The Beam,structural, cataloged under National Stock Number 9540-00-555-0819, 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 16 commercial cross-references from 13 manufacturers, enabling identification through both NSN and commercial part number lookups. 12 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Cancelled.
| Parameter | Value |
|---|---|
| NSN | 9540-00-555-0819 |
| Primary Part Number | FS50102-2010 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Hiller Aircraft Corporation |
| Status | CANCELLED |
| Third Tip Style | FULL RADIUS |
| Basic Shape Style | T SHAPE |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Right Side Top Flange Thickness | 0.078 INCHES NOMINAL IN |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 7075 |
| Left Side Top Flange Thickness | 0.078 INCHES NOMINAL IN |
| Top Flange Width | 2.000 INCHES NOMINAL IN |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Third Tip Relationship to Preceding Tips | NOT IDENTICAL |
| First Tip Radius | 0.078 INCHES NOMINAL IN |
| Nondefinitive Spec/std Data | T6 TEMPER |
| Weight Per Unit Measure | 0.277 POUNDS PER LINEAR FOOT LBS |
| Heat Treatment | T-6 SOLUTION HEAT TREATED |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Fabrication Method | EXTRUDED |
| Left Side Top Flange Distance to Center of Both Flanges | 1.000 INCHES NOMINAL IN |
| First Tip Style | LOWER RADIUS |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Second Tip Relationship to First Tip | IDENTICAL |
| Leg Thickness | 0.078 INCHES NOMINAL IN |
| Third Tip Radius | 0.039 INCHES NOMINAL IN |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Right Side Top Flange Distance to Center of Both Flanges | 1.000 INCHES NOMINAL IN |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| FS50102-2010 | Hiller Aircraft Corporation (USA) |
| 6352 | Reynolds Metals Co (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| AND10136-2001 | Airforce-Navy Aeronautical Design Standard |
| RY32009 | Northrop Grumman Systems Corporation (USA) |
| 1325206 | The Boeing Company (USA) |
| 40290 | Bohn Aluminum and Brass Co Div of Gulf and Western Mfg Co Sub of Gulf and Western Industries (USA) |
| 1325206 | The Boeing Company (USA) |
| S140 | Textron Aviation Inc (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| HT192 | Kaiser Aluminum and Chemical Corp Trentwood Works-Marketing Dept (USA) |
| 18387 | International Light Metals Corp Sub of Martin Marietta Corp (USA) |
| AMS10136-2001 | Sae International Dba Sae International (USA) |
| S140 | Cessna Aircraft Company Dba Textron Aviation (USA) |
| AMS10136-2001 | Society of Automotive Engineers Inc (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
NSN 9540-00-555-0819 is a Beam,structural, manufactured by Hiller Aircraft Corporation, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-00-555-0819 has 16 cross-referenced part numbers: FS50102-2010 (Hiller Aircraft Corporation), 6352 (Reynolds Metals Co), AMS-QQ-A-200/11 (Society of Automotive Engineers Inc), AND10136-2001 (Airforce-Navy Aeronautical Design Standard), RY32009 (Northrop Grumman Systems Corporation) and 11 more.
There are 12 known substitutes for 9540-00-555-0819: 5305-00-010-0149, 5960-00-038-1637, 6685-00-075-6867 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for FS50102-2010: Third Tip Style: FULL RADIUS; Basic Shape Style: T SHAPE; Length: 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT; Right Side Top Flange Thickness: 0.078 INCHES NOMINAL IN. 25 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-00-555-0819 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.