2530-01-449-1746 ARM,CONTROL,VEHICULAR SUSPENSION Index 5920-01-449-1748 FUSE,CARTRIDGE

National Stock Number:
9540-01-449-1747

Federal Supply Class:
9540

National Item Identification Number:
014491747

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:
CVC10012-1005MP80378TRIUMPH AEROSTRUCTURES, LLC


Techincal Specification:
FIRST TIP OUTER RADIUS0.062 INCHES NOMINAL
TOP FLANGE WIDTH5.200 INCHES NOMINAL
OVERALL HEIGHT2.700 INCHES NOMINAL
RIGHT SIDE TOP FLANGE THICKNESS1.190 INCHES NOMINAL
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG0.300 INCHES NOMINAL
NONDEFINITIVE SPEC/STD DATA6AL-2SN-4ZR-2MO COMPOSITION AND ANNEALED CONDITION
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES1.770 INCHES NOMINAL
THIRD TIP RELATIONSHIP TO PRECEDING TIPSIDENTICAL W/FIRST TIP
HEAT TREATMENTANNEALED
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES3.430 INCHES NOMINAL
FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG0.300 INCHES NOMINAL
RIGHT TOP INSIDE ANGLE80.0 DEGREES NOMINAL
LEFT SIDE TOP FLANGE THICKNESS1.190 INCHES NOMINAL
MATERIALTITANIUM ALLOY, MIL-T-81556
BASIC SHAPE STYLET SHAPE
FIRST TIP STYLESQUARE W/ INNER AND OUTER CORNER RADII
FABRICATION METHODEXTRUDED
LEFT TOP INSIDE ANGLE100.0 DEGREES NOMINAL
LEG THICKNESS0.600 INCHES NOMINAL
FIRST TIP INNER RADIUS0.062 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL


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