NSN 9540-01-354-5859
Part Details | STRUCTURAL ANGLE
9540-01-354-5859 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: 1E118, 1E-118, QQA2003, QQ-A-200/3, AMSQQA2003, AMS-QQ-A-200/3, 60105782024T81, 60-10578/2024-T81, 9540-01-354-5859, 01-354-5859, 9540013545859, 013545859
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
95 | MAR 01, 1992 | 01-354-5859 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-01-354-5859
Part Number | Cage Code | Manufacturer |
---|---|---|
1E-118 | 43999 | BOEING COMPANY, THEDBA BOEING |
QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
60-10578/2024-T81 | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-01-354-5859
Characteristic | Specifications |
---|---|
MATERIAL | ALUMINUM ALLOY 2024 |
MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 3 FED SPEC 1ST MATERIAL RESPONSE |
FABRICATION METHOD | EXTRUDED |
HEAT TREATMENT | T-81 SOLUTION HEAT TREATED |
LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
BASIC SHAPE STYLE | ANGLE |
OVERALL HEIGHT | 1.000 INCHES NOMINAL |
OVERALL WIDTH | 1.000 INCHES NOMINAL |
LEFT SIDE FLANGE THICKNESS | 0.093 INCHES NOMINAL |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.093 INCHES NOMINAL |
BASE FLANGE THICKNESS | 0.093 INCHES NOMINAL |
LEFT INSIDE ANGLE | 75.0 DEGREES NOMINAL |
FIRST TIP STYLE | RIGHT QUARTER RADIUS |
FIRST TIP RADIUS | 0.078 INCHES NOMINAL |
SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
SECOND TIP STYLE | UPPER RADIUS |
SECOND TIP RADIUS | 0.046 INCHES NOMINAL |
WEIGHT PER UNIT MEASURE | 0.214 POUNDS PER LINEAR FOOT |
NONDEFINITIVE SPEC/STD DATA | T81 TEMPER |