Part Details | STRUCTURAL ANGLE
9540-00-119-9030 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: 7346, 734-6, 1M263, QQA2003, QQA200-3, AMSQQA2003, AMS-QQA200-3, BAC15034363, BAC1503-4363, 9540-00-119-9030, 00-119-9030, 9540001199030, 001199030
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | JAN 01, 1963 | 00-119-9030 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-00-119-9030
Part Number | Cage Code | Manufacturer |
---|---|---|
734-6 | 01634 | ALUMINUM CO OF AMERICA |
1M263 | 76301 | BOEING COMPANY, THEDBA BOEING |
QQA200-3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
AMS-QQA200-3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
BAC1503-4363 | 81205 | THE BOEING COMPANYDBA BOEING |
Technical Data | NSN 9540-00-119-9030
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 | 1.250 INCHES NOMINAL |
OVERALL WIDTH | 2.500 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.188 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
FIRST TIP STYLE | RIGHT QUARTER RADIUS |
FIRST TIP RADIUS | 0.094 INCHES NOMINAL |
SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
SECOND TIP STYLE | UPPER RADIUS |
SECOND TIP RADIUS | 0.094 INCHES NOMINAL |
WEIGHT PER UNIT MEASURE | 0.548 POUNDS PER LINEAR FOOT |
NONDEFINITIVE SPEC/STD DATA | T-4 TEMPER |