NSN 9540-00-251-2568
Part Details | STRUCTURAL ANGLE
9540-00-251-2568 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: DIE78Y, ASTM B221, 1M127, BAC15034162, BAC1503-4162, QQA2003, QQ-A-200/3, LS3257, 2382, AMSQQA2003, AMS-QQ-A-200/3, CVC1950, 9540-00-251-2568, 00-251-2568, 9540002512568, 002512568
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-251-2568 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-00-251-2568
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| DIE78Y | 01634 | ALUMINUM CO OF AMERICA |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| 1M127 | 76301 | BOEING COMPANY, THEDBA BOEING |
| BAC1503-4162 | 82918 | BOEING COMPANY, THEDBA BOEING |
| QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| LS3257 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| 2382 | 01484 | REYNOLDS METALS CO |
| AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| CVC1950 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 9540-00-251-2568
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 1.250 INCHES NOMINAL |
| OVERALL WIDTH | 1.250 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 | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.047 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | UPPER RADIUS |
| SECOND TIP RADIUS | 0.047 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.270 POUNDS PER LINEAR FOOT |