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National Stock Number: 9540-00-140-2396
Federal Supply Class: 9540
National Item Identification Number: 001402396
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:
1MA100D03-10164 | 76301 | THE BOEING COMPANY | AMS-QQ-A-200/11 | 0U583 | SAE INTERNATIONAL | AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | AMS4154 | 0U583 | SAE INTERNATIONAL | AND10133-2401 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | AND10133-2401/AMS4154-T6511 | 14153 | DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER PHILADELPHIA | AND10133-2401/QQ-A-200/11-T6511 | 14153 | DEFENSE LOGISTICS AGENCY DBA DEFENSE SUPPLY CENTER PHILADELPHIA | ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | LS10133-2401-5 | 98897 | LOCKHEED MARTIN CORP | QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
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Techincal Specification:
BASE FLANGE THICKNESS | 0.125 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-6511 SOLUTION HEAT TREATED | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | LEFT SIDE FLANGE THICKNESS | 0.125 INCHES NOMINAL | LENGTH | 12.000 FEET NOMINAL | OVERALL HEIGHT | 2.500 INCHES NOMINAL | OVERALL WIDTH | 2.500 INCHES NOMINAL | MATERIAL | ALUMINUM ALLOY 7075 | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6511 TEMPER | SECOND TIP RADIUS | 0.125 INCHES NOMINAL | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | SECOND TIP STYLE | UPPER RADIUS | WEIGHT PER UNIT MEASURE | 0.740 POUNDS PER LINEAR FOOT |
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