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PR-936 Load Table
®
Date Issued: November 6, 2020
PR-936 Panels Grade 80 (applies to roof application only)
®
Physical Properties: Per Foot Width - In accordance with the CSA S136-01 - Limit States Design
Gauge Thickness Weight Yield Section Moment Factored Moment Specified
(in) (lb/ft ) Stress Modulus of Inertia Resistance Crippling
2
(ksi) Bearing N = 1.5 in.
Mid Support Mid Span Mid Support End Interior
in 3 in 3 in 4 ft-lb ft-lb lb lb
29 0.0142 0.595 80 0.0114 0.0167 0.00693 51.09 75.36 104 173
26 0.0184 0.782 80 0.0157 0.0255 0.00913 70.71 114.78 183 283
2
Load Tables Maxium specified Uniformly Distributed load in lb/ft (psf)
1 Span 2 Span 3 Span
Span Notes:
Gauge Gauge Gauge 1. Properties and loads are based on Grade 80
Steel with a minimum yield stress of 80 ksi and
ft 29 26 29 26 29 26 a maximum yield stress under factored loads of
54 ksi.
B 68 94 100 153 106 147
2 2. Figures in Row B indicate the load capacity
D 76 100 180 237 143 188 based on strength. Strength capacity B should
be checked against[Specified Live Load] +
B 44 60 64 98 68 94
2.5 [0.833 x Specified Dead Load].
D 39 51 92 122 73 96 3. Figures in Row D indicate the load capacity
B 30 42 45 68 47 65 based on deflection of 1/180th span. For
3 allowable deflection of 1/90th of the span, values
D 22 30 53 70 42 56 in Row D can be doubled, but must not exceed
the value in Row B. Deflection capacity should
B 22 31 33 50 35 48 be checked against Specified Load(s).
3.5
D 14 19 34 44 27 35 4. Specified web crippling capacity should be
checked against specified load at support
B 17 24 25 38 27 37 location.
4
D 9 12 23 30 18 24 Notes to the Designer:
1. The Load Tables were developed in accordance
B 13 19 20 30 21 29 with CSA S136-16 - North American Specification
4.5 for the Design of Cold Formed Steel Structural
D 7 9 16 21 13 17 Members and S136S1-04 - Supplement 2004 to
the North American Specification for the Design
B 11 15 16 24 17 24 of Cold Formed Steel Structural Members.
5
D 5 6 12 15 9 12 2. The Load Tables were developed using Limit
States Design principles.
B 9 12 13 20 14 19
5.5 3. The Load Tables are based on specified
D 4 5 9 11 7 9 uniformly distributed loads only.
B 8 10 11 17 12 16
6 4. The effective moment of inertia for deflection
D 3 4 7 9 5 7 determination has been calculated at a specified
live load stress of 0.6Fy.
B 6 9 10 14 10 14
6.5 5. Specified Web Crippling loads were determined
D 2 3 5 7 4 5 using a bearing width of 1.5”.
B 6 8 8 12 9 12 6. The load tables do not consider the effect of
7 pattern loading.
D 2 2 4 6 3 4
7. The load tables do not account for concentrated
B 5 7 7 11 8 10 loads.
7.5
D 1 2 3 5 3 4 8. All span applications assumes all spans are
equal.
B 4 6 6 10 7 9
8
D 1 2 3 4 2 3
Sect. 2 - Pg. 6 PRICES SUBJECT TO CHANGE WITHOUT NOTICE
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