The Angle,structural, cataloged under National Stock Number 9540-01-233-0627, 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 National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use. Government technical data includes 18 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 10 commercial cross-references from 8 manufacturers, enabling identification through both NSN and commercial part number lookups. 10 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-01-233-0627 |
| Primary Part Number | NAS341-15-7075-0 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use |
| Status | ACTIVE |
| Heat Treatment | O-ANNEALED |
| Left Side Flange Thickness | 0.250 INCHES NOMINAL IN |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Second Tip Style | UPPER RADIUS |
| Material | ALUMINUM ALLOY 7075 |
| First Tip Radius | 0.250 INCHES NOMINAL IN |
| Base Flange Thickness | 0.250 INCHES NOMINAL IN |
| Basic Shape Style | ANGLE |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Second Tip Radius | 0.250 INCHES NOMINAL IN |
| Nondefinitive Spec/std Data | O TEMPER |
| Specification/standard Data | 76301-1MA100 MANUFACTURERS STANDARD |
| Material Document and Classification | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE |
| First Tip Style | RIGHT QUARTER RADIUS |
| Fillet Radius Where Left Flange Joins Base Flange | 0.250 INCHES NOMINAL IN |
| Fabrication Method | EXTRUDED |
| Weight Per Unit Measure | 0.959 POUNDS PER LINEAR FOOT LBS |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
| Part Number | Manufacturer |
|---|---|
| PA3323 | Transtar Metals Corp (USA) |
| K10-199 | Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company (USA) |
| 60-3292 | Transtar Metals Corp (USA) |
| NAS341-15-7075-0 PRIMARY | National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use (USA) |
| QQ-A-200/11 | Federal Specifications Promulgated by General Services Administration Washington DC (USA) |
| 1MA100D01-10103 | The Boeing Company Div Defense (USA) |
| AMS-QQ-A-200/11 | Sae International Dba Sae International (USA) |
| NAS341-15 | National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use (USA) |
| 18525 | Alcoa/reynolds Metals Company (USA) |
| AMS-QQ-A-200/11 | Society of Automotive Engineers Inc (USA) |
NSN 9540-01-233-0627 is a Angle,structural, manufactured by National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-01-233-0627 has 10 cross-referenced part numbers: PA3323 (Transtar Metals Corp), K10-199 (Lockheed Martin Corporation Div Lockheed Martin Aeronautics Company), 60-3292 (Transtar Metals Corp), NAS341-15-7075-0 (National Aerospace Standards Committee Aerospace Industries Association of America Inc Not for Rfq or Solicitation Use), QQ-A-200/11 (Federal Specifications Promulgated by General Services Administration Washington DC) and 5 more.
There are 10 known substitutes for 9540-01-233-0627: 9540-00-505-6481, 6145-00-954-4564, 9540-01-030-2706 and 7 more. Verify interchangeability with system specifications before substitution.
Key specifications for NAS341-15-7075-0: Heat Treatment: O-ANNEALED; Left Side Flange Thickness: 0.250 INCHES NOMINAL IN; Length: 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT; Second Tip Style: UPPER RADIUS. 20 total characteristics are documented in the Federal Logistics Information System.