The Angle,structural, cataloged under National Stock Number 9540-01-166-6927, 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 Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company. Government technical data includes 17 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 9 commercial cross-references from 9 manufacturers, enabling identification through both NSN and commercial part number lookups. 7 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-166-6927 |
| Primary Part Number | K10D29T76511 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company |
| Status | ACTIVE |
| Left Side Flange Thickness | 0.063 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 7075 |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Base Flange Thickness | 0.063 INCHES NOMINAL IN |
| Heat Treatment | T-76511 SOLUTION HEAT TREATED |
| Basic Shape Style | ANGLE |
| Material Document and Classification | AMS-Q-A-200/15 FED SPEC SINGLE MATERIAL RESPONSE |
| First Tip Style | RIGHT QUARTER RADIUS |
| Nondefinitive Spec/std Data | 7075 ALLOY AND T76511 TEMPER |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Fillet Radius Where Left Flange Joins Base Flange | 0.125 INCHES NOMINAL IN |
| First Tip Radius | 0.063 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.150 POUNDS PER LINEAR FOOT LBS |
| Second Tip Radius | 0.063 INCHES NOMINAL IN |
| Fabrication Method | EXTRUDED |
| Second Tip Style | UPPER RADIUS |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| K10D29T76511 | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company (USA) |
| 10134-1201 | Transtar Metals Corp (USA) |
| 10164602 | Nimikkeistokeskus Ncb Finland (FIN) |
| AMS-QQ-A-200/15 | Sae International Dba Sae International (USA) |
| 1MA100D06-10044 | The Boeing Company Div Defense (USA) |
| AMS-QQ-A-200/15 | Society of Automotive Engineers Inc (USA) |
| QQ-A-200/15 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| AND10134-1201 | Airforce-Navy Aeronautical Design Standard |
NSN 9540-01-166-6927 is a Angle,structural, manufactured by Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-166-6927 has 9 cross-referenced part numbers: K10D29T76511 (Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company), 10134-1201 (Transtar Metals Corp), 10164602 (Nimikkeistokeskus Ncb Finland), AMS-QQ-A-200/15 (Sae International Dba Sae International), 1MA100D06-10044 (The Boeing Company Div Defense) and 4 more.
There are 7 known substitutes for 9540-01-166-6927: 9540-00-145-4524, 9540-00-185-3995, 4730-00-268-3696 and 4 more. Verify interchangeability with system specifications before substitution.
Key specifications for K10D29T76511: Left Side Flange Thickness: 0.063 INCHES NOMINAL IN; Material: ALUMINUM ALLOY 7075; Left Inside Angle: 90.0 DEGREES NOMINAL; Base Flange Thickness: 0.063 INCHES NOMINAL IN. 19 total characteristics are documented in the Federal Logistics Information System.