The Beam,structural, cataloged under National Stock Number 9540-01-363-6179, 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 Div Defense. Government technical data includes 23 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 7 commercial cross-references from 6 manufacturers, enabling identification through both NSN and commercial part number lookups. 8 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-363-6179 |
| Primary Part Number | 1MA160D01-10071 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | The Boeing Company Div Defense |
| Status | ACTIVE |
| Third Tip Style | FULL RADIUS |
| Nondefinitive Spec/std Data | O TEMPER |
| Material | ALUMINUM ALLOY 7075 |
| Right Side Top Flange Distance to Center of Both Flanges | 0.875 INCHES NOMINAL IN |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Right Side Top Flange Thickness | 0.156 INCHES NOMINAL IN |
| Left Side Top Flange Distance to Center of Both Flanges | 0.875 INCHES NOMINAL IN |
| Third Tip Relationship to Preceding Tips | NOT IDENTICAL |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Fabrication Method | EXTRUDED |
| First Tip Style | LOWER RADIUS |
| Third Tip Radius | 0.078 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.548 POUNDS PER LINEAR FOOT LBS |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Leg Thickness | 0.156 INCHES NOMINAL IN |
| First Tip Radius | 0.156 INCHES NOMINAL IN |
| Basic Shape Style | T SHAPE |
| Heat Treatment | O-ANNEALED |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Second Tip Relationship to First Tip | IDENTICAL |
| Left Side Top Flange Thickness | 0.156 INCHES NOMINAL IN |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Top Flange Width | 1.750 INCHES NOMINAL IN |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AMS 4476 | Sae International Dba Sae International (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
| 1MA160D01-10071 PRIMARY | The Boeing Company Div Defense (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| AND10136-1606/QQ-A-200/11-TO | Airforce-Navy Aeronautical Design Standard |
NSN 9540-01-363-6179 is a Beam,structural, manufactured by The Boeing Company Div Defense, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-363-6179 has 7 cross-referenced part numbers: AMS 4476 (Sae International Dba Sae International), AMS-QQ-A-200/11 (Society of Automotive Engineers Inc), AMS-QQ-A-200/11 (Sae International Dba Sae International), 1MA160D01-10071 (The Boeing Company Div Defense), ASTM B221 (American Society for Testing and Materials Dba Astm International) and 2 more.
There are 8 known substitutes for 9540-01-363-6179: 9540-00-006-8478, 9540-01-369-9117, 9540-01-428-2774 and 5 more. Verify interchangeability with system specifications before substitution.
Key specifications for 1MA160D01-10071: Third Tip Style: FULL RADIUS; Overall Height: 1.375 INCHES NOMINAL IN; Nondefinitive Spec/std Data: O TEMPER; Material: ALUMINUM ALLOY 7075. 24 total characteristics are documented in the Federal Logistics Information System.