NSN 9540-01-616-5487
Part Details | STRUCTURAL BEAM
9540-01-616-5487 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: S2210381T, 9540-01-616-5487, 01-616-5487, 9540016165487, 016165487
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | FEB 19, 2013 | 01-616-5487 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
T SHAPE
Cross Reference | NSN 9540-01-616-5487
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| S2210381T | 88277 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 9540-01-616-5487
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-430, ALLOY 2024 FED SPEC 1ST MATERIAL RESPONSE |
| BASIC SHAPE STYLE | T SHAPE |
| OVERALL HEIGHT | 2.438 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE THICKNESS | 0.188 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE THICKNESS | 0.188 INCHES NOMINAL |
| LEG THICKNESS | 0.250 INCHES NOMINAL |
| TOP FLANGE WIDTH | 2.000 INCHES NOMINAL |
| SPECIAL FEATURES | TEMPER T3511 |
| END ITEM IDENTIFICATION | C-17A GLOBEMASTERIII |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BEAM, STRUCTURAL |