To receive competitive purchasing options on part number HS1006DD61-0708 by Boeing Company The, look no further than NSN Direct. For your reference, this item has the NSN 9540-01-478-9730 and is listed with the description “Beam Structural.” If this matches your needs, we encourage you to fill out the partially-completed quote request form on this page to kick off procurement. By providing comprehensive information about your requirements, such as your desired quantity, pricing, and fulfillment speed, our experts can formulate the most fitting solutions for you. We want to ensure that this process is quick and effortless, so we routinely respond to requests within 15 minutes of receiving and reviewing them.
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In addition to our streamlined quotation service, we also aim to make the process of finding products simple. As such, if you require other Boeing Company The parts produced under the CAGE Code 8V613, you can peruse our manufacturer or CAGE Code catalogs, or use our search engine and filters. Furthermore, if you want to locate items similar to part number HS1006DD61-0708, you can glean from the first four digits of its NSN 9540-01-478-9730 that it belongs to the FSC 9540 Structural Shapes Nonferrous Base Metal. This being said, do not hesitate to request quotes on part number HS1006DD61-0708 and any other NSN parts that we feature to experience unrivaled procurement.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-478-9730 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014789730 | N | A | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| A | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| HS1006DD61-0708 | 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 | 0.050 INCHES NOMINAL |
| MRC | Decoded Requirement | Clear Text Reply |
| BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 1.000 INCHES NOMINAL |
| ABKW | Overall Height | 1.180 INCHES NOMINAL |
| AGTA | Basic Shape Style | T SHAPE |
| CXCY | Part Name Assigned By Controlling Agency | EXTRUSION, TEE, ALUMINUM ALLOY |
| AJJP | Leg Thickness | 0.050 INCHES NOMINAL |
| ABRY | Length | 7.250 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 | 0.050 INCHES NOMINAL |
| BQJG | Top Flange Width | 2.000 INCHES NOMINAL |
| BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.062 INCHES NOMINAL |
| BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.062 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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