The Beam,structural, cataloged under National Stock Number 9540-00-554-4986, 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 21 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 12 commercial cross-references from 9 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 | 9540-00-554-4986 |
| Primary Part Number | 1114110A |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | The Boeing Company |
| Status | CANCELLED |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Heat Treatment | T-4 SOLUTION HEAT TREATED |
| Basic Shape Style | T SHAPE |
| Leg Thickness | 0.051 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 2024 |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.094 INCHES NOMINAL IN |
| Right Side Top Flange Distance to Center of Both Flanges | 1.000 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.170 POUNDS PER LINEAR FOOT LBS |
| Left Side Top Flange Distance to Center of Both Flanges | 1.000 INCHES NOMINAL IN |
| Nondefinitive Spec/std Data | T4 TEMPER |
| Material Document and Classification | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| Right Side Top Flange Thickness | 0.051 INCHES NOMINAL IN |
| Fabrication Method | EXTRUDED |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Left Side Top Flange Thickness | 0.051 INCHES NOMINAL IN |
| Third Tip Relationship to Preceding Tips | IDENTICAL W/FIRST TIP |
| Second Tip Relationship to First Tip | IDENTICAL |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.094 INCHES NOMINAL IN |
| First Tip Style | SQUARE END |
| Top Flange Width | 2.000 INCHES NOMINAL IN |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| 1114110A | The Boeing Company (USA) |
| 1114110-2400 | The Boeing Company (USA) |
| 1114110A | The Boeing Company (USA) |
| 60-11342 | Transtar Metals Corp (USA) |
| P2916 | Reynolds Metals Co (USA) |
| 30674 | Aluminum Co of America (USA) |
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
| 2916 | Alcoa/reynolds Metals Company (USA) |
| 42819 | International Light Metals Corp Sub of Martin Marietta Corp (USA) |
| PA6594 | Transtar Metals Corp (USA) |
| AMS-QQ-A-200/3 | Sae International Dba Sae International (USA) |
| QQA200-3 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
NSN 9540-00-554-4986 is a Beam,structural, manufactured by The Boeing Company, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-00-554-4986 has 12 cross-referenced part numbers: 1114110A (The Boeing Company), 1114110-2400 (The Boeing Company), 1114110A (The Boeing Company), 60-11342 (Transtar Metals Corp), P2916 (Reynolds Metals Co) and 7 more.
There are 12 known substitutes for 9540-00-554-4986: 5977-00-084-9174, 3110-00-156-1904, 5325-00-185-0001 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for 1114110A: Length: 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT; Heat Treatment: T-4 SOLUTION HEAT TREATED; Basic Shape Style: T SHAPE; Leg Thickness: 0.051 INCHES NOMINAL IN. 22 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-00-554-4986 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.