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National Stock Number: 9540-01-459-5962
Federal Supply Class: 9540
National Item Identification Number: 014595962
Description: BEAM,STRUCTURAL
Detail: 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.
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Manufacturer Information:
1MA163B01-10022 | 76301 | THE BOEING COMPANY | 60-9855 | 29321 | TRANSTAR METALS CORP |
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Techincal Specification:
BASIC SHAPE STYLE | T SHAPE | FABRICATION METHOD | EXTRUDED | FIRST TIP STYLE | SQUARE END | FSC APPLICATION DATA | F-15I | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL | LEFT SIDE TOP FLANGE THICKNESS | 0.400 INCHES NOMINAL | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL | LEG THICKNESS | 0.400 INCHES NOMINAL | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | OVERALL HEIGHT | 1.500 INCHES NOMINAL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE | MATERIAL | ALUMINUM ALLOY 2024 | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.000 INCHES NOMINAL | RIGHT SIDE TOP FLANGE THICKNESS | 0.400 INCHES NOMINAL | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL | TOP FLANGE WIDTH | 2.000 INCHES NOMINAL |
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