916 NE 96 St (8)Engineering
File / Jobname: ODEJUL14
Keymark Engineering
Truss Calculations
Cover Letter
Software Version Number: 3.305
Company: DECON WORLD WIDE, INC. Date: 7/17/98 (U.N.O $080y
Page - Truss Truss Date Notes Page - Truss Truss Da%
1 — Gen.Notes ❑ 26- ,
2 — Gen.Notes ❑ 27-
3 — G01_20 ❑ 28-
4 — G02_20 ❑ 29-
5 — J01_20 ❑ 30-
6 — J02_20 ❑ 31-
7 — J03_20 ❑ 32-
8— T01_20 ❑ 33-
9 — T02_20 ❑ 34-
10- T03_20 ❑ 35-
11- T04_20 ❑ 36-
12- TO5_20 ❑ 37-
13- T06_20 ❑ 38-
14- T07_20 ❑ 39-
15- Detail DJ01 ❑ 40-
16- Detail DJ02 ❑ 41-
17- Detail DJ03 ❑ 42-
18- ❑ 43-
19- ❑ 44-
20- ❑ 45-
21- ❑ 46-
22- ❑ 47-
23- ❑ 48-
24- ❑ 49-
25- ❑ 50-
2905 Wilderness Place, Suite 202 !Boulder, Colorado 80301 1 303 - 443 -80331 FAX 303 - 443 -2196
1. COi- DESIGN
This design is Wan individual building component and has been based on information provided by the client. The truss designer disclaims any responsibility for
damages as a result of faulty or incorrect information, specifications, and/or designs furnished to the truss designer by the client and the correctness or accuracy of this
information as it may relate to a specific project. The truss designer accepts no responsibility and exercises no control with regard to fabrication, handling, shipment, and
installation of trusses. The truss has been designed as an individual building component in accordance with the AISI Truss Design Guide and the AISI Cold Formed Steel
Design Manual. This component shall be incorporated as part of the building design by a Building Designer (registered architect or professional engineer, as applicable).
The Building Designer shall review the design loading, truss geometry, and all other aspects of the component design shown ':o ensure that the data shown are in
agreement with the local building codes, local climatic records for snow or wind loads, project specifications, or special applied loads.
2. FABRICATION NOTES
Prior to fabrication, the fabricator shall review this drawing to verify that this drawing is in conformance with the fabricator's plans and to realize a continuing
responsibility for such verification. Fabrication of trusses shall not proceed until the fabricator has certified drawings in hand.
3. PRECAUTIONARY NOTES
Trusses are to be handled with particular care during banding, bundling, and delivery and installation to avoid damage. Temporary and permanent bracing for holding
trusses in a straight and plumb position and for resisting lateral forces shall be designed and installed by others. Careful handling is essential and erection bracing is
always required. Normal precautionary action for trusses requires such temporary bracing during installation between trusses to avoid toppling and dominoing. The
supervision of erection of trusses shall be under the control of persons experienced in the installation of trusses. Professional advice shall be sought if needed.
Concentration of construction loads greater than the design loads shall not be applied to the trusses at any time. No loads other than the weight of the erectors shall be
applied to trusses until after all fastening and bracing is completed.
CEE SHAPES
4. MATERIAL AND MEMBER SPECIFICATION
20 and 18 gage chords and webs, and track shall conform to ASTM A 653 SQ Grade 33 (minimum Fy = 33 KSI).
16, 14, and 12 gage chords and webs, and track shall conform to ASTM A 653 SQ Grade 50 (minimum Fy = 50 KSI). All "CEE" shapes shall have 1 5/8 inch, 2 inch,
or 2'A" flanges. Lips for the 1 5/8 inch flange shall be 'A inch. Lips for 2 inch and 2'A inch flange widths shall be 5/8 inch.
All material shall be galvanized with a minimum of 060 coating . Prepunched holes in the "CEE" members are prohibited.
Material design thickness shall be as follows:
22 gage: .0283 inch
20 gage: .0346 inch
18 gage: .0451 inch
16 gage: .0566 inch
"CEE" Shape Definition:
FLANGE
14 gage: .0713 inch
12 gage: .1017 inch
10 gage: .1242 inch
UP
MEMBER DESIGNATION KEY
Top chord, bottom chord, and web shall be "CEE" shapes, with designations as follows:
SNNN -YY ZZZZ
S - Designates "CEE" shape
NNN- Designates flange width, measured in hundredths of an inch (158, 200, or 250)
YY- Designates minimum delivered thickness of base steel in thousandths of an inch
ZZZZ - Designates depth of "CEE" , measured in hundredths of an inch
Minimum delivered thickness of base metal shall be as follows:
22 gage: .027 inch
20 gage: 0.033 inch 14 gage: 0.068 inch
18 gage: 0.043 inch 12 gage: 0.097 inch
16 gage: 0.054 inch 10 gage: 0.118 inch
5. BRACING NOTES
The bracing conditions for the top and bottom chords are stated on the face of the drawing, and the bracing shall be installed exactly where shown.
CHORD BRACING WITH PURLIN
When "PURLIN" are called for, the chord shall be braced laterally and against twisting at an on center spacing no greater than the purlin spacing indicated.
SPARSE CHORD BRACING
When the bracing is called "SPARSE ", the chord shall be braced laterally at each panel point that sees chord compression in any load case. If a series of panel points see
only tension, then altemate panel point may be braced provided that the distance between two braces does not exceed 120 inches. Braces at panel points shall be installed
within 6 inches of the panel point, attached to either the chord or a web.
Chord braces shall be so installed as to prevent lateral displacement of all of the trusses as a unit. Each bearing point shall be designed to provide lateral support for the
truss perpendicular to the plane of the truss. Bracing shown on this drawing is not erection bracing, wind bracing, portal bracing, or similar bracing which is part of the
building design and which shall be considered by the Building Designer. Bracing shown is for the lateral support of truss members only to reduce buckling length of the
individual truss member. The design of the individual truss member brace and the anchorage of the brace shall be considered by the building designer. Additional
bracing of the overall structure may be required. For specific truss bracing requirements, contact the Building designer.
Special Bracing Requirement for Out of Plane "CEE" Truss:
Provide permanent positive lateral brace for the top chord at bearing points to prevent twisting of the truss under load at the bearing
points.
6. SPLICES
No splicing of truss members shall be permitted without a certified splicing detail for the specific truss showing the exact method and location of splicing.
7. MODIFICATION OF TRUSS MEMBERS u,
No truss member shall be cut or otherwise modified without the specific written permission of the Truss Designer.
8. TRUSS TO TRUSS CONNECTION DESIGN
Truss to truss connection design is not provided with this component truss design.
`a..
9. TRUSS TO STRUCTURE CONNECTION DESIGN
The design of connections between the truss component and other elements of the overall structure is not provided with this component truss design.
10. FASTENER DESIGN INFORMATION
Fasteners shall be either #l0, #12, or'' /." self drilling screws (SDS), as noted on the face of the drawing, and shall be installed in accordance with the AISI design
recommendations. Each fastener shall be installed with a minimum spacing as listed on the face of the drawing, and a minimum edge margin as listed on the face o
drawing. Note that the screw shall penetrate the last ply in the connection, including gussets as applicable, and at least three threads shall be visible beyond the last ply.
11. PONDING WARNING
This truss has not been investigated for the effects of ponding. The Building Designer shall ensure that adequate drainage has been provided, and that the roof system as a
whole is not susceptible to ponding.
N ?"
12. POINT LOADS
Point loads other than those specifically shown on the truss design drawings shall be limited to 140 pounds, and shall not be located closer together along a chord
member than 4 feet. Do not attach any point load to the truss webs. Any such point load shall be attached in such a way as to minimize twisting of the chord. Any such
point load shall be attached as close as possible to a chord panel point. Such miscellaneous point loads are not additional allowed loading on the truss, and instead shall
be accounted for as part of the Dead or Live design loads shown on the Truss Design Drawing. Point loads larger than those described above shall require the specific
written permission of the truss designer.
13. TYPICAL WEB TO CHORD CONNECTION
At all panel points where more than one web is attached to a chord, the two webs shall be either touching or separated by no more than '/. inch. All webs shall be installed
in such a fashion that some portion of the web extends to within 3/8" of the outer profile of the truss. All webs shall be square cut at their ends, unless noted otherwise.
14, TYPICAL GUSSET PLATE REQUIREMENTS
When gusset plates are called for on the face of the drawings, the dimensions of the gusset plates shall as a minimum be as required to accommodate all of the required
fasteners at each joint, with due regard for fastener edge margin and spacing. The dimensions listed in the gusset plate schedule shall be used only if all fasteners can be
placed with due regard for fastener edge margin and spacing. If a gusset design requires a re- entrant comer, the radius of the fillet shall be a minimum of 3/16'. Any
joint which cannot accommodate the correct number of fasteners with due regard to fastener edge margin and spacing shall receive a gusset plate whether a gusset plate is
called for on the face of the drawing or not. If the installer cannot install the fasteners with due regard for fastener edge margin and spacing at a specific joint, he shall
contact the truss designer for clarification before proceeding with truss fabrication.
15. HORIZONTAL TRUSS DEFLECTION
The building designer shall consider the effects of horizontal deflection of the truss on the entire structure. The building designer shall either design the truss to structure
connection to allow the truss to move horizontally at one support, or design the truss to structure connection and the entire structure to resist the horizontal thrust resulting
from a restrained bearing condition. All restrained bearing conditions shall be reported to the truss designer to allow for proper analysis of the truss for this condition.
16. DEFINITION OF LOADS
The truss is designed solely for the design loadings explicitly listed on the design drawing. "Standard Loadings" and "Distributed Loadings" are in pounds per square
foot. "Standard Loading" is applied to the entire chord, unless replaced by a "Distributed Load ". The self weight of the truss is' mot automatically considered, and shall
instead be included by the user in the dead loading applied to the truss. Wind load is not automatically considered.
Under standard loading, the load direction is always vertical. Distributed loads REPLACE standard loading for the members noted, and are NOT additive to standard
loading. Distributed live loads may be either vertical, horizontal, or normal to the member. Distributed dead loads are always oriented vertically.
GUSSET PLATES
Joint#
Gauge
Size
77
Refer to Attachment A
for Gusset Plate Usage
KEYemart ■
Ver 3.305
DECON WORLD WIDE, INC.
2652 NW 31st Avenue
Ft. Lauderdale, FL 33311
(954) 485 -8800 FAX: (954) 485 -8809
JOB NAME SPAN PITCH QTY OHL OHR PLYS SPACING
ODEJUL14 \G01_20 8 -4 -13 2.1209 2 2 -9 -15 0 -0 -0 1 1 -0 -0
Material
T/C to be: S162 -68 6.
B/C to be: S162 -33 3.625
Webs to be: S162 -43 3.625
CSI
0 -7 -8
0 -i-0
2 -9 -10
2 -9 -10
2 -9 -10
2 -9 -10
Material CSI P #Screws Brc
1- 2 TCHORD S162-68 6. .85 -822 2
2- 3 TCHORD S162 -68 6. .04 -124 2
3- 4 TCHORD S162-68 6. .03 -22 2
5- 6 BCHORD S162 -33 3.625 .15 107 2
6- 7 BCHORD S162 -33 3.625 .35 824 4
7- 8 BCHORD S162 -33 3.625 .24 -170 2
1- 8 WEB S162 -43 3.625 .21 1421 6
1- 7 WEB S162 -43 3.625 .15 998 6
2- 7 WEB S162 -43 3.625 .04 287 2
2- 6 WEB S162-43 3.625 .18 -788 4
3- 6 WEB S162 -43 3.625 .04 261 2
3- 5 WEB 5162 -43 3.625 .03 -116 2
4- 5 WEB S162 -43 3.625 .02 112 2
9- 1 TCHORD S162 -68 6. .80 -105 2
"8 SCREWS" Indicates the number of 810 screws at the end of the
member. Screw counts indicated at interior points of continuous
members shall be neglected. Allowable shear per screw as follows:
22 GA:1661b8; 20 GA:2401bs; 18 GA:2631bs; 16 GA:3701bs; 14 GA:
4671b8; 12 GA:4671bs; 10 GA:4671bs. Maintain screw spacing at
9/16" min. Maintain edge margin at 9/16 "min.
1 -1 -7
0 - ? -0
5 -7 -3
2 -9 -10
2 -9 -10
5 -7 -3
1 -7 -6
0 - p - 0
8 -4 -13
2 -9 -10
2 -9 -10
8 -4 -13
2 -1 -5
4
0 - p - 0
Deflection (loc)
TC .85 Vert LL .03" L/999 7
BC .35 Horz TL .00" 5
WB TC CONTINUOUSLY SHEATHED
BC CONTINUOUSLY SHEATHED Design Loadings
Reactions SUMMARY LOAD CASE 1
JT TYPE LC BRG WID REACT JT MAX REACT MAX UPLIFT TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
8 P 1 6.000 894. 8 894. -1386. 0 0 0 0
5 R 1 2.000 151. 5 151. -91. JT DIR LIVE DEAD POINT LOADS
9 Vert 240.0 200.0
8 P 2 6.000 171.H SECTION DIR LIVE DEAD DISTRIBUTED LOADS
8 P 2 6.000 -1386. 5- 6 Vert 40.8 29.9
5 R 2 2.000 -91. 6- 7 Vert 45.6 25.5
8 P 3 6.000 42. 7- 8 Vert 39.9 34.3
5 R 3 2.000 42. Note:Distributed Loads Replace Standard Loads
LOAD CASE 2
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
.0 .0 .0 .0
JT DIR LIVE :BEAD POINT LOADS
9 Vert -688.0 80.0
SECTION DIR LIVE DEAD DISTRIBUTED LOADS
1- 4 Norm -86.1 5.0
5- 8 Vert .0 5.0
9- 1 Norm -86.1 5.0
Note:Distributed Load: Replace Standard Loads
LOAD CASE 3
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
.0 .0 10.0 .0
7/17/98
1:47pm
Page 1 of 1
ALL GENERAL NOTES FOUND ON PAGES 1 AND 2 OF THIS DRAWING PACKAGE SHALL BE CONSIDERED AS AN INTEGRAL PART OF THIS COMPONENT DESIGN DOCUM
NOTE THAT THE PROFESSIONAL ENGINEER'S SEAL INDICATES ONLY THAT THE TRUSS ASSEMBLY SHOWN ON THIS SHEET MEETS THE MINIMUM APPLICABLE DESIGN
CRITERIA FOR THE LOADS, LOADING CONDITIONS, TRUSS MEMBER CONFIGURATIONS, AND SPANS LISTED ON THIS SHEET.
GUSSET PLATES
Joint#
Gauge
Size
//
Refer to Attachment A
for Gusset Plate Usage
KEYemart
Ver 3.305
JOB NAME
ODEJUL14 \G02 20
0 -7 -8
01-0
12
3 -0 -0
3 -0 -0
3 -0 -0
3 -0 -0
14 P 2 6.000 -1117.
8 R 2 6.000 -1117.
14 P 3 6.000 410.
8 R 3 6.000 410.
Material
T/C to be: S162 -54 3.625
B/C to be: 5162 -54 3.625
Webs to be: 5162 -33 3.625
Material
1- 2 TCHORD S162 -54
2- 3 TCHORD S162-54
3- 4 TCHORD S162 -54
4- 5 TCHORD S162-54
5- 6 TCHORD S162 -54
6- 7 TCHORD S162 -54
8- 9 BCHORD 5162 -54
9 -10 BCHORD S162 -54
10 -11 BCHORD S162 -54
11 -12 BCHORD S162 -54
12 -13 BCHORD S162 -54
13 -14 BCHORD S162 -54
1 -14 WEB S162 -33
1 -13 WEB S162 -33
2 -13 WEB S162 -33
2 -12 WEB S162 -33
3 -12 WEB S162 -33
3 -11 WEB S162 -33
4 -11 WEB S162 -33
5 -11 WEB S162 -33
5 -10 WEB 5162 -33
6 -10 WEB S162 -33
6- 9 WEB 5162 -33
7- 9 WEB 5162 -33
7- 8 WEB 5162 -33
15- 1 TCHORD S162 -54
16- 7 TCHORD S162 -54
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
0 -p -0
CSI
BC .53
WB .72
.64
.75
.69
.69
.75
.64
.23
.53
.49
.49
.53
.23
.54
.72
.15
.14
.08
.11
.06
.12
.08
.14
.15
.72
.54
.20
.20
DECON WORLD WIDE, INC.
2652 NW 31st Avenue
Ft. Lauderdale, FL 33311
(954) 485 -8800 FAX: (954) 485 -8809
SPAN PITCH QTY OHL OHR
17 -6 -0 3.0000 1 2 -0 -0 2 -0 -0
1
-3858
-4512
-4849
-4849
-4501
-3852
0
3676
4349
4360
3682
0
-1748
3703
-495
719
418
586
322
599
419
715
-495
3696
-1748
43
43
6 -0 -0
3 -0 -0
1 -4 -8 2 -1 -8
13 12
3 -1 -13
6 -1 -13
12
14
14
14
14
12
2
10
12
12
10
2
8
16
4
4
2
4
2
4
2
4
4
16
8
2
2
0 - ? -0
8 -9 -0
2 -9 -0
1NV,t"
3 V �wvJ 2 I •. - 41111121....
..i%1■_"
.00-101. •
. _ - -
It! ,
2 -7 -3
TC CONTINUOUSLY SHEATHED
BC CONTINUOUSLY SHEATHED
Reactions SUMMARY
JT TYPE LC BRG WID REACT JT MAX REACT MAX UPLIFT
14 P 1 6.000 1856. 14 1856. -1117.
8 R 1 6.000 1856. 8 1856. -1117.
CSI P #Screws Brc
11 -6 -0
2 -9 -0
1 1
2 -1 -8 2 -1 -8
4
11
0 - ? - 0
2 -7 -3
8 -9 -0 11 -4 -3
Deflection
Vert TL .27"
Horz TL .05"
10
0-0 -0
14 -6 -0
JT DIR
12 Vert
10 Vert
1 -0 -0
3 -1 -13
14 -6 -0
(loc)
L/776 1 -12
SECTION DIR
8 -10 Vert
10 -12 Vert
12 -14 Vert
Note:Distributed
LOAD CASE 2
TOP LL TOP DL
60.0 30.0
PLYS
1
1-4-8
9
0 -? -0
17 -6 -0
1 -0 -0
1
3 -0 -0
17 -6 -0
SPACING
1 -0 -0
0 -7 -8
12
0 -p -0
Design Loadings
LOAD CASE 1
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
60.0 30.0 .0 .0
LIVE DEAD POINT LOADS
175.3 :.20.7
175.3 :.20.7
LIVE DEAD DISTRIBUTED LOADS
.0 20.0
85.0 86.7
.0 20.0
Loader Replace Standard Loads
BOT LL BOT DL STANDARD LOADING
.0 .0
SECTION DIR LIVE: DEAD DISTRIBUTED LOADS
1- 7 Norm -113.0 5.0
8 -14 Vert .0 5.0
15- 1 Norm -113.0 5.0
7 -16 Norm -113.0 5.0
Note:Distributed Loads Replace Standard Loads
LOAD CASE 3
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
.0 30.0 1C.0 .0
"11 SCREWS" Indicates the number of It10 screws at the end of the
member. Screw counts indicated at interior points of continuous
members shall be neglected. Allowable shear per screw as follows:
22 GA:1661bs; 20 GA:2401bs; 18 GA:2631bs; 16 GA:3701be; 14 GA:
4671bs; 12 GA:4671bs; 10 GA:4671bs. Maintain screw spacing at
9/16" min. Maintain edge margin at 9/16 "min.
7/17/98
1:48pm
Page 1 of 1
N'%z
ALL GENERAL NOTES FOUND ON PAGES 1 AND 2 OF THIS DRAWING PACKAGE SHALL BE CONSIDERED AS AN INTEGRAL PART OF THIS COMPONENT DESIGN DOCUME
NOTE THAT THE PROFESSIONAL ENGINEER'S SEAL INDICATES ONLY THAT THE TRUSS ASSEMBLY SHOWN ON THIS SHEET METTS THE MINIMUM APPLICABLE DESIGN
CRITERIA FOR THE LOADS, LOADING CONDITIONS, TRUSS MEMBER CONFIGURATIONS, AND SPANS LISTED ON THIS SHEET.
GUSSET PLATES
Joint#
Gauge
Size
//
Refer to Attachment A
for Gusset Plate Usage
KEYsmart
Ver 3.305
JOB NAME SPAN PITCH QTY OHL OHR PLYS SPACING
ODEJUL14 \J01_20 1 -10 -9 3.0032 4 2 -0 -0 0 -0 -0 1 2 -0 -0
Reactions
CSI
SUMMARY
JT TYPE LC BRG WID REACT JT MAX REACT MAX UPLIFT
4 P 1 6.000 833. 4 833. -1240.
3 R 1 2.000 -226. 3 325. -226.
4 P 2 6.000 167.H
4 P 2 6.000 -1240.
3 R 2 2.000 325.
4 P 3 6.000 158.
3 R 3 2.000 34.
Material
T/C to be: S162 -54 3.625
B/C to be: S162 -33 3.625
Webs to be: S162 -33 3.625
Material CSI P #Screws Brc
1- 2 TCHORD S162 -54 3.625 .85 -100 2
3- 4 BCHORD S162 -33 3.625 .06 -167 2
1- 4 WEB S162 -33 3.625 .25 1249 6
1- 3 WEB S162 -33 3.625 .03 169 2
2- 3 WEB S162 -33 3.625 .11 -344 2
5- 1 TCHORD S162 -54 3.625 .85 97 2
"H SCREWS" Indicates the number of U10 screws at the end of the
member. Screw counts indicated at interior points of continuous
members shall be neglected. Allowable shear per screw as follows:
22 GA:1661bs; 20 GA:2401bs; 18 GA:2631bs; 16 GA:3701bs; 14 GA:
4671bs; 12 GA:4671bs; 10 GA:4671bs. Maintain screw spacing at
9/16" min. Maintain edge margin at 9/16 "min.
DECON WORLD WIDE, INC.
2652 NW 31st Avenue
Ft. Lauderdale, FL 33311
(954) 485 -8800 FAX: (954) 485 -8809
0 -7 -8
0 -0-
1 -10 -9
1 -10 -9
1 -10 -9
1 -10 -9
Deflection (loc)
TC .85 Vert TL .00" L/999 3 -4
BC .05 Horz TL .00" 3
WB TC CONTINUOUSLY SHEATHED
BC CONTINUOUSLY SHEATHED
0 -0 -0
Design Loadings
LOAD CASE 1
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
JT DIR LIVE DEAD POINT LOADS
5 Vert 120.0 7.00.0
LOAD CASE 2
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
JT DIR LIVE DEAD POINT LOADS
5 Vert -344.0 40.0
SECTION DIR LIVE DEAD DISTRIBUTED LOADS
1- 2 Norm -86.1 5.0
3- 4 Vert .0 5.0
5- 1 Norm -86.1 5.0
Note:Distributed Loads Replace Standard Loads
LOAD CASE 3
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
.0 15.0 10.0 10.0
V
7/17/98
1:47pm
Page 1 of 1
ALL GENERAL NOTES FOUND ON PAGES 1 AND 2 OF THIS DRAWING PACKAGE SHALL BE CONSIDERED AS AN INTEGRAL PART OP THIS COMPONENT DESIGN DOCUMENT
NOTE THAT THE PROFESSIONAL ENGINEER'S SEAL INDICATES ONLY THAT THE TRUSS ASSEMBLY SHOWN ON THIS SHEET MEETS THE MINIMUM APPLICABLE DESIGN
CRITERIA FOR THE LOADS, LOADING CONDITIONS, TRUSS MEMBER CONFIGURATIONS, AND SPANS LISTED ON THIS SHEET.
GUSSET PLATES
Joint#
Gauge
Size
Refer to Attachment A
for Gusset Plate Usage
KEYsmart
Ver 3.305
DECON WORLD WIDE, INC.
2652 NW 31st Avenue
Ft. Lauderdale, FL 33311
(954) 485 -8800 FAX: (954) 485 -8809
JOB NAME SPAN PITCH QTY OHL OHR PLYS SPACING
ODEJUL14 \J02_20 3 -10 -9 3.0015 4 2 -0 -0 0 -0 -0 1 2 -0 -0
Reactions
4 P 3 6.000 211.
3 R 3 2.000 120.
Material
T/C to be: S162 -43 3.625
B/C to be: S162-33 3.625
Webs to be: S162-33 3.625
1
0 -7 -8
CSI Deflection (loc)
TC .71 Vert TL .01" L/999 3 -4
BC .10 Ho rz TL .00"
TC CONTINUOUSLY SHEATHED
BC CONTINUOUSLY SHEATHED
SUMMARY
JT TYPE LC BRG WID REACT JT MAX REACT MAX UPLIFT
4 P 1 6.000 440. 4 440. -667.
3 R 1 2.000 167. 3 167. -248.
4 P 2 6.000 253.H
4 P 2 6.000 -667.
3 R 2 2.000 -248.
Material CSI P #Screws Brc
1- 2 TCHORD S162 -43 3.625 .71 -69 2
3- 4 BCHORD S162 -33 3.625 .20 -253 2
1- 4 WEB S162 -33 3.625 .13 686 4
1- 3 WEB S162 -33 3.625 .05 254 2
2- 3 WEB 5162 -33 3.625 .05 246 2
5- 1 TCHORD S162 -43 3.625 .55 43 2
"8 SCREWS" Indicates the number of 810 screws at the end of the
member. Screw counts indicated at interior points of continuous
members shall be neglected. Allowable shear per screw as follows:
22 GA:1661bs; 20 GA:2401bs; 18 GA:2631bs; 16 GA:3701bs; 14 GA:
4671bs; 12 GA:4671bs; 10 GA:4671bs. Maintain screw spacing at
9/16" min. Maintain edge margin at 9/16 "min.
3 -10 -9
1 -10 -9
3
0- 0 - 0
3 -10 -9
3 -10 -9
Design Loadings
LOAD CASE 1
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
LOAD CASE 2
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
SECTION DIR LIVE DEAD DISTRIBUTED LOADS
1- 2 Norm -86.1 5.0
3- 4 Vert .0 5.0
5- 1 Norm -86.1 5.0
Note:Distributed Loads Replace Standard Loads
LOAD CASE 3
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
.0 15.0 10.0 10.0
1 -7 -2
2
7/17/98
1:47pm
Page 1 of 1
ALL GENERAL NOTES FOUND ON PAGES 1 AND 2 OF THIS DRAWING PACKAGE SHALL BE CONSIDERED AS AN INTEGRAL PART OF THIS COMPONENT DESIGN DOCUMENT
NOTE THAT THE PROFESSIONAL ENGINEER'S SEAL INDICATES ONLY THAT THE TRUSS ASSEMBLY SHOWN ON THIS SHEET MEETS THE MINIMUM APPLICABLE DESIGN
CRITERIA FOR THE LOADS, LOADING CONDITIONS, TRUSS MEMBER CONFIGURATIONS, AND SPANS LISTED ON THIS SHEET.
GUSSET PLATES
Joint#
Gauge
Size
/
/
Refer to Attachment A
for Gusset Plate Usage
KEYemart
Ver 3.305
JOB NAME SPAN PITCH QTY OHL OHR PLYS SPACING
ODEJUL14 \J03_20 6 -0 -0 3.0000 4 2 -0 -0 0 -0 -0 1 2 -0 -0
Reactions
CSI
SUMMARY
0 -7 -8
0 -p -0
JT TYPE LC BRG WID REACT JT MAX REACT MAX UPLIFT
6 P 1 6.000 540. 6 540. -788.
4 R 1 2.000 300. 4 300. -450.
6 P 2 6.000 344.H
6 P 2 6.000 -788.
4 R 2 2.000 -450.
6 P 3 6.000 280
4 R 3 2.000 200
Material
T/C to be: S162 -43 3.625
B/C to be: S162 -33 3.625
Webs to be: S162 -33 3.625
DECON WORLD WIDE, INC.
2652 NW 31st Avenue
Ft. Lauderdale, FL 33311
(954) 485 -8800 FAX: (954) 485 -8809
3 -0 -0
3 -0 -0
3 -0 -0
3 -0 -0
Material CSI P #Screws Brc
1- 2 TCHORD S162-43 3.625 .68 -444 2
2- 3 TCHORD 5162 -43 3.625 .31 -65 2
4- 5 BCHORD S162-33 3.625 .30 -587 4
5- 6 BCHORD S162-33 3.625 .23 -344 2
1- 6 WEB S162 -33 3.625 .16 786 4
1- 5 WEB S162-33 3.625 .08 388 2
2- 5 WEB 5162 -33 3.625 .02 104 2
2- 4 WEB S162 -33 3.625 .14 623 4
3- 4 WEB S162 -33 3.625 .05 238 2
7- 1 TCHORD S162-43 3.625 .55 43 2
"4 SCREWS" Indicates the number of #10 screws at the end of the
member. Screw counts indicated at interior points of continuous
members shall be neglected. Allowable shear per screw as follows:
22 GA:1661bs; 20 GA:2401bs; 18 GA:2631bs; 16 GA:3701bs; 14 GA:
4671bs; 12 GA:4671bs; 10 GA:4671bs. Maintain screw spacing at
9/16" min. Maintain edge margin at 9/16 "min.
1 -4 -8
0 -q -0
6 -0 -0
3-0-0
Deflection (loc)
TC .68 Vert LL -.01" L/999 5
BC .10 H orz TL .00" 4
WB TC CONTINUOUSLY SHEATHED
BC CONTINUOUSLY SHEATHED
3 -0 -0
6 -0 -0
2 -1 -8
3
0 -p -0
Design Loadings
LOAD CASE 1
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
LOAD CASE 2
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
SECTION DIR LIVI: DEAD DISTRIBUTED LOADS
1- 3 Norm -86.1 5.0
4- 6 Vert .0 5.0
7- 1 Norm -86.1 5.0
Note:Distributed Loade Replace Standard Loads
LOAD CASE 3
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
.0 15.0 10.0 10.0
7/17/98
1:47pm
Page 1 of 1
kci)
7
ALL GENERAL NOTES FOUND ON PAGES 1 AND 2 OF THIS DRAWING PACKAGE SHALL BE CONSIDERED AS AN INTEGRAL PART' OF THIS COMPONENT DESIGN DOCUMENT.
NOTE THAT THE PROFESSIONAL ENGINEER'S SEAL INDICATES ONLY THAT THE TRUSS ASSEMBLY SHOWN ON THIS SHEET MEETS THE MINIMUM APPLICABLE DESIGN
CRITERIA FOR THE LOADS, LOADING CONDITIONS, TRUSS MEMBER CONFIGURATIONS, AND SPANS LISTED ON THIS SHEET.
GUSSET PLATES
Joint#
Gauge
Size
77
Refer to Attachment A
for Gusset Plate Usage
KEYsmart
Ver 3.305
JOB NAME
SPAN PITCH QTY OHL OHR PLYS SPACING
ODEJUL14 \T01_20 17 -6 -0 3.0000 1 2 -0 -0 2 -0 -0 1 2 -0 -0
9 -6 -0
4 -0 -0 4 -0 -0 1 -6 -0
I I
0 -7 -8 1 -7 -8 2 -7 -8 2 -7 -8
0 -? -0
Reactions
12
3
Material
T/C to be: S162 -43 3.625
B/C to be: S162 -33 3.625
Webs to be: S162 -33 3.625
4 -0 -0
4 -0 -0
4 -0 -0
JT TYPE LC BRG WID REACT
12 P 1 6.000 1142.
7 R 1 6.000 1143.
12 P 2 6.000 1020.
7 R 2 6.000 1020.
12 P 3 6.000 672.
7 R 3 6.000 673.
CSI
DECON WORLD WIDE, INC.
2652 NW 31st Avenue
Ft. Lauderdale, FL 33311
(954) 485 -8800 FAX: (954) 485 -8809
2
11
0 -0 -0
8 -0 -0
4 -1 -13
8 -1 -13
10 9
0 -1-0 0 -0 -0
1 -2 -6
9 -4 -3
13 -6 -0
4 -0 -0
4 -1 -13
13 -6 -0
1 -7 -8
0 -0 -0
Deflection (loc)
TC .83 Vert TL .16" L/999 8 -9
BC .81 Horz TL .03" 7
TC CONTINUOUSLY SHEATHED
BC CONTINUOUSLY SHEATHED
SUMMARY
JT MAX REACT MAX UPLIFT
12 1142. -1020.
7 1143. -1020.
Material CSI P #Screws Brc
1- 2 TCHORD S162-43 3.625 .83 -2183 1
2- 3 TCHORD S162 -43 3.625 .74 -1837
3- 4 TCHORD S162 -43 3.625 .40 -1739
4- 5 TCHORD S162 -43 3.625 .74 -1830
5- 6 TCHORD S162 -43 3.625 .83 -2182 1
7- 8 BCHORD S162 -33 3.625 .29 0
8- 9 BCHORD 5162 -33 3.625 .80 2064 1
9 -10 BCHORD 5162 -33 3.625 .41 1732
10 -11 BCHORD S162 -33 3.625 .81 2066 1
11 -12 BCHORD S162-33 3.625 .29 0
1 -12 WEB S162 -33 3.625 .33 -1084
1 -11 WEB 5162 -33 3.625 .61 2072 1
2 -11 WEB S162 -33 3.625 .04 222
2 -10 WEB S162 -33 3.625 .13 350
3 -10 WEB S162 -33 3.625 .04 189
4 -10 WEB S162 -33 3.625 .00 12
4- 9 WEB S162 -33 3.625 .04 187
5- 9 WEB S162 -33 3.625 .14 352
5- 8 WEB S162 -33 3.625 .04 221
6- 8 WEB S162 -33 3.625 .61 2070 1
6- 7 WEB 5162 -33 3.625 .33 -1084
13- 1 TCHORD S162 -43 3.625 .35 43
14- 6 TCHORD S162 -43 3.625 .35 43
"# SCREWS" Indicates the number of #10 screws at the end of the
member. Screw counts indicated at interior points of continuous
members shall be neglected. Allowable shear per screw as follows:
22 GA:1661bs; 20 GA:2401bs; 18 GA:2631bs; 16 GA:3701bs; 14 GA:
4671b8; 12 GA:4671bs; 10 GA:4671bs. Maintain screw spacing at
9/16" min. Maintain edge margin at 9/16 "min.
17 -6 -0
4 -0 -0
1
4 -0 -0
17 -6 -0
12
0 -7 -8
0 -? -0
Design Loadings
LOAD CASE 1
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
LOAD CASE 2
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
SECTION DIR LIVE DEAD DISTRIBUTED LOADS
1- 6 Norm -56.5 5.0
7 -12 Vert .0 5.0
13- 1 Norm -56.5 5.0
6 -14 Norm -56.5 5.0
Note:Distributed Loads Replace Standard Loads
LOAD CASE 3
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
.0 15.0 10.0 10.0
7/17/98
1:47pm
Page 1 of 1
ALL GENERAL NOTES FOUND ON PAGES 1 AND 2 OF THIS DRAWING PACKAGE SHALL BE CONSIDERED AS AN INTEGRAL PART OF THIS COMPONENT DESIGN DOCUMENT.
NOTE THAT THE PROFESSIONAL ENGINEER'S SEAL INDICATES ONLY THAT THE TRUSS ASSEMBLY SHOWN ON THIS SHEET MEETS THE MINIMUM APPLICABLE DESIGN
CRITERIA FOR THE LOADS, LOADING CONDITIONS, TRUSS MEMBER CONFIGURATIONS, AND SPANS LISTED ON THIS SHEET.
GUSSET PLATES
Joint#
Gauge
Size
,///////'//
Refer to Attachment A
for Gusset et Pllate Usage
KEYsmart
1Ver 3.305
JOB NAME
ODEJUL14 \T02 20
JT
10
6
1-
2-
3
4
6
7
8
9-
2
3
4
4
5
5
11
12
1
1 -
2-
TYPE LC
P 1
R 1
2 TCHORD
3 TCHORD
4 TCHORD
5 TCHORD
7 BCHORD
8 BCHORD
9 BCHORD
10 BCHORD
10 WEB
9 WEB
9 WEB
8 WEB
8 WEB
8 WEB
7 WEB
7 WEB
6 WEB
1 TCHORD
5 TCHORD
0 -7 -8 1 -8 -10 2 -9 -12 1 -8 -10
01 -0
10 P 2 6.000
6 R 2 6.000
10 P 3 6.000
6 R 3 6.000
Material
S162 -43
S162 -43
S162 -43
S162 -43
S162 -33
S162 -33
S162 -33
S162 -33
S162 -33
5162 -33
S162 -33
S162 -33
S162 -33
S162-33
S162 -33
S162-33
S162-33
S162 -43
S162 -43
TC
Reactions SUMMARY
BRG WID REACT
6.000 1143.
6.000 1143.
Material
T/C to be: S162 -43 3.625
B/C to be: S162 -33 3.625
Webs to be: S162 -33 3.625
-1020.
-1020.
673.
673.
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
4 -4 -8
4 -4 -8
4 -4 -8
4 -4 -8
SPAN
17 -6 -0
CSI
BC .86
CONTINUOUSLY SHEATHED
CONTINUOUSLY SHEATHED
CSI P #Screws Brc
.87
.78
.78
.87
.32
.86
.86
.32
.33
.66
.04
.20
.10
.20
.04
.66
.33
.35
.35
DECON WORLD WIDE, INC.
2652 NW 31st Avenue
Ft. Lauderdale, FL 33311
(954) 485 -8800 FAX: (954) 485 -8809
JT MAX REACT MAX UPLIFT
10 1143. -1020.
6 1143. -1020.
-2212
-1735
-1735
-2212
0
2092
2092
0
-1082
2097
217
480
444
480
217
2097
-1082
43
43
0 -? -0
10
8
8
10
2
10
10
2
6
10
2
2
2
2
2
10
6
2
2
8 -9 -0
4 -4 -8
4 -4 -8
8 -9 -0
Vert
Horz
"# SCREWS" Indicates the number of 810 screws at the end of the
member. Screw counts indicated at interior points of continuous
members shall be neglected. Allowable shear per screw as follows:
22 GA:1661bs; 20 GA:2401bs; 18 GA:2631b8; 16 GA:3701bs; 14 GA:
4671bs; 12 GA:4671b8; 10 GA:4671b8. Maintain screw spacing at
9/16" min. Maintain edge margin at 9/16 "min.
PITCH QTY OHL OHR PLYS
2.9993 3 2 -0 -0 2 -0 -0 1
0 -q -0
13 -1 -8
4 -4 -8
4 -4 -8
13 -1 -8
0 -q -0
Deflection (loc)
LL .17" L/999 8 -9
TL
17 -6 -0
4 -4 -R
4 -4 -8
17 -6 -0
SPACING
2 -0 -0
0 -7 -8
0 -9 -0
7/17/98
1:47pm
Page 1 of 1
Design Loadings
LOAD CASE 1
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
LOAD CASE 2
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
SECTION DIR LIVE DEAD DISTRIBUTED LOADS
1- 5 Norm -56.5 5.0
6 -10 Vert .0 5.0
11- 1 Norm -56.5 5.0
5 -12 Norm -56.5 5.0
Note:Distributed Loads Replace Standard Loads
LOAD CASE 3
TOP LL TOP DL HOT LL BOT DL STANDARD LOADING
.0 15.0 10.0 10.0
ALL GENERAL NOTES FOUND ON PAGES 1 AND 2 OF THIS DRAWING PACKAGE SHALL BE CONSIDERED AS AN INTEGRAL PART OF THIS COMPONENT DESIGN DOCUMEN
NOTE THAT THE PROFESSIONAL ENGINEER'S SEAL INDICATES ONLY THAT THE TRUSS ASSEMBLY SHOWN ON THIS SHEET HEM'S THE MINIMUM APPLICABLE DESIGN
CRITERIA FOR THE LOADS, LOADING CONDITIONS, TRUSS MEMBER CONFIGURATIONS, AND SPANS LISTED ON THIS SHEET.
GUSSET PLATES
Joint ##
Gauge
Size
/ e//' / ////'
/
Refer to Attachment A
for Gusset Plate Usage
KEYsmart
Ver 3.305
SPAN PITCH QTY OHL OHR PLYS SPACING
ODEJUL14 \T03 20 17 -6 -0 2.9993 2 2 -0 -0 2 -0 -0 1 2 -0 -0
JOB NAME
0 -7 -8 1 -8 -12
0-0 -0
10 P 2 6.000 -342.
9 R 2 6.000 -905.
6 R 2 6.000 -812.
10 P 3 6.000 125.
9 R 3 6.000 732.
6 R 3 6.000 488.
Material
T/C to be: S162 -43 3.625
B/C to be: S162 -33 3.625
Webs to be: S162 -33 3.625
4 -5 -0
4 -5 -0
4 -5 -0
4 -5 -0
CSI
0 -q -0
8 -9 -0
4 -4 -0
4 -4 -0
8 -9 -0
TC .69 Vert LL -.07" L/999 7 -8
BC .53 Horz TL .01" 6
WB .39
TC CONTINUOUSLY SHEATHED
BC CONTINUOUSLY SHEATHED
Reactions SUMMARY
JT TYPE LC BRC WID REACT JT MAX REACT MAX UPLIFT
10 P 1 6.000 309. 10 309. -342.
9 R 1 6.000 1115. 9 1115. -905.
6 R 1 6.000 861. 6 861. -812.
Material CSI P #Screws Brc
1- 2 TCHORD S162 -43 3.625 .55 335 2
2- 3 TCHORD S162 -43 3.625 .61 -712 4
3- 4 TCHORD 5162 -43 3.625 .53 -706 4
4- 5 TCHORD S162 -43 3.625 .69 -1373 6
6- 7 BCHORD S162 -33 3.625 .23 0 2
7- 8 BCHORD S162 -33 3.625 .53 1280 6
8- 9 BCHORD S162-33 3.625 .37 311 2
9 -10 BCHORD S162-33 3.625 .31 0 2
1 -10 WEB S162-33 3.625 .09 365 2
1- 9 WEB S162 -33 3.625 .11 285 2
2- 9 WEB S162 -33 3.625 .31 -978 6
2- 8 WEB S162 -33 3.625 .29 988 6
3- 8 WEB S162-33 3.625 .02 97 2
4- 8 WEB S162 -33 3.625 .28 -679 4
4- 7 WEB S162 -33 3.625 .03 143 2
5- 7 WEB S162 -33 3.625 .39 1284 6
5- 6 WEB S162 -33 3.625 .25 817 4
11- 1 TCHORD S162-43 3.625 .35 43 2
12- 5 TCHORD S162-43 3.625 .38 43 2
"# SCREWS" Indicates the number of #10 screws at the end of the
member. Screw counts indicated at interior points of continuous
members shall be neglected. Allowable shear per screw as follows:
22 GA:1661bs; 20 GA:2401bs; 18 GA:2631bs; 16 GA:3701bs; 14 GA:
4671bs; 12 GA:4671bs; 10 GA:4671bs. Maintain screw spacing at
9/16" min. Maintain edge margin at 9/16 "min.
DECON WORLD WIDE, INC.
2652 NW 31st Avenue
Ft. Lauderdale, FL 33311
(954) 485 -8800 FAX: (954) 485 -8809
0 -? -0
13 -1 -8
4 -4 -8
2 -9 -12 1 -8 -10 0 -7 -8
4 -4 -8
13 -1 -8
0-0 -0
Deflection (loc)
Design Loadings
LOAD CASE 1
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
LOAD CASE 2
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
SECTION DIR LIV;'s DEAD DISTRIBUTED LOADS
1- 5 Norm -56.5 5.0
6 -10 Vert .0 5.0
11- 1 Norm -56.5 5.0
5 -12 Norm -56.5 .0
Note:Distributed Loads Replace Standard Loads
LOAD CASE 3
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
.0 15.0 10.0 10.0
17 -6 -0
4 -4 -8
4 -4 -8
17 -6 -0
1
0 -p -0
7/17/98
1:47pm
Page 1 of 1
ALL GENERAL NOTES FOUND ON PAGES 1 AND 2 OF THIS DRAWING PACKAGE SHALL BE CONSIDERED AS AN INTEGRAL PART OF THIS COMPONENT DESIGN DOCUME
NOTE THAT THE PROFESSIONAL ENGINEER'S SEAL INDICATES ONLY THAT THE TRUSS ASSEMBLY SHOWN ON THIS SHEET MEETS THE MINIMUM APPLICABLE DESIGN
CRITERIA FOR THE LOADS, LOADING CONDITIONS, TRUSS MEMBER CONFIGURATIONS, AND SPANS LISTED ON THIS SHEET.
GUSSET PLATES
Joint#
Gauge
Size
Refer to Attachment A
for Gusset Plate Usage
i
KEYsmart
Ver 3.305
JOB NAME
SPAN PITCH QTY OHL OHR PLYS SPACING
ODEJUL14 \T0420 13 -4 -0 2.9980 1 0 -0 -0 2 -0 -0 1 2 -0 -0
0 -0 -0
8 P 2 6.000 -174.H
8 P 2 6.000 -612.
5 R 2 6.000 -834.
8 P 3 6.000 462.
5 R 3 6.000 531.
Material
T/C to be: S162-43 3.625
B/C to be: S162-33 3.625
Webs to be: S162-33 3.625
4 -7 -0
4 -7 -0
CSI
DECON WORLD WIDE, INC.
2652 NW 31st Avenue
Ft. Lauderdale, FL 33311
(954) 485 - 8800 FAX: (954) 485 -8809
0 - q -0
4 -4 -8
8 -11 -8
Material CSI P #Screws Brc
1- 2 TCHORD S162 -43 3.625 .76 -949 4
2- 3 TCHORD S162 -43 3.625 .58 -951 4
3- 4 TCHORD S162 -43 3.625 .71 -1567 6
5- 6 BCHORD S162 -33 3.625 .24 0 2
6- 7 BCHORD S162 -33 3.625 .59 1468 8
7- 8 BCHORD S162 -33 3.625 .25 174 2
1- 8 WEB S162 -33 3.625 .21 -683 4
1- 7 WEB 5162 -33 3.625 .31 910 4
2- 7 WEB 5162 -33 3.625 .03 157 2
3- 7 WEB S162-33 3.625 .26 -626 4
3- 6 WEB S162 -33 3.625 .03 156 2
4- 6 WEB S162 -33 3.625 .44 1472 8
4- 5 WEB S162-33 3.625 .27 -874 4
9- 4 TCHORD S162 -43 3.625 .35 43 2
"8 SCREWS" Indicates the number of 810 screws at the end of the
member. Screw counts indicated at interior points of continuous
members shall be neglected. Allowable shear per screw as follows:
22 GA:1661bs; 20 GA:2401bs; 18 GA:2631bs; 16 GA:3701bs; 14 GA:
4671bs; 12 GA:4671bs; 10 GA:4671bs. Maintain screw spacing at
9/16" min. Maintain edge margin at 9/16 "min.
0 - ? - 0
4 -4 -8
13 -4 -0
Deflection (loc)
TC .76 Vert LL -.08" L/999 6 -7
BC .59 Horz TL .01" 5
TC CONTINUOUSLY SHEATHED
BC CONTINUOUSLY SHEATHED
Reactions SUMMARY
JT TYPE LC BRG WID REACT JT MAX REACT MAX UPLIFT
8 P 1 6.000 720. 8 720. -612.
5 R 1 6.000 927. 5 927. -834.
Design Loadings
LOAD CASE 1
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
LOAD CASE 2
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
SECTION DIR LIVE: DEAD DISTRIBUTED LOADS
1- 4 Norm -56.5 5.0
5- 8 Vert .0 5.0
4- 9 Norm -56.5 5.0
Note:Distributed Loads Replace Standard Loads
LOAD CASE 3
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
.0 15.0 10.0 10.0
0 -0 -0
7/17/98
1:47pm
Page 1 of 1
ALL GENERAL NOTES FOUND ON PAGES 1 AND 2 OF THIS DRAWING PACKAGE SHALL BE CONSIDERED AS AN INTEGRAL PART OF THIS COMPONENT DESIGN DOCUMENT
NOTE THAT THE PROFESSIONAL ENGINEER'S SEAL INDICATES ONLY THAT THE TRUSS ASSEMBLY SHOWN ON THIS SHEET ME:3TS THE MINIMUM APPLICABLE DESIGN
CRITERIA FOR THE LOADS, LOADING CONDITIONS, TRUSS MEMBER CONFIGURATIONS, AND SPANS LISTED ON THIS SHEET.
GUSSET PLATES
Joint#
Gauge
Size
� /
Refer to Attachment A
for Gusset Plate Usage
KEYsmart
Ver 3.305
JOB NAME
ODEJUL14 \T05 20
Reactions
JT
6
4
1- 2
2- 3
4- 5
5- 6
1- 6
1- 5
2- 5
3- 5
3- 4
TYPE
P
R
LC
1
1
Material
TCHORD
TCHORD
BCHORD
BCHORD
WEB
WEB
WEB
WEB
WEB
BC
BRG WID
6.000
6.000
6 P 2 6.000
4 R 2 6.000
6 P 3 6.000
4 R 3 6.000
Material
T/C to be: 5162 -43 3.625
B/C to be: S162 -33 3.625
Webs to be: S162-33 3.625
S162 -43
S162 -43
S162 -33
S162-33
S162 -33
S162 -33
5162 -33
S162 -33
S162-33
-435.
-433.
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
3.625
327.
327.
SPAN PITCH QTY OHL OHR
9 -4 -0 2.9980 2 0 -0 -0 0 -0 -0
1 -8 -0
0 -p -0
.71
.78
.30
.29
.15
.16
.06
.16
.15
6
DECON WORLD WIDE, INC.
2652 NW 31st Avenue
Ft. Lauderdale, FL 33311
(954) 485 -8800 FAX: (954) 485 -8809
4 -7 -0
4-7-0
F
1
-557
-559
0
4
-475
513
269
511
-473
12
3
4 -7 -0
4 -7 -0
CSI
TC .30
WB .16
TC CONTINUOUSLY SHEATHED
CONTINUOUSLY SHEATHED
SUMMARY
REACT JT MAX REACT MAX
513. 6 513. -435.
513. 4 513. -433.
CSI P #Screws
4
4
2
2
2
4
2
4
2
"It SCREWS° Indicates the number of #10 screws at the end of the
member. Screw counts indicated at interior points of continuous
members shall be neglected. Allowable shear per screw as follows:
22 GA:1661ba; 20 GA:2401bs; 18 GA:2631bs; 16 GA:3701bs; 14 GA:
4671bs; 12 GA:4671bs; 10 GA:4671bs. Maintain screw spacing at
9/16" min. Maintain edge margin at 9/16 "min.
UPLIFT
Brc
2 -9- 2
5
0 - p -0
Deflection
Vert TL .02"
Horz TL .00"
9 -4 -0
4 -9 -0
4 -9 -0
9 -4 -0
12
3
(loc)
L/999 4 -5
4
CC
PLYS
1
1 -7 -8
3
4
SPACING
2 -0 -0
Design Loadings
LOAD CASE 1
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
LOAD CASE 2
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
SECTION DIR LIVR DEAD DISTRIBUTED LOADS
1- 3 Norm -56.5 5.0
4- 6 Vert .0 5.0
Note:Distributed Loadn Replace Standard Loads
LOAD CASE 3
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
.0 15.0 10.0 10.0
7/17/98
1:47pm
Page 1 of 1
ALL GENERAL NOTES FOUND ON PAGES 1 AND 2 OF THIS DRAWING PACKAGE SHALL BE CONSIDERED AS AN INTEGRAL PART OF THIS COMPONENT DESIGN DOCUMENT
NOTE THAT THE PROFESSIONAL ENGINEER'S SEAL INDICATES ONLY THAT THE TRUSS ASSEMBLY SHOWN ON THIS SHEET MELTS THE MINIMUM APPLICABLE DESIGN
CRITERIA FOR THE LOADS, LOADING CONDITIONS, TRUSS MEMBER CONFIGURATIONS, AND SPANS LISTED ON THIS SHEET.
GUSSET PLATES
Joint#
Gauge
Size
77
Refer to Attachment A
for Gusset Plate Usage
KEYSmart
Ver 3.305
DECON WORLD WIDE, INC.
2652 NW 31st Avenue
Ft. Lauderdale, FL 33311
(954) 485 -8800 FAX: (954) 485 -8809
JOB NAME SPAN PITCH QTY OHL OHR PLYS SPACING
ODEJUL14 \T06_20 4 -0 -0 3.0000 1 2 -0 -0 0 -0 -0 1 2 -0 -0
Reactions
Material
T/C to be: S162 -33 3.625
B/C to be: S162 -33 3.625
Webs to be: S162 -33 3.625
SUMMARY
0 -7 -8
JT TYPE LC BRG WID REACT JT MAX REACT MAX UPLIFT
4 P 1 6.000 445. 4 445. -419.
3 R 1 6.000 175. 3 175. -159.
4 P 2 6.000 170.H
4 P 2 6.000 -419.
3 R 2 6.000 -159.
4 P 3 6.000 215.
3 R 3 6.000 125.
Material CSI P #Screws Brc
1- 2 TCHORD S162 -33 3.625 .62 -54 2
3- 4 BCHORD S162 -33 3.625 .22 -169 2
1- 4 WEB S162-33 3.625 .12 439 2
1- 3 WEB S162 -33 3.625 .03 170 2
2- 3 WEB S162 -33 3.625 .04 165 2
5- 1 TCHORD S162 -33 3.625 .47 43 2
"# SCREWS" Indicates the number of #10 screws at the end of the
member. Screw counts indicated at interior points of continuous
members shall be neglected. Allowable shear per screw as follows:
22 GA:1661bs; 20 GA:2401bs; 18 GA:2631bs; 16 GA:3701bs; 14 GA:
4671bs; 12 GA:4671bs; 10 GA:4671bs. Maintain screw spacing at
9/16" min. Maintain edge margin at 9/16 "min.
4 -0 -0
4 -0 -0
1 -7 -8
2
3
0- Q -0
4 -0 -0
4 -0 -0
CSI Deflection (loc)
TC .62 Vert TL .01" L/999 3 -4
B C .22 Horz TL .00" 3
TC CONTINUOUSLY SHEATHED
BC CONTINUOUSLY SHEATHED
Design Loadings
LOAD CASE 1
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
LOAD CASE 2
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
SECTION DIR LIV3 DEAD DISTRIBUTED LOADS
1- 2 Norm -56.5 5.0
3- 4 Vert .0 5.0
5- 1 Norm -56.5 5.0
Note:Distributed Loadi, Replace Standard Loads
LOAD CASE 3
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
.0 15.0 10.0 10.0
7/17/98
1:47pm
Page 1 of 1
ALL GENERAL NOTES FOUND ON PAGES 1 AND 2 OF THIS DRAWING PACKAGE SHALL BE CONSIDERED AS AN INTEGRAL PART OF THIS COMPONENT DESIGN DOCUMENT.
NOTE THAT THE PROFESSIONAL ENGINEER'S SEAL INDICATES ONLY THAT THE TRUSS ASSEMBLY SHOWN ON THIS SHEET MEETS THE MINIMUM APPLICABLE DESIGN
CRITERIA FOR THE LOADS, LOADING CONDITIONS, TRUSS MEMBER CONFIGURATIONS, AND SPANS LISTED ON THIS SHEET.
GUSSET PLATES
Joint#
Gauge
Size
//
Refer to Attachment A
for Gusset Plate Usage
KEYsmart
Ver 3.305
JOB NAME SPAN PITCH QTY OHL OHR PLYS
ODEJUL14 \T07_20 4 -2 -0 .0000 1 0 -0 -0 0 -0 -0 1
Reactions SUMMARY
JT TYPE
4 P
3 R
LC BRG WID
1 8.000
1 8.000
Material
T/C to be: S162-33 3.625
8/C to be: S162 -33 3.625
Webs to be: S162-33 3.625
Material
1- 2 TCHORD S162 -33
3- 4 BCHORD S162-33
1- 4 WEB S162 -33
1- 3 WEB S162 -33
2- 3 WEB S162 -33
BC
CSI
BC .25
WB .06
CONTINUOUSLY SHEATHED
CONTINUOUSLY SHEATHED
REACT
229.
229.
4 P 2 8.000 -194.
3 R 2 8.000 -194.
4 P 3 8.000 146.
3 R 3 8.000 146.
DECON WORLD WIDE, INC.
2652 NW 31st Avenue
Ft. Lauderdale, FL 33311
(954) 485 -8800 FAX: (954) 485 -8809
JT
4
3
0-
0-
•
MAX REACT
229.
229.
CSI P #Screws Brc
3.625 .63 0 2
3.625 .25 0 2
3.625 .06 214 2
3.625 .00 0 2
3.625 .06 214 2
Vert
Horz
MAX UPLIFT
-194.
-194.
"N SCREWS" Indicates the number of #10 screws at the end of the
member. Screw counts indicated at interior points of continuous
members shall be neglected. Allowable shear per screw as follows:
22 GA:1661bs; 20 GA:2401bs; 18 GA:2631bs; 16 GA:3701bs; 14 GA:
4671bs; 12 GA:4671bs; 10 GA:4671bs. Maintain screw spacing at
9/16" min. Maintain edge margin at 9/16 "min.
4 -2 -0
4 -2 -0
4 -2 -0
4 -2 -0
3
-0
Deflection (loc)
TL
TL .00" L/999 3 -4
rk
r
SPACING
2 -0 -0
Design Loadings
LOAD CASE 1
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
LOAD CASE 2
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
30.0 15.0 .0 10.0
SECTION DIR LIVE; DEAD DISTRIBUTED LOADS
1- 2 Norm -56.5 5.0
3- 4 Vert .0 5.0
Note:Distributed Loads Replace Standard Loads
LOAD CASE 3
TOP LL TOP DL BOT LL BOT DL STANDARD LOADING
.0 15.0 10.0 10.0
7/17/98
1:47pm
Page 1 of 1
ALL GENERAL NOTES FOUND ON PAGES 1 AND 2 OF THIS DRAWING PACKAGE SHALL BE CONSIDERED AS AN INTEGRAL PART OF THIS COMPONENT DESIGN DOCUMENT.
NOTE THAT THE PROFESSIONAL ENGINEER'S SEAL INDICATES ONLY THAT THE TRUSS ASSEMBLY SHOWN ON THIS SHEET MEETS THE MINIMUM APPLICABLE DESIGN
CRITERIA FOR THE LOADS, LOADING CONDITIONS, TRUSS MEMBER CONFIGURATIONS, AND SPANS LISTED ON THIS SHEET.
#10 SDS ' QUANTITY
PER TRUSS DESIGN
DRAWING. DRAWING
FOR WEB. PLACE
SfS THRI J WER ANl
INTO GUSSET. MINIMUM
QUANTITY OF SDS IS (4).
1/4 "(MA
#10 SDS ti QUANTITY
PER TRUSS DESIGN
DRAWING. DRAWING
FOR CHORDS. PLACE
SDS THRU GUSSET AND
INTO CHORD. MINIMUM
QUANTITY OF SDS IS (3).
FLAT FE GUSSET
4 "x 8 "x 16 GA.
DETAIL REFERENCE NUMBER
DJO1
T ITLE : "CEE" SHAPE TOP CHORD PITCH BREAK
iREV.000
SAT E :07/22/98 J DRWG. BY:
ROGER TALBERT
DWG.
SCALE: I - 2
Key mark
NGINEERING
#10 SDS QUANTITY PER
TRUSS DESIGN DRAWING
PLACE SDS THRU DIAGONAL
WEB (IF IT EXISTS), THEN
THRU GUSSET AND INTO
THE CHORD
TOP CHORD
•-s.
/
/
/ /
/ ` .
`IN : , N.
/ /
N.
/ / N.
< / `.
■ / N.
N. /.
N. / .
/ /
/ /
I--
L
1/4" (MAX.)
DIAGONAL WEB AS REQUIRED
#10 SDS N QUANTITY PER
TRUSS DESIGN DRAWING.
PLACE SDS THRU WEB,
THRU GUSSET AND INTO CHORD.
v�ERTi
tAIrn
VVCD
TOP CHORD
FLAT Fj GUSSET
4 "x 8 "x 16 GA.
DETAIL REFERENCE NUMBER
DJ02
TITLE : °CEE° TOP CHORD ANGLED PITCH BREAK
• EV.000
DATE :07/22/98
DRWG. BY:
ROGER TALBERT ISCALE: I° -2°
Key mark
NGINEERING
DETAIL A
TRUSS WEB
TOP CHORD
NOTE:
BEARING
ENHANCER ANGLE
REQUIRED FOR
EACH BEARING
POINT WHEN THE
REACTION
EXCEEDS THE
FOLLOWING
NOTE:
INDICATED BY:
jjj
#10 SDS AS PER TOP CHORD
COPE TOP
FLANGE OF
R OT S OWNHORD
S
TRUSS
ENGINEERING
. - - --
� ,�,, -'`-
BOTTOM
CHORD GA.
REACTION
(LB.)
#12 SDS
AS PER TRUSS
ENGINEERING
1 1/2"x 3 1/2"
x O' -3 3/4"
x16 GA BEARING
ENHANCER ANGLE
20
500
-'-
,
18
700
-
_.
' ff
A
%^
j �� / / /�,,. ; , -,
/ / ,,,-
/,,,
WEB
16
1400
BEARING --`-
ENHANCER
ANGLE
3 3/4"
BEARING ENHANCER
3 1/2"
1 GA.
—
.-2,2,2. ► Q ROTTOnA CHORD
NOTE: #10 SDS — QUANTITY PER
BEARING WIDTH
6" MINIMUM TRUSS DESIGN DRAWING.
PLACE SDS THRU WEB, THRU
BEARING ENHANCER ANGLE
(IF PRESENT) AND INTO
BOTTOM CHORD
/
1 1/2"
DETAIL REFERENCE NUMBER
DJ03
T I T L_ E : BEARING ENHANCER . ezec -�
REV.000
00
Ke mark
E
ENGINEERING
DATE:07/22/98
DRWG. BY: ROGER TALBERT
u_ M
° �' G ' I —4
SCALE: