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National Stock Number: 9540-00-145-5710
Federal Supply Class: 9540
National Item Identification Number: 001455710
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:
34724 | 01634 | ALUMINUM CO OF AMERICA | AMS-QQ-A-200/2 | 0U583 | SAE INTERNATIONAL | AMS-QQ-A-200/2 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | AND10134-2408 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | QQ-A-200/2 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
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Techincal Specification:
BASE FLANGE THICKNESS | 0.188 INCHES NOMINAL | BASIC SHAPE STYLE | ANGLE | FABRICATION METHOD | EXTRUDED | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.250 INCHES NOMINAL | FIRST TIP RADIUS | 0.188 INCHES NOMINAL | FIRST TIP STYLE | RIGHT QUARTER RADIUS | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED | LEFT SIDE FLANGE THICKNESS | 0.188 INCHES NOMINAL | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | OVERALL HEIGHT | 2.000 INCHES NOMINAL | OVERALL WIDTH | 2.500 INCHES NOMINAL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/2 FED SPEC SINGLE MATERIAL RESPONSE | MATERIAL | ALUMINUM ALLOY 2014 | NONDEFINITIVE SPEC/STD DATA | 2014 ALLOY AND T6 TEMPER | SECOND TIP RADIUS | 0.188 INCHES NOMINAL | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | SECOND TIP STYLE | UPPER RADIUS | WEIGHT PER UNIT MEASURE | 0.970 POUNDS PER LINEAR FOOT |
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