9540-01-232-6069 BEAM,STRUCTURAL Index 9905-01-232-6071 PLATE,IDENTIFICATION

National Stock Number:
9540-01-232-6070

Federal Supply Class:
9540

National Item Identification Number:
012326070

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.


Manufacturer Information:
SS1512-178286SIKORSKY AIRCRAFT CORPORATION


Techincal Specification:
BASIC SHAPE STYLEZ SHAPE
BOTTOM FLANGE WIDTH0.780 INCHES NOMINAL
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE BOTTOM RIGHT FLANGE JOINS WEB FLANGE/LEG0.094 INCHES NOMINAL
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG0.094 INCHES NOMINAL
FIRST TIP STYLESQUARE END
LEFT SIDE TOP FLANGE THICKNESS0.032 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-250/13 FED SPEC 1ST MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 7075 AND ALUMINUM ALLOY 7072
OVERALL HEIGHT1.060 INCHES NOMINAL
RIGHT SIDE BOTTOM FLANGE THICKNESS0.032 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL
TOP FLANGE WIDTH0.250 INCHES NOMINAL
WEB FLANGE THICKNESS0.032 INCHES NOMINAL


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