The Angle,structural, cataloged under National Stock Number 9540-01-164-7575, 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 17 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 9 commercial cross-references from 9 manufacturers, enabling identification through both NSN and commercial part number lookups. 8 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Cancelled.
| Parameter | Value |
|---|---|
| NSN | 9540-01-164-7575 |
| Primary Part Number | LS10134-1005-5 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Lockheed Martin Corp |
| Status | CANCELLED |
| First Tip Radius | 0.063 INCHES NOMINAL IN |
| Left Side Flange Thickness | 0.063 INCHES NOMINAL IN |
| Fillet Radius Where Left Flange Joins Base Flange | 0.125 INCHES NOMINAL IN |
| Heat Treatment | T-6511 SOLUTION HEAT TREATED |
| Material | ALUMINUM ALLOY 7075 |
| Basic Shape Style | ANGLE |
| Weight Per Unit Measure | 0.141 POUNDS PER LINEAR FOOT LBS |
| Base Flange Thickness | 0.063 INCHES NOMINAL IN |
| Nondefinitive Spec/std Data | 7075 ALLOY AND T6511 TEMPER |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| First Tip Style | RIGHT QUARTER RADIUS |
| Second Tip Radius | 0.063 INCHES NOMINAL IN |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Fabrication Method | EXTRUDED |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Second Tip Style | UPPER RADIUS |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| LS10134-1005-5 | Lockheed Martin Corp (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| 10164595 | Nimikkeistokeskus Ncb Finland (FIN) |
| 1MA100D03-10029 | The Boeing Company Div Defense (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
| K10D26T6511 | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| AND10134-1005 | Airforce-Navy Aeronautical Design Standard |
NSN 9540-01-164-7575 is a Angle,structural, manufactured by Lockheed Martin Corp, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-01-164-7575 has 9 cross-referenced part numbers: LS10134-1005-5 (Lockheed Martin Corp), AMS-QQ-A-200/11 (Society of Automotive Engineers Inc), 10164595 (Nimikkeistokeskus Ncb Finland), 1MA100D03-10029 (The Boeing Company Div Defense), ASTM B221 (American Society for Testing and Materials Dba Astm International) and 4 more.
There are 8 known substitutes for 9540-01-164-7575: 9540-00-009-0594, 9540-00-145-4521, 9540-00-146-0730 and 5 more. Verify interchangeability with system specifications before substitution.
Key specifications for LS10134-1005-5: First Tip Radius: 0.063 INCHES NOMINAL IN; Left Side Flange Thickness: 0.063 INCHES NOMINAL IN; Fillet Radius Where Left Flange Joins Base Flange: 0.125 INCHES NOMINAL IN; Overall Height: 0.875 INCHES NOMINAL IN. 19 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-01-164-7575 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.