For competitive procurement options on part number HS1006AA63B0200 from Boeing Company The (CAGE Code 8V613), look no further than Just Parts Unlimited. With the form presented on this page, you can submit information on your needs to receive tailored procurement solutions from our staff.
Part Number HS1006AA63B0200 Details:
Part number HS1006AA63B0200 is manufactured by Boeing Company The and listed with the item name Beam Structural. Classified under NSN 9540-01-478-9726, the NIIN of this item is 014789726, its INC is 37018, and its NCB code is 01 (USA).
For organization and identification purposes, this item is listed within the Federal Supply Group (FSG) 95 Metal Bars Sheets and Shapes and Class (FSC) 9540 Structural Shapes Nonferrous Metal. These details are important for confirming parts before making a purchase.
Disclaimer: This is a quotation for the goods listed above. This quotation is meant as an estimate and does not reflect a final bill or invoice. All quotations are subject to change until acceptance by ASAP Semiconductor of a binding Purchase Order, and quotations may be withdrawn or revised at the sole discretion of ASAP Semiconductor. This quotation is subject to the ASAP Semiconductor Terms & Conditions available at https://www.asapsemi.com/terms-conditions.aspx . All United States Government and Department of Defense bids are quoted as CAGE code 6RE77 from ASAP Semiconductor’s Anaheim, California facility. Any quotation from ASAP Semiconductor without 6RE77 is void.
How to Get Started on Procurement
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9540-01-478-9726 Item PartTypeName: 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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