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Structural Beam

Model / MPN: CVC10031-16CA | NSN: 9540-01-475-0888
ITAR Registered seal

A structural shape fabricated from a ferrous or nonferrous material and resembles the following cross-sectional forms: for the letter h, both flanges of the h section are equal or longer than the width measured along the axis of the web; for the letter i, a 16 2/3 percent slope on the inside face of the ferrous type flange, either one or both of the nonferrous type flanges are shorter than the length measured along the axis of the web; for the letters t and z, on nonferrous type, the web is usually at right angles to the flanges. Letter h section may have a of 5 percent slope on the inside face of the flanges.

Product Details
NATO Stock Number
9540-01-475-0888
Sold in multiples of
FT
DEMIL
DEMIL/MLI
Fabrication Method
Any acceptable
Overall Height
2.050 inches
Length
Between 10.000 feet and 12.000 feet
Left Side Top Flange Thickness
0.055 inches
Right Side Top Flange Thickness
0.055 inches
End Application
Intermediate; aircraft b-2 bomber (atb)
Basic Shape Style
I shape
Right Side Bottom Flange Thickness
0.015 inches
Left Side Bottom Flange Thickness
0.015 inches
Left Side Top Flange Distance To Center Of Both Flanges
0.630 inches
Left Side Bottom Flange Distance To Center Of Both Flanges
0.630 inches
Right Side Top Flange Distance To Center Of Both Flanges
0.680 inches
Right Side Bottom Flange Distance To Center Of Both Flanges
0.680 inches
Web Flange Thickness
0.055 inches
Top Flange Width
1.310 inches
Bottom Flange Width
1.310 inches
First Tip Style
Square end
Second Tip Relationship To First Tip
Identical
Right Top Inside Angle
169.0 degrees
Left Top Inside Angle
11.0 degrees
Left Bottom Inside Angle
11.0 degrees
Right Bottom Inside Angle
169.0 degrees
Material
Aluminum alloy, qq-a-430, alloy 7075
Material
Aluminum alloy 7075
Material Specification
Qq-a-430, alloy 7075 federal specification 1st material response
CVC10031 Series Parts

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CVC10031-16CA Cross Reference