The Angle,structural, cataloged under National Stock Number 9540-01-071-6533, 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 Sae International Dba Sae International. Government technical data includes 17 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 12 commercial cross-references from 8 manufacturers, enabling identification through both NSN and commercial part number lookups. 7 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-071-6533 |
| Primary Part Number | SAE-AMS-QQ-A-200/8 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Sae International Dba Sae International |
| Status | ACTIVE |
| Material | ALUMINUM ALLOY 6061 |
| Weight Per Unit Measure | 0.426 POUNDS PER LINEAR FOOT LBS |
| Basic Shape Style | ANGLE |
| Material Document and Classification | AMS-QQ-A-200/8 FED SPEC SINGLE MATERIAL RESPONSE |
| Second Tip Radius | 0.125 INCHES NOMINAL IN |
| Fabrication Method | EXTRUDED |
| First Tip Style | RIGHT QUARTER RADIUS |
| Base Flange Thickness | 0.125 INCHES NOMINAL IN |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Fillet Radius Where Left Flange Joins Base Flange | 0.156 INCHES NOMINAL IN |
| Nondefinitive Spec/std Data | 6061 ALLOY AND T6511 TEMPER |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Heat Treatment | T-6511 SOLUTION HEAT TREATED |
| First Tip Radius | 0.125 INCHES NOMINAL IN |
| Left Side Flange Thickness | 0.125 INCHES NOMINAL IN |
| Second Tip Style | UPPER RADIUS |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| SAE-AMS-QQ-A-200/8 | Sae International Dba Sae International (USA) |
| AMS10134-2001 | Sae International Dba Sae International (USA) |
| K10B116T6511 | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company (USA) |
| AMS-QQ-A-200/8 | Society of Automotive Engineers Inc (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) |
| AND10134-2001/QQ-A-200/8-T6511 | Defense Logistics Agency Dba Defense Supply Center Philadelphia (USA) |
| AND10134-2001 | Airforce-Navy Aeronautical Design Standard |
| 9540PL0901169 | Jednolity Indeks Materialowy - Uniform Material Index (POL) |
| AMS10134-2001 | Society of Automotive Engineers Inc (USA) |
| 9540PL1820581 | Jednolity Indeks Materialowy - Uniform Material Index (POL) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
NSN 9540-01-071-6533 is a Angle,structural, manufactured by Sae International Dba Sae International, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-071-6533 has 12 cross-referenced part numbers: SAE-AMS-QQ-A-200/8 (Sae International Dba Sae International), AMS10134-2001 (Sae International Dba Sae International), K10B116T6511 (Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company), AMS-QQ-A-200/8 (Society of Automotive Engineers Inc), QQ-A-200/8 (Federal Specifications Promulgated by General Services Administration Washington DC) and 7 more.
There are 7 known substitutes for 9540-01-071-6533: 9540-00-140-2401, 9540-00-145-5715, 9540-00-145-7541 and 4 more. Verify interchangeability with system specifications before substitution.
Key specifications for SAE-AMS-QQ-A-200/8: Overall Height: 1.000 INCHES NOMINAL IN; Overall Width: 2.000 INCHES NOMINAL IN; Material: ALUMINUM ALLOY 6061; Weight Per Unit Measure: 0.426 POUNDS PER LINEAR FOOT LBS. 19 total characteristics are documented in the Federal Logistics Information System.