NSN 9540-00-595-6457
Part Details | STRUCTURAL ANGLE
9540-00-595-6457 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: 8285, 10058, 5436, ASTM B221, 1M33, QQA20011, QQ-A-200/11, AMSQQA20011, AMS-QQ-A-200/11, SAE AMSSTD184, SAE AMS-STD-184, SAE AMSQQA200A, SAE AMS-QQ-A-200A, SAE AMSQQA20011, SAE AMS-QQ-A-200/11, 6011142, 60-11142, PA5455, CVC1954, 9540-00-595-6457, 00-595-6457, 9540005956457, 005956457
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-595-6457 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-00-595-6457
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 8285 | 77783 | ALCOA/REYNOLDS METALS COMPANY |
| 10058 | 77783 | ALCOA/REYNOLDS METALS COMPANY |
| 5436 | 01634 | ALUMINUM CO OF AMERICA |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| 1M33 | 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 |
| SAE AMS-STD-184 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| SAE AMS-QQ-A-200A | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| SAE AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 60-11142 | 29321 | TRANSTAR METALS CORP |
| PA5455 | 06012 | TRANSTAR METALS CORP |
| CVC1954 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 9540-00-595-6457
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-6 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 | 1.500 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.070 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.150 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.100 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | SQUARE END |
| SECOND TIP RADIUS | 0.150 INCHES NOMINAL |
| SECOND TIP DIAMETER | 0.300 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.320 POUNDS PER LINEAR FOOT |