The Beam,structural, cataloged under National Stock Number 9540-01-071-4737, 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 6 commercial cross-references from 6 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 | 9540-01-071-4737 |
| Primary Part Number | AND10136-2008 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Airforce-Navy Aeronautical Design Standard |
| Status | ACTIVE |
| Left Side Top Flange Distance to Center of Both Flanges | 1.000 INCHES NOMINAL IN |
| Fabrication Method | EXTRUDED |
| First Tip Style | LOWER RADIUS |
| Material | ALUMINUM ALLOY 2024 |
| First Tip Radius | 0.125 INCHES NOMINAL IN |
| Third Tip Style | FULL RADIUS |
| Left Side Top Flange Thickness | 0.125 INCHES NOMINAL IN |
| Heat Treatment | T-3511 SOLUTION HEAT TREATED |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Basic Shape Style | T SHAPE |
| Third Tip Relationship to Preceding Tips | NOT IDENTICAL |
| Nondefinitive Spec/std Data | T3511 TEMPER |
| Material Document and Classification | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| Third Tip Radius | 0.0625 INCHES NOMINAL IN |
| Leg Thickness | 0.125 INCHES NOMINAL IN |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Second Tip Relationship to First Tip | IDENTICAL |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Top Flange Width | 2.000 INCHES NOMINAL IN |
| Right Side Top Flange Distance to Center of Both Flanges | 1.000 INCHES NOMINAL IN |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.541 POUNDS PER LINEAR FOOT LBS |
| Right Side Top Flange Thickness | 0.125 INCHES NOMINAL IN |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AND10136-2008 | Airforce-Navy Aeronautical Design Standard |
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
| K40A128T3511 | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company (USA) |
| MS14376E057 | Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M |
| AMS-QQ-A-200/3 | Sae International Dba Sae International (USA) |
| 10136-2008 | Transtar Metals Corp (USA) |
NSN 9540-01-071-4737 is a Beam,structural, manufactured by Airforce-Navy Aeronautical Design Standard, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-071-4737 has 6 cross-referenced part numbers: AND10136-2008 (Airforce-Navy Aeronautical Design Standard), AMS-QQ-A-200/3 (Society of Automotive Engineers Inc), K40A128T3511 (Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company), MS14376E057 (Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M), AMS-QQ-A-200/3 (Sae International Dba Sae International) and 1 more.
There are 2 known substitutes for 9540-01-071-4737: 9540-00-555-0816, 9540-01-281-7897. Verify interchangeability with system specifications before substitution.
Key specifications for AND10136-2008: Left Side Top Flange Distance to Center of Both Flanges: 1.000 INCHES NOMINAL IN; Fabrication Method: EXTRUDED; First Tip Style: LOWER RADIUS; Material: ALUMINUM ALLOY 2024. 25 total characteristics are documented in the Federal Logistics Information System.