Thank you for taking interest in Triumph Aerostructures Llc part number CVC10011-1017MP, which is listed with the NSN 9540-01-456-6379 and a product description of “Beam Structural.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
Note : We Will Not Share Your Information To Any Third Parties.
Alongside part number CVC10011-1017MP, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Beam Structural part with the NSN 9540-01-456-6379. For example, you can browse other Triumph Aerostructures Llc components that were produced under CAGE Code 80378 or listings that belong to FSC 9540 Structural Shapes Nonferrous Base Metal with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number CVC10011-1017MP and other desired offerings on Aerospace Spare.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
9540-01-456-6379 Item PartTypeName: BEAM,STRUCTURAL | 9540 | 014566379 | 0 | N | ||
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
U | A | 0 | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
MIL-T-81556 | 5 | 1 | 4 |
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-4 |
HEAT | Heat Treatment | DUPLEX ANNEALED |
ADXR | Left Side Top Flange Thickness | 0.870 INCHES NOMINAL |
ZZZT | Nondefinitive Spec/Std Data | COMPOSITION 6AL-2SN-4ZR-2MO AND CONDITION DUPLEX ANNEALED |
ABRY | Length | 12.000 FEET NOMINAL |
BPXG | Right Side Top Flange Distance To Center Of Both Flanges | 1.735 INCHES NOMINAL |
AGTA | Basic Shape Style | T SHAPE |
AJJP | Leg Thickness | 0.510 INCHES NOMINAL |
CRZC | Right Top Inside Angle | 90.0 DEGREES NOMINAL |
BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 1.695 INCHES NOMINAL |
BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.380 INCHES NOMINAL |
ADXS | Right Side Top Flange Thickness | 0.870 INCHES NOMINAL |
BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.380 INCHES NOMINAL |
MRC | Decoded Requirement | Clear Text Reply |
BQJG | Top Flange Width | 3.430 INCHES NOMINAL |
CNBD | First Tip Inner Radius | 0.062 INCHES NOMINAL |
ABKW | Overall Height | 2.860 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 |
If You’re Ever Looking for NSN parts Or Have an Aircraft On Ground Situation, Don’t forget That We offer Competitive Pricing and Guaranteed On-Time Delivery.
Request for Quote