The Angle,structural, cataloged under National Stock Number 9540-00-145-8450, 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 12 commercial cross-references from 11 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 | 9540-00-145-8450 |
| Primary Part Number | AND10133-1402 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Airforce-Navy Aeronautical Design Standard |
| Status | CANCELLED |
| Nondefinitive Spec/std Data | 7075 ALLOY AND T6 TEMPER OR T6511 TEMPER |
| First Tip Radius | 0.094 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 7075 |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Left Side Flange Thickness | 0.094 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.330 POUNDS PER LINEAR FOOT LBS |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Second Tip Radius | 0.094 INCHES NOMINAL IN |
| First Tip Style | RIGHT QUARTER RADIUS |
| Basic Shape Style | ANGLE |
| Base Flange Thickness | 0.094 INCHES NOMINAL IN |
| Second Tip Style | UPPER RADIUS |
| Fillet Radius Where Left Flange Joins Base Flange | 0.188 INCHES NOMINAL IN |
| Heat Treatment | T-6 SOLUTION HEAT TREATED OR T-6511 SOLUTION HEAT TREATED |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AND10133-1402 | Airforce-Navy Aeronautical Design Standard |
| RY30015 | Northrop Grumman Systems Corporation (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| AMS4154 | Sae International Dba Sae International (USA) |
| HA369 | Kaiser Aluminum and Chemical Corp Wire and Cable Div (USA) |
| 2-1306 | Lockheed Martin Corporation Div Rotary and Mission Systems (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| 11113-1 | International Light Metals Corp Sub of Martin Marietta Corp (USA) |
| 40354 | Bohn Aluminum and Brass Co Div of Gulf and Western Mfg Co Sub of Gulf and Western Industries (USA) |
| 5734 | Reynolds Metals Co (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
NSN 9540-00-145-8450 is a Angle,structural, manufactured by Airforce-Navy Aeronautical Design Standard, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-00-145-8450 has 12 cross-referenced part numbers: AND10133-1402 (Airforce-Navy Aeronautical Design Standard), RY30015 (Northrop Grumman Systems Corporation), AMS-QQ-A-200/11 (Society of Automotive Engineers Inc), AMS4154 (Sae International Dba Sae International), HA369 (Kaiser Aluminum and Chemical Corp Wire and Cable Div) and 7 more.
There are 12 known substitutes for 9540-00-145-8450: 5330-00-119-4205, 3455-00-194-0550, 5975-00-194-8863 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for AND10133-1402: Nondefinitive Spec/std Data: 7075 ALLOY AND T6 TEMPER OR T6511 TEMPER; First Tip Radius: 0.094 INCHES NOMINAL IN; Material: ALUMINUM ALLOY 7075; Overall Width: 1.500 INCHES NOMINAL IN. 18 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-00-145-8450 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.