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National Stock Number:
9540-00-078-6091
Federal Supply Class:
9540
National Item Identification Number:
000786091
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-200/8 | 0U583 | SAE INTERNATIONAL | | AMS-QQ-A-200/8 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | | AND10134-3005 | 99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN STANDARD | | QQ-A-200/8 | 81348 | FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC | | SAE-AMS-QQ-A-200/8 | 0U583 | SAE INTERNATIONAL |
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Techincal Specification:
| BASIC SHAPE STYLE | ANGLE | | BASE FLANGE THICKNESS | 0.250 INCHES NOMINAL | | FABRICATION METHOD | EXTRUDED | | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.250 INCHES NOMINAL | | FIRST TIP RADIUS | 0.250 INCHES NOMINAL | | FIRST TIP STYLE | RIGHT QUARTER RADIUS | | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED | | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL | | LEFT SIDE FLANGE THICKNESS | 0.250 INCHES NOMINAL | | LENGTH | 10.000 FEET NOMINAL | | OVERALL HEIGHT | 2.500 INCHES NOMINAL | | OVERALL WIDTH | 3.000 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | AMS-QQ-A-200/8 FED SPEC SINGLE MATERIAL RESPONSE | | MATERIAL | ALUMINUM ALLOY 6061 | | NONDEFINITIVE SPEC/STD DATA | 6061 ALLOY AND T6 TEMPER | | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL | | SECOND TIP RADIUS | 0.250 INCHES NOMINAL | | SECOND TIP STYLE | UPPER RADIUS | | WEIGHT PER UNIT MEASURE | 1.560 POUNDS PER LINEAR FOOT |
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