NSN 9540-01-232-5769
Part Details | STRUCTURAL ANGLE
9540-01-232-5769 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: 1MA100D0310277, 1MA100D03-10277, QQA20011, QQ-A-200/11, AMSQQA20011, AMS-QQ-A-200/11, 605245, 60-5245, 9540-01-232-5769, 01-232-5769, 9540012325769, 012325769
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | MAY 16, 1986 | 01-232-5769 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-01-232-5769
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1MA100D03-10277 | 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 |
| 60-5245 | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-01-232-5769
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-6511 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.750 INCHES NOMINAL |
| OVERALL WIDTH | 1.950 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.080 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.080 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 | 0.352 POUNDS PER LINEAR FOOT |
| SPECIFICATION/STANDARD DATA | 76301-1A100 MANUFACTURERS STANDARD |
| NONDEFINITIVE SPEC/STD DATA | T6511 TEMPER |