Mfg Part Number: HS1006DD15-2121
Alternate P/N: HS1006DD152121
NSN : 9540-01-478-9728
NIIN : 014789728
CAGE Code : 8V613
Manufacturer: Boeing Company The
Item Name : Beam Structural
Thank you for your interest in our available parts and components on NSN Target. Beam Structural is an item listed with the part number HS1006DD15-2121, and it is manufactured by Boeing Company The. This particular item HS1006DD15-2121 is currently available for purchase through our website today, and our team of industry experts are on standby 24/7x365 to provide rapid lead-times and competitive pricing. To begin the purchasing process, we invite you to fill out and submit an Instant RFQ form as provided through our website. Once received, a member of our staff will reach out to you in 15 minutes or less to provide a quote that has been personalized to fit your individual needs.
NSN Parts is a website that is owned and operated by ASAP Semiconductor, and we serve as a leading independent distributor of NSN parts and components that serve many industries and applications. Throughout our extensive part and manufacturer catalogues, we carry a variety of top requested components that you may need, including HS1006DD15-2121 with NSN 9540014789728 and other parts manufactured by Boeing Company The. Quality is of the utmost importance to us at NSN Parts, and we have established ourselves as an FAA AC 00-56B, AS9120B, and ISO 9001:2015 certified enterprise. Get started today with a personalized quote and experience how we are revolutionizing the parts procurement process.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9540-01-478-9728 Item Description: BEAM,STRUCTURAL | 9540 | 014789728 | N | |||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
HS1006DD15-2121 | 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 | 0.125 INCHES NOMINAL |
MRC | Decoded Requirement | Clear Text Reply |
ABKW | Overall Height | 1.000 INCHES NOMINAL |
BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 1.000 INCHES NOMINAL |
ABRY | Length | 21.656 INCHES NOMINAL |
AGTA | Basic Shape Style | T SHAPE |
CXCY | Part Name Assigned By Controlling Agency | EXTRUSION, TEE, ALUMINUM ALLOY |
AJJP | Leg Thickness | 0.125 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 | 0.125 INCHES NOMINAL |
BQJG | Top Flange Width | 2.000 INCHES NOMINAL |
BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.094 INCHES NOMINAL |
BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.094 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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