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National Stock Number: 9540-00-251-1798
Federal Supply Class: 9540
National Item Identification Number: 002511798
Description: ANGLE,STRUCTURAL
Detail: 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.
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Manufacturer Information:
16766 | 27610 | INTERNATIONAL LIGHT METALS CORP SUB OF MARTIN MARIETTA CORP | 1M138 | 76301 | THE BOEING COMPANY | AMS-QQ-A-200/3 | 0U583 | SAE INTERNATIONAL | 60-647 | 29321 | TRANSTAR METALS CORP | 3996 | 77783 | ALCOA/REYNOLDS METALS COMPANY | AMS-QQ-A-200/3 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | DIE10468 | 01634 | ALUMINUM CO OF AMERICA | PA3235 | 06012 | TRANSTAR METALS CORP | CVC1963 | 80378 | TRIUMPH AEROSTRUCTURES, LLC | BAC1503-5824 | 81205 | THE BOEING COMPANY | ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | QQA-A-200/3 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
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Techincal Specification:
BASE FLANGE THICKNESS | 0.156 INCHES NOMINAL | BASIC SHAPE STYLE | ANGLE | FABRICATION METHOD | EXTRUDED | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.156 INCHES NOMINAL | FIRST TIP RADIUS | 0.078 INCHES NOMINAL | FIRST TIP STYLE | RIGHT QUARTER RADIUS | HEAT TREATMENT | T-4 SOLUTION HEAT TREATED | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | LEFT SIDE FLANGE THICKNESS | 0.156 INCHES NOMINAL | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/3 FED SPEC SINGLE MATERIAL RESPONSE | MATERIAL | ALUMINUM ALLOY 2024 | NONDEFINITIVE SPEC/STD DATA | 2024 ALLOY AND T4 TEMPER | OVERALL HEIGHT | 1.500 INCHES NOMINAL | OVERALL WIDTH | 1.500 INCHES NOMINAL | SECOND TIP RADIUS | 0.078 INCHES NOMINAL | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | SECOND TIP STYLE | UPPER RADIUS | WEIGHT PER UNIT MEASURE | 0.540 POUNDS PER LINEAR FOOT |
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