The Beam,structural, cataloged under National Stock Number 9540-01-079-3301, 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 1 commercial cross-reference from 1 manufacturer, enabling identification through both NSN and commercial part number lookups. 3 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-079-3301 |
| Primary Part Number | AND10136-2402 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Airforce-Navy Aeronautical Design Standard |
| Status | ACTIVE |
| Fabrication Method | EXTRUDED |
| Right Side Top Flange Distance to Center of Both Flanges | 1.250 INCHES NOMINAL IN |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | IDENTICAL |
| Weight Per Unit Measure | 0.540 POUNDS PER LINEAR FOOT LBS |
| Nondefinitive Spec/std Data | 7075 ALLOY AND 0 TEMPER |
| Material | ALUMINUM ALLOY 7075 |
| Material Document and Classification | QQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Basic Shape Style | T SHAPE |
| Third Tip Radius | 0.063 INCHES NOMINAL IN |
| Third Tip Relationship to Preceding Tips | NOT IDENTICAL |
| Right Side Top Flange Thickness | 0.125 INCHES NOMINAL IN |
| First Tip Radius | 0.125 INCHES NOMINAL IN |
| Left Side Top Flange Distance to Center of Both Flanges | 1.250 INCHES NOMINAL IN |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Heat Treatment | O-ANNEALED |
| Third Tip Style | LOWER RADIUS |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Left Side Top Flange Thickness | 0.125 INCHES NOMINAL IN |
| Leg Thickness | 0.156 INCHES NOMINAL IN |
| First Tip Style | LOWER RADIUS |
| Top Flange Width | 2.500 INCHES NOMINAL IN |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AND10136-2402 | Airforce-Navy Aeronautical Design Standard |
NSN 9540-01-079-3301 is a Beam,structural, manufactured by Airforce-Navy Aeronautical Design Standard, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-079-3301 has 1 cross-referenced part number: AND10136-2402 (Airforce-Navy Aeronautical Design Standard).
There are 3 known substitutes for 9540-01-079-3301: 9540-00-242-5433, 9540-00-502-0755, 9540-00-596-3220. Verify interchangeability with system specifications before substitution.
Key specifications for AND10136-2402: Fabrication Method: EXTRUDED; Right Side Top Flange Distance to Center of Both Flanges: 1.250 INCHES NOMINAL IN; Fillet Radius Where Top Left Flange Joins Web Flange/leg: 0.125 INCHES NOMINAL IN; Second Tip Relationship to First Tip: IDENTICAL. 25 total characteristics are documented in the Federal Logistics Information System.