Aerospace Performance Parts is pleased to offer immediate purchasing options for Triumph Aerostructures Llc part number CVC10010-111CA, which you have taken interest in. This Beam Structural item is listed alongside the NSN 9540-01-471-8266 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number CVC10010-111CA or any other FSC 9540 Structural Shapes Nonferrous Base Metal components we carry from Triumph Aerostructures Llc under CAGE Code 80378, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 9540-01-471-8266 part number CVC10010-111CA today, knowing we will support all your operational needs with care.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-471-8266 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014718266 | 0 | N | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | U | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| CVC10010-111CA | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| ABKW | OVERALL HEIGHT | 1.950 INCHES NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.200 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.750 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.200 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 3.500 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBJ | FIRST TIP OUTER RADIUS | 0.032 INCHES NOMINAL |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | O-ANNEALED |
| AARN | FABRICATION METHOD | EXTRUDED |
| ABRY | LENGTH | 20.000 FEET NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.200 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.200 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.750 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.200 INCHES NOMINAL |
| BRFD | WEIGHT PER UNIT MEASURE | 1.284 POUNDS PER LINEAR FOOT |
| CNBD | FIRST TIP INNER RADIUS | 0.032 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FEAT | SPECIAL FEATURES | WS IS AIRCRAFT,B-2 BOMBER (ATB) |
| MATL | MATERIAL | ALUMINUM ALLOY, 7075 |
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