The Angle,structural, cataloged under National Stock Number 9540-00-288-3735, 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 Society of Automotive Engineers Inc. Government technical data includes 17 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 16 commercial cross-references from 15 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 | 9540-00-288-3735 |
| Primary Part Number | AMS-QQ-A-200/3 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Society of Automotive Engineers Inc |
| Status | ACTIVE |
| Fabrication Method | EXTRUDED |
| Second Tip Radius | 0.125 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 2024 |
| Weight Per Unit Measure | 0.830 POUNDS PER LINEAR FOOT LBS |
| Fillet Radius Where Left Flange Joins Base Flange | 0.188 INCHES NOMINAL IN |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Second Tip Style | UPPER RADIUS |
| Basic Shape Style | ANGLE |
| Left Side Flange Thickness | 0.250 INCHES NOMINAL IN |
| First Tip Radius | 0.125 INCHES NOMINAL IN |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| First Tip Style | RIGHT QUARTER RADIUS |
| Nondefinitive Spec/std Data | 2024 ALLOY AND T3511 TEMPER |
| Material Document and Classification | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| Heat Treatment | T-3511 SOLUTION HEAT TREATED |
| Base Flange Thickness | 0.250 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
| 16011 | International Light Metals Corp Sub of Martin Marietta Corp (USA) |
| S189 | Cessna Aircraft Company Dba Textron Aviation (USA) |
| BAC1503-5826 | The Boeing Company Div Legacy Wichita (USA) |
| 1M133 | The Boeing Company Div Defense (USA) |
| 13880-3 | International Light Metals Corp Sub of Martin Marietta Corp (USA) |
| 50310 | National Distillers and Chemical Corp Bridgeport Brass Co Div (USA) |
| 5928 | Bohn Aluminum and Brass Co Div of Gulf and Western Mfg Co Sub of Gulf and Western Industries (USA) |
| QQ-A-200/3 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| LS3395 | Lockheed Martin Corp (USA) |
| 77D | Aluminum Co of America (USA) |
| 5742 | Alcoa/reynolds Metals Company (USA) |
| 2055 | Reynolds Metals Co (USA) |
| S189 | Textron Aviation Inc (USA) |
| AMS-QQ-A-200/3 | Sae International Dba Sae International (USA) |
NSN 9540-00-288-3735 is a Angle,structural, manufactured by Society of Automotive Engineers Inc, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-00-288-3735 has 16 cross-referenced part numbers: AMS-QQ-A-200/3 (Society of Automotive Engineers Inc), 16011 (International Light Metals Corp Sub of Martin Marietta Corp), S189 (Cessna Aircraft Company Dba Textron Aviation), BAC1503-5826 (The Boeing Company Div Legacy Wichita), 1M133 (The Boeing Company Div Defense) and 11 more.
There are 12 known substitutes for 9540-00-288-3735: 5305-00-091-4013, 4810-00-202-5594, 3110-00-227-2981 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for AMS-QQ-A-200/3: Fabrication Method: EXTRUDED; Overall Height: 1.500 INCHES NOMINAL IN; Second Tip Radius: 0.125 INCHES NOMINAL IN; Material: ALUMINUM ALLOY 2024. 19 total characteristics are documented in the Federal Logistics Information System.