Rotable Parts Exchange serves as a comprehensive source for military products, aerospace equipment, and Beam Structural items. You have expressed particular interest in part number CVC10031-16CA, a Triumph Aerostructures Llc component we offer that is presented with the NSN 9540-01-475-0888 for straightforward identification and procurement. By completing and submitting the Request for Quote form provided on this page, you can obtain pricing details on this NSN part for your comparisons. Once our staff members receive and review your submitted information, a dedicated account manager will directly contact you with a response within 15 minutes or less.
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We strive to streamline the purchasing process and simplify it as much as possible, which includes providing detailed listings for all components to help customers pinpoint their exact needs. For instance, part number CVC10031-16CA is manufactured by Triumph Aerostructures Llc under the CAGE Code 80378. Additionally, by using the initial digits of the NSN 9540-01-475-0888, you can discover that this component is associated with the FSC 9540 Structural Shapes Nonferrous Base Metal. If you have any specific questions about our database, you may always give us a call or email, as we would be delighted to assist you however we can. Otherwise, we encourage you to secure a quote for part number CVC10031-16CA at your earliest convenience.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-475-0888 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014750888 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| CVC10031-16CA | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| CSMZ | Left Top Inside Angle | 11.0 DEGREES NOMINAL |
| CWKK | Right Bottom Inside Angle | 169.0 DEGREES NOMINAL |
| ADXR | Left Side Top Flange Thickness | 0.055 INCHES NOMINAL |
| ABRY | Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| MRC | Decoded Requirement | Clear Text Reply |
| BMPR | Left Side Bottom Flange Thickness | 0.015 INCHES NOMINAL |
| AGTA | Basic Shape Style | I SHAPE |
| BPXN | Web Flange Thickness | 0.055 INCHES NOMINAL |
| MDCL | Material Document And Classification | QQ-A-430, ALLOY 7075 FED SPEC 1ST MATERIAL RESPONSE |
| BMPQ | Right Side Bottom Flange Thickness | 0.015 INCHES NOMINAL |
| BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 0.630 INCHES NOMINAL |
| CTBR | Left Bottom Inside Angle | 11.0 DEGREES NOMINAL |
| BPXH | Right Side Bottom Flange Distance To Center Of Both Flanges | 0.680 INCHES NOMINAL |
| ADXS | Right Side Top Flange Thickness | 0.055 INCHES NOMINAL |
| BPXF | Left Side Bottom Flange Distance To Center Of Both Flanges | 0.630 INCHES NOMINAL |
| BPXG | Right Side Top Flange Distance To Center Of Both Flanges | 0.680 INCHES NOMINAL |
| BQJG | Top Flange Width | 1.310 INCHES NOMINAL |
| BQJH | Bottom Flange Width | 1.310 INCHES NOMINAL |
| AGAV | End Item Identification | INTERMEDIATE; AIRCRAFT B-2 BOMBER (ATB) |
| CRZC | Right Top Inside Angle | 169.0 DEGREES NOMINAL |
| ABKW | Overall Height | 2.050 INCHES NOMINAL |
| AARN | Fabrication Method | ANY ACCEPTABLE |
| MATT | Material | ALUMINUM ALLOY 7075 |
| CNQJ | Second Tip Relationship To First Tip | IDENTICAL |
| CMZY | First Tip Style | SQUARE END |
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