You are currently exploring our in-stock options for part number CVC10010-1004GA with the NSN 9540014355246. 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 CVC10010-1004GA is listed alongside the NSN 9540-01-435-5246 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 CVC10010-1004GA seamless.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9540-01-435-5246 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014355246 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
CVC10010-1004GA | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 2.000 INCHES NOMINAL |
ABRY | LENGTH | 12.000 FEET NOMINAL |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.440 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.440 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.440 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.475 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.475 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.380 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.380 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 4.950 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
CNBD | FIRST TIP INNER RADIUS | 0.062 INCHES NOMINAL |
CNBJ | FIRST TIP OUTER RADIUS | 0.062 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
HEAT | HEAT TREATMENT | ANNEALED |
MATT | MATERIAL | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | COMPOSITION AB-1 AND CONDITION ANNEALED |
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