You are currently exploring our in-stock options for part number 1MA160B04-10297 with the NSN 9540013390389. This product is listed with the description “Beam Structural” and is manufactured by Boeing Company The. 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 1MA160B04-10297 is listed alongside the NSN 9540-01-339-0389 and belongs to the FSC 9540 Structural Shapes Nonferrous Base Metal. Additionally, it is also under the CAGE Code 76301, which is assigned to Boeing Company The. 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 1MA160B04-10297 seamless.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-339-0389 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 013390389 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1MA160B04-10297 | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.080 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE END |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| MATT | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/3,ALLOY 2024 |
| AARN | FABRICATION METHOD | EXTRUDED |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.080 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.200 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.530 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.080 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.250 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 0.396 POUNDS PER LINEAR FOOT |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CSMZ | LEFT TOP INSIDE ANGLE | 89.0 DEGREES NOMINAL |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 8511 TEMPER |
| ABKW | OVERALL HEIGHT | 1.630 INCHES NOMINAL |
| ABRY | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| AGAV | END ITEM IDENTIFICATION | F-15 AIRCRAFT |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.090 INCHES NOMINAL |
| CRZC | RIGHT TOP INSIDE ANGLE | 91.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | T-8511 SOLUTION HEAT TREATED |
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