Part Details | STRUCTURAL ANGLE
9540-00-145-5803 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: 13633, 1159929, 1159929, QQA2003, QQ-A-200/3, 12746, S8969, 60208, 60-208, 9540-00-145-5803, 00-145-5803, 9540001455803, 001455803
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-145-5803 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-00-145-5803
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 13633 | 01634 | ALUMINUM CO OF AMERICA |
| 1159929 | 88277 | BOEING COMPANY, THEDBA BOEING |
| 1159929 | 18355 | BOEING COMPANY, THEDBA BOEING |
| QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| 12746 | 27610 | INTERNATIONAL LIGHT METALS CORPSUB OF MARTIN MARIETTA CORP |
| S8969 | 26512 | NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS |
| 60-208 | 29321 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-00-145-5803
| Characteristic | Specifications |
|---|---|
| MATERIAL | ALUMINUM ALLOY 2024 |
| MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200 TO 3 FED SPEC 1ST MATERIAL RESPONSE |
| FABRICATION METHOD | EXTRUDED |
| HEAT TREATMENT | T-4 SOLUTION HEAT TREATED |
| LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| BASIC SHAPE STYLE | ANGLE |
| OVERALL HEIGHT | 2.500 INCHES NOMINAL |
| OVERALL WIDTH | 4.000 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.125 INCHES NOMINAL |
| LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
| FIRST TIP STYLE | SQUARE END |
| SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
| WEIGHT PER UNIT MEASURE | 0.960 POUNDS PER LINEAR FOOT |
| NONDEFINITIVE SPEC/STD DATA | T4 TEMPER |