The Beam,structural, cataloged under National Stock Number 9540-00-516-8015, 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 The Boeing Company. Government technical data includes 20 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. 4 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-00-516-8015 |
| Primary Part Number | S1440034 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | The Boeing Company |
| Status | ACTIVE |
| Weight Per Unit Measure | 0.180 POUNDS PER LINEAR FOOT LBS |
| Second Tip Relationship to First Tip | IDENTICAL |
| Heat Treatment | T-6 SOLUTION HEAT TREATED |
| Fabrication Method | EXTRUDED |
| Top Flange Width | 0.812 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 7075 |
| Right Bottom Inside Angle | 90.0 DEGREES NOMINAL |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Nondefinitive Spec/std Data | T6 TEMPER |
| Fillet Radius Where Bottom Right Flange Joins Web Flange/leg | 0.062 INCHES NOMINAL IN |
| Basic Shape Style | Z SHAPE |
| First Tip Radius | 0.025 INCHES NOMINAL IN |
| First Tip Style | FULL RADIUS |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Right Side Bottom Flange Thickness | 0.050 INCHES NOMINAL IN |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.062 INCHES NOMINAL IN |
| Bottom Flange Width | 0.812 INCHES NOMINAL IN |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Web Flange Thickness | 0.050 INCHES NOMINAL IN |
| Left Side Top Flange Thickness | 0.050 INCHES NOMINAL IN |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| S1440034 | The Boeing Company (USA) |
| 8429 | Alcoa/reynolds Metals Company (USA) |
| 60-1928 | Transtar Metals Corp (USA) |
| PA2141 | Transtar Metals Corp (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| QQA200-11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| S1440034 | The Boeing Company (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
NSN 9540-00-516-8015 is a Beam,structural, manufactured by The Boeing Company, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-00-516-8015 has 8 cross-referenced part numbers: S1440034 (The Boeing Company), 8429 (Alcoa/reynolds Metals Company), 60-1928 (Transtar Metals Corp), PA2141 (Transtar Metals Corp), AMS-QQ-A-200/11 (Society of Automotive Engineers Inc) and 3 more.
There are 4 known substitutes for 9540-00-516-8015: 5340-00-117-4756, 5910-00-126-9172, 4030-00-234-8862 and 1 more. Verify interchangeability with system specifications before substitution.
Key specifications for S1440034: Weight Per Unit Measure: 0.180 POUNDS PER LINEAR FOOT LBS; Overall Height: 1.000 INCHES NOMINAL IN; Second Tip Relationship to First Tip: IDENTICAL; Heat Treatment: T-6 SOLUTION HEAT TREATED. 21 total characteristics are documented in the Federal Logistics Information System.