NSN 9540-00-596-3016
Part Details | STRUCTURAL ANGLE
9540-00-596-3016 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: 23299, ASTM B221, 1E241, QQA267, QQ-A-267, QQA2003, QQ-A-200/3, AMSQQA2003, AMS-QQ-A-200/3, CVC2071, 9540-00-596-3016, 00-596-3016, 9540005963016, 005963016
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | JAN 01, 1963 | 00-596-3016 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-00-596-3016
Part Number | Cage Code | Manufacturer |
---|---|---|
23299 | 01634 | ALUMINUM CO OF AMERICA |
ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
1E241 | 43999 | BOEING COMPANY, THEDBA BOEING |
QQ-A-267 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
CVC2071 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 9540-00-596-3016
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 0.875 INCHES NOMINAL |
OVERALL WIDTH | 0.875 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.062 INCHES NOMINAL |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.047 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.062 INCHES NOMINAL |
LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
FIRST TIP STYLE | SQUARE END |
SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
WEIGHT PER UNIT MEASURE | 0.130 POUNDS PER LINEAR FOOT |