The Angle,structural, cataloged under National Stock Number 9540-01-233-0624, 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 Airforce-Navy Aeronautical Design Standard. Government technical data includes 17 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 9 commercial cross-references from 6 manufacturers, enabling identification through both NSN and commercial part number lookups. 6 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-233-0624 |
| Primary Part Number | AND10133-1201-7075-0 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Airforce-Navy Aeronautical Design Standard |
| Status | ACTIVE |
| Fabrication Method | EXTRUDED |
| Fillet Radius Where Left Flange Joins Base Flange | 0.188 INCHES NOMINAL IN |
| Second Tip Radius | 0.063 INCHES NOMINAL IN |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Material | ALUMINUM ALLOY 7075 |
| First Tip Style | RIGHT QUARTER RADIUS |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| First Tip Radius | 0.063 INCHES NOMINAL IN |
| Second Tip Style | UPPER RADIUS |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Heat Treatment | O-ANNEALED |
| Basic Shape Style | ANGLE |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Specification/standard Data | 76301-1MA100 MANUFACTURERS STANDARD |
| Nondefinitive Spec/std Data | O TEMPER |
| Left Side Flange Thickness | 0.063 INCHES NOMINAL IN |
| Base Flange Thickness | 0.063 INCHES NOMINAL IN |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AND10133-1201-7075-0 | Airforce-Navy Aeronautical Design Standard |
| 1MA100D01-10050 | The Boeing Company Div Defense (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| AMS10133-1201 | Sae International Dba Sae International (USA) |
| AMS10133-1201 | Society of Automotive Engineers Inc (USA) |
| AND10133-1201 | Airforce-Navy Aeronautical Design Standard |
| 10133-1201 | Transtar Metals Corp (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
NSN 9540-01-233-0624 is a Angle,structural, manufactured by Airforce-Navy Aeronautical Design Standard, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-233-0624 has 9 cross-referenced part numbers: AND10133-1201-7075-0 (Airforce-Navy Aeronautical Design Standard), 1MA100D01-10050 (The Boeing Company Div Defense), AMS-QQ-A-200/11 (Society of Automotive Engineers Inc), AMS10133-1201 (Sae International Dba Sae International), AMS10133-1201 (Society of Automotive Engineers Inc) and 4 more.
There are 6 known substitutes for 9540-01-233-0624: 9540-00-078-6073, 9540-00-236-3955, 9540-00-486-6169 and 3 more. Verify interchangeability with system specifications before substitution.
Key specifications for AND10133-1201-7075-0: Fabrication Method: EXTRUDED; Fillet Radius Where Left Flange Joins Base Flange: 0.188 INCHES NOMINAL IN; Second Tip Radius: 0.063 INCHES NOMINAL IN; Left Inside Angle: 90.0 DEGREES NOMINAL. 19 total characteristics are documented in the Federal Logistics Information System.