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 CVC10010-161GA, a Triumph Aerostructures Llc component we offer that is presented with the NSN 9540-01-469-3308 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 CVC10010-161GA is manufactured by Triumph Aerostructures Llc under the CAGE Code 80378. Additionally, by using the initial digits of the NSN 9540-01-469-3308, 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 CVC10010-161GA at your earliest convenience.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-469-3308 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014693308 | 0 | N | A | |
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | A | 0 | |||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| CVC10010-161GA | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| CNPS | First Tip Thickness | 0.990 INCHES MINIMUM AND 1.010 INCHES MAXIMUM |
| CNPT | Second Tip Thickness | 0.990 INCHES MINIMUM AND 1.010 INCHES MAXIMUM |
| MRC | Decoded Requirement | Clear Text Reply |
| CSMZ | Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| HEAT | Heat Treatment | ANNEALED |
| ABKW | Overall Height | 4.440 INCHES NOMINAL |
| ADXR | Left Side Top Flange Thickness | 0.115 INCHES MINIMUM AND 0.135 INCHES MAXIMUM |
| ABRY | Length | 18.800 INCHES MINIMUM AND 18.820 INCHES MAXIMUM |
| BPXG | Right Side Top Flange Distance To Center Of Both Flanges | 2.560 INCHES NOMINAL |
| MATT | Material | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
| AGTA | Basic Shape Style | T SHAPE |
| AJJP | Leg Thickness | 0.115 INCHES MINIMUM AND 0.135 INCHES MAXIMUM |
| CRZC | Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 2.560 INCHES NOMINAL |
| BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.110 INCHES MINIMUM AND 0.130 INCHES MAXIMUM |
| ADXS | Right Side Top Flange Thickness | 0.115 INCHES MINIMUM AND 0.135 INCHES MAXIMUM |
| BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.110 INCHES MINIMUM AND 0.130 INCHES MAXIMUM |
| BQJG | Top Flange Width | 5.120 INCHES NOMINAL |
| FEAT | Special Features | ALONG LENGTH FLANGES ON BOTH SIDES NARROW FROM NORMAL WIDTH FROM CENTER (AT 4.04 IN. FROM FIRST TIP) TO 1.01 IN. FROM CENTER (AT 6.73 IN. FROM FIRST TIP); FLANGES WIDEN FROM 1.01 IN. FROM CENTER (AT 13.18 IN. FROM FIRST TIP) TO NORMAL WIDTH (AT 15.88 IN. FROM FIRST TIP); WEAPONS SYSTEM IS AIRCRAFT, B-2 BOMBER (ATB) |
| CNPD | First Tip Taper Length | 0.690 INCHES MINIMUM AND 0.710 INCHES MAXIMUM |
| CNQK | Second Tip Style | LEFT TAPER LENGTH |
| AARN | Fabrication Method | EXTRUDED |
| CMZY | First Tip Style | RIGHT TAPER LENGTH |
| CNPF | Second Tip Taper Length | 0.690 INCHES MINIMUM AND 0.710 INCHES MAXIMUM |
| CNQJ | Second Tip Relationship To First Tip | NOT IDENTICAL |
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