Whether you are in the market for NSN parts, military and defense parts, aerospace parts, or other similar product solutions, Buy Military Fasteners is your one-stop shop with an expansive selection tracing back to premier manufacturers and entities that we trust. Thank you for taking an interest in part number HS1006AA41B0027, a Boeing Company The item that is listed alongside the description “Beam Structural” and the NSN 9540014789727. As part number HS1006AA41B0027 is ready for purchase on our website at any time, you are invited to fill out and submit the RFQ form provided on this page for the means of requesting a quote for your comparisons. All that we ask is that you supply us with crucial details such as your target price and expected shipping time frame, that way we can best customize a solution that caters to your unique requirements and constraints alike.
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As customers explore our vast selection, they can take advantage of services like our CAGE Code search features or database filters to quickly locate products of interest for purchase. For example, part number HS1006AA41B0027 is listed alongside the NSN 9540-01-478-9727, meaning that it also belongs to FSC 9540 Structural Shapes Nonferrous Base Metal. With this in mind, kick off procurement with us today with assurance that we can even fulfill your most difficult needs.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-478-9727 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014789727 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| HS1006AA41B0027 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| CNQL | Third Tip Relationship To Preceding Tips | IDENTICAL W/FIRST TIP |
| MATT | Material | ALUMINUM ALLOY 7075 |
| HEAT | Heat Treatment | T-6 SOLUTION HEAT TREATED OR T-6511 SOLUTION HEAT TREATED |
| ADXR | Left Side Top Flange Thickness | 0.062 INCHES NOMINAL |
| CSMZ | Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| ABRY | Length | 0.844 INCHES NOMINAL |
| MRC | Decoded Requirement | Clear Text Reply |
| BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 0.750 INCHES NOMINAL |
| AGTA | Basic Shape Style | T SHAPE |
| CXCY | Part Name Assigned By Controlling Agency | EXTRUSION, TEE, ALUMINUM ALLOY |
| AJJP | Leg Thickness | 0.062 INCHES NOMINAL |
| CRZC | Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| BPXG | Right Side Top Flange Distance To Center Of Both Flanges | 0.750 INCHES NOMINAL |
| MDCL | Material Document And Classification | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
| ADXS | Right Side Top Flange Thickness | 0.062 INCHES NOMINAL |
| BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.125 INCHES NOMINAL |
| BQJG | Top Flange Width | 1.500 INCHES NOMINAL |
| BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.125 INCHES NOMINAL |
| AGAV | End Item Identification | APACHE HELICOPTER |
| CMZY | First Tip Style | SQUARE END |
| ABKW | Overall Height | 2.500 INCHES NOMINAL |
| AARN | Fabrication Method | EXTRUDED |
| CNQJ | Second Tip Relationship To First Tip | IDENTICAL |
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