Mfg Part Number: CVC10011-69CA
Alternate P/N: CVC1001169CA
NSN : 9540-01-429-3018
NIIN : 014293018
CAGE Code : 80378
Manufacturer: Triumph Aerostructures Llc
Item Name : Beam Structural
Here at Internet For Aviation, we have CVC10011-69CA Beam Structural from Triumph Aerostructures Llc, as well as a variety of other parts from reliable manufacturers. As the only independent distributor with a No China Sourcing policy, we go to great lengths to ensure that we source responsibly when it comes to certified standard items. If you’re in need of a specific CVC10011-69CA to aid you in your aircraft repair capabilities, simply search by NSN part number, NSN or Cage Code on our parts directory. Submit an instant RFQ and a representative will get back to you in as little as 15 minutes.
Note : We Will Not Share Your Information To Any Third Parties.
We pride ourselves in our abilities to deliver quality superior grade aviation parts in a timely schedule. Thanks to the various supply chain locations that we have across the United States. We can execute fast shipping times that outpace our competitors. Unlike other competitors, we can promise same day shipping and delivery right to the very place you need. We’re leaders in our industry thanks to our parts streamlining process which includes quick stock and acquisition of the certified product and fast shipping. For whatever needs you have, be they Beam Structural and CVC10011-69CA parts, we can procure and deliver in a schedule that fits with you! Contact us today for an immediate quote!
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-429-3018 Item Description: Beam Structural | 9540 | 014293018 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| CVC10011-69CA | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| MATT | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
| BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.120 INCHES NOMINAL |
| CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.161 INCHES NOMINAL |
| AARN | FABRICATION METHOD | EXTRUDED |
| ABRY | LENGTH | 12.000 FEET NOMINAL |
| ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.161 INCHES NOMINAL |
| AJJP | LEG THICKNESS | 0.161 INCHES NOMINAL |
| BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 5.740 INCHES NOMINAL |
| BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.120 INCHES NOMINAL |
| BQJG | TOP FLANGE WIDTH | 8.480 INCHES NOMINAL |
| CNBD | FIRST TIP INNER RADIUS | 0.030 INCHES NOMINAL |
| CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| MATL | MATERIAL | ALUMINUM ALLOY, QQ-A-200/11, ALLOY 7075 |
| CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 7075 AND TEMPER 0 |
| ABKW | OVERALL HEIGHT | 3.360 INCHES NOMINAL |
| AGTA | BASIC SHAPE STYLE | T SHAPE |
| BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.740 INCHES NOMINAL |
| CMZY | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
| CNBJ | FIRST TIP OUTER RADIUS | 0.030 INCHES NOMINAL |
| HEAT | HEAT TREATMENT | O-ANNEALED |
Semiconductor's Certifications and Memberships
 |
“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”. |
We Hope that You'll Choose Buy Aviation Parts as Your Quick and Convenient Parts Distributor In the Future.
Request for Quote
