The Angle,structural, cataloged under National Stock Number 9540-00-078-6073, 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 Lockheed Martin Corp. Government technical data includes 16 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 10 commercial cross-references from 8 manufacturers, enabling identification through both NSN and commercial part number lookups. 6 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Cancelled.
| Parameter | Value |
|---|---|
| NSN | 9540-00-078-6073 |
| Primary Part Number | LS10134-1201-2 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Lockheed Martin Corp |
| Status | CANCELLED |
| Material Document and Classification | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| Base Flange Thickness | 0.062 INCHES NOMINAL IN |
| Second Tip Radius | 0.062 INCHES NOMINAL IN |
| Fillet Radius Where Left Flange Joins Base Flange | 0.188 INCHES NOMINAL IN |
| Nondefinitive Spec/std Data | 2024 ALLOY AND T3511 TEMPER |
| Material | ALUMINUM ALLOY 2024 |
| First Tip Radius | 0.062 INCHES NOMINAL IN |
| Length | 10.000 FEET NOMINAL FT |
| Weight Per Unit Measure | 0.191 POUNDS PER LINEAR FOOT LBS |
| Left Side Flange Thickness | 0.062 INCHES NOMINAL IN |
| First Tip Style | RIGHT QUARTER RADIUS |
| Second Tip Style | UPPER RADIUS |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Heat Treatment | T-3511 SOLUTION HEAT TREATED |
| Basic Shape Style | ANGLE |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| LS10134-1201-2 PRIMARY | Lockheed Martin Corp (USA) |
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
| AND10133-1201 | Airforce-Navy Aeronautical Design Standard |
| 9540PL0900325 | Jednolity Indeks Materialowy - Uniform Material Index (POL) |
| QQ-A-200/3 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| LS10133-1201-2 | Lockheed Martin Corp (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| K1031T8511 | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company (USA) |
| K10A31T3511 | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company (USA) |
| AMS-QQ-A-200/3 | Sae International Dba Sae International (USA) |
NSN 9540-00-078-6073 is a Angle,structural, manufactured by Lockheed Martin Corp, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-00-078-6073 has 10 cross-referenced part numbers: LS10134-1201-2 (Lockheed Martin Corp), AMS-QQ-A-200/3 (Society of Automotive Engineers Inc), AND10133-1201 (Airforce-Navy Aeronautical Design Standard), 9540PL0900325 (Jednolity Indeks Materialowy - Uniform Material Index), QQ-A-200/3 (Federal Specifications Promulgated by General Services Administration Washington DC) and 5 more.
There are 6 known substitutes for 9540-00-078-6073: 9540-00-236-3955, 9540-00-486-6169, 9540-01-072-0172 and 3 more. Verify interchangeability with system specifications before substitution.
Key specifications for LS10134-1201-2: Material Document and Classification: AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE; Base Flange Thickness: 0.062 INCHES NOMINAL IN; Second Tip Radius: 0.062 INCHES NOMINAL IN; Fillet Radius Where Left Flange Joins Base Flange: 0.188 INCHES NOMINAL IN. 19 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-00-078-6073 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.