44ÿBÿrCsÿ44\ÿ
/0ÿ5;Iÿ>_?ÿ5ÿIÿ32ÿ6ÿ4516ÿ<32ÿ5662ÿ q N>
445ÿ=ÿ4356158ÿ:160ÿSK;TUVÿ56Cÿ
=4ÿ<:_45ÿ4629ÿ58ÿ25229ÿÿ
/0ÿN>Eÿ1ÿ203ÿIÿ23==1156ÿ5860ÿ6ÿ
652329ÿ2ÿ:ÿ2ÿ6ÿ56ÿ58D;5234158ÿ
446ÿI60ÿ60ÿ56ÿ5ÿ>?;@A;ÿ
712ÿ230ÿ2ÿ=529ÿ18062ÿÿ<34<2ÿ:160ÿ1816ÿDÿ
43Cÿ[ÿF18CÿTC
36<362CÿM2ÿ153ÿÿ]ÿ58ÿ36<362ÿ6ÿ
<<615Dÿ56ÿ4<29ÿ772ÿ5ÿ60ÿ712C
Q86R9
3ÿR.2
80Q3061
ÿÿÿ
0123425ÿ0789
19
89
ÿ19
!ÿ#$%!&#ÿ'(ÿ#$%!&(%)!%ÿ*+%ÿ,+''-ÿ./0ÿ%1ÿ
+%ÿ*ÿ./0ÿ%ÿ'+ÿ#!(1ÿ*+%ÿ,+''-ÿ#!#ÿ+*ÿ2!ÿ
$+'%+!%ÿ'(ÿ/345ÿ,+(!6
,ÿ*(!ÿ#$%!&(%)!%7ÿ#!(ÿ*+%ÿ,+''-ÿ+%ÿ
%!,+)'-ÿ2!ÿ/345ÿ,+(!ÿ*%+,ÿ./0ÿ%1ÿ#+ÿ*+%ÿ
#$%!&ÿ!%,'#ÿ+'ÿ/83ÿ$+''!$+%#ÿ'(ÿ4ÿ9ÿ:+&!%ÿ
$+''!$+%6
;<=>?@ÿBC;?DEF?BGC;
[ ubÿsbgÿl`sdrjÿgljÿhcesgjdÿaecafegÿvb`cdÿ
•–‚—ÿieglbfgÿhcbhjcÿhcbgjagebsÿ̀y`eskgÿ
kg`geaÿdekal`cyjtÿ}kjÿ̀ÿicekgÿkgc`hÿiljsÿ
l`sdresyÿ–‚k€ÿieglÿgljÿicekgÿkgc`hÿar̀qhÿ
kjafcjdÿgbÿj`cglÿycbfsdt
B˜Gÿ™Žš›ŒÿFŽŒ‡„†ŽÿKŠŒ‡…„†Žˆ
V}Y
mX
[ Vxbedÿœlbgÿhrfynesÿbcÿcjqbx`rÿbwÿ̀s~ÿ
CG?>;ÿD>H<DIBCHÿI>JBF>ÿI>;FDBK?BGC
L2!#!ÿ'#%$+'#ÿ'$(!ÿ-(!'!#ÿ*+%ÿ#!ÿ'(ÿ
,+''-ÿ+*ÿ2!ÿ(!)$!6ÿ/'ÿ$#!ÿ+*ÿM!#+'#ÿ2ÿ$''+ÿ
!ÿ'#&!%!(ÿ&2ÿ2!#!ÿ'#%$+'#1ÿ:!#!ÿ$+'#ÿ2!ÿ
:%+($ÿ#::!%ÿ+%ÿ,'*$%!%6ÿ/ÿ#ÿ2!ÿ%!#:+'#Nÿ+*ÿ
2!ÿ!M:,!'ÿ'#!%ÿ+ÿ!'#%!ÿ2ÿÿ*!(!%1ÿ#!ÿ'(ÿ
+$ÿ$+(!#ÿ%!ÿ*++&!(6
;<=>?@ÿBC;?DEF?BGC;
O!!:ÿ2!#!ÿ/'#+'ÿ/'#%$+'#ÿ*+%ÿ'(#%ÿ#*!Nÿ
'(ÿ2!ÿ:%!)!'+'ÿ+*ÿ$$(!'#6
L2!ÿ'*+%,+'ÿ'ÿ2!#!ÿ'#%$+'#ÿ,#ÿ!ÿ%!(ÿ'(ÿ
'(!%#++(ÿNÿ!)!%Nÿ:!%#+'ÿ#'-ÿ2#ÿ(!)$!6
L2!ÿ*++&'-ÿ!,#ÿ#2%!ÿ&%''-#ÿ+*ÿÿ-!'!%ÿ'%!ÿ
%!'-ÿ+ÿ2!ÿ'#+'ÿ'(ÿ#%:ÿ+*ÿ2!ÿPQRÿ
+%ÿPQRSÿ#!%!#ÿ$+'%+!%6
R!ÿ#%!ÿ+ÿ2!!(ÿ2!#!ÿ&%''-#ÿ+ÿ:%!)!'ÿ:!%#+'ÿ
'T%Nÿ+%ÿ!M:,!'ÿ(,-!6
Ymÿqbdfrjÿwcbqÿgljÿabsgcbrrjcÿ•bcÿbgljcÿ
`aajkkbc~ÿqbdfrj—€ÿqj`sesyÿweckgÿcjqbxjÿ
hbijcÿwcbqÿgljÿfsegtÿYwÿgljÿfsegÿkiegaljkÿgbÿ
v`ggjc~ÿbhjc`gebs€ÿi`egÿwbcÿ̀rrÿžukÿgbÿybÿ
bfgt
[ –rfyyesyÿbcÿfshrfyyesyÿ̀ÿYmÿqbdfrjÿwcbqÿ
`ÿhbijcjdÿabsgcbrrjcÿklbfrdÿsbgÿa`fkjÿ
d`q`yjÿgbÿjegljcÿgljÿabsgcbrrjcÿbcÿYmÿ
qbdfrjÿl`cdi`cjtÿpbijxjc€ÿsbgjÿgl`gÿ̀rrÿ
Ymÿqbdfrjkÿ̀cjÿesegèreŸjdÿfhbsÿkg`gebsÿ
kg`cgfhÿ̀sdÿewÿsbgÿ•absgesfbfkr~—ÿhcjkjsgÿ
wbrrbiesyÿ̀ÿhbijcÿa~arj€ÿierrÿvjÿ
esbhjc`vrjt
[ ubÿsbgÿhrfyÿesÿqbcjÿgl`sÿ•]—ÿYmn ¡npÿ
qbdfrjkÿesgbÿ̀ÿkesyrjÿabsgcbrrjctÿubesyÿkbÿ
ierrÿl`xjÿfsj¢hjagjdÿjwwjagkÿbsÿgljÿ
kbwgi`cj€ÿ̀sdÿq`~ÿbxjcrb`dÿgljÿhbijcÿ
kfhhr~t
[ Ymÿqbdfrjkÿ̀cjÿdjkeysjdÿgbÿvjÿdecjagr~ÿ
hrfyyjdÿesgbÿgljÿU‚n]£ ÿbcÿU‚n¡££ÿ
absgcbrrjcÿbcÿdecjagr~ÿ̀gg`aljdÿqbdfrjktÿ
ubÿsbgÿfkjÿ̀ÿcevvbsÿa`vrjÿbcÿj¢gjsdÿgljÿ
rjsyglÿbwÿgljÿYƒmÿa`vrjÿ̀kÿglekÿierrÿ
esacj`kjÿc`dègjdÿkeys`rÿsbekj€ÿ
djacj`kesyÿ̀s`rbyÿkg`vereg~€ÿ̀sdÿq`~ÿ
esgcbdfajÿabqqfsea`gebsÿhcbvrjqkt
UVWXY
XZ
[ Vÿ]^ÿ_`aÿbcÿ]^ÿ_daÿaecafegÿhbijckÿgljÿ
Ymno^npÿqbdfrjÿ̀sdÿ̀gg`aljdÿabsgcbrrjctÿ
uekabssjagÿhbijcÿvjwbcjÿeskg`rr̀gebsÿbcÿ
kjcxeaesyÿgbÿhcjxjsgÿjrjagcea`rÿklbazÿbcÿ
j{fehqjsgÿd`q`yjt
[ |`zjÿ̀rrÿabssjagebskÿesÿ̀aabcd`sajÿieglÿ
s`gebs`rÿ̀sdÿrba`rÿjrjagcea`rÿabdjktÿ}kjÿ
abhhjcÿabsdfagbckÿbsr~t
[ bÿcjdfajÿgljÿcekzÿbwÿwecjÿbcÿjrjagcea`rÿ
klbaz€ÿeskg`rrÿesÿ̀ÿabsgcbrrjdÿjsxecbsqjsgÿ
cjr̀gexjr~ÿwcjjÿbwÿabsg`qes`sgkt
[ U‚ÿabsgcbrrjckÿ̀sdÿYƒmÿqbdfrjkÿ̀cjÿbsr~ÿ
esgjsdjdÿwbcÿfkjÿ̀kÿqbsegbcesyÿ̀sdÿ
ÿ'#'-ÿ2!ÿ$+'%+!%ÿ'(ÿ
absgcbrÿdjxeajktÿbÿhcjxjsgÿd`g`ÿrbkkÿbcÿ 03LQ7 //*3
45ÿ,+(!ÿÿ2!ÿ#,!ÿ,!1ÿ%!*!%ÿ+ÿ2!ÿ
j{fehqjsgÿd`q`yj€ÿdbÿsbgÿfkjÿwbcÿ̀s~ÿ
PQR
ÿ+%ÿPQRSÿ/0L¦§§¦L/30ÿ
bgljcÿhfchbkjkt
/0L¨©ªL/30ÿ-(!ÿ!%%!ÿ+ÿ'#ÿ2!ÿ
PQRÿ+%ÿPQRSÿ$+'%+!%6ÿ/'ÿ2#ÿ$#!1ÿ
2!ÿ/345ÿ,+(!ÿ#ÿN:$Nÿ2!ÿ«::%+)!(ÿ
;L2„!…ÿ„*+†‡+ÿI&†'ˆ-‡ÿ‰!,#
…Š‹ÿŒ%!ÿÿK$ŠŒ‡+…'%„N†ÿŽ'+!ˆ#ÿ2ÿ&ÿ2!:ÿ
:+&!%ÿ#+%$!¬1ÿ#!(ÿ­®ÿ̄°±²³ÿ+*ÿÿPQR0´R
´P¨ÿ,+(!6ÿ¦ÿ,µ,,ÿ+*ÿÿ((+'ÿ/3S
:%!)!'ÿ!M:,!'ÿ(,-!ÿ+%ÿ+##ÿ+*ÿ(ÿ$#!(ÿNÿ
5ÿ,+(!#ÿ%!ÿ#::+%!(6ÿ!!ÿ¶-6ÿ6
#$ÿ(#$2%-!6
L2!ÿ,T+%ÿ#!:#ÿ+ÿ'#'-ÿ'(ÿ#%'-ÿ2!ÿ/345ÿ
,+(!ÿ%!ÿ+'!(ÿ#ÿ*++&#7
t ´2N#$Nÿ,+'ÿ2!ÿ/345ÿ,+(!ÿ&2ÿ2!ÿ
[ ‘g`geaÿal`cyjkÿhcbdfajÿxbrg`yjkÿleylÿ
PQRÿ+%ÿPQRSÿ$+'%+!%6ÿ!!ÿ·3©0L/0¸ÿ
jsbfylÿgbÿd`q`yjÿjrjagcbseaÿ
#!$+'6ÿ·¹!ÿ#%!ÿ2ÿ2!ÿ/83ÿ':ÿ$+''!$+%ÿ#ÿ
abqhbsjsgktÿljÿqeacbhcbajkkbckÿ̀sdÿ
:%+:!%Nÿ#!!(ÿ'+ÿ2!ÿ/83ÿ$+''!$+%ÿ+'ÿ2!ÿ$+'
`kkbaègjdÿaecafegc~ÿieglesÿYmno^npÿ
%+!%ÿº+%ÿ*ÿ#!(1ÿ'+2!%ÿ/3S5ÿ,+(!»6ÿ̈!*!%ÿ+ÿ
qbdfrjkÿ̀cjÿkjskegexjÿgbÿkg`geaÿdekal`cyjtÿ
2!ÿ:%!)+#ÿ/83ÿ·+(!ÿª+''!$+%ÿ́%!$+'#ÿ
’brrbiÿgljkjÿhcja`fgebskÿiljsÿeskg`rresy€ÿ
#
!$+'6
kjcxeaesyÿbcÿbhjc`gesyÿgljÿk~kgjq“
]
t
·
¹!ÿ&%'-ÿ$+''!$+'#ÿ*+%ÿ!%2ÿ-%+'(1ÿ4ÿ9$ÿ
[ Ubczÿesÿ̀ÿkg`geaÿwcjjÿ̀cj`t
:
+
&!
(ÿ/83ÿ&%'-6ÿ!!ÿP/̈/0¸ÿ#!$+'6
[ uekal`cyjÿ̀s~ÿkg`geaÿjrjagceaeg~ÿ~bfÿq`~ÿ ot ¦::N%ÿÿ:+'&!
%ÿ'(ÿ:!%*+%,ÿ'ÿ'ÿ$2!$¹+6ÿ!!ÿ
l`xjÿ̀aafqfr̀gjdtÿuekal`cyjÿkg`geaÿ
´3PQ¨ÿ
©´ÿ
¦0.ÿ/0/L/¦§ÿª5QªO3©Lÿ#!$+'6
jrjagceaeg~ÿv~ÿgbfalesyÿ̀ÿzsbisÿkjafcjr~ÿ
ycbfsdjdÿbv”jagt
BC;?<¤¤<?BGCÿ<CIÿ;?<D?¥EKÿ
GE?¤BC>
V}YmX
0123425ÿ0789
19
89
ÿ19
3ÿ/('-ÿ?*,!ÿ*A!ÿ*ÿ.$%4!4ÿE0Fÿ9*'%ÿ,%$-ÿ*(4ÿ%$;G'()ÿ;%'+ÿ
*,ÿ4$!,ÿ-!ÿ01:3ÿ!H+*(,'$(ÿ.$4/%!@ÿB$/(-'()ÿ*ÿ
Fÿ9*'%ÿ!(,/9!,ÿ*;;/9*-!ÿ*%')(.!(-ÿ$#ÿ;$((!;-$9,ÿ
!ÿ#$%%$&'()ÿ*++%'!,ÿ-$ÿ.$/(-'()ÿ*ÿ0123ÿ.$4/%!ÿ&'-ÿ E0
?
!
-&!!(ÿ*%%ÿ.$4/%!,@
*ÿ5678ÿ$9ÿ567:ÿ;$(-9$%%!9<
Fÿ9*'%ÿ.$/(-'()ÿ',ÿ'.+9*;-';*%Iÿ,;9!&,ÿ'(ÿ.$/(-'()ÿ
= !ÿ/('-,ÿ.*>ÿ?!ÿ.$/(-!4ÿ'(ÿ*(>ÿ$9'!(-*-'$(@ÿ0-ÿ',ÿ($-ÿ = 0-*#ÿ?E0
,
ÿ.*>ÿ?!ÿ/,!4ÿ$(ÿ-!ÿ;$(-9$%%!9ÿ*(4ÿ-!(ÿ'(ÿ-!ÿ01
(!;!,,*9>ÿ-$ÿ9!.$A!ÿ-!ÿ;$A!9,ÿ?!#$9!ÿ.$/(-'()@
23ÿ.$4/%!@ÿB$/(-'()ÿ-*?ÿ4'.!(,'$(,ÿ*9!ÿ, $&(ÿ'(ÿ
= B$/(-'()ÿ$(ÿ*ÿ@2ÿ'(@ÿCÿ..Dÿ&'4!ÿE0Fÿ9*'%ÿ',ÿ
9!;$..!(4!4@ÿ7$-ÿ-!ÿ;$(-9$%%!9ÿ?*,!ÿ*(4ÿ-!ÿ012 J')@ÿ@
z{|x}
x|x~}ÿ€‚ÿvvƒ
}
€„‡wÿvvƒ
w|„~w
€…}ÿvvƒ
…|„x~„…ÿ€„†xÿvvƒ
ˆ‰Š|w‡„
z{|x}
‹zŒŽ‰ÿŠ‰ˆ‰‰ÿ
‰‰‘ÿ{’ÿŽŠŒÿ
’‘{vÿ{‰ÿ“zÿ{ÿ
Ž{”‰‘ÿ“z•
…|x~y
€„…wÿvvƒ
ˆ‰Š|w‡„
z{|„…
z{|„…
z{|x}
x|„~}
x|„~}
…|x~y
€yxÿvvƒ €yxÿvvƒ
€„…wÿvvƒ
{‰Œ›ÿ‰–‰‘{zÿŽ‹ÿ—‘z‰‹ÿ˜‰‘Œz{Œÿ{’ÿ”zŒÿ™“z‹‰ÿvŽšÿ{ÿŒ”{ˆÿ”‰ÿ‹zv‰Œz{Œÿ{ÿŒŽ–‰•
˜‰‘z’šÿŽ––ÿv‰ŽŒ“‘‰v‰Œÿ‹‘z––z™•
‹zÿv{“z™ÿzŒÿ‘‰{vv‰‹‰‹ÿ{˜‰‘ÿŽŠÿv{“z™•ÿÿŒ‰‰ÿ’z™“‘‰ÿw•
vwxwyx
KLMNÿPNÿQRSÿTUVWXLWMÿYLTZW[LUW[ÿLWÿLW\]Z[ÿ^TT_N
?@ /9(ÿ$##ÿ-!ÿ+$&!9ÿ-$ÿ-!ÿ;$(-9$%%!9ÿ*(4ÿ
`9$;!4/9!ÿÿ+9$A'4!,ÿ,-!+ÿ?>ÿ,-!+ÿ.$/(-'()ÿ'(,-9/;-'$(,ÿ
4',;$((!;-ÿ-!ÿ+$&!9ÿ;$94@ÿ7!ÿ,/9!ÿ-*-ÿ*%%ÿ$#ÿ
#$9ÿ-!ÿ0123ÿ.$4/%!ÿ$(ÿ*(ÿ!H',-'()ÿ'(,-*%%!4ÿE0Fÿ9*'%@
-!ÿk6E,ÿ*9!ÿ$##@ÿB*G!ÿ,/9!ÿ-*-ÿ-!ÿ
F16a<0#ÿ-!ÿ5678ÿ$9ÿ567:ÿ;$(-9$%%!9ÿ',ÿ*%9!*4>ÿ
;$(-9$%%!9ÿ',ÿ($-ÿ9/(('()ÿ$##ÿ$#ÿ?*--!9>ÿ+$&!9@
'(ÿ/,!<
;@ l!.$A!ÿ*(>ÿ$-!9ÿ+$&!9ÿ,$/9;!<ÿF`75`B
maÿC&*%%ÿ.$/(-DIÿF`7`5l3ÿ$9ÿF`7`5l
*@ 7*;Gÿ/+ÿ'-,ÿ;$(#')/9*-'$(ÿ-$ÿ>$/9ÿ̀bÿ/,'()ÿ
mF3ÿCE0Fÿ.$/(-Dÿ.$4/%!@ÿnUÿWUXÿ
F'*)*9*ÿcdeÿ5$9G?!(;ÿ@(@((@ÿ ',ÿ',ÿ
iZ\UWWZ\XÿRÿofpqrfsqtuÿC&*%%ÿ.$/(-ÿ
4$(!ÿ/,'()ÿ*ÿ+%*-#$9.ÿ;$((!;-'$(ÿ-$ÿ-!ÿ
.$4/%!Dÿ*#-!9ÿ'(,-*%%'()ÿ*(4ÿ+$&!9'()ÿ-!ÿ01
;$(-9$%%!9Iÿ/,'()ÿ-!ÿ?*;G/+ÿ;$..*(4ÿ'(ÿ-!ÿ
23ÿ.$4/%!@ÿ !ÿ0123ÿ, $/%4ÿ?!ÿ-!ÿ$(%>ÿ
fgRXhUiTÿjYTLWL[XiRXLUWÿA'!&@
+$&!9ÿ,$/9;!ÿ#$9ÿ-!ÿ5678ÿ;$(-9$%%!9@
0123425ÿ0789
19
89
ÿ19
tK=Rÿ
tK=RÿX
tK=Rÿ
tK=Rÿ
tK=Rÿ
ÿ!"ÿ#$%ÿ&$'ÿ(%)"
x=>:?=ÿKN=ÿU:KK:>ÿ@V6ÿQ:PP=QK:<ÿRDCTjJkÿKNGKÿQ:?=<ÿKN=ÿRDGJKHQÿF@5ÿD:QSHPTÿQDHRO
z:JHKH:PÿKN=ÿ@6Aÿ>:BCD=ÿ:PÿKN=ÿ<GHDIÿKHDKHPTÿK:ÿN::SÿF@5ÿ<GHDÿKGUJÿ:?=<ÿ:P=ÿ=BT=ÿ:EÿKN=ÿF@5ÿ<GHDOÿjt==ÿWHTOÿ
Xk
yJ=ÿGÿJQ<=LB<H?=<ÿK:ÿR<MÿB:LPÿKN=ÿRDGJKHQÿD:QSHPTÿQDHRIÿGPBÿRCJNÿB:LPÿGPBÿHPÿ:PÿKN=ÿ@6AIÿK:ÿE:<Q=ÿKN=ÿ
QDHRÿK:ÿJPGRÿ:?=<ÿKN=ÿ=BT=ÿ:EÿKN=ÿF@5ÿ<GHDO
tDHB=ÿKN=ÿ@6Aÿ>:BCD=ÿGD:PTÿKN=ÿF@5ÿ<GHDÿK:ÿQ:PP=QKÿHKJÿXR:JHKH:PÿRDCTÿHPK:ÿp8|Xÿ:<ÿp8|iÿ
Q:PK<:DD=<ÿj:<ÿHEÿCJ=BIÿGP:KN=<ÿ@6iAÿ>:BCD=kOÿpHKNÿGDDÿ>:BCD=JÿQ:PP=QK=BIÿKN=ÿ@6Aÿ>:BCD=ÿHJÿGKÿ:P=ÿ
=PBOÿuGS=ÿJC<=ÿKNGKÿGDDÿ>:BCD=JÿG<=ÿEH<>DMÿJ=GK=BO
7:ÿS==RÿKNHJÿGJJ=>UDMÿE<:>ÿJDHBHPTÿ:PÿKN=ÿF@5ÿ<GHDIÿJ=QC<=ÿKN=ÿ@6AÿjDGJKÿ>:BCD=kÿLHKNÿQDHRJÿR<:?HB=BÿUMÿ
KN=ÿF@5ÿ<GHDÿ?=PB:<Iÿ:<ÿRDGQ=ÿGÿJQ<=LÿHPÿ:P=ÿ:EÿKN=ÿ>:CPKHPTÿKGUJÿHPÿKN=ÿUGJ=ÿ:EÿKN=ÿ@6Aÿ>:BCD=O
†Ž}~‚€ƒÿ†~}ÿ…‚€ÿ†‡‚ˆ
}~€‚€ƒÿ~€ÿ…‚€ÿ†‡‚ˆ
‰Š‹ŠŒ
‰Š‹ŠŒŒ
‘’“”Š•–
—˜”‹™
‘’“”Š•–
Š®”‹¦Œ™ÿ
ž¯–ÿ‰‰Ÿ
™ž–”¥§¦–Œÿ™‰‰Ÿ
ÿ
‰Š‹ŠŒ™
—˜”‹™
š›ÿ˜ÿ‘˜
žŠŸÿ‰˜ š¡’¢
‘’“”–˜”–Œÿ£¤’ÿ
¢š››˜¤’ ¥”–¦§ÿž–§–ÿ‰‰Ÿ
Œ”‹¦§ÿž–ŒŠÿ‰‰Ÿ
‘’“”Š•–
—˜”–Œ
—˜”–Œ
–•”––¦‹ŠÿžŠŒ‹ÿ‰‰Ÿ
–‹”‹¥¦Œ™ÿž‹™ÿ‰‰Ÿ
–Œ”–‹¦–Œÿž™Š¥ÿ‰‰Ÿ
—˜”–Œ
—˜”‹™
¨˜’©ÿÿ—ªÿ—¨¢£¡¡—¨«
—˜”–Œÿÿ‰˜ š¡’¢
¬’ÿ—˜”‹™ÿ‰˜ š¡’
—¨¢£¡¡¢ÿ£ÿ¬’ÿ’¨ ÿ
˜ªÿ¬’ÿ­¬£—¨
*$+"ÿ,"ÿ-./01/2ÿ3'ÿ(%)$%+ÿ)&$'4"
56789 7:ÿ<=>:?=ÿ@6Aÿ>:BCD=ÿE<:>ÿF@5ÿ<GHDIÿJDHB=ÿHKÿGLGMÿE<:>ÿ:KN=<ÿ>:BCD=JOÿ@PJ=<KÿGÿJQ<=LB<H?=<ÿHPÿKN=ÿQ=PK=<ÿ
RDGJKHQÿD:QSHPTÿKGUÿGPBÿRCDDÿB:LPLG<BJIÿKN=PÿDHEKÿKN=ÿCPHKÿ:CKLG<BJOÿ@Kÿ>GMÿU=ÿP=Q=JJG<MÿK:ÿ<=>:?=ÿGPÿ
@V6ÿQ:PP=QK:<ÿRDCTÿGJÿJN:LPÿGKÿKN=ÿK:Rÿ:EÿWHTÿXO
YZ[\]ÿ_[`Zabÿ[c]ÿbd\efc[_ÿ rf\fcs
_7NZg
[
b
f
Zc
h
t==ÿWHTOÿÿK:ÿD:QGK=ÿQ:PP=QK:<JÿGPBÿ:KN=<ÿQ:>R:P=PKJÿ:Pÿ
KN=ÿQ:PK<:DD=<O
=ÿ@6Aÿ>:BCD=ÿR<:?HB=JÿiÿCPH?=<JGDÿHPRCKJÿ
uGS=ÿQ:PP=QKH:PJÿK:ÿKN=ÿ@6AÿQ:PK<:DD=<ÿHPÿKN=ÿ
JCRR:<KHPTÿGPGD:TÿHPRCKJÿjK=>R=<GKC<=Iÿ<=JHJKGPQ=Iÿ
PTÿ:<B=<O
?:DKGT=ÿGPBÿQC<<=PKkÿGPBÿBHTHKGDÿHPRCKJÿjQ:PKGQKÿQD:JC<=Iÿ E:D!D:"LHv:
PP=QKÿKN=ÿ=G<KNÿT<:CPBÿLH<=ÿjLHKNÿJRGB=ÿQ:PP=Q
RCDJ=ÿQ:CPKkÿGPBÿlÿ:CKRCKJ9ÿÿ<=DGMÿjXÿmGQVQBIÿOÿnÿ
K:<kÿE<:>ÿKN=ÿ=G<KNÿT<:CPBÿDCTÿ:PÿKN=ÿ@6iAÿ
>GoOkÿ:CKRCKJÿGPBÿlÿGPGD:Tÿ:CKRCKJÿjÿmBQkOÿpH<HPTÿ
>:BCD=ÿK:ÿGÿP=G<UMÿ=G<KNÿT<:CPBÿR:HPKOÿt==ÿ
K=<>HPGDÿR:JHKH:PJÿG<=ÿJN:LPÿHPÿWHTOÿÿGD:PTÿLHKNÿq8Fÿ
wx6y5F@5wÿJ=QKH:PÿE:<ÿB=KGHDJO
D:QGKH:PJO
," z<=RG<=ÿR:L=<ÿLH<HPTÿjD=G?=ÿKN=ÿCPHKÿR:L=<=Bÿ:EEkOÿ
t==ÿz:L=<ÿpH<HPTÿJ=QKH:PÿE:<ÿB=KGHDJO
0" v:PP=QKÿ@V6ÿLH<HPTOÿt==ÿ@PRCKJÿGPBÿ6CKRCKJÿJ=Q
KH:PJO
1" nRRDMÿR:L=<ÿK:ÿKN=ÿCPHKOÿt==ÿz6p8xÿyzÿn5Fÿ@5@
7@nqÿvA8v{6y7ÿJ=QKH:PJO
0123425ÿ0789
19
89
ÿ19
›‰Š‰‘Œÿ•”Œ¡ ›œ ›— ›˜ ››ž ›Ÿ›™ ›š›§ ›œ¥
Œ‹Œ“Šÿ¦›’
“‘‘ˆ ’“– ’“– ’“– ’“– ’“–
Œ—
Œž
¢›“ˆ£ÿœ¤œ¥ œ — ˜  ž Ÿ ™ š § œ¥ Œœ¥¦ Œ˜¥¦Œ ¥¦ŒŸŒ™¥¦Œš ¢“‘‘ˆ
Œ“ˆ£ÿœ¤š
›œœ’— ›—›˜ ˜’ › ›žž’Ÿ›Ÿ ›™ ™’š›š ›§§’œš›œ¥ Œœ ¥¦ Œ— Œ˜ ¥¦ Œ Œž ¥¦ ŒŸ Œ™ ¥¦ Œš
ˆ‰Š‹Œÿ‰‹‘
’“‹‹”’‘“•
›“ÿ•”Œ¡ÿ
”›ˆ
ª“Œ•›ÿ
ˆ‘Œ‘ˆÿ”›
“©”•ÿ”›
œ ¥¦ —˜ ¥¦ ž ¥¦ Ÿ ™ ¥¦ š œ ¥¦ —˜ ¥¦ ž ¥¦ Ÿ ™ ¥¦ š
‹‰¦”•ˆŒ ‰œ ‰— ¥¦ ‰ž ‰Ÿ ¥¦ ‰§ ‰œ¥ ¥¦ ‰œ˜‰œ ¥¦ —¨—‹
‰‹‘ˆ
¢ˆ£ÿœ¤œŸ ¥¦ ‰˜ ‰ ¥¦ ‰™ ‰š ¥¦ ‰œœ‰œ— ¥¦ ‰œž‰œŸ—ÿ¦Œ’
“•ÿ¦›’
–—˜—™š
“©”•
!ÿ#$%&'ÿ(%)*!+ÿ,-$+#ÿ.*(ÿ/0ÿ1!/ÿ23/ÿ445ÿ1,ÿ
”Œ•‘¨ÿ
Š•“‹›ÿ
’“‹‹”’‘“•ÿ
Š
,ÿ,')<!ÿ1!ÿ?1(/ÿ3Cÿ&'#ÿ9:3;ÿ4)+*.#k,ÿf-),1&1)!ÿ
-)<#%ÿ=)!!#=&)%ÿ1,ÿ.)=$&#+ÿ$&ÿ&'#ÿ.)<#%ÿ=)%!#%ÿ)8ÿ&'#ÿ*!1&/ÿ
-.*(ÿ&'#ÿ=)!!#=&)%ÿ8%)4ÿ&'#ÿ4)+*.#ÿ$!+ÿ4$q#ÿ
-%)61+#+ÿ)!ÿ&'#ÿ7$,#ÿ)8ÿ&'#ÿ9:3;ÿ4)+*.#ÿ2$,ÿ<#..ÿ$,ÿ p!
&'#ÿ=)!&%)..#%ÿ$!+ÿ&'#ÿ9:>;5ÿ8)%ÿ=)!!#=&1)!ÿ&)ÿ#$%&'ÿ =)!!#=&1)!,ÿ&)ÿ1&ÿ$,ÿ,')<!/
(%)*!+/ÿ?)%ÿ4$@14*4ÿ-%)&#=&1)!ÿ8%)4ÿ#.#=&%),&$&1=ÿ
ÿ!)&ÿ$--.dÿf3ÿgÿ-)<#%ÿ2%#1!,#%&ÿ=)!!#=&)%ÿ
+1,='$%(#ÿ)%ÿ)&'#%ÿ8)%4,ÿ)8ÿAB9Cÿ=)!!#=&ÿ#$='ÿ#$%&'ÿ h:cAi o)
.
*
(ÿ1!&)ÿ&'#ÿ9:3;5ÿ*!&1.ÿ$..ÿ)&'#%ÿ<1%1!(ÿ1,ÿ
(%)*!+ÿ*,1!(ÿ$ÿD>ÿEFÿ)%ÿ.$%(#%ÿ<1%#/ÿG##-ÿ&'#,#ÿ<1%#,ÿ
=
)
4.#&#+Cÿ1!=.*+1!(ÿ9:3;ÿ1!-*&,ÿ$!+ÿ)*&
$,ÿ,')%&ÿ$,ÿ-),,17.#/ÿ
-*&,/ÿH##ÿl:EArÿplÿhoÿ9h9c9sÿe;AeG
:pcÿ,#=&1)!/
H##ÿ?1(/ÿ3ÿ8)%ÿ&'#ÿ.)=$&1)!ÿ)8ÿ&'#ÿ#$%&'ÿ(%)*!+1!(ÿ<1%#ÿ8)%ÿ
9:3;/
tA$u='ÿ)v8wÿ&'#ÿ0ÿ*!16#%,$.ÿ1!-*&,ÿ2p95ÿ=$!ÿ,*--)%&ÿ$!dÿ)!#ÿ)8ÿ
&'#ÿ8)..)<1!(i
‰“¤˜
©”ª¤—¥œ
m cd-#ÿGÿ)'4ÿc'#%41,&)%ÿ2$.,)ÿ,##ÿh)&#ÿ1!ÿ
r#,1,&16#ÿqÿ)'4,ÿ,#=&1)!5
m r#,1,&16#ÿGÿ)'4,
m ÿg+=
”Œ•‘¨ÿŠ•“‹›
m 3fÿ4
—ÿ¦›’ÿ“©”•ÿ
m n1!$%dÿ9!-*&
›”›‰’Œ‘”›ÿ—ÿ¦Œ’ÿ
ˆ¡ÿ¢“Œ•‰‘¡ÿ
‘•Œ‹ˆ«“•–”•ÿ
‹”‰‘¨”•ÿˆ‰›”ÿ“«ÿ
ˆ”’“‹›Œ•¡ÿ‘‰”›ÿ
‘“ÿ”Œ•‘¨ÿŠ•“‹›
‰‹”ÿ¦“‘ŒŠ”
¢–Œ‰‹ˆ£
—ÿ¦›’
“•
‹“‘ÿ’•‰‘‰’Œ£
‹”‰‘¨”•ÿˆ‰›”ÿ‘‰”›ÿ
‘“ÿ”Œ•‘¨
­¬ —ÿ¦›’
–—˜—™§
IJKLÿNLÿOPQNRQSÿTUVWXÿKVYZ[\ÿ]Y[[T]WJY[L
^c'#_`
ÿb
ÿ9:3;ÿ4)+*.#ÿ=$!ÿ7#ÿ-)<#%#+ÿ7dÿ<1%1!(ÿ&)ÿ$ÿ
\T\J]UWT\ÿe.$,,ÿfCÿf3ÿgÿ&%$!,8)%4#%Cÿ)%ÿ&)ÿ$ÿf3g+=ÿ
-)<#%ÿ,)*%=#/ÿc'#ÿ9:3;ÿ-%)61+#,ÿ-)<#%ÿ&)ÿ&'#ÿ
$&&$='#+ÿ=)!&%)..#%ÿ$!+ÿ*-ÿ&)ÿ&<)ÿ$&&$='#+ÿ9:>;ÿ
4)+*.#,ÿ218ÿ*,#+5/
h:cAi 98ÿ-)<#%1!(ÿ8%)4ÿ$ÿf3ÿgÿ&%$!,8)%4#%Cÿ+)ÿ!)&ÿ
-)<#%ÿ)&'#%ÿ#j*1-4#!&ÿ<1&'ÿ1&/ÿ:&'#%<1,#Cÿ=)!
+*=&#+ÿ!)1,#ÿ-%)7.#4,ÿ4$dÿ%#,*.&/ÿ.,)Cÿ+)ÿ!)&ÿ
(%)*!+ÿ#1&'#%ÿ,1+#ÿ)8ÿ&'#ÿ&%$!,8)%4#%k,ÿf3gÿ,#=
)!+$%d/
l)<#%ÿ=)!,*4-&1)!ÿ+#-#!+,ÿ)!ÿ1!,&$..#+ÿ$==#,,)%1#,ÿ
$!+ÿ)-&1)!ÿ=$%+,Cÿ$!+ÿ4$dÿ6$%dÿ8%)4i
m EAnfÿ)%ÿEAn>ÿ=)!&%)..#%ÿ<1&'ÿ9:3;ÿ4)+*.#ÿ
$.)!#iÿ$--%)@14$&#.dÿ0/ÿg ÿ2e5ÿ)%ÿ0/ÿEÿ2oe5
m EAnfÿ)%ÿEAn>ÿ<1&'ÿ9:3;Cÿfÿ$++1&1)!$.ÿ9:
>;ÿ4)+*.#,Cÿ-.*,ÿ)-&1)!ÿ7)$%+,iÿ*-ÿ&)ÿfÿg ÿ2e5ÿ)%ÿ
fE 2oe5/
xc'y#`ÿ1!z
wv
-*&,ÿ,*--)%&ÿGÿc'#%41,&)%ÿ&#4-#%$&*%#ÿ,#!,)%,ÿ
*,1!(ÿ$ÿ{XTV|J}WYVO[~ZWYJ[W/ÿ9!-*&ÿ$==*%$=dÿ1,ÿ1!ÿ&'#ÿ
%$!(#ÿ)8ÿ€ÿ)8ÿ,-$!/ÿndÿ+#8$*.&Cÿ=)!6#%,1)!ÿ1,ÿ8)%ÿ
,&$!+$%+ÿcd-#ÿÿ&'#%41,&)%ÿ,#!,)%Cÿ<1&'ÿ$ÿ,#!,)%ÿ%$!(#ÿ)8ÿ
‚ÿ&)ÿ‚ÿ?ÿ2f/‚ÿ&)ÿ/f‚ÿe5/ÿp,1!(ÿ$ÿ=)!6#%,1)!ÿ&d-#ÿ
)8ÿƒc$7*.$%ÿc'#%41,&)%„Cÿ$ÿ+188#%#!&ÿ&'#%41,&)%ÿ%#,-)!,#ÿ
=*%6#ÿ=$!ÿ7#ÿ,-#=181#+ÿ7dÿ14-)%&1!(ÿ$ÿ&'#%41,&)%ÿ
=*%6#/@4.ÿ81.#/ÿe*%%#!&.dCÿ&'#ÿh+1)ÿ4)+*.#ÿ=)!&$1!,ÿ$!ÿ@4.ÿ
8).+#%ÿ<1&'ÿ&'#%41,&)%ÿ=*%6#,ÿ8)%ÿ$ÿr$+1)ÿH'$=qÿ,#!,)%ÿ
4)+#.ÿfÿ$!+ÿcA>ÿGÿ&d-#ÿ,#!,)%/ÿ
e*,&)41…#+ÿ&'#%41,&)%ÿ@4.ÿ81.#,ÿ4$dÿ7#ÿ#+1&#+ÿ)%ÿ
#@-)%&#+ÿ28)%ÿ%#*,#5/ÿH##ÿ&'#ÿh1$($%$ÿ†ÿh+1)ÿF*1+#ÿ8)%ÿ
4)%#ÿ+#&$1.,/ÿ?1(/ÿÿ,')<,ÿ&'#ÿ<1%1!(ÿ+1$(%$4/
‰œ¥¦ ‰— ‰˜ ¥¦ ‰
œ¥®
‘¨”•–‰ˆ‘“•
ˆ¨‰”›”› ÿ‘©‰ˆ‘”›
’Œª”ÿ—¥¥«‘ÿ¢Ÿœ–£
–Œ¯‰––
ˆ¨‰”› ˆ‘›ÿ‰‹
”‹’“ˆ•”
IJKLÿRLÿ{XTV|J}WYVÿ‡JVJ[KL
–—˜—™¥
0123425ÿ0789
19
89
ÿ19
@+6=ÿ‹ÿ0(:80ÿ/()ÿ8+3+,6ÿ4+2632;=ÿ@:3ÿ2ÿ-.70)ÿ4+2632;ÿ
'()ÿ+,-./0ÿ12ÿ,ÿ!3")24ÿ2#ÿ3ÿ)$0%+0/&
+5)ÿ0+6,27ÿ8+/(+,ÿ2ÿ32,6)ÿ93:;ÿ 1:,/21/ÿ.0)ÿ/()ÿŒNLJGDrIJKLGMNFJGÿ+,ÿ/()ÿ0/2/+:,ÿ
2/2V20)=ÿ@:3ÿ:/()3ÿ43Yÿ1:,/21/0<ÿ.0)ÿ/()ÿ
ÿ/:ÿ<ÿ:(;0=ÿ>+3+,6ÿ+0ÿ/()ÿ02;)ÿ20ÿ0(:8,ÿ9:3ÿ2ÿ 4NNe
DfJIJKLGMNFJG=ÿÿ
'()3;+0/:3ÿ/);-)32/.3)ÿ0),0:3=ÿ?))ÿ@+6=ÿ=
À·¦¤¨ À·¼ À·Á ¤¨ À·Ê
A)0+0/+5)ÿ0+6,270ÿ3)B.+3)ÿ2ÿCDEFEGFHDIJKLGMNFJG=
OP'QR STÿ+,-./0ÿ23)ÿ:-/+;+U)4ÿ/:ÿ-3:5+4)ÿ/()ÿV)0/ÿ3)0: ÍÎÏÐÑ
ÿ¼¤ÿ¶Òÿ̧ȤÓÿ©À¹ÔÿªÔª±¬
7./+:,ÿ23:.,4ÿ/()ÿWÿ:(;ÿ32,6)=ÿ@:3ÿ2ÿ0),0:3ÿ ¯º­Å¬Æ
¾·­·¾À¾ÿ©´¬±±ÿ¹·¾¬ÿÇÿ¼Èÿ¾«
À«¬ÿ³®·­¹Æÿ
8+/(ÿ2ÿ32,6)ÿ923ÿ93:;ÿWÿ:(;0ÿX0.1(ÿ20ÿ
ÕÖ×ØÙÚÛÜØÝ×ÙÝÖÜØÙ
:(;ÿ/Y-)Z<ÿ3)0:7./+:,ÿ8+77ÿV)ÿ-::3=ÿ':ÿ.0)ÿ0.1(ÿ2ÿ
0),0:3<ÿ+/ÿ+0ÿ3)1:;;),4)4ÿ2ÿ/32,0;+//)3ÿ/(2/ÿ-3:
«¶·¬±©¬©ÿ̧¹´·«¹¬©
«¶·¬±© «¹À©ÿ·­
ªº»±¬ÿ¼¤¤²¹ÿ°½¦¾µ
4.1)0ÿ2ÿ[41ÿ:3ÿ;\ÿ0+6,27ÿV)ÿ+,0/277)4=ÿ>+3)ÿ/()ÿ
¬­ª±®«À¯¬
¾º¿·
¾À¾
/32,0;+//)3ÿ/:ÿ/()ÿSTÿ211:34+,6ÿ/:ÿ/()ÿÿ[41ÿ:3ÿ
À·¦¤¨ À·¼À·Á ¤¨ À·Ê
]^ÿ;\ÿ+,0/3.1/+:,0=
!"ÿ_`a
'()ÿ+,-./0ÿ0.--:3/ÿ0)79-:8)3)4ÿÿ[41ÿ0),0:30=ÿT,-./ÿ
+;-)42,1)ÿ+0ÿ63)2/)3ÿ/(2,ÿWÿ:(;0=ÿÿ5:7/ÿ211.321Yÿ+0ÿ
b^cÿ:9ÿ0-2,<ÿ8+/(:./ÿ.0)3ÿ127+V32/+:,=ÿ@+6=ÿÿ0(:80ÿ/()ÿ
8+3+,6ÿ4+2632;=ÿÿ[41ÿ0),0:30ÿ3)B.+3)0ÿ2ÿ
dNeGfgDIJKLGMNFJG=
À·¦¤¨ À·¼À·Á ¤¨À·Ê
¤¥¦¤ÿ̈©ªÿ«¬­«®¯
°«¬±²¥³®´¬¯¬©ÿ
«¬­«®¯µ
䥦¤
«¶·¬±©¬©ÿ̧¹´·«¹¬©
Ĩ©ª ªº»±
¬ÿ̧¼¤¤²¹ÿ°½¦¾µ
¾º¿·¾À¾
¯º­Å¬Æÿ¤¥¦¤ÿ̈©ªÿ
·­³À¹ÿ·¾³¬©º­ª¬ÿÇÿÈÉÿ®¶¾«
«¶·¬±©
«¹À©ÿ·­
¬­ª±®«À¯¬
¾¼Á¼Â¦
hFgiÿkiÿlmnlÿdopÿqFrFJgi
s'(!t)ÿ+,ÿ-&u
./0ÿ0.--:3/ÿ0)79-:8)3)4ÿ]^ÿ;\ÿ0),0:30=ÿT,-./ÿ
211.321Yÿ+0ÿb^cÿ:9ÿ0-2,<ÿ8+/(:./ÿ.0)3ÿ127+V32/+:,=ÿ@+6=ÿÿ
0(:80ÿ/()ÿ8+3+,6ÿ4+2632;<ÿ8(+1(ÿ3)B.+3)0ÿ2ÿ]ÿ:(;ÿ
3)0+0/:3ÿ8+3)4ÿ213:00ÿ/()ÿ+,-./ÿ/)3;+,270=ÿ]^ÿ;\ÿ
0),0:30ÿ270:ÿ3)B.+3)ÿ/()ÿdNeGfgDIJKLGMNFJG=ÿ
À·¦¤¨ À·¼À·Á ¤¨ À·Ê
Ê¥¼¤ÿ¾ºÿ«¬­«®¯
°«¬±²¥³®´¬¯¬©ÿ
«¬­«®¯µ
Ã
Ì
Ä
¯º­Å¬Æÿ¤¥¼¤ÿ¾º
«¶·¬±©¬©ÿ̧¹´·«¹¬©
ªº»±¬ÿ̧¼¤¤²¹ÿ°½¦¾µ
¾º¿·¾À¾
ÊËËÿ®¶¾ÿ̄¬«·«¹®¯
°«À³³±·¬©ÿ́ ·¹¶ÿÀ­·¹µ
«¶·¬±© «¹À©ÿ·­
¬­ª±®«À¯¬
hFgiÿviÿwmxlÿyzÿqFrFJgi
¾¼Á¼Â¼
À«¬ÿ³®·­¹Æÿ
çÖÖèÚéØÜØÝ×ÙÝÖÜØÙ
ÞßàÿâãäåæâåÐ
«¶·¬±©¬©ÿ̧¹´·«¹¬©
ªº»±¬ÿ¼¤¤²¹ÿ°½¦¾µ
¾º¿·¾À¾
«¶·¬±© «¹À©ÿ·­
¬­ª±®«À¯¬
hFgiÿŽiÿFJfrÿFJKLGÿqFrFJgi
¾¼Á¼ÂÁ
‚
‚
'()ÿTP]†ÿ;:4.7)ÿ(20ÿÿ4+6+/27ÿ3)72Yÿ:./-./0ÿ2,4ÿ‹
ÿ5:7/ÿ2,27:6ÿ:./-./0=
Q21‘(}ÿ3)7ÿ2‚
‚
Yÿ:./-./ÿ+0ÿ32/)4ÿ2/ÿ^]ÿ[21ÿ:3ÿ[41ÿ2/ÿ=ÿ\=ÿA)72Yÿ
:./-./0ÿ(25)ÿ‡P[ÿX;)/27ÿ:’+4)ÿ523+0/:3Zÿ0.--3)00:30ÿ/:ÿ
0.--:3/ÿ+,4.1/+5)ÿ/Y-)ÿ7:240ÿ0.1(ÿ20ÿ()25Yÿ4./Yÿ3)72Yÿ
1:+70=
“zC”I
”•
CDefEÿfrDÿJNGÿrfGDoÿ–NrÿzŒÿyfFJEÿ—eFJDÿeDHDe˜ÿ
KNqDrDoÿeNfoEÿ—FJEGDfo™ÿxwÿdÿyfšFyLy˜iÿ
”DHDrÿLEDÿG›DÿpNJGrNeeDrEÿKNqDrÿGrfJE–NryDrÿ
GNÿKNqDrÿIœÿeNfoEiÿžEFJgÿpNJGrNeeDrÿ
GrfJE–NryDrÿFJGrNoLpDEÿKNGDJGFfeeÿofyfgFJgÿ
EqFGp›FJgÿGrfJEFDJGEÿFJGNÿG›DÿpNJGrNeeDri
S0)ÿ2ÿNNeDfJLGKLG“rFGfŸeDÿ+,ÿ/()ÿ0/2/+:,ÿ9:3ÿ)21(ÿ
:./-./=ÿ@+6=ÿÿ0(:80ÿ2,ÿ)’2;-7)ÿ8+3+,6ÿ4+2632;=ÿ
ÿ
¼Êÿ̈ºªÿ
¹¯º­«²®¯¾¬¯ ºª
­«
°«¬¬ÿ́º¯­·­Åÿ ¾º·
°±·­¬µ
º»®¨¬µ
®¯
{'()|ÿ.},~+5)ÿ€3|027ÿ‚+,-./0ÿ0.--:3/ÿV:/(ÿ-.70)ÿ1:,/21/0ÿ2,4ÿ
¼Êÿ̈©ªÿ³®´¬¯
«À³³±Ô
Ã
Ä
¼Êÿ̈©ª
¼Êÿ̈©ª
ë¦
ë¼
ëÁ
Êÿ̈ºª
ëÊ ±¼®º©«
,:3;27ÿ43YÿX)B.+-;),/ÿ0/2/.0Zÿ1:,/21/0=
ƒ „.70)ÿ1:,/21/0ÿ;2Yÿ(25)ÿ2ÿ1(2,6):90/2/)ÿX…P?Zÿ
©¦ ª ©¼©Á ª ©Ê
¦ÿ̧¼
Áÿ̧Ê ¾¼Á¼ê¤
93)B.),1Yÿ:9ÿ.-ÿ/:ÿ^ÿ†Uÿ8+/(ÿ2ÿcÿ4./Yÿ1Y17)=
OP'QR ‡+,+;.;ÿ48)77ÿ/+;)ÿ;.0/ÿV)ÿˆ^ÿ;0=
hFgiÿ iÿCDefÿNLGKLGÿqFrFJgÿoFfgrfyi
X…:,/21/0ÿ;.0/ÿ3);2+,ÿ:-),ÿ2/ÿ7)20/ÿ^ÿ;0ÿ2,4ÿ
V)ÿ17:0)4ÿ2/ÿ7)20/ÿ^ÿ;0Z
OP'QR -:0+/+:,ÿ¡Pÿ1:,,)1/:3ÿ-7.6ÿ(20ÿÿ1:;;:,ÿ
/)3;+,270ÿ¢…£ÿXÿ^<ÿÿÿ]<ÿÿÿ<ÿÿÿ‹<ÿÿÿZ<ÿ
ƒ ?/2,4234ÿ43Yÿ1:,/21/0ÿ;.0/ÿ(25)ÿ2ÿÿ†UÿX:3ÿ7)00Zÿ…P?ÿ
8(+1(ÿ23)ÿ+0:72/)4ÿ93:;ÿ)21(ÿ:/()3=ÿ'(+0ÿ12,ÿV)ÿ
93)B.),1Y<ÿ8+/(ÿ;+,+;.;ÿ48)77ÿ/+;)ÿˆÿ;0=
.0)9.7ÿ8(),ÿ-:8)3+,6ÿ7:240ÿ93:;ÿ4+99)3),/ÿ^]ÿ
X…:,/21/0ÿ;.0/ÿ3);2+,ÿ:-),ÿ2/ÿ7)20/ÿÿ;0ÿ2,4ÿV)ÿ
[21ÿ0:.31)0=
17:0)4ÿ2/ÿ7)20/ÿÿ;0Zÿ
‰:/(ÿ/Y-)0ÿ:9ÿ43Yÿ1:,/21/0ÿ0.--:3/ÿ=ÿ[41ÿ:-),ÿ1+31.+/0ÿ
:3ÿÿŠ\ÿ0(:3/1+31.+/ÿ1.33),/=
ÿÿ !ÿ"#$#%"ÿ&'(&)$#*ÿ+*ÿ$),ÿ*$ÿ-!ÿÿ!.ÿ&"ÿ
)$#(ÿ'ÿ#,ÿ/$*(ÿ-0&12ÿ.3ÿ$'(ÿ$"ÿ4&"&/ÿ#,*%1,ÿ#,ÿ
)4*2ÿ5'(*ÿ'*6$ÿ7*$#&'3ÿ$),ÿ(&1&#$ÿ"#$#%"ÿ !ÿ
&'(&)$#"ÿ$)#&4&#ÿ$"ÿ+"8
9 :;;ÿÿ*$ÿ7'<'ÿ)%**'#ÿ+"2
9 :=ÿÿ*$ÿ)"(<$(ÿ)%**'#ÿ+"2
>,*+*3ÿ$'ÿ:=ÿ"#$#%"ÿ&'(&)$#"ÿ#,$#ÿ#,ÿ$(ÿ&"ÿ
7*(2
?'@$AB1CÿK%
DÿFG
HIGHJ
#7%#"ÿ-K.ÿ$*ÿ*+*')(ÿ/ÿ#,ÿ#*6&'$"ÿ
$/(ÿLÿ$'(ÿÿMÿ-1*%'(.2ÿ$),ÿKÿ)$'ÿ"%77ÿ$ÿ
6$N&6%6ÿ+ÿOÿ6ÿ4*ÿ#,ÿ'#&*ÿÿ#ÿÿM()ÿ*$'12ÿ>,ÿ
6&'&6%6ÿ&'7%#ÿ&67($')ÿ+ÿ$ÿ(4&)ÿ)'#*(ÿ/ÿ$'ÿ
Kÿ6%"#ÿ/ÿ1*$#*ÿ#,$'ÿPÿ,6"2ÿ>7&)$ÿ&*&'1ÿ+*ÿ$'ÿ
Kÿ&"ÿ",'ÿ&'ÿ0&12ÿ2
0*ÿ$),ÿK3ÿ%"ÿ$ÿQRSTUVW:XTYXTZ[\TU]SWÿ&'ÿ#,ÿ"#$#&'ÿ
($#$/$"2ÿÿ
¥¬¤¥ÿ¦®¯ÿ®°¦±̄°
±¿À¾¶ÿ±©À°®£¿¯°
±²ÿÁ°£¶°Âÿ¶³£¿
§Ã¥¥ÿij©²
¯Ä©©Ä¿ÿºÅ¼
±¿À¾¶ÿºÆ¼
²³±°´®°®µÿ¶·±²¶°®ÿ
¯£¸´°µÿ§¥¥ÿ¹¶ÿº»¤©¼ÿ
©£½±©¾©
£¤ ¥¦ £§ £¨ ¥¦ £« ©§¨§ª¤
^\V_ÿa_ÿb=USRVÿRXTYXTÿc\[\=Vÿd\UV[Ue_
fFghi?jkÿlkfmjnohnFp
q'ÿ#,ÿr&$1$*$ÿ"#$#&'ÿ&'#*+$)ÿ#ÿ#,ÿs tPÿ$'(ÿ
s tuÿ)'#**3ÿ$),ÿq<Kÿ6(%ÿ$77$*"ÿ$"ÿ'ÿ
vd\RwRU[dÿ%'(*ÿ#,ÿ"#$#&'x"ÿvd\RvWTcR[y2ÿq+ÿ$ÿ
)'#**ÿ,$"ÿ'ÿ'ÿqKOzÿ6(%3ÿ#,ÿr(&r#*{ÿ
,$"ÿ$ÿ"&'1ÿvd\RwRU[dÿ)67''#3ÿ,*ÿ#,ÿ|qÿ}*#~ÿ
7*7*#ÿ+ÿ#,ÿvd\RwRU[dÿ&"ÿ2ÿÿ0&12ÿ3ÿ#72
57'ÿ(&")4*3ÿ&+ÿ#,ÿ)'#**ÿ,$"ÿ6%#&7ÿ
qKuzÿ6(%"3ÿ#,ÿ6(%ÿ)""#ÿ#ÿ#,ÿ)'#**ÿ&"ÿ
#,ÿ+&*"#ÿvd\RwRU[dÿ-7*7*#ÿqÿ}*#ÿ€.3ÿ#,ÿ'N#ÿ6(%ÿ
&'ÿ#,ÿ),$&'ÿ&"ÿvd\RwRU[d€ÿ-7*7*#ÿqÿ}*#ÿ.3ÿ$'(ÿ#,ÿ
#,&*(ÿ6(%ÿ&"ÿvd\RwRU[dÿ-7*7*#ÿqÿ}*#ÿ‚.2ÿÿ0&12ÿ
3ÿ/##62
2ÿÿ
·°¸¬§¥¤
±Ä¬¨«
±ÄÿÀĶÿ¤
·°¸¬§¥¤
±Ä¬¤» ±Ä¬¤»
±Ä¬¤»
±Ä¬¤»
±Ä
±Ä
±Ä
±Ä
ÀĶÿ¤ ÀĶÿ§ ÀĶÿ̈ ÀĶÿ«
0123425ÿ0789
19
89
ÿ19
rK> 8 'ÿ#&6ÿ$ÿ7*(ÿqKÿ6(%x"ÿ"#$#%"ÿ !ÿ&"ÿ
'#ÿ&#3ÿ$ÿ%#7%#"ÿ$*ÿ&'ÿ|+$&"$+~ÿ"#$#ÿ-$ÿ*$ÿ
%#7%#"ÿK003ÿ$'(ÿ$ÿK"ÿ$*ÿ$#ÿ$ÿ4#ÿ4.2ÿ
ÿ0&12ÿÿ+*ÿ)$#&'ÿ+ÿ#,ÿqKuzÿ"#$#%"ÿ
!2
$),ÿ#7ÿ&'7%#ÿ*ÿ%#7%#ÿ%"(ÿ*Š%&*"ÿ$ÿ"7)&$ÿr&$1$*$ÿ
!&*)#ÿq'7%#<K%#7%#ÿ-r(&.ÿ7&'#ÿ#ÿ/ÿ$(((ÿ&'ÿ#,ÿ"#$#&'ÿ
($#$/$"2ÿ>,"ÿ)67''#"ÿ$)#ÿ$"ÿ#,ÿ"#$#&'ÿ&'#*+$)ÿ
#ÿ#,ÿ7,"&)$ÿq<Kÿ7&'#"2ÿ>,ÿr(&ÿ7&'#"ÿ'((ÿ+*ÿ
$),ÿ&'7%#ÿ*ÿ%#7%#ÿ#7ÿ$*ÿ'#(ÿ&'ÿ7*4&%"ÿ&*&'1ÿ
")#&'"ÿ&'ÿ]RSd;U†W2
0*ÿr(&ÿ)67''#ÿ(#$&"3ÿ"ÿ#,ÿr(&ÿ‹%&(ÿ&'ÿ
r&$1$*$ÿŒÿ'&'ÿz73ÿ*ÿ#,ÿ"$6ÿ()%6'#ÿ&'ÿ}!02
oFikjÿoÿ?plÿnpnhn?Žÿ
mkmFh
€_ }%1ÿ&'ÿ#,ÿPOÿMÿ)'')#*ÿ7%1ÿ#ÿ$77ÿ7*2ÿ>,ÿ
qKOzÿ/$*(ÿ$'(ÿ"#$#%"ÿ !ÿ&ÿ&'&#&$ÿ/ÿK++ÿ
-0&12ÿ.3ÿ/%#ÿ#,ÿ}*ÿ !ÿ'ÿ#,ÿqKOzÿ",%(ÿ
/ÿ&#2ÿÿ#,ÿ)'#**ÿ"%++&)&'#ÿ#&6ÿ#ÿ/#ÿ-$#ÿ
$"#ÿPÿ6&'%#".2
_ 571*$(ÿ#,ÿ)'#**ÿ+&*6$*ÿ&+ÿ')""$*ÿ-&+ÿ)'
#**ÿ,$"ÿ$ÿr&$1$*$ÿ/%&(ÿ$*&*ÿ#,$'ÿ#,ÿs*{
/'),.2ÿ5"&'1ÿ$ÿs*{/'),3ÿ7'ÿ$ÿ7$#+*6ÿ
)'')#&'ÿ#ÿ#,ÿ)'#**2ÿ5"ÿ#,ÿ‘Ree\‰‰\R=…
\=VÿZ\
’U[dÿ#ÿ(ÿ#,&"2ÿ0*ÿ6*ÿ(#$&"3ÿ"ÿ#,ÿ
“” •ÿr&$1$*$ÿŒÿq'"#$ÿ$'(ÿ#$*#%7ÿ‹%&(3ÿ$"ÿ
$4$&$/ÿ&'ÿ#,ÿs*{/'),ÿ'&'ÿz }ÿ-()ÿ“$)ÿ
#$*#%7.2ÿ–${ÿ"%*ÿ#ÿ&'"#$ÿ#,ÿr(&ÿ"+#$*ÿ
6(%2
‚_ M*&+ÿ#,$#ÿ#,ÿqKOzÿ/$*(ÿ"#$#%"ÿ !ÿ&"ÿ'ÿ&#ÿ
#ÿ1*'2
—_ 5"&'1ÿs*{t'),3ÿ7'ÿ#,ÿ"#$#&'ÿ-&+ÿ*%''&'1.3ÿ*ÿ
7'ÿ$ÿ7$#+*6ÿ)'')#&'ÿ$'(ÿ"#$*#ÿ#,ÿ"#$#&'ÿ
%"&'1ÿ˜TUT\R=ÿ™\[W†TR[2
š_ q+ÿ'#ÿ$*$(ÿ7*"'#3ÿ$((ÿ$'ÿr(&r#*{ÿ)67
''#ÿ#ÿ#,ÿ"#$#&'x"ÿ!*&4*"ÿ”'#$&'*ÿ$'(ÿ%"ÿ
|–$'$1*~ÿ4&"ÿ$'(ÿ|$*'ÿ–(~ÿ#ÿ(&")4*ÿ$'(ÿ
$((ÿr(&ÿ)67''#"ÿ#ÿ#,ÿ"#$#&'ÿ($#$/$"2ÿÿ
K0>s› ÿ! ”›q}>qKrÿ")#&'2ÿ0*ÿ6*ÿ
(#$&"ÿ$/%#ÿr(&ÿ)67''#"3ÿ*+*ÿ#ÿ#,ÿr(&ÿ
‹%&(3ÿ$"ÿ$4$&$/ÿ&'ÿs*{/'),ÿ'&'ÿz7ÿ
-()ÿr(&.2
jkŽ?hklÿlFmœkph?hnFp
0*ÿ6*ÿ&'+*6$#&'ÿ'ÿ)'+&1%*&'1ÿ$'(ÿ%"&'1ÿs tPÿ
"*&"ÿ)'#**"3ÿ)'"%#ÿ#,ÿ+&'1ÿ()%6'#"8
9 s tPÿq'"#$$#&'ÿq'"#*%)#&'"2
9 “” ÿr&$1$*$ÿŒÿq'"#$ÿ$'(ÿ#$*#%7ÿ‹%&(
9 r&$1$*$ÿŒÿr(&ÿ‹%&(
9 r&$1$*$ÿŒÿ5"*ÿ‹%&(
9 qKuzÿq'"#$$#&'ÿq'"#*%)#&'"
p>ÿ*žÿ
jIBAŸ @Hÿ@¡HJ
7$)ÿ$ÿ+$%#ÿ%'&#3ÿ*(*ÿ$'(ÿ&'"#$ÿ$ÿ'ÿqKOzÿ
$))""*ÿ6(%2
^\V_ÿ€ƒ_ÿZ„w…ƒ€ÿ†R=T[RSSW[ÿvd\RwRU[dÿ‡YR[Tˆÿ rK> 8 s tPÿ*ÿs tuÿ"*&"ÿ7*(%)#"ÿ(ÿ'#ÿ
U‰‰\V=eW=T_
,$4ÿ"7)&$ÿ|+&(ÿ*7$)6'#ÿ%'&#"~3ÿ*ÿ0›5x"3ÿ
&#,ÿ"7$*$#ÿ7$*#ÿ'%6/*"2
K')ÿ#,ÿ7*$#&'1ÿ""#6ÿ&('#&+&"ÿ#,ÿr!qKÿ
7*)""*"3ÿ#,ÿq<Kÿ/$*(ÿ"#$#%"ÿ !ÿ'ÿ$),ÿqKÿ6(%ÿ
#%*'"ÿ1*'2ÿ>,ÿ1*'ÿ"#$#%"ÿ !ÿ6$'"ÿ#,$#ÿ#,ÿ
q+ÿ#,ÿ+$%#ÿqKOzÿ6(%ÿ&"ÿ"#&ÿ&'ÿ$**$'#ÿ)*(&#ÿ6$ÿ
)'#**ÿ&"ÿ$/ÿ#ÿ)66%'&)$#ÿ&#,ÿ#,ÿq<K2ÿq#ÿ("ÿ'#ÿ /ÿ*)&4(ÿ/ÿ*#%*'&'1ÿ&#ÿ#ÿz'2ÿtÿ"%*ÿ#ÿ
&'(&)$#ÿ$'#,&'1ÿ$/%#ÿ#,ÿ"#$#%"ÿ+ÿ#,ÿr&$1$*$ÿ"#$#&'ÿ )'#$)#ÿz'ÿ+*ÿ$ÿ*#%*'ÿ$%#,*&¢$#&'ÿ-›.ÿ'%6/*ÿ
*ÿ&#"ÿr(&ÿ)67''#"2
/+*ÿ",&77&'1ÿ$'ÿ&#6ÿ+*ÿ*#%*'ÿ)*(&#2ÿÿ
› >5›rqr‹ÿÿ! 0 ”>qM ÿ5rq>ÿ")#&'ÿ+*ÿ(#$&"2
©§¨§ª§
0123425ÿ0789
19
89
ÿ19
<GLTU V"W)"ÿ)0")+!9ÿ*ÿ!"$ÿ'G1>C1ÿ/ 08%"Aÿ+(ÿ+:ÿ
:()!9%#ÿ)", //"!0"0ÿ(=*(ÿ! )/*%ÿ(",=!+,*%ÿ
:8XX )(ÿ)":8),"ÿF"ÿ8:"0ÿ(ÿ"%+/+!*("ÿ(="ÿX ::+1
F+%+(#ÿWÿ*ÿ:W($*)"ÿ+::8"ÿ)ÿ
/+:1, !W+98)*(+!ÿX)F%"/-
YZ[\]^\Z\_^
Y`abcdÿfdgchidjdkl
mno
pq
rstsÿuvÿwwÿxyÿwuvsÿzÿ
wwsÿwÿxzÿwuvÿusÿsxzÿ
suÿvvÿ{|ÿ}ÿsyÿssÿwÿ
~wuvsÿswÿsw|
L ÿ)"X%*,"ÿ(="ÿ'G1>C1ÿ*,,"::)#ÿ/ 08%"ÿ+!ÿ(="ÿW+"%0Aÿ
X),""0ÿ*:ÿW%%$:U
wssÿ€|ÿwwszÿsÿ‚s{wss|
s{ÿ’ J:+!9ÿ(="ÿ*XX)X)+*("ÿ<+*9*)*ÿ: W($*)"ÿ( %AÿF*,Mÿ8Xÿ(="ÿ, !()%%")ÿ,!W+98)*(+!ÿ(ÿ# 8)ÿŒ“s{ÿ€ K"/ ;"ÿX $")ÿ(ÿ(="ÿ'G1>C1ÿ, !()%%")-ÿL="ÿ8!+(ÿ:= 8%0ÿX $")ÿ0 $!ÿ*8(/*(+,*%%#s{ÿ” K",)0ÿX :+(+!:ÿWÿ*%%ÿ'•Gÿ$+)+!9ÿ9 +!9ÿ(ÿ(="ÿ'G1>C1-ÿ'Wÿ!","::*)#Aÿ%*F"%ÿ, !!",():ÿ(ÿ*;+0ÿ
/+:1, !!",(+!ÿ%*(")ÿŽ*W(")ÿ'G1>C1ÿ/ 08%"ÿ+:ÿ)"X%*,"0<GLTU L="ÿ: W($*)"ÿ(=*(ÿ)8!:ÿ!ÿ(="ÿŠTV1DO3ÿ, !()%%")ÿ"–X",(:ÿ(="ÿ(")/+!*%ÿX :+(+!:ÿ(ÿF"ÿ(="ÿ:*/"ÿ+!ÿ
(="ÿ)"X%*,"/"!(ÿ'G1>C1ÿ/ 08%"Aÿ+!ÿ)0")ÿ(ÿ, %%",(ÿ0*(*ÿW)/ÿ)ÿ(ÿ, !()%ÿ(="ÿ*((*,="0ÿ0";+,":s{ÿ— 'Wÿ*!#ÿ'•GÿX +!(:ÿ=*;"ÿ;%(*9"Aÿ(8)!ÿ(="ÿ0";+,":ÿWWAÿ)ÿ0+:, !!",(ÿX $")ÿ(ÿ(="/s{ÿ˜ J!X%89ÿ*%%ÿ, !!",():ÿW)/ÿ(="ÿ'G1>C1ÿ/ 08%"Aÿ+!,%80+!9ÿ*%%ÿ'•Gÿ, !!",():ÿ*!0ÿ"*)(=ÿ9)8!0ÿ$+)"s{ÿ™ K"/ ;"ÿ*!#ÿ:,)"$:ÿ)ÿ7'<ÿ)*+%ÿ,%+X:ÿ:",8)+!9ÿ(="ÿ'G1>C1ÿ/ 08%"Aÿ)"/ ;+!9ÿ+(ÿW)/ÿ+(:ÿ/ 8!(+!9s{ÿš B 8!(ÿ(="ÿ)"X%*,"/"!(ÿ'G1>C1ÿ/ 08%"ÿ*:ÿ+(ÿ$*:ÿX)";+8:%#Aÿ8:+!9ÿ(="ÿ:*/"ÿ7'<ÿ)*+%ÿ%,*(+!ÿ*!0•)ÿ:,)"$:s{ÿ› K",!!",(ÿ(="ÿ"*)(=ÿ9)8!0ÿ$+)"ÿ(ÿ(="ÿ9)8!0+!9ÿ%89s{ÿœ K",!!",(ÿ*%%ÿ'•Gÿ, !!",():ÿ(ÿ(="ÿ'G1>C1ÿ/ 08%"s{ÿ’'Wÿ*!#ÿWÿ# 8)ÿ'•GÿX +!(:ÿ=*;"ÿ; %(*9"Aÿ(8)!ÿ(="ÿ0";+,":ÿF*,Mÿ!Aÿ)ÿ)", !!",(ÿX $")ÿ(ÿ(="/s{ÿ’’K":()"ÿX $")ÿ(ÿ(="ÿ'G1>C1ÿ/ 08%"ÿ*!0ÿX")W)/ÿ*ÿ,=",M8(ÿ8:+!9ÿ<+*9*)*ÿžÿŠ )MF"!,=ÿŽ:""ÿŒGŠTKÿ
JŒÿ<7ÿ'<'L'.ÿ“T“ŸGJLÿ:",(+!s{ÿ’€‹ )ÿ/ )"ÿ0"(*+%:Aÿ:""ÿ(="ÿ<+*9*)*ÿžÿ<0+ÿ?8+0"ÿ*!0ÿS“Tÿ<+*9*)*ÿžÿ'!:(*%%ÿ*!0ÿE(*)(8Xÿ?8+0"‹ )ÿX)X")ÿ,)"0+(ÿ!ÿ*!ÿ+!1$*))*!(#ÿ8!+(Aÿ:=+Xÿ(="ÿ0"W",(+;"ÿ
8!+(ÿ(ÿ !"#$"%%ÿ$+(=+!ÿ>Oÿ0*#:<GLTEU'Wÿ(="ÿ0"W",(+;"ÿ8!+(ÿ+:ÿ8!0")ÿ$*))*!(#AÿW%%$ÿ Œ)+)ÿ(ÿ)"(8)!+!9ÿ(="ÿ8!+(Aÿ,!(*,(ÿ!"ÿWÿ(="ÿ !"#$"%%ÿ
)"(8)!ÿ+!:()8,(+!:ÿX);+0"0ÿ+!ÿ(=+:ÿ:",(+!-ÿ'Wÿ(="ÿ WW+,":ÿ(ÿF(*+!ÿ*ÿ)"(8)!ÿ*8(= )+*(+!ÿŽKÿ!8/F")ÿ*!0ÿ
8!+(ÿ+:ÿ8(ÿWÿ$*))*!(#Aÿ0+:,*)0ÿ(="ÿ8!+((=")ÿ+!:()8,(+!:-ÿE""ÿ%*:(ÿX*9"ÿWÿ0 ,8/"!(ÿW)ÿ
R 7 ÿ! (ÿ)"(8)!ÿ*!ÿ8(1W1$*))*!(#ÿ'G1>C1ÿ !"#$"%%ÿ,!(*,(ÿ+!W)/*(+!-ÿŒ%"*:"ÿX);+0"U
/ 08%"ÿ(ÿ !"#$"%%Œ)08,(ÿ/ 0"%
R L=")"ÿ+:ÿ! ÿˆ)"(8)!ÿW)ÿ)"X*+)1*!01)"(8)!‰ÿ:")1 ‘‘ E"
+*%ÿ!8/F")
;+,"ÿ*;*+%*F%"ÿW)ÿ*!#ÿWÿ(="ÿŠTV1DO3ÿ)ÿ ‘ <8)/F
")ÿWÿ(="ÿ0"W",(
ŠTV1POOÿ:")+":ÿX)08,(:‘ <*(8)"ÿWÿ0"W",(
f^]ƒf\[\„ÿZÿ…^†^_][‡^ÿƒ\[]
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

Similar documents