The Angle,structural, cataloged under National Stock Number 9540-00-596-2777, 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 16 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 8 commercial cross-references from 7 manufacturers, enabling identification through both NSN and commercial part number lookups. 7 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Cancelled.
| Parameter | Value |
|---|---|
| NSN | 9540-00-596-2777 |
| Primary Part Number | AND10133-2002 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Airforce-Navy Aeronautical Design Standard |
| Status | CANCELLED |
| Second Tip Radius | 0.125 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Fillet Radius Where Left Flange Joins Base Flange | 0.250 INCHES NOMINAL IN |
| Left Side Flange Thickness | 0.125 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 6061 |
| Heat Treatment | T-6511 SOLUTION HEAT TREATED OR T-6 SOLUTION HEAT TREATED |
| Second Tip Style | UPPER RADIUS |
| First Tip Style | RIGHT QUARTER RADIUS |
| Basic Shape Style | ANGLE |
| Material Document and Classification | AMS-QQ-A-200/8 FED SPEC SINGLE MATERIAL RESPONSE |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Nondefinitive Spec/std Data | 6061 ALLOY AND T6 TEMPER |
| Base Flange Thickness | 0.125 INCHES NOMINAL IN |
| First Tip Radius | 0.125 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.590 POUNDS PER LINEAR FOOT LBS |
| Fabrication Method | EXTRUDED |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AND10133-2002 | Airforce-Navy Aeronautical Design Standard |
| FS10105-2020-2 | Hiller Aircraft Corporation (USA) |
| SAE-AMS-QQ-A-200/8 | Sae International Dba Sae International (USA) |
| HA15 | Kaiser Aluminum and Chemical Corp Trentwood Works-Marketing Dept (USA) |
| BAC1503-8813 | The Boeing Company Div Legacy Wichita (USA) |
| AMS-QQ-A-200/8 | Sae International Dba Sae International (USA) |
| AMS-QQ-A-200/8 | Society of Automotive Engineers Inc (USA) |
| 77V | Aluminum Co of America (USA) |
NSN 9540-00-596-2777 is a Angle,structural, manufactured by Airforce-Navy Aeronautical Design Standard, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-00-596-2777 has 8 cross-referenced part numbers: AND10133-2002 (Airforce-Navy Aeronautical Design Standard), FS10105-2020-2 (Hiller Aircraft Corporation), SAE-AMS-QQ-A-200/8 (Sae International Dba Sae International), HA15 (Kaiser Aluminum and Chemical Corp Trentwood Works-Marketing Dept), BAC1503-8813 (The Boeing Company Div Legacy Wichita) and 3 more.
There are 7 known substitutes for 9540-00-596-2777: 9540-00-140-2404, 9540-00-145-8447, 9540-00-186-6334 and 4 more. Verify interchangeability with system specifications before substitution.
Key specifications for AND10133-2002: Second Tip Radius: 0.125 INCHES NOMINAL IN; Second Tip Relationship to First Tip: NOT IDENTICAL; Fillet Radius Where Left Flange Joins Base Flange: 0.250 INCHES NOMINAL IN; Left Side Flange Thickness: 0.125 INCHES NOMINAL IN. 18 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-00-596-2777 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.