The Angle,structural, cataloged under National Stock Number 9540-00-727-8537, 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 Aluminum Co of America. Government technical data includes 17 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 20 commercial cross-references from 14 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 | 9540-00-727-8537 |
| Primary Part Number | 22885 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Aluminum Co of America |
| Status | ACTIVE |
| Weight Per Unit Measure | 0.130 POUNDS PER LINEAR FOOT LBS |
| Second Tip Radius | 0.031 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 2014 |
| Length | 12.000 FEET NOMINAL FT |
| Fillet Radius Where Left Flange Joins Base Flange | 0.062 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| First Tip Style | RIGHT QUARTER RADIUS |
| Fabrication Method | EXTRUDED |
| Basic Shape Style | ANGLE |
| Heat Treatment | T-4 SOLUTION HEAT TREATED |
| Nondefinitive Spec/std Data | 2024 ALLOY AND T4 TEMPER |
| Material Document and Classification | AMS-QQ-A-200/2 FED SPEC SINGLE MATERIAL RESPONSE |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Second Tip Style | UPPER RADIUS |
| Base Flange Thickness | 0.062 INCHES NOMINAL IN |
| First Tip Radius | 0.031 INCHES NOMINAL IN |
| Left Side Flange Thickness | 0.062 INCHES NOMINAL IN |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| 22385 | Aluminum Co of America (USA) |
| E121108 | Hughes Missile Systems Co San Diego (USA) |
| 4091 | Alcoa/reynolds Metals Company (USA) |
| AMS-STD-184 | Society of Automotive Engineers Inc (USA) |
| PA4065 | Transtar Metals Corp (USA) |
| 60-138 | Transtar Metals Corp (USA) |
| BAC1503-1511 | The Boeing Company Div Defense (USA) |
| QQA200-2 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| S107 | Cessna Aircraft Company Dba Textron Aviation (USA) |
| AMS-QQ-A-200/2 | Society of Automotive Engineers Inc (USA) |
| 22885 PRIMARY | Aluminum Co of America (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| PA4064 | Transtar Metals Corp (USA) |
| AMS-QQ-A-200/2 ALLOY 2014 TMPR T | Society of Automotive Engineers Inc (USA) |
| FS10101-1008-1 | Hiller Aircraft Corporation (USA) |
| E121108 | General Dynamics Corp Convair Div Lindbergh Field Facility (USA) |
| 4091 | Reynolds Metals Co (USA) |
| E121108 | Tracor Flight Systems Inc Sub of Tracor Inc (USA) |
| S179 | Cessna Aircraft Company Dba Textron Aviation (USA) |
| 15751 | International Light Metals Corp Sub of Martin Marietta Corp (USA) |
NSN 9540-00-727-8537 is a Angle,structural, manufactured by Aluminum Co of America, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-00-727-8537 has 20 cross-referenced part numbers: 22385 (Aluminum Co of America), E121108 (Hughes Missile Systems Co San Diego), 4091 (Alcoa/reynolds Metals Company), AMS-STD-184 (Society of Automotive Engineers Inc), PA4065 (Transtar Metals Corp) and 15 more.
There are 12 known substitutes for 9540-00-727-8537: 4820-00-071-2436, 3110-00-120-3732, 5330-00-152-0312 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for 22885: Weight Per Unit Measure: 0.130 POUNDS PER LINEAR FOOT LBS; Second Tip Radius: 0.031 INCHES NOMINAL IN; Material: ALUMINUM ALLOY 2014; Length: 12.000 FEET NOMINAL FT. 19 total characteristics are documented in the Federal Logistics Information System.