The Angle,structural, cataloged under National Stock Number 9540-00-179-9588, 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 28 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 6 commercial cross-references from 6 manufacturers, enabling identification through both NSN and commercial part number lookups. 2 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-00-179-9588 |
| Primary Part Number | LS10134-1001-6 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Lockheed Martin Corp |
| Status | ACTIVE |
| Basic Shape Style | ANGLE |
| Material | ALUMINUM ALLOY 7075 |
| Left Side Flange Thickness | 0.063 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.120 POUNDS PER LINEAR FOOT LBS |
| Fillet Radius Where Left Flange Joins Base Flange | 0.125 INCHES NOMINAL IN |
| Heat Treatment | O-ANNEALED |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| First Tip Style | RIGHT QUARTER RADIUS |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Nondefinitive Spec/std Data | 7075 ALLOY AND 0 TEMPER |
| Material | ALUMINUM ALLOY 7075 |
| First Tip Radius | 0.063 INCHES NOMINAL IN |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Second Tip Style | UPPER RADIUS |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Nondefinitive Spec/std Data | 7075 ALLOY AND 0 TEMPER |
| Weight Per Unit Measure | 0.120 POUNDS PER LINEAR FOOT LBS |
| Left Side Flange Thickness | 0.063 INCHES NOMINAL IN |
| Heat Treatment | O-ANNEALED |
| First Tip Style | RIGHT QUARTER RADIUS |
| First Tip Radius | 0.063 INCHES NOMINAL IN |
| Base Flange Thickness | 0.063 INCHES NOMINAL IN |
| Fillet Radius Where Left Flange Joins Base Flange | 0.125 INCHES NOMINAL IN |
| Fabrication Method | EXTRUDED |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Basic Shape Style | ANGLE |
| Second Tip Radius | 0.063 INCHES NOMINAL IN |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| LS10134-1001-6 | Lockheed Martin Corp (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) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| AND10134-1001 | Airforce-Navy Aeronautical Design Standard |
NSN 9540-00-179-9588 is a Angle,structural, manufactured by Lockheed Martin Corp, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-00-179-9588 has 6 cross-referenced part numbers: LS10134-1001-6 (Lockheed Martin Corp), QQ-A-200/11 (Federal Specifications Promulgated by General Services Administration Washington DC), ASTM B221 (American Society for Testing and Materials Dba Astm International), AMS-QQ-A-200/11 (Sae International Dba Sae International), AMS-QQ-A-200/11 (Society of Automotive Engineers Inc) and 1 more.
There are 2 known substitutes for 9540-00-179-9588: 9540-00-846-3670, 9540-01-071-6544. Verify interchangeability with system specifications before substitution.
Key specifications for LS10134-1001-6: Basic Shape Style: ANGLE; Material: ALUMINUM ALLOY 7075; Overall Width: 1.000 INCHES NOMINAL IN; Left Side Flange Thickness: 0.063 INCHES NOMINAL IN. 30 total characteristics are documented in the Federal Logistics Information System.