The Angle,structural, cataloged under National Stock Number 9540-00-288-1145, 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 Society of Automotive Engineers Inc. Government technical data includes 16 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 14 commercial cross-references from 10 manufacturers, enabling identification through both NSN and commercial part number lookups. 12 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-00-288-1145 |
| Primary Part Number | AMS-QQ-A-200/3 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Society of Automotive Engineers Inc |
| Status | ACTIVE |
| Second Tip Style | UPPER RADIUS |
| First Tip Radius | 0.250 INCHES NOMINAL IN |
| First Tip Style | RIGHT QUARTER RADIUS |
| Material | ALUMINUM ALLOY 2024 |
| Fabrication Method | EXTRUDED |
| Basic Shape Style | ANGLE |
| Fillet Radius Where Left Flange Joins Base Flange | 0.250 INCHES NOMINAL IN |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Nondefinitive Spec/std Data | 2024 ALLOY AND T3511 TEMPER |
| Left Side Flange Thickness | 0.250 INCHES NOMINAL IN |
| Weight Per Unit Measure | 1.110 POUNDS PER LINEAR FOOT LBS |
| Base Flange Thickness | 0.250 INCHES NOMINAL IN |
| Heat Treatment | T-3511 SOLUTION HEAT TREATED |
| Second Tip Radius | 0.250 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Material Document and Classification | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
| AMS-QQ-A-200/3-T3511-0.250X2X10 | Society of Automotive Engineers Inc (USA) |
| 110-503062 | Hiller Aircraft Corporation (USA) |
| 12551-1 | International Light Metals Corp Sub of Martin Marietta Corp (USA) |
| AND10133-2004 | Airforce-Navy Aeronautical Design Standard |
| 2-1327 | Lockheed Martin Corporation Div Rotary and Mission Systems (USA) |
| QQ-A-200/3 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| 1047972 | The Boeing Company (USA) |
| 1047972 | The Boeing Company (USA) |
| 1245442 | The Boeing Company (USA) |
| 1822 | Alcoa/reynolds Metals Company (USA) |
| 1245442 | The Boeing Company (USA) |
| CDS148 | Chase Aircraft Co Inc |
NSN 9540-00-288-1145 is a Angle,structural, manufactured by Society of Automotive Engineers Inc, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-00-288-1145 has 14 cross-referenced part numbers: AMS-QQ-A-200/3 (Society of Automotive Engineers Inc), AMS-QQ-A-200/3-T3511-0.250X2X10 (Society of Automotive Engineers Inc), 110-503062 (Hiller Aircraft Corporation), 12551-1 (International Light Metals Corp Sub of Martin Marietta Corp), AND10133-2004 (Airforce-Navy Aeronautical Design Standard) and 9 more.
There are 12 known substitutes for 9540-00-288-1145: 5999-00-035-7934, 3110-00-144-8958, 4730-00-243-1484 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for AMS-QQ-A-200/3: Second Tip Style: UPPER RADIUS; First Tip Radius: 0.250 INCHES NOMINAL IN; First Tip Style: RIGHT QUARTER RADIUS; Material: ALUMINUM ALLOY 2024. 18 total characteristics are documented in the Federal Logistics Information System.