The Beam,structural, cataloged under National Stock Number 9540-00-720-1332, 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 Northrop Grumman Systems Corporation. Government technical data includes 24 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 15 commercial cross-references from 12 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 | 9540-00-720-1332 |
| Primary Part Number | RY32013 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Northrop Grumman Systems Corporation |
| Status | CANCELLED |
| Basic Shape Style | T SHAPE |
| Weight Per Unit Measure | 0.420 POUNDS PER LINEAR FOOT LBS |
| Leg Thickness | 0.094 INCHES NOMINAL IN |
| First Tip Radius | 0.094 INCHES NOMINAL IN |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Third Tip Relationship to Preceding Tips | NOT IDENTICAL |
| Material | ALUMINUM ALLOY 7075 |
| Left Side Top Flange Thickness | 0.094 INCHES NOMINAL IN |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Third Tip Style | FULL RADIUS |
| First Tip Style | LOWER RADIUS |
| Top Flange Width | 2.500 INCHES NOMINAL IN |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Heat Treatment | O-ANNEALED |
| Fabrication Method | EXTRUDED |
| Second Tip Relationship to First Tip | IDENTICAL |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Left Side Top Flange Distance to Center of Both Flanges | 1.250 INCHES NOMINAL IN |
| Nondefinitive Spec/std Data | O TEMPER |
| Third Tip Radius | 0.047 INCHES NOMINAL IN |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Right Side Top Flange Distance to Center of Both Flanges | 1.250 INCHES NOMINAL IN |
| Right Side Top Flange Thickness | 0.094 INCHES NOMINAL IN |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Acquisition Status | CANCELLED |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| RY32013 | Northrop Grumman Systems Corporation (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| 40196 | Bohn Aluminum and Brass Co Div of Gulf and Western Mfg Co Sub of Gulf and Western Industries (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| AMS 10136-2401 | Sae International Dba Sae International (USA) |
| AND10136-2401/ASTM B221-0 | Defense Logistics Agency Dba Defense Supply Center Philadelphia (USA) |
| HT200 | Kaiser Aluminum and Chemical Corp Trentwood Works-Marketing Dept (USA) |
| AMS 10136-2401 | Society of Automotive Engineers Inc (USA) |
| S1245835 | The Boeing Company (USA) |
| 10136-2401 | Transtar Metals Corp (USA) |
| AND10136-2401 | Airforce-Navy Aeronautical Design Standard |
| 8726 | Reynolds Metals Co (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
| S1245835 | The Boeing Company (USA) |
NSN 9540-00-720-1332 is a Beam,structural, manufactured by Northrop Grumman Systems Corporation, classified under FSC 9540 (No Item Name Available). Status: cancelled.
NSN 9540-00-720-1332 has 15 cross-referenced part numbers: RY32013 (Northrop Grumman Systems Corporation), QQ-A-200/11 (Federal Specifications Promulgated by General Services Administration Washington DC), AMS-QQ-A-200/11 (Society of Automotive Engineers Inc), 40196 (Bohn Aluminum and Brass Co Div of Gulf and Western Mfg Co Sub of Gulf and Western Industries), ASTM B221 (American Society for Testing and Materials Dba Astm International) and 10 more.
There are 12 known substitutes for 9540-00-720-1332: 5330-00-146-9532, 9540-00-236-3943, 9540-00-236-5241 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for RY32013: Basic Shape Style: T SHAPE; Weight Per Unit Measure: 0.420 POUNDS PER LINEAR FOOT LBS; Leg Thickness: 0.094 INCHES NOMINAL IN; First Tip Radius: 0.094 INCHES NOMINAL IN. 25 total characteristics are documented in the Federal Logistics Information System.
NSN 9540-00-720-1332 is currently cancelled. Check with the Defense Logistics Agency for current availability and authorized substitutes.