NSN 9540-00-188-6276
Part Details | STRUCTURAL BEAM
9540-00-188-6276 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: DIE13891, ASTM B221, QQA2003, QQ-A-200/3, E711219, E711219, 5940, AMSQQA2003, AMS-QQ-A-200/3, BAC150528902, BAC1505-28902, E711219, CVC2134, 9540-00-188-6276, 00-188-6276, 9540001886276, 001886276
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | JAN 01, 1963 | 00-188-6276 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
T SHAPE
SQUARE END
SQUARE END
SQUARE END
SQUARE END
Cross Reference | NSN 9540-00-188-6276
Part Number | Cage Code | Manufacturer |
---|---|---|
DIE13891 | 01634 | ALUMINUM CO OF AMERICA |
ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
E711219 | 0WLU1 | GENERAL DYNAMICS CORPCONVAIR DIV |
E711219 | 14170 | HUGHES MISSILE SYSTEMS COSAN DIEGO |
5940 | 01484 | REYNOLDS METALS CO |
AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
BAC1505-28902 | 81205 | THE BOEING COMPANYDBA BOEING |
E711219 | 7B709 | TRACOR FLIGHT SYSTEMS INCSUB OF TRACOR INC |
CVC2134 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 9540-00-188-6276
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
LENGTH | 10.000 FEET MINIMUM AND 20.000 FEET MAXIMUM |
BASIC SHAPE STYLE | T SHAPE |
OVERALL HEIGHT | 1.000 INCHES NOMINAL |
LEFT SIDE TOP FLANGE THICKNESS | 0.090 INCHES NOMINAL |
RIGHT SIDE TOP FLANGE THICKNESS | 0.090 INCHES NOMINAL |
LEG THICKNESS | 0.090 INCHES NOMINAL |
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL |
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 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 |
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 | 0.320 POUNDS PER LINEAR FOOT |