To receive competitive purchasing options on part number CVC10010-1004GA by Triumph Aerostructures Llc, look no further than NSN Direct. For your reference, this item has the NSN 9540-01-435-5246 and is listed with the description “Beam Structural.” If this matches your needs, we encourage you to fill out the partially-completed quote request form on this page to kick off procurement. By providing comprehensive information about your requirements, such as your desired quantity, pricing, and fulfillment speed, our experts can formulate the most fitting solutions for you. We want to ensure that this process is quick and effortless, so we routinely respond to requests within 15 minutes of receiving and reviewing them.
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In addition to our streamlined quotation service, we also aim to make the process of finding products simple. As such, if you require other Triumph Aerostructures Llc parts produced under the CAGE Code 80378, you can peruse our manufacturer or CAGE Code catalogs, or use our search engine and filters. Furthermore, if you want to locate items similar to part number CVC10010-1004GA, you can glean from the first four digits of its NSN 9540-01-435-5246 that it belongs to the FSC 9540 Structural Shapes Nonferrous Base Metal. This being said, do not hesitate to request quotes on part number CVC10010-1004GA and any other NSN parts that we feature to experience unrivaled procurement.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-435-5246 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014355246 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| CVC10010-1004GA | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.000 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.440 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.440 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.440 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.475 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.475 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.380 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.380 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 4.950 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBD | FIRST TIP INNER RADIUS | 0.062 INCHES NOMINAL |
| CNBJ | FIRST TIP OUTER RADIUS | 0.062 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | ANNEALED |
| MATT | MATERIAL | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | COMPOSITION AB-1 AND CONDITION ANNEALED |
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