The Beam,structural, cataloged under National Stock Number 9540-01-199-4602, 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 Airforce-Navy Aeronautical Design Standard. Government technical data includes 22 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 6 commercial cross-references from 6 manufacturers, enabling identification through both NSN and commercial part number lookups. 3 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-199-4602 |
| Primary Part Number | AND10138-0403 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Airforce-Navy Aeronautical Design Standard |
| Status | ACTIVE |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.094 INCHES NOMINAL IN |
| Fabrication Method | EXTRUDED |
| Web Flange Thickness | 0.050 INCHES NOMINAL IN |
| First Tip Radius | 0.050 INCHES NOMINAL IN |
| Material | ALUMINUM ALLOY 7075 |
| Basic Shape Style | Z SHAPE |
| Weight Per Unit Measure | 0.118 POUNDS PER LINEAR FOOT LBS |
| Material Document and Classification | AMS-Q-A-200/15 FED SPEC SINGLE MATERIAL RESPONSE |
| Nondefinitive Spec/std Data | T76511 TEMPER |
| Top Flange Width | 0.750 INCHES NOMINAL IN |
| First Tip Style | LOWER RADIUS |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Right Bottom Inside Angle | 90.0 DEGREES NOMINAL |
| Bottom Flange Width | 0.750 INCHES NOMINAL IN |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Fillet Radius Where Bottom Right Flange Joins Web Flange/leg | 0.094 INCHES NOMINAL IN |
| Second Tip Radius | 0.050 INCHES NOMINAL IN |
| Left Side Top Flange Thickness | 0.050 INCHES NOMINAL IN |
| Right Side Bottom Flange Thickness | 0.050 INCHES NOMINAL IN |
| Heat Treatment | T-76511 SOLUTION HEAT TREATED |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Second Tip Style | UPPER RADIUS |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| AND10138-0403 | Airforce-Navy Aeronautical Design Standard |
| AMS-QQ-A-200/15 | Sae International Dba Sae International (USA) |
| 1MA180D06-10007 | The Boeing Company Div Defense (USA) |
| QQ-A-200/15 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| 10138-0403 | Transtar Metals Corp (USA) |
| AMS-QQ-A-200/15 | Society of Automotive Engineers Inc (USA) |
NSN 9540-01-199-4602 is a Beam,structural, manufactured by Airforce-Navy Aeronautical Design Standard, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-199-4602 has 6 cross-referenced part numbers: AND10138-0403 (Airforce-Navy Aeronautical Design Standard), AMS-QQ-A-200/15 (Sae International Dba Sae International), 1MA180D06-10007 (The Boeing Company Div Defense), QQ-A-200/15 (Federal Specifications Promulgated by General Services Administration Washington DC), 10138-0403 (Transtar Metals Corp) and 1 more.
There are 3 known substitutes for 9540-01-199-4602: 9540-01-029-7087, 9540-01-086-1811, 9540-01-168-9305. Verify interchangeability with system specifications before substitution.
Key specifications for AND10138-0403: Fillet Radius Where Top Left Flange Joins Web Flange/leg: 0.094 INCHES NOMINAL IN; Overall Height: 0.500 INCHES NOMINAL IN; Fabrication Method: EXTRUDED; Web Flange Thickness: 0.050 INCHES NOMINAL IN. 23 total characteristics are documented in the Federal Logistics Information System.