NSN 9540-01-616-7168
Part Details | STRUCTURAL BEAM
9540-01-616-7168 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: S1482282T, 9540-01-616-7168, 01-616-7168, 9540016167168, 016167168
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | FEB 25, 2013 | 01-616-7168 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
T SHAPE
Cross Reference | NSN 9540-01-616-7168
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| S1482282T | 88277 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 9540-01-616-7168
| 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 | 1.250 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE THICKNESS | 0.094 INCHES NOMINAL |
| FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL |
| TOP FLANGE WIDTH | 2.000 INCHES NOMINAL |
| SPECIAL FEATURES | TEMPER T3511 |
| END ITEM IDENTIFICATION | C-17A AIRCRAFT |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | BEAM, STRUCTURAL |