Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number CVC10010-1020GA, a Triumph Aerostructures Llc item with the NSN 9540014355244 that is listed alongside the description “Beam Structural.” If you are interested in part number CVC10010-1020GA and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number CVC10010-1020GA is specifically listed with the NSN 9540-01-435-5244, and this code can be used to determine that it falls under FSC 9540 Structural Shapes Nonferrous Base Metal. Additionally, while tracing back to Triumph Aerostructures Llc, this NSN part was specifically produced under CAGE Code 80378. With our services and dedication to simple procurement in mind, get started with us today!
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9540-01-435-5244 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014355244 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
CVC10010-1020GA | 5 | 2 | 3 |
MRC | Criteria | Characteristic |
---|---|---|
CNQJ | Second Tip Relationship To First Tip | IDENTICAL |
CNQL | Third Tip Relationship To Preceding Tips | IDENTICAL W/FIRST TIP |
MATT | Material | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
HEAT | Heat Treatment | ANNEALED |
ADXR | Left Side Top Flange Thickness | 0.650 INCHES NOMINAL |
ZZZT | Nondefinitive Spec/Std Data | COMPOSITION AB-1 AND CONDITION ANNEALED |
ABRY | Length | 12.000 FEET NOMINAL |
BPXG | Right Side Top Flange Distance To Center Of Both Flanges | 1.275 INCHES NOMINAL |
MRC | Decoded Requirement | Clear Text Reply |
ABKW | Overall Height | 8.800 INCHES NOMINAL |
AGTA | Basic Shape Style | T SHAPE |
AJJP | Leg Thickness | 0.680 INCHES NOMINAL |
CRZC | Right Top Inside Angle | 90.0 DEGREES NOMINAL |
BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 1.275 INCHES NOMINAL |
BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.380 INCHES NOMINAL |
ADXS | Right Side Top Flange Thickness | 0.650 INCHES NOMINAL |
BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.380 INCHES NOMINAL |
BQJG | Top Flange Width | 2.550 INCHES NOMINAL |
CNBD | First Tip Inner Radius | 0.062 INCHES NOMINAL |
AARN | Fabrication Method | EXTRUDED |
CSMZ | Left Top Inside Angle | 90.0 DEGREES NOMINAL |
CMZY | First Tip Style | SQUARE W/ INNER AND OUTER CORNER RADII |
CNBJ | First Tip Outer Radius | 0.062 INCHES NOMINAL |
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