NSN 9540-00-231-2912

Part Details | STRUCTURAL BEAM

9540-00-231-2912 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.

Alternate Parts: DIE22899, BAC150526360, BAC1505-26360, 1M558, QQA2003, QQ-A-200/3, E711111, E711111, 14784, AMSQQA2003, AMS-QQ-A-200/3, E711111, 604493, 60-4493, 60309, 60-309, 9540-00-231-2912, 00-231-2912, 9540002312912, 002312912

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95JAN 01, 196300-231-291237018 ( BEAM, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

T SHAPE

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Cross Reference | NSN 9540-00-231-2912
Part Number Cage Code Manufacturer
DIE2289901634ALUMINUM CO OF AMERICA
BAC1505-2636082918BOEING COMPANY, THEDBA BOEING
1M55876301BOEING COMPANY, THEDBA BOEING
QQ-A-200/381348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
E7111110WLU1GENERAL DYNAMICS CORPCONVAIR DIV
E71111114170HUGHES MISSILE SYSTEMS COSAN DIEGO
1478427610INTERNATIONAL LIGHT METALS CORPSUB OF MARTIN MARIETTA CORP
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
E7111117B709TRACOR FLIGHT SYSTEMS INCSUB OF TRACOR INC
60-449329321TRANSTAR METALS CORP
60-30929321TRANSTAR METALS CORP
Technical Data | NSN 9540-00-231-2912
Characteristic Specifications
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-3511 SOLUTION HEAT TREATED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE T SHAPE
OVERALL HEIGHT1.000 INCHES NOMINAL
LEFT SIDE TOP FLANGE THICKNESS0.050 INCHES NOMINAL
RIGHT SIDE TOP FLANGE THICKNESS0.050 INCHES NOMINAL
LEG THICKNESS0.050 INCHES NOMINAL
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES0.937 INCHES NOMINAL
RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES0.937 INCHES NOMINAL
FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG0.094 INCHES NOMINAL
FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG0.094 INCHES NOMINAL
TOP FLANGE WIDTH1.875 INCHES NOMINAL
LEFT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
RIGHT TOP INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE SQUARE END
SECOND TIP RELATIONSHIP TO FIRST TIP IDENTICAL
THIRD TIP RELATIONSHIP TO PRECEDING TIPS IDENTICAL W/FIRST TIP
WEIGHT PER UNIT MEASURE0.170 POUNDS PER LINEAR FOOT
NONDEFINITIVE SPEC/STD DATA2024 ALLOY AND T3511 TEMPER