9540-01-077-0095 ANGLE,STRUCTURAL Index 1650-01-077-0097 SERVOCYLINDER

National Stock Number:
9540-01-077-0096

Federal Supply Class:
9540

National Item Identification Number:
010770096

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:
65201-06025-00678286SIKORSKY AIRCRAFT CORPORATION
65201-06025-006QQA200-1178286SIKORSKY AIRCRAFT CORPORATION


Techincal Specification:
BASIC SHAPE STYLET SHAPE
FABRICATION METHODDIE CAST
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG0.188 INCHES NOMINAL
FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG0.188 INCHES NOMINAL
FIRST TIP STYLESQUARE END
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES0.950 INCHES NOMINAL
LEFT SIDE TOP FLANGE THICKNESS0.100 INCHES NOMINAL
LEFT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
LEG THICKNESS0.100 INCHES NOMINAL
LEG TIP THICKNESS0.040 INCHES NOMINAL
LENGTH0.198 FEET NOMINAL
OVERALL HEIGHT2.350 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-200/11 FED SPEC 1ST MATERIAL RESPONSE
MATERIALALUMINUM ALLOY 7075
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES0.950 INCHES NOMINAL
RIGHT SIDE TOP FLANGE THICKNESS0.100 INCHES NOMINAL
RIGHT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL
TOP FLANGE WIDTH1.900 INCHES NOMINAL


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