HS1006DD61-0708
View detailed technical data, stock status, and sourcing information for: HS1006DD61-0708
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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.
1.180 inches nominal overall height, extruded fabrication method, 0.050 inches nominal left side top flange thickness, 0.050 inches nominal right side top flange thickness, 7.250 inches nominal length
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
- 1.180 inches nominal
- Length
- 7.250 inches nominal
- Left Side Top Flange Thickness
- 0.050 inches nominal
- Right Side Top Flange Thickness
- 0.050 inches nominal
- End Item Identification
- apache helicopter
- Basic Shape Style
- t shape
- Leg Thickness
- 0.050 inches nominal
- Left Side Top Flange Distance To Center Of Both Flanges
- 1.000 inches nominal
- Right Side Top Flange Distance To Center Of Both Flanges
- 1.000 inches nominal
- Fillet Radius Where Top Left Flange Joins Web Flange/Leg
- 0.062 inches nominal
- Fillet Radius Where Top Right Flange Joins Web Flange/Leg
- 0.062 inches nominal
- Top Flange Width
- 2.000 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-4 solution heat treated or t-3511 solution heat treated
- Material
- aluminum alloy 2024
- Material Document And Classification
- qq-a-200/3 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 |
|---|---|
| HS1006DD61-0708 | Structural Beam |
FAQs
Find helpful answers about installation, operation, maintenance, compliance, and troubleshooting.
What is the FSCG of the NSN 9540-01-478-9730?
Does the NSN 9540-01-478-9730 have a Schedule B code assigned?
Does NSN 9540-01-478-9730 require demilitarization?
Does NSN 9540-01-478-9730 contain precious materials?
Does NSN 9540-01-478-9730 contain hazardous materials?
When the NSN 9540-01-478-9730 was assigned to the Federal Catalog?
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