The Beam,structural, cataloged under National Stock Number 9540-00-596-3225, 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 24 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 8 commercial cross-references from 6 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 | 9540-00-596-3225 |
| Primary Part Number | AND10136-2005 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Airforce-Navy Aeronautical Design Standard |
| Status | CANCELLED |
| First Tip Style | LOWER RADIUS |
| Second Tip Relationship to First Tip | IDENTICAL |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 7075 |
| Weight Per Unit Measure | 0.360 POUNDS PER LINEAR FOOT LBS |
| Heat Treatment | T-6 SOLUTION HEAT TREATED |
| First Tip Radius | 0.094 INCHES NOMINAL IN |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Third Tip Radius | 0.047 INCHES NOMINAL IN |
| Right Side Top Flange Distance to Center of Both Flanges | 1.000 INCHES NOMINAL IN |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Nondefinitive Spec/std Data | T6 TEMPER |
| Right Side Top Flange Thickness | 0.094 INCHES NOMINAL IN |
| Third Tip Style | FULL RADIUS |
| Left Side Top Flange Distance to Center of Both Flanges | 1.000 INCHES NOMINAL IN |
| Fabrication Method | EXTRUDED |
| Top Flange Width | 2.000 INCHES NOMINAL IN |
| Basic Shape Style | T SHAPE |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Leg Thickness | 0.094 INCHES NOMINAL IN |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Left Side Top Flange Thickness | 0.094 INCHES NOMINAL IN |
| Third Tip Relationship to Preceding Tips | NOT IDENTICAL |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AND10136-2005 | Airforce-Navy Aeronautical Design Standard |
| 40212 | Bohn Aluminum and Brass Co Div of Gulf and Western Mfg Co Sub of Gulf and Western Industries (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
| AMS10136-2005 | Society of Automotive Engineers Inc (USA) |
| 6189B | Alcoa/reynolds Metals Company (USA) |
| AMS10136-2005 | Sae International Dba Sae International (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
NSN 9540-00-596-3225 is a Beam,structural, manufactured by Airforce-Navy Aeronautical Design Standard, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-00-596-3225 has 8 cross-referenced part numbers: AND10136-2005 (Airforce-Navy Aeronautical Design Standard), 40212 (Bohn Aluminum and Brass Co Div of Gulf and Western Mfg Co Sub of Gulf and Western Industries), AMS-QQ-A-200/11 (Sae International Dba Sae International), AMS10136-2005 (Society of Automotive Engineers Inc), 6189B (Alcoa/reynolds Metals Company) and 3 more.
There are 12 known substitutes for 9540-00-596-3225: 5999-00-030-1997, 6210-00-203-5995, 4730-00-374-6943 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for AND10136-2005: First Tip Style: LOWER RADIUS; Second Tip Relationship to First Tip: IDENTICAL; Fillet Radius Where Top Right Flange Joins Web Flange/leg: 0.125 INCHES NOMINAL IN; Material: ALUMINUM ALLOY 7075. 25 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-00-596-3225 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.