The Beam,structural, cataloged under National Stock Number 9540-00-596-3208, 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 24 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. 12 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-00-596-3208 |
| Primary Part Number | FS50102-1410-1 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Hiller Aircraft Corporation |
| Status | ACTIVE |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Third Tip Radius | 0.047 INCHES NOMINAL IN |
| Nondefinitive Spec/std Data | T4 TEMPER |
| Material Document and Classification | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE |
| Material | ALUMINUM ALLOY 2024 |
| Heat Treatment | T-4 SOLUTION HEAT TREATED |
| First Tip Radius | 0.094 INCHES NOMINAL IN |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Leg Thickness | 0.094 INCHES NOMINAL IN |
| Left Side Top Flange Thickness | 0.094 INCHES NOMINAL IN |
| Third Tip Style | FULL RADIUS |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Second Tip Relationship to First Tip | IDENTICAL |
| Fabrication Method | EXTRUDED |
| Left Side Top Flange Distance to Center of Both Flanges | 0.687 INCHES NOMINAL IN |
| Top Flange Width | 1.375 INCHES NOMINAL IN |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.260 POUNDS PER LINEAR FOOT LBS |
| Third Tip Relationship to Preceding Tips | NOT IDENTICAL |
| First Tip Style | LOWER RADIUS |
| Basic Shape Style | T SHAPE |
| Right Side Top Flange Thickness | 0.094 INCHES NOMINAL IN |
| Right Side Top Flange Distance to Center of Both Flanges | 0.688 INCHES NOMINAL IN |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| FS50102-1410-1 | Hiller Aircraft Corporation (USA) |
| HT159 | Kaiser Aluminum and Chemical Corp Trentwood Works-Marketing Dept (USA) |
| 50372 | National Distillers and Chemical Corp Bridgeport Brass Co Div (USA) |
| 32003 | Northrop Grumman Systems Corporation (USA) |
| QQ-A-267 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| DIEAND10136-1304 | Aluminum Co of America (USA) |
| AMS-QQ-A-200/3 | Sae International Dba Sae International (USA) |
| QQ-A-200/3 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| 31277 | Bohn Aluminum and Brass Co Div of Gulf and Western Mfg Co Sub of Gulf and Western Industries (USA) |
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
NSN 9540-00-596-3208 is a Beam,structural, manufactured by Hiller Aircraft Corporation, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-00-596-3208 has 10 cross-referenced part numbers: FS50102-1410-1 (Hiller Aircraft Corporation), HT159 (Kaiser Aluminum and Chemical Corp Trentwood Works-Marketing Dept), 50372 (National Distillers and Chemical Corp Bridgeport Brass Co Div), 32003 (Northrop Grumman Systems Corporation), QQ-A-267 (Federal Specifications Promulgated by General Services Administration Washington DC) and 5 more.
There are 12 known substitutes for 9540-00-596-3208: 5330-00-383-8779, 3110-00-421-9388, 5930-00-432-2731 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for FS50102-1410-1: Left Top Inside Angle: 90.0 DEGREES NOMINAL; Fillet Radius Where Top Right Flange Joins Web Flange/leg: 0.125 INCHES NOMINAL IN; Third Tip Radius: 0.047 INCHES NOMINAL IN; Nondefinitive Spec/std Data: T4 TEMPER. 25 total characteristics are documented in the Federal Logistics Information System.