You have reached the Request for Quote (RFQ) page for part number HS1006AA41B0027, an item sourced from Boeing Company The (CAGE Code 8V613) that is classified with the item name Beam Structural. Here, you can utilize our online form to quickly secure tailored pricing and procurement options from our staff as the first step of procurement. With responses always being quick, be sure to get started as soon as possible if you would like to learn more about this part number.
Important Details for Part Number HS1006AA41B0027
The part number HS1006AA41B0027 is associated with Boeing Company The, identified by the CAGE Code 8V613, and is typically referenced under the item name Beam Structural. It is categorized under the NSN 9540-01-478-9727, with the NIIN 014789727, INC 37018, and NCB code 01 (USA). Additionally, this part falls under the Federal Supply Group (FSG) 95 and Federal Supply Class (FSC) 9540 Structural Shapes Nonferrous Base Metal. For more information, these classifications provide further context about the component.
With the form provided, be sure to present our staff with key details on your needs, such as your target pricing, required quantity, and expected turnaround time. Once we receive and review your request for part HS1006AA41B0027, a member of our staff will contact you in 15 minutes or less to present customized solutions for your comparisons. Once you make a purchase with us, you can expect our staff to work closely with you through each step of fulfillment to ensure that all needs are met with care and efficiency.
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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