NATO Stock Number
9540-01-469-9501
Sold in multiples of
EA
DEMIL
NO
Fabrication Method
Extruded
Overall Height
1.500 inches
Length
32.900 inches
Left Side Top Flange Thickness
0.125 inches
Right Side Top Flange Thickness
0.125 inches
End Application
Aircraft cen sec
Basic Shape Style
I shape
First Tip Radius
0.010 inches
Right Side Bottom Flange Thickness
0.125 inches
Left Side Bottom Flange Thickness
0.125 inches
Left Side Top Flange Distance To Center Of Both Flanges
1.250 inches
Left Side Bottom Flange Distance To Center Of Both Flanges
1.250 inches
Right Side Top Flange Distance To Center Of Both Flanges
1.250 inches
Right Side Bottom Flange Distance To Center Of Both Flanges
1.250 inches
Fillet Radius Where Top Left Flange Joins Web Flange/leg
0.125 inches
Fillet Radius Where Bottom Left Flange Joins Web Flange/leg
0.125 inches
Fillet Radius Where Top Right Flange Joins Web Flange/leg
0.125 inches
Fillet Radius Where Bottom Right Flange Joins Web Flange/leg
0.125 inches
Web Flange Thickness
0.125 inches
Top Flange Width
2.500 inches
Bottom Flange Width
2.500 inches
First Tip Style
Left quarter radius
Second Tip Radius
0.010 inches
Second Tip Relationship To First Tip
Not identical
Second Tip Style
Right quarter radius
Third Tip Relationship To Preceding Tips
Identical w/first tip
Fourth Tip Relationship To Preceding Tips
Identical w/second tip
Right Top Inside Angle
90.0 degrees
Left Top Inside Angle
90.0 degrees
Left Bottom Inside Angle
90.0 degrees
Right Bottom Inside Angle
90.0 degrees
Material
Aluminum alloy, qq-a-200/11
Material
Aluminum alloy 7075
Material Specification
Qq-a-200/11 federal specification 1st material response
Specification Data
81348-qq-a-200/11e/canceled/ government specification and 99237-and10140 government standard