NSN 9540-00-148-4308

Part Details | STRUCTURAL ANGLE

9540-00-148-4308 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: AND101330702, AND10133-0702, ASTM B221, 14188213600, 1418821-3600, 1418821, QQA20011, QQ-A-200/11, AMS101330702, AMS10133-0702, AMSQQA20011, AMS-QQ-A-200/11, 9540-00-148-4308, 00-148-4308, 9540001484308, 001484308

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
95JAN 01, 196300-148-430837017 ( ANGLE, STRUCTURAL )
REFERENCE DRAWINGS & PICTURES

ANGLE

RIGHT QUARTER RADIUS

UPPER RADIUS

RIGHT QUARTER RADIUS

UPPER RADIUS

Cross Reference | NSN 9540-00-148-4308
Part Number Cage Code Manufacturer
AND10133-070299237AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD
ASTM B22181346AMERICAN SOCIETY FOR TESTING ANDMATERIALS
1418821-360088277BOEING COMPANY, THEDBA BOEING
141882188277BOEING COMPANY, THEDBA BOEING
QQ-A-200/1181348FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES
AMS10133-070281343SOCIETY OF AUTOMOTIVE ENGINEERS INC
AMS-QQ-A-200/1181343SOCIETY OF AUTOMOTIVE ENGINEERS INC
Technical Data | NSN 9540-00-148-4308
Characteristic Specifications
FABRICATION METHOD EXTRUDED
HEAT TREATMENT T-6 SOLUTION HEAT TREATED
BASIC SHAPE STYLE ANGLE
OVERALL HEIGHT0.875 INCHES NOMINAL
OVERALL WIDTH0.875 INCHES NOMINAL
LEFT SIDE FLANGE THICKNESS0.094 INCHES NOMINAL
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE0.094 INCHES NOMINAL
BASE FLANGE THICKNESS0.094 INCHES NOMINAL
LEFT INSIDE ANGLE90.0 DEGREES NOMINAL
FIRST TIP STYLE RIGHT QUARTER RADIUS
FIRST TIP RADIUS0.094 INCHES NOMINAL
SECOND TIP RELATIONSHIP TO FIRST TIP NOT IDENTICAL
SECOND TIP STYLE UPPER RADIUS
SECOND TIP RADIUS0.094 INCHES NOMINAL
WEIGHT PER UNIT MEASURE0.190 POUNDS PER LINEAR FOOT