The Angle,structural, cataloged under National Stock Number 9540-00-585-7202, 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 17 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 18 commercial cross-references from 13 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 | 9540-00-585-7202 |
| Primary Part Number | 1325738 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | The Boeing Company |
| Status | CANCELLED |
| Base Flange Thickness | 0.125 INCHES NOMINAL IN |
| Fillet Radius Where Left Flange Joins Base Flange | 0.156 INCHES NOMINAL IN |
| Fabrication Method | EXTRUDED |
| Material | ALUMINUM ALLOY 2014 |
| First Tip Style | RIGHT QUARTER RADIUS |
| First Tip Radius | 0.125 INCHES NOMINAL IN |
| Heat Treatment | T-4 SOLUTION HEAT TREATED |
| Weight Per Unit Measure | 0.390 POUNDS PER LINEAR FOOT LBS |
| Nondefinitive Spec/std Data | 2014 ALLOY AND T4 TEMPER |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Material Document and Classification | AMS-QQ-A-200/2 FED SPEC SINGLE MATERIAL RESPONSE |
| Second Tip Radius | 0.125 INCHES NOMINAL IN |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Left Side Flange Thickness | 0.125 INCHES NOMINAL IN |
| Second Tip Style | UPPER RADIUS |
| Basic Shape Style | ANGLE |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| 1325738 | The Boeing Company (USA) |
| S380-64BBDD | Kurz-Kasch Inc (USA) |
| 1325738 | The Boeing Company (USA) |
| AMS10134-1407 | Society of Automotive Engineers Inc (USA) |
| AND10134-1407 | Airforce-Navy Aeronautical Design Standard |
| QQ-A-200/2 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| AMS10134-1407 | Sae International Dba Sae International (USA) |
| 997258-01 | Ge Aviation Systems Llc (USA) |
| 7136 | Reynolds Metals Co (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| 15208 | International Light Metals Corp Sub of Martin Marietta Corp (USA) |
| AMS-QQ-A-200/2 | Society of Automotive Engineers Inc (USA) |
| 31444 | Bohn Aluminum and Brass Co Div of Gulf and Western Mfg Co Sub of Gulf and Western Industries (USA) |
| AMS-QQ-A-200/2 | Sae International Dba Sae International (USA) |
| 1243290 | The Boeing Company (USA) |
| 2-1308 | Lockheed Martin Corporation Div Rotary and Mission Systems (USA) |
| 1243290 | The Boeing Company (USA) |
| HA44 | Kaiser Aluminum and Chemical Corp Trentwood Works-Marketing Dept (USA) |
NSN 9540-00-585-7202 is a Angle,structural, manufactured by The Boeing Company, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-00-585-7202 has 18 cross-referenced part numbers: 1325738 (The Boeing Company), S380-64BBDD (Kurz-Kasch Inc), 1325738 (The Boeing Company), AMS10134-1407 (Society of Automotive Engineers Inc), AND10134-1407 (Airforce-Navy Aeronautical Design Standard) and 13 more.
There are 12 known substitutes for 9540-00-585-7202: 5995-00-054-4584, 2530-00-107-0043, 3110-00-135-9657 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for 1325738: Base Flange Thickness: 0.125 INCHES NOMINAL IN; Fillet Radius Where Left Flange Joins Base Flange: 0.156 INCHES NOMINAL IN; Fabrication Method: EXTRUDED; Material: ALUMINUM ALLOY 2014. 19 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-00-585-7202 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.