The Angle,structural, cataloged under National Stock Number 9540-01-369-9117, 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 Federal Specifications Promulgated by General Services Administration Washington DC. Government technical data includes 16 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 10 commercial cross-references from 5 manufacturers, enabling identification through both NSN and commercial part number lookups. 11 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-369-9117 |
| Primary Part Number | QQ-A-200/11 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Federal Specifications Promulgated by General Services Administration Washington DC |
| Status | ACTIVE |
| Base Flange Thickness | 0.250 INCHES NOMINAL IN |
| Heat Treatment | O-ANNEALED |
| Material | ALUMINUM ALLOY 7075 |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Second Tip Style | UPPER RADIUS |
| First Tip Radius | 0.125 INCHES NOMINAL IN |
| Second Tip Radius | 0.125 INCHES NOMINAL IN |
| First Tip Style | RIGHT QUARTER RADIUS |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Fillet Radius Where Left Flange Joins Base Flange | 0.125 INCHES NOMINAL IN |
| Length | 10.000 INCHES MINIMUM AND 12.000 INCHES MAXIMUM IN |
| Nondefinitive Spec/std Data | 7075 ALLOY AND ANNEALED CONDITION |
| Left Side Flange Thickness | 0.125 INCHES NOMINAL IN |
| Basic Shape Style | ANGLE |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Fabrication Method | EXTRUDED |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| 1MA100D01-10164 | The Boeing Company Div Defense (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
| AND10133-2401 | Airforce-Navy Aeronautical Design Standard |
| 1MA100-10164 | The Boeing Company Div Defense (USA) |
| AMS10133-2401 | Society of Automotive Engineers Inc (USA) |
| AMS 4476 | Sae International Dba Sae International (USA) |
| AMS 4476 | Society of Automotive Engineers Inc (USA) |
| AMS10133-2401 | Sae International Dba Sae International (USA) |
NSN 9540-01-369-9117 is a Angle,structural, manufactured by Federal Specifications Promulgated by General Services Administration Washington DC, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-369-9117 has 10 cross-referenced part numbers: QQ-A-200/11 (Federal Specifications Promulgated by General Services Administration Washington DC), 1MA100D01-10164 (The Boeing Company Div Defense), AMS-QQ-A-200/11 (Society of Automotive Engineers Inc), AMS-QQ-A-200/11 (Sae International Dba Sae International), AND10133-2401 (Airforce-Navy Aeronautical Design Standard) and 5 more.
There are 11 known substitutes for 9540-01-369-9117: 9540-00-006-8478, 9540-00-140-2396, 9540-00-839-2134 and 8 more. Verify interchangeability with system specifications before substitution.
Key specifications for QQ-A-200/11: Base Flange Thickness: 0.250 INCHES NOMINAL IN; Heat Treatment: O-ANNEALED; Material: ALUMINUM ALLOY 7075; Left Inside Angle: 90.0 DEGREES NOMINAL. 18 total characteristics are documented in the Federal Logistics Information System.