Part Details | STRUCTURAL ANGLE
9540-00-288-1145 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: AND101332004, AND10133-2004, 1822, ASTM B221, 1245442, 1245442, 1047972, 1047972, CDS148, QQA2003, QQ-A-200/3, 110503062, 110-503062, 125511, 12551-1, 21327, 2-1327, AMSQQA2003T35110.250X2X10, AMS-QQ-A-200/3-T3511-0.250X2X10, AMSQQA2003, AMS-QQ-A-200/3, 9540-00-288-1145, 00-288-1145, 9540002881145, 002881145
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-288-1145 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
RIGHT QUARTER RADIUS
UPPER RADIUS
RIGHT QUARTER RADIUS
UPPER RADIUS
Cross Reference | NSN 9540-00-288-1145
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AND10133-2004 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGNSTANDARD |
| 1822 | 77783 | ALCOA/REYNOLDS METALS COMPANY |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| 1245442 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 1245442 | 18355 | BOEING COMPANY, THEDBA BOEING |
| 1047972 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 1047972 | 18355 | BOEING COMPANY, THEDBA BOEING |
| CDS148 | 81025 | CHASE AIRCRAFT CO INC |
| QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| 110-503062 | 89446 | HILLER AIRCRAFT CORPORATION |
| 12551-1 | 27610 | INTERNATIONAL LIGHT METALS CORPSUB OF MARTIN MARIETTA CORP |
| 2-1327 | 38597 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| AMS-QQ-A-200/3-T3511-0.250X2X10 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Technical Data | NSN 9540-00-288-1145
| Characteristic | Specifications |
|---|---|
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-3511 SOLUTION HEAT TREATED |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 2.000 INCHES NOMINAL |
| OVERALL WIDTH | 2.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.250 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.250 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.250 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | RIGHT QUARTER RADIUS |
| FIRST TIP RADIUS | 0.250 INCHES NOMINAL |
| SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
| SECOND TIP STYLE | UPPER RADIUS |
| SECOND TIP RADIUS | 0.250 INCHES NOMINAL |
| WEIGHT PER UNIT MEASURE | 1.110 POUNDS PER LINEAR FOOT |