The Angle,structural, cataloged under National Stock Number 9540-01-363-7422, 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 18 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 8 commercial cross-references from 7 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 | 9540-01-363-7422 |
| Primary Part Number | 1MA100D06-10027 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | The Boeing Company Div Defense |
| Status | ACTIVE |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Second Tip Style | SQUARE W/ INNER AND OUTER CORNER RADII |
| Heat Treatment | T-76511 SOLUTION HEAT TREATED |
| First Tip Inner Radius | 0.125 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 7075 |
| Fillet Radius Where Left Flange Joins Base Flange | 0.125 INCHES NOMINAL IN |
| Second Tip Outer Radius | 0.010 INCHES NOMINAL IN |
| First Tip Style | SQUARE W/ INNER AND OUTER CORNER RADII |
| Fabrication Method | EXTRUDED |
| Second Tip Inner Radius | 0.125 INCHES NOMINAL IN |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Basic Shape Style | ANGLE |
| Nondefinitive Spec/std Data | T76511 TEMPER |
| Weight Per Unit Measure | 0.231 POUNDS PER LINEAR FOOT LBS |
| Base Flange Thickness | 0.125 INCHES NOMINAL IN |
| First Tip Outer Radius | 0.010 INCHES NOMINAL IN |
| Left Side Flange Thickness | 0.125 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AMS 4317 | Society of Automotive Engineers Inc (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| QQ-A-200/15 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| AMS 4317 | Sae International Dba Sae International (USA) |
| AMS-QQ-A-200/15 | Society of Automotive Engineers Inc (USA) |
| 1MA100D06-10027 PRIMARY | The Boeing Company Div Defense (USA) |
| 10134-1004 | Transtar Metals Corp (USA) |
| AND10134-1004/QQ-A-200/15 | Airforce-Navy Aeronautical Design Standard |
NSN 9540-01-363-7422 is a Angle,structural, manufactured by The Boeing Company Div Defense, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-363-7422 has 8 cross-referenced part numbers: AMS 4317 (Society of Automotive Engineers Inc), ASTM B221 (American Society for Testing and Materials Dba Astm International), QQ-A-200/15 (Federal Specifications Promulgated by General Services Administration Washington DC), AMS 4317 (Sae International Dba Sae International), AMS-QQ-A-200/15 (Society of Automotive Engineers Inc) and 3 more.
There are 6 known substitutes for 9540-01-363-7422: 9540-01-169-6520, 9540-01-176-1078, 9540-01-363-7427 and 3 more. Verify interchangeability with system specifications before substitution.
Key specifications for 1MA100D06-10027: Left Inside Angle: 90.0 DEGREES NOMINAL; Second Tip Style: SQUARE W/ INNER AND OUTER CORNER RADII; Heat Treatment: T-76511 SOLUTION HEAT TREATED; Overall Height: 0.750 INCHES NOMINAL IN. 20 total characteristics are documented in the Federal Logistics Information System.