Part Details | STRUCTURAL ANGLE
9540-00-118-3144 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: 15820, ASTM B221, S149, QQA2003, QQ-A-200/3, AMSQQA2003, AMS-QQ-A-200/3, 9540-00-118-3144, 00-118-3144, 9540001183144, 001183144
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | OCT 16, 1968 | 00-118-3144 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-00-118-3144
Part Number | Cage Code | Manufacturer |
---|---|---|
15820 | 01634 | ALUMINUM CO OF AMERICA |
ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
S149 | 71379 | CESSNA AIRCRAFT COMPANYDBA TEXTRON AVIATION |
QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-118-3144
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 0.750 INCHES NOMINAL |
OVERALL WIDTH | 0.750 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.075 INCHES NOMINAL |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.075 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.075 INCHES NOMINAL |
LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
FIRST TIP STYLE | RIGHT QUARTER RADIUS |
FIRST TIP RADIUS | 0.031 INCHES NOMINAL |
SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
SECOND TIP STYLE | UPPER RADIUS |
SECOND TIP RADIUS | 0.031 INCHES NOMINAL |
WEIGHT PER UNIT MEASURE | 0.130 POUNDS PER LINEAR FOOT |