The Beam,structural, cataloged under National Stock Number 9540-01-029-9062, 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 The Boeing Company Div Defense. Government technical data includes 21 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 9 commercial cross-references from 7 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 | 9540-01-029-9062 |
| Primary Part Number | 1M5164 |
| Item Name | Beam,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | The Boeing Company Div Defense |
| Status | ACTIVE |
| Second Tip Relationship to First Tip | IDENTICAL |
| Right Side Top Flange Distance to Center of Both Flanges | 1.200 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.324 POUNDS PER LINEAR FOOT LBS |
| Material | ALUMINUM ALLOY 7075 |
| First Tip Style | SQUARE END |
| Left Side Top Flange Thickness | 0.064 INCHES NOMINAL IN |
| Left Side Top Flange Distance to Center of Both Flanges | 1.200 INCHES NOMINAL IN |
| Basic Shape Style | T SHAPE |
| Right Side Top Flange Thickness | 0.064 INCHES NOMINAL IN |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| Nondefinitive Spec/std Data | TO TEMPER |
| Top Flange Width | 2.400 INCHES NOMINAL IN |
| Right Top Inside Angle | 90.0 DEGREES NOMINAL |
| Leg Thickness | 0.064 INCHES NOMINAL IN |
| Left Top Inside Angle | 90.0 DEGREES NOMINAL |
| Fabrication Method | EXTRUDED |
| Fillet Radius Where Top Left Flange Joins Web Flange/leg | 0.130 INCHES NOMINAL IN |
| Heat Treatment | O-ANNEALED |
| Third Tip Relationship to Preceding Tips | IDENTICAL W/FIRST TIP |
| Fillet Radius Where Top Right Flange Joins Web Flange/leg | 0.130 INCHES NOMINAL IN |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| 1M5164 | The Boeing Company Div Defense (USA) |
| MS14372E071 | Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M |
| 60-4254 | Transtar Metals Corp (USA) |
| PA6211 | Transtar Metals Corp (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
| 61128 | Aluminum Co of America (USA) |
| 1MA160D03-10218 | The Boeing Company Div Defense (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
NSN 9540-01-029-9062 is a Beam,structural, manufactured by The Boeing Company Div Defense, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-029-9062 has 9 cross-referenced part numbers: 1M5164 (The Boeing Company Div Defense), MS14372E071 (Military Standards Promulgated by Military Departments Under Authority of Defense Standardization Manual 4120 3-M), 60-4254 (Transtar Metals Corp), PA6211 (Transtar Metals Corp), AMS-QQ-A-200/11 (Society of Automotive Engineers Inc) and 4 more.
There are 12 known substitutes for 9540-01-029-9062: 5120-00-240-5609, 2910-00-384-0669, 9540-00-500-5302 and 9 more. Verify interchangeability with system specifications before substitution.
Key specifications for 1M5164: Second Tip Relationship to First Tip: IDENTICAL; Right Side Top Flange Distance to Center of Both Flanges: 1.200 INCHES NOMINAL IN; Weight Per Unit Measure: 0.324 POUNDS PER LINEAR FOOT LBS; Material: ALUMINUM ALLOY 7075. 22 total characteristics are documented in the Federal Logistics Information System.