|
|
National Stock Number: 9540-00-251-2580
Federal Supply Class: 9540
National Item Identification Number: 002512580
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.
|
Manufacturer Information:
13167-1 | 27610 | INTERNATIONAL LIGHT METALS CORP SUB OF MARTIN MARIETTA CORP | 14161-3 | 27610 | INTERNATIONAL LIGHT METALS CORP SUB OF MARTIN MARIETTA CORP | 2163 | 01484 | REYNOLDS METALS CO | DIE734U | 01634 | ALUMINUM CO OF AMERICA | CVC1985 | 80378 | TRIUMPH AEROSTRUCTURES, LLC | BAC1503-8895 | 82918 | THE BOEING COMPANY | QQA200-3 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC | LS3320 | 98897 | LOCKHEED MARTIN CORP |
|
Techincal Specification:
BASE FLANGE THICKNESS | 0.187 INCHES NOMINAL | BASIC SHAPE STYLE | ANGLE | FABRICATION METHOD | EXTRUDED | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.250 INCHES NOMINAL | FIRST TIP RADIUS | 0.125 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 | 0.187 INCHES NOMINAL | LENGTH | 10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/3 FED SPEC 1ST MATERIAL RESPONSE | MATERIAL | ALUMINUM ALLOY 2024 | NONDEFINITIVE SPEC/STD DATA | T4 TEMPER | OVERALL HEIGHT | 2.000 INCHES NOMINAL | OVERALL WIDTH | 2.500 INCHES NOMINAL | SECOND TIP RADIUS | 0.125 INCHES NOMINAL | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | SECOND TIP STYLE | UPPER RADIUS | WEIGHT PER UNIT MEASURE | 0.990 POUNDS PER LINEAR FOOT |
|