NSN 9540-01-264-8337
Part Details | STRUCTURAL BEAM
9540-01-264-8337 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: 1MA160D0310277, 1MA160D03-10277, 9540-01-264-8337, 01-264-8337, 9540012648337, 012648337
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | OCT 06, 1987 | 01-264-8337 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
T SHAPE
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Cross Reference | NSN 9540-01-264-8337
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1MA160D03-10277 | 76301 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 9540-01-264-8337
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 7075 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 11 FED SPEC 1ST MATERIAL RESPONSE |
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | O-ANNEALED |
| BASIC SHAPE STYLE | T SHAPE |
| OVERALL HEIGHT | 2.120 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE THICKNESS | 0.063 INCHES NOMINAL |
| LEG THICKNESS | 0.063 INCHES NOMINAL |
| TOP FLANGE WIDTH | 2.170 INCHES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |