The Angle,structural, cataloged under National Stock Number 9540-00-251-3096, 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 Tracor Flight Systems Inc Sub of Tracor Inc. Government technical data includes 17 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 23 commercial cross-references from 18 manufacturers, enabling identification through both NSN and commercial part number lookups. 12 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-00-251-3096 |
| Primary Part Number | E121108 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Tracor Flight Systems Inc Sub of Tracor Inc |
| Status | ACTIVE |
| Material | ALUMINUM ALLOY 2024 |
| Weight Per Unit Measure | 0.130 POUNDS PER LINEAR FOOT LBS |
| Second Tip Style | UPPER RADIUS |
| First Tip Radius | 0.031 INCHES NOMINAL IN |
| Material Document and Classification | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| Fabrication Method | EXTRUDED |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Left Side Flange Thickness | 0.062 INCHES NOMINAL IN |
| Base Flange Thickness | 0.062 INCHES NOMINAL IN |
| First Tip Style | RIGHT QUARTER RADIUS |
| Fillet Radius Where Left Flange Joins Base Flange | 0.062 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Nondefinitive Spec/std Data | 2024 ALLOY AND T4 TEMPER |
| Basic Shape Style | ANGLE |
| Second Tip Radius | 0.031 INCHES NOMINAL IN |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Heat Treatment | T-4 SOLUTION HEAT TREATED |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| E121108 | Tracor Flight Systems Inc Sub of Tracor Inc (USA) |
| 15751 | International Light Metals Corp Sub of Martin Marietta Corp (USA) |
| BAC1503-1511 | The Boeing Company Div Legacy Wichita (USA) |
| S107 | Textron Aviation Inc (USA) |
| AMS-QQ-A-200/3 | Sae International Dba Sae International (USA) |
| S179 | Cessna Aircraft Company Dba Textron Aviation (USA) |
| 60-138 | Transtar Metals Corp (USA) |
| FS10101-1008-1 | Hiller Aircraft Corporation (USA) |
| 22885 | Aluminum Co of America (USA) |
| S107 | Cessna Aircraft Company Dba Textron Aviation (USA) |
| QQ-A-200/3 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| DIE22385 | Aluminum Co of America (USA) |
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
| PA4065 | Transtar Metals Corp (USA) |
| 50636 | National Distillers and Chemical Corp Bridgeport Brass Co Div (USA) |
| PA4064 | Transtar Metals Corp (USA) |
| E121108 | Bae Systems Technology Solutions & Services Inc. (USA) |
| 4091 | Reynolds Metals Co (USA) |
| E121108 | General Dynamics Corp Convair Div Lindbergh Field Facility (USA) |
| E121108 | Hughes Missile Systems Co San Diego (USA) |
NSN 9540-00-251-3096 is a Angle,structural, manufactured by Tracor Flight Systems Inc Sub of Tracor Inc, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-00-251-3096 has 23 cross-referenced part numbers: E121108 (Tracor Flight Systems Inc Sub of Tracor Inc), 15751 (International Light Metals Corp Sub of Martin Marietta Corp), BAC1503-1511 (The Boeing Company Div Legacy Wichita), S107 (Textron Aviation Inc), AMS-QQ-A-200/3 (Sae International Dba Sae International) and 18 more.
There are 12 known substitutes for 9540-00-251-3096: 3110-00-120-3732, 5330-00-152-0312, 3930-00-175-0084 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for E121108: Material: ALUMINUM ALLOY 2024; Weight Per Unit Measure: 0.130 POUNDS PER LINEAR FOOT LBS; Second Tip Style: UPPER RADIUS; First Tip Radius: 0.031 INCHES NOMINAL IN. 19 total characteristics are documented in the Federal Logistics Information System.