NSN 9540-01-233-4811
Part Details | STRUCTURAL ANGLE
9540-01-233-4811 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: 75A1500652004, 75A150065-2004, 9540-01-233-4811, 01-233-4811, 9540012334811, 012334811
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | MAY 30, 1986 | 01-233-4811 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-233-4811
Part Number | Cage Code | Manufacturer |
---|---|---|
75A150065-2004 | 76301 | BOEING COMPANY, THEDBA BOEING |
Technical Data | NSN 9540-01-233-4811
Characteristic | Specifications |
---|---|
MATERIAL | ALUMINUM ALLOY |
FABRICATION METHOD | EXTRUDED |
LENGTH | 0.604 FEET MINIMUM AND 0.605 FEET MAXIMUM |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 0.750 INCHES MINIMUM AND 0.860 INCHES MAXIMUM |
OVERALL WIDTH | 1.900 INCHES MINIMUM AND 1.960 INCHES MAXIMUM |
LEFT SIDE FLANGE THICKNESS | 0.040 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.030 INCHES MINIMUM AND 0.050 INCHES MAXIMUM |
LEFT INSIDE ANGLE | 86.0 DEGREES NOMINAL |
FIRST TIP STYLE | SQUARE END |
SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
USAGE DESIGN | AIRCRAFT |