NSN 9540-01-193-2604

Part Details | STRUCTURAL ANGLE

9540-01-193-2604 A structural shape fabricated from a ferrous or nonferrous material and resembling the letter L in cross-sectional form. The edges may have a bulb, be rounded, and the inside corner may have a fillet.

Alternate Parts: AND101342008, AND10134-2008, ASTM B221, 1MA100D0610123, 1MA100D06-10123, QQA20015, QQ-A-200/15, 101342008, 10134-2008, 9540-01-193-2604, 01-193-2604, 9540011932604, 011932604

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95OCT 31, 198401-193-260437017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

RIGHT QUARTER RADIUS

UPPER RADIUS

RIGHT QUARTER RADIUS

UPPER RADIUS

Cross Reference | NSN 9540-01-193-2604
Part Number Cage Code Manufacturer
AND10134-200899237AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD
ASTM B22181346AMERICAN SOCIETY FOR TESTING ANDMATERIALS
1MA100D06-1012376301BOEING COMPANY, THEDBA BOEING
QQ-A-200/1581348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
10134-200829321TRANSTAR METALS CORP
Technical Data | NSN 9540-01-193-2604
Characteristic Specifications
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-76511 SOLUTION HEAT TREATED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT1.500 INCHES NOMINAL
OVERALL WIDTH2.000 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.188 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.188 INCHES NOMINAL
BASE FLANGE THICKNESS0.188 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE RIGHT QUARTER RADIUS
FIRST TIP RADIUS0.188 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
SECOND TIP STYLE UPPER RADIUS
SECOND TIP RADIUS0.188 INCHES NOMINAL
WEIGHT PER UNIT MEASURE0.737 POUNDS PER LINEAR FOOT