The Angle,structural, cataloged under National Stock Number 9540-01-071-6525, 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 18 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 11 commercial cross-references from 11 manufacturers, enabling identification through both NSN and commercial part number lookups. 8 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-071-6525 |
| 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 |
| Left Side Flange Thickness | 0.072 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 2024 |
| Fabrication Method | EXTRUDED |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Fillet Radius Where Left Flange Joins Base Flange | 0.090 INCHES NOMINAL IN |
| Base Flange Thickness | 0.072 INCHES NOMINAL IN |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Nondefinitive Spec/std Data | 2024 ALLOY AND T3511 TEMPER |
| Second Tip Radius | 0.070 INCHES NOMINAL IN |
| First Tip Radius | 0.070 INCHES NOMINAL IN |
| First Tip Style | RIGHT QUARTER RADIUS |
| Second Tip Style | UPPER RADIUS |
| Material Document and Classification | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| Specification/standard Data | 81755-K10 MANUFACTURERS STANDARD |
| Weight Per Unit Measure | 0.231 POUNDS PER LINEAR FOOT LBS |
| Basic Shape Style | ANGLE |
| Heat Treatment | T-3511 SOLUTION HEAT TREATED |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| K10A46T3511 | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company (USA) |
| MS14284E161 | Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M |
| 9540PL0901167 | Jednolity Indeks Materialowy - Uniform Material Index (POL) |
| 60194 | International Light Metals Corp Sub of Martin Marietta Corp (USA) |
| AMS-QQ-A-200/3 | Sae International Dba Sae International (USA) |
| QQ-A-200/3 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| 60-14750 | Transtar Metals Corp (USA) |
| 34911 | Alcoa/reynolds Metals Company (USA) |
| 11202-A | Pimalco Inc. Div Alcoa Inc Global Hard Alloy Extrusions (USA) |
NSN 9540-01-071-6525 is a Angle,structural, manufactured by Society of Automotive Engineers Inc, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-071-6525 has 11 cross-referenced part numbers: AMS-QQ-A-200/3 (Society of Automotive Engineers Inc), ASTM B221 (American Society for Testing and Materials Dba Astm International), K10A46T3511 (Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company), MS14284E161 (Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M), 9540PL0901167 (Jednolity Indeks Materialowy - Uniform Material Index) and 6 more.
There are 8 known substitutes for 9540-01-071-6525: 5305-00-068-0508, 4320-00-546-6702, 5845-00-876-9800 and 5 more. Verify interchangeability with system specifications before substitution.
Key specifications for AMS-QQ-A-200/3: Left Side Flange Thickness: 0.072 INCHES NOMINAL IN; Material: ALUMINUM ALLOY 2024; Fabrication Method: EXTRUDED; Second Tip Relationship to First Tip: NOT IDENTICAL. 20 total characteristics are documented in the Federal Logistics Information System.