HS1006AA41B0027
View detailed technical data, stock status, and sourcing information for: HS1006AA41B0027
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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 maximum of 5 percent slope on the inside face of the flanges.
0.844 inches nominal length, 0.062 inches nominal right side top flange thickness, extruded fabrication method, 2.500 inches nominal overall height, 0.062 inches nominal left side top flange thickness
Product Characteristics
Below you’ll find the complete technical specifications and performance data for this part, including material details and compliance information.
- Fabrication Method
- extruded
- Overall Height
- 2.500 inches nominal
- Length
- 0.844 inches nominal
- Left Side Top Flange Thickness
- 0.062 inches nominal
- Right Side Top Flange Thickness
- 0.062 inches nominal
- End Item Identification
- apache helicopter
- Basic Shape Style
- t shape
- Leg Thickness
- 0.062 inches nominal
- Left Side Top Flange Distance To Center Of Both Flanges
- 0.750 inches nominal
- Right Side Top Flange Distance To Center Of Both Flanges
- 0.750 inches nominal
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg
- 0.125 inches nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg
- 0.125 inches nominal
- Top Flange Width
- 1.500 inches nominal
- First Tip Style
- square end
- Second Tip Relationship To First Tip
- identical
- Third Tip Relationship To Preceding Tips
- identical w/first tip
- Right Top Inside Angle
- 90.0 degrees nominal
- Left Top Inside Angle
- 90.0 degrees nominal
- Part Name Assigned By Controlling Agency
- extrusion, tee, aluminum alloy
- Heat Treatment
- t-6 solution heat treated or t-6511 solution heat treated
- Material
- aluminum alloy 7075
- Material Document And Classification
- qq-a-200/11 fed spec 1st material response
Related Parts
This NSN group includes multiple components designed to meet specific performance and operational standards. Each listing provides detailed specs, functionality data, and replacement compatibility information:
| Part Number | Name |
|---|---|
| HS1006AA41B0027 | Structural Beam |
FAQs
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What is the FSCG of the NSN 9540-01-478-9727?
Does the NSN 9540-01-478-9727 have a Schedule B code assigned?
Does NSN 9540-01-478-9727 require demilitarization?
Does NSN 9540-01-478-9727 contain precious materials?
Does NSN 9540-01-478-9727 contain hazardous materials?
When the NSN 9540-01-478-9727 was assigned to the Federal Catalog?
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