NSN 9540-01-459-4675
Part Details | STRUCTURAL ANGLE
9540-01-459-4675 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: 1MA100D0110403, 1MA100D01-10403, QQA20011, QQ-A-200/11, AMSQQA20011, AMS-QQ-A-200/11, 6024077, 60-24077, 9540-01-459-4675, 01-459-4675, 9540014594675, 014594675
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | OCT 02, 1998 | 01-459-4675 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE

SQUARE END

SQUARE END

Cross Reference | NSN 9540-01-459-4675
Part Number | Cage Code | Manufacturer |
---|---|---|
1MA100D01-10403 | 76301 | BOEING COMPANY, THEDBA BOEING |
QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
60-24077 | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-01-459-4675
Characteristic | Specifications |
---|---|
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | O-ANNEALED |
LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 3.500 INCHES NOMINAL |
OVERALL WIDTH | 3.500 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.265 INCHES NOMINAL |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.156 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.265 INCHES NOMINAL |
LEFT INSIDE ANGLE | 80.0 DEGREES NOMINAL |
FIRST TIP STYLE | SQUARE END |
SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
WEIGHT PER UNIT MEASURE | 2.135 POUNDS PER LINEAR FOOT |
END ITEM IDENTIFICATION | F-15I ACFT |