Mfg Part Number: CVC10010-121GA
Alternate P/N: CVC10010121GA
NSN : 9540-01-463-0446
NIIN : 014630446
CAGE Code : 80378
Manufacturer: Triumph Aerostructures Llc
Item Name : Beam Structural
If you’re in need of NSN parts, Purchasing Synergy is the ultimate source. As an ASAP Semiconductor company, we have access to a vast and diverse inventory of parts and components like CVC10010-121GA for the aerospace, civil aviation, defense, electronics, and industrial markets. This includes parts such as Beam Structural from Triumph Aerostructures Llc with Cage Code 80378 as well as part numbers like CVC10010-121GA and FSC 9540 Structural Shapes Nonferrous Base Metal with014630446. Purchasing Synergy has more than two billion new and obsolete parts readily available with short lead times and competitive prices and, as we are an AS9120B, ISO 9001:2015, and FAA AC 00-56B accredited business, and the only independent distributor with a No China Sourcing Pledge, each part we sell is fully traceable or comes directly from the manufacturer.
Our website offers a range of parametric search capabilities which allow our customers to search for parts through a number like CVC10010-121GA and filters, one of which is National Stock Number, or NSN. A National Stock Number is an identifier applied to any item of supply that is repeatedly procured, stocked, stored, issued, and used throughout the federal supply system. Purchasing Synergy has a broad selection of NSN parts such as 9540014630446 from manufacturers like Triumph Aerostructures Llc. To begin the purchasing process immediately, submit an RFQ today.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9540-01-463-0446 Item Description: Beam Structural | 9540 | 014630446 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
Cvc10010-121ga | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.060 INCHES NOMINAL |
ABRY | LENGTH | 12.000 FEET NOMINAL |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.080 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.080 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.080 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.500 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.500 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.120 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.120 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 3.000 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE END |
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 |
MATL | MATERIAL | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | COMPOSITION AB-1 AND CONDITION ANNEALED |
AARN | FABRICATION METHOD | EXTRUDED |
ABKW | OVERALL HEIGHT | 1.060 INCHES NOMINAL |
ABRY | LENGTH | 12.000 FEET NOMINAL |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.080 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.080 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | T SHAPE |
AJJP | LEG THICKNESS | 0.080 INCHES NOMINAL |
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.500 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.500 INCHES NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.120 INCHES NOMINAL |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.120 INCHES NOMINAL |
BQJG | TOP FLANGE WIDTH | 3.000 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | SQUARE END |
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 |
MATL | MATERIAL | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
ZZZT | NONDEFINITIVE SPEC/STD DATA | COMPOSITION AB-1 AND CONDITION ANNEALED |
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