| Part Number: CVC10012-1005MP | Manufacturer: Triumph Aerostructures Llc | NSN: 9540-01-449-1747 (9540014491747) | Item Name : beam structural | CAGE Code: 80378 | FSC: 9540 Structural Shapes Nonferrous Base Metal | Alternate P/N : CVC100121005MP |
The CVC10012-1005MP with NSN 9540014491747 is available in stock! Thanks for your interest in AerospaceSimplified.com. CVC10012-1005MP, Beam Structural part is manufactured by Triumph Aerostructures Llc. Want to request a quote for it? Please fill the form below with contact details, expected delivery date, and quantity.
AerospaceSimplified.com is owned and operated by ASAP Semiconductor – a leading distributor of Triumph Aerostructures Llc NSN parts in US. We stock ready-to-ship NSN parts from over 5000 manufacturers. We have headquarters in California, We can ship products the same day. A dedicated sales executive will contact you within 15 minutes of receiving the RFQ for CVC10012-1005MP part. For even faster service you can call us at +1-714-705-4780. For multiple part number, you can email us your Bill of Materials (BOM) at sales@aerospacesimplified.com
For safe and secure sourcing on the go, download the ASAP Semiconductor app on Google Play or the Apple App Store.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-449-1747 Item Description: Beam Structural | 9540 | 014491747 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| Cvc10012-1005mp | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.700 INCHES NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 1.190 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 1.190 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.600 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.770 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 3.430 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.300 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.300 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 5.200 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 | 80.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 100.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | ANNEALED |
| MATL | MATERIAL | TITANIUM ALLOY, MIL-T-81556 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | COMPOSITION 6AL-2SN-4ZR-2MO AND CONDITION ANNEALED |
| AARN | FABRICATION METHOD | EXTRUDED |
| ABKW | OVERALL HEIGHT | 2.700 INCHES NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 1.190 INCHES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 1.190 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| AJJP | LEG THICKNESS | 0.600 INCHES NOMINAL |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.770 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 3.430 INCHES NOMINAL |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.300 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.300 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 5.200 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 | 80.0 DEGREES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 100.0 DEGREES NOMINAL |
| HEAT | HEAT TREATMENT | ANNEALED |
| MATL | MATERIAL | TITANIUM ALLOY, MIL-T-81556 |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | COMPOSITION 6AL-2SN-4ZR-2MO AND CONDITION ANNEALED |
All Orders are Fulfilled in the U.S.A.
All shipments must comply with U.S.A export laws.
No exceptions.
The only independent distributor
with a NO CHINA SOURCING Pledge
“We Proudly Support Intrepid Fallen Heroes Fund that serves United States Military Personal experiencing the Invisible Wounds of War : Traumatic Brain Injury (TBI) and Post Traumatic Stress (PTS). Please visit website (www.fallenheroesfund.org) and help in their valiant effort”.
Glad You Chose Aerospace Simplified as Your Parts Distributor Website today. We Hope that You Will Remember Us the Next Time You’re Looking for Required Parts.
Request for Quote
