The Beam,structural, cataloged under National Stock Number 9540-01-363-8543, 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 24 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. 6 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-363-8543 |
| Primary Part Number | 1MA160D03-10089 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | The Boeing Company Div Defense |
| Status | ACTIVE |
| First Tip Radius | 0.078 INCHES NOMINAL IN |
| Heat Treatment | T-6511 SOLUTION HEAT TREATED |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Third Tip Style | FULL RADIUS |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Material | ALUMINUM ALLOY 7075 |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.277 POUNDS PER LINEAR FOOT LBS |
| Fabrication Method | EXTRUDED |
| Nondefinitive Spec/std Data | 7075 ALLOY AND T6511 TEMPER |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Material Document and Classification | AMS-QQ-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Third Tip Relationship to Preceding Tips | NOT IDENTICAL |
| Left Side Top Flange Distance to Center of Both Flanges | 1.000 INCHES NOMINAL IN |
| Basic Shape Style | T SHAPE |
| Leg Thickness | 0.078 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | IDENTICAL |
| Third Tip Radius | 0.039 INCHES NOMINAL IN |
| Top Flange Width | 2.000 INCHES NOMINAL IN |
| Right Side Top Flange Distance to Center of Both Flanges | 1.000 INCHES NOMINAL IN |
| First Tip Style | LOWER RADIUS |
| Right Side Top Flange Thickness | 0.078 INCHES NOMINAL IN |
| Left Side Top Flange Thickness | 0.078 INCHES NOMINAL IN |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AND10136-2001 | Airforce-Navy Aeronautical Design Standard |
| AMS10136-2001 | Society of Automotive Engineers Inc (USA) |
| 1MA160D03-10089 PRIMARY | The Boeing Company Div Defense (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| AND10136-2001/QQ-A-200/11-T6511 | Defense Logistics Agency Dba Defense Supply Center Philadelphia (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
| AMS10136-2001 | Sae International Dba Sae International (USA) |
NSN 9540-01-363-8543 is a Beam,structural, manufactured by The Boeing Company Div Defense, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-363-8543 has 8 cross-referenced part numbers: AND10136-2001 (Airforce-Navy Aeronautical Design Standard), AMS10136-2001 (Society of Automotive Engineers Inc), 1MA160D03-10089 (The Boeing Company Div Defense), AMS-QQ-A-200/11 (Society of Automotive Engineers Inc), AND10136-2001/QQ-A-200/11-T6511 (Defense Logistics Agency Dba Defense Supply Center Philadelphia) and 3 more.
There are 6 known substitutes for 9540-01-363-8543: 9540-00-242-5443, 9540-00-486-6388, 9540-00-555-0819 and 3 more. Verify interchangeability with system specifications before substitution.
Key specifications for 1MA160D03-10089: First Tip Radius: 0.078 INCHES NOMINAL IN; Heat Treatment: T-6511 SOLUTION HEAT TREATED; Length: 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT; Third Tip Style: FULL RADIUS. 25 total characteristics are documented in the Federal Logistics Information System.