NSN 9540-00-517-0376

Part Details | STRUCTURAL ANGLE

9540-00-517-0376 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: AND101351401, AND10135-1401, ASTM B221, S1332462, S1332462, QQA20011, QQ-A-200/11, AMS101351401, AMS10135-1401, AMSQQA20011, AMS-QQ-A-200/11, 9540-00-517-0376, 00-517-0376, 9540005170376, 005170376

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95JAN 01, 196300-517-037637017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

SQUARE END

SQUARE END

Cross Reference | NSN 9540-00-517-0376
Part Number Cage Code Manufacturer
AND10135-140199237AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD
ASTM B22181346AMERICAN SOCIETY FOR TESTING ANDMATERIALS
S133246288277BOEING COMPANY, THEDBA BOEING
S133246218355BOEING COMPANY, THEDBA BOEING
QQ-A-200/1181348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
AMS10135-140181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
Technical Data | NSN 9540-00-517-0376
Characteristic Specifications
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-6 SOLUTION HEAT TREATED
LENGTH10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT0.875 INCHES NOMINAL
OVERALL WIDTH1.500 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.078 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.117 INCHES NOMINAL
BASE FLANGE THICKNESS0.078 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE SQUARE END
SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
SECOND TIP STYLE SQUARE END
SECOND TIP RADIUS0.117 INCHES NOMINAL
SECOND TIP DIAMETER0.234 INCHES NOMINAL
WEIGHT PER UNIT MEASURE0.250 POUNDS PER LINEAR FOOT