The Angle,structural, cataloged under National Stock Number 9540-00-197-9846, 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 Airforce-Navy Aeronautical Design Standard. Government technical data includes 27 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 5 commercial cross-references from 4 manufacturers, enabling identification through both NSN and commercial part number lookups. 5 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Cancelled.
| Parameter | Value |
|---|---|
| NSN | 9540-00-197-9846 |
| Primary Part Number | AND10134-2008 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Airforce-Navy Aeronautical Design Standard |
| Status | CANCELLED |
| Left Side Flange Thickness | 0.188 INCHES NOMINAL IN |
| Second Tip Style | UPPER RADIUS |
| Base Flange Thickness | 0.188 INCHES NOMINAL IN |
| Left Side Flange Thickness | 0.188 INCHES NOMINAL IN |
| Nondefinitive Spec/std Data | 6061 ALLOY AND T6 TEMPER |
| Second Tip Style | UPPER RADIUS |
| Material | ALUMINUM ALLOY 6061 |
| Basic Shape Style | ANGLE |
| Length | 20.000 FEET MINIMUM AND 30.000 FEET MAXIMUM FT |
| Heat Treatment | T-6 SOLUTION HEAT TREATED |
| Fillet Radius Where Left Flange Joins Base Flange | 0.188 INCHES NOMINAL IN |
| Base Flange Thickness | 0.188 INCHES NOMINAL IN |
| Material Document and Classification | AMS-QQ-A-200/8 FED SPEC SINGLE MATERIAL RESPONSE |
| Material | ALUMINUM ALLOY 6061 |
| First Tip Radius | 0.188 INCHES NOMINAL IN |
| Length | 20.000 FEET MINIMUM AND 30.000 FEET MAXIMUM FT |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| First Tip Radius | 0.188 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Second Tip Radius | 0.188 INCHES NOMINAL IN |
| Basic Shape Style | ANGLE |
| Nondefinitive Spec/std Data | 6061 ALLOY AND T6 TEMPER |
| Material Document and Classification | AMS-QQ-A-200/8 FED SPEC SINGLE MATERIAL RESPONSE |
| Fabrication Method | EXTRUDED |
| First Tip Style | RIGHT QUARTER RADIUS |
| Weight Per Unit Measure | 0.740 POUNDS PER LINEAR FOOT LBS |
| Weight Per Unit Measure | 0.740 POUNDS PER LINEAR FOOT LBS |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AND10134-2008 | Airforce-Navy Aeronautical Design Standard |
| AMS-QQ-A-200/8 | Society of Automotive Engineers Inc (USA) |
| QQ-A-200/8 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| SAE-AMS-QQ-A-200/8 | Sae International Dba Sae International (USA) |
| AMS-QQ-A-200/8 | Sae International Dba Sae International (USA) |
NSN 9540-00-197-9846 is a Angle,structural, manufactured by Airforce-Navy Aeronautical Design Standard, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-00-197-9846 has 5 cross-referenced part numbers: AND10134-2008 (Airforce-Navy Aeronautical Design Standard), AMS-QQ-A-200/8 (Society of Automotive Engineers Inc), QQ-A-200/8 (Federal Specifications Promulgated by General Services Administration Washington DC), SAE-AMS-QQ-A-200/8 (Sae International Dba Sae International), AMS-QQ-A-200/8 (Sae International Dba Sae International).
There are 5 known substitutes for 9540-00-197-9846: 9540-00-234-0598, 9540-00-542-2705, 9540-00-720-1762 and 2 more. Verify interchangeability with system specifications before substitution.
Key specifications for AND10134-2008: Left Side Flange Thickness: 0.188 INCHES NOMINAL IN; Second Tip Style: UPPER RADIUS; Base Flange Thickness: 0.188 INCHES NOMINAL IN; Left Side Flange Thickness: 0.188 INCHES NOMINAL IN. 30 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-00-197-9846 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.