The Beam,structural, cataloged under National Stock Number 9540-01-428-2774, is classified within Federal Supply Class 9540 (No Item Name Available) of the Metal Bars, Sheets, and Shapes group. The primary manufacturer of record is Triumph Aerostructures, Llc Dba Triumph Aerostructures - Vought Integrated Programs Division. Government technical data includes 21 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 8 commercial cross-references from 7 manufacturers, enabling identification through both NSN and commercial part number lookups. 10 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-428-2774 |
| Primary Part Number | CVC10012-154CA |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Triumph Aerostructures, Llc Dba Triumph Aerostructures - Vought Integrated Programs Division |
| Status | ACTIVE |
| Left Side Top Flange Distance to Center of Both Flanges | 2.561 INCHES NOMINAL IN |
| Length | 12.000 FEET NOMINAL FT |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 7075 |
| Leg Thickness | 0.120 INCHES NOMINAL IN |
| Right Top Inside Angle | 70.0 DEGREES NOMINAL |
| Right Side Top Flange Thickness | 0.120 INCHES NOMINAL IN |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Nondefinitive Spec/std Data | 7075 ALLOY AND ANNEALED CONDITION |
| Third Tip Relationship to Preceding Tips | IDENTICAL W/FIRST TIP |
| Top Flange Width | 5.250 INCHES NOMINAL IN |
| Fabrication Method | EXTRUDED |
| Left Top Inside Angle | 110.0 DEGREES NOMINAL |
| First Tip Style | SQUARE END |
| Weight Per Unit Measure | 1.108 POUNDS PER SQUARE FOOT LBS |
| Heat Treatment | O-ANNEALED |
| Right Side Top Flange Distance to Center of Both Flanges | 2.689 INCHES NOMINAL IN |
| Left Side Top Flange Thickness | 0.120 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | IDENTICAL |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Basic Shape Style | T SHAPE |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| CVC10012-154CA PRIMARY | Triumph Aerostructures, Llc Dba Triumph Aerostructures - Vought Integrated Programs Division (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| 60-21307 PRIMARY | Transtar Metals Corp (USA) |
| 7075-0 | Defense Logistics Agency Dba Defense Supply Center Philadelphia (USA) |
| AMS4476 | Sae International Dba Sae International (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
NSN 9540-01-428-2774 is a Beam,structural, manufactured by Triumph Aerostructures, Llc Dba Triumph Aerostructures - Vought Integrated Programs Division, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-428-2774 has 8 cross-referenced part numbers: CVC10012-154CA (Triumph Aerostructures, Llc Dba Triumph Aerostructures - Vought Integrated Programs Division), AMS-QQ-A-200/11 (Sae International Dba Sae International), QQ-A-200/11 (Federal Specifications Promulgated by General Services Administration Washington DC), ASTM B221 (American Society for Testing and Materials Dba Astm International), 60-21307 (Transtar Metals Corp) and 3 more.
There are 10 known substitutes for 9540-01-428-2774: 9540-00-006-8478, 5365-00-507-3267, 5970-01-153-0577 and 7 more. Verify interchangeability with system specifications before substitution.
Key specifications for CVC10012-154CA: Overall Height: 2.478 INCHES NOMINAL IN; Left Side Top Flange Distance to Center of Both Flanges: 2.561 INCHES NOMINAL IN; Length: 12.000 FEET NOMINAL FT; Fillet Radius Where Top Right Flange Joins Web Flange/leg: 0.125 INCHES NOMINAL IN. 23 total characteristics are documented in the Federal Logistics Information System.