NSN 9540-01-239-6529
Part Details | STRUCTURAL BEAM
9540-01-239-6529 A structural shape fabricated from a ferrous or nonferrous material and resembles the following cross-sectional forms: For the letter H, both flanges of the H section are equal or longer than the width measured along the axis of the web; for the letter I, a 16 2/3 percent slope on the inside face of the ferrous type flange, either one or both of the nonferrous type flanges are shorter than the length measured along the axis of the web; for the letters T and Z, on nonferrous type, the web is usually at right angles to the flanges. Letter H section may have a maximum of 5 percent slope on the inside face of the flanges.
Alternate Parts: 6520909031101, 65209-09031-101, 9540-01-239-6529, 01-239-6529, 9540012396529, 012396529
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | SEP 01, 1986 | 01-239-6529 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
I SHAPE
Cross Reference | NSN 9540-01-239-6529
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 65209-09031-101 | 78286 | SIKORSKY AIRCRAFT CORPORATIONDBA SIKORSKY |
Technical Data | NSN 9540-01-239-6529
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 3 FED SPEC 1ST MATERIAL RESPONSE |
| FABRICATION METHOD | EXTRUDED |
| LENGTH | 7.000 FEET MINIMUM |
| BASIC SHAPE STYLE | I SHAPE |
| LEFT SIDE TOP FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| TOP FLANGE WIDTH | 0.625 INCHES NOMINAL |