You are currently exploring our in-stock options for part number CVC10010-161GA with the NSN 9540014693308. This product is listed with the description “Beam Structural” and is manufactured by Triumph Aerostructures Llc. If you are looking to purchase this part, we encourage you to complete and submit the RFQ form below with as much information as you can provide, such as your desired quantity, budget, shipping time frame, and more. Within 15 minutes of receiving and reviewing your submission, one of our experts will reach out with a quote that is tailored to your needs.
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We supply all relevant information alongside the listings on our website, that way you know you are always getting the exact item you require. For example, part number CVC10010-161GA is listed alongside the NSN 9540-01-469-3308 and belongs to the FSC 9540 Structural Shapes Nonferrous Base Metal. Additionally, it is also under the CAGE Code 80378, which is assigned to Triumph Aerostructures Llc. At Aerospace Procurement, you can trust that each product in our inventory is up to industry standards, as we are committed to various quality assurance practices. For example, we uphold a strict NO CHINA SOURCING pledge to ensure that each part is shipped out alongside its manufacturer trace documentation and qualifying certifications. These practices and more allow us to operate with AS9120B, ISO 9001:2015, and FAA AC 00-56B accreditation. Get in contact with us today to see how we can make the procurement process for part number CVC10010-161GA seamless.
| 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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