Aerospace Engineering Solutions is proud to offer immediate purchasing options on Triumph Aerostructures Llc part number CVC10010-145GA, a Beam Structural product we carry that is listed with the NSN 9540-01-444-3319 for ease of identification. If you would like to learn more about this item, be sure to complete the Request for Quote (RFQ) form provided on this page. By including essential details like your target price, desired quantity, and expected fulfillment timeline, you are ensured a fully customized quote from our team.
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For your reference, this product is traceable to Triumph Aerostructures Llc through the CAGE Code 80378, as well as categorized under FSC 9540 Structural Shapes Nonferrous Base Metal based on the first four digits of the NSN 9540-01-444-3319. Using such information, you can easily narrow down exact items of need for an ease of procurement. With our quotation service in mind, be sure to submit a completed form when you are ready to begin. Should you wish to speak with one of our representatives to discuss services, you can also give us a call or email at your convenience. With all that we offer, choose Aerospace Engineering Solutions for part number CVC10010-145GA and other NSN items of need.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-444-3319 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014443319 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| MIL-T-81556 | 5 | 1 | 4 |
| MRC | Criteria | Characteristic |
|---|---|---|
| CSMZ | Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| HEAT | Heat Treatment | ANNEALED |
| ADXR | Left Side Top Flange Thickness | 0.150 INCHES NOMINAL |
| MRC | Decoded Requirement | Clear Text Reply |
| ABRY | Length | 12.000 FEET NOMINAL |
| BPXG | Right Side Top Flange Distance To Center Of Both Flanges | 1.075 INCHES NOMINAL |
| ABKW | Overall Height | 1.060 INCHES NOMINAL |
| MATT | Material | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 (6AL-4V) |
| AGTA | Basic Shape Style | T SHAPE |
| AJJP | Leg Thickness | 0.090 INCHES NOMINAL |
| CRZC | Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 1.075 INCHES NOMINAL |
| BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.125 INCHES NOMINAL |
| ADXS | Right Side Top Flange Thickness | 0.150 INCHES NOMINAL |
| ZZZT | Nondefinitive Spec/Std Data | COMPOSITION AB-1 (6AL-4V) AND CONDITION ANNEALED |
| BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.125 INCHES NOMINAL |
| BQJG | Top Flange Width | 2.150 INCHES NOMINAL |
| CNQJ | Second Tip Relationship To First Tip | IDENTICAL |
| 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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