If your operations demand part number HS1006AA41B0027, an item produced by Boeing Company The and listed with the description “Beam Structural,” look no further than this page. At your convenience, you can complete the Request for Quote (RFQ) form below with details like your budget, desired quantity, and anticipated fulfillment timeline to receive customized procurement options on part number HS1006AA41B0027. Our representatives will happily treat you to competitive pricing and swift lead times upon their receipt and review of a completed form, regularly responding in 15 minutes or less.
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If you are interested, be sure to explore our website further for related CAGE Code 8V613 items or other various products manufactured by Boeing Company The. We also present a catalog of all related FSC 9540 Structural Shapes Nonferrous Base Metal parts that we currently carry for your perusal. Regardless of what you decide to purchase from us, we will work closely with you to provide dependable, authentic products while ensuring that we address every requirement possible. This being said, get started on requesting quotes for part number HS1006AA41B0027 and any other NSN parts you need on Sky Forge Components to experience our unrivaled fulfillment services.
| 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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