The Angle,structural, cataloged under National Stock Number 9540-00-540-5941, 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 26 commercial cross-references from 16 manufacturers, enabling identification through both NSN and commercial part number lookups. 12 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Cancelled.
| Parameter | Value |
|---|---|
| NSN | 9540-00-540-5941 |
| Primary Part Number | 10133-0701 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Transtar Metals Corp |
| Status | CANCELLED |
| Fillet Radius Where Left Flange Joins Base Flange | 0.094 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 7075 |
| Base Flange Thickness | 0.063 INCHES NOMINAL IN |
| Heat Treatment | O-ANNEALED |
| Left Side Flange Thickness | 0.063 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Fabrication Method | EXTRUDED |
| First Tip Style | RIGHT QUARTER RADIUS |
| Basic Shape Style | ANGLE |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Weight Per Unit Measure | 0.130 POUNDS PER LINEAR FOOT LBS |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Second Tip Radius | 0.063 INCHES NOMINAL IN |
| First Tip Radius | 0.063 INCHES NOMINAL IN |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Nondefinitive Spec/std Data | 7075 ALLOY AND 0 TEMPER |
| Second Tip Style | UPPER RADIUS |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| S97 | Textron Aviation Inc (USA) |
| AMS-QQ-A-200/11 ALLOY 7075 TMPR | Sae International Dba Sae International (USA) |
| 10133-0701 PRIMARY | Transtar Metals Corp (USA) |
| AMS10133-0701 | Society of Automotive Engineers Inc (USA) |
| S101 | Textron Aviation Inc (USA) |
| 17157 | International Light Metals Corp Sub of Martin Marietta Corp (USA) |
| AMS-STD-184 | Society of Automotive Engineers Inc (USA) |
| 50669 | National Distillers and Chemical Corp Bridgeport Brass Co Div (USA) |
| AND10133-0701 | Airforce-Navy Aeronautical Design Standard |
| AND10133-0701 | Sae International Dba Sae International (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| AND10133-0701/ASTM B221-0 | Defense Logistics Agency Dba Defense Supply Center Philadelphia (USA) |
| AMS-QQ-A-200/11 ALLOY 7075 TMPR | Society of Automotive Engineers Inc (USA) |
| HA359 | Kaiser Aluminum and Chemical Corp Trentwood Works-Marketing Dept (USA) |
| S101 | Cessna Aircraft Company Dba Textron Aviation (USA) |
| QQ-A-277 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| S97 | Cessna Aircraft Company Dba Textron Aviation (USA) |
| 40304 | Bohn Aluminum and Brass Co Div of Gulf and Western Mfg Co Sub of Gulf and Western Industries (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| AMS-STD-184 | Sae International Dba Sae International (USA) |
NSN 9540-00-540-5941 is a Angle,structural, manufactured by Transtar Metals Corp, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-00-540-5941 has 26 cross-referenced part numbers: S97 (Textron Aviation Inc), AMS-QQ-A-200/11 ALLOY 7075 TMPR (Sae International Dba Sae International), 10133-0701 (Transtar Metals Corp), AMS10133-0701 (Society of Automotive Engineers Inc), S101 (Textron Aviation Inc) and 21 more.
There are 12 known substitutes for 9540-00-540-5941: 5999-00-035-7980, 5950-00-063-9122, 2915-00-098-9010 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for 10133-0701: Fillet Radius Where Left Flange Joins Base Flange: 0.094 INCHES NOMINAL IN; Material: ALUMINUM ALLOY 7075; Base Flange Thickness: 0.063 INCHES NOMINAL IN; Heat Treatment: O-ANNEALED. 19 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-00-540-5941 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.