Part Details | STRUCTURAL ANGLE
9540-00-145-7557 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: 10996, 11623, ASTM B221, 101639, S109, QQA2003, QQ-A-200/3, AMSQQA2003, AMS-QQ-A-200/3, BAC1503450, BAC1503-450, 6011572, 60-11572, PA5520, 9540-00-145-7557, 00-145-7557, 9540001457557, 001457557
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 95 | JAN 01, 1963 | 00-145-7557 | 37017 ( ANGLE, STRUCTURAL ) |
REFERENCE DRAWINGS & PICTURES
ANGLE
SQUARE END
SQUARE END
Cross Reference | NSN 9540-00-145-7557
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 10996 | 77783 | ALCOA/REYNOLDS METALS COMPANY |
| 11623 | 01634 | ALUMINUM CO OF AMERICA |
| ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING ANDMATERIALS |
| 101639 | 70898 | BEECHCRAFT CORPORATIONDBA TEXTRON AVIATION |
| S109 | 71379 | CESSNA AIRCRAFT COMPANYDBA TEXTRON AVIATION |
| QQ-A-200/3 | 81348 | FEDERAL SPECIFICATIONSPROMULGATED BY GENERAL SERVICES |
| AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| BAC1503-450 | 81205 | THE BOEING COMPANYDBA BOEING |
| 60-11572 | 29321 | TRANSTAR METALS CORP |
| PA5520 | 06012 | TRANSTAR METALS CORP |
Technical Data | NSN 9540-00-145-7557
| 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 | 0.500 INCHES NOMINAL |
| OVERALL WIDTH | 0.500 INCHES NOMINAL |
| LEFT SIDE FLANGE THICKNESS | 0.050 INCHES NOMINAL |
| FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.050 INCHES NOMINAL |
| BASE FLANGE THICKNESS | 0.050 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 | 0.058 POUNDS PER LINEAR FOOT |