NSN 9540-00-188-6267
Part Details | STRUCTURAL BEAM
9540-00-188-6267 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: 3094, BAC150513900, BAC1505-13900, QQA2003, QQA200-3, LS3216, AMSQQA2003, AMS-QQA200-3, 9540-00-188-6267, 00-188-6267, 9540001886267, 001886267
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-188-6267 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
T SHAPE
SQUARE END
SQUARE END
SQUARE END
SQUARE END
Cross Reference | NSN 9540-00-188-6267
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3094 | 01634 | ALUMINUM CO OF AMERICA |
| BAC1505-13900 | 82918 | BOEING COMPANY, THEDBA BOEING |
| QQA200-3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| LS3216 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| AMS-QQA200-3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-188-6267
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY |
| FABRICATION METHOD | EXTRUDED |
| LENGTH | 0.125 FEET NOMINAL |
| BASIC SHAPE STYLE | T SHAPE |
| OVERALL HEIGHT | 1.500 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE THICKNESS | 0.050 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE THICKNESS | 0.050 INCHES NOMINAL |
| LEG THICKNESS | 0.050 INCHES NOMINAL |
| LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.625 INCHES NOMINAL |
| RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 0.625 INCHES NOMINAL |
| FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.094 INCHES NOMINAL |
| FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.094 INCHES NOMINAL |
| TOP FLANGE WIDTH | 1.250 INCHES NOMINAL |
| LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
| WEIGHT PER UNIT MEASURE | 0.169 POUNDS PER LINEAR FOOT |