Thank you for taking an interest in part number HS1006AA41B0027, a Boeing Company The product we have in stock that is listed alongside the NSN 9540014789727 and the description “Beam Structural.” As part number HS1006AA41B0027 is readily available 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 important information such as your target price and expected shipping time frame so that we can best tailor a solution that caters to your unique needs and restrictions alike.
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To ensure that you only procure the exact items you require for carrying out operations, we list all aerospace parts, military and defense parts, and other product offerings with all applicable information for identification. 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. Furthermore, this NSN part is specifically manufactured under CAGE Code 8V613, a unique identifier belonging to the manufacturer for a specific facility. With all of this in mind, kick off purchasing with us today and see why so many customers steadily choose us for their operational 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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