The Beam,structural, cataloged under National Stock Number 9540-00-119-2133, 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 Cessna Aircraft Company Dba Textron Aviation. Government technical data includes 23 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 7 commercial cross-references from 7 manufacturers, enabling identification through both NSN and commercial part number lookups. 6 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-00-119-2133 |
| Primary Part Number | S318 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Cessna Aircraft Company Dba Textron Aviation |
| Status | ACTIVE |
| Third Tip Style | FULL RADIUS |
| Heat Treatment | T-3511 SOLUTION HEAT TREATED |
| Third Tip Relationship to Preceding Tips | NOT IDENTICAL |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Third Tip Radius | 0.094 INCHES NOMINAL IN |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.125 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | IDENTICAL |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Left Side Top Flange Distance to Center of Both Flanges | 0.938 INCHES NOMINAL IN |
| Left Side Top Flange Thickness | 0.094 INCHES NOMINAL IN |
| Leg Thickness | 0.094 INCHES NOMINAL IN |
| Basic Shape Style | T SHAPE |
| Nondefinitive Spec/std Data | 2024 ALLOY AND T3511 TEMPER |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| First Tip Radius | 0.094 INCHES NOMINAL IN |
| Right Side Top Flange Thickness | 0.094 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.320 POUNDS PER LINEAR FOOT LBS |
| Right Side Top Flange Distance to Center of Both Flanges | 0.938 INCHES NOMINAL IN |
| First Tip Style | LOWER RADIUS |
| Top Flange Width | 1.876 INCHES NOMINAL IN |
| Material Document and Classification | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE |
| Material | ALUMINUM ALLOY 2024 |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| S318 | Cessna Aircraft Company Dba Textron Aviation (USA) |
| AMS-QQ-A-200/3 | Sae International Dba Sae International (USA) |
| QQA200-3 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| S318 | Textron Aviation Inc (USA) |
| ASTM B221 | American Society for Testing and Materials Dba Astm International (USA) |
| AMS-QQ-A-200/3 | Society of Automotive Engineers Inc (USA) |
| AND10136-1702 | Airforce-Navy Aeronautical Design Standard |
NSN 9540-00-119-2133 is a Beam,structural, manufactured by Cessna Aircraft Company Dba Textron Aviation, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-00-119-2133 has 7 cross-referenced part numbers: S318 (Cessna Aircraft Company Dba Textron Aviation), AMS-QQ-A-200/3 (Sae International Dba Sae International), QQA200-3 (Federal Specifications Promulgated by General Services Administration Washington DC), S318 (Textron Aviation Inc), ASTM B221 (American Society for Testing and Materials Dba Astm International) and 2 more.
There are 6 known substitutes for 9540-00-119-2133: 5935-00-162-5006, 5330-00-251-3199, 3120-00-368-5839 and 3 more. Verify interchangeability with system specifications before substitution.
Key specifications for S318: Third Tip Style: FULL RADIUS; Heat Treatment: T-3511 SOLUTION HEAT TREATED; Third Tip Relationship to Preceding Tips: NOT IDENTICAL; Left Top Inside Angle: 90.0 DEGREES NOMINAL. 24 total characteristics are documented in the Federal Logistics Information System.