Part Details | STRUCTURAL ANGLE
9540-00-403-5155 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: 237665, 197325, ASTM B221, QQA20011, QQ-A-200/11, AMSQQA20011, AMS-QQ-A-200/11, 604740, 60-4740, CVC1000223, CVC10002-23, 9540-00-403-5155, 00-403-5155, 9540004035155, 004035155
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JUN 26, 1970 | 00-403-5155 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-00-403-5155
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 237665 | 01634 | ALUMINUM CO OF AMERICA |
| 197325 | 01634 | ALUMINUM CO OF AMERICA |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 60-4740 | 29321 | TRANSTAR METALS CORP |
| CVC10002-23 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 9540-00-403-5155
| 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 | 0.760 INCHES NOMINAL |
| OVERALL WIDTH | 0.900 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.060 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.090 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.060 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 82.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| WEIGHT PER UNIT MEASURE | 0.120 POUNDS PER LINEAR FOOT |