The Angle,structural, cataloged under National Stock Number 9540-01-071-4712, 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 15 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 10 commercial cross-references from 9 manufacturers, enabling identification through both NSN and commercial part number lookups. 6 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Cancelled.
| Parameter | Value |
|---|---|
| NSN | 9540-01-071-4712 |
| Primary Part Number | K10A10T3511 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company |
| Status | CANCELLED |
| Base Flange Thickness | 0.050 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | IDENTICAL |
| Material | ALUMINUM ALLOY 2024 |
| Left Side Flange Thickness | 0.050 INCHES NOMINAL IN |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Nondefinitive Spec/std Data | T3511 TEMPER |
| Fabrication Method | EXTRUDED |
| First Tip Style | SQUARE END |
| Specification/standard Data | 81755-K10 MANUFACTURERS STANDARD |
| Material Document and Classification | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| Fillet Radius Where Left Flange Joins Base Flange | 0.125 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.166 POUNDS PER LINEAR FOOT LBS |
| Basic Shape Style | ANGLE |
| Heat Treatment | T-3511 SOLUTION HEAT TREATED |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| K10A10T3511 | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company (USA) |
| 23098 | Alcoa/reynolds Metals Company (USA) |
| MS14284E171 | Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M |
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
| PA4187 | Transtar Metals Corp (USA) |
| QQ-A-200/3 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| 69945 | Aluminum Co of America (USA) |
| 60-3703 | Transtar Metals Corp (USA) |
| 50183-A | Pimalco Inc. Div Alcoa Inc Global Hard Alloy Extrusions (USA) |
| AMS-QQ-A-200/3 | Sae International Dba Sae International (USA) |
NSN 9540-01-071-4712 is a Angle,structural, manufactured by Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-01-071-4712 has 10 cross-referenced part numbers: K10A10T3511 (Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company), 23098 (Alcoa/reynolds Metals Company), MS14284E171 (Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M), AMS-QQ-A-200/3 (Society of Automotive Engineers Inc), PA4187 (Transtar Metals Corp) and 5 more.
There are 6 known substitutes for 9540-01-071-4712: 6645-00-536-1529, 3020-00-811-3149, 5940-01-052-2413 and 3 more. Verify interchangeability with system specifications before substitution.
Key specifications for K10A10T3511: Base Flange Thickness: 0.050 INCHES NOMINAL IN; Second Tip Relationship to First Tip: IDENTICAL; Material: ALUMINUM ALLOY 2024; Left Side Flange Thickness: 0.050 INCHES NOMINAL IN. 17 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-01-071-4712 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.