Part Details | STRUCTURAL BEAM
9540-00-027-5677 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: LS7580, 9540-00-027-5677, 00-027-5677, 9540000275677, 000275677
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-027-5677 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
Z SHAPE
SQUARE END
SQUARE END
SQUARE END
SQUARE END
Cross Reference | NSN 9540-00-027-5677
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| LS7580 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
Technical Data | NSN 9540-00-027-5677
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| FABRICATION METHOD | EXTRUDED |
| LENGTH | 0.089 FEET NOMINAL |
| BASIC SHAPE STYLE | Z SHAPE |
| OVERALL HEIGHT | 0.408 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE THICKNESS | 0.156 INCHES NOMINAL |
| RIGHT SIDE BOTTOM FLANGE THICKNESS | 0.090 INCHES NOMINAL |
| FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.250 INCHES NOMINAL |
| WEB FLANGE THICKNESS | 0.055 INCHES NOMINAL |
| TOP FLANGE WIDTH | 1.000 INCHES NOMINAL |
| BOTTOM FLANGE WIDTH | 1.055 INCHES NOMINAL |
| LEFT TOP INSIDE ANGLE | 81.0 DEGREES NOMINAL |
| RIGHT BOTTOM INSIDE ANGLE | 98.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| WEIGHT PER UNIT MEASURE | 0.350 POUNDS PER LINEAR FOOT |