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Thank you for taking an interest in the top-caliber NSN products we feature here on AI NSN Parts. On this page, you can submit a quote request for part number HS1006DD15-2211, a Beam Structural item that is manufactured by Boeing Company The. Listed alongside the NSN 9540014789731 within our database, part number HS1006DD15-2211 is conveniently ready for purchase at any time.
To ensure listings like part number HS1006DD15-2211 are ready for swift installation, we have a rigorous quality assurance program in place. As such, we make it easy for you to inquire about popular NSNs like 9540-01-478-9731, as well as the many other Boeing Company The products produced under CAGE Code 8V613 that interest you. For the benefit of our customers, we carefully vet every entity that we source from, guaranteeing that you only receive superior-caliber offerings in every order. With these dedications, you can always purchase from us with confidence. Furthermore, we also organize our stock based on Federal Supply Classes, so you can find popular items under FSCs like 9540 Structural Shapes Nonferrous Base Metal. Do not hesitate to submit the RFQ form below, and within 15 minutes or less of submission, one of our experts will reach out with a customized solution. Get started today and see why so many customers steadily depend on AI NSN Parts for their operational needs.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-478-9731 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014789731 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| HS1006DD15-2211 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| CNQL | Third Tip Relationship To Preceding Tips | IDENTICAL W/FIRST TIP |
| MATT | Material | ALUMINUM ALLOY 2024 |
| HEAT | Heat Treatment | T-4 SOLUTION HEAT TREATED OR T-3511 SOLUTION HEAT TREATED |
| CSMZ | Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| ADXR | Left Side Top Flange Thickness | 0.125 INCHES NOMINAL |
| MRC | Decoded Requirement | Clear Text Reply |
| ABKW | Overall Height | 1.000 INCHES NOMINAL |
| BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 1.000 INCHES NOMINAL |
| ABRY | Length | 22.344 INCHES NOMINAL |
| AGTA | Basic Shape Style | T SHAPE |
| CXCY | Part Name Assigned By Controlling Agency | EXTRUSION, TEE, ALUMINUM ALLOY |
| AJJP | Leg Thickness | 0.125 INCHES NOMINAL |
| CRZC | Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| BPXG | Right Side Top Flange Distance To Center Of Both Flanges | 1.000 INCHES NOMINAL |
| MDCL | Material Document And Classification | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE |
| ADXS | Right Side Top Flange Thickness | 0.125 INCHES NOMINAL |
| BQJG | Top Flange Width | 2.000 INCHES NOMINAL |
| BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.094 INCHES NOMINAL |
| BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.094 INCHES NOMINAL |
| AGAV | End Item Identification | APACHE HELICOPTER |
| CMZY | First Tip Style | SQUARE END |
| AARN | Fabrication Method | EXTRUDED |
| CNQJ | Second Tip Relationship To First Tip | IDENTICAL |
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