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National Stock Number: 9540-00-140-4975
Federal Supply Class: 9540
National Item Identification Number: 001404975
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:
AMS-QQ-A-200/11 | 0U583 | SAE INTERNATIONAL | AMS-QQ-A-200/11 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | AMS4154 | 0U583 | SAE INTERNATIONAL | AND10133-1404 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | LS10133-1404-5 | 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 | 0.188 INCHES NOMINAL | BASIC SHAPE STYLE | ANGLE | FABRICATION METHOD | EXTRUDED | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.188 INCHES NOMINAL | FIRST TIP RADIUS | 0.188 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 | 0.188 INCHES NOMINAL | LENGTH | 21.667 FEET NOMINAL | OVERALL HEIGHT | 1.500 INCHES NOMINAL | OVERALL WIDTH | 1.500 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 T6511 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 | 13.680 POUNDS PER PIECE |
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