The Beam,structural, cataloged under National Stock Number 9540-00-684-6190, 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 24 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. 9 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-00-684-6190 |
| Primary Part Number | AMS-QQ-A-200/11 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Society of Automotive Engineers Inc |
| Status | ACTIVE |
| Leg Thickness | 0.125 INCHES NOMINAL IN |
| Fabrication Method | EXTRUDED |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Basic Shape Style | T SHAPE |
| First Tip Style | FULL RADIUS |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 7075 |
| Left Side Top Flange Thickness | 0.125 INCHES NOMINAL IN |
| Nondefinitive Spec/std Data | T6 TEMPER |
| Second Tip Relationship to First Tip | IDENTICAL |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Right Side Top Flange Distance to Center of Both Flanges | 3.550 INCHES NOMINAL IN |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Top Flange Width | 4.875 INCHES NOMINAL IN |
| Third Tip Relationship to Preceding Tips | NOT IDENTICAL |
| Right Side Top Flange Thickness | 0.125 INCHES NOMINAL IN |
| Third Tip Style | LEFT QUARTER RADIUS |
| Left Side Top Flange Distance to Center of Both Flanges | 1.325 INCHES NOMINAL IN |
| Third Tip Radius | 0.063 INCHES NOMINAL IN |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| First Tip Radius | 0.063 INCHES NOMINAL IN |
| Heat Treatment | T-6 SOLUTION HEAT TREATED |
| Weight Per Unit Measure | 0.850 POUNDS PER LINEAR FOOT LBS |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| PA12499 | Transtar Metals Corp (USA) |
| 22652 | Alcoa/reynolds Metals Company (USA) |
| S6105-2133 | Sikorsky Aircraft Corporation Dba Sikorsky Aircraft Corp (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
| 60-12464 | Transtar Metals Corp (USA) |
| 46690 | International Light Metals Corp Sub of Martin Marietta Corp (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
NSN 9540-00-684-6190 is a Beam,structural, manufactured by Society of Automotive Engineers Inc, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-00-684-6190 has 8 cross-referenced part numbers: AMS-QQ-A-200/11 (Society of Automotive Engineers Inc), PA12499 (Transtar Metals Corp), 22652 (Alcoa/reynolds Metals Company), S6105-2133 (Sikorsky Aircraft Corporation Dba Sikorsky Aircraft Corp), AMS-QQ-A-200/11 (Sae International Dba Sae International) and 3 more.
There are 9 known substitutes for 9540-00-684-6190: 5935-00-088-0200, 5930-00-259-7876, 2805-00-361-7436 and 6 more. Verify interchangeability with system specifications before substitution.
Key specifications for AMS-QQ-A-200/11: Leg Thickness: 0.125 INCHES NOMINAL IN; Fabrication Method: EXTRUDED; Length: 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT; Fillet Radius Where Top Left Flange Joins Web Flange/leg: 0.125 INCHES NOMINAL IN. 25 total characteristics are documented in the Federal Logistics Information System.