NSN 9540-01-353-6235
Part Details | STRUCTURAL ANGLE
9540-01-353-6235 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: 1E523, QQA2003, QQ-A-200/3, AMSQQA2003, AMS-QQ-A-200/3, 603593, 60-3593, 9540-01-353-6235, 01-353-6235, 9540013536235, 013536235
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | FEB 13, 1992 | 01-353-6235 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-01-353-6235
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1E523 | 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 |
| 60-3593 | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-01-353-6235
| 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-3511 SOLUTION HEAT TREATED |
| LENGTH | 12.000 FEET NOMINAL |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.250 INCHES NOMINAL |
| OVERALL WIDTH | 2.500 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.094 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.062 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.062 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | UPPER RADIUS |
| SECOND TIP RADIUS | 0.062 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.275 POUNDS PER LINEAR FOOT |
| NONDEFINITIVE SPEC/STD DATA | T3511 TEMPER |