The Channel,structural, cataloged under National Stock Number 9540-01-125-6393, 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 23 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 11 commercial cross-references from 9 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 | 9540-01-125-6393 |
| Primary Part Number | AND10137-1003 |
| Item Name | Channel,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Airforce-Navy Aeronautical Design Standard |
| Status | CANCELLED |
| Left Side Flange Height | 0.625 INCHES NOMINAL IN |
| Fillet Radius Where Left Flange Joins Base Flange | 0.125 INCHES NOMINAL IN |
| Base Flange Thickness | 0.063 INCHES NOMINAL IN |
| Right Inside Angle | 90.0 DEGREES NOMINAL |
| Fillet Radius Where Right Flange Joins Base Flange | 0.125 INCHES NOMINAL IN |
| First Tip Radius | 0.063 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 2024 |
| Basic Shape Style | CHANNEL |
| Second Tip Style | LEFT QUARTER RADIUS |
| Right Side Flange Thickness | 0.063 INCHES NOMINAL IN |
| First Tip Style | RIGHT QUARTER RADIUS |
| Right Side Flange Height | 0.625 INCHES NOMINAL IN |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Material Document and Classification | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| Fabrication Method | EXTRUDED |
| Nondefinitive Spec/std Data | T3511 TEMPER |
| Specification/standard Data | 81755-K20 MANUFACTURERS STANDARD |
| Weight Per Unit Measure | 0.167 POUNDS PER LINEAR FOOT LBS |
| Left Side Flange Thickness | 0.063 INCHES NOMINAL IN |
| Heat Treatment | T-3511 SOLUTION HEAT TREATED |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Second Tip Radius | 0.063 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AND10137-1003 | Airforce-Navy Aeronautical Design Standard |
| 9540PL1013489 | Jednolity Indeks Materialowy - Uniform Material Index (POL) |
| MS14366E027 | Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M |
| AND10137-1001 | Aeronautical Standards Group Dept of Navy and Air Force (USA) |
| K20A15T3511 | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company (USA) |
| QQ-A-200/3 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| AND10137-1001 | Airforce-Navy Aeronautical Design Standard |
| QQA267TEMPERT4 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| 10137-1003 | Transtar Metals Corp (USA) |
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
| AMS-QQ-A-200/3 | Sae International Dba Sae International (USA) |
NSN 9540-01-125-6393 is a Channel,structural, manufactured by Airforce-Navy Aeronautical Design Standard, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-01-125-6393 has 11 cross-referenced part numbers: AND10137-1003 (Airforce-Navy Aeronautical Design Standard), 9540PL1013489 (Jednolity Indeks Materialowy - Uniform Material Index), MS14366E027 (Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M), AND10137-1001 (Aeronautical Standards Group Dept of Navy and Air Force), K20A15T3511 (Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company) and 6 more.
There are 5 known substitutes for 9540-01-125-6393: 9540-00-595-8549, 9540-00-596-2971, 9540-00-596-3160 and 2 more. Verify interchangeability with system specifications before substitution.
Key specifications for AND10137-1003: Left Side Flange Height: 0.625 INCHES NOMINAL IN; Fillet Radius Where Left Flange Joins Base Flange: 0.125 INCHES NOMINAL IN; Base Flange Thickness: 0.063 INCHES NOMINAL IN; Right Inside Angle: 90.0 DEGREES NOMINAL. 24 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-01-125-6393 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.