The Angle,structural, cataloged under National Stock Number 9540-00-117-4810, 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 Textron Aviation Inc. Government technical data includes 16 verified specifications, sourced from the Federal Logistics Information System (FLIS). This item has 4 commercial cross-references from 4 manufacturers, enabling identification through both NSN and commercial part number lookups. 8 verified substitutes exist in the FLIS interchangeability database. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 9540-00-117-4810 |
| Primary Part Number | S76 |
| Item Name | Angle,structural |
| FSC / FSG | 9540 / 95 — No Item Name Available |
| Manufacturer | Textron Aviation Inc |
| Status | ACTIVE |
| Fillet Radius Where Left Flange Joins Base Flange | 0.156 INCHES NOMINAL IN |
| Second Tip Relationship to First Tip | NOT IDENTICAL |
| Material | ALUMINUM ALLOY 2024 |
| Second Tip Style | UPPER RADIUS |
| First Tip Radius | 0.078 INCHES NOMINAL IN |
| Weight Per Unit Measure | 0.438 POUNDS PER LINEAR FOOT LBS |
| Basic Shape Style | ANGLE |
| Left Inside Angle | 90.0 DEGREES NOMINAL |
| Length | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM FT |
| Base Flange Thickness | 0.156 INCHES NOMINAL IN |
| Heat Treatment | T-4 SOLUTION HEAT TREATED |
| Second Tip Radius | 0.078 INCHES NOMINAL IN |
| Material Document and Classification | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE |
| Left Side Flange Thickness | 0.156 INCHES NOMINAL IN |
| First Tip Style | RIGHT QUARTER RADIUS |
| Nondefinitive Spec/std Data | T4 TEMPER |
| Acquisition Status | ACTIVE |
| HAZMAT | No |
NSN 9540-00-117-4810 is a Angle,structural, manufactured by Textron Aviation Inc, classified under FSC 9540 (No Item Name Available). Status: active.
NSN 9540-00-117-4810 has 4 cross-referenced part numbers: S76 (Textron Aviation Inc), QQA200-3 (Federal Specifications Promulgated by General Services Administration Washington DC), 734GG (Aluminum Co of America), S76 (Cessna Aircraft Company Dba Textron Aviation).
There are 8 known substitutes for 9540-00-117-4810: 5826-00-071-4629, 3455-00-250-0778, 9540-00-251-2569 and 5 more. Verify interchangeability with system specifications before substitution.
Key specifications for S76: Fillet Radius Where Left Flange Joins Base Flange: 0.156 INCHES NOMINAL IN; Second Tip Relationship to First Tip: NOT IDENTICAL; Material: ALUMINUM ALLOY 2024; Second Tip Style: UPPER RADIUS. 18 total characteristics are documented in the Federal Logistics Information System.