Buy Mil Spares is your sourcing solution for top-quality military and defense parts, aerospace parts, and other similar products that are necessary for operational fulfillment. You have reached the RFQ page for part number HS1006DD61-0708, a Beam Structural item that is listed with the NSN 9540-01-478-9730 for an ease of identification. Manufactured by Boeing Company The and readily available for procurement today, you are always welcome to request a quote on this NSN part to receive tailored pricing information and fulfillment options from our team. Simply offer us important information like your desired quantity, price, and fulfillment timeframe, and our team will supply you with a tailored quote on part number HS1006DD61-0708 in 15 minutes or less.
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To ensure that customers quickly identify and procure exact items, we list everything with as much relevant information as possible. For example, while part number HS1006DD61-0708 is manufactured by Boeing Company The, it is specifically done so under CAGE Code 8V613, a unique identifier assigned to a specific facility by the DLA that supplies to various government or defense agencies. Furthermore, using the first digits of the NSN 9540-01-478-9730, one can also determine that this part falls under FSC 9540 Structural Shapes Nonferrous Base Metal. With this in mind, continue exploring our website today, and see how we can help you secure competitive pricing and rapid lead times on all desired NSN parts.
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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