The Beam,structural, cataloged under National Stock Number 9540-01-465-2910, 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 23 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 4 commercial cross-references from 4 manufacturers, enabling identification through both NSN and commercial part number lookups. 2 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-465-2910 |
| Primary Part Number | AND10136-2408 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Airforce-Navy Aeronautical Design Standard |
| Status | ACTIVE |
| Third Tip Style | FULL RADIUS |
| First Tip Style | LOWER RADIUS |
| Basic Shape Style | T SHAPE |
| Third Tip Radius | 0.078 INCHES NOMINAL IN |
| Left Side Top Flange Distance to Center of Both Flanges | 1.250 INCHES NOMINAL IN |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Material | ALUMINUM ALLOY 7075 |
| Heat Treatment | ANNEALED |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Leg Thickness | 0.156 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | IDENTICAL |
| Top Flange Width | 2.500 INCHES NOMINAL IN |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Material Document and Classification | AMS-QQ-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Nondefinitive Spec/std Data | 7075 ALLOY AND ANNEALED CONDITION |
| Fabrication Method | EXTRUDED |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Left Side Top Flange Thickness | 0.156 INCHES NOMINAL IN |
| Right Side Top Flange Distance to Center of Both Flanges | 1.250 INCHES NOMINAL IN |
| Third Tip Relationship to Preceding Tips | NOT IDENTICAL |
| Right Side Top Flange Thickness | 0.156 INCHES NOMINAL IN |
| First Tip Radius | 0.156 INCHES NOMINAL IN |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AND10136-2408 | Airforce-Navy Aeronautical Design Standard |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| AND10136-2408/QQ-A-200/11-0 | Defense Logistics Agency Dba Defense Supply Center Philadelphia (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
NSN 9540-01-465-2910 is a Beam,structural, manufactured by Airforce-Navy Aeronautical Design Standard, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-465-2910 has 4 cross-referenced part numbers: AND10136-2408 (Airforce-Navy Aeronautical Design Standard), AMS-QQ-A-200/11 (Society of Automotive Engineers Inc), AND10136-2408/QQ-A-200/11-0 (Defense Logistics Agency Dba Defense Supply Center Philadelphia), AMS-QQ-A-200/11 (Sae International Dba Sae International).
There are 2 known substitutes for 9540-01-465-2910: 9540-00-234-0623, 9540-00-933-9657. Verify interchangeability with system specifications before substitution.
Key specifications for AND10136-2408: Third Tip Style: FULL RADIUS; First Tip Style: LOWER RADIUS; Basic Shape Style: T SHAPE; Third Tip Radius: 0.078 INCHES NOMINAL IN. 24 total characteristics are documented in the Federal Logistics Information System.