NSN 9520-01-424-4799
Part Details | STRUCTURAL BEAM
9520-01-424-4799 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: LS3908, 9520-01-424-4799, 01-424-4799, 9520014244799, 014244799
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 29, 1996 | 01-424-4799 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9520-01-424-4799
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| LS3908 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 9520-01-424-4799
| Characteristic | Specifications |
|---|---|
| LEG THICKNESS | 0.080 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.400 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.810 INCHES NOMINAL |
| SPECIAL FEATURES | MATERIAL ALUMINUM ALLOY 2024-T4; ONE SIDE OF T IS 125 DEG ANGLE |
| END ITEM IDENTIFICATION | HERCULES; LOCKHEED AERONAUTICAL SYSTEMS |