Part No. : HS1006AA63B0200 | Manufacturer : boeing company the | Item Name: beam structural |
NSN: 9540-01-478-9726 (9540014789726) | CAGE Code: 8V613 | FSC: 9540 Structural Shapes Nonferrous Base Metal |
If you require part number HS1006AA63B0200 from Boeing Company The which is described as a Beam Structural component ASAP Logistic Solutions is your sourcing solution. On this page, you can request a quote on part number HS1006AA63B0200 which is listed under the Federal Supply Class 9540 Structural Shapes Nonferrous Base Metal. To ensure that you only procure the exact item you need to be sure to note that this particular product is listed with the NSN 9540014789726 and was produced under the CAGE Code 8V613. To learn more about this listing or to simply initiate the purchasing process, complete and submit the RFQ form on this page for part HS1006AA63B0200 today Within 15 minutes of receiving and reviewing a completed request based on the information you provide a member of our staff will contact you to provide a tailored solution to your comparison needs. HS1006AA63B0200
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9540-01-478-9726 Item Description: Beam Structural | 9540 | 014789726 | 0 | N | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | A | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
Hs1006aa63b0200 | 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 |
CSMZ | Left Top Inside Angle | 90.0 DEGREES NOMINAL |
ADXR | Left Side Top Flange Thickness | 0.060 INCHES NOMINAL |
ABRY | Length | 2.000 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 | 0.060 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 | 0.060 INCHES NOMINAL |
BQJG | Top Flange Width | 1.500 INCHES NOMINAL |
BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.125 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 |
AARN | Fabrication Method | EXTRUDED |
ABKW | Overall Height | 3.250 INCHES NOMINAL |
CNQJ | Second Tip Relationship To First Tip | IDENTICAL |
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