NSN 9540-01-049-0767
Part Details | STRUCTURAL BEAM
9540-01-049-0767 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: 1M57242, QQA20013, QQ-A-200/13, AMSQQA20013, AMS-QQ-A-200/13, PA22100, 9540-01-049-0767, 01-049-0767, 9540010490767, 010490767
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | OCT 10, 1977 | 01-049-0767 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 9540-01-049-0767
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1M57242 | 76301 | BOEING COMPANY, THEDBA BOEING |
| QQ-A-200/13 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS-QQ-A-200/13 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| PA22100 | 06012 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-01-049-0767
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7178 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 13 FED SPEC 1ST MATERIAL RESPONSE |
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| WEIGHT PER UNIT MEASURE | 0.604 POUNDS PER LINEAR FOOT |
| NONDEFINITIVE SPEC/STD DATA | T6511 TEMPER |