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National Stock Number:
9540-01-445-5937
Federal Supply Class:
9540
National Item Identification Number:
014455937
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:
| 207-4-408 | 80378 | TRIUMPH AEROSTRUCTURES, LLC | | CVC10012-189GA | 80378 | TRIUMPH AEROSTRUCTURES, LLC |
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Techincal Specification:
| BASIC SHAPE STYLE | T SHAPE | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL | | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.125 INCHES NOMINAL | | FIRST TIP STYLE | SQUARE END | | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.170 INCHES NOMINAL | | LEFT SIDE TOP FLANGE THICKNESS | 0.713 INCHES NOMINAL | | LEFT TOP INSIDE ANGLE | 88.0 DEGREES NOMINAL | | LEG THICKNESS | 0.200 INCHES NOMINAL | | LENGTH | 12.000 FEET NOMINAL | | OVERALL HEIGHT | 2.210 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | 207-4-408, COMP 6AL-4V MFR REF SINGLE MATERIAL RESPONSE | | MATERIAL | TITANIUM ALLOY UNS R56400 | | NONDEFINITIVE SPEC/STD DATA | 6AL-4V COMPOSITION | | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.380 INCHES NOMINAL | | RIGHT SIDE TOP FLANGE THICKNESS | 0.713 INCHES NOMINAL | | RIGHT TOP INSIDE ANGLE | 92.0 DEGREES NOMINAL | | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL | | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP | | TOP FLANGE WIDTH | 4.550 INCHES NOMINAL |
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