The Angle,structural, cataloged under National Stock Number 9540-00-119-9028, 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 Hiller Aircraft Corporation. Government technical data includes 16 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 10 commercial cross-references from 10 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 | 9540-00-119-9028 |
| Primary Part Number | FS10103-1612-2 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Hiller Aircraft Corporation |
| Status | ACTIVE |
| Base Flange Thickness | 0.125 INCHES NOMINAL IN |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Material Document and Classification | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| Second Tip Style | UPPER RADIUS |
| Left Side Flange Thickness | 0.125 INCHES NOMINAL IN |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Material | ALUMINUM ALLOY 2024 |
| Heat Treatment | T-3511 SOLUTION HEAT TREATED |
| Nondefinitive Spec/std Data | 2024 ALLOY AND T3511 TEMPER |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Fillet Radius Where Left Flange Joins Base Flange | 0.125 INCHES NOMINAL IN |
| First Tip Radius | 0.125 INCHES NOMINAL IN |
| Basic Shape Style | ANGLE |
| First Tip Style | RIGHT QUARTER RADIUS |
| Weight Per Unit Measure | 0.410 POUNDS PER LINEAR FOOT LBS |
| Second Tip Radius | 0.125 INCHES NOMINAL IN |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| FS10103-1612-2 | Hiller Aircraft Corporation (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| 60-1451 | Transtar Metals Corp (USA) |
| QQ-A-200/3 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| AMS-QQ-A-200/3 | Sae International Dba Sae International (USA) |
| LS3441 | Lockheed Martin Corp (USA) |
| 734-2 | Aluminum Co of America (USA) |
| 5739 | Alcoa/reynolds Metals Company (USA) |
| BAC1503-4223 | The Boeing Company Div Legacy Wichita (USA) |
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
NSN 9540-00-119-9028 is a Angle,structural, manufactured by Hiller Aircraft Corporation, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-00-119-9028 has 10 cross-referenced part numbers: FS10103-1612-2 (Hiller Aircraft Corporation), ASTM B221 (American Society for Testing and Materials Dba Astm International), 60-1451 (Transtar Metals Corp), QQ-A-200/3 (Federal Specifications Promulgated by General Services Administration Washington DC), AMS-QQ-A-200/3 (Sae International Dba Sae International) and 5 more.
There are 7 known substitutes for 9540-00-119-9028: 3110-00-100-0637, 4510-00-126-8879, 9540-00-145-8422 and 4 more. Verify interchangeability with system specifications before substitution.
Key specifications for FS10103-1612-2: Base Flange Thickness: 0.125 INCHES NOMINAL IN; Length: 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT; Material Document and Classification: AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE; Overall Height: 1.250 INCHES NOMINAL IN. 18 total characteristics are documented in the Federal Logistics Information System.