We appreciate your interest in Triumph Aerostructures Llc part number CVC10012-188GA, which is currently ready for procurement here on Prompt Aerospace. For your reference, part number CVC10012-188GA is listed with the NSN 9540-01-435-8308 and description “Beam Structural.” If this is the item you are seeking and you would like to request a quote for your comparisons, simply complete the form below with information like your desired quantity, budget, and anticipated fulfillment timeframe. We regularly respond to requests within 15 minutes of receiving them, using the details we are offered to curate the most ideal purchasing options.
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If you want to explore other items produced by Triumph Aerostructures Llc under the CAGE Code 80378 or that similarly fall under the FSC 9540 Structural Shapes Nonferrous Base Metal, keep in mind that since we list everything with relevant information, you can easily locate related part numbers using our search engine or catalogs. We also excel at tracking down parts with long lead times or that are generally hard to find, meaning that we can serve you even if you do not see exactly what you need on our website. With all of this being said, we are ready to help you source any of the NSN 9540-01-435-8308 parts and Beam Structural items your operations require, so request a quote today.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-435-8308 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014358308 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| CVC10012-188GAX144 | 5 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| CSMZ | Left Top Inside Angle | 55.0 DEGREES NOMINAL |
| HEAT | Heat Treatment | ANNEALED |
| ADXR | Left Side Top Flange Thickness | 0.320 INCHES NOMINAL |
| ABRY | Length | 12.000 FEET NOMINAL |
| BPXG | Right Side Top Flange Distance To Center Of Both Flanges | 1.800 INCHES NOMINAL |
| MATT | Material | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
| AGTA | Basic Shape Style | T SHAPE |
| AJJP | Leg Thickness | 0.150 INCHES NOMINAL |
| CRZC | Right Top Inside Angle | 125.0 DEGREES NOMINAL |
| BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 1.360 INCHES NOMINAL |
| BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.125 INCHES NOMINAL |
| ADXS | Right Side Top Flange Thickness | 0.320 INCHES NOMINAL |
| ZZZT | Nondefinitive Spec/Std Data | COMPOSITION AB-1 AND CONDITION ANNEALED |
| BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.125 INCHES NOMINAL |
| BQJG | Top Flange Width | 3.160 INCHES NOMINAL |
| CNQJ | Second Tip Relationship To First Tip | IDENTICAL |
| ABKW | Overall Height | 2.910 INCHES NOMINAL |
| MRC | Decoded Requirement | Clear Text Reply |
| AARN | Fabrication Method | EXTRUDED |
| CMZY | First Tip Style | SQUARE END |
| CNQL | Third Tip Relationship To Preceding Tips | IDENTICAL W/FIRST TIP |
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