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National Stock Number: 9540-00-145-8404
Federal Supply Class: 9540
National Item Identification Number: 001458404
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:
2-1340 | 38597 | LOCKHEED MARTIN CORPORATION | AMS-QQ-A-200/11 | 0U583 | SAE INTERNATIONAL | AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | AMS10133-1601 | 0U583 | SAE INTERNATIONAL | AMS10133-1601 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | AMS4154 | 0U583 | SAE INTERNATIONAL | AND10133-1601 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | ASTM B221 | 81346 | AMERICAN SOCIETY FOR TESTING AND MATERIALS | QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
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Techincal Specification:
BASE FLANGE THICKNESS | 0.094 INCHES NOMINAL | BASIC SHAPE STYLE | ANGLE | FABRICATION METHOD | EXTRUDED | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.250 INCHES NOMINAL | FIRST TIP RADIUS | 0.094 INCHES NOMINAL | FIRST TIP STYLE | RIGHT QUARTER RADIUS | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED OR T-6511 SOLUTION HEAT TREATED | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | LEFT SIDE FLANGE THICKNESS | 0.094 INCHES NOMINAL | OVERALL HEIGHT | 1.750 INCHES NOMINAL | OVERALL WIDTH | 1.750 INCHES NOMINAL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-Q-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE | MATERIAL | ALUMINUM ALLOY 7075 | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T6 TEMPER OR T6511 TEMPER | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | SECOND TIP RADIUS | 0.094 INCHES NOMINAL | SECOND TIP STYLE | UPPER RADIUS | WEIGHT PER UNIT MEASURE | 0.400 POUNDS PER LINEAR FOOT |
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