The Beam,structural, cataloged under National Stock Number 9540-00-988-8623, 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 23 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 10 commercial cross-references from 7 manufacturers, enabling identification through both NSN and commercial part number lookups. 12 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-00-988-8623 |
| Primary Part Number | S1383060 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | The Boeing Company |
| Status | ACTIVE |
| Fabrication Method | EXTRUDED |
| Weight Per Unit Measure | 1.310 POUNDS PER LINEAR FOOT LBS |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| First Tip Outer Radius | 0.031 INCHES NOMINAL IN |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Material | ALUMINUM ALLOY 7075 |
| Third Tip Relationship to Preceding Tips | IDENTICAL W/FIRST TIP |
| Heat Treatment | T-6 SOLUTION HEAT TREATED |
| Left Side Top Flange Distance to Center of Both Flanges | 1.312 INCHES NOMINAL IN |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.188 INCHES NOMINAL IN |
| Right Side Top Flange Thickness | 0.250 INCHES NOMINAL IN |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Nondefinitive Spec/std Data | T6 TEMPER |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.188 INCHES NOMINAL IN |
| Left Side Top Flange Thickness | 0.250 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | IDENTICAL |
| Leg Thickness | 0.250 INCHES NOMINAL IN |
| Top Flange Width | 2.625 INCHES NOMINAL IN |
| First Tip Inner Radius | 0.031 INCHES NOMINAL IN |
| First Tip Style | SQUARE W/ INNER AND OUTER CORNER RADII |
| Right Side Top Flange Distance to Center of Both Flanges | 1.313 INCHES NOMINAL IN |
| Basic Shape Style | T SHAPE |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| S1383060 | The Boeing Company (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| 59112 | Aluminum Co of America (USA) |
| PA6326 | Transtar Metals Corp (USA) |
| 56112 | International Light Metals Corp Sub of Martin Marietta Corp (USA) |
| S1383060 | The Boeing Company (USA) |
| 60-3018 | Transtar Metals Corp (USA) |
| 60-308 | Transtar Metals Corp (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
NSN 9540-00-988-8623 is a Beam,structural, manufactured by The Boeing Company, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-00-988-8623 has 10 cross-referenced part numbers: S1383060 (The Boeing Company), QQ-A-200/11 (Federal Specifications Promulgated by General Services Administration Washington DC), 59112 (Aluminum Co of America), PA6326 (Transtar Metals Corp), 56112 (International Light Metals Corp Sub of Martin Marietta Corp) and 5 more.
There are 12 known substitutes for 9540-00-988-8623: 5950-00-058-3816, 7510-00-224-6732, 4820-00-231-9664 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for S1383060: Fabrication Method: EXTRUDED; Weight Per Unit Measure: 1.310 POUNDS PER LINEAR FOOT LBS; Left Top Inside Angle: 90.0 DEGREES NOMINAL; First Tip Outer Radius: 0.031 INCHES NOMINAL IN. 24 total characteristics are documented in the Federal Logistics Information System.