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) |
---|---|---|---|
95 | FEB 22, 2002 | 01-494-7775 | 37018 ( BEAM, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
T SHAPE

Cross Reference | NSN 9540-01-494-7775
Part Number | Cage Code | Manufacturer |
---|---|---|
LS043-0762 | 43999 | BOEING COMPANY, THEDBA BOEING |
AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
60-8169 | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-01-494-7775
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
BASIC SHAPE STYLE | T SHAPE |
OVERALL HEIGHT | 1.500 INCHES NOMINAL |
LEFT SIDE TOP FLANGE THICKNESS | 0.080 INCHES NOMINAL |
RIGHT SIDE TOP FLANGE THICKNESS | 0.080 INCHES NOMINAL |
LEG THICKNESS | 0.080 INCHES NOMINAL |
LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 2.312 INCHES NOMINAL |
TOP FLANGE WIDTH | 3.750 INCHES NOMINAL |
RIGHT TOP INSIDE ANGLE | 86.0 DEGREES NOMINAL |
END ITEM IDENTIFICATION | B1-B AIRCRAFT |