6830-01-441-0088 HELIUM Index 1377-01-441-0090 CORD ASSEMBLY,DETONATING

National Stock Number:
9540-01-441-0089

Federal Supply Class:
9540

National Item Identification Number:
014410089

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:
CVC10012-220GA80378TRIUMPH AEROSTRUCTURES, LLC


Techincal Specification:
BASIC SHAPE STYLET SHAPE
FABRICATION METHODEXTRUDED
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG0.250 INCHES NOMINAL
FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG0.250 INCHES NOMINAL
FIRST TIP STYLESQUARE END
HEAT TREATMENTANNEALED
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES1.390 INCHES NOMINAL
LEFT SIDE TOP FLANGE THICKNESS0.150 INCHES NOMINAL
LEFT TOP INSIDE ANGLE55.0 DEGREES NOMINAL
LEG THICKNESS0.150 INCHES NOMINAL
LENGTH12.000 FEET NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONMIL-T-81556, COMP AB-1 MIL SPEC SINGLE MATERIAL RESPONSE
MATERIALTITANIUM ALLOY
NONDEFINITIVE SPEC/STD DATAAB-1 COMPOSITION AND ANNEALED CONDITION
OVERALL HEIGHT3.630 INCHES NOMINAL
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES2.250 INCHES NOMINAL
RIGHT SIDE TOP FLANGE THICKNESS0.150 INCHES NOMINAL
RIGHT TOP INSIDE ANGLE125.0 DEGREES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIPIDENTICAL
THIRD TIP RELATIONSHIP TO PRECEDING TIPSIDENTICAL W/FIRST TIP
TOP FLANGE WIDTH3.640 INCHES NOMINAL


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