Thank you for considering Boeing Company The part number L2102057 1RS, a component we stock that is further identified by the NSN 9540-01-443-7365 and product description “Beam Structural.” This item is currently available for purchase on our website today, and you can obtain a tailored quote at any time by completing the form on this page. To help us provide the best solution, please include critical details like your quantity requirements, target pricing, and delivery preferences within the submitted request. Once we receive your form, our team will promptly review provided information and respond with a quote that aligns with your needs.
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Alongside part number L2102057 1RS, we encourage you to explore other offerings we carry from Boeing Company The that have been produced under CAGE Code 43999, as well as similar products classified under FSC 9540 Structural Shapes Nonferrous Base Metal that may suit your projects. We can help you obtain pricing on all items that you are interested in, securing the most optimal solution for you. We are also happy to discuss any requirements that you may have, presenting specialized options for many restrictions and needs alike. With our services in mind, please submit your request for part number L2102057 1RS today and discover why Marine Defence Parts is a trusted partner for naval and defense procurement.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9540-01-443-7365 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014437365 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
200062001-01 | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | ANY ACCEPTABLE |
ABRY | LENGTH | 23.970 INCHES MINIMUM AND 24.030 INCHES MAXIMUM |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.115 INCHES MINIMUM AND 0.135 INCHES MAXIMUM |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.115 INCHES MINIMUM AND 0.135 INCHES MAXIMUM |
AGAV | III END ITEM IDENTIFICATION | B-1B AIRCRAFT |
AGTA | BASIC SHAPE STYLE | T SHAPE |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.760 INCHES MINIMUM AND 0.780 INCHES MAXIMUM |
BQJG | TOP FLANGE WIDTH | 1.670 INCHES MINIMUM AND 1.690 INCHES MAXIMUM |
CMZY | FIRST TIP STYLE | SQUARE END |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
CRZC | RIGHT TOP INSIDE ANGLE | 95.2167 DEGREES MINIMUM AND 96.2167 DEGREES MAXIMUM |
CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | FLANGE,RS |
FEAT | SPECIAL FEATURES | USED IN THE HS PROJECT. THE /1RS IS USED TO MAKE P/N -003/005/007/009/0013/015/017/019/023/025/027 |
MATT | MATERIAL | ALUMINUM ALLOY 7075 |
ZZZV | III FSC APPLICATION DATA | STRUCTURAL SHAPES |
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