The Angle,structural, cataloged under National Stock Number 9540-00-502-1620, 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 Airforce-Navy Aeronautical Design Standard. Government technical data includes 16 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. 5 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-00-502-1620 |
| Primary Part Number | AND10134-1404 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Airforce-Navy Aeronautical Design Standard |
| Status | ACTIVE |
| Second Tip Radius | 0.125 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 6061 |
| Fabrication Method | EXTRUDED |
| Left Side Flange Thickness | 0.125 INCHES NOMINAL IN |
| First Tip Radius | 0.125 INCHES NOMINAL IN |
| Fillet Radius Where Left Flange Joins Base Flange | 0.156 INCHES NOMINAL IN |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| First Tip Style | RIGHT QUARTER RADIUS |
| Material Document and Classification | AMS-QQ-A-200/8 FED SPEC SINGLE MATERIAL RESPONSE |
| Base Flange Thickness | 0.125 INCHES NOMINAL IN |
| Nondefinitive Spec/std Data | 6061 ALLOY AND T6511 TEMPER |
| Heat Treatment | T-6511 SOLUTION HEAT TREATED |
| Second Tip Style | UPPER RADIUS |
| Weight Per Unit Measure | 0.354 POUNDS PER LINEAR FOOT LBS |
| Basic Shape Style | ANGLE |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AND10134-1404 | Airforce-Navy Aeronautical Design Standard |
| 1MA100C03-10069 | The Boeing Company Div Defense (USA) |
| QQ-A-200/8 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| AMS-QQ-A-200/8 | Sae International Dba Sae International (USA) |
| AMS-QQ-A-200/8 | Society of Automotive Engineers Inc (USA) |
| K10B103T6511 | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company (USA) |
| 10164556 | Nimikkeistokeskus Ncb Finland (FIN) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| AND10134-1404/QQ-A-200/8-T6511 | Defense Logistics Agency Dba Defense Supply Center Philadelphia (USA) |
NSN 9540-00-502-1620 is a Angle,structural, manufactured by Airforce-Navy Aeronautical Design Standard, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-00-502-1620 has 9 cross-referenced part numbers: AND10134-1404 (Airforce-Navy Aeronautical Design Standard), 1MA100C03-10069 (The Boeing Company Div Defense), QQ-A-200/8 (Federal Specifications Promulgated by General Services Administration Washington DC), AMS-QQ-A-200/8 (Sae International Dba Sae International), AMS-QQ-A-200/8 (Society of Automotive Engineers Inc) and 4 more.
There are 5 known substitutes for 9540-00-502-1620: 9540-00-140-4978, 9540-00-145-4528, 9540-00-933-9374 and 2 more. Verify interchangeability with system specifications before substitution.
Key specifications for AND10134-1404: Second Tip Radius: 0.125 INCHES NOMINAL IN; Material: ALUMINUM ALLOY 6061; Fabrication Method: EXTRUDED; Left Side Flange Thickness: 0.125 INCHES NOMINAL IN. 18 total characteristics are documented in the Federal Logistics Information System.