You are currently exploring our in-stock options for part number AMS4617 with the NSN 9540014699501. This product is listed with the description “Beam Structural” and is manufactured by Sae International. If you are looking to purchase this part, we encourage you to complete and submit the RFQ form below with as much information as you can provide, such as your desired quantity, budget, shipping time frame, and more. Within 15 minutes of receiving and reviewing your submission, one of our experts will reach out with a quote that is tailored to your needs.
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We supply all relevant information alongside the listings on our website, that way you know you are always getting the exact item you require. For example, part number AMS4617 is listed alongside the NSN 9540-01-469-9501 and belongs to the FSC 9540 Structural Shapes Nonferrous Base Metal. Additionally, it is also under the CAGE Code 0U583, which is assigned to Sae International. At Aerospace Procurement, you can trust that each product in our inventory is up to industry standards, as we are committed to various quality assurance practices. For example, we uphold a strict NO CHINA SOURCING pledge to ensure that each part is shipped out alongside its manufacturer trace documentation and qualifying certifications. These practices and more allow us to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. Get in contact with us today to see how we can make the procurement process for part number AMS4617 seamless.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9540-01-469-9501 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014699501 | 0 | N | A | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | U | 0 | |||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
AMS10140-1404 | 5 | 1 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
ABKW | OVERALL HEIGHT | 1.500 INCHES NOMINAL |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | ACFT CEN SEC |
AJJB | FIRST TIP RADIUS | 0.010 INCHES NOMINAL |
BMPR | LEFT SIDE BOTTOM FLANGE THICKNESS | 0.125 INCHES NOMINAL |
BPXF | LEFT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
BPXH | RIGHT SIDE BOTTOM FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
BPXK | FILLET RADIUS WHERE BOTTOM LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
BPXM | FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 2.500 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | LEFT QUARTER RADIUS |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
CTBR | LEFT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
FEAT | SPECIAL FEATURES | WEAPONS SYSTEM IS AIRCRAFT, B-2 BOMBER (ATB) |
ZZZK | SPECIFICATION/STANDARD DATA | 81348-QQ-A-200/11E/CANCELED/ GOVERNMENT SPECIFICATION AND 99237-AND10140 GOVERNMENT STANDARD |
AARN | FABRICATION METHOD | EXTRUDED |
ABRY | LENGTH | 32.900 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | I SHAPE |
BMPQ | RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.125 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 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 |
BPXN | WEB FLANGE THICKNESS | 0.125 INCHES NOMINAL |
BQJH | BOTTOM FLANGE WIDTH | 2.500 INCHES NOMINAL |
CMZZ | SECOND TIP RADIUS | 0.010 INCHES NOMINAL |
CNQK | SECOND TIP STYLE | RIGHT QUARTER RADIUS |
CNQN | FOURTH TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/SECOND TIP |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
CWKK | RIGHT BOTTOM INSIDE ANGLE | 90.0 DEGREES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11 |
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