| Mfg Part Number: CVC10011-71GA | Alternate P/N: CVC1001171GA | NSN : 9540-01-435-5694 |
| NIIN : 014355694 | CAGE Code : 80378 | Manufacturer: Triumph Aerostructures Llc |
| Item Name : Beam Structural | FSC : 9540 Structural Shapes, Nonferrous Base Metal |
Thank you for choosing Aircraft Parts Supplier for all your operational needs. You have reached our NSN RFQ Page which features our in-demand NSN 9540-01-435-5694 parts and components such as Beam Structural manufactured by Triumph Aerostructures Llc. Some of these items include part number CVC10011-71GA, and various others, all of which have been subjected to a number of quality assurance measures, tests, verifications, and assessments. At Aircraft Parts Supplier, we make it our priority to only source from top global manufacturers that we trust, assuaging the worry of not receiving quality items from us.
The part CVC10011-71GA with NSN 9540-01-435-5694 that we feature by the manufacturer Triumph Aerostructures Llc are paired alongside CAGE Code 80378 is available and readt to ship. Aircraft Parts Supplier carries a variety of NSN products, allowing us to be the go-to supplier for countless businesses. If you are familiar with the NSN associated with the item you are in search of, we invite you to take advantage of it. Similarly, other information regarding the NSN items you wish to purchase is equally as helpful, so please provide such details in the provided RFQ form below. When you fill out a form, in return, you will be provided a competitive quote for your comparisons in just 15 minutes or less.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 9540-01-435-5694 Item Description: Beam Structural | 9540 | 014355694 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| Cvc10011-71ga | 5 | 2 | 3 |
| MRC | Criteria | Characteristic |
|---|---|---|
| CSMZ | Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| HEAT | Heat Treatment | ANNEALED |
| ADXR | Left Side Top Flange Thickness | 0.438 INCHES NOMINAL |
| ABRY | Length | 12.000 FEET NOMINAL |
| BPXG | Right Side Top Flange Distance To Center Of Both Flanges | 1.565 INCHES NOMINAL |
| MATT | Material | TITANIUM ALLOY, MIL-T-81556, COMP AB-1 |
| MRC | Decoded Requirement | Clear Text Reply |
| AGTA | Basic Shape Style | T SHAPE |
| ABKW | Overall Height | 1.310 INCHES NOMINAL |
| AJJP | Leg Thickness | 0.150 INCHES NOMINAL |
| CRZC | Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| BPXD | Left Side Top Flange Distance To Center Of Both Flanges | 1.435 INCHES NOMINAL |
| BPXJ | Fillet Radius Where Top Left Flange Joins Web Flange/Leg | 0.125 INCHES NOMINAL |
| ADXS | Right Side Top Flange Thickness | 0.438 INCHES NOMINAL |
| ZZZT | Nondefinitive Spec/Std Data | COMPOSITION AB-1 AND CONDITION ANNEALED |
| BPXL | Fillet Radius Where Top Right Flange Joins Web Flange/Leg | 0.125 INCHES NOMINAL |
| BQJG | Top Flange Width | 3.000 INCHES NOMINAL |
| CNQJ | Second Tip Relationship To First Tip | IDENTICAL |
| AARN | Fabrication Method | EXTRUDED |
| CMZY | First Tip Style | SQUARE END |
| CNQL | Third Tip Relationship To Preceding Tips | IDENTICAL W/FIRST TIP |
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