Part Details | STRUCTURAL ANGLE
9540-00-251-2651 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: 3887, 24183, 14044, ASTM B221, 101635, 1M132, BAC5825, 11617, QQA2003, QQ-A-200/3, FS101051515, FS10105-1515, T2761, 15932, HA32, 2171, 2-171, LS1463, A954, A1806, 121, P3887A, AMSQQA2003, AMS-QQ-A-200/3, 60160, 60-160, PA10517, 9540-00-251-2651, 00-251-2651, 9540002512651, 002512651
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-251-2651 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-00-251-2651
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 3887 | 77783 | ALCOA/REYNOLDS METALS COMPANY |
| 24183 | 01634 | ALUMINUM CO OF AMERICA |
| 14044 | 01634 | ALUMINUM CO OF AMERICA |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| 101635 | 70898 | BEECHCRAFT CORPORATIONDBA TEXTRON AVIATION |
| 1M132 | 76301 | BOEING COMPANY, THEDBA BOEING |
| BAC5825 | 82918 | BOEING COMPANY, THEDBA BOEING |
| 11617 | 99267 | BOHN ALUMINUM AND BRASS CODIV OF GULF AND WESTERN MFG CO |
| QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| FS10105-1515 | 89446 | HILLER AIRCRAFT CORPORATION |
| T2761 | 03462 | HOWMET CORPWHITEHALL CASTING DIV |
| 15932 | 27610 | INTERNATIONAL LIGHT METALS CORPSUB OF MARTIN MARIETTA CORP |
| HA32 | 10383 | KAISER ALUMINUM AND CHEMICAL CORPTRENTWOOD WORKS-MARKETING DEPT |
| 2-171 | 38597 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| LS1463 | 98897 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN AERONAUTICS |
| A954 | 91054 | NORANDAL USA INCSALES OFFICE |
| A1806 | 91054 | NORANDAL USA INCSALES OFFICE |
| 121 | 01484 | REYNOLDS METALS CO |
| P3887A | 01484 | REYNOLDS METALS CO |
| AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| 60-160 | 29321 | TRANSTAR METALS CORP |
| PA10517 | 06012 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-00-251-2651
| 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 | 0.750 INCHES NOMINAL |
| OVERALL WIDTH | 1.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.093 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 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 | 0.093 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | UPPER RADIUS |
| SECOND TIP RADIUS | 0.093 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 0.190 POUNDS PER LINEAR FOOT |