NSN 9540-00-540-5913
Part Details | STRUCTURAL ANGLE
9540-00-540-5913 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: 69200, ASTM B221, QQA20011, QQ-A-200/11, AMSQQA20011, AMS-QQ-A-200/11, CVP1307, 9540-00-540-5913, 00-540-5913, 9540005405913, 005405913
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | JAN 01, 1963 | 00-540-5913 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE W/ INNER AND OUTER CORNER RADII
SQUARE W/ INNER AND OUTER CORNER RADII
Cross Reference | NSN 9540-00-540-5913
Part Number | Cage Code | Manufacturer |
---|---|---|
69200 | 01634 | ALUMINUM CO OF AMERICA |
ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
CVP1307 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 9540-00-540-5913
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 1.000 INCHES NOMINAL |
OVERALL WIDTH | 1.200 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.078 INCHES NOMINAL |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.120 INCHES NOMINAL |
OUTER RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.031 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.078 INCHES NOMINAL |
LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII |
FIRST TIP INNER RADIUS | 0.031 INCHES NOMINAL |
FIRST TIP OUTER RADIUS | 0.031 INCHES NOMINAL |
SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
WEIGHT PER UNIT MEASURE | 0.200 POUNDS PER LINEAR FOOT |