Part Details | STRUCTURAL ANGLE
9540-00-145-5730 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: 8881, 137073, 137073, QQA2003, QQA200-3, AMSQQA2003, AMS-QQA200-3, 9540-00-145-5730, 00-145-5730, 9540001455730, 001455730
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | JAN 01, 1963 | 00-145-5730 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-00-145-5730
Part Number | Cage Code | Manufacturer |
---|---|---|
8881 | 01634 | ALUMINUM CO OF AMERICA |
137073 | 88277 | BOEING COMPANY, THEDBA BOEING |
137073 | 18355 | BOEING COMPANY, THEDBA BOEING |
QQA200-3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
AMS-QQA200-3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-145-5730
Characteristic | Specifications |
---|---|
MATERIAL | ALUMINUM ALLOY |
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | T-4 SOLUTION HEAT TREATED AND NATURAL AGED |
LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 0.500 INCHES NOMINAL |
OVERALL WIDTH | 0.625 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.125 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 | 0.150 POUNDS PER LINEAR FOOT |
NONDEFINITIVE SPEC/STD DATA | T4 TEMPER |