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National Stock Number:
9540-01-445-8317
Federal Supply Class:
9540
National Item Identification Number:
014458317
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 | | CVC10001-302CA | 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 | 0.150 INCHES NOMINAL | | BASIC SHAPE STYLE | ANGLE | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL | | FIRST TIP OUTER RADIUS | 0.032 INCHES NOMINAL | | FIRST TIP INNER RADIUS | 0.032 INCHES NOMINAL | | FIRST TIP STYLE | SQUARE W/ INNER AND OUTER CORNER RADII | | HEAT TREATMENT | ANNEALED | | LEFT INSIDE ANGLE | 83.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.150 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 ANNEALED CONDITION | | OVERALL HEIGHT | 1.800 INCHES NOMINAL | | OVERALL WIDTH | 1.850 INCHES NOMINAL | | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
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