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Quality guaranteed We sell only warrantied and traceable partsMfg Part Number: CVC10010-129CA
Alternate P/N: CVC10010129CA
NSN : 9540-01-437-2661
NIIN : 014372661
Manufacturer: Vought Aircraft Industries Inc
Item Name : Beam Structural
In our inventory, we have more than two billion new and obsolete NSN part like CVC10010-129CA. Aviation Sphere can offer an impressive selection of NSN parts. This includes parts like CVC10010-129CA Beam Structural from manufacturer Vought Aircraft Industries Inc and many more, all of which are available with short lead times and competitive prices. For parts not in our inventory, our dedicated account managers can help you track them down through our international supply chain network that extends across the United States, Canada, and the United Kingdom. Furthermore, Aviation Sphere is an AS9120B, ISO 9001:2015, and FAA AC 0056B accredited business, as well as the only independent distributor with a strict No China Sourcing Pledge, allowing us to ensure that each part part like CVC10010-129CA, you purchase from us is fully traceable or comes directly from its manufacturer.
Our website offers a number of parametric search capabilities, one of which allows you to search specifically for NSN part like CVC10010-129CA. This means you can quickly sort through National Stock Numbers such as 9540014372661 and find parts from quality manufacturers like Vought Aircraft Industries Inc and many others. To begin the purchasing process immediately, submit an RFQ today. Our team of dedicated account managers is standing by and will respond to all inquiries in 15 minutes or less.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-437-2661 Item Description: Beam Structural | 9540 | 014372661 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| Cvc10010-129ca | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AJJP | LEG THICKNESS | 0.110 INCHES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 2.750 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBD | FIRST TIP INNER RADIUS | 0.020 INCHES NOMINAL |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER T0 |
| CNBJ | FIRST TIP OUTER RADIUS | 0.020 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| ABKW | OVERALL HEIGHT | 1.350 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.375 INCHES NOMINAL |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.375 INCHES NOMINAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.110 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.110 INCHES NOMINAL |
| AARN | FABRICATION METHOD | EXTRUDED |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
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