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National Stock Number: 9540-01-429-3012
Federal Supply Class: 9540
National Item Identification Number: 014293012
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 | CVC10002-78CH | 80378 | TRIUMPH AEROSTRUCTURES, LLC | QQ-A-200/11 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
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Techincal Specification:
BASE FLANGE THICKNESS | 0.250 INCHES NOMINAL | BASIC SHAPE STYLE | ANGLE | FABRICATION METHOD | EXTRUDED | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL | FIRST TIP INNER RADIUS | 0.020 INCHES NOMINAL | FIRST TIP OUTER RADIUS | 0.020 INCHES NOMINAL | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII | HEAT TREATMENT | T-73511 SOLUTION HEAT TREATED | LEFT INSIDE ANGLE | 75.0 DEGREES NOMINAL | LEFT SIDE FLANGE THICKNESS | 0.100 INCHES NOMINAL | LENGTH | 12.000 FEET NOMINAL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-200/11 FED SPEC SINGLE MATERIAL RESPONSE | MATERIAL | ALUMINUM ALLOY 7075 | NONDEFINITIVE SPEC/STD DATA | 7075 ALLOY AND T73511 TEMPER | OVERALL HEIGHT | 1.500 INCHES NOMINAL | OVERALL WIDTH | 3.284 INCHES NOMINAL | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
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