The Angle,structural, cataloged under National Stock Number 9540-01-071-3506, 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 6 commercial cross-references from 5 manufacturers, enabling identification through both NSN and commercial part number lookups. 5 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-071-3506 |
| Primary Part Number | K10B99T6511 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company |
| Status | ACTIVE |
| First Tip Style | RIGHT QUARTER RADIUS |
| Base Flange Thickness | 0.125 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.360 POUNDS PER LINEAR FOOT LBS |
| Basic Shape Style | ANGLE |
| Second Tip Radius | 0.125 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 6061 |
| Heat Treatment | T-6511 SOLUTION HEAT TREATED |
| Second Tip Style | UPPER RADIUS |
| Nondefinitive Spec/std Data | T6511 TEMPER |
| Material Document and Classification | AMS-QQ-A-200/8 FED SPEC SINGLE MATERIAL RESPONSE |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Left Side Flange Thickness | 0.125 INCHES NOMINAL IN |
| Fillet Radius Where Left Flange Joins Base Flange | 0.188 INCHES NOMINAL IN |
| First Tip Radius | 0.125 INCHES NOMINAL IN |
| Fabrication Method | EXTRUDED |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| K10B99T6511 | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company (USA) |
| AMS-QQ-A-200/8 | Society of Automotive Engineers Inc (USA) |
| SAE-AMS-QQ-A-200/8 | Sae International Dba Sae International (USA) |
| AND10133-1203 | Airforce-Navy Aeronautical Design Standard |
| AMS-QQ-A-200/8 | Sae International Dba Sae International (USA) |
| QQ-A-200/8 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
NSN 9540-01-071-3506 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 9540-01-071-3506 has 6 cross-referenced part numbers: K10B99T6511 (Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company), AMS-QQ-A-200/8 (Society of Automotive Engineers Inc), SAE-AMS-QQ-A-200/8 (Sae International Dba Sae International), AND10133-1203 (Airforce-Navy Aeronautical Design Standard), AMS-QQ-A-200/8 (Sae International Dba Sae International) and 1 more.
There are 5 known substitutes for 9540-01-071-3506: 9540-00-145-8399, 9540-00-184-2801, 9540-00-197-9840 and 2 more. Verify interchangeability with system specifications before substitution.
Key specifications for K10B99T6511: First Tip Style: RIGHT QUARTER RADIUS; Base Flange Thickness: 0.125 INCHES NOMINAL IN; Overall Height: 1.250 INCHES NOMINAL IN; Weight Per Unit Measure: 0.360 POUNDS PER LINEAR FOOT LBS. 19 total characteristics are documented in the Federal Logistics Information System.