The Angle,structural, cataloged under National Stock Number 9540-00-251-2628, 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 Jednolity Indeks Materialowy - Uniform Material Index. Government technical data includes 16 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 20 commercial cross-references from 20 manufacturers, enabling identification through both NSN and commercial part number lookups. 12 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Cancelled.
| Parameter | Value |
|---|---|
| NSN | 9540-00-251-2628 |
| Primary Part Number | 9540PL1768266 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Jednolity Indeks Materialowy - Uniform Material Index |
| Status | CANCELLED |
| Weight Per Unit Measure | 0.281 POUNDS PER LINEAR FOOT LBS |
| Heat Treatment | T-3511 SOLUTION HEAT TREATED |
| First Tip Radius | 0.093 INCHES NOMINAL IN |
| First Tip Style | RIGHT QUARTER RADIUS |
| Material | ALUMINUM ALLOY 2024 |
| Second Tip Style | UPPER RADIUS |
| Fillet Radius Where Left Flange Joins Base Flange | 0.125 INCHES NOMINAL IN |
| Nondefinitive Spec/std Data | 2024 ALLOY AND T3511 TEMPER |
| Material Document and Classification | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| Base Flange Thickness | 0.125 INCHES NOMINAL IN |
| Fabrication Method | EXTRUDED |
| Second Tip Radius | 0.093 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Basic Shape Style | ANGLE |
| Left Side Flange Thickness | 0.125 INCHES NOMINAL IN |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| 9540PL1768266 | Jednolity Indeks Materialowy - Uniform Material Index (POL) |
| CVC1915 | Triumph Aerostructures, Llc Dba Triumph Aerostructures - Vought Integrated Programs Division (USA) |
| E112301 | Hughes Missile Systems Co San Diego (USA) |
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
| 5943 | Bohn Aluminum and Brass Co Div of Gulf and Western Mfg Co Sub of Gulf and Western Industries (USA) |
| E112301 | Bucks Shoes (USA) |
| QQ-A-200/3 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| BAC1503-2733 | The Boeing Company Div Legacy Wichita (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| S172 | Textron Aviation Inc (USA) |
| 1M125 | The Boeing Company Div Defense (USA) |
| 118 | Alcoa/reynolds Metals Company (USA) |
| 77B | Aluminum Co of America (USA) |
| AMS-QQ-A-200/3 | Sae International Dba Sae International (USA) |
| 2-134 | Lockheed Martin Corporation Div Rotary and Mission Systems (USA) |
| S172 | Cessna Aircraft Company Dba Textron Aviation (USA) |
| VS250-11 | General Dynamics Corp (USA) |
| LS3224 | Lockheed Martin Corp (USA) |
| 50E2-9 | Lockheed Martin Corporation Dba Lockheed Martin Rotary and Mission Systems Div Rms- C6isr (USA) |
| 111411 | The Boeing Company (USA) |
NSN 9540-00-251-2628 is a Angle,structural, manufactured by Jednolity Indeks Materialowy - Uniform Material Index, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-00-251-2628 has 20 cross-referenced part numbers: 9540PL1768266 (Jednolity Indeks Materialowy - Uniform Material Index), CVC1915 (Triumph Aerostructures, Llc Dba Triumph Aerostructures - Vought Integrated Programs Division), E112301 (Hughes Missile Systems Co San Diego), AMS-QQ-A-200/3 (Society of Automotive Engineers Inc), 5943 (Bohn Aluminum and Brass Co Div of Gulf and Western Mfg Co Sub of Gulf and Western Industries) and 15 more.
There are 12 known substitutes for 9540-00-251-2628: 9540-00-145-5752, 9540-00-148-4347, 5330-00-295-8709 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for 9540PL1768266: Weight Per Unit Measure: 0.281 POUNDS PER LINEAR FOOT LBS; Heat Treatment: T-3511 SOLUTION HEAT TREATED; Overall Width: 1.000 INCHES NOMINAL IN; First Tip Radius: 0.093 INCHES NOMINAL IN. 18 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-00-251-2628 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.