NSN 9540-01-447-5591
Part Details | STRUCTURAL BEAM
9540-01-447-5591 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: BAC151011467075T6511, BAC1510-1146-7075-T6511, BAC15101146, BAC1510-1146, 9540-01-447-5591, 01-447-5591, 9540014475591, 014475591
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | AUG 08, 1997 | 01-447-5591 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9540-01-447-5591
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| BAC1510-1146-7075-T6511 | 81205 | THE BOEING COMPANYDBA BOEING |
| BAC1510-1146 | 81205 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 9540-01-447-5591
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 11 FED SPEC 1ST MATERIAL RESPONSE |
| SPECIAL FEATURES | USED ON THE CHINOOK HELICOPTER |