The Angle,structural, cataloged under National Stock Number 9540-01-071-5885, 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 Transtar Metals 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. 6 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Cancelled.
| Parameter | Value |
|---|---|
| NSN | 9540-01-071-5885 |
| Primary Part Number | 10134-1201 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Transtar Metals Corp |
| Status | CANCELLED |
| Base Flange Thickness | 0.063 INCHES NOMINAL IN |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Fillet Radius Where Left Flange Joins Base Flange | 0.125 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 2024 |
| Basic Shape Style | ANGLE |
| Second Tip Radius | 0.063 INCHES NOMINAL IN |
| Nondefinitive Spec/std Data | 2024 ALLOY AND T3511 TEMPER |
| Left Side Flange Thickness | 0.063 INCHES NOMINAL IN |
| Second Tip Style | UPPER RADIUS |
| Weight Per Unit Measure | 0.149 POUNDS PER LINEAR FOOT LBS |
| Material Document and Classification | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| Fabrication Method | EXTRUDED |
| First Tip Radius | 0.063 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Heat Treatment | T-3511 SOLUTION HEAT TREATED |
| First Tip Style | RIGHT QUARTER RADIUS |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| 10134-1201 | Transtar Metals Corp (USA) |
| K10A29T3511 | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| MS14284E111 | Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M |
| AMS-QQ-A-200/3 | Sae International Dba Sae International (USA) |
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
| AND10134-1201 | Airforce-Navy Aeronautical Design Standard |
| 9540PL0901159 | Jednolity Indeks Materialowy - Uniform Material Index (POL) |
| QQ-A-200/3 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
NSN 9540-01-071-5885 is a Angle,structural, manufactured by Transtar Metals Corp, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-01-071-5885 has 9 cross-referenced part numbers: 10134-1201 (Transtar Metals Corp), K10A29T3511 (Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company), ASTM B221 (American Society for Testing and Materials Dba Astm International), MS14284E111 (Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M), AMS-QQ-A-200/3 (Sae International Dba Sae International) and 4 more.
There are 6 known substitutes for 9540-01-071-5885: 9540-00-145-4524, 9540-00-185-3995, 9540-01-071-7367 and 3 more. Verify interchangeability with system specifications before substitution.
Key specifications for 10134-1201: Base Flange Thickness: 0.063 INCHES NOMINAL IN; Left Inside Angle: 90.0 DEGREES NOMINAL; Fillet Radius Where Left Flange Joins Base Flange: 0.125 INCHES NOMINAL IN; Material: ALUMINUM ALLOY 2024. 19 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-01-071-5885 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.