Part Number : HS1006AA41B0027 | Manufacturer : Boeing Company The | ||
NSN : 9540-01-478-9727 (9540014789727) | |||
Item Name : Beam Structural | CAGE Code : 8V613 | ||
NIIN : 01-478-9727 (014789727) | |||
FSC Code : 9540 Structural Shapes Nonferrous Base Metal | |||
FSG Code : 95 Metal Bars Sheets and Shapes | |||
INC Code : 37018 | |||
NCB Code : 01 | Country : USA |
Thank you for taking an interest in part number HS1006AA41B0027, that of which is listed with the description Beam Structural; Manufactured by Boeing Company The and listed alongside the NSN 9540014789727, part number HS1006AA41B0027 is available for immediate purchase on our website. As such, to learn more about this offering while receiving a competitive quote for your comparisons, be sure to fill out and submit the RFQ form presented on this page. Within 15 minutes of us receiving and reviewing a completed form, a member of our staff will contact you to present a tailored solution for your comparisons.
Part Number : HS1006AA41B0027 | Manufacturer : Boeing Company The | ||
NSN Number : 9540-01-478-9727 (9540014789727) | |||
Item Name : Beam Structural | CAGE Code : 8V613 | ||
NIIN : 014789727 | |||
FSC CODE : 9540 Structural Shapes Nonferrous Base Metal |
Thank you for taking an interest in part number HS1006AA41B0027, that of which is listed with the description Beam Structural; Manufactured by Boeing Company The and listed alongside the NSN 9540014789727, part number HS1006AA41B0027 is available for immediate purchase on our website. As such, to learn more about this offering while receiving a competitive quote for your comparisons, be sure to fill out and submit the RFQ form presented on this page. Within 15 minutes of us receiving and reviewing a completed form, a member of our staff will contact you to present a tailored solution for your comparisons.
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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