NSN 9540-01-494-7775

Part Details | STRUCTURAL BEAM

9540-01-494-7775 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: LS0430762, LS043-0762, AMSQQA2003, AMS-QQ-A-200/3, 608169, 60-8169, 9540-01-494-7775, 01-494-7775, 9540014947775, 014947775

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95FEB 22, 200201-494-777537018 ( BEAM, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

T SHAPE

BEAM,STRUCTURAL | 9540-01-494-7775, 014947775
Cross Reference | NSN 9540-01-494-7775
Part Number Cage Code Manufacturer
LS043-076243999BOEING COMPANY, THEDBA BOEING
AMS-QQ-A-200/381343SOCIETY OF AUTOMOTIVE ENGINEERS INC
60-816929321TRANSTAR METALS CORP
Technical Data | NSN 9540-01-494-7775
Characteristic Specifications
FABRICATION METHOD EXTRUDED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE T SHAPE
OVERALL HEIGHT1.500 INCHES NOMINAL
LEFT SIDE TOP FLANGE THICKNESS0.080 INCHES NOMINAL
RIGHT SIDE TOP FLANGE THICKNESS0.080 INCHES NOMINAL
LEG THICKNESS0.080 INCHES NOMINAL
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES2.312 INCHES NOMINAL
TOP FLANGE WIDTH3.750 INCHES NOMINAL
RIGHT TOP INSIDE ANGLE86.0 DEGREES NOMINAL
END ITEM IDENTIFICATIONB1-B AIRCRAFT